V29 航天用液压元件与附件 标准查询与下载

SAE AS5174D-2008 扩口管接头和异径接头的配件

FITTING, UNION AND REDUCER, FLAREDTABLE 1A-DIMENSION A/12/TABLE 1B-DIMENSION CTABLE 1C-DIMENSIONS AND WEIGHTS/10/

Fitting, Union and Reducer, Flared

NF L41-211*NF EN 2624:2007 航空航天系列.液压系统元件的压力脉冲测试

Aerospace series - Pressure impulse testing of hydraulic system components.

BS ISO 6771:2007 航空航天.流体系统和部件.压力和温度分类

This International Standard specifies the pressure classes and temperature types for the basic systems and component systems that are commonly used in aerospace fluid systems. Classes and types in the lower ranges represent systems in common use. Those in the higher ranges represent systems that are in less common use or that are used in developmental systems.

Aerospace - Fluid systems and components - Pressure and temperature classifications

BS EN 2624:2007 航空航天系列.水压系统元件的压力脉冲测试

This test method shall be used to verify the structural integrity of certain hydraulic components under pressure impulse-type loading. For the purpose of pressure impulse testing the hydraulic system components shall be divided into passive and active components. This standard establishes the requirements and the procedures for impulse testing of passive hydraulic components only. Unless otherwise specified in the detail specification or in existing component related standards, the following procedures shall be used. Active hydraulic components shall be tested according to tailored test requirements as specified in detail specifications.

Aerospace series - Pressure impulse testing of hydraulic system components

ISO 6771:2007 航空航天.流体系统和部件.压力和温度分类

This International Standard specifies the pressure classes and temperature types for the basic systems and component systems that are commonly used in aerospace fluid systems. Classes and types in the lower ranges represent systems in common use. Those in the higher ranges represent systems that are in less common use or that are used in developmental systems.

Aerospace - Fluid systems and components - Pressure and temperature classifications

SAE AS35411B-2007 润滑配件

This SAE Aerospace Standard (AS) covers the requirements for threaded lubrication fittings, straights and elbows, to be used for admitting and retaining lubricants supplied by pressure lubricating equipment. The purpose of this standard is to replace MIL-F-3541 with a document consistent with the performance requirements of the specification it supersedes.

Fittings, Lubrication

SAE AS15720B-2007 VII类耐腐蚀钢.250-28锥螺纹喉口或表面裂纹液压润滑配件

FITTING, LUBRICATION, HYDRAULIC, THROAT OR SURFACE CHECK, .250-28 TAPER THREADS, CORROSION RESISTANT STEEL, TYPE VIITABLE 1 - DIMENSIONS AD WEIGHTS

Fitting, Lubrication, Hydraulic, Throat or Surface Check, .250-28 Taper Threads, Corrosion Resistant Steel, Type VII

BS ISO 7169:2007 航空航天.液压系统用24°锥形的、压力范围截至3000psi或21000kPa的可拆卸管接头.采购规范(英制/米制)

This International Standard specifies performance and quality requirements for the qualification and manufacture of standard 24° cone fittings and manufacture of 24° cone fittings to ensure reliable performance or equivalent inch-dimensioned fitting ends to ensure reliable performance in aircraft hydraulic systems. This International Standard specifies baseline criteria for the design and manufacture of system fittings that are qualification-tested on engines. This International Standard covers fittings of the temperature types and pressure classes specified in ISO 6771.

Aerospace - Separable tube fittings for fluid systems, for 24 ° cones, for pressures up to 3000 psi or 21000 kPa - Procurement specification, inch/metric

SAE AS4499C-2007 180°对180°金属增强传导的聚四氟乙烯盘绕扩口软管组件

HOSE ASSEMBLY, CONVOLUTED, POLYTETRAFLUOROETHYLENE, METALLIC REINFORCED CONDUCTIVE, FLARED, STRAIGHT TO STRAIGHT

HOSE ASSEMBLY, CONVOLUTED, POLYTETRAFLUOROETHYLENE, METALLIC REINFORCED CONDUCTIVE, FLARED, STRAIGHT TO STRAIGHT

SAE AS4941A-2007 航空航天系列.商用航空器液压部件的一般要求

This SAE Aerospace Standard (AS) provides requirements for components that are used in commercial aircraft hydraulic systems. It is to be used in conjunction with a Procurement Specification for each component. This specification shall be used to develop Procurement Specifications for components. It also provides information to be included in the Procurement Specification in Appendix A and a checklist for design reviews in Appendix B. It does not provide information on distribution elements such as hoses, pipe couplings and general tubing.

(R) Aerospace - General Requirements for Commercial Aircraft Hydraulic Components

SAE ARP4379A-2007 航空航天.活塞隔离开的圆柱状液压蓄能器

This SAE Aerospace Recommended Practice (ARP) is intended as a guide in defining the requirements for aerospace piston separated hydraulic accumulators, including details pertinent to the design, fabrication, and performance of the accumulator. This type of accumulator has a piston separator and contains both high-pressure gas and fluid. The accumulator is used in aerospace hydraulic systems of the following types as defined in SAE AS 5440 with design operating pressures of up to 8000 psi (55,160 kPa). Type I: -65 to +160 °F (-54 to +71 °C) fluid temperature Type II: -65 to +275 °F (-54 to +135 °C) fluid temperature For commercial aerospace or helicopter applications, the information and guidelines of SAE ARP 4752 or SAE ARP 4925 respectively, are considered.

