共找到 2370 条与 航空航天用流体系统和零部件 相关的标准,共 158 页
This European Standard specifies the characteristics of pressure plugs for pipe couplings 8°30', in titanium alloy, for aerospace applications.
Aerospace series - Pipe coupling 8°30' in titanium alloy - Pressure plugs
The purpose of this European Standard is to specify the dimensions and tolerances for orbital-welding fittings, intended for stainless steel fluid pipes to EN 3717.
Aerospace series - Weld lip - Geometrical configuration
This European Standard specifies the characteristics of the fluid fittings, flanged, 90° elbowed, sealing by O-ring, for 0,8 mm thick tubes. NOTE Flanged fitting installation hole and assembly, see EN 3633 and TR 3634.
Aerospace series - Fluid fittings@ flanged@ 90��lbowed - Sealing by O-ring for 0@8 mm thick tubes
This European Standard specifies the characteristics of equipped blind ferrules for pipe couplings 8°30', in titanium alloy, for aerospace applications.
Aerospace series - Pipe coupling 8°30' in titanium alloy - Equipped blind ferrules
This European Standard specifies the characteristics of swivel nuts for inch series pipe couplings, 37°, in heat resisting steel, for aerospace applications. Nominal pressure: Class D in accordance with ISO 6771.
Aerospace series - Pipe coupling@ 37��in heat resisting steel - Swivel nuts - Inch series
Aerospace series - Pipe coupling, in heat resisting steel or in heat resisting nickel alloy - Coupling end, welded - Design configuration - Inch series
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FITTING, UNION AND REDUCER, FLARELESS
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FITTING, ADAPTER, FLARELESS TO FLARED
Aerospace series - Pipe coupling, in heat resisting steel or in heat resisting nickel alloy - Coupling end, welded - Design configuration - Inch series; German and English version EN 4549:2014
本标准规定了民用飞机液压系统的试验要求和方法。 本标准适用于工作压力在21MPa~56MPa之间、工作温度在-55℃~232℃之间的飞机液压系统。
Test requirements for commercial aircraft hydraulic systems
本标准规定了液压脉冲试验台的关键部件组成、要求和操作方法。 本标准适用于液压软管组件、硬管、盘旋管、接头、作动筒、阀、压力容器及类似液压系统部件的标准液压脉冲试验台的研制。
General requirement for hydraulic impulse test stand
本标准规定了民用飞机气动系统附件的技术要求和验证要求等。 本标准适用于民用飞机气动系统附件的设计、制造、试验和验收。
General requirements for pneumatic system components of civil aircraft
本标准规定了民用飞机燃油系统附件压降试验的一般要求,试验方法的分类和选取、试验步骤及试验结果处理等。 本标准适用于工作介质为燃油的民用飞机燃油系统附件的压降试验。
Pressure drop test methods for fuel system components of civil aircraft
本标准规定了民用飞机燃油系统附件耐久性试验的一般要求、试验项目和试验程序、试验方法、试验数据录取和处理、试验结果评定及试验报告的编写等。 本标准适用于民用飞机燃油系统各附件的耐久性试验。
Endurance test requirements for fuel system accessories of civil aircraft
本标准规定了民用飞机气动系统的设计要求(包括设计依据、设计准则、一般要求、详细要求、设计程序及设计验证)和安装要求。 本标准适用于民用飞机气动系统设计和安装。
Design and installation requirements for pneumatic system of civil aircraft
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PLUG - PIPE, CADMIUM PLATED, STEEL UNS G87400, COUNTERSUNK HEX
This SAE Aerospace Standard (AS) defines the requirements for polytetrafluoroethylene (PTFE) lined, metallic reinforced, hose assemblies suitable for use in aerospace hydraulic, fuel and lubricating oil systems at temperatures between -67 °F and 450 °F for Class I assemblies, -67 °F and 275 °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 additio
Hose Assembly, Polytetrafluoroethylene, Metallic Reinforced, Up to 1500 psi and 450 °F, Hydraulic and Pneumatic
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FITTING ASSY, TEE, REDUCER, SWIVEL ON SIDE, REDUCED BODY, FLARELESS
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FITTING ASSY, ELBOW, REDUCER, 45°, SWIVEL, REDUCED BODY, FLARELESS
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FITTING ASSY, TEE, REDUCER, SWIVEL ON RUN, REDUCED BODY, FLARELESS
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