23 December 2025, Volume 38 Issue 6
    

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  • GAO Peili, XIE Guoxin, LUO Jianbin
    China Surface Engineering. 2025, 38(6): 1-11. https://doi.org/10.11933/j.issn.1007-9289.20250326002
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    Novel intelligent lubricating materials and surfaces exhibit on-demand responsiveness and adaptability. The biomimetic self-regulating mechanism empowers in-service tribo-pairs with the autonomy to sense external environmental stimuli and adaptively modulate interfacial lubrication states. Such capabilities provide a groundbreaking solution for the “online sensing-decision-execution” intelligent transformation of advanced equipment in aerospace and defense sectors. Concurrently, the AI-driven intelligent inverse design of lubricating materials has revolutionized the traditional trial-and-error paradigm, enabling highly efficient and demand-responsive customization of lubrication for mechanical interfaces. This innovation provides a novel pathway for establishing a scientific framework for high-performance and high-reliability lubrication materials and surface systems capable of addressing diverse complex operational conditions. The intelligent evolution of lubricating materials and surfaces is progressively redefining the research paradigms in mechanical interface science, potentially unlocking breakthrough opportunities to advance frontier tribological theories and technologies. This paper discusses current research on self-lubricating, self-repairing, and self-diagnosing intelligent lubricating materials and surfaces, the frontier progress of AI-accelerated inverse design, and their future development trends, taking intelligent lubricating materials and surfaces and their AI paradigms as the pointcut. Currently, self-lubricating tribo-pairs that are environmentally robust and operationally adaptable use solid lubricating materials as the matrix, with liquid or solid-liquid-coupled lubricants as the dispersed phase. Effectively enhancing the interfacial lubrication performance can be achieved by releasing trace liquid lubricants to form fluid or boundary films. Two primary approaches are used for incorporating liquid lubricants into a tribo-pair matrix: porous-based self-storing and lubricating strategies and capsule-based self-storing and lubricating strategies. The development of capsule-based self-storage and lubrication techniques makes it a novel solid superlubrication method after carbon-based superlubrication and two-dimensional material superlubrication. This method enables macroscopic superlubrication at temperatures between 0 and 250 ℃. Although intelligent capsule-based self-storing and lubricating technologies can significantly reduce friction and wear on tribo-pair surfaces, material degradation and surface damage are inevitable during prolonged service. It is important to promptly repair wear and damage to improve the wear resistance and service life of tribo-pair materials. Intelligent surface healing technologies for tribo-pairs can be broadly categorized into extrinsic and intrinsic types. Extrinsic repair typically employs stimulus-responsive materials (for example, microcapsules or microvascular networks) to encapsulate active repair agents that are autonomously released upon external stimulus-induced damage, thereby facilitating physicochemical reactions for localized repair. Intrinsic repair leverages the reversible reorganization of dynamic covalent bonds (for example, Diels-Alder (DA) bonds, acylhydrazone bonds, and disulfide bonds) or non-covalent interactions (for example, hydrogen bonds, metal-ligand coordination, and host-guest interactions) to enable autonomous damage repair. Moreover, excessive wear on tribo-pair surfaces generates clearance, and its enlargement exacerbates vibration during equipment operation and reduces service life. Thus, it is imperative to endow tribo-pairs with self-diagnostic capabilities for real-time monitoring of wear locations and damage severity, enabling intelligent lifecycle management and predictive maintenance of equipment. Three approaches are the primary focus of the current intelligent self-diagnostic technologies: dye-based chromatic detection, electrical signal diagnostics, and optical signal diagnostics. The latest paradigm in the research and development of lubricating materials and surfaces, driven by AI, is the fourth paradigm after empirical, theoretical, and computational science paradigms. The primary technical approach involves employing machine-learning models to establish potential mapping relationships between the properties (such as composition and structure) of lubricant materials and surfaces and their lubrication performance. This enables prediction of the lubrication performance of new materials and surfaces. Furthermore, by integrating optimization algorithms or deep-reinforcement-learning techniques, global optimization within the high-dimensional nonlinear design space of lubricant materials and surfaces can be achieved rapidly, thereby facilitating the efficient inverse design of materials and surfaces with target attributes. This transformative research paradigm is expected to decipher the lubrication and friction reduction mechanisms at mechanical interfaces, overcome the efficiency limitations of traditional trial-and-error iterative methods, and ultimately realize demand-driven customization of lubricant materials and surface designs.
  • MENG Fanwei, YE Fuxing, YAO Yuan, SUN Kaiqi, SONG Ziqi
    China Surface Engineering. 2025, 38(6): 12-22. https://doi.org/10.11933/j.issn.1007-9289.20240904001
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    Thermal barrier coatings (TBCs) technology has been widely employed in the thermal protection of aero-engine blades. The blade surfaces are coated with ceramic materials that exhibit excellent thermophysical properties, high-temperature stability, mechanical strength, and resistance to high-temperature corrosion, thereby ensuring the longevity of aero-engines. However, the traditional 6wt.%-8wt.% Y2O3-stabilized ZrO2 (YSZ), commonly used to prepare TBCs, undergoes a phase transition with severe volume expansion, rapid sintering and severe high-temperature melt corrosion above 1 200 ℃, leading to premature coating failure. To address the increasing service temperature of high-performance aero-engine, developing the novel TBCs material is urgently required. Recent advancements in research of ‘high-entropy' alloys have inspired the application of the composition design of novel ceramic materials. The synthesis and performance evaluation of high-entropy ceramic materials have thus provided new avenues for the development of novel TBC materials. The outstanding performance of the high-entropy ceramic materials is primarily attributed to four inherent effects: ① thermodynamically high-entropy effect; ② dynamically sluggish diffusion effect; ③ severe lattice distortion; ④ cocktail effect. Relevant studies have demonstrated that these four distinctive effects associated with high-entropy materials provide a degree of flexibility in composition design and property regulation, which is not present in traditional TBCs or single-component TBCs materials. Furthermore, the comprehensive performance of high-entropy TBCs ceramics is comparatively better, as evidenced reduced thermal conductivity, a coefficient of thermal expansion (CTE) that is well-matched with the alloy substrate, and the exceptional high-temperature stability. This paper presents a summary of the current research status of high-entropy thermal barrier ceramics offering an analysis of component design and performance optimization based on the characteristics and the nature of bonding in the crystal structure. The analysis covers five key aspects: thermal conductivity, thermal expansion performance, high-temperature resistance to sintering and phase stability, mechanical properties and resistance to high-temperature CaO-MgO-Al2O3-SiO2 CMAS corrosion. Elements with large mass disorder and ionic radius disorder are used for the synthesis of high-entropy TBCs materials to form a larger degree of lattice distortion, which can expand the phonon collision chances, decreasing the phonon mean free path and reducing the thermal conductivity. Anions and cations with minor differences in electronegativity can form ionic bonds with weak bonding strengths to obtain materials with higher CTE. Similarly, the formation of ionic bonds with strong bonding strength is beneficial for improving the mechanical properties, such as hardness and fracture toughness. The ions with the large radius difference compete for the same lattice site together, forming a more severe lattice distortion, which hinders matter diffusion. It leads to the sluggish diffusion phenomenon that contributes to high temperature stability. The concept of high entropy, based on the nature of multi-component single-phase solid solutions, offers a novel approach to the composition design and property regulation of novel TBCs materials, which has attracted considerable research interest. By summarizing and analyzing the radius disorder, mass order, and bond strength, the high-entropy thermal barrier ceramics with optimized composition based on the nature of ion can exhibit enhanced thermal physical properties, CTE, mechanical properties, high-temperature resistance to sintering and phase stability, and resistance to CMAS corrosion, exhibiting the potential for further development. However, the preparation and performance of high-entropy thermal barrier ceramic materials is the research mainstream, which is not entirely applicable. Moreover, several problems need further research and to provide solutions during manufacturing, thereby promoting its development and maturity, such as element segregation and phase transition. In this study, the theoretical guidance on the composition, design, performance optimization, and regulation of high-entropy TBCs materials and an outlook on the prospective applications is offered.
  • ZHOU Xinzhao, YANG Jiajun, WANG Xiaobo, JIN Zefeng, ZHANG Liwen, CHEN Huawei
    China Surface Engineering. 2025, 38(6): 23-40. https://doi.org/10.11933/j.issn.1007-9289.20250714003
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    The development of precision medicine requires efficient, stable, and multifunctional biomechanical interfaces. The abundant micro / nanostructures and functional mechanisms found in nature provide important inspiration for interface design; however, research on biomimetic bio-machine interfaces for precision medicine still lacks in-depth and systematic reviews. This paper systematically summarizes representative biomimetic strategies in interface design, with a particular focus on the principles and applications of antifouling, adhesion enhancement, directional liquid transport, and microneedle penetration structures in interface construction. It further discusses the advantages and limitations of advanced manufacturing technologies, such as laser processing and 3D printing, for the fabrication of multiscale biomimetic structures. Typical applications in precision medicine, including antifouling electrosurgical scalpels, adhesive patches, wearable microfluidic diagnostic sensors, and drug delivery systems, have demonstrated the remarkable benefits of biomimetic structures for improving interfacial adaptability, functional integration, and clinical applicability. Finally, this study explores the crucial role of emerging technologies, such as artificial intelligence, stimuli-responsive materials, and multi-material 3D printing, in driving the advancement of biomimetic bio-machine interfaces. Despite notable progress in biomimetic design and manufacturing, this field remains in its early stages and faces multiple challenges. For instance, natural multifunctional interfaces often exhibit highly complex material compositions and hierarchical multiscale features, making high-precision and consistent biomimetic reconstruction across the macro- and microscales highly dependent on breakthroughs in advanced manufacturing. Current biomimetic approaches are largely confined to isolated structural or material mimicry, with limited progress in the integrated codesign of structures, materials, and functions. Moreover, the intelligent responsiveness and multifunctional integration of interface systems remain underdeveloped, and achieving external-field-driven control (e.g., mechanical, thermal, acoustic, optical, electrical, and chemical) of interface properties is key to advancing system intelligence. Currently, most biomimetic functional interfaces remain in the proof-of-concept stage, and their long-term durability, biocompatibility, and safety require further validation for clinical and real-world applications. Biomechanical interfaces are expected to evolve beyond static designs to dynamic and adaptive systems. By integrating stimuli-responsive materials with flexible sensing networks, such interfaces can achieve real-time environmental perception and feedback regulation, enabling closed-loop intelligent medical devices, such as adaptive neural interfaces and dynamic drug-delivery microneedle arrays. Multiscale simulations (e.g., molecular dynamics and finite element analysis) can accurately predict the mechanical, electrical, and biological behaviors at the interface. Furthermore, coupling biomimetic design with artificial intelligence, particularly machine and deep learning, promises to establish data-driven platforms for interface design, enabling an integrated workflow from natural structure extraction and material selection to manufacturing pathway planning and performance prediction, thus advancing the paradigm from experience-driven to data-driven biomimetic design. Breakthroughs in key technologies such as multimaterial cooperative printing and scalable micro / nanoscale manufacturing are critical for establishing standardized and modular fabrication systems with improved reproducibility and consistency. Simultaneously, systematic frameworks for long-term biocompatibility assessment must be developed to ensure clinical safety and stability. In summary, this study proposes two guiding strategies—dynamic biomimetic design enabled by smart materials and intelligent interface design enabled by artificial intelligence—to fill a critical gap in the literature. These perspectives provide valuable insights for the future development of biomimetic interface design and manufacturing for precision medicine.
  • FANG Xiang, MA Jing, YU Kaihuan, LI Ning, QIANG Li
    China Surface Engineering. 2025, 38(6): 41-79. https://doi.org/10.11933/j.issn.1007-9289.20241126001
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    The accelerated development of modern industry and information technology has resulted in a notable surge in demand for high-performance materials capable of functioning in extreme environments, particularly in the domains of friction and electromagnetic wave absorption. MXene-based materials have attracted considerable interest owing to their exceptional properties, including high electrical conductivity, a unique layered structure, outstanding mechanical properties, chemical stability, and abundant surface functional groups. However, a comprehensive and systematic review of recent progress in the application of MXene-based materials in tribology and electromagnetic wave absorption remains unavailable. To address this gap, an in-depth and systematic review of the structural properties, preparation methods, and performance mechanisms of MXene-based materials in these applications is presented. The fundamental structural characteristics of MXene are examined, including its two-dimensional configuration, chemical composition, and surface modifications. These attributes are considered to be critical in understanding the multifunctional performance of MXene. Furthermore, the intrinsic properties of MXene, including its exceptional electrical conductivity and mechanical flexibility, are analyzed in detail. The preparation and processing techniques of MXene and its derivatives are also explored, with a focus on the ways in which various processes, ranging from conventional wet chemical etching to advanced composite fabrication methods, are employed to tailor MXene materials for specific performance requirements. In the field of tribology, MXene-based materials have the potential to significantly reduce friction and enhance wear resistance. The preparation and processing of MXene has been the subject of considerable study, and the results have highlighted notable advantages over traditional two-dimensional materials, such as graphene and molybdenum disulfide. In particular, the achievement of lower coefficients of friction and wear rates has been demonstrated. These superior tribological properties are primarily attributed to the unique two-dimensional structure and surface chemistry of MXene. The integration of MXene into lubricants or composites has been demonstrated to enhance friction reduction and anti-wear performance, yielding coefficients of friction and wear rates that exceed those of conventional materials. Furthermore, MXene functions effectively as a cross-linking agent in polymer systems, significantly improving their tribological characteristics by reinforcing their mechanical integrity and enhancing surface interactions. In the field of electromagnetic wave absorption, MXene-based materials demonstrate exceptional wave energy attenuation capabilities, attributable to their high electrical conductivity, superior dielectric loss, and tunable surface chemistry. These properties facilitate the efficient conversion of electromagnetic energy into other forms of energy, enabling optimal absorption performance across a wide frequency range. The surface functionalization and formation of composites with materials such as polymers, magnetic nanoparticles, or carbon-based structures have further enhanced the efficiency and bandwidth of the absorption process. Furthermore, the layered structure of MXene facilitates multiple internal reflections of electromagnetic waves, thereby significantly enhancing its absorption capabilities. A comparative analysis of various composite designs and processing techniques demonstrates that MXene-based materials outperform traditional wave-absorbing materials, such as ferrite and carbonyl iron powders, particularly in lightweight and flexible applications. These advantages position MXene-based materials as a highly promising solution for modern electronic devices, stealth technology, and electromagnetic interference shielding, addressing critical demands in these advanced technological fields. Despite the remarkable properties and potential of MXene-based materials across a range of applications, a number of challenges remain. These include stability issues under extreme conditions, such as limited resistance to oxidation and thermal degradation, as well as the complexity involved in designing multifunctional composites and the high costs associated with large-scale production. To overcome these obstacles, several improvement strategies are proposed. These include surface functionalization to enhance environmental stability, the integration of MXene with other nanomaterials to augment multifunctionality, and the optimization of preparation processes to reduce production costs. The implementation of these strategies is expected to significantly broaden the practical applications of MXene-based materials, thereby rendering them more feasible for industrial and technological use. In conclusion, the present study offers a systematic review of the research progress on MXene-based materials in the fields of tribology and electromagnetic wave absorption. This includes a detailed analysis of their unique properties, underlying mechanisms, and preparation methods. The findings provide a comprehensive understanding of the current advancements while identifying critical challenges and future research directions. Given their exceptional performance characteristics and versatile potential, MXene-based materials are anticipated to play a pivotal role in addressing the demands of modern industry and advanced technologies. It is likely that their continued development will yield innovative solutions for applications in high-performance friction materials, electromagnetic interference shielding, and beyond, underscoring their importance as a transformative material platform.
  • ZHANG Yanke, GAO Chenke, YE Yumin, LIU Wenna
    China Surface Engineering. 2025, 38(6): 80-92. https://doi.org/10.11933/j.issn.1007-9289.20241007002
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    With the progress of science and technology and improvements in living standards, the demand for electronic equipment has gradually changed from rigid and bulky to flexible and lightweight. Consequently, flexible electronic devices have become increasingly popular. Flexible wearable electronic devices are the development and innovation of flexible devices and have gained wide attention in the fields of healthcare, motion tracking, and environmental monitoring owing to their advantages such as light weight, portability, high integration, and good shape preservation. However, the long-term stability of wearable devices is challenged by their complex working environments, both from the external environment and secretions of human skin (rain, sweat, food residue, etc.). Inspired by the special biological surfaces in nature, the realization of special functions of materials or devices by regulating surface wettability has become a research hotspot. Surface wettability regulation has significant advantages for optimizing the design of solid-liquid interface interactions. Because liquid droplets can form spheres and quickly roll off, superhydrophobic surfaces have versatile functionalities such as waterproofing, self-cleaning, anti-corrosion, and antibacterial properties. This provides new opportunities to improve the performance and prolong the life of wearable electronic devices. For example, its excellent waterproof function can prevent external moisture intrusion, reduce the risk of short circuit and corrosion, and extend the service life, thus ensuring the stable operation of the device in wet environments. Self-cleaning and anti-contamination properties can keep the device clean, ensure accurate signal transmission and stable performance, eliminate the hassle of frequent cleaning, and improve the user experience. In addition, the superhydrophobic surface can reduce liquid accumulation, maintain device cleanliness, and improve comfort levels, laying the foundation for the wide application of superhydrophobic surfaces in flexible wearable electronics. This study focuses on the application of superhydrophobic surfaces in flexible wearable devices. First, the working principle of a superhydrophobic surface is introduced. The key to obtaining a superhydrophobic surface is to reduce the surface energy and increase the surface roughness. The preparation methods for superhydrophobic surfaces, including electrochemical deposition, electrospinning, chemical vapor deposition, and etching, are briefly described. This is followed by the application of superhydrophobic surfaces in flexible electronic devices. First, the application of superhydrophobic coatings in sensors is introduced. When a superhydrophobic coating is applied in the microchannel modification of a sweat sensor, the sweat transfer rate is significantly increased; thus, the sensing performance is improved. Superhydrophobic surfaces can provide sensors with moisture resistance, liquid resistance, self-cleaning, and weather resistance properties, significantly improving their service life. Second, the applications of superhydrophobic coatings in energy-conversion devices (such as nanogenerators) are described. Because the working principle of friction nanogenerators is to collect the electrostatic energy generated by contact charging, the waterproofing performance of the superhydrophobic coating helps friction nanogenerators collect more energy from the flowing water. Subsequently, the application of superhydrophobic coatings to energy-storage devices that provide energy support for flexible wearable electronic devices is introduced. Superhydrophobic coatings can significantly improve the safety and stability of energy storage devices. Although superhydrophobic coatings have certain applications, their service stability still faces challenges. Finally, it is pointed out that high mechanical stability, good environmental durability, and high light transmittance are challenges for the future development of superhydrophobic surfaces for wearable devices.
  • HE Hao, FAN Qixiang, WANG Tiegang, LIU Yanmei, CAO Fengting
    China Surface Engineering. 2025, 38(6): 93-113. https://doi.org/10.11933/j.issn.1007-9289.20250127001
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    Marine biofouling poses a persistent challenge for submerged mechanical equipment, leading to accelerated corrosion, operational inefficiencies, and significant economic losses. The accumulation of microbial communities on marine surfaces not only damages equipment but also substantially increases maintenance costs, creating a critical bottleneck for sustainable marine resource development. Addressing this issue through effective antifouling solutions has become a global research priority in marine engineering. Current antifouling technologies primarily encompass mechanical removal, ultrasonic cleaning, and protective coatings, with antifouling coatings emerging as the most widely adopted solution due to their cost-effectiveness, ease of application, and superior performance. There is a wide variety of antifouling coatings, each with distinct antifouling mechanisms. However, comprehensive reviews on the antifouling performance, advantages, and disadvantages of both traditional and novel antifouling coatings remain scarce. Thus, a comprehensive review is conducted on the research advancements of both traditional and novel antifouling coatings, such as natural antifoulant coatings, biomimetic coatings, self-healing coatings, etc. Their research status, antifouling mechanisms, and remaining challenges are discussed. Traditional antifouling coatings can be categorized into matrix-insoluble and matrix-soluble types. The former operate through the gradual release of embedded biocidal compounds that deter or eliminate fouling organisms. However, these coatings exhibit significant limitations, including short service lifetimes and complex application requirements, which restrict their widespread adoption in marine applications. Self-polishing antifouling coatings (SPCs), the most currently commercially successful matrix-soluble system, dominating 90% of the global market, utilize hydrolyzable polymer side chains to enable controlled antifoulant release. However, their uneven release kinetics (initial excess followed by insufficiency) compromises long-term performance, and their dependence on toxic biocides raises environmental concerns. In contrast to these traditional coatings that rely on biocidal agents, fouling-release coatings achieve antifouling effects solely through their low surface energy, preventing fouling organisms from firmly adhering. Under water flow, fouling organisms detach easily, providing excellent antifouling performance without harming the marine environment. However, these coatings perform poorly under static conditions, and their adhesion to substrate needs improvement. Natural antifoulant coatings derive their active substances from antifouling compounds secreted by plants and animals or their synthetic analogs. They reduce marine biofouling by inhibiting adhesion processes and interfering with microbial signaling systems. Compared to traditional antifoulants, natural antifoulants are less toxic and significantly reduce environmental impact. However, challenges such as broad-spectrum efficacy and long-term durability remain unresolved. Biomimetic coatings utilize micro- and nanostructures from self-cleaning natural surfaces (via 3D printing, laser etching, or transfer techniques) to achieve efficient and eco-friendly antifouling effects, showing high application potential. However, these coatings often suffer from low mechanical strength, poor adaptability, and high production costs. Self-healing marine coatings integrate specialized repair agents that autonomously mend surface damage, overcoming key limitations of conventional systems by extending service life and maintaining antifouling efficacy. Despite their potential for significant economic and performance benefits, commercialization challenges persist, including complex fabrication, high costs, and difficulties in scaling beyond laboratory prototypes. Photocatalytic coatings rely on photocatalysts to undergo redox reactions under specific light wavelengths, decomposing seawater and dissolved oxygen to generate reactive oxygen species (ROS). These ROS penetrate cell membranes, damage microbial DNA, and cause cell rupture, achieving antifouling through microbial inactivation. These coatings are safe, efficient, non-toxic, and pollution-free. However, their performance is highly dependent on UV intensity and light energy utilization, requiring further improvements in stability. Hydrogel coatings contain high water content (typically >70%, even >90%), forming a dense and dynamic hydration layer through hydrogen bonding between polymer chains and water molecules. This layer effectively blocks fouling organism attachment. However, their poor mechanical properties and weak adhesion limit broader applications. Despite the variety of marine antifouling coatings available, single mechanism approaches generally fail to meet the complex demands of marine environments, particularly regarding long-term efficacy, broad-spectrum performance, and environmental safety. To overcome these limitations, we propose the strategic integration of multiple antifouling mechanisms within hybrid coating systems. This synergistic approach aims to combine the advantages of different technologies while mitigating their individual weaknesses, paving the way for next-generation antifouling solutions that balance performance, durability, and ecological sustainability. The findings provide valuable insights for developing advanced marine coatings.
  • PIAO Zhongyu, AN Biao, WANG Haidou, DI Yuelan, CHEN Rong, DONG Lihong
    China Surface Engineering. 2025, 38(6): 114-123. https://doi.org/10.11933/j.issn.1007-9289.20240308001
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    In recent years, with the continuous increase in the speed of spacecraft, the high-temperature environment endured by the combustion chamber of engines has become increasingly severe. To prevent structural failure caused by the harsh high-temperature conditions inside the combustion chamber, there is an urgent need for technological innovation in thermal protection for aerospace engine combustion chambers. This article focuses on the influence of micro-structures on the inner wall of regenerative cooling channels on the overall cooling capacity and heat transfer uniformity of the cooling channels. In order to achieve micro-structure modification of the narrow and long cooling channel inner wall, this study utilizes selective laser melting (SLM) additive manufacturing technology. By optimizing the SLM process parameters and acid pickling process, the study successfully fabricated high-quality, integrated, downstream-oriented rectangular micro-grooves with a minimum size of 200 μm as modified micro-structures on the inner wall of the cooling channel. To investigate the effect of the structural dimensions of the downstream-oriented rectangular micro-grooves on the heat transfer performance of regenerative cooling channels, experiments were conducted on smooth single cooling channels and single cooling channels with three different scales of micro-groove structures using a self-built circulating water tunnel experimental platform to test flow resistance and heat transfer performance. The experimental results show that when the size of the micro-groove structure is in the range of 250 to 450 μm, compared with smooth cooling channels, cooling channels containing micro-grooves exhibit a significant enhancement in heat transfer efficiency. The enhancement in heat transfer efficiency is positively correlated with the structural size of the micro-grooves, and the cooling channel with 450 μm micro-grooves demonstrates the best heat transfer capability, with an approximate 73% increase compared to smooth channels. However, along with the enhancement in heat transfer capability brought about by the presence of micro-groove structures, the flow resistance of the cooling channel also increases, albeit to a lesser extent, with a roughly 26% increase in flow resistance brought about by the 450 μm micro-grooves. To further explore the mechanism of how micro-groove structures of different sizes regulate heat transfer capability, particle image velocimetry (PIV) technology was employed to obtain surface velocity fields and vorticity fields of different scale micro-groove structures. Analysis of the velocity fields and vorticity fields reveals that the presence of micro-groove structures disrupts the flow structure of the boundary layer on the inner wall of the cooling channel, resulting in a thinning of the velocity boundary layer and intensifying the velocity gradient at the boundary, thereby enhancing the momentum and energy exchange between fluid layers at the boundary. This further confirms the regulation of flow resistance and heat transfer performance of the cooling channel by micro-groove structures. Based on the above experimental results, this study innovatively proposes the concept of arranging micro-groove structures reasonably in parallel cooling channels to increase heat transfer capability in localized areas with a small increase in flow resistance, thus preventing local overheating-induced cooling structure failure and thereby improving the overall heat transfer uniformity of regenerative cooling channels. To verify this concept, this study takes the example of parallel three cooling channels and tests the influence of micro-groove structures of different scales on the heat transfer uniformity of parallel three cooling channels. The experimental results show that through the reasonable arrangement of micro-grooves in parallel cooling channels, the heat transfer uniformity of parallel three cooling channels can be improved by approximately 34%.
