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热喷涂技术:2021,13(3):11-15
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航空发动机叶片叶尖耐磨封严涂层技术及其发展
(1.中航沈飞民用飞机有限责任公司;2.矿冶科技集团有限公司)
Technologies and Development of Abrasive Coatingsfor Aeroengine Blade Tip
(1.AVIC SAC Commercial Aircraft Company LTD.;2.BGRIMM Technology Group)
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中文摘要: 航空发动机封严涂层体系是控制其转子和静止件间隙的主要措施, 其中叶片叶尖耐磨封严涂层可以使叶尖 在与机匣或外环块封严结构或涂层刮擦时得到保护, 并达到缝隙最小化的设计要求。 本文综述了国内外叶片叶尖 耐磨封严涂层的材料组成、 制备工艺、 应用及其优缺点, 简述了国内耐磨封严涂层技术现状及发展要求, 提出了 针对新型高性能航空发动机的发展迫切需要加强对具有耐磨颗粒凸出于粘结金属相的高性能叶尖耐磨封严涂层、 钛合金和镍基单晶高温合金叶片叶尖涂覆工艺研究的建议, 以进一步提高航空发动机封严结构体系的可靠性, 延 长使用寿命, 有效提高发动机燃油效率。
Abstract:A seal coating system for an aeroengine is a major measure to control the clearance between rotary blades and a corresponding stationary casing liner. Abrasive coating applied to the tip of a blade is intended to protect it from wear damage as a result of its scraping against a seal liner or coating for a casing or a shroud component, thereby minimize the blade tip clearance. The materials, preparation, merit and disadvantage, applications of abrasive coatings for the blade tip were described in this paper. The state of the art of the abrasive coatings and their development requirements in China were also briefed. A variety of technologies are urgently demanded, namely novel abrasive coatings for advanced high performance aeroengines, abrasive coatings and their optimizations for titanium alloy and nickel base single crystal superalloy blades, as well as test and evaluation technologies such as that for the abradable matching property between the blade tip coating and corresponding abradable liner or coatings under service conditions, aimed to improve the reliability and lifetime of seal structure systems for aeroengines
文章编号:     中图分类号:TG174.4    文献标志码:
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引用文本:
闫峰,刘建明,黄凌峰,章德铭.航空发动机叶片叶尖耐磨封严涂层技术及其发展[J].热喷涂技术,2021,13(3):11-15.
YanFeng,LiuJianming,HuangLingfeng,ZhangDeming.Technologies and Development of Abrasive Coatingsfor Aeroengine Blade Tip[J].Thermal Spray Technology,2021,13(3):11-15.

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