V29 航天用液压元件与附件 标准查询与下载

KS W ISO 8574:2009 航空航天.液压系统管路安装.弯管的合格试验

이 표준은 항공우주 유압 시스템에서 사용되는 곡관의 충격 피로 강도를 분류하고 결정하기 위

Aerospace－Hydraulic system tubing－Qualification tests for bent tubes

SAE AS5169A-2009 舱门插头和泄放阀配件

Fitting, Port Plug and Bleeder

SAE AS5230A-2009 非扩口式组合及异径配件

Fitting, Union and Reducer, Flareless

SAE AS5232A-2009 非扩口端异径适配器配件

Fitting, Adapter, Reducer, Port to Flareless

SAE AS8791B-2009 聚四氟乙烯(PTFE)树脂的液压和气动固定器(支承环）

This specification and part standard covers polytetrafluoroethylene (PTFE) resin material and the dimensional requirements for retainers (back-up rings) previously covered by SAE AS 8791 and SAE AS 8791/1 which superseded MIL-R-8791 and MIL-R-8791/1. The retainers are intended for use in hydraulic and pneumatic system components as anti-extrusion devices in conjunctionwith packings and O-rings.

Hydraulic and Pneumatic Retainers (Back-Up Rings), Polytetrafluoroethylene (PTFE) Resin

SAE AIR1228A-2009 标准脉冲发送机设备和操作

This SAE Aerospace Information Report (AIR) establishes the specifications and descriptions of the critical componentsand operational guidelines for the standard hydraulic impulse machine for testing hydraulic hose assemblies, tubing, coils,fittings and similar fluid system components.This revision to the AIR1228 provides a description of a system that meets the requirements for specifications including:AS603, AS4265, and ARP1383. This impulse system utilizes closed loop servo control with specifically generatedcommand signal waveforms.Data accuracy and integrity are emphasized in this revision. Knowing the uncertainty of the pressure measurement isimportant whether using a resonator tube system, as described in the original release of this document, or a closed-loopsystems as described in this release. The accuracy of the data measurement system and consistency of the pressurewaveform are fundamental to test validity, regardless of the system type. This is discussed in more detail in Section 5.The standard impulse test system is established for the following purposes:A. As referee in the event of conflicting data from two or more nonstandard impulse machines. Such a referee systemmight be built by an impartial testing activity.B. A design guide for future test systems being built by manufacturers and users, or the upgrading of present systems.C. A design guide for higher pressure test systems or special purpose machines being designed.It is not the intention of this document to obsolete present resonator type machines. The specification for the resonatortype machine is available in the original release of this document.A simple block diagram of the revised system is shown in Figure 1.

(R) Standard Impulse Machine Equipment and Operation

SAE ARP4553A-2008 液压自移动式航空蓄能器

This SAE Aerospace Recommended Practice (ARP) is intended to provide design and qualification requirements for self-displacing hydraulic accumulators. These requirements are intended to be included in the Producrement Specification for the accumulator. Those requirements identified by the use of "shall" are considered to be essential requirements; those requirements identified by the use of "should" are considered to be optional requirements for inclusion in the Specificaiton at the discretion of the Purchaser. In addition, test methods for production acceptance and qualification purposes are provided. The accumulator is intended for use in military aerospace hydraulic systems with rated pressures of up to 8000 psi (55,158 kPa) and of the following types as specified in SAE AS 5440: Type I: -65 to +160 °F (-54 to +71 °C) fluid temperature; Type II: -65 to +275 °F (-54 to +135 °C) fluid temperature. The accumulator is also inteded for commercial aerospace and helicopter hydraulic systems.

Aerospace Accumulator, Hydraulic, Self-Displacing

QJ 1142A-2008 气体单向阀通用规范

General specification for gas check valves

QJ 3305-2008 导弹（运载火箭）阀门制造通用要求

General requirements for missile (launch vehicle) valve manufacturing

QJ 1214A-2008 气体安全阀通用规范

General specification for gas safety valves

QJ 1112A-2008 手动截止阀通用规范

General Specifications for Manual Globe Valves

QJ 1143A-2008 导弹（运载火箭）用气体减压阀通用规范

General specifications for gas pressure relief valves for missiles (launch vehicles)

SAE AS85720A-2008 动态梁密封、高压、可拆液压系统管配件的通用规范

This specification covers the design requirements and test procedures for separable beam seal fittings which include end fittings (see 2.4.2), connectors (see 2.4.3), and boss fittings for use in aerospace fluid systems. Design requirements are for Class 5000 and 8000 in titanium, and corrosion resistant steel (CRES)

Fittings, Tube, Fluid Systems, Separable, High Pressure, Dynamic Beam Seal, General Specification for

SAE AS5960A-2008 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, hoseassembly 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 AS33515C-2008 闷头非扩口管连接件用配件终端标准尺寸规格

Fitting End, Standard Dimensions for Bulkhead Flareless Tube Connections

Fitting End, Standard Dimensions for Bulkhead Flareless Tube Connections

BS ISO 23935:2008 航空器.气载流体系统元件用环境试验程序.在指定火灾区域的耐火性

Aircraft. Environmental test procedures for airborne fluid system components. Resistance to fire in designated fire zones

SAE AS5803-2008 3000 psi液压轴向陷型内螺纹非扩口45°弯头组装配件

Fitting Assembly, 45° Elbow, Female Flareless, Axially Swaged, Hydraulic, 3000 psi

Fitting Assembly, 45° Elbow, Female Flareless, Axially Swaged, Hydraulic, 3000 psi

SAE AS5081-2008 3000 PSI液压轴向陷型的内螺纹无扩口90°装配组件

FITTING ASSEMBLY, 90°,FEMALE FLARELESS, AXIALLY SWAGED,HYDRAULIC, 3000 PSI

FITTING ASSEMBLY, 90°,FEMALE FLARELESS, AXIALLY SWAGED,HYDRAULIC, 3000 PSI

GJB 6399-2008 导弹和运载火箭用液压泵可靠性要求和试验方法

本标准规定了导弹和运载火箭用液压泵可靠性要求和可靠性验证试验方法。 本标准适用于导弹和运载火箭液压伺服系统液压泵（以下简称液压泵）的可靠性设计、试制、定型和批生产的可靠性验证试验。

Reliability requirements and testing methods for hydraulic pumps of missiles and launch vechicles

SAE ARP490F-2008 电液伺服阀

This SAE Aerospace Recommended Practice (ARP) provides definitions and background information for understandingthe physical performance, and test procedures of electrohydraulic flow control servovalves.The recommendations are confined to interface definition and input/output characteristics. This ARP does not restrict orattempt to define the internal characteristics of servovalves. As such, the recommendations are equally applicable tovalves having different internal functioning, different ratings, different physical size, and valves used with different fluids. Incertain instances, standards for valve design are recommended for the purpose of interchangeability, as for example,valve polarity, mounting bolt and fluid port locations.The ARP provides extensive guidance for the preparation of Procurement Specifications and for functional testing. Asample Procurement Specification is provided in Appendix A. The primary focus of this ARP is on four-way valves. Threewayvalves are discussed to a limited extent and terminology for pressure control valves is presented in Appendix B.This ARP is applicable to fluid power systems in all types of flight vehicles, and it is applicable to Military, Civil and Spacedesign/certification standards. Additional specifications or specialized test procedures may be necessary to define specialrequirements for specific control systems, and such considerations are beyond the scope of this ARP.

(R) Electrohydraulic Servovalves