俱利锋,屈笑宇,雷鸣,寇宝智.电传飞机典型异常振动的诊断与处置技术研究[J].装备环境工程,2022,19(9):129-136. JU Li-feng,QU Xiao-yu,LEI Ming,KOU Bao-zhi.Diagnosis and Treatment Technology of Typical Abnormal Vibration of Fly-by-Wire Aircraft[J].Equipment Environmental Engineering,2022,19(9):129-136.
电传飞机典型异常振动的诊断与处置技术研究
Diagnosis and Treatment Technology of Typical Abnormal Vibration of Fly-by-Wire Aircraft
  
DOI:10.7643/issn.1672-9242.2022.09.019
中文关键词:  气动伺服弹性  颤振  振动  舵面  偏度  指令中图分类号:V217 文献标识码:A 文章编号:1672-9242(2022)09-0129-08
英文关键词:aeroservoelasticity  flutter  vibration  control surface  deflection  instruction
基金项目:
作者单位
俱利锋 中国飞行试验研究院飞机所,西安 710089 
屈笑宇 西安交通大学 电信学部,西安 710048 
雷鸣 中国飞行试验研究院飞机所,西安 710089 
寇宝智 中国飞行试验研究院飞机所,西安 710089 
AuthorInstitution
JU Li-feng Chinese Flight Test Establishment, Aircraft Flight Test Technology Institute, Xi'an 710089, China 
QU Xiao-yu Department of Telecommunications, Xi'an Jiaotong University, Xi'an 710048, China 
LEI Ming Chinese Flight Test Establishment, Aircraft Flight Test Technology Institute, Xi'an 710089, China 
KOU Bao-zhi Chinese Flight Test Establishment, Aircraft Flight Test Technology Institute, Xi'an 710089, China 
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中文摘要:
      目的 对电传飞机典型的异常振动问题进行研究,形成电传飞机异常振动的诊断和处置技术。方法 首先对气动伺服弹性问题的基本原理和气动伺服弹性失稳可能引发的危害进行简要的介绍。然后对某电传飞机试飞过程中出现的异常振动现象进行详细描述,通过不同类型数据的对比分析,对该异常振动问题进行准确定位和诊断,进而给出相应的应对措施。最后通过正式的飞行试验对处置措施的准确性进行验证。结果 经过对异常振动问题的处理与分析,明确了该异常振动发生的根本原因,通过处置措施的有效落实,已顺利完成该型机的颤振/ASE飞行试验工作。结论 通过本文的异常振动处置方法的研究,为以后类似问题的准确诊断和处置提供了有益的参考和借鉴。
英文摘要:
      The typical abnormal vibration of Fly-By-Wire aircraft is studied for the diagnosis and treatment technology. Firstly, the basic principle of aeroservoelasticity and the possible harm caused by aeroservoelasticity instability are introduced briefly. Then, the abnormal vibration phenomenon in the flight test of a Fly-By-Wire aircraft is described in detail. Through the comparative analysis on different types of data, the abnormal vibration is accurately located and diagnosed, and then the corresponding countermeasures are given. Finally, the accuracy of disposal measures is verified by the formal flight test. Through the treatment and analysis of the abnormal vibration in this paper, the root cause of the abnormal vibration is clarified. According to the effective implementation of the treatment measures proposed in this paper, the flutter/ASE flight test of this aircraft has been successfully completed. The research on abnormal vibration disposal method in this paper has produced useful reference for the accurate diagnosis and treatment of similar problems in the future.
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