(R) Aerospace - Accumulator, Hydraulic, Cylindrical, Piston Separated

GJB 5874-2006 数字式电磁阀通用规范

本规范规定了数字式电磁阀（以下简称电磁阀）产品的要求、质量保证规定、交货准备及说明事项等要求。 本规范适用于航空航天燃油、液压以及气动系统用电磁阀的设计、制造和验收。用于其它系统的电磁阀可参照执行。

General specification of digital Solenoid valve

SAE AS5550A-2006 5080 PSI超细牙螺纹非扩口端环锁适配器组件

FITTING ASSEMBLY, RING LOCKED, ADAPTER, FLARELESS TO PORT, EXTRA FINE THREADS, 5080 PSI FSC 4730FIGURE 1 - FITTING ASSEMBLYTABLE 1A - DIMENSIONS A-ETABLE 1B - DIMENSIONS F-M AND WEIGHTS

FITTING ASSEMBLY, RING LOCKED, ADAPTER, FLARELESS TO PORT, EXTRA FINE THREADS, 5080 PSI FSC 4730

SAE AS1715D-2006 耦合、柔性、变化空腔、螺纹箍管末端垫圈

(R) WASHER, COUPLING, FLEXIBLE, VARIABLE CAVITY, THREADED, FERRULE TYPE TUBE ENDS FSC 4730

Washer, Coupling, Flexible, Variable Cavity, Threaded, Ferrule Type Tube Ends

SAE AS1716D-2006 耦合、柔性、变化空腔、螺纹箍管末端、米制箍

(R) FERRULE, COUPLING, FLEXIBLE, VARIABLE CAVITY, THREADED, FERRULE TUBE END FSC 4730

(R) FERRULE, COUPLING, FLEXIBLE, VARIABLE CAVITY, THREADED, FERRULE TUBE END FSC 4730

SAE AS1717D-2006 耦合、柔性的、变化空腔、螺纹箍型管末端止动装置

(R) RETAINER, COUPLING, FLEXIBLE, VARIABLE CAVITY, THREADED FERRULE TYPE TUBE ENDS FSC 4730

(R) RETAINER, COUPLING, FLEXIBLE, VARIABLE CAVITY, THREADED FERRULE TYPE TUBE ENDS FSC 4730

SAE AS1718D-2006 耦合、柔性的、变化空腔、螺纹箍型管末端

(R) COUPLING BODY, FLEXIBLE, VARIABLE CAVITY, THREADED FERRULE TYPE TUBE ENDS FSC 4730

(R) COUPLING BODY, FLEXIBLE, VARIABLE CAVITY, THREADED FERRULE TYPE TUBE ENDS FSC 4730

DIN EN 2608:2006 航空航天系列.8°30'带锁环的螺纹适配器的安装和移动要求

This standard specifies the installation and removal requirements for adaptors, threaded, with lockring for pipe couplings 8?0' according to EN 2603. This standard establishes an accurate procedure of adaptor installation, removal and reinstallation to ensure the repeatability of the installation operation and to ensure the effective compliance to sealing and locking requirements. The adaptor shown on all figures of this standard is given as an example for the 8?0' interface according to EN 2604. This procedure is used for adaptors 8?0', for nominal pressure up to 28000 kPa.

Aerospace series - Installation and removal requirements for 8°30' adaptors, threaded, with lockring; German and English version EN 2608:2005

GJB 5553-2006 飞机液压系统地面供油接头结构和尺寸

本标准规定了飞机液压系统地面供油接头的类型和尺寸。 本标准适用于飞机液压油泵车、清洗车和液压试验台的液压系统供油、回油接头，也适用于直升机地面供油接头。

Structure and size of ground supply fluid adapter for aircraft hydraulic system

SAE AS5860-2006 液压气动、聚四氟乙烯树脂、单向旋转和静态盖的气袋(替补密封环）

This Aerospace Standard (AS) covers scarf-cut polytetrafluoroethylene (PTFE) retainers (back-up rings) for use in static glands in accordance with AS5857. They are for use in hydraulic and pneumatic system components as anti-extrusion devices in conjunction with O-rings, packings and other elastomeric seals. Because of the construction of groove dimensions, back-ups specific to rod applications are designated R - Rod (Female), back-ups specific to piston applications are designated P - Piston (Male). Retainers specified herein have been designed for a temperature range of -65 °F to 275 °F (-54 °C to 135 °C) and a nominal operating pressure of 3000 psi (20.7 MPa) for code 09 material and 5000 psi (34.5 MPa) for code 10 material. Material codes are based on AMS 3678 material types. Consideration has been made to accommodate cylinder breathing on piston applications, calculated at .002 inch/inch diameter/1,000 psi (.051 mm/mm diameter/6.9 MPa) to ensure a minimum 50% lap at -65 °F (-54 °C). This has required an increase in the diameter on certain larger sizes and a slight overlap at ambient will therefore be apparent. These parts have been designed such that the overlap at 275 °F (135 °C) will not result in axial compression of the O-rings, even in the worst tolerance stack-up situation.

Retainers (Back-up rings), Hydraulic and Pneumatic, Polytetrafluoroethylene Resin, Single Turn, Static Gland