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涡轮起动机中斜撑离合器的瞬态冲击与楔合特性研究

卢敏 陈利强 李政民卿

航空科学技术2024,Vol.35Issue(3):70-76,7.
航空科学技术2024,Vol.35Issue(3):70-76,7.DOI:10.19452/j.issn1007-5453.2024.03.008

涡轮起动机中斜撑离合器的瞬态冲击与楔合特性研究

Analysis on the Transient Impact and Wedging Performance of the Sprag Clutch in the Turbine Starter

卢敏 1陈利强 2李政民卿1

作者信息

  • 1. 南京航空航天大学,江苏 南京 210016
  • 2. 航空工业金城南京机电液压工程研究中心,江苏 南京 211106
  • 折叠

摘要

Abstract

Extending the steady wedging to transient impact is an important component of top-down design for sprag clutch.Based on the theory of mechanical dynamics,the impact differential equation of the sprag clutch is established by correlating the load and response characteristics of the input and output parts,and the dynamic principle and general law are revealed that contained in the process of the clutch running from transient wedging to stable transmission.On this basis,the comprehensive stress analysis model of the transmission shafts is deduced.Moreover,the inspection method of the overall performance using the contact stress,comprehensive stress and gripping angle,etc is proposed.Finally,taking a common sprag clutch component as an example,the short-term load conditions in the turbo starter environment are studied from both theoretical calculation and simulation analysis,which verifies the principle and analysis model proposed in this paper,so they are of great significant for this kind of clutch in design and verification analysis.

关键词

涡轮起动机/斜撑离合器/瞬态冲击/正向设计/综合应力

Key words

turbine starter/sprag clutch/transient impact/top-down design/comprehensive stress

分类

机械制造

引用本文复制引用

卢敏,陈利强,李政民卿..涡轮起动机中斜撑离合器的瞬态冲击与楔合特性研究[J].航空科学技术,2024,35(3):70-76,7.

基金项目

航空科学基金(202028052007) Aeronautical Science Foundation of China(202028052007) (202028052007)

航空科学技术

1007-5453

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