北京航空航天大学学报 ›› 2018, Vol. 44 ›› Issue (8): 1603-1608.doi: 10.13700/j.bh.1001-5965.2017.0748

• 论文 • 上一篇    下一篇

三床型机载制氧系统控制设计与实验验证

蒋东升1,2, 卜雪琴1, 林贵平1, 孙兵1, 黄俊1, 方玲2, 赵宏韬1,2   

  1. 1. 北京航空航天大学 航空科学与工程学院, 北京 100083;
    2. 航空工业合肥江航飞机装备有限公司, 合肥 230051
  • 收稿日期:2017-12-04 修回日期:2018-01-08 出版日期:2018-08-20 发布日期:2018-08-29
  • 通讯作者: 卜雪琴 E-mail:buxueqin@buaa.edu.cn
  • 作者简介:蒋东升,男,博士研究生。主要研究方向:机载分子筛制氧、电子氧调器;卜雪琴,女,博士,副教授,硕士生导师。主要研究方向:飞行器环境控制、飞机防除冰。

Control design and experimental verification of three-bed onboard oxygen generation system

JIANG Dongsheng1,2, BU Xueqin1, LIN Guiping1, SUN Bing1, HUANG Jun1, FANG Ling2, ZHAO Hongtao1,2   

  1. 1. School of Aeronautic Science and Engineering, Beijing University of Aeronautics and Astronautics, Beijing 100083, China;
    2. AVIC Hefei Jianghang Aircraft Equipment Co., Ltd., Hefei 230051, China
  • Received:2017-12-04 Revised:2018-01-08 Online:2018-08-20 Published:2018-08-29

摘要: 为解决两床型机载制氧系统在实际应用过程中出现的输出压力波动大及低空氧浓度偏高等问题,需研制与开发三床型机载制氧系统。为此,依据系统控制逻辑,采用电磁阀驱动电控气动阀循环工作的控制模式,开展了三床型机载制氧系统的控制设计,提出了高低空分段调节循环周期的控制方法,并在不同输入压力、流量条件下,对三床型机载制氧系统进行了循环周期实验,探索了产品气氧浓度随循环周期时间的变化规律。研究结果表明:当采用高空循环周期为6 s,低空循环周期为9 s,高低空分段高度为3.5 km等控制参数时,系统控制设计可适用于三床型机载制氧系统,并满足三床型机载制氧系统控制设计的需求。

关键词: 三床, 机载制氧系统, 系统控制, 循环周期, 实验

Abstract: Two-bed onboard oxygen generation system is facing the problem of large pressure fluctuation of output gas and high oxygen concentration at low altitude during the practical application process. In order to solve these problems, three-bed onboard oxygen generation system needs to be developed. According to the system control logic, the control mode that the electronic controlled pneumatic servo valve worked circularly was adopted. The control design of three-bed onboard oxygen generation system has been proposed. The control method of segmented regulation was proposed, in which different cycle time was applied depending on the altitude. Under different input pressure and flow conditions, the experiments of the three-bed onboard oxygen generation system were performed to investigate the influence of the cycle time on the oxygen concentration of product gas. The study results show that when the cycle time for low altitude and high altitude is determined to be 9 s and 6 s, respectively, and the segmented altitude is determined to be 3.5 km, the system control design is suitable for the three-bed onboard oxygen generation system, and meets the requirements for the control design of three-bed oxygen generation system.

Key words: three-bed, onboard oxygen generation system, system control, cycle period, experiment

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