V21 管件、卡箍、密封件 标准查询与下载

SAE AS1733E-2009 带螺纹的套环型II型管端固定腔刚性管联接体

Body, Coupling, Rigid, Fixed Cavity, Threaded, Ferrule Type Tube Ends, Type II

SAE AS1732E-2009 带螺纹的套环型管端I型固定腔刚性管联接体

Body, Coupling, Rigid, Fixed Cavity, Threaded, Ferrule Type Tube Ends, Type I

SAE AS4623D-2009 航空器液压系统重型275℉、3000psi对位芳族增强聚四氟乙烯软管组件

This document defines the requirements for heavy-duty polytetrafluoroethylene (PTFE) lined, para-aramid reinforced, hose assembly suitable for use in 275 °F, 3000 psi aircraft systems where rapid rate pulsing and torsional/longitudinal flexing may occur in addition to normal hydraulic system loading. Size -16 and -20 are limited to +225 °F service.

Hose Assembly, Polytetrafluoroethylene, Para-Aramid Reinforced, 3000 psi, 275 °F, Heavy-Duty, Aircraft Hydraulic Systems

SAE AS1582E-2009 3000 psi外螺纹非扩口式完整焊接环适配器配件

Fitting, Adapter, External Thread Flareless to Integral Weld Ring 3000 psi

BS ISO 27996:2009 航空航天液体系统.弹性体密封件.存储和保存期

Aerospace fluid systems - Elastomer seals - Storage and shelf life

SANS 814:2009 普通飞机软管夹(螺杆传动型)

Covers the requirements for the materials, dimensions, construction, strength, finish, packing and marking of worm-drive type hose clips for use in aircraft and for general purposes. Sections on sampling and methods of test are included.

General purpose and aircraft hose clips (Worm-drive Type)

SAE AMS6372L-2009 0.95Cr 0.20Mo(0.33-0.38C)(SAE 4135)机械钢管

This specification covers an aircraft-quality, low-alloy steel in the form of mechanical tubing. This tubing has been used typically for parts, 0.75 inch (19 mm) and under in section thickness at time of heat treatment, requiring a through-hardening steel capable of developing hardness as high as 40 HRC when properly hardened and tempered and for parts of greater thickness but requiring proportionately lower hardness, but usage is not limited to such applications.

Steel Tubing, Mechanical, 0.95Cr 0.20Mo (0.33-0.38C) (SAE 4135)

SAE AS5174E-2009 扩口式组合及异径配件

Fitting, Union and Reducer, Flared

BS EN 3631:2008 航空航天系列.90°弯度法兰安装的液体配件.0.8mm厚度管用O型密封圈密封

The purpose of this standard is to define the characteristics of the fluid fittings, flanged, 90° elbowed, sealing by O-ring, for 0,8 mm thick tubes.

Aerospace series - Fluid fittings, flanged, 90° elbowed - Sealing by O-ring for 0,8 mm thick tubes

SAE AS4862A-2009 六角头外部螺纹管插头配件

Fitting, Plug, Pipe, External Thread, Hex Head

SAE AS1710D-2009 带套圈的螺纹型可变空腔柔性燃料耦合件

This SAE Aerospace Standard (AS) defines the requirements for a threaded flexible coupling assembly, which utilizes ferrules or machined tube end fittings to join tubing and components in aircraft fuel and fuel vent or other systems. This coupling assembly is designed for use from -65 to +200 °F and at 125 psig peak working pressure, and the coupling assembly may be used in other fluid systems when requirements are within the limits.

Coupling, Fuel, Flexible, Variable Cavity, Threaded Type With Ferrules

SAE J1273-2009 液压软管组件推荐实施规程

SAE J 1273 provides guidelines for selection, routing, fabrication, installation, replacement, maintenance, and storage of hose and hose assemblies for hydraulic fluid-power systems. Many of these SAE Recommended Practices also may be suitable for other hoses and systems.

Recommended Practices for Hydraulic Hose Assemblies

SAE AS6013A-2009 3000 psi,275 ℉直通对直通的非扩口钛管接头用对位芳纶增强聚四氟乙烯软管组件

Hose Assembly, Polytetrafluoroethylene, Para Aramid Reinforced, 275°F, 3000 PSI, Flareless, Titanium Fittings, Straight to Straight

SAE AS5804A-2009 3000 psi液压分支轴向陷型内螺纹非扩口三通组装配件

Fitting Assembly, Tee, Female Flareless and Axially Swaged on the Run, Axially Swaged on the Branch, Hydraulic, 3000 PSI

SAE AS4687D-2009 固定螺母减压器非扩口和短非扩口90°弯头配件组装

Fitting Assembly, Elbow, 90°, Flareless and Short Flareless, Reducer, Retained Nut

SAE AS4684C-2009 固定螺母非扩口和短非扩口45°弯头配件

Fitting Assembly, Elbow, 45°, Flareless and Short Flareless, Reducer, Retained Nut

SAE AS603B-2009 液压软管,管道和配件的脉冲测试

This SAE Aerospace Standard (AS) establishes the requirements and procedures for impulse testing of hose, tubing, and fitting assemblies for use in aerospace hydraulic systems of 8000 psi nominal operating pressure or less. It also refers to standard impulse test equipment to be used in conducting these impulse tests.

Impulse Testing of Hydraulic Hose, Tubing, and Fitting Assemblies

ISO 27996:2009 航空航天液体系统.弹性体密封件.存储和保存期

Aerospace fluid systems - Elastomer seals - Storage and shelf life

SAE AS28775A-2008 预成型MS28775 O形密封环包装

Packing, Preformed MS28775 O-Ring

SAE AS568C-2008 O形环的航空航天尺寸标准

This Aerospace Standard specifies the inside diameters, cross-sections, tolerances, and size identification codes (dash numbers) for O-rings used in sealing applications and for straight thread tube fitting boss gaskets. The dimensions and tolerances specified in this standard are suitable for any elastomeric material provided that suitable tooling is available. This standard is intended to be used in the preparation of Company, Military, or other Standard Drawings for O-Rings. Each dash number, which should be appended to an appropriate Drawing or Standard number, identifies one nominal size O-Ring only. No attempt is made in this AS to indicate which of the O-Ring sizes listed under this system should be included in any particular Standard Drawing. Its only purpose is to standardize O-Ring sizes and dimensional tolerances and the means of identifying them dimensionally.

Aerospace Size Standard for O-Rings