共找到 252 条与 发动机辅助系统及其附件 相关的标准,共 17 页
Propeller Shaft Ends - Flanged Small Aircraft Engine
Propeller Shaft Ends - Flanged Small Aircraft Engine
Magnetos. Flange mounting and drive.
Armoured spark plugs for piston engines.
Armoured ignition cable ends for piston engined aircraft.
Starters for piston engines in aircraft. Fixing and drive on engine side.
Hub, Flanged - Spline Type Wood Propeller No. 10, No. 20
Hub, Flanged - Spline Type Wood Propeller No. 10, No. 20
Cones, Front, Propeller Hub
Cones, Front, Propeller Hub
This Aerospace Standard (AS) covers the requirements for polytetrafluoroethylene (PTFE) hose assemblies for use in aerospace hydraulic fuel, and lubricating oil systems at temperatures between -67 degrees F and 450 degrees F for Class I assemblies, -67 degrees F and 275 degrees F for Class II assemblies, and at nominal pressures up to 1500 psi. The hose assemblies are also suitable for use within the same temperature and pressure limitations in aerospace pneumatic systems where some gaseous diffusion through the wall of the PTFE liner can be tolerated. The use of these hose assemblies in pneumatic storage systems is not recommended. In addition, installations in which the limits specified herein are exceeded, or in which the application is not covered specifically by this standard, for example oxygen, shall be subject to the approval of the purchaser.
Nomenclature-Engine Cooling Fan (Inactive for New Design After August 9, 1973)
为了适应整体油箱及有密封和疲劳要求的铆接技术的科研和生产的需要,经整体油箱采用自封铆接,特制订本文件,作为各单位编制自封铆接生产说明书和工艺规程的主要依据。
Integral fuel tank self-sealing riveting (trial)
Specification for flow regulators for liquid oxygen kerosene engines
Management requirements for conventional liquid propellant safety protective equipment
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