SAE AS8054-2005

AIRBORNE ENGINE VIBRATION MONITORING (EVM) SYSTEM, GUIDELINES FOR PERFORMANCE STANDARD FOR

被代替

SAE AS8054-2005 发布历史

This SAE Aerospace Standard (AS) provides guidelines for the functional, performance, qualification and acceptance testing, and documentation requirements for the components of an airborne engine vibration monitoring (EVM) system which is intended for use as a turbojet engine rotor unbalance indicating system, per FAR 25.1305 (D)(3) on transport category airplanes. For the purpose of this document, this means a system which can provide real-time flight deck displays of engine vibration caused by rotor unbalance, throughout the flight envelope, which are suitable for: a Relating to engine vibration limits (where such limits are specified) b Use in ice shedding procedures c Helping the flight crew to determine which engine has the higher level of vibration, following an engine damage event. As a minimum, the functional capability for such a system shall include the ability to compute and display vibration levels specifically related to the rotational speed(s) of the engine rotor(s).

SAE AS8054-2005由美国机动车工程师协会 US-SAE 发布于 2005-10-28。

SAE AS8054-2005的历代版本如下：

• 2012年 SAE AS8054A-2012
• 2005年 SAE AS8054-2005
• 1996年 SAE AS8054-1996 航空发动机振动监测(EVM)系统性能标准指南

非常抱歉，我们暂时无法提供预览，您可以试试： 免费下载 SAE AS8054-2005 前三页，或者稍后再访问。

注意： 点击下载后，生成下载文件时间比较长，请耐心等待......

标准号

SAE AS8054-2005

发布

2005年

发布单位

美国机动车工程师协会

替代标准

SAE AS8054A-2012

当前最新

SAE AS8054A-2012

 

 

适用范围

This SAE Aerospace Standard (AS) provides guidelines for the functional, performance, qualification and acceptance testing, and documentation requirements for the components of an airborne engine vibration monitoring (EVM) system which is intended for use as a turbojet engine rotor unbalance indicating system, per FAR 25.1305 (D)(3) on transport category airplanes. For the purpose of this document, this means a system which can provide real-time flight deck displays of engine vibration caused by rotor unbalance, throughout the flight envelope, which are suitable for: a Relating to engine vibration limits (where such limits are specified) b Use in ice shedding procedures c Helping the flight crew to determine which engine has the higher level of vibration, following an engine damage event. As a minimum, the functional capability for such a system shall include the ability to compute and display vibration levels specifically related to the rotational speed(s) of the engine rotor(s).

SAE AS8054-2005相似标准