  • DONG Gang, HU Jiandong, WANG Yongqiang, LI Guoming, JIANG Xiaofeng, ZHANG Qunli, YAO Jianhua
    China Surface Engineering. 2025, 38(6): 124-134. https://doi.org/10.11933/j.issn.1007-9289.20240319001
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    During their service period, the last-stage blades of steam turbines are highly susceptible to cavitation damage at the steam inlet, which significantly affects the long-term performance of these turbines. Cavitation leads to the dimensional loss of the blades, resulting in reduced efficiency and, in extreme cases, mechanical failure of the unit. Cavitation is a phenomenon in which vapor bubbles form in low-pressure regions and collapse when moving into higher-pressure areas, causing localized shock waves that erode material surfaces. The inlet region of turbine blades is particularly vulnerable due to constant exposure to fluctuating pressures and high-velocity steam flow. To combat this issue and ensure the continued operation of steam turbines, repairing damaged turbine blades is an essential maintenance task. One promising approach to address cavitation damage involves restoring blade dimensions by means of laser cladding technology, which enables the deposition of a cladding layer onto the worn areas of the blades. In this study, a cladding layer composed of 17-4PH steel, the same material used in the original turbine blades, is fabricated on damaged blade surfaces using laser cladding. 17-4PH stainless steel, a martensitic precipitation-hardening material, is chosen because of its high strength, corrosion resistance, and ability to be age-hardened, making it suitable for turbine blade repair. The deposited cladding layer is then subjected to post-heat treatment, specifically direct aging treatments, to enhance the microstructure and improve its resistance to cavitation, which is critical to ensure the longevity of the repaired blades. The direct aging treatments are conducted at three temperatures: 530, 580, and 630 ℃, in a high-temperature box furnace. These temperatures are selected to investigate their effects on the mechanical properties and microstructure of the cladding layer. For a thorough analysis of the microstructural changes induced by the aging treatments, several advanced characterization techniques are employed, including optical microscopy, X-ray diffraction, scanning electron microscopy, and electron backscatter diffraction. Each technique provides complementary insights into the grain structure, phase composition, and distribution of precipitates in the aged cladding layer. In addition, the cavitation resistance of the treated specimens is evaluated using an ultrasonic testing system, which simulates the erosive effects of cavitation on the material surface by subjecting it to high-frequency vibrations in a liquid medium. The results of this study reveal that direct aging treatment plays a critical role in relieving internal residual stresses in the cladding layer, which are introduced during the laser cladding process. Moreover, it enhances the microstructural stability by increasing the content of retained austenite and promoting the precipitation of strengthening phases. These changes improve the material's ability to withstand the aggressive erosive action of cavitation. Interestingly, mass loss due to cavitation in the cladding layer exhibits a non-linear trend in terms of aging temperature. Specifically, the cumulative mass loss initially increases as the aging temperature increases but decreases after reaching a certain point. The lowest mass loss, measured at 60.6 mg, is observed in the specimen aged at 530 ℃, representing a substantial reduction of approximately 58% as compared with the as-deposited state, where mass loss was recorded at 145.4 mg. By contrast, the specimen aged at 630 ℃ experiences relatively higher mass loss, suggesting that excessively high aging temperatures may not be beneficial for cavitation resistance. Surface roughness, another crucial indicator of cavitation resistance, is also significantly improved after aging. The optimal surface roughness of 180 µm is observed in the specimen treated at 580 ℃, indicating superior resistance to cavitation damage. These findings suggest that selecting a suitable aging temperature is critical for achieving a balance between improving the mechanical properties and cavitation resistance of the cladding layer. Therefore, applying suitable direct aging temperatures to the 17-4PH cladding layer promotes homogenization of the microstructure and enhances the material's resistance to cavitation. This provides a potent strategy for extending the life and maintaining the integrity of turbine blades, offering important engineering guidance for the repair and restoration of cavitation-damaged turbine blades.
  • WANG Weiguang, CAI Long, LEI Mingkai, LI Yupeng, LÜ Xiangping, LI Mengqi
    China Surface Engineering. 2025, 38(6): 135-151. https://doi.org/10.11933/j.issn.1007-9289.20230828001
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    The surface morphology of cylindrical thrust pad has been proven to have an important influence on the lubrication performance about the water-lubricated thrust bearing of nuclear reactor coolant pump, in order to identify the lubrication influence of different radial position and depth of circumferential trapezoidal groove on the surface of cylindrical thrust pad. Based on the surface mesh of thrust pad, the surface texture deviation is considered, the surface texture of the cylindrical surface on the sector thrust pad and its circumferential trapezoidal grooves are constructed, and the simplified Reynolds equation is solved by finite difference method. The results show that the thickness of water film decreases with the increase of the depth of the circumferential trapezoidal groove on the thrust pad surface, when the pressure of water film increases, the temperature of water film increases slightly, axial stiffness and axial damping increase significantly, the lubrication performance of the thrust pad decreases when the pressure peak on the surface of the thrust pad is separated into two pressure peaks on the inner side and the outer side. Finally, compared with the different grooves, circumferential trapezoidal grooves fixed depth, as the radial position of groove moves from inside to outside, the minimum water film thickness decreases first and then increases, and the maximum water film pressure rises, falls and rises again, shows that the M-shaped change rule, the maximum water film temperature increases first and then decreases, and the axial stiffness and axial damping increases first and then decreases,when the depth of circumferential trapezoidal groove is less than 0.1 mm, the pressure peaks are not obviously separated and still have good lubrication performance, the lubrication performance does not change greatly when the depth of circumferential trapezoidal groove is greater than 0.3 mm. The minimum water film thickness decreases first and then increases with the change of the position of the circumferential trapezoidal groove of the thrust pad from the inside to the outside, and decreases by 0.41 times with the increase of the depth of the groove. The maximum water film temperature increases first and then decreases, and increases by only 1.5% with the increase of the groove depth, and increases by 0.5% with the increase of the groove depth. The power loss of water film lubrication increases first and then decreases, and increases by 1.45 times with the increase of groove depth. The average water film shear stress increases first and then decreases, and increases by 1.96 times with the increase of groove depth. The minimum water film shear stress decreases first and then increases, and the minimum negative pressure value of -0.045 MPa appears at the position where the depth of the circumferential groove is 0.1 mm and the radial width is 0.6 times of the pad width, and the absolute value of the minimum water film shear stress is less than ambient pressure of the medium 0.1 MPa is not prone to cavitation erosion. For the crown thrust pad, except axial stiffness and damping, the lubrication performance of the annular trapezoidal groove shows a downward trend, but a reasonable setting of the annular groove can significantly increase the axial liquid film stiffness while reducing the acceptable liquid film thickness, which has a good support for the stable operation of the nuclear reactor coolant pump rotor. At the same time, pay attention to control the negative pressure area of the water outlet side, so as to suppress the influence of cavitation erosion caused by negative cavitation pressure. When the groove is preferred, the cavitation pressure can be controlled at 10% of the standard atmospheric pressure, that is, a smaller negative pressure level -0.01-0 MPa. The above conclusions provide technical support for the surface topography design, high performance manufacturing and bench test of the water-lubricated thrust pad of the extended nuclear reactor coolant pump, and have a certain reference value for the reliability design and in-service operation of the nuclear reactor coolant pump on the surface trace limit of the thrust pad, and are helpful for the research on the influence of surface scratches and textures of other topographies on lubrication.
  • YOU Ruizhi, TU Chuanjun, LUO Hong, HUANG Xia, LIU Yanli, ZENG Xiaobin, LIU Shitong
    China Surface Engineering. 2025, 38(6): 152-160. https://doi.org/10.11933/j.issn.1007-9289.20240228002
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    With the development of modern industry, the actual working conditions of mechanical seals tend to be harsh, and stricter requirements have been proposed for the mechanical strength, wear resistance, and service life of mechanical seal materials. Carbon-graphite is a type of graphite sealing material that plays an important role in mechanical sealing because of its excellent thermal shock resistance, self-lubricating performance, and corrosion resistance. However, owing to the limitations of traditional technology, numerous pores are present in the matrix of traditional carbon-graphite materials, which leads to poor airtightness and greater brittleness. Under the action of stress and wear in actual working conditions, the traditional carbon-graphite material is prone to brittle fracture, which leads to the failure of the sealing system. To address the common issue of carbon materials used for mechanical sealing, which often suffer from brittle chipping under operational conditions, fine-structured carbon graphite was used as the research object in this study. To enhance durability, a composite was produced using ultrafine carbon aggregates compounded with a coal asphalt binder. This mixture underwent multiple mixing and homogenization steps, followed by premolding, isostatic pressing, and a one-stage baking process to create carbon-graphite blocks. Green petroleum coke with a certain volatile component was used as a solid-phase densifier to adjust and control the internal porous structure of the blocks, reduce the porosity rate, shorten the sharp crack areas, and improve the strength of the carbon phase interface, thereby improving the mechanical strength and anti-wear performance of the carbon-graphite material. Using X-ray diffraction (XRD), Raman spectroscopy, scanning electron microscopy (SEM), polarized optical microscopy (POM), and other characterization methods and friction and wear performance tests, the inhibition degree of the typical defective structure of carbon-graphite by green petroleum coke was investigated, and the effect of green petroleum coke on the pore structure and porosity of carbon-graphite materials was analyzed to elucidate the effect of green petroleum coke on the densification and surface anti-wear performance of the carbon-graphite materials. The results showed that the baked blocks (10wt.% green petroleum coke), which have the two-level skeleton reinforced structure, demonstrate better densification, significantly shortening sharp crack areas and reducing porosity by 59.41%. Notably, their flexural strength reaches 99.79 MPa and compressive strength hits 273.94 MPa—an approximately 207% increase in both cases compared to the blocks without green petroleum coke addition. Moreover, the friction coefficient was reduced by 27.74% and the abrasion rate was reduced by 69.23% as a consequence of the improvement in the mechanical properties, which promoted anti-wear performance. By adjusting the skeleton structure of fine-structured carbon-graphite materials with green petroleum coke, the interfacial matching of different carbon phases formed by the main aggregate and binder is improved, and the formation of surface cracks is suppressed. First, the fine green petroleum coke particles filled the interstices of the main aggregate particles, blocking the porosity and reducing the pore size, forming an independent and unconnected pore structure that inhibited the initiation and propagation of microcracks. In addition, the green petroleum coke particles dispersed in the matrix can partially replace the binder and reduce the pores formed by the volatiles escaping from the binder pitch area during heat treatment. Meanwhile, the green petroleum coke particles distributed on the surface of the pressed powder further strengthen the bonding between different particles, reduce the distribution of defects between the carbon phase interfaces, and promote the synchronous thermal shrinkage of different carbon phases in the carbon-graphite materials. Therefore, as a consequence of the green petroleum coke, the anti-wear performance of materials under dry friction conditions is improved, providing a new strategy for the selection of mechanical seal materials.
  • WANG Linqing, WU Shanshan, YANG Jun, TIAN Zhuoying, WANG Junjun
    China Surface Engineering. 2025, 38(6): 161-170. https://doi.org/10.11933/j.issn.1007-9289.20240326006
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    Transparent hydrophobic films exhibiting superior mechanical resistance to impact abrasion, as observed in conditions such as sand impact, have garnered significant interest owing to their potential applications in domains such as solar photovoltaics, construction, and automotive industries. To achieve hydrophobic characteristics, a micro-nanostructure is typically constructed with appropriate roughness and low surface energy. However, a trade-off exists between these two factors. Although a rough surface potentially enhances hydrophobic properties, it can adversely affect mechanical robustness because micro-nano structures are typically delicate and susceptible to wear and impact damage in practical applications. Additionally, a rough surface reduces the optical transparency owing to Mie and Rayleigh scattering of visible light. Therefore, developing a material that effectively combines transparency, hydrophobicity, and impact resistance remains a challenge. High-entropy oxides (HEOs) show considerable promise in integrating these properties owing to their excellent mechanical characteristics, such as hardness and toughness, and their high thermal stability. Transparent and hydrophobic HEOs have been achieved by altering their constituent elements. Consequently, a HfCeYZr oxide (HfCeYZrO) film is proposed, meeting the required properties of hydrophobicity, transparency, and impact resistance. Cerium, a lanthanide, and its oxide are inherently hydrophobic owing to their unique electronic structures. Furthermore, the oxides of Hf, Y, and Zr, which have low electronegativities, exhibit hydrophobicity. Additionally, Hf, Ce, Y, and Zr oxides exhibit high transparency in the visible wavelength range. HfCeYZrO films were deposited on quartz glass via RF reactive magnetron sputtering in an Ar and O2 gas mixture. The effect of the oxygen flow ratio (${{f}_{{{\mathrm{O}}_{\mathrm{2}}}}}$=O2/(O2+Ar)) on the microstructure and properties of HfCeYZrO films was investigated to optimize deposition process parameters and enhance the wetting behavior, optical transmittance, and mechanical durability of the films. The surface morphology, phase structure, chemical composition, wetting behavior, and optical transmittance of the HfCeYZrO films were examined via atomic force microscopy, X-ray diffraction, X-ray photoelectron spectrometry, contact angle goniometry, and ultraviolet-visible-near infrared spectroscopy. The mechanical durability was assessed via a linear abrasion test. The findings indicated that all HfCeYZrO films exhibited a NaCl-type face-centered cubic crystal structure without any other secondary phases and/or impurities. The surface roughness, crystallite size, and chemical composition of the films were strongly influenced by ${{f}_{{{\mathrm{O}}_{\mathrm{2}}}}}$. As ${{f}_{{{\mathrm{O}}_{\mathrm{2}}}}}$ increased from 5% to 11%, surface roughness increased from 1.3 nm to 2.4 nm, crystallite size decreased from 3.0 nm to 1.8 nm. However, as ${{f}_{{{\mathrm{O}}_{\mathrm{2}}}}}$ increased to 14%, surface roughness decreased to 1.9 nm and crystallite size increased to 2.0 nm. As ${{f}_{{{\mathrm{O}}_{\mathrm{2}}}}}$ increased from 5% to 11%, the percentage content of the primary surface adsorbed components (C-C / C-H) initially increased from 64.49% to 83.01%, and subsequently decreased to 79.20% as ${{f}_{{{\mathrm{O}}_{\mathrm{2}}}}}$ is increased to 14%. These parameters determined the surface wettability and optical transmittance of the HfCeYZrO films. As ${{f}_{{{\mathrm{O}}_{\mathrm{2}}}}}$ increased from 5% to 14%, the water contact angle initially increased and then decreased, whereas the optical transmittance decreased. Specifically, the HfCeYZrO films deposited at ${{f}_{{{\mathrm{O}}_{\mathrm{2}}}}}$ of 11% exhibited high hydrophobicity, characterized by a water contact angle of 108.6°, and exhibited high transmittance exceeding 60% at a wavelength of 550 nm. These properties were attributed to the synergistic effect of surface roughness and chemical composition. Additionally, the films exhibited stable mechanical properties, with only 18.52% decrease in the optical transmittance and 3.88% decrease in the contact angle after 20 cycles of linear wear, thereby providing protection against linear mechanical abrasion. These results underscore the potential of transparent hydrophobic films exhibiting stable mechanical properties for practical applications in daily life.
