Investigation of high-speed abrasion behavior of an abradable seal rubber in aero-engine fan application

被引:20
|
作者
Xuan, Haijun [1 ,2 ]
Zhang, Na [1 ,2 ]
Lu, Bin [1 ,2 ]
Cheng, Lijun [3 ]
Hong, Weirong [3 ]
机构
[1] Zhejiang Univ, Coll Energy Engn, High Speed Rotating Machinery Lab, Hangzhou 310027, Zhejiang, Peoples R China
[2] Collaborat Innovat Ctr Adv Aeroengine, Beijing 100083, Peoples R China
[3] Aviat Ind Corp China, Beijing Inst Aeronaut Mat, Beijing 100095, Peoples R China
关键词
Abradability; Abrasion test equipment; Aero-engine; Silicone seal rubber; Wear mechanism; WEAR BEHAVIOR; FRICTION; COATINGS;
D O I
10.1016/j.cja.2017.02.019
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
Abradable seal rubber has been widely used in aero-engine fans to improve their efficiency by reducing the clearance between rotating and stationary components. To investigate the high-speed scraping behavior between a vulcanized silicone rubber and a Ti-6Al-4V fan blade and evaluate the abradable performance of seal rubber, abrasion tests were conducted at a blade tip velocity of 50-300 m/s with an incursion rate of 100 mu m/s. The influences of the blade tip velocity on the wear mechanism and interaction forces were specially analyzed. It is shown that abrasive wear and pattern wear are the predominant wear mechanisms, and pattern wear can be seen as the emergence and propagation of cracks. With an increase of the blade tip velocity, both of the final incursion depth and wear mass loss of seal rubber exhibit growth trends. The gradual changes of rubbing forces with an increase of rubbing time are the characteristic of abrasive wear, and force curves with unstable mutations are a reflection of pattern wear. At a constant incursion rate of 100 mu m/s, the maximum values of interaction forces decrease first and then grow with an increase of the blade tip velocity, and the blade tip velocity of 150 m/s becomes the cut-off point between abrasive wear and pattern wear. (C) 2017 Production and hosting by Elsevier Ltd. on behalf of Chinese Society of Aeronautics and Astronautics.
引用
收藏
页码:1615 / 1623
页数:9
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