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

SAE AIR 4922-1996(R2008) 发布历史

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.

SAE AIR 4922-1996(R2008)由美国机动车工程师协会 US-SAE 发布于 1996-10-01。

SAE AIR 4922-1996(R2008) 在中国标准分类中归属于: V38 液压、冷气系统及其附件。

SAE AIR 4922-1996(R2008) 发布之时，引用了标准

• SAE ARP 4752 

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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

无

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.