V29 航天用液压元件与附件 标准查询与下载

SAE AS5972D-2012 T字形轴向锻造液压5080 PSI配件总成

Fitting Assembly, Tee, Axially Swaged, Hydraulic, 5080 PSI

SAE AS5969C-2012 联合轴向锻造液压5080 PSI装配总成

This standard was prepared to provide an envelope requirements for an axially swaged, filed attachable, 5000 PSI, tube fitting.

Fitting Assembly, Union, Axially Swaged, Hydraulic, 5080 PSI

SAE AS685D-2012 试用环形密封液体连接轮毂

Not available.

Piloted Ring Seal Fluid Connection Bosses

SAE AS683D-2012 液体连接的安装程序和力矩

To establish standard installation procedures for fluid connection parts listed in this standard.

Installation Procedures and Torques for Fluid Connections

SAE AS598-2012 用于液压驱动系统中微粒污染物的宇航测微法和显微镜计数

The purpose of this technique is to provide a means of determining the severity of particulate contamination in fluid power systems. AS598 was prepared by SAE A6C1 panel and supersedes ARP598C. AS598 retained the technical content of ARP598C with more prescriptive requirements for the material used to carry out the analysis. The widely used technique has since been replaced in many instances with automatic particle counters (APC) but remains a proven, accurate and reliable technique. This SAE Aerospace Standard (AS) defines the materials, apparatus and procedure for sizing and counting of particulate contamination, 5 um or greater, in hydraulic fluid samples by membrane filtration with microscopic counting. The microscopic counting method is capable of counting particulate matter in samples withdrawn from fluid power systems as identified by the 12 classes of AS4059 and projected beyond these for the five standard ranges specified and can thus serve as the primary document to determine acceptability. It is also capable of revealing but not measuring evidence of abnormal amount of water, other fluids, fine particulate and other materials, especially fibers and metals. It is applicable to all military, civil, space vehicles and test equipment.

Aerospace Microscopic Sizing and Counting of Particulate Contamination for Fluid Power Systems

SAE AIR5455A-2012 试验尘埃污染物和颗粒计数器校准的变化对实验室过滤器元件性能和液体清洁度等级的影响

This document has been declared "Stabilized" and will no longer be subjected to periodic reviews for currency. Users are responsible for verifying references and continued suitability or technical requirements. New technology may exist. This SAE Aerospace Information Report (AIR) discusses the impact of the ISO Test Dusts, chosen as replacement contaminants for the Arizona Test Dusts (AC Test Dusts), and the ISO calibration procedure ISO 11171 for automatic particle counters, which replaces the calibration procedure ISO 4402 (1991), on laboratory performance of filter elements utilized in aerospace lubrication, hydraulic and fuel systems, and fluid cleanliness levels determined with automatic particle counters.

Impact of Changes in Test Dust Contaminants and Particle Counter Calibration on Laboratory Filter Element Performance and Fluid Cleanliness Classes

ANSI/AMCA 500-D-2012 测试空气流动速率用节气闸的实验室方法

The purpose of this standard is to establish uniform laboratory test methods for dampers. The characteristics to be determined include, as appropriate, air leakage, pressure drop, dynamic closure, and operational torque. This standard may be used as a basis for testing dampers when air is used as the test gas. This public review islimited to the changes made to the document since the previous public review.

Laboratory Methods of Testing Dampers for Rating

SAE AS6124-2011 安装和检查程序中使用的铝制轴向型锻配件

This procedure establishes the instructions to prepare tube ends, install and inspect axially swaged permanent tube fittings qualified to AS6116. This procedure is applicable when specified on the engineering drawing or in the procurement document.

Aluminum Axially Swaged Fittings, Installation and Inspection Procedure

BS ISO 22072:2011 航空航天.电动液压致动装置(EHA).采购规范中确定的特性

Aerospace. Electrohydrostatic actuator (EHA). Characteristics to be defined in procurement specifications

SAE AS6117-2011 部件装配:活接头,以轴向锻接法连接,可承受最高液压为1500 PSI

Fitting, Assembly, Union, Axially Swaged, Hydraulic, Up to 1500 PSI

SAE AIR1922A-2011 液压泵寿命的航天系统集成的影响因素

This AIR presents the following factors that affect hydraulic piston pump life and performance: a. the need to supply hydraulic fluid at the correct pressure and quality to the pum inlet port; b. Considerations for the pum output; c. Factors to be considered for the pump case drain lines; d. The mounting of the hydraulic pump; e. Hydraulic fluid properties, including cleanliness.

