49.080 航空航天用流体系统和零部件 标准查询与下载

SAE AS5550B-2013 5080 PSI超细牙螺纹非扩口到端口适配器环状锁定配件总装

Fitting Assembly, Ring Locked, Adapter, Flareless to Port, Extra Fine Threads, 5080 PSI

SAE ARP1383C-2013 航空航天.液压元件的脉冲测试

This SAE Aerospace Recommended Practice (ARP) defines impulse test procedures that are recommended for hydraulic components.

Aerospace - Impulse Testing of Hydraulic Components

SAE MA2119B-2013 端口连接环锁定到60度非扩口管末端公制接头组件

Adapter Assembly, Port Connection Ring Locked to 60 degree Flareless Tube End, Metric

SAE AS5008A-2013 外部锻造活接头的液压配件

Fitting, Union, External Swage, Hydraulic

SAE AS4459B-2013 额定压力3000磅/平方英寸(21 000 kPa)外部锻造流体系统管道配件

This SAE Aerospace Standard (AS) establishes the requirements for externally swaged tube-fitting assemblies used in aircraft fluid systems in the following pressure classes: B (1500 psi or 10 500 Kpa), and D (3000 psi or 21 000 kPa), and in temperature types I (-65 to 160 degree F or -55 to 70 degree C), and II (-65 to 275 degree F or -55 to 135 degree C) of AS2001. This specificaiton covers a common Cres, titanium, and aluminum fittings that may be used for a range of operating pressures up to 3000 psi with different tubing materials and tubing wall thicknesses and is assembled with the same tooling in accordance with AS 5902.

Fittings, Tube, Fluid System 3000 psig (21 000 kPa) Rated Pressure, Externally Swaged, Specification for

SAE ARP6255-2013 用于燃气发动机油润滑能力测定的航空工业润滑剂摩擦学评估者(ALTE)方法

Employing ""ball-on-cylinder"" philosophy, a non-rotating steel ball is held in a vertically mounted chuck and using an applied load is forced against an axially mounted steel cylinder. The test cylinder is rotated at a fixed speed while being partially immersed in a lubricant reservoir. This maintains the cylinder in a wet condition and continuously transports a lubricating film of test fluid to the ball and cylinder interface. The diameter of the wear scar generated on the test ball is used as a measure of the fluid's lubricating properties. The apparatus can be used, by adjusting the operating conditions, to reproduce two different wear mechanisms; mild

Aviation Lubricant Tribology Evaluator (ALTE) Method to Determine the Lubricating Capability of Gas Turbine Lubricants

SAE AS5960B-2013 航空器液压系统用400℉(204℃)、5080 psi(35000 kPa)金属编织物加固的聚四氟乙烯软管组件

This document defines the requirements for polytetrafluoroethylene (PTFE) lined, metallic braid reinforced, hose assembly suitable for use in 400 °F (204 °C), 5080 psi (35 000 kPa) aircraft hydraulic systems. NOTE: The SI metric units defined herein are soft conversion units.

Hose Assembly, Polytetrafluoroethylene, Metallic Braid Reinforced, 5080 psi (35 000 kPa), 400 °F (204 °C), Aircraft Hydraulic Systems

SAE AIR1243C-2013 帽材密封用抗不密封设计原则

This SAE Aerospace Information Report (AIR) provides information on anti blow-by design practice for cap-strip seals. Suggestions for piston cap strip seal sidewall notch design and other anti blow-by design details are also described. It also includes information on two key investigations based on the XC-142 as part of the text and as Appendix A. The purpose of this document is to provide adequate information to the designer so that the problem will not reoccur.

Anti Blow-By Design Practice for Cap Strip Seals

SAE AS4680B-2013 支管台用短非扩口和非扩口减径管联合配件

Fitting, Union, Reducer, Short Flareless and Flareless to Boss

SAE AS4694B-2013 短非扩口盖,空心端,盖形螺母装配总成

Scope is unavailable.

Fitting Assembly, Cap, Hollow End, Acorn, Short Flareless

SAE AS4691F-2013 运行中的留用螺母减径管短非扩口和非扩口三通装配总成

Fitting Assembly, Tee, Flareless and Short Flareless, Reducer, Retained Nut on Run

SAE ARP4493A-2013 航空航天.直接驱动伺服器

This SAE Aerospace Recommended Practice (ARP) is intended as a guide to aid in the specification and testing of Direct Drive Servovalves, but does not include the associated electronic controller. The recommendations contained in this ARP are primarily confined to the input and output characteristics of Direct Drive Servovalves (DDV). The only exception to this approach involves the definition and specification of chip shear force, which is not typically measurable by nondestructive external testing. The information presented should be useful in standardizing the terminology, the specification of physical and performance parameters, and the test procedures

Aerospace - Direct Drive Servovalves

SAE AS4677B-2013 运行中的舱壁支管台强侧短非扩口三通配件

Fitting, Tee, Bulkhead, on Run, Boss on Side, Short Flareless

SAE AS4681B-2013 短非扩口和非扩口减径管/扩充器舱壁联合配件

Fitting, Union, Reducer/Expander Bulkhead, Flareless and Short Flareless

SAE AS4676B-2013 运行中的舱壁和支管台短非扩口三通配件

Fitting, Tee, Bulkhead and Boss on Run, Short Flareless

SAE AS1003H-2013 运行中的舱壁标准和减径管非扩口三通配件

Fitting, Tee, Standard and Reducer, Bulkhead on Run, Flareless

ASD-STAN PREN 4552-2013 航空航天系列 管接头 37°，球形，耐热钢 直管接头，焊接端 英制系列（P 2 版）

Aerospace series Pipe coupling 37°, spherical, in heat resisting steel Straight nipples, welded end Inch series (Edition P 2)

KS W 1112-2012 飞机垫片

Gasket sheet for aircraft

SAE AS604E-2012 液压重量级400℉,3000 psi,金属加固,聚四氟乙烯软管接头

This Aerospace Standard (AS) defines the requirements for a heavy braid polytetrafluoroethylene (PTFE) lined, metallic reinforced, hose assembly suitable for use in high temperature, 400 °F, high pressure, 3000 psi, aircraft hydraulic fluid systems, also for use in pneumatic systems which allow some gaseous diffusion through the PTFE wall. The -20 size operating temperature is limited to 275 °F maximum.

Hose Assembly, Polytetrafluoroethylene, Metallic Reinforced, 3000 psi, 400 °F, Heavyweight, Hydraulic

SAE AS614C-2012 液压和气动,重型,400℉,4000 psi金属加强,聚四氟乙烯软管接头

This SAE Aerospace Standards (AS) defines the requirements for heavy duty polytetrafluoroethylene (PTFE) lined, metallic reinforced, hose assemblies suitable for use in high temperature, high pressure, 4000 psi, aircraft and missile hydraulic fluid systems.

Hose Assembly, Polytetrafluoroethylene, Metallic Reinforced, 4000 psi, 400°F, Heavy Duty, Hydraulic and Pneumatic