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基于FBG的飞机起落架载荷测试技术研究
引用本文:褚园园,吴越,黄鹏宇,陈诗,闫光.基于FBG的飞机起落架载荷测试技术研究[J].半导体光电,2022,43(1):182-187.
作者姓名:褚园园  吴越  黄鹏宇  陈诗  闫光
作者单位:北京信息科技大学光电测试技术及仪器教育部重点实验室,北京100192;北京信息科技大学光纤传感与系统北京实验室,北京100016,北京信息科技大学光纤传感与系统北京实验室,北京100016
基金项目:国家自然科学基金项目(51675053).*通信作者:闫光E-mail:584851848@qq.com
摘    要:针对某型飞机起落架三向载荷的监测需求,提出了一种采用光纤光栅(Fiber Bragg Grating,FBG)传感和多元线性回归相结合的起落架载荷测试方法。通过对起落架进行有限元仿真分析,得到了不同载荷作用下起落架的应变分布,根据应变分布特征确定FBG应变传感器的布片位置,形成应变传感网络。在此基础上,进行了主起落架地面静态载荷标定试验,并通过多元线性回归的方法形成应变-载荷计算方程组,最后对载荷计算方程组进行了验证性试验。研究结果表明,基于FBG的起落架载荷测试方法能有效反算起落架的三向载荷,反算得到的载荷与施加载荷的相对误差在5%以内,满足实际工程应用需求。

关 键 词:飞机起落架  光纤光栅传感器  载荷测试  标定方程
收稿时间:2021/8/25 0:00:00

Research on Load Testing Technology of Aircraft Landing Gear Based on FBG
CHU Yuanyuan,WU Yue,HUANG Pengyu,CHEN Shi,YAN Guang.Research on Load Testing Technology of Aircraft Landing Gear Based on FBG[J].Semiconductor Optoelectronics,2022,43(1):182-187.
Authors:CHU Yuanyuan  WU Yue  HUANG Pengyu  CHEN Shi  YAN Guang
Affiliation:Key Laboratory of Optoelectronic Measurement Technology and Instrument of the Ministry of Education, Beijing Information Science & Technology University, Beijing 100192, CHN;Beijing Laboratory of Optical Fiber Sensing and System, Beijing Information Science and Technology University, Beijing 100016, CHN
Abstract:In order to meet the monitoring requirements of three-way load of a certain aircraft landing gear, a landing gear load test method was proposed based on fiber Bragg grating (FBG) sensing and multiple linear regression. The strain distribution of the landing gear under different loads was obtained with finite element analysis software. According to the characteristics of strain distribution, the position of the FBG strain sensor was determined, and the strain sensing network was formed. On this basis, the ground static load calibration experiment of the main landing gear was carried out, and the strain-load calculation equations were formed by multiple linear regression method. Finally, the load calculation equations were verified by experiments. The research results show that the method based on fiber Bragg grating can effectively back-calculate the three-way load of landing gear, and the relative error between the back-calculated load and the applied load is within 5%, which meets the actual engineering requirements.
Keywords:aircraft landing gear  fiber Bragg grating sensor  load test  calibration equations
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