共找到 2302 条与 管件、卡箍、密封件 相关的标准,共 154 页
Aerospace series. Pipe coupling, 37
Aerospace series. Pipe coupling 8
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GASKET - 37° FLARED TUBE FITTING, NICKEL, AMS5553
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GASKET - 37° FLARED TUBE FITTING, COPPER, AMS4500
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PADS, OIL INLET AND OUTLET, TYPES I, II & III - FOR AIRPLANE CONNECTIONS AIRCRAFT ENGINES
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
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GASKET - COPPER, CADMIUM PLATED, TUBE CONNECTION
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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ELBOW, TUBE - 45°, BULKHEAD, FLARELESS TUBE UNIVERSAL TO FLARED TUBE
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ELBOW, TUBE - 90°, BULKHEAD, FLARELESS TUBE UNIVERSAL TO FLARED TUBE
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ADAPTER, FLARELESS TUBE, BULKHEAD AND UNIVERSAL TO FLARED TUBE
Aerospace series. Pipe coupling, in heat resisting steel or in heat resisting nickel alloy. Coupling end, welded. Design configuration. Inch series
This document establishes standard gland dimensions for low pressure static radial O-ring seal applications and provides recommendations for modifying these glands in special applications. No provisions are made in this document for anti-extrusion devices.
Gland Design, Elastomeric O-Ring Seals, Static Radial and Face 800 psi Maximum Service
This SAE Aerospace Standard (AS) describes the procedures for the flammability testing of aircraft firewall sealants in accordance with the requirements of FAR Part 25 Sections 25.865, 25.867, 25.1191, and 25.1193. This test method is intended to determine the capability of sealant materials to control the passage of and effects from fire.
Test Method for Aerospace Firewall Sealant Flame Penetration
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TUBING, FLARED, STANDARD DIMENSIONS FOR, DESIGN STANDARD
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BUSHING, SLEEVE FLANGED, PRESS FIT, REAM TYPE
This specification covers a tetrafluoroethylene/propylene rubber (FEPM) in the form of molded rings.
Rings, Sealing, Tetrafluoroethylene/Propylene Rubber (Fepm) Hydraulic Fluid and Synthetic Oil Resistance 70 to 80
This specification covers a tetrafluoroethylene/propylene rubber (FEPM) in the form of molded rings.
Rings, Sealing, Tetrafluoroethylene/Propylene Rubber (Fepm) Hydraulic Fluid and Synthetic Oil Resistant 85 to 95
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