  • QIN Hongling, XIAO Jinwen, TANG Wei, GU Weikun, LI Ming, SANG Xitao, WU Siqi, HE Wei, ZHAO Xinze
    China Surface Engineering. 2025, 38(6): 171-183. https://doi.org/10.11933/j.issn.1007-9289.20241230001
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    Current-carrying friction pairs are critical components in high-end applications such as motors, rail transit, and aerospace systems. These components serve dual functions: transmitting electrical energy and sustaining mechanical friction. Consequently, their reliability is essential to overall system performance. One key factor affecting their performance is current polarity, which significantly affects overheating, arcing, and surface degradation. This study investigates the causes and consequences of polarity effects through field investigations of carbon brush-collector ring systems in hydroelectric generators, supported by failure case analyses and theoretical frameworks. It was found that current polarity primarily governs the oxidation and transfer of surface films at the contact interface of current-carrying friction pairs, thereby regulating the physical and chemical properties of these films. In particular, polarity influences the growth of oxide layers and electrochemical reactions within the water film at the interface—a phenomenon broadly classified as anodic oxidation (AO). Material transfer from the anodic to the cathodic friction pair is attributed not only to arc-induced material migration but also to anodic oxidation mechanisms. For instance, in the carbon brush-steel slip ring system, the negative slip ring (acting as the anode) displayed more intense surface oxidation, forming a film primarily composed of metal oxides. Conversely, the positive slip ring (acting as the cathode) exhibited suppressed oxidation, with a surface film dominated by carbon-transfer deposits. These findings clearly demonstrate the strong influence of current polarity on surface film formation. Further analysis revealed a significant asymmetry in contact resistance under different polarities. This variation is attributed to the distinct surface film compositions and their associated conduction mechanisms. Additionally, current polarity impacts contact temperature, which in turn affects the thermal stability of the friction pair. By integrating case studies, the research systematically examines the interrelationships among contact resistance, localized temperature rise, and arc generation—placing particular emphasis on the severe damage caused by surface arcing. The results indicate that arc erosion characteristics are closely tied to current polarity. Specifically, anodic current-carrying components are more susceptible to thermal erosion, including melting and evaporation—an effect collectively referred to as “anodic evaporation”. This study provides a comprehensive analysis of the fundamental mechanisms, contributing factors, and final manifestations of polarity effects. It explores how polarity governs surface film formation, how these films affect contact resistance and temperature, and how these factors collectively affect arc probability and surface degradation. The interplay among surface films, temperature rise, and arc formation is examined in detail. Focusing on the carbon brush-steel slip ring system, the study highlights differences in wear and surface damage under opposing polarities, explaining the severe erosion of negative slip rings and abnormal wear on negative carbon brushes. Based on these findings, a mitigation strategy is proposed: reducing temperature through optimized cooling structures to interrupt the positive feedback loop between heat buildup and arc formation. Finally, the study summarizes the intrinsic mechanisms underlying polarity effects in current-carrying friction pairs, using the carbon brush-steel slip ring system as a representative case. It introduces the principle of “anodic protection” to provide both theoretical support and practical guidance for the optimal design, long-term reliability, and maintenance of such systems. Ultimately, this study aims to deepen the understanding of polarity effects on surface film formation, interface degradation, and system performance, while offering new insights for future research in this field.
  • CHEN Jun, XU Zhengyi, WANG Yanqiu, SHAO Yawei, WANG Junyi
    China Surface Engineering. 2025, 38(6): 184-198. https://doi.org/10.11933/j.issn.1007-9289.20240125002
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    Silanization is a new surface treatment technology that has been studied and applied to metal materials. However, its application to carbon steel is not ideal because of the low hydroxyl content, loose structure, and uneven chemical composition of the oxide film obtained after the acid washing, alkali washing, or natural oxidation of carbon steel, which results in poor-quality surface silane film formation. Therefore, researchers have attempted to add oxidants during the pretreatment process to oxidize the substrate and improve its surface condition; however, there has been no relevant research on the addition of oxidants to alkaline pretreatment solutions at room temperature for substrate pretreatment. This is because most oxidants have weak oxidizing properties under alkaline conditions at room temperature and cannot meet these requirements. However, sodium persulfate (Na2S2O8) as an oxidant can generate highly oxidizing free radicals under alkaline conditions and has relatively stable oxidizing properties, which can complete the oxidation treatment of steel under normal temperature alkaline conditions. In addition, most researchers have overlooked the fact that carbon steel is easily eroded by an acidic silane hydrolysis solution during the silanization process, which can damage its original surface state. Therefore, adding an appropriate amount of a corrosion inhibitor to the pre-treatment solution is an effective means by which to improve the stability of the substrate surface in an acidic silane hydrolysis solution during the silane film formation process without affecting the silane hydrolysis solution. Benzotriazole (BTA), which is an organic corrosion inhibitor, exhibits a good corrosion inhibition effect on steel materials and can provide short-term protection for the carbon steel surface in an acidic hydrolysis solution during the silane film formation process. Therefore, this study used a combination of the corrosion inhibitor BTA and oxidant Na2S2O8 in pretreatment to improve the surface state of carbon steel before silanization treatment and enhance its stability in an acidic silane hydrolysis solution. XPS, SEM, AFM, and contact angle testing were used to analyze and characterize the microstructure of the pretreated carbon steel surface and the subsequently attached silane film. Electrochemical impedance spectroscopy (EIS) and dynamic potential polarization testing were used to compare the corrosion resistances of the silane films before and after the introduction of BTA and Na2S2O8. The results show that after adding BTA to the alkaline pretreatment solution, the BTA molecules can be chemically adsorbed on the surface of the carbon steel. This not only reduces the probability of matrix pitting corrosion in an acidic hydrolysis solution and improves the integrity of the silane film layer on the carbon steel surface but also inhibits the corrosion of the corrosive medium at the interface between the silane film and matrix. When the BTA concentration is 5 g / L, the corrosion current density of silane film in the NaCl solution during the initial soaking period decreases from 1.58×10-7 A·cm-2 to 3.01×10-8 A·cm-2, and the corrosion current density after soaking for 144 h decreases from 1.01×10-6 A·cm-2 to 2.56×10-7 A·cm-2. The short-term and the long-term corrosion resistance of the silane film were significantly improved. When BTA was used in combination with Na2S2O8, the oxidation effect of Na2S2O8 on the substrate further increased the hydroxyl content on the substrate surface and reduced the erosion of the acidic silane solution on the substrate surface, thereby resulting in an improvement in the quality of the silane film on the carbon steel surface. When the concentration of Na2S2O8 is 3 g / L, the corrosion current density of the silane film during the initial immersion in NaCl solution decreases from 3.01×10-8 A·cm-2 to 2.29×10-8 A·cm-2, thereby further improving the short-term corrosion resistance of the siliconized sample. The results verify that the simultaneous introduction of oxidants and corrosion inhibitors in alkaline pretreatment solutions can increase the hydroxyl content on the surface of carbon steel and inhibit the corrosion of the acidic silane hydrolysis solution on the surface of carbon steel. Therefore, this study has referential value for improving the corrosion resistance of silane films on the surface of carbon steel through a pretreatment process.
  • REN Xiaoyong, LIU Kaixue, LI Gang, FENG Shaowei, WANG Jie, REN Yilong, CHENG Jie, GAO Xuemin
    China Surface Engineering. 2025, 38(6): 199-208. https://doi.org/10.11933/j.issn.1007-9289.20240415001
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    The surface treatment of titanium alloy fasteners is one of the main methods for preventing “sticking” and “biting” during assembly and disassembly. It is necessary to investigate the frictional and wear characteristics of titanium alloy samples after different surface treatments, reveal their wear mechanism, and improve the tribological properties of their surfaces. In addition, it is crucial to reduce the factor of friction, improve wear resistance, and design highly reliable titanium-alloy fasteners. In this study, a manual-spraying method was developed for applying aluminum and MoS2 treatments to samples after pulse-anodizing treatment (PA) to leave the surface untreated. Four surface states of TC4 titanium alloy (no treatment [LT], pulsed-anodizing treatment, pulsed-anodizing and aluminum-coating composite treatment [PA-Al], and pulsed-anodizing and molybdenum disulfide composite treatment [PA-MoS2]) were investigated, and a 10-mm-diameter TC4 titanium alloy ball was used as the grinding object. The frictional and wear characteristics of TC4 titanium alloys in different surface states were determined under 1 and 4 N loads using a UMT-3 friction- and wear-testing machine. The wear morphologies of the wear marks and wear spots on the surface of the ball were characterized using an ultradepth field microscope, a three-dimensional white-light interferometer, a focused-ion beam scanning electron microscope, and an accompanying energy dispersive spectrometer. The wear volume and wear rate were calculated to determine the differences in wear resistance, examine the wearing mechanism, and analyze the differences in wear resistance under different test loads. Under test loads of 1 and 4 N, the wear marks of the LT sample are the widest and deepest, the factor of friction fluctuates significantly with an average value of approximately 0.53, and the main element is Ti. In addition, Al, V, O, and C are observed, and the wear mechanisms are mainly plowing and adhesive wear. The wear morphology of the PA-Al sample shows discontinuous spalling, the factor of friction fluctuates slightly, and the stability value is approximately 0.58. More Al and O elements are observed on the surface of the sample, and alumina is formed on the surface, indicating high hardness and brittleness; thus, the sample is prone to brittleness. Spalling pits are formed on the surface, effective solid lubrication films rarely form on the surface of the sample, the run-together period is extended, and the coefficient of friction is high. The wear mechanisms of the PA-Al sample are spalling and abrasive wear. The wear marks on the PA-MoS2 samples are shallow and continuous, the factor of friction fluctuates slightly, the stability value is approximately 0.25, and the main elements are S and Mo, with low amounts of C, O, and Si. Relatively dense TiO2 coatings are generated on the surface of the PA sample, indicating high hardness, good antifriction, and high bonding strength with the substrate; therefore, the wear resistance of the material improves significantly. The wear mark of the PA sample is the narrowest, and the factor of friction is approximately 0.16. The wear rates under the low and high loads are 5.8×10-4 and 5.7×10-4 mm3 / (N·m), respectively, indicating that the sample exhibits the best wear resistance. Its main elements are Ti and O, with low amounts of Al, C, P, and Mo. The wear rates of the samples are ranked from high to low as follows: PA-Al>PA-MoS2>LT>PA. This demonstrates that the pulse-anodized-treated TC4 titanium alloy exhibits the best antifriction wear resistance, and the interlayer shearing force of MoS2 on the surface of the PA-MoS2 sample is small. This improves the lubrication characteristics; however, because it has a rough surface microstructure, the frictional resistance is the second best, and the wear resistance further decreases under a load of 4 N. This proves the significant advantages of PA in improving the antifriction wear resistance of TC4 titanium alloys and provides a strong technical support and experimental basis for the surface treatment of titanium alloy fasteners.
