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某型航空发动机轴承保持架异常磨损原因分析
引用本文:王威,杨玉龙,陈朝刚.某型航空发动机轴承保持架异常磨损原因分析[J].机械研究与应用,2014(6):171-172.
作者姓名:王威  杨玉龙  陈朝刚
作者单位:1. 海军驻沈阳地区发动机专业军事代表室,辽宁 沈阳,110043
2. 沈阳黎明航空发动机 集团 有限责任公司,辽宁 沈阳,110043
摘    要:某型航空发动机为我国第三代战机主要动力装置,在试车后检查时发现,该发动机轴承保持架兜孔横梁存在异常磨损的偏磨现象。为摸清故障原因,对其尺寸按新品出厂标准进行了再次测量,找出了异常磨损是由于加工时拉刀刃口相邻面垂直度不合格,导致兜孔横梁与端面垂直度偏大引起了异常磨损。

关 键 词:航空发动机  圆柱滚子轴承  失效分析  机械加工

Cause Analysis of Abnormal Wear of the Bearing Retainer in Aeroengine
WANG Wei,YANG Yu-long,CHEN Chao-gang.Cause Analysis of Abnormal Wear of the Bearing Retainer in Aeroengine[J].Mechanical Research & Application,2014(6):171-172.
Authors:WANG Wei  YANG Yu-long  CHEN Chao-gang
Affiliation:WANG Wei, YANG Yu-long , CHEN Chao-gang (1. Navy Stationing in Shenyang Military Representative Office on Engine, Shenyang Liaoning 110043, China; 2. Shengyang Liming Aero-Engine( Group ) CorpOration Ltd, Shenyang Liaoning 110043, China)
Abstract:A certain type of aeroengine is the main power plant of the third-generation fighter in China. Through commissioning inspection,we find that the beams of engine bearing retainer were abrased abnormally. In order to find out the causes of the malfunction,its size was measured again according to the factory standards,and finally it is found that the abnormal abrasion is due to the larger perpendicularity of the beam and the end face which is caused by disqualification of the perpendicularity between blade adjacent faces in the pulling process.
Keywords:aircraft engine  cylindrical roller bearing  failure analysis  machining
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