SAE AIR 1083B-1994
军用飞机的机载液压和控制系统的生存能力

Airborne Hydraulic and Control System Survivability for Military Aircraft

SAE AIR 1083B-1994 发布历史

This SAE Aerospace Information Report (AIR) provides the hydraulic system designer with the various design options and techniques currently available to enhance the survivability of hydraulic systems. A comprehensive knowledge of the hostile environment to which the air vehicle will be exposed will form the basis upon which the overall design philosophy is formulated. The designer should strive to achieve at the absolute minimum acceptable flying quality level to complete the operational mission for which the aircraft is designed; i.e., the aircraft can be controlled and the mission terminated safely, including landing. This AIR will attempt to address the following threats: a. typical small arms fire (5,56, 7.62, 12.7 and 14.5 mm AP); b. cannon (20, 30, and 40 mm API/HEI); c. NBC/EMI/EMP/beamed particle; and d. chemical/biological. Protection against missiles is beyond the scope of this AIR. Except for electronic counter-measures or evasive maneuvers, no practice technology exists which allows a hydraulic system to survive a direct hit by a missile or large caliber anti-aircraft projectile. The AIR addresses the following major topics: a. design concepts and architecture; b. design implementation; c. subsystem mechanization; and d. component design. This document provides the fluid power design engineer with information and design considerations to enhance the airborne hydraulic and control system survivability under combat conditions.

SAE AIR 1083B-1994由美国机动车工程师协会 US-SAE 发布于 1994-06-01。

SAE AIR 1083B-1994 在中国标准分类中归属于: V38 液压、冷气系统及其附件，在国际标准分类中归属于: 49.080 航空航天用流体系统和零部件,49.090 机上设备和仪器。

SAE AIR 1083B-1994的历代版本如下：

• 1994年06月01日 SAE AIR 1083B-1994 军用飞机的机载液压和控制系统的生存能力

SAE AIR 1083B-1994 军用飞机的机载液压和控制系统的生存能力 于 2012-04-11 变更为 SAE AIR 1083C-2012 军用飞机的机载液压和控制系统的生存能力。

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标准号

SAE AIR 1083B-1994

发布日期

1994年06月01日

实施日期

废止日期

无

中国标准分类号

V38

国际标准分类号

49.080;49.090

发布单位

US-SAE

代替标准

SAE AIR 1083C-2012

适用范围

This SAE Aerospace Information Report (AIR) provides the hydraulic system designer with the various design options and techniques currently available to enhance the survivability of hydraulic systems. A comprehensive knowledge of the hostile environment to which the air vehicle will be exposed will form the basis upon which the overall design philosophy is formulated. The designer should strive to achieve at the absolute minimum acceptable flying quality level to complete the operational mission for which the aircraft is designed; i.e., the aircraft can be controlled and the mission terminated safely, including landing. This AIR will attempt to address the following threats: a. typical small arms fire (5,56, 7.62, 12.7 and 14.5 mm AP); b. cannon (20, 30, and 40 mm API/HEI); c. NBC/EMI/EMP/beamed particle; and d. chemical/biological. Protection against missiles is beyond the scope of this AIR. Except for electronic counter-measures or evasive maneuvers, no practice technology exists which allows a hydraulic system to survive a direct hit by a missile or large caliber anti-aircraft projectile. The AIR addresses the following major topics: a. design concepts and architecture; b. design implementation; c. subsystem mechanization; and d. component design. This document provides the fluid power design engineer with information and design considerations to enhance the airborne hydraulic and control system survivability under combat conditions.