V29 航天用液压元件与附件 标准查询与下载

AECMA PREN 3207-1996 航空航天系列.橡胶封口胶技术规范.第1版

This "Aerospace series" Standard has been drawn up under the responsibility of AECMA (The European Association of Aerospace Industries). It is published on yell0 w paper in three equivalent versions (English, French, German). It will be submitted as a draft European Standard to CEN (European Committee for Standardization) for formal vote.

Aerospace Series Rubber Compounds Technical Specification Edition 1

JIS W 2922:1996 飞行器.液压元件.认可元件用指示流体的标记

この規格は，航空機の油圧系統に使用される構成部品(配管，ホース及び継手を除く。)の現場における組立て又は試験作業中に，その構成部品に適正な作動油を容易に判別できるようにするための表示方式について規定する。この表示は，構成部品を航空機に取り付ける際の便を，意図したものではない。

Aircraft -- Hydraulic components -- Marking to indicate fluid for which component is approved

SAE AIR4994-1996 高压气动压缩机用于航空航天应用的用户指南

Gas compressors (air and other compressible fluids) have been used sporadically since the 1940's for various utility functions in aerospace applications. They have been used to provide power to gun purge and drive systems, engine or APU starters (recharge accumulators), reservoir pressurization, cockpit pressurization, braking systems, canopy seals, engine control divides, landing gear activation, and boosted flight controls. In current state-of-the-art aircraft, most pneumatic system power is extracted from a stage of compression in the turbo-jet engine. As more and more demands are put on new generation engines for fuel economy and performance there is an increasing need for a new source of pneumatic power. This document is intended to describe current state-of-the-art technology in compressors, define the limitations, discuss enhancements needed and attempt to predict the needs of the future

High Pressure Pneumatic Compressors Users Guide for Aerospace Applications

SAE HS-1417-1996 SAE 流体密封手册径向唇形密封件 1996 版 [取代：SAE HS J1417]

This handbook contains the latest information available on elastomeric radial lip seals including J 1901, Lip Force Measurement: Radial lip Seals. Also included is information on application considerations, seal design, material selection, inspection and testing, performance, and industry Recommended Practices

SAE Fluid Sealing Handbook Radial Lip Seals 1996 Edition [Superseded: SAE HS J1417]

DIN ISO 7319:1996 航空航天.流体系统.24度锥形公制联轴器界面 (ISO 7319:1992)

The document defines the geometry of the interface of removable 24?cone couplings for fluid systems in aircraft. The connection with the pipe of each one of the connecting elements may be of different design.

Aerospace - Fluid systems - Interface of 24° cone metric couplings (ISO 7319:1992)

DIN ISO 7320:1996 航空航天.流体系统用螺纹密封联轴器.尺寸 (ISO 7320:1992)

The document establishes a system for sealing the port connection of couplings used in the aerospace industry. It specifies dimensions to achieve interchangeability of the port connection, the fitting end and a seal. The seal may be a standard O-ring or a special ring.#,,#

Aerospace - Couplings, threaded and sealed, for fluid systems - Dimensions (ISO 7320:1992)

DIN ISO 6772:1996 航空航天.流体系统.液压软管、管道和连接组件的脉冲试验 (ISO 6772:1988)

This document specifies the requirements and the procedures for impulse testing of hose, tubing, and fitting assemblies for use in aerospace hydraulic systems. Requirements may apply, when appropriate, to components used in other aerospace fluid systems.

Aerospace - Fluid systems - Impulse testing of hydraulic hose, tubing and fitting assemblies (ISO 6772:1988)

DIN ISO 6773:1996 航空航天.流体系统.管道和配件的热冲击试验 (ISO 6773:1994)

The document provides an environmental test method for thermal shock testing of fluid system piping and fittings, excluding hose and hose assemblies.#,,#

Aerospace - Fluid systems - Thermal shock testing of piping and fittings (ISO 6773:1994)

DIN ISO 9634:1996 航空航天.流体系统.塑料保护帽和保护塞尺寸 (ISO 9634:1994)

Aerospace - Fluid systems - Dimensions of plastic protective caps and plugs (ISO 9634:1994)

SAE MA2005B-1995 24°锥形的可拆分公制航空液压系统管道配件用一般规格(ISO 7169标准)

This document specifies performance and quality requirements for the qualification and manufacturer of 24?cone fittings to ensure reliable performance in aircraft hydraulic systems. This document specifies baseline criteria for the design and manufacture of system fittings that are qualification tested on engines. This document covers fittings of temperature types and pressure classes specified in MA2001.

Tube Fittings, Aerospace Fluid Systems, Separable, for 24° Cone, General Specification, Metric (ISO 7169)

SAE AS4843-1995 用于流体连接的珠状饰配件

This SAE Aerospace Standard (AS) establishes the requirements for beaded fluid connection fittings (see Section 6) for use in all types of fluid systems. Fittings shall be furnished in the types and styles designated by the applicable AN or other engineering standard drawings. This specification is the same as MIL-F-5509 as applicable to beaded fittings except for updated materials and process specifications and industry coordinated general improvements. It is intended to serve as a procurement specification for the fittings described herein and in Section 6.

