中国机械工程 ›› 2024, Vol. 35 ›› Issue (04): 636-645,690.DOI: 10.3969/j.issn.1004-132X.2024.04.007

• 机械基础工程 • 上一篇    下一篇

基于摩擦热效应的刷式密封摩擦副匹配性实验研究

杨艺潇1;孙丹1;兰可心1;赵欢1;冯毓钟2;张杰一3,4   

  1. 1.沈阳航空航天大学航空发动机学院辽宁省航空宇航推进系统先进测试技术重点实验室,沈阳,110136
    2.中国航发贵州黎阳航空动力有限公司,贵阳,550081
    3.中国航空发动机集团有限公司沈阳发动机研究所,沈阳,110015
    4.中国航空发动机集团有限公司航空发动机动力传输航空科技重点实验室,沈阳,110015
  • 出版日期:2024-04-25 发布日期:2024-05-29
  • 通讯作者: 孙丹(通信作者),男,1981年生,教授、博士研究生导师。研究方向为航空发动机先进密封技术。E-mail:phd_sundan@163.com。
  • 作者简介:杨艺潇,男,1999年生,硕士研究生。研究方向为刷式密封摩擦磨损特性。E-mail:sau_yixiao_yang@163.com。
  • 基金资助:
    国家自然科学基金(52075346,52375195);辽宁省教育厅面上项目(LJKZ0179)

Experimental Study of Matching of Brush Seal Friction Pairs Based on Frictional Heating Effects

YANG Yixiao1;SUN Dan1;LAN Kexin1;ZHAO Huan1;FENG Yuzhong2;ZHANG Jieyi3,4   

  1. 1.Liaoning Key Lab of Advanced Test Technology for Aerospace Propulsion System,School of
    Aero-Engine,Shenyang Aerospace University,Shenyang,110136
    2.AECC Guizhou Liyang Aviation Power Company Limited,Guiyang,550081
    3.Shenyang Engine Research Institute,Aero Engine Corporation of China,Shenyang,110015
    4.Key Laboratory for Power Transmission of Aero Engine,Aero Engine Corporation of China,
    Shenyang,110115

  • Online:2024-04-25 Published:2024-05-29

摘要: 刷丝与转子涂层相互作用产生的摩擦热效应直接影响刷式密封的密封性能和使用寿命。分析了刷式密封摩擦副之间的摩擦热效应理论,设计搭建了刷式密封摩擦副摩擦热效应实验装置,设计加工了6种不同结构参数与刷丝材料的刷式密封实验件和4种不同涂层材料的摩擦转盘,实验研究了工况参数、结构参数以及不同摩擦副材料对刷式密封摩擦热效应的影响,通过对比分析刷式密封最高温度以及磨损前后摩擦副的磨损形貌及磨损量,获取了刷丝与转子涂层材料的匹配性关系。研究结果表明:刷式密封最高温度会随着摩擦时长的增加先迅速升高后趋于稳定,随着干涉量的增大而升高,干涉量由0.3 mm增大至0.4 mm,刷丝平均最高温升达39.96 ℃;最高温度随着刷丝束厚度的增加而升高,随着后挡板保护高度的增大而降低;当刷丝材料为钴基高温合金GH605时,最佳转子涂层材料为WC,当刷丝材料为镍基高温合金GH4169时,最佳转子涂层材料为ZrO2,此两种匹配材料能够在相同工况下产生较低的摩擦热量,且耐磨性能高于其他匹配材料。

关键词: 刷式密封, 摩擦热效应, 摩擦副, 匹配性, 干涉量

Abstract: The frictional heating effects caused by the interaction between brush seal wire and rotor coating directly affected the sealing performance and service life of brush seals. The theory of frictional heating effects between brush seal frictional pairs was analyzed. The experimental device of frictional heating effects between brush seal frictional pairs was designed and built. Six brush seal experimental parts with different structural parameters and brush wire materials and four frictional turntables with different coating materials were designed and processed. The effects of working condition parameters, structural parameters and different frictional pair materials on the frictional heating effects of brush seals were studied experimentally. By comparing and analyzing the maximum temperature of brush seals and the wear morphology and wear amount of frictional pairs before and after wear, the matching relationship between brush wire and rotor coating material was obtained. The results show that the maximum temperature of brush seals increases rapidly and then tends to be stable with the increase of friction time, and increases with the increase of interference. When the interference increases from 0.3 mm to 0.4 mm, the average maximum temperature of brush wires rises to 39.96 ℃. The maximum temperature increases with the increase of the brush thickness and decreases with the increase of the rear baffle protection height. When the brush wire material is cobaltbased superalloy GH605, the best rotor coating material is WC; when the brush wire material is nickelbased superalloy GH4169, the best rotor coating material is ZrO2.These two matching materials may produce lower friction heat under the same working conditions, and the wear resistance is higher than that of other matching materials.


Key words: brush seal, frictional heating effect, friction pair, matching, interference

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