SAE AIR 4922-1996(R2008)
主飞行控制液压驱动系统接口定义

Primary Flight Control Hydraulic Actuation System Interface Definition


 

 

非常抱歉,我们暂时无法提供预览,您可以试试: 免费下载 SAE AIR 4922-1996(R2008) 前三页,或者稍后再访问。

如果您需要购买此标准的全文,请联系:

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 AIR 4922-1996(R2008)
发布日期
1996年10月01日
实施日期
废止日期
中国标准分类号
V38
发布单位
US-SAE
引用标准
Part 25"Airworthiness Standards:Transport Category Airplanes" Code of Federal Regulations,Aeronautics and Space. MIL-A-8870 MIL-H-5440 MIL-H-83282 SAE ARP 1383 SAE ARP 4386 SAE ARP 4752 SAE AIR 4253 SAE AIR 1657 MIL-E-5400
适用范围
This SAE Aerospace Information Report (AIR) provides a description of the interfaces and their requirements for generic and specific hydraulic actuation systems used in the flight control systems of manned aircraft.Included are the basic control system characteristics and functional requirements, and the essential interfaces (structural, mechanical, hydraulic power, control input, status monitoring, and environment). Major design issues, requirements, and other considerations are presented and discussed.




Copyright ©2007-2022 ANTPEDIA, All Rights Reserved
京ICP备07018254号 京公网安备1101085018 电信与信息服务业务经营许可证:京ICP证110310号