  • LI Sai, AI Xingang, CHEN Dongxu, XU Zhen, ZHOU Yanwen, LI Shengli, ZHAO Tan
    China Surface Engineering. 2025, 38(6): 209-218. https://doi.org/10.11933/j.issn.1007-9289.20240920002
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    Stainless steel has a wide range of applications in the nuclear power field due to its excellent corrosion resistance. However, in high-temperature and high-pressure water and irradiation and other specific environments in long-term service, stainless steel is prone to pitting corrosion, crevice corrosion, and other local corrosion damage and stress corrosion cracking and other problems. Hence, the service life is significantly reduced, leading to serious economic consequences and safety risks for the nuclear power plant. Therefore, investigating effective localized corrosion prevention and control technology and the corresponding mechanism is the key to addressing the problem of localized corrosion damage of stainless steel for nuclear power generation-and remains a matter of significant concern. Research on the corrosion resistance of laser-modified layer on the surface of 304 stainless steel with the addition of Y2O3, especially on its corrosion behavior in high-temperature and high-pressure water environment, and the corresponding mechanism have been rarely reported. Therefore, to improve the corrosion resistance and service life of stainless steel in the operating environment of nuclear power, laser cladding technology is used to prepare laser-modified layers with varying Y2O3 content on the surface of 304 stainless steel used for nuclear power generation. Furthermore, laser cladding is used to examine the influence of the Y2O3 additions on the microstructure of the laser-modified layer, the corrosion resistance and corrosion behavior in high-temperature and pressurized water, and to discuss the relevant corrosion failure mechanisms. The results show that moderate addition of Y2O3 (in the range of 0.5wt.%-1.0wt.%) can significantly reduce the number of defects in the laser cladding layer on the surface of 304 stainless steel, and thereby, can significantly improve its corrosion resistance. However, excessive addition of Y2O3 leads to the formation of Y2O3 clusters, which in turn slightly increases the number of defects. When the mass percentage of Y2O3 is 1.0%, the corrosion potential of the modified layer is -257 mV (vs. SCE) and the corrosion current density is 2.410×10-7 A·cm-1, which is more than 110 mV (vs. SCE) higher than that of the modified layer without the addition of Y2O3. Additionally, the current density decreases by 2 orders of magnitude. When the mass percentage of Y2O3 is 2.0%, the corrosion resistance decreases due to the stress concentration caused by the clusters of Y2O3, which increases the defects in the modified layer. Micro-area hydrochemical calculations revealed that, under conditions of 290  ℃ and 3×10-6 dissolved oxygen in high-temperature, high-pressure water, the incubation period for localized corrosion on the laser-cladded surface of 304 stainless steel with varying Y₂O₃ content is the range of approximately 22-30 h. Combined with the results of electrochemical noise monitoring, it can be observed that the laser-cladded surfaces of 304 stainless steel with varying Y₂O₃ content exhibit two main forms of corrosion failure in high-temperature, high-pressure water. When Y2O3 is not added, there are more defects in the modified layer, and in the early stage of exposure, the dissolved oxygen inside the defects is sufficient. Furthermore, the dissolved metal cation combines with the oxygen to generate metal oxides. Additionally, as exposure time increases, the dissolved oxygen within defects is gradually depleted, while oxygen from the surrounding solution struggles to diffuse inward. This results in the accumulation of excess metal cations inside the defects. To maintain electrical neutrality, anions from the surrounding solution migrate into the defect under electrostatic forces and combine with metal cations to form metal complexes. However, these complexes are unstable in high-temperature, high-pressure environments and easily hydrolyze, releasing H⁺ ions. This lowers the local pH within the defect, leading to acidification and intensified corrosion. Over time, this autocatalytic process results in severe pitting corrosion. When excess Y2O3 is added, it tends to agglomerate, causing stress concentrations that increase susceptibility to stress corrosion during exposure. As exposure continues, changes in the water chemistry within cracks lead to the formation of an oxygen concentration cell, further accelerating corrosion. Eventually, as cracks expand, the oxide film ruptures, and the dominant failure mode of the modified layer shifts to uniform corrosion.
  • CHEN Jun, WEI Jianhao, LI Wei, HAO Shengzhi, WANG Yinong
    China Surface Engineering. 2025, 38(6): 219-228. https://doi.org/10.11933/j.issn.1007-9289.20240326003
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    As a high-quality carbon structural steel with a carbon content of 0.42%-0.5%, 45# steel is an important material in material science owing to its favorable plasticity, high toughness, and excellent workability. Tempered 45# steel is widely used in the manufacture of gears, racks, bearings, and other key components. Under harsh conditions of high loads and high speeds, the surfaces of 45# steel components typically undergo severe wear. The surface integrity of components affects their service life and may result in accidents if the components are worn out. To improve the wear resistance of 45# steel, annealed 45# steel is first tempered and subsequently cut into cylindrical specimens in this study. Subsequently, water abrasive sandpaper is used to polish the specimens. Next, the specimens are irradiated with different number of pulses using high-current pulsed electron beam (HCPEB) technology under the following operating parameters: accelerating voltage, 26 kV; pulse width, 2 μs; energy density, 4 J / cm2; and number of pulses, 1, 3, 8, and 15. Changes in the surface morphology and roughness of the samples before and after irradiation are observed using a LEICA DMi8 metallurgical microscope and an OLYMPUS OLS4000 laser confocal microscope. Changes in the surface hardness of the samples before and after irradiation are measured using an HV-1000Z digital micro Vickers hardness tester. Changes in the grain-size distribution and grain orientation of the samples before and after irradiation are analyzed using a SYMMETRY2-type electron backscatter diffraction probe of a scanning electron microscope. Friction and wear tests are performed using an HSR-2M high-speed reciprocating friction tester. The amount of wear on the samples before and after irradiation is measured using the OLYMPUS OLS4000 laser confocal microscope. Changes in residual stress on the surface of the sample before and after irradiation are tested using an XL-640 stress gauge, with the center of the sample surface being the test position. The results show a crater morphology on the irradiated surface. Additionally, as the number of pulses increases, the number of craters decreases gradually, whereas the crater size and the sample-surface roughness increase gradually. After irradiation, the grains are refined, the average size range of the grains reduces from 1.5-29.5 μm in the unirradiated samples to 1.5-9.5 μm in the 15-pulses irradiated samples, and the percentage of grains with a diameter of 0-1.5 μm increases from 17.54% in the unirradiated samples to 92.54% in the 15-pulses irradiated samples. As the number of pulses increases, the surface hardness of the samples increases from 257.9 HV in the unirradiated sample to 371.4 HV in the 15-pulse irradiated samples. The wear volume, depth, and width of the wear trace on the samples are minimal after eight pulses, and the wear volume reduced by approximately 94% compared with that of the unirradiated samples. In this study, to address the increasing demand for the application of 45# steel, HCPEB technology is used to irradiate 45# steel with different pulse times, and the trends and mechanisms of changes in its surface morphology, grain orientation, grain size, residual stress, hardness, and wear-resistant properties before and after irradiation are investigated systematically. Subsequently, a relationship is established between the number of HCPEB irradiations on the surface of 45# steel and the friction and wear properties, and the optimum irradiation parameters for improving the wear-resistant properties of 45# steel are determined. The irradiation of #45 steel surfaces using HCPEB technology can improve the surface hardness and surface wear resistance of #45 steel components for a wide range of applications in harsh environments.
  • GAO Chong, DONG Lihong, LIU Bin, ZHANG Yupeng
    China Surface Engineering. 2025, 38(6): 229-239. https://doi.org/10.11933/j.issn.1007-9289.20241215001
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    With the increase in space launch frequency, the reuse of components to prolong the service life of structures is a feasible and effective technical method of improving the fatigue performance of components through surface strengthening processes. Currently, for the rolled 5B70-H32 new aerospace aluminum alloy, whether surface strengthening can achieve the effect of prolonging the service life, the process parameters corresponding to the strengthening and prolonging of the service life, and the fatigue damage behavior of the strengthened samples have not been studied and discussed in depth. To explore the influence of the strengthening process parameters on the fatigue properties of the rolled 5B70-H32 aluminum alloy, the fatigue life and crack growth rate of the samples before and after ultrasonic impact strengthening were tested. The gradient microstructure of the samples in the thickness direction after ultrasonic impact strengthening was observed using electron backscatter diffraction (EBSD). The residual stress distribution in the thickness direction of the base metal and strengthened sample was measured using electrolytic polishing combined with X-ray diffraction. The results showed that, under the same fatigue load, the average fatigue life of the specimens after ultrasonic impact strengthening was higher than that of the untreated specimens, and the fatigue life of the specimens after 400% ultrasonic impact strengthening was the highest, which was about 114% higher than that of the untreated specimens. The crack growth rate curves of the base metal and the CT specimen after 400% ultrasonic impact strengthening were fitted. The results showed that m, which describing the sensitivity of crack growth rate to stress intensity factor amplitude, before strengthening was 2.043 1 and m after strengthening was 1.890 32. Ultrasonic impact strengthening contributed to delaying the crack propagation rate in the 5B70-H32 aluminum alloy. The 400% ultrasonic impact coverage is the optimal strengthening parameter to improve fatigue life. To further clarify the influence mechanism of the microstructure of the rolled 5B70-H32 aluminum alloy after ultrasonic impact strengthening on the fatigue performance, the crack propagation panorama obtained by scanning electron microscopy and the influence range of the ultrasonic impact residual stress were superimposed. The crack tip was controlled in the range of 200-400 μm from the surface, which was used as the observation area for the effect of the microstructure on crack propagation after ultrasonic impact strengthening. EBSD was used for monitoring. By comparing the microstructure of the base metal with the crack propagation morphology after ultrasonic impact treatment, we found that an increase in dislocations, grain boundaries, second phases, and adjacent grains with different orientations delayed crack propagation. This was due to the formation of a unique rolling grain gradient refinement and inhomogeneous grain structure on the surface of the rolled 5B70-H32 aluminum alloy. Different degrees of grain refinement were produced at various depths of the microstructure during the evolution and formation of an uneven grain structure during rolled grain gradient refinement. The small-angle grain boundary was introduced into the grains and the number of adjacent grains with different orientations increased. Compared with the base metal, a residual compressive stress of 183.4 MPa was introduced on the surface after 400% ultrasonic impact coverage treatment. The introduced residual compressive stress effectively reduced the stress intensity factor at the crack tip, delayed cracking, and promoted crack turning. Ultrasonic impact can delay cracking and promote crack turning by forming a rolling grain gradient to refine the non-uniform grain structure and introduce residual compressive stress, thereby improving the fatigue performance of the rolled 5B70-H32 aluminum alloy. The research results reveal the influence mechanism of ultrasonic impact strengthening on the crack propagation of the rolled 5B70-H32 aluminum alloy, which provides a research idea for improving the fatigue performance of aluminum alloys.
  • HUANG Xiao, ZHAI Aoshuang, PENG Junqing, WANG Xin, TIAN Haoliang, ZHOU Shujun
    China Surface Engineering. 2025, 38(6): 240-250. https://doi.org/10.11933/j.issn.1007-9289.20240416002
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    Titanium alloy blades and engine cases experience local temperature increases under extreme conditions, such as impact and friction, causing titanium alloy parts to catch fire. The NiCrFeAl / BN thermal insulation flame-retardant coating can effectively prevent the occurrence of titanium fires. Preparing thermal insulation and flame-retardant coatings on the surface of titanium alloys is crucial to prevent titanium fires. The thermal insulation effect and crack propagation of the NiCrFeAl / BN flame-retardant coating during thermal shock cycles have not been thoroughly studied. The temperature and stress distribution of the coating system with NiCrFeAl / BN as the thermal insulation layer, YSZ as the flame-retardant layer, and NiCoCrAlY as the bonding layer during the thermal shock cycles were simulated using the finite element method, and the development process of cracks during the thermal shock cycle was studied. A thermal-mechanical coupled two-dimensional finite element model of the coating system was established to study the temperature and stress changes of the coating and substrate during the thermal cycles. The crack initiation and propagation model was built by combining the extended finite element method (XFEM) and cohesive element. Using this combined model, the initiation and propagation behavior of the surface crack, internal crack, and interface crack in the coating system was simulated. The conventional finite element method must reconstruct the mesh when solving crack propagation problems, which limits its application. The XFEM uses extended shape functions to describe discontinuous displacement fields, which have significant advantages in simulating crack propagation without updating the mesh model. XFEM allows cracks to propagate freely under stress, rather than being forced to propagate along grid boundaries, and can penetrate the grid during propagation. Therefore, the Abaqus software XFEM was used to study the initiation and propagation of vertical cracks. The four materials of the substrate and coatings are divided into four cross-sectional zones. Each layer, from bottom to top, is as follows: a titanium alloy TC11 substrate with a thickness of 10 mm, a NiCoCrAlY metal bonding layer with a thickness of 0.15 mm, a YSZ ceramic thermal insulation layer with a thickness of 0.2 mm, and a NiCrFeAl / BN sealing surface layer with a thickness of 1.2 mm. In the alternating cold and hot environment, thermal stress is generated inside the coating. When the thermal stress accumulates to a certain degree, the coating may crack. Based on the actual thermal cycling experiment process of the coating sample, a transient analysis of the thermal coupling of the sample model is performed to simulate the cyclic process of the coating from heating to the insulation stage and then to water cooling. The temperature is raised from 20 ℃ to 750 ℃ within 15 s, maintained at 750 ℃ for 300 s, and finally cooled from 750 ℃ to 20 ℃ by water cooling within 30 s, which is considered as one cycle. A small crack is pre-set on the surface of the coating. During the first heating and insulation stage, the crack in the coating does not propagate. However, during the cooling stage, stress concentrates at the crack tip. When the stress reaches the failure criterion, the crack begins to increase along the direction of maximum stress. In the subsequent thermal cycle, the vertical crack continues to propagate, and if the coating is subjected to sufficient thermal stress, the vertical crack may penetrate the coating. With the increase in thermal shock cycles, the initial microcracks gradually spread to the interior of the coating and gradually approach a state of stability. When subjected to 400 cycles of water cooling and heating, no interface cracks appear between the coating and the substrate, and the maximum stress occurs at the interface between the coating and the substrate. After 543 thermal cycles, interface cracks are observed, starting from the vicinity of the NiCoCrAlY bonding layer and extending horizontally. At this point, stress is redistributed, and the cracked coating is nearly free from the influence of stress. The substrate is subjected to significant stress, and the evolution of interface cracks ultimately led to coating peeling and failure.
