首页 | 本学科首页   官方微博 | 高级检索  
     

飞机座舱气动式压力调节系统稳定性仿真研究
引用本文:胡良谋,朱芳镇,焦强.飞机座舱气动式压力调节系统稳定性仿真研究[J].机床与液压,2021,49(20):150-153.
作者姓名:胡良谋  朱芳镇  焦强
作者单位:空军工程大学航空工程学院,陕西西安710038;中国航空综合技术研究所,北京100028;中国人民解放军94691部队,福建福州350007
基金项目:航空科学基金资助项目(20150796009)
摘    要:建立某型飞机座舱气动式压力调节系统工作在恒压调节区时的数学模型,并进行系统的稳定性和动态性能的仿真试验研究。结果表明:所提出的压力调节系统的稳定性和动态性能较好。分别分析气密座舱体积和控制腔体积对系统稳定性和动态性能的影响。研究结果为深入了解飞机座舱气动式压力调节系统的工作原理、工作过程、稳定性和动态性能提供了参考。

关 键 词:座舱气动式压力调节系统  稳定性  动态性能

Research on Stability Simulation of Cabin Pneumatic Pressure Control System for Aircraft
HU Liangmou,ZHU Fangzhen,JIAO Qiang.Research on Stability Simulation of Cabin Pneumatic Pressure Control System for Aircraft[J].Machine Tool & Hydraulics,2021,49(20):150-153.
Authors:HU Liangmou  ZHU Fangzhen  JIAO Qiang
Abstract:The mathematical model of a certain aircraft cabin pneumatic pressure control system working in invariable control area was established, and the stability and dynamic characteristic of the system was simulated. The results show that the stability and dynamic characteristic of the cabin pneumatic pressure control system are good. The influence of the cabin cubage and the control cavity cubage on stability and dynamic characteristic of the cabin pneumatic pressure control were studied respectively. The research results provide reference for understanding the working principle, working course, stability and dynamic characteristics of cabin pneumatic pressure control system.
Keywords:Cabin pneumatic pressure control system  Stability  Dynamic characteristic
本文献已被 万方数据 等数据库收录!
点击此处可从《机床与液压》浏览原始摘要信息
点击此处可从《机床与液压》下载全文
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号