| 注册
首页|期刊导航|北京航空航天大学学报|民机飞机液压刹车系统动态特性参数灵敏度分析方法

民机飞机液压刹车系统动态特性参数灵敏度分析方法

孟庆堂 马新起 杨鹏 白璐 王壮壮 刘晓超 焦宗夏

北京航空航天大学学报2026,Vol.52Issue(8):2708-2719,12.
✕
北京航空航天大学学报2026,Vol.52Issue(8):2708-2719,12.DOI:10.13700/j.bh.1001-5965.2025.0690

民机飞机液压刹车系统动态特性参数灵敏度分析方法

Sensitivity analysis method for dynamic characteristics parameters of hydraulic braking system in civil aircraft

孟庆堂 1马新起 2杨鹏 3白璐 3王壮壮 2刘晓超 2焦宗夏2

作者信息

  • 1. 北京航空航天大学 自动化科学与电气工程学院,北京 100191||中国商用飞机有限责任公司上海飞机设计研究院,上海 201210
  • 2. 北京航空航天大学 自动化科学与电气工程学院,北京 100191
  • 3. 中国商用飞机有限责任公司上海飞机设计研究院,上海 201210
  • 折叠

摘要

Abstract

A thorough theoretical and experimental investigation of the dynamic properties of the aircraft hydraulic braking system was carried out in order to improve the braking performance and dependability of civil aircraft under challenging runway circumstances.A detailed nonlinear mathematical model of the hydraulic braking system was established,incorporating key components such as the brake control valve and hydraulic pipelines.Based on this model,a parameter sensitivity analysis method was introduced to address the system's multi-parameter problem.The analysis quantitatively determined that the most important factors affecting the dynamic response characteristics of the system were the actuator piston's effective area,the actuator return spring's stiffness,and the flow-pressure coefficient of the valve.Finally,a hardware-in-the-loop experimental platform for the aircraft braking system was constructed to carry out experimental validation of the dynamic response.The results clarified the key factors affecting the braking system's dynamic response,confirmed the correctness of the theoretical analysis,and provided a clear direction for the design and optimization of hydraulic braking systems for civil aircraft.

关键词

飞机刹车系统/液压动态特性/数学模型/参数灵敏度分析/半实物实验

Key words

aircraft braking system/hydraulic dynamic characteristics/mathematical model/parameter sensitivity analysis/hardware-in-the-loop experiment

分类

航空航天

引用本文复制引用

孟庆堂,马新起,杨鹏,白璐,王壮壮,刘晓超,焦宗夏..民机飞机液压刹车系统动态特性参数灵敏度分析方法[J].北京航空航天大学学报,2026,52(8):2708-2719,12.

基金项目

国家自然科学基金(52505050) (52505050)

中国博士后科学基金(2025T181117,2024M764076) (2025T181117,2024M764076)

流体动力基础件与机电系统全国重点实验室开放基金(GZKF-202428) National Natural Science Foundation of China(52505050) (GZKF-202428)

China Postdoctoral Science Foundation(2025T181117,2024M764076) (2025T181117,2024M764076)

Open Foundation of the State Key Laboratory of Fluid Power and Mechatronic Systems(GZKF-202428) (GZKF-202428)

北京航空航天大学学报

1001-5965

访问量0
|
下载量0
段落导航相关论文