引用本文:
【打印本页】   【HTML】   【下载PDF全文】   View/Add Comment  【EndNote】   【RefMan】   【BibTex】
←前一篇|后一篇→ 过刊浏览    高级检索
本文已被:浏览 3481次   下载 2457 本文二维码信息
码上扫一扫!
分享到: 微信 更多
封严涂层可磨耗性测试用高温超高速可磨耗试验装置
张娜1,2, 宣海军1,2, 卢斌1,2, 沈婕3, 洪伟荣1
1.浙江大学 能源工程学院, 杭州 310027;2.先进航空发动机协同创新中心, 北京 100083;3.北京矿冶研究总院 金属材料研究所, 北京 100160
摘要:
为评价航空发动机气路密封中封严涂层材料在极端工况下的可磨耗性能,自主研制了一套模拟涂层与转子部件之间摩擦磨损行为的高温超高速可磨耗试验装置。采用大功率交流电机经由增速设备驱动主轴和试验轮盘-叶片结构高速稳定运转;采用高精密XY双向进给平台带动涂层试样进行径向和轴向进给,实现与高速旋转叶片的碰磨;通过超音速火焰加热涂层试样模拟其高温工况;高速碰磨产生的碰磨力、冲击加速度、摩擦热分别通过三向测力仪、加速度传感器、红外测温仪进行测量,并由高速数据采集系统进行高频采集、存储和分析。试验装置可实现叶尖线速度20~450 m/s、径向和轴向进给速率2~2 000 μm/s、最高加热温度1 200 ℃的磨耗试验,试验过程稳定、结果可靠。
关键词:  可磨耗试验  试验装置  封严涂层  可磨耗性  航空发动机
DOI:10.11933/j.issn.1007-9289.20161127001
分类号:V263.14;TG115.58
基金项目:中央高校基本科研业务费(2013XZZX005);国家高技术研究发展计划(863项目)(2012AA03A512)
High-temperature and High-speed Abadable Tester for Abradability Test of Seal Coatings
ZHANG Na1,2, XUAN Hai-jun1,2, LU Bin1,2, SHEN Jie3, HONG Wei-rong1
1.College of Energy Engineering, Zhejiang University, Hangzhou 310027;2.Collaborative Innovation Center for Advanced Aero-engine, Beijing 100083;3.Institute of Metallic Materials, Beijing General Research Institute of Mining and Metallurgy, Beijing 100160
Abstract:
To evaluate the abradability of gas seal coating materials under extreme conditions, a high-temperature and high-speed abradable tester was developed, which can be used to simulate the high-speed rubbing behavior between seal coatings and rotating components in aero-engines. The simulated disk and blade were able to run stably at high speed connected with a shaft driven by an AC motor with high power and a gear increaser. The feeding movement of the coating sample in radial and axial directions was completed by a XY feeding platform with high precision to simulate the rubbing interaction with the high-speed rotating blade. The coating sample was heated by a supersonic flame to simulate the high temperature environment. Rubbing forces, impact acceleration and friction heat were measured using the multicomponent dynamometer, acceleration sensor and infrared thermometer and the data was collected and analyzed through a high-speed data acquisition system. Test results show that abrasion tests can be conducted stably using this tester with reliable results when the blade tip velocity varied from 20 to 450 m/s, incursion rate from 2 to 2 000 μm/s, and heating temperature from RT to 1 200 ℃.
Key words:  abrasion test  test equipment  seal coating  abradability  aero-engine