Research of the Aero Engine Accessory Gearbox Structure Design Method

doi:10.16578/j.issn.1004.2539.2017.03.041

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Research of the Aero Engine Accessory Gearbox Structure Design Method

更新时间：2022-10-20

- Research of the Aero Engine Accessory Gearbox Structure Design Method
- Vol. 41, Issue 3, Pages: 211-216(2017)
- 作者机构：
  
  1. 中国航发沈阳发动机设计研究所
  2. 中国航发航空发动机动力传输航空科技重点实验室
- 作者简介：
- 基金信息：
- DOI：10.16578/j.issn.1004.2539.2017.03.041
  CLC：
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[1]郭梅,陈聪慧,胡兴海,侯明曦.航空发动机附件机匣结构设计方法研究[J].机械传动,2017,41(03):211-216.

Research of the Aero Engine Accessory Gearbox Structure Design Method. [J]. 41(3):211-216(2017)
[1]郭梅,陈聪慧,胡兴海,侯明曦.航空发动机附件机匣结构设计方法研究[J].机械传动,2017,41(03):211-216. DOI： 10.16578/j.issn.1004.2539.2017.03.041.

Research of the Aero Engine Accessory Gearbox Structure Design Method. [J]. 41(3):211-216(2017) DOI： 10.16578/j.issn.1004.2539.2017.03.041.

摘要

对具有代表性的航空发动机附件机匣结构设计方法进行研究,分析了附件机匣内壳体、齿轮、轴承等重要零部件结构特点,总结各部件长期使用中出现过的故障和问题,提出工程应用优化的结构使用建议,为高可靠性附件机匣设计提供参考。

Abstract

The research of the representative aero engine accessory gearbox structure design method and the analysis of the structure characteristics of the important components including the casings,gears and bearings are accomplished. The failures and questions occurred in the accessory gearbox components used for a long term are summarized,the applying suggestion of engineering application optimized structures are proposed,which contributes to the reference of high reliability accessory gearbox design.

关键词

航空发动机附件机匣结构形式高可靠性

Keywords

Aero engineAccessory gearboxStructural formHigh reliability

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Key Laboratory for Power Transmission Technology of Aero-Engine,Aero Engine

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