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飞机环控系统发动机动态引气地面试验设备总体设计方法

吴豪 郑永贵 刘猛 王浚

刘向群, 魏振忠, 张韧, 等 . 基于参数估计的航空直流电动机虚拟测试系统[J]. 北京航空航天大学学报, 2001, 27(5): 544-547.
引用本文: 吴豪,郑永贵,刘猛,等. 飞机环控系统发动机动态引气地面试验设备总体设计方法[J]. 北京航空航天大学学报,2025,51(2):573-583 doi: 10.13700/j.bh.1001-5965.2023.0014
LIU Xiang-qun, WEI Zhen-zhong, ZHANG Ren, et al. A Virtual Instrument System Based on Parameter IdentificationDeveloped to Test Permanent Magnet DC Motor[J]. Journal of Beijing University of Aeronautics and Astronautics, 2001, 27(5): 544-547. (in Chinese)
Citation: WU H,ZHENG Y G,LIU M,et al. Overall design method of ground test equipment for engine dynamic air bleed of aircraft environmental control system[J]. Journal of Beijing University of Aeronautics and Astronautics,2025,51(2):573-583 (in Chinese) doi: 10.13700/j.bh.1001-5965.2023.0014

飞机环控系统发动机动态引气地面试验设备总体设计方法

doi: 10.13700/j.bh.1001-5965.2023.0014
详细信息
    通讯作者:

    E-mail:liumeng@buaa.edu.cn

  • 中图分类号: V245

Overall design method of ground test equipment for engine dynamic air bleed of aircraft environmental control system

More Information
  • 摘要:

    飞机环控系统(ECS)在动态工作时的故障是困扰环控系统设计和改进的一大难题。传统ECS地面试验设备只具备稳态供气或小范围慢速动态供气的能力,难以复现ECS在空中快速剧烈动态引气的环境。为弥补环控系统动态试验能力的不足,建立了参数覆盖范围最大、动态指标最高的环控引气双发动态模拟试验台,可以为环控系统模拟不同发动机在不同工作状态下的动态引气环境。使用总阀调压、冷热掺混调温的方式实现温度压力联合调节,合理分配各环节阻力关系以减弱调压-调温过程的耦合;使用旁路加热器供热、换热器换热的方式保证温度调节的快速性;采用双阀联动控制保证压力调节的大范围和高精度,双流量计互补测量以保证稳态测量精度和动态测量速度;基于传统分布式控制系统建立反射内存卡快速交互网络,实现控制系统的快速响应,采用基于专家系统的查表比例积分微分(PID)算法提升控制器的控制效果。试验结果显示所设计试验台具备快速、大覆盖范围的动态调温调压能力。

     

  • 图 1  试验台供气压力/流量调节方法

    Figure 1.  Air supply pressure/flow regulation method of test bench

    图 2  试验台供气温度调节方法

    Figure 2.  Air supply temperature adjustment method of test bench

    图 3  试验台调压调温流程[15]

    Figure 3.  Pressure regulation and temperature adjustment process of test bench[15]

    图 4  冲压过程中的回流现象

    Figure 4.  Backflow phenomenon in stamping process

    图 5  试验台单路供气流程

    Figure 5.  Single-branch air supply of test bench

    图 6  线性阀门流量特性畸变

    Figure 6.  Distortion of flow characteristics of linear valve

    图 7  等百分比阀门流量特性曲线

    Figure 7.  Flow characteristics of equal percentage valve

    图 8  中压5级供气路的试验段入口供气管路

    Figure 8.  Air supply pipe at inlet of test section of medium-pressure 5-stage air supply circuit

    图 9  测控系统框架示意图

    Figure 9.  Schematic diagram of measurement and control system structure

    图 10  改进PID算法原理示意图

    Figure 10.  Schematic diagram of principle of improved PID algorithm

    图 11  试验台局部图1

    Figure 11.  Partial view of test bench (No. 1)

    图 12  试验台局部图2

    Figure 12.  Partial view of test bench (No. 2)

    图 13  高压9级引气路定斜率控制

    Figure 13.  Constant slope control of high-pressure 9-stage air bleed circuit

    图 14  外涵道引气路定斜率控制

    Figure 14.  Constant slope control of external ulvert air bleed circuit

    表  1  环控引气双发动态模拟试验台引气参数要求

    Table  1.   Air bleed parameter requirements of environmental control air bleed dual-engine dynamic simulation test bench

    供气环境 出口压力
    (绝压)/MPa
    压力变化率/
    (kPa·s−1
    可控制压力
    范围/MPa
    出口温度/℃ 加温变化率/
    (℃·s−1
    可控制温度
    范围/℃
    出口流量/
    (kg·h−1
    高压9级引气路 0.101~3.5 50~1000 0.2~3.5 20~650 5~90 40~650 0~8000
    中压5级引气路 0.101~2.5 50~800 0.2~2.5 20~500 5~90 40~500 0~8000
    低压外涵引气路 0.101~0.8 2~20 105~220 20~150 5~40 20~150 0~15000
    下载: 导出CSV
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出版历程
  • 收稿日期:  2023-01-11
  • 录用日期:  2023-03-13
  • 网络出版日期:  2023-03-24
  • 整期出版日期:  2025-02-28

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