V29 航天用液压元件与附件 标准查询与下载

SAE ARP899B-1984 永久型液压系统管道配件的一般要求

This ARP establishes the basic test and design requirements for permanently attached tube fittings for use in aerospace fluid systems. Definitions of fitting and related terms are included in 6.3. This document recommends the tooling envelope, design criteria, and test requirements for tube fittings attached to tubing by methods which are usually considered to be permanent (brazing, welding, swaging, shrink fit, etc.).

Tube Fittings, Fluid Systems, Permanent Type, General Requirements for

NAVY DOD-PRF-24574-1978 低高压氧化气体混合物润滑液体

This specification covers lubricating fluid for use in oxidizing gas systems, including oxygen and cocipressed air for air and oil - free nitrogen system at pressures above 10,300 kilopascals (kPa) (1500 pounds per square

LUBRICATING FLUID FOR LOW AND HIGH PRESSURE OXIDIZING GAS MIXTURES

AIR FORCE MIL-B-6362 F (1)-1978 N-1B极端冷天气保护罩

This amendment forms-a part of lrlilitary Specification MIL-ìj-b362F(USRF), dated 8 Eeptemùer 1976, and is approved for use by all Departments aad Agencies of the Department of Defense.

BOOTS, EXTREME COLD WEATHER, N-1B

SAE AS3226-1978 轮毂T形管.AMS 5646

Tube, Tee, Boss - AMS 5646 FSC 4730

Tube, Tee, Boss - AMS 5646 FSC 4730

AIR FORCE MIL-B-6362 F-1976 N-1B极端冷天气保护罩

This specification covers one type of man's heavy rubber-soled boot which is designated N-1B.

BOOTS, EXTREME COLD WEATHER, N-1B

SAE ARP900A-1975 低温滤波器评估方法R(2002)

The purpose of this test procedure is to present test methods that can be utilized to evaluate the filtration and operating characteristics of filters that will be utilized in a cryogenic system. The methods presented herein are intended to supplement standard filter testing specifications to allow evaluation of filter performance characteristics in areas that could be affected by extreme low temperatures. The test methods can be utilized to evaluate filters up to and including 60 gpm (230 lpm) capacity. If higher flow rate filters are to be evaluated in accordance with the test methods presented herein, it will be necessary to increase the system flow capacity and the size of effluent sampling system. The test methods presented herein do not encompass testing of cryogenic bypass relief valves, delta P indicators, gages, or components other than a basic filter housing and element. This procedure includes equivalent metric units (in parentheses) as reference information, where deemed useful.

Methods for Evaluating Cryogenic Filters R(2002)

NAVY MIL-V-24109 A-1971 液压与气动高压快速换墨盒的球型阀和角型阀(尺寸1 / 8 -1 -1/4英寸)

This specification covers the design,construction, test and operatingrequirements for manually operated quick change cartridge trim globe and angle valves with nominal pressure rating of 6000 pounds per square inch gage (psig) for H .uPs.e h iynd raulic and pneumatic systems,

VALVES, GLOBE, ANGLE, QUICK CHANGE CARTRIDGE TRIM, HIGH PRESSURE (H.P.) HYDRAULIC AND PNEUMATIC (SIZES 1/8 - 1-1/4 INCHES)

SAE ARP1084-1969 运行中零部件的液压外部泄漏

The purpose of this document is to provide guide lines for allowable leakage for in-service aircraft hydraulic components at a nominal 100 F temperature and to outline the procedure for measuring such leakage. The limits to be applied to any specific aircraft should be adjusted before inclusion in a maintenance manual. Leakage as hereafter referred to in this document shall mean external leakage. The allowable leakage for hydraulic components has been documented in various military specifications concerning components. The leakage requirements given in the military specifications are intended in part to control the quality, assembly and proper functioning of the components. However, components that are in service sometimes develop leakage rates in excess of the specified amount. The does not necessarily imply that the components have degraded to a degree that they no longer provide reliable operation or that they would be detrimental to the system. The intent of this ARP is to establish a level of allowable leakage that will be applicable only to in-service hydraulic components. It is hoped that this will result in minimizing what is often the unnecessary removal of hydraulic components from an aircraft.

Hydraulic External Leakage for In-Service Components

NAVY MIL-V-23219-1962 高压空气减少阀组

Scope. - This specification cbvcrs thc design, construction, test and operating requirements for high pressure air reducing valve manifolds for the ASROC launcher.

VALVE MANIFOLDS, HIGH PRESSURE AIR REDUCING

NF L43-110:1966 飞机液压装置.软管插入接头

AIRCRAFT FLUID INSTALLATIONS. PLUG-IN UNIONS FOR FLEXIBLE HOSES.

QJ 1361-1988修改单 液压伺服系统安全、溢流阀通用技术条件

General technical specifications for hydraulic servo system safety and relief valves