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反推装置操纵力动力学仿真与优化改进

刘鹏宇

测控技术2024,Vol.43Issue(12):66-75,10.
测控技术2024,Vol.43Issue(12):66-75,10.DOI:10.19708/j.ckjs.2024.12.302

反推装置操纵力动力学仿真与优化改进

Dynamic Simulation and Improvement Study of Thrust Reverser Control Force

刘鹏宇1

作者信息

  • 1. 中国航发成都发动机有限公司,四川成都 610500
  • 折叠

摘要

Abstract

The failure of control force and torque of a grab-type thrust reverser affects the flexibility of the thrust reverser and the deceleration effect on aircraft landing.The modelling object is simplified by studying the transmission characteristics of the control mechanism,an efficient dynamic simulation 3D model of the thrust reverser control mechanism is established,and the motion simulation results are verified,which can meet the needs of component motion visualisation and control dynamics research.The variation curve and upper limit of the control force and torque,the influence of friction and the influence of pulley and tie rod debugging are stud-ied by simulation.The research results provide research ideas and evaluation bases for solving the above prob-lems,and improvement measures such as changing the index of the control force to the reference value of 25 N and lengthening the tie rod-003 to reduce the control torque are proposed.

关键词

反推装置/操纵力/动力学仿真/改进措施

Key words

thrust reverser/control force/dynamic simulation/improvement measure

分类

航空航天

引用本文复制引用

刘鹏宇..反推装置操纵力动力学仿真与优化改进[J].测控技术,2024,43(12):66-75,10.

基金项目

四川省重大科技专项(2021ZDZX0002) (2021ZDZX0002)

测控技术

OACSTPCD

1000-8829

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