  • ZHANG Maojun, ZHAO Chunli, DONG Ying, LI Xuesong, ZHANG Mingming, WANG Guofu
    China Surface Engineering. 2025, 38(6): 251-258. https://doi.org/10.11933/j.issn.1007-9289.20241101001
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    The computational cost of existing rib-flow-field-simulation methods has increased significantly because of the high demand for near-wall grid accuracy, which restricts engineering applications. In this paper, an efficient modeling method based on turbulence model modification is proposed to solve the bottleneck problem A new modeling approach based on the k-ω shear stress transport (SST) turbulence model is proposed. This method involves modifying the dissipation equation in the SST turbulence model, with the generated term in the turbulence dissipation equation being multiplied by a function to alter the turbulence dissipation near the wall. This approach enables the reproduction of the variation in velocity shift, ΔU+, in the logarithmic law region. Utilizing the previously studied and published experimental data on U-shaped and V-shaped ribs, this paper introduces the correction coefficient A of an alternative rib structure. The modeling model is obtained based on the k-ω SST turbulence model, and the relationship between the turbulence model parameter A and the rib scales of these two shapes is established. Subsequent theoretical derivation reveal a quantitative relationship between rib scale h+, modulation parameter A, and velocity offset ΔU+. We demonstrate that adjusting A can represent laying ribs of different shapes, and the corresponding drag reduction effect can also be directly reflected by the curved motion of the velocity profile in the logarithmic law region. The user-defined functions (UDF) in Fluent was used to modify the turbulence dissipation equation, thereby correcting the turbulence equation. The calculation results of the modular model were obtained, and the rib model calculation results were compared. A thorough analysis of the turbulent flow field in the proximity of the wall of the smooth plate and the rib surface was conducted, showing that the drag reduction effect of the rib surface is associated with the variation in the dimensionless velocity profile curve, designated as ΔU+. When ΔU+ > 0, the drag reduction effect was produced, whereas when ΔU+ < 0, a drag increase effect was produced. Additionally, alterations in the geometry of the rib surface resulted in corresponding changes in the velocity profile curve in the logarithmic law region. Furthermore, the velocity offset ΔU+ and the h+ of the rib were parabolically distributed. Through theoretical derivation, the quantitative relationship between the modular parameter A and the rib-scale h+ and the velocity offset ΔU+ is established, and adjusting A can represent the laying of ribs of different shapes and the corresponding drag reduction effect can also be directly reflected by the curve motion of the velocity profile in the logarithmic law region. The UDF was employed to modify the turbulence dissipation equation, thereby establishing and realizing the relationship between the aforementioned modeling parameters and the flow field velocity profile, thus completing the model. Comparison of the rib and modular models'calculation results revealed consistent outcomes, demonstrating the modular model's capability to accurately simulate the rib-induced wall surface drag reduction with reduced computational demands The modulated model was shown to have a beneficial effect on the rib substitution under specific working conditions. Through this modular model, the simulation of the near-wall flow field details can be circumvented, thereby reducing the number of calculations and calculation time. Through theoretical modeling, the physical characteristics of the ribs were mapped to the modified parameters of the turbulence equation, and an equivalent flow control simulation without geometric modeling was achieved, providing an efficient numerical analysis method for the drag reduction design of ribs.
  • FENG Yikang, ZHOU Cheng, SU Zebin, GOU Junfeng, YANG Yang, ZHANG Xiaodong, WANG You, YU Keqiang, LIU Wen, LUO Xiaofeng
    China Surface Engineering. 2025, 38(6): 259-270. https://doi.org/10.11933/j.issn.1007-9289.20240408003
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    Nowadays, various compositions of Al2O3-based ceramic coatings have been studied and applied. Among these, Al2O3-Cr2O3 coatings have attracted attention due to their excellent comprehensive performance. Graphene possesses outstanding hydrophobicity, self-lubricating properties, and corrosion resistance, and has been widely used to enhance the corrosion resistance of organic coatings. Researchers have found that the addition of graphene to Al2O3 bulk materials and coatings can improve their mechanical properties and wear resistance. However, the effect of graphene nanosheets on the corrosion behavior of Al2O3-based coatings has not yet been fully revealed. Therefore, studying the corrosion behavior of graphene-modified Al2O3-Cr2O3 coatings is of great significance. Nanostructured Al2O3-Cr2O3 powders with varying contents of graphene nanosheets were firstly prepared using traditional ball milling and spray granulation. Atmospheric plasma spraying (APS) technology was employed to deposit double-layer coatings on 45# steel substrates. NiCrAlY was used as the bond coating, while the top coatings were Al2O3-Cr2O3 with different graphene nanosheet contents. The morphologies and compositions of the powders and coatings were characterized using SEM and EDS. The corrosion resistance of the coatings was evaluated through electrochemical and immersion tests. The macro- and microstructures of corroded coatings were observed, and the corrosion products were analyzed using SEM, XRD, and Raman spectroscopy to reveal the corrosion mechanisms. Spherical Al2O3-Cr2O3 powders, both with and without graphene, were successfully prepared. However, the powder morphology became irregular when the graphene content increased to 6%. Test results showed that the corrosion resistance of the coatings initially increased and then decreased as the graphene content rose, even though coating porosity increased almost linearly. The self-corrosion potential (Ecorr) firstly increased and then decreased with increasing graphene content, while the self-corrosion current density (Icorr) exhibited an opposite trend. The coating with 1% graphene (AC-1) showed excellent corrosion resistance, with its Ecorr increasing by 89 mV and Icorr decreasing by 26% compared to the coating without graphene. Additionally, the polarization resistance of the AC-1 coating was approximately twice that of the unmodified coating. Pore resistance decreased with increasing graphene content, likely due to higher porosity. The immersion corrosion rate curves fluctuated over time, but the AC-1 coating maintained a relatively low corrosion rate compared to other coatings, decreasing by up to 29% relative to the unmodified coating. In contrast, the coating with 6% graphene (AC-6) exhibited the poorest corrosion resistance. Immersion in NaCl solution led to severe corrosion of the steel substrate, with noticeable rust on the coatings. The number of pores and lamellar interfaces increased after immersion, and corrosion products accumulated at pore edges. Corrosion mainly occurred at the interface between the substrate and the bond coating. The primary corrosion products were iron oxides, iron hydroxides, and FeOOH, with a small amount of Cl-containing products also detected. The effects of graphene on coating porosity and the diffusion of corrosive media determined the variations in corrosion rates. The addition of graphene to Al2O3-Cr2O3 coatings inhibited the diffusion of corrosive media into pores due to its hydrophobicity, thereby improving corrosion resistance. However, excessive graphene increased coating porosity—owing to its high melting point—thus deteriorating corrosion resistance. This study clarifies the influence of graphene nanosheets on the corrosion resistance of Al2O3-Cr2O3 coatings and provides a theoretical basis for preparing high-performance Al2O3-based ceramic coatings.
  • KONG Xinru, LIU Xiaoling, SUN Xiaowei, GUO Yang
    China Surface Engineering. 2025, 38(6): 271-279. https://doi.org/10.11933/j.issn.1007-9289.20241212002
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    Lubricants are used in modern industrial applications to enhance energy efficiency and reduce material damage by minimizing friction and preventing wear in both sliding and rolling contacts. Zinc dialkyldithiophosphate (ZDDP), the most extensively used anti-wear additive in engine oils, has been the subject of extensive research over the past few decades. Studies have shown that ZDDP undergoes tribochemical reactions to form a robust phosphate glass-based tribofilm on friction surfaces, effectively preventing direct contact between two surfaces. Although significant progress has been achieved toward understanding the drivers of tribofilm growth, tribofilm formation has been considered to follow a stress-promoted thermal activation model. However, an ongoing debate, as well as extended discussion, persists regarding the precise nature of the underlying mechanism involved in the overall tribofilm formation process. To systematically investigate the key factors influencing tribofilm growth, we developed a non-Newtonian point-contact thermal elastohydrodynamic lubrication (EHL) model incorporating the Ghanbarzadeh tribofilm growth model under the assumption of smooth contact surfaces. The pressure is computed using the multigrid method, elastic deformation is determined using the multigrid integration method, and temperature field is analyzed using the sequential column sweeping technique. This model provides a detailed and comprehensive examination of how various influencing factors, such as temperature, pressure, shear stress, and slide-roll ratio, collectively affect and determine the distribution characteristics of the tribofilm thickness. Furthermore, the influencing mechanisms and underlying interactions of these factors are thoroughly explored and interpreted from the perspective of temperature variation. The results demonstrate that temperature is a critical driving factor for tribofilm growth. Even under EHL conditions, as the temperature increases, the increase in the solid surface temperature becomes more pronounced, resulting in a significant increase in the tribofilm thickness, which exhibits an exponential growth trend. Additionally, by comparing three lubricants with different friction properties, we observed that shear stress significantly promotes tribofilm growth. Specifically, lubricants with high EHL friction, characterized by their higher pressure-viscosity coefficients, generate greater shear forces, resulting in thicker tribofilms than those with low EHL friction. This finding validated the stress-promoted thermal activation model. Moreover, both the pressure and the slide-roll ratio significantly influence the thickness of the tribofilm. An increase in either parameter promotes tribofilm formation. Specifically, when the slide-roll ratio is relatively low, the influence of pressure on the thickness of the tribofilm is minimal and can almost be considered negligible. In contrast, as the slide-roll ratio increases to higher levels, the effect of pressure on the tribofilm thickness becomes increasingly significant and much more pronounced. In particular, when the slide-roll ratio is high, a significant increase in pressure causes a marked and considerable increase in the thickness of the tribofilm. This phenomenon can primarily be attributed to the combined and notable effects of the pressure and slide-roll ratio on the temperature of the contact surfaces. These changes in the temperature directly and significantly contribute to the variations observed in the tribofilm thickness. Consequently, the role of pressure in enhancing and promoting the tribofilm growth should not be underestimated and should be carefully considered. Under EHL conditions, the tribofilm formation process is primarily controlled and influenced by key factors such as shear stress, pressure, and temperature within the contact region, which is consistent with the well-established stress-promoted thermal activation model. Furthermore, in the context of EHL, a more accurate and comprehensive representation of the various factors that affect the growth of the tribofilm can be achieved by considering the variations in temperature within the contact region and thereby generating the distribution of the tribofilm.
  • CHEN Xu, YANG Hongyu, YAN Jianhui, WU Jiwen, CHEN Fang
    China Surface Engineering. 2025, 38(6): 280-291. https://doi.org/10.11933/j.issn.1007-9289.20240401002
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    Q235 steel shows broad application prospects in construction engineering, machinery manufacturing, and other fields. However, its low hardness has been a key factor restricting its rapid development. As a low-carbon steel, Q235 cannot improve its performance through martensitic phase transformation. To address this issue, surface strengthening treatments are required. Plasma cladding technology, due to its rapid melting and cooling, fine microstructure, and other characteristics, can significantly enhance the surface properties of the workpiece. Mo-Si-B alloys possess high strength, hardness, and wear resistance, and exhibit great potential for application. However, the brittleness and processing difficulties of Mo-Si-B alloys have seriously limited their application in complex structural parts. In recent years, the development of surface modification technologies such as plasma cladding has provided new ideas for the application of Mo-Si-B materials, and more scholars are turning to research on Mo-Si-B coatings. Mo-Si-B powder is a refractory powder typically prepared by crushing and screening or gas atomization methods. However, these methods face challenges such as irregular shape, large particle size, and satellite powder, which affect the quality of the coating. The spray drying method, widely used to prepare refractory metal powders based on tungsten alloys due to its high spheroidization rate and uniform particle size, has not yet been applied to Mo-Si-B spherical powder preparation. Therefore, to overcome the shortcomings of low surface hardness and poor wear resistance of Q235 steel and extend its service life under complex working conditions, Fe-Mo-Si-B spherical powder was prepared using the spray drying method and used as the cladding powder. A Fe-Mo-Si-B coating was deposited on the surface of Q235 steel via plasma cladding technology. The elemental distribution, microstructure, phase composition, hardness, and fracture toughness of the coatings were characterized by X-ray diffraction (XRD), scanning electron microscopy (SEM), energy-dispersive spectrometry (EDS), and microhardness testing. The effects of cladding current and scanning speed on the phase composition, microstructure, microhardness, and fracture toughness of the coatings were studied to provide guidance for optimizing Mo-Si-B coating process parameters on iron substrates. The results showed that the coating microstructure consisted of dendrites under different process parameters. With increasing cladding current, the dilution rate and the width of the single-pass coating increased, surface defects such as raw edges and unmelted particles disappeared, and the microstructure became coarser. With increasing scanning speed, the dilution first decreased and then increased, while the microstructure gradually refined—mainly due to changes in the temperature gradient (G) to solidification rate (R) ratio. The main phases of the coating were Fe3Mo2 λ-Fe2Mo, R-Fe3Mo2, μ-Fe7Mo6, (Fe,Si)3B, and Fe3B. These dispersed phases significantly improved the coating's microhardness. The formation of metastable phases like Fe3Mo and R-Fe3Mo2 was attributed to the rapid solidification during cladding, which restricted atomic diffusion and hindered full elemental reactions. As the cladding current increased, the coating's microhardness decreased while fracture toughness increased. At a cladding current of 80 A, the maximum microhardness was 1 138 HV. At 120 A, the maximum fracture toughness was 9.94 MPa·m1/2. With increasing scanning speed, the microhardness first increased and then decreased, while fracture toughness first decreased and then increased. At a scanning speed of 130 mm / min, the maximum microhardness was 1 028 HV and the minimum fracture toughness was 5.41 MPa·m1/2. The coating exhibited transgranular fracture, and the primary toughening mechanisms were crack bridging and crack deflection.
