机械科学与技术2017，Vol.36Issue(4)：653-656,4.DOI:10.13433/j.cnki.1003-8728.2017.0427
三环驱动轴对称矢量喷管喉道逆运动学建模
Inverse Kinematics Modeling for Throat Area of Axial-symmetric Vectoring Exhaust Nozzle Driving by Three Rings
李建鹏 1赵志刚 1李有德 1孟佳东1
作者信息
- 1. 兰州交通大学 机电工程学院,兰州 730070
- 折叠
摘要
Abstract
The axial-symmetric vectoring exhaust nozzle driving by three ringsis one of the convergent/divergent type nozzles.In this paper,the inverse kinematics modeling for throat area of axial-symmetric vectoring exhaust nozzle is given by using the relative rotation angle method.The three dimensional model for nozzle was built via CATIA software and its kinematics simulation was carried out via ADAMS,the computer simulation results showed that the mechanic design was reasonable and the kinematics modeling was effective,which provided an important reference for optimizing and controllingthe axial-symmetric vectoring exhaust nozzles driving by three rings.关键词
三环驱动轴对称矢量喷管/喉道面积/逆运动学建模/仿真Key words
axial-symmetric vectoring exhaust nozzles driving by three rings/throat area/inverse kinematics modelling/computer simulation分类
航空航天引用本文复制引用
李建鹏,赵志刚,李有德,孟佳东..三环驱动轴对称矢量喷管喉道逆运动学建模[J].机械科学与技术,2017,36(4):653-656,4.