Fittings, Beaded, Fluid Connection

AECMA PREN 3545-005-1995 航空航天系列. 尾部密封和无密封塑料护套、锁紧装置、工作温度操作温度-55°C至175°C的矩形电接点.第005部分;固定护套装配用插头编码和附件系统

This draft is now available for public comment and your views and technical comments on it would be appreciated. If you have no specific comments to make hut find it generally acceptable it would be helpful if you would notify US accordingly. Suggestions entailing revision of the text should indicate the preferred wording. Please quote the relevant clause number against any comment.

Aerospace Series Connectors, Electrical, Rectangular, with Sealed and Non-Sealed Rear, Plastic Housing, Locking Device, Operating Temperatures - 55 Degrees C to 175 Degrees C Part 005 : Female Coding and Attachment System for Mounting on Free Housing (Pl

AECMA PREN 3545-007-1995 航空航天系列. 尾部密封和无密封塑料护套、锁紧装置、工作温度操作温度-55°C至175°C的矩形电接点.第007部分;电缆钳.产品标准

This standard is part of the series of EN metallic material standards for aerospace applications. The general organization of this series is described in EN 4258.

Aerospace Series Connectors, Electrical, Rectangular, with Sealed and Non-Sealed Rear, Plastic Housing, Locking Device, Operating Temperatures - 55 Degrees C to 175 Degrees C Part 007 : Cable Clamp Product Standard Edition P 1

AECMA PREN 3545-006-1995 航空航天系列. 尾部密封和无密封塑料护套、锁紧装置、工作温度操作温度-55°C至175°C的矩形电接点.第006部分;固定护套装配用插座编码和附件系统

This draft is now availabl for public comment and your views and t e c h n i c a l comments on it would be a p p r e c i a t e d . I f you have no s p e c i f i c comments t o make b u t f I n d it g e n e r a l l y a c c e p t a h l e it would be h e l p f u l I f you would n o t I f y us a c c o r d I n g l y . S u g g e s t I o n s e n t a I l I n g r e v I s I o n of t h e t e x t should I n d I c a t e t h e p r e f e r r e d wording. P l e a s e quote the r e l e v a n t c l a u s e number a g a I n s t any conFent

Aerospace Series Connectors, Electrical, Rectangular, with Sealed and Non-Sealed Rear, Plastic Housing, Locking Device, Operating Temperatures - 55 Degrees C to 175 Degrees C Part 006: Male Coding and Attachment System for Mounting on Fixed Housing (Rece

AECMA PREN 3545-004-1995 航空航天系列. 尾部密封和无密封塑料护套、锁紧装置、工作温度操作温度-55°C至175°C的矩形电接点.第004部分;带有插座触点的连接器.产品标准

This draft is now available for public comment and your views and technical comments on it would be appreciated. If you have no specific comments to make hut find it generally acceptable it would be helpful if you would notify US accordingly. Suggestions entailing revision of the text should indicate the preferred wording. Please quote the relevant clause number against any comment.

Aerospace Series Connectors, Electrical, Rectangular, with Sealed and Non-Sealed Rear, Plastic Housing, Locking Device, Operating Temperatures - 55 Degrees C to 175 Degrees C Part 004 : Connectors with Male Contacts Product Standard Edition P 1

NAVY MIL-V-24272 B (1)-1995 高压天然气减少阀组

This amendment forms a part of MILV 24272B(SH), dated 30 August 1985, and is approved for use by all Departments and Agencies of the Department of Defense.

VALVE MANIFOLDS, HIGH PRESSURE GAS REDUCING

SAE ARP4904-1994(R2008) 液压元件的计算机控制测试设备用性能指南

This SAE Aerospace Recommended Practice (ARP) establishes software capability guidelines forcomputer controlled test equipment, hereinafter referred to as automatic test equipment (ATE), for testing hydraulic components. A typical ATE system is shown in Figure 1. The items herein have been selected as potential features which may or may not be applicable to a particular application. This document does not address software development requirements, qualification procedures, or hardware design requirements, but encourages users to refer to existing documents, defined in 2.1.1, for guidance on such issues.

Capability Guidelines for Computer Controlled Test Equipment for Hydraulic Components

SAE AS1376D-1994 可变换尺寸,中心体部分,成型流体配件设计标准

ALTERNATE DIMENSIONS, CENTER BODY SECTION,SHAPE FLUID FITTING, DESIGN STANDARD.ALTERNATE DIMENSIONS, CENTER BODY SECTION,SHAPE FLUID FITTING, DESIGN STANDARD.ALTERNATE DIMENSIONS, CENTER BODY SECTION, SHAPE FLUID FITTING, DESIGN STANDARD FSC 4730

ALTERNATE DIMENSIONS, CENTER BODY SECTION, SHAPE FLUID FITTING, DESIGN STANDARD FSC 4730

SAE ARP1258B-1993 液压管接头的特殊柔性疲劳试验的质量要求

This SAE Aerospace Recommended Practice (ARP) establishes the method for qualification testing of tube joints and fitting attachments, using the flexure test method described in ARP1185. This qualification test method allows the determination of S-N type stress versus cycles or D-N type deflection versus cycles curves, as illustrated in AIR1418 as an alternate to flexure testing to a minimum endurance stress level.

Qualification of Hydraulic Tube Joints to Specified Flexure Fatigue Requirements

2M 60-1993 航空航天液压系统用的24°圆锥状可拆管配件规范

Specification for separable tube fittings, 24 cone, for aerospace fluid systems