航空发动机主要参数检测电路设计思路
항공발동궤주요삼수검측전로설계사로
The Conception of Aero-Engine Main Parameter Detection Circuit Design
  • 万方数据
    科技视界 과기시계
    Science&Technology Vision
    2014年 9期 5-5,30 ,共2页

    赵鹏%蔡忠春%谢斌

    조붕%채충춘%사빈

    转速检测%温度检测%位置检测 轉速檢測%溫度檢測%位置檢測
    전속검측%온도검측%위치검측
    Speed detection%Temperature detection%Position detection
    航空检测设备对于航空发动机的维修保障至关重要。本文通过理论分析与外场实践相结合针对航空发动机的转速、涡轮后燃气温度、位置等主要参数的检测电路提出设计思路。
    항공검측설비대우항공발동궤적유수보장지관중요。본문통과이론분석여외장실천상결합침대항공발동궤적전속、와륜후연기온도、위치등주요삼수적검측전로제출설계사로。
    Air testing equipment for aircraft engine maintenance support is crucial. In this paper , through theoretical analysis and field practice for aircraft engine speed , gas temperature after the exit of turbo ,position and so on detection circuit of the main parameters ,such as design idea is put forward .
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