Aerospace System Integration Factors that Affect Hydraulic Pump Life

SAE AS5440A-2011 军用飞机液压系统的设计和安装要求

This specification covers the design and installation requirements for Types I and II aircraft hydraulic systems.

Hydraulic Systems, Military Aircraft, Design and Installation, Requirements for

SAE AIR4543B-2010 航空航天液压执行机构课程学习

This Aerospace Information Report (AIR) contains Lessons Learned from aerospace actuation, control and fluid power systems technologies. The lessons were prepared by engineers from the aerospace industry and government services as part of SAE Committee A-6, Aerospace Fluid Power, Actuation, and Control Technologies, and were presented to the A-6 during meetings held from 1989 through 1999. The document is organized into five sections covering systems, actuation, hydromechanical components, electrical components and miscellaneous, each further divided into subsections. The lessons presented in a concise format of Problem, Issue, Solution and Lesson Learned, often with accompanying descriptive diagrams and illustrations for clarity and understanding. Because of the potential growth in the size of the document as new lessons are published, those presented to the A-6 Committee in 2000 and later years are planned to be released in separate slash number documents, AIR4543/1, AIR4543/2 and so on.

Aerospace Hydraulics and Actuation Lessons Learned

SAE AS1650B-2010 无螺纹的,柔性,固定型控,自压焊式联轴器组装采购规范

This aerospace specification defines the requirements for a threadless, flexible, self-bonding coupling assembly which,when installed on machined fixed cavity ferrules, provides a flexible connection for joining tubing and components inaircraft fuel, vent or other systems. This assembled coupling, hereafter referred to as the assembly, is designed for usefrom -65 to +400 °F and at 125 psig nominal operating pressure.

Coupling Assembly, Threadless, Flexible, Fixed Cavity, Self-Bonding, Procurement Specification

ISO 11639:2010 航空航天.软组件零件号码

Aerospace - Part numbering for hose assemblies

SAE AIR5005A-2010 航空航天.商用航空器液压系统

This SAE Aerospace Information Report (AIR) has been compiled to provide information on hydraulic systems fitted to commercial aircraft. Data has been provided for the following aircraft types: a. Wide body jet airliners; b. Narrow body jet airliners; c. Turboprop/commuter aircraft; d. Business jet aircraft The airliners that have been included in this document are generally in operational service with either airlines or cargo operators. Information on aircraft that have been retired from in-service use has been included for reference purposes. No information is presented for aircraft that are currently being developed.

Aerospace - Commercial Aircraft Hydraulic Systems

SAE AS15001C-2010 I型钢锥螺纹.250-28表面裂纹液压润滑配件

Fitting, Lubrication, Hydraulic, Surface Check, .250-28 Taper Threads, Steel, Type I

SAE ARP5376B-2010 液压流体的固体颗粒污染系统取样和测量用方法、地点和标准

This SAE Aerospace Recommended Practice (ARP) provides procedures for assuring cleanliness of sampling equipment, for performing the sampling process, and for measuring and reporting the sample particle count. The ARP gives procedures for cleaning sample bottles, when used, and recommends the solvents to be applied and how these solvents should be prepared. Requirements for the selection of the sampling point, sampling method, and sampling frequency are also specified. This ARP also recommends three measuring methods for determining the level of solid particle contamination of hydraulic fluids used in aerospace hydraulics. These are: a. on-line automatic particle counting; b. automatic particle counting method using bottle samples; and c. microscopic particle count method using bottle samples.

Methods, Locations and Criteria for System Sampling and Measuring the Solid Particle Contamination of Hydraulic Fluids

BS ISO 8153-1:2009 航空航天.流体系统和零组件.软管总成术语

Aerospace - Fluid systems and components - Terminology of hose assemblies

SAE ARP1280B-2009 航空航天.液压动力输送装置的应用指南

This SAE Aerospace Recommended Practice (ARP) is an application guide for hydraulic power transfer units, and describes the various types, typical design approaches, their operational characteristics and limitations, circuit recommendations, typical applications. The scope of this ARP is limited to devices that transfer power between hydraulic systems and do so by means of rotary subassemblies such as hydraulic motors and pumps. The purpose of this document is to apprise the system designer of the available options in power transfer units, configuration tradeoffs, and system design precautions in their application.

Aerospace - Application Guide for Hydraulic Power Transfer Units