V38 液压、冷气系统及其附件 标准查询与下载

DIN EN 3867:2007 航空航天系列.管连接件、活动法兰和密封件.TI-P64001型钛合金法兰

The document specifies the characteristics of flanges for pipe couplings in titanium alloy TI-P64001 for aerospace applications.

Aerospace series - Pipe couplings, loose flanges and seals - Flanges in titanium alloy TI-P64001; German and English version EN 3867:2004

DIN EN 3869:2007 航空和航天系列.管道联接件、活动法兰和密封件.铝合金碳氟橡胶和电枢密封件

The document specifies the characteristics of seals for pipe couplings in fluorocarbon rubber and armature in aluminium alloy for aerospace applications.

Aerospace series - Pipe couplings, loose flanges and seals - Seals in fluorocarbon rubber and armature in aluminium alloy; German and English version EN 3869:2004

DIN EN 3868:2007 航空航天系列.管连接件、活动法兰和密封件.TI-P64001型钛合金焊接法兰联接件

The document specifies the characteristics of welded flanged connectors in titanium alloy TI-P64001 for aerospace applications.

Aerospace series - Pipe couplings, loose flanges and seals - Flange connectors, welded, in titanium alloy TI-P64001; German and English version EN 3868:2004

GJB 5886-2006 飞机液压系统工作液含水量检测方法

本标准规定了用卡尔菲休原理的库仑法和容量法检测飞机液压系统工作液含水量的方法。 本标准适用于飞机液压系统工作液含水量的检测，其它系统的工作液可参照执行。不适用含醛、酮、磷产品的工作液检测。

Determination method for water content of operating fluid for aviation hydraulic system

HB 7799-2006 飞机液压系统工作液采样点设计要求

本标准规定了军用飞机液压系统工作液采样点的通用设计要求和验证要求。 本标准适用于按GJB 638A-1997设计的液压系统在研制阶段的工作液采样点设计和验证。其他流体系统工作液采样点设计也可参照执行。

Requirements of hydraulic system nuid sampling position design for aircraft

BS F 159:2006 用符合BS F 153抗油硅橡胶材料制成的弹性环形密封圈("O"形圈)特性.规范

This British Standard specifies requirements for elastomeric toroidal sealing rings (“O” rings) manufactured from oil-resistant silicone rubber material conforming to BS F 153. This material standard is to be used in conjunction with BS EN 3207 and SBAC TS 49.

Properties of elastomeric toroidal sealing rings ("O" rings) manufactured from oil resistant silicone rubber material conforming to BS F 153 - Specification

BS F 164:2006 用符合BS F 154氟硅橡胶材料制成的弹性环形密封圈("O"形圈)的特性.规范

This British Standard specifies requirements for elastomeric toroidal sealing rings (“O” rings) manufactured from fluorosilicone rubber material conforming to BS F 154. This material standard is to be used in conjunction with BS EN 3207 and SBAC TS 49.

Properties of elastomeric toroidal sealing rings ("O" rings) manufactured from fluorosilicone rubber material released to BS F 154 - Specification

BS F 162:2006 用符合BS F 156二元乙丙橡胶材料制成的弹性环形密封圈("O"形圈)特性.规范

This British Standard specifies requirements for elastomeric toroidal sealing rings (“O” rings) manufactured from ethylene–propylene rubber material conforming to BS F 156. This material standard is to be used in conjunction with BS EN 3207 and SBAC TS 49.

Properties of elastomeric toroidal sealing rings ("O" rings) manufactured from ethylene-propylene rubber material conforming to BS F 156 - Specification

SAE ARP4835-2006 飞机液压动力热释放阀门

This SAE Aerospace Recommended Practice (ARP) establishes the general requirements for hydraulic thermal expansion relief valves used in aircraft and missile hydraulic systems having operating pressures and temperatures as identified.

Aerospace Fluid Power-Hydraulic Thermal Expansion Relief Valves

SAE AMS2615F-2006 规定的液压压力试验

This specification provides requirements and procedures for hydraulic-pressure leak testing of parts.

Pressure Testing, Hydraulic Pressure as Specified [Replaced: SAE AMS 2616E, SAE AMS 2616D, SAE AMS 2620E, SAE AMS 2620D, SAE AMS 2625E, SAE AMS 2625D] [Superseded: SAE MAM 2615B, SAE MAM 2615A, SAE MAM 2616C, SAE MAM 2616B]

ISO 8829-2:2006 航空.聚四氟乙烯(PTFE)内软管组件试验方法.第2部分:非金属编织物

This part of ISO 8829 specifies test methods for flexible polytetrafluoroethylene (PTFE) inner tubes with non-metallic braided hose and hose assemblies used in aircraft fluid systems, in the pressure and temperature ranges covered by pressure classes and temperature types, as specified in ISO 6771. This part of ISO 8829 applies to the hose and the hose coupling. The tests and assembly requirements for the connecting end fