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飞机座舱气动式压力调节系统稳定性仿真研究
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航空科学基金资助项目(20150796009)


Research on Stability Simulation of Cabin Pneumatic Pressure Control System for Aircraft
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    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。

    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.

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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.
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

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  • 在线发布日期: 2023-04-07
  • 出版日期: 2021-10-28