某型直升机滑油压力表指示误差的诊断与排除
DOI:
CSTR:
作者:
作者单位:

1.海军航空工程学院青岛校区 青岛 266041;2.海军航空工程学院航空训练基地 青岛 266109

作者简介:

通讯作者:

中图分类号:

TN72TH89

基金项目:


Oil pressure indicator misdirection diagnosis and removal of a helicopter
Author:
Affiliation:

1.Naval Aeronautical Engineering Institute Qingdao Branch, Qingdao 266041, China; 2.Aeronautical Training Center of Naval Aeronautical Engineering Institute, Qingdao 266109, China

Fund Project:

  • 摘要
  • |
  • 图/表
  • |
  • 访问统计
  • |
  • 参考文献
  • |
  • 相似文献
  • |
  • 引证文献
  • |
  • 资源附件
  • |
  • 文章评论
    摘要:

    滑油压力是飞机润滑系统工作状态的重要参数。针对某型直升机换装新型飞参信号适配器后出现机上减速器滑油压力表数值显示偏大的故障,从系统内部结构原理出发,综合现代电路测试技术和正确的分析思路,指出故障现象是由内部运算放大电路设计缺陷导致过压损坏引起的。经过机理分析、故障复现与确认后,参考相关电路设计文献后对运算放大电路重新进行了设计,并进行了实验及实装可靠性验证,排除了故障现象,避免了盲目的分解检查,确保了飞行安全。

    Abstract:

    Oil pressure is a valuable parameter indicating condition of aircraft lubrication system problem of reducer oil pressure indicator’s value is larger was proposed after installating a new flight data signal adapter and it was pointed out that it was caused by design detect of internal amplifier circuit which leaded to overvoltage damage.The conclusion was made from internal system structure theory,combining modern electronic testing technology and correct analysis method.Fault phenomenon was removed by redesign of amplifier circuit after mechanism analysis, fault reproduction and validation,refering to relevant literature on the circuit design and experimental and mounting reliability verification.Blind decomposition inspection was avoided,and flying safety was guaranteed.

    参考文献
    相似文献
    引证文献
引用本文

邸亚洲,申江江.某型直升机滑油压力表指示误差的诊断与排除[J].国外电子测量技术,2016,35(9):41-44

复制
分享
文章指标
  • 点击次数:
  • 下载次数:
  • HTML阅读次数:
  • 引用次数:
历史
  • 收稿日期:
  • 最后修改日期:
  • 录用日期:
  • 在线发布日期: 2016-10-20
  • 出版日期:
文章二维码