  • GAO Yuan, HU Lele, WANG Wei, WANG Kuaishe
    China Surface Engineering. 2025, 38(6): 292-302. https://doi.org/10.11933/j.issn.1007-9289.20240425002
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    Friction and wear account for approximately 30% of global energy dissipation and 80% of mechanical component failures, resulting in annual economic losses equivalent to 2%-7% of global gross domestic product (GDP). Superlubricity, characterized by friction coefficients below 0.01, has emerged as a transformative concept. However, its industrial implementation remains limited by insufficient load-bearing capacity and prolonged running-in periods. Existing liquid-based superlubricity systems, including acid-based aqueous solutions, hydrated materials, ionic liquids, and oil-based lubricants, achieve ultralow friction coefficients ranging from 0.002 to 0.01, but their operational contact pressures rarely exceed 130 MPa. Although solid-liquid hybrid systems incorporating two-dimensional nanomaterials, such as black phosphorus, demonstrate improved load-bearing capabilities, significant research gaps persist in understanding their lubrication behavior at metallic tribological interfaces, which dominate industrial machinery. This study presents a hydroxylated black phosphorus quantum dot (BPQD-EG)-based aqueous lubrication system synergized with NaOH, enabling stable superlubricity under high contact pressures. A BPQD-EG was synthesized via high-energy ball milling of red phosphorus, using ethylene glycol as a surface modifier. The high resolution transmission electron microscope (HRTEM) revealed spherical BPQD-EG nanoparticles averaging 3.39 nm in size, with lattice fringes of 0.203 nm corresponding to the 040 crystallographic plane. The X-ray photoelectron spectroscopy (XPS) and fourier transform infrared spectroscopy (FTIR) analyses confirmed hydroxyl grafting through P-O-H bonding at 533.3 eV and 3 429 cm-1, respectively, validating successful surface functionalization. Superlubricity performance was evaluated using a four-ball tribometer under varying loads and rotational speeds. The BPQD-EG aqueous solution achieved superlubricity with a friction coefficient of approximately 0.009 under conditions where the applied load was below 40 N or the rotational speed exceeded 1 400 revolutions per minute. During the running-in process, oxidation occurred on the metal surface, forming FexOy species (Fe2O3 / FeOOH) that enhanced surface polarity. Although the BPQD-EG underwent partial oxidation, it retained a high density of hydroxyl groups (P-O-H). These hydroxylated BPQD-EG nanoparticles bonded to the metal surface via hydrogen bonding, forming a lubricating film that prevented direct contact between the friction pair surfaces, effectively reducing the friction coefficient and minimizing wear. Notably, the addition of NaOH significantly extended the superlubricity regime, achieving a stable friction coefficient of 0.007 under a 60 N load for 5 000 s. Compared to previous BPQD-EG systems, this represents a 50% increase in maximum load capacity (from 40 to 60 N) and a 43% reduction in the running-in period, demonstrating enhanced efficiency for industrial applications. Hydrated Na+ ions were adsorbed onto the negatively charged steel interface, generating repulsive hydration forces that supported high loads. The hydroxylated BPQD-EG / NaOH system reduced the wear scar diameter by 66% compared to BPQD-EG alone, demonstrating superior anti-wear performance. The XPS analysis of the wear surfaces confirmed that the addition of NaOH enhanced P-O-H bonding, increasing the number of hydroxyl groups on the BPQD surface and facilitating the formation of a hydrogen-bonded network. In contrast, the addition of NaCl increased the friction coefficient to approximately 0.125 and significantly enlarged the wear scar diameter. The wear surfaces exhibited coarse plowing grooves and adhesive spalling pits, resulting in a rough internal morphology. This suggests that Cl⁻ ions disrupt the hydrogen-bonded network, promoting direct metal-to-metal contact between friction pairs, which induces adhesive wear; subsequently, the detached debris intensifies abrasive wear. The destructive effect of Cl- on the hydrogen-bonded network is further evident in the corrosion severity of steel balls: after six months of tribological testing, steel balls lubricated with BPQD-EG / NaCl showed severe corrosion damage, whereas those lubricated with BPQD-EG / NaOH maintained a passive state with negligible surface corrosion due to the alkaline conditions (pH ≈ 8.5). These findings confirm that the BPQD-EG / NaOH synergistic system exhibits superior environmental stability compared to NaCl-containing systems through sustained passivation. Overall, this work provides a novel strategy for designing robust water-based superlubricity systems using functionalized nanomaterials and ionic hydration effects, advancing their potential for industrial applications in high-load-bearing systems.
  • GUO Hongfei, WU Jiafang, HOU Xiaohu, ZENG Chao, ZHAO Min
    China Surface Engineering. 2025, 38(6): 303-314. https://doi.org/10.11933/j.issn.1007-9289.20240414001
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    The spray-deposited 7055 aluminum alloy has ultra-high strength, excellent machinability, and good heat treatment performance. However, aluminum alloys often exhibit surface cracks and fatigue failures during service, which affect their service life and safety. Solution treatment is a common metal-material processing technology. By dissolving certain elements of the alloy into the matrix, the microstructure and properties of the alloy can be significantly improved. In this study, 7055 aluminum alloy was subjected to single-stage solution treatment at 470  ℃ for 2 h and double-stage solution treatment at 440  ℃ for 4 h + 490  ℃ for 30 min. Water quenching was carried out at room temperature, with a transfer time of less than 25 s. Through solution treatment of the spray-deposited 7055 aluminum alloy, it was observed that the microstructure of the alloy changed significantly. Hardness and tensile tests of the extruded alloy and the solution-treated alloys were carried out, and the average values of the sample data were taken. Finally, the fatigue life values of the three samples were obtained through tensile-tensile fatigue tests on the extruded, single-stage solution, and double-stage solution samples. To further study the effect of solution treatment on the microstructure and properties of the 7055 aluminum alloy, advanced detection techniques such as scanning electron microscopy (SEM) and electron backscatter diffraction (EBSD) were used. SEM can provide high-resolution surface and cross-sectional images to help observe the microstructure and defects in the material. EBSD can provide detailed information on crystal orientation and grain boundary distribution, which is helpful for understanding the microstructural characteristics of materials. The second phase, grain size, grain orientation, recrystallization evolution, fatigue properties, and fatigue fracture of the spray-deposited 7055 aluminum alloy during solution treatment were studied using SEM. Combined with the changes in alloy hardness, the optimal solution treatment process was determined, providing a research basis for optimizing the solution process of spray-deposited 7055 aluminum alloy. The microstructure of the alloy was controlled through the solution treatment process to improve its mechanical properties and fatigue resistance. The effects of the solution treatment process on the microstructure, fatigue properties, and fatigue fracture of the spray-deposited 7055 aluminum alloy were studied using SEM and EBSD. The results show that, after the two-stage solution treatment at 440  ℃ / 4 h + 490  ℃ / 30 min, the size of the insoluble phase Al₂CuMg and the impurity phase Al₇Cu₂Fe in the matrix decreased, and the proportion of the second phase decreased by 10.2%. The degree of recrystallization improved, the grain boundaries became clearer, the grain size was more evenly distributed, and the hardness of the alloy significantly improved. The hardness values of the as-extruded alloy and the single-stage and double-stage solution-treated alloys were 101 HV, 134 HV, and 182 HV, respectively. Their tensile strengths were 356 MPa, 435 MPa, and 559 MPa, respectively. Tensile-tensile fatigue tests were carried out on the three samples: extruded state, single-stage solution, and double-stage solution. The test parameters were as follows: under a maximum stress of 300 MPa and a stress ratio of R = 0.1, three samples were selected for each state, and the average fatigue life values were obtained. The average fatigue lives at the 300 MPa stress level were 12 000, 34 000, and 56 000 cycles, respectively. The results showed that the two-stage solution treatment played an active role in improving the mechanical and fatigue properties of the 7055 aluminum alloy. This provides a reference for optimizing the heat treatment process of 7000-series aluminum alloys.
  • WANG Ying, HU Ningbo, ZHANG Yan, SONG Renguo, LIU Lin, YUAN Ningyi, DING Jianning
    China Surface Engineering. 2025, 38(6): 315-324. https://doi.org/10.11933/j.issn.1007-9289.20240418001
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    Titanium alloys are widely utilized in aerospace, marine ships, biomedicine, and other fields owing to their lightweight, high specific strength, low elastic modulus, good corrosion resistance, and good biocompatibility. Although titanium alloys exhibit some degree of corrosion resistance owing to the oxide film on their surface, the naturally formed oxide film is thin and susceptible to degradation, resulting in limited corrosion resistance. In particular, in the harsh conditions of high-salt and high-humidity marine environments, titanium and its alloy parts will suffer severe electrochemical corrosion and crevice corrosion when working, which greatly limits their large-scale application. Micro-arc oxidation technology is widely used in metal surface protection because of its simple operation, green environmental protection, and induced strong adhesion between the film and the substrate. However, a single micro-arc oxidation film has holes and cracks on the surface, which limits its anti-corrosion performance. At present, the primary methods used to improve the performance are in-situ sealing by adding insoluble micro-nano particles and post-sealing methods combined with other surface technologies. Micro-arc oxidation technology combined with self-assembly of low surface energy materials has been used to construct superhydrophobic films on the surface of magnesium and aluminum alloys to improve their corrosion resistance. However, there are few related studies on titanium alloy surfaces. In this study, post-sealing was used to construct micro-nano structures on the surface of TC4 titanium alloy using micro-arc oxidation technology. Combined with the surface modification with low-surface-energy octadecyltrimethoxysilane, which not only provided it with a lower surface energy but also exerted a filling effect on the micropores and cracks produced by micro-arc oxidation, a long-term anti-corrosion superhydrophobic composite film was constructed on the surface of TC4 titanium alloy. The surface morphology, composition, and phase composition were characterized by scanning electron microscopy, energy-dispersive X-ray spectroscopy, Fourier-transform infrared spectroscopy, and X-ray diffraction. The wettability and corrosion resistance of the film were tested using a contact angle measuring instrument and an electrochemical workstation, respectively. The results showed that the ceramic-based superhydrophobic composite film had TiO2 as the main component and was successfully constructed on the surface of the TC4 titanium alloy. Compared with the TC4 titanium alloy substrate, the water contact angle of the superhydrophobic film increased from 48°± 2°to 154°±1.8°, and the corrosion current density decreased from 2.346×10-6 A·cm-2 to 9.481×10-10 A·cm-2, reflecting a reduction of approximately four orders of magnitude. The self-corrosion voltage increased from -0.480 V to 0.454 V, increasing by 0.934 V. The impedance increased by approximately two orders of magnitude, reaching up to 4.97×107 Ω. To assess the corrosion durability of the superhydrophobic film, the samples were immersed in 3.5wt.% NaCl solution for one week and exposed to air for one week, respectively. Even after these treatments, the impedance remained in the 107 Ω range, indicating that the film exhibited sustained corrosion resistance. This performance is attributed to the micro-nanostructures within the superhydrophobic film, which capture and retain air upon exposure, forming a stable air layer on the surface. This air layer effectively prevents corrosive media from directly contacting the substrate, thereby enhancing both the corrosion resistance and durability of the coated sample. This study provides both experimental and theoretical foundations for the surface corrosion protection of titanium alloys and offers valuable insights for expanding their application in marine environments.
  • QIAO Da, ZENG Wu, XIAO Bo
    China Surface Engineering. 2025, 38(6): 325-337. https://doi.org/10.11933/j.issn.1007-9289.20240306001
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    With the pursuit of higher thermal efficiency in gas turbines, the turbine inlet temperature is continually increasing. Consequently, thermal barrier coatings (TBCs) are widely employed to effectively reduce the temperature of the base metal. However, owing to the complex material system of TBCs, they are prone to delamination during service, which can lead to overheating and corrosion failure of the base metal. To understand the influence of different material properties on stress distribution and damage evolution within the coating system, an in-depth analysis of the material system is essential. A finite element simulation was conducted, simplifying the coating interface into an ideal sinusoidal curve. The effects of plasticity and creep in the TBC materials on stress distribution at the coating interface were analyzed on a layer-by-layer cumulative basis, considering the dynamic growth of the thermally grown oxide (TGO) layer. Because TBCs produced by the atmospheric plasma spray (APS) process are prone to spalling at the interface between the ceramic layer and the TGO layer, a cohesive element was introduced at this interface to systematically study the evolution of interfacial damage. The results showed that spalling was more likely to occur when thermal spraying was performed at higher temperatures, resulting in higher residual stresses in the TBCs at room temperature. The results showed that due to thermal spraying occurring at higher temperature, the coating exhibited higher residual stress at room temperature, leading to a greater likelihood of peeling. When the dynamic growth of the TGO layer was considered, the resulting thermal growth stresses were found to be significantly greater than the thermal mismatch stresses—nearly tripling the normal stress at the interface. This also shifted the location of maximum normal stress from the peak to the off-peak site, causing a sharp increase in stress at the off-peak location. At elevated temperatures, the yield strength of TBC materials decreases, making them more prone to plastic deformation. During thermal cycling, a ratcheting effect was observed in the coating materials. Owing to the continuity of the coating interface, displacements among the different materials were coordinated, leading to a redistribution of coating stress. The plasticity of the ceramic layer was not considered owing to its brittle nature. However, the plasticity of the bonding layer, TGO layer, and base metal were analyzed. The bonding layer's plasticity effectively reduced interfacial stresses—by approximately 40% for normal stress and 18% for shear stress. Conversely, the plasticity of the TGO layer nearly offset the stress-relief effect provided by the bonding layer. The substrate's plasticity had negligible effect on coating stresses. Although the creep properties of the materials did not significantly alter the stress distribution pattern, they did affect the magnitude of the stress values. Creep in the bonding layer reduced the normal and shear stresses by 20% and 35%, respectively. Meanwhile, creep in the ceramic layer slightly reduced stress, whereas creep in the TGO layer slightly increased it. Damage was first observed at the off-peak site of the interface and expanded bilaterally, eventually propagating into the ceramic or TGO layer. When surface cracks in the ceramic layer intersected with cracks at the coating interface, the coating experienced spalling and ultimately failed. The influence of TBC material properties on coating stresses was analyzed using a multifactorial coupled model that accounted for TGO growth and interface morphology. The findings of this study provide valuable guidance for the development of thermal barrier coatings and failure analysis.
  • DING Zhaoqun, LU Laixiao, CHEN Qingqiang, WANG Zhonglei, SHI Qilong
    China Surface Engineering. 2025, 38(6): 338-348. https://doi.org/10.11933/j.issn.1007-9289.20240827005
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    The demand for high-performance lightweight materials is increasing in industrial fields such as aviation, automotive manufacturing, and marine engineering. Aluminum alloys are widely used because of their excellent mechanical properties and corrosion resistance. However, in the forming process of aluminum alloy components, the problems of surface quality and dimensional accuracy gradually become prominent, which affects the overall performance of the parts. As a solution, shot peening can improve the mechanical properties of materials, but in thin-walled structural components, particularly aluminum alloy thin-walled components used in aviation, the macroscopic deformation caused by laser shot peening remains a challenge. Excessive deformation not only affects dimensional accuracy but may also cause assembly difficulties and decreased structural performance. Therefore, understanding the quantitative relationship between laser peening parameters and the deformation of thin-walled parts and establishing accurate prediction models are crucial for optimizing the processes and controlling deformation. This study investigated the effects of laser peening treatment with different power densities on the macroscopic dimensions, residual stress distribution, surface integrity, and microstructure of 7050-T7451 aluminum alloy thin-walled parts. A multi-gradient power density ranging from 2 to 6 GW / cm2 was used for laser peening treatment of the 7050-T7451 aluminum alloy. Subsequently, the macroscopic dimensions were measured using a Performance 7107 coordinate measuring instrument. Surface morphology and contour data were obtained using a KC-X1000 series laser spectroscopic confocal microscope, and the residual stress distribution was detected using a PROTO series X-ray diffraction stress analyzer. Two samples were cut at approximately 1 / 4 of the center of the laser peening area of each sample, one of which was used for microhardness measurement and the other for SEM observation after corrosion treatment. When the power density exceeded 4 GW / cm2, the surface quality of the workpiece significantly decreased. Therefore, the experimental results for 4 GW/cm2 and below were analyzed in detail. The results showed that with an increase in the laser power density, the center of the workpiece bulged upward, and the residual compressive stress significantly increased, approaching saturation at 3.5 GW / cm2. Laser peening also resulted in an increase in the surface roughness and microhardness and the appearance of micropores in the microstructure. Based on the equivalent bending moment method, a quantitative description model of the maximum deflection of aluminum alloy thin plates by laser peening and workpiece structural parameters was established to accurately predict the deformation of the workpieces under different laser power densities. The results not only reveal the quantitative relationship between power density and deformation, but also provide a theoretical basis for the precise control of the laser peening process and optimization of the process parameters. Through these studies, the power density threshold range for the laser peening treatment of the 7050-T7451 aluminum alloy was determined. Within the range of 2 to 3.5 GW / cm2, laser peening can effectively increase residual compressive stress, strengthen the surface of the workpiece, and avoid excessive thermal effects and surface damage caused by excessive energy, thereby achieving the best strengthening effect. Laser peening significantly improves the physical and mechanical properties of 7050-T7451 aluminum alloy. Experiments have shown that at different laser power densities, laser peening increases the surface roughness of the material, with a maximum surface microhardness of 222.9 HV and a maximum residual compressive stress of 312.1 MPa. These changes significantly enhance the fatigue and wear resistance of the material, demonstrating the effectiveness of laser peening for the surface strengthening of aluminum alloys. Research has revealed a close correlation between the power density of laser peening and the macroscopic deformation of 7050-T7451 aluminum alloy. As the power density increased, the degree of deformation of the workpiece gradually increased and tended to stabilize at 3.5 GW / cm2 with a maximum bulge height of approximately 0.43 mm. By establishing a quantitative description model of the laser-shot-peening and workpiece structural parameters, this paper establishes a relationship model between the equivalent bending moment, laser power density, and thin-plate thickness. In summary, this paper examines the impact of laser peening on thin-walled aluminum alloy parts and provides a theoretical basis for controlling and optimizing laser peening processes, which is essential for promoting the development of related industrial fields.
  • FAN Jinhu, DING Kunying, ZHANG Tao, XIE Chunhai, JI Yun, LIN Guoding, LU Jintao
    China Surface Engineering. 2025, 38(6): 349-361. https://doi.org/10.11933/j.issn.1007-9289.20241205005
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    Yb2Si2O7 (abbreviated as YbDS) has been identified as a potential environmental barrier coating (EBC) material for application on the surface of silicon carbide ceramic matrix composites (SiC-CMCs). However, investigations on the mechanical rub-impact characteristics of this coating remain limited. To gain a deeper understanding of the rub-impact mechanisms between YbDS and inconel 625 high-temperature alloy blades, this paper develops a force-thermal-wear coupling model based on Archard's wear theory, accounting for the influence of frictional heating under actual working conditions. This model aims to elucidate the interaction and coupling behaviors during the rub-impact process. A 150-200 μm silicon bonding layer was prepared on the SiC substrate, followed by a 1 000 μm ceramic top layer. Prior to top-layer deposition, the silicon layer underwent in-situ reaction to form a silicon carbide bonding layer via vacuum heat treatment at 1 400 ℃ for 4 h. Two types of Si / YbDS bilayer EBCs with different porosities were fabricated using atmospheric plasma spraying. The coatings were evaluated experimentally for hardness, elastic modulus, wear coefficient, rub-impact force, and temperature distribution in the rub-impact area under various working conditions during high-speed rotor-blade rub-impact tests. The wear depth, frictional heating, and rub-impact force of the coatings were simulated using ANSYS Workbench based on the Archard wear model. Additionally, laser confocal scanning microscopy (LCSM) and scanning electron microscopy (SEM) were employed to analyze the wear depth, wear morphology, and material transfer between the blade tips and coatings after rub impact. The Archard wear model was further refined to incorporate temperature-dependent characteristics of the ceramic coating. The results indicated that adding 5wt.% polyphenyl ester (PHB) to the YbDS powder reduced the Brinell hardness of the coating by 20% and increased the wear coefficient by a factor of 4. The maximum normal rub-impact force under various working conditions decreased by 7.24%-21.13%. During atmospheric plasma spraying, most of the PHB vaporized, leaving pores or cracks within the coating. This modification reduced the coating hardness and enhances wearability without compromising the adhesion performance of the substrate material. In finite-element iterative simulations of the thermal-stress-wear coupling process, a fully coupled approach was employed to continuously update the geometry of the contact surface, enabling a more accurate representation of the force-thermal-wear coupling phenomena during rub impact. The simulation results revealed the variations and distribution characteristics of wear depth, temperature, and contact stress under four working conditions, which agreed with the experimental findings. The wear depth was significantly affected by the rotational speed, with the wear depth under low-speed conditions exceeding that under high-speed conditions for the same parameters. The temperature of the rub-impact area was strongly influenced by the penetration rate and rotational speed. At the same rotational speed and depth of penetration, the friction temperature was positively correlated with the penetration rate, and this effect gradually weakened as the rotational speed increased. The maximum normal rub-impact force was primarily influenced by the penetration rate, exhibiting a positive correlation; however, this effect weakened with increasing rotational speed. In the process of high-speed rub impact, which was affected by thermal friction, adhesion transfer of the coating to the blade occurred. Considering the influence of frictional heating under actual working conditions, the modified Archard model produced simulation values that aligned more closely with the experimental results, with the error in the normal rub-impact force controlled to within 7% when the single-pass cutting depth was 0.6 μm. This comprehensive analysis of the rub-impact behavior of YbDS coatings and inconel 625 blades provides insights into their frictional wear performance and cutting characteristics for real-world engineering applications.
  • ZHANG Hongwei, CHEN Tao, YAN Xichao, SHI Songyi, XIE Mingzhao, QIN Hailong
    China Surface Engineering. 2025, 38(6): 362-370. https://doi.org/10.11933/j.issn.1007-9289.20240224001
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    The GH4169 alloy, characterized by its excellent strength and fatigue resistance, is extensively utilized in alloy disk components of aerospace engines. However, due to the harsh operating environments, creep deformation over long service periods not only affects the normal operation and assembly of aerospace engines but can also lead to structural fractures if the deformation becomestoo significant. Such fractures can result in catastrophic turbine disk failures, causing engine malfunctions. To address the issue of creep deformation failures in GH4169 high-temperature alloy disk components, an investigation was conducted into the creep behavior of GH4169 tensile specimens under different stress levels at 650 ℃. This study involved analyzing the creep deformation patterns of the material under various stress conditions and integrating both the theta projection method and the combined time hardening (CTH) constitutive models. For the structural analysis of GH4169 high-temperature alloy turbine disks, a coupled creep model was developed by integrating the theta projection method with the CTH model. This approach aimed to improve the accuracy of creep stage predictions under different stress conditions by combining the strengths of both models. A CREEP user subroutine for a coupled model suitable for a turbine disk structure under a wide range of stress levels was also developed. Utilizing the elastoplastic finite element analysis method in ABAQUS, this coupled creep constitutive model was applied to simulate the elastoplastic and creep deformation responses of GH4169 high-temperature alloy test bars at 650 ℃ under various stress conditions. To validate the computational accuracy of the subroutine, simulation results were compared with experimental data from GH4169 tensile creep tests. The comparison confirmed the reliability of the coupled model, which integrates the theta projection method and CTH creep model. Furthermore, thecoupled model was employed to analyze creep deformation in a specific GH4169 high-temperature alloy turbine disk component withinan aerospace engine. Rotational creep experimental results of the GH4169 alloy disk components were compared with simulation outcomes from three different creep models: the theta projection method, the CTH model, and the coupled model combining both approaches. This study revealed that the theta projection method accurately predicts the third stage of creep induced by high stress, while the CTH creep model provides greater precision in capturing deformation during the first two stages. However, the coupled model developed in this study offers a more comprehensive and accurate description of the creep behavior of GH4169 high-temperature alloy disk structures across various stress levels and creep stages than either model alone. In the elastoplastic finite element simulation, stress was found to be most concentrated at the disk core and most dispersed at the disk rim. As creep time progressed, the disk rim tended to remain in the first and second stages of creep for a longer period, while the disk core transitioned to the third stage more rapidly, exhibiting the most pronounced creep deformation. Additionally, stress relaxation was more significant at the disk core than at the rim. These findings support the reliability of GH4169 high-temperature alloy disk components in aerospace applications and provide engineering guidance for enhancing the structural design of turbine disks.
  • LI Yong, LI Qing, XIONG Zhi, XIE Weiwei, WU Mingliang, LIU Gang, WANG Yansong, CHANG Zhe, HAN Tianpeng
    China Surface Engineering. 2025, 38(6): 371-382. https://doi.org/10.11933/j.issn.1007-9289.20241025001
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    Laser-cladded NiCrBSi coatings, which are used as coatings resistant to high-temperature corrosion and erosion, have been applied to a certain extent in the protection of high-temperature heating surfaces of utility boilers. During the deep peak-shaving process of thermal power units, due to the uneven flue gas temperature in the furnace, overtemperature tube burst often occurs, resulting in unplanned shutdowns. However, safety evaluations of the long-term service performance of NiCrBSi coatings are still lacking. In this study, TP347HFG, a material commonly used for furnace tubes, was selected as the base material, and NiCrBSi coatings were prepared on its surface using laser cladding technology. Different heat-treatment parameters were sequentially selected to simulate the temperature fluctuations during pipe operation. The heat-treatment temperatures were designed as 650, 750, 850, and 950 ℃, with holding times of 50, 100, 200, 500, 1 000, and 2 000 h. The performance of the NiCrBSi coating was evaluated based on high-temperature tensile properties at 650 ℃. The fracture morphologies were analyzed using SEM to reveal the fracture mechanisms of the NiCrBSi coating during high-temperature service. The results indicate that, compared with uncoated furnace tubes, the NiCrBSi coating enhances the high-temperature yield strength of the furnace tubes. However, with increasing heat-treatment temperature and prolonged duration, the yield strength of the coated tubes gradually decreases. At the same heat-treatment temperature, the high-temperature tensile strength of the coated furnace tubes initially decreases and then increases with prolonged holding time. When the holding time reaches 200 h, the high-temperature tensile strength of the coated furnace tubes reaches its lowest value at all heat-treatment temperatures. The evolution of the high-temperature tensile properties of the coated furnace tubes is primarily influenced by the high-temperature degradation of the material and microstructural changes in the coating material. As the heat-treatment temperature and holding time increase, the size of the precipitated phases (carboborides) and grains of the substrate metal increase significantly, which inevitably decrease the yield strength of the coated tubes. Furthermore, with an increase in the heating temperature and holding time, elements such as C and B in the NiCrBSi coating diffuse into the base material, exacerbating carbide precipitation near the material surface. This increases both the size and quantity of precipitates within the dimples at the fracture surface. This provides an elemental basis for the precipitation of carbides on the surface of the substrate material, increasing the quantity of surface carbides. Owing to their inherent brittleness, carbides act as nucleation sites and propagation paths for cracks. Second, during the long-term high-temperature exposure experiments, the surface of the NiCrBSi coating undergoes progressively increasing oxidation. A large amount of Si, Cr, and B elements diffuse toward the surface, forming an oxide film composed of SiO2, Cr2O3, and B2O3. During the tensile process, the oxide layer, owing to its brittle nature and lack of plastic deformation characteristics, reduces the mechanical properties of the coating and ultimately becomes a site for crack initiation. The results provide data support for the design of coatings resistant to high-temperature corrosion and erosion during the deep peak-shaving process of power generation units.