用户名: 密码: 登 录   个人中心   系统维护   用户注册  联系我们
当前位置 >首页 > 标准信息

全文阅读 全文下载 章节阅读

基本信息

AIR1873
Guide to Limited Engine Monitoring Systems for Aircraft Gas Turbine Engines
Guide to Limited Engine Monitoring Systems for Aircraft Gas Turbine Engines
2012-03-01
有效
【范围】 This Aerospace Information Report (AIR) describes a Limited Engine Monitoring System that can be used by the flight crew or the maintenance staff, or both, to monitor the health of gas turbine engines in aircraft. This AIR considers monitoring of gas path performance and mechanical parameters, and systems such as low cycle fatigue counters and engine history recorders. It also considers typical measurement system accuracies and the!r impact. This AIR is intended as a technical guide. It is not intended to be used as a legal document or standard. AIR 1873 supplements ARP 1587 Aircraft Gas Turbine Engi ne Monitoring System Guide.strRefField
【与前一版的变化】

被引文件

Aircraft Gas Turbine Engine Health Management System Guide
Software Interfaces for Ground-Based Monitoring Systems
Guide to Life Usage Monitoring and Parts Management for Aircraft Gas Turbine Engines
(R) Guidelines for Integrating Typical Engine Health Management Functions Within Aircraft Systems
Aircraft Gas Turbine Engine Health Management System Guide
Software Interfaces for Ground-Based Monitoring Systems
Guide to Life Usage Monitoring and Parts Management for Aircraft Gas Turbine Engines
(R) Guidelines for Integrating Typical Engine Health Management Functions Within Aircraft Systems

相关标准

A Guide for the Selection of Quick-Disconnect Couplings for Aerospace Fluid Systems
BAROMETRY FOR ALTIMETER CALIBRATION
Aircraft Accessory Drag Torque During Engine Starts
Numeral, Letter and Symbol Dimensions for Aircraft Instrument Displays
Some Factors Affecting Visibility of Aircraft Navigation and Anticollision Lights
Electromagnetic Interference on Aircraft From Jet Engine Charging
Bibliography of References Pertaining to The Effects of Oxygen on Ignition and Combustion of Materials
Performance of Low Pressure Ratio Ejectors for Engine Nacelle Cooling
Construction and Calibration of Parallel Plate Transmission Line for Electromagnetic Interference Susceptibility Testing
Installation of Liquid Oxygen Systems in Civil Aircraft

包含图表

formula 1
formula 2
formula 3
PARAMETER DEFINITION
formula 4
formula 5
formula 6
formula 7
Typical Trend Data E
Typical Measurement
Steady State Criteri
Example of Engine Pe
Sample Trend Plot
Example of EGT-Diver
Example of EGT Margi
EMS Flow Chart Diagr

标准反馈


  • 问题类型:
    反    馈: