Design and characteristics of reverse direct-acting high-pressure reducing valve for pneumatic actuator

被引：0
|
作者：
Liu Y. [1 ]
Wang X. [1 ]
Qin X. [1 ]
Wang H. [1 ]
Chen Q. [1 ]
Zhao S. [2 ]
机构：
[1] Key Laboratory of Pressure Systems and Safety, East China University of Science and Technology, Ministry of Education, Shanghai
[2] Shanghai Spaceflight Precision Machinery Institute, Shanghai
来源：
Beijing Hangkong Hangtian Daxue Xuebao/Journal of Beijing University of Aeronautics and Astronautics | 2022年 / 48卷 / 07期
关键词：
AMESim; characteristic analysis; design method; pneumatic actuator; pressure reducing valve;
D O I：
10.13700/j.bh.1001-5965.2021.0292
中图分类号：
学科分类号：
摘要：
Pneumatic actuator is the key component of the flight attitude control system for air-defense missile, directly influences flying stability and attitude control ability. Missile-borne high-pressure gas provides power for pneumatic actuator through pressure reduction, which can reduce the space occupied by the pneumatic system and increase missile range by carrying more gas. For a particular type of missile, a reverse non-balanced direct-acting high-pressure reducing valve with conical clack was designed. Mathematical models of thermodynamic and static analysis were built for the valve and the design & check software were developed. The simulation models with steady and unsteady inlet pressure were built based on AMESim, and the characteristics of pressure, flow rate and spool displacement were analyzed. Results show that the pressure reducing valve has good pressure and flow characteristics under design parameters, and the theoretical calculation and simulation results agree well. © 2022 Beijing University of Aeronautics and Astronautics (BUAA). All rights reserved.
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页码：1164 / 1173
页数：9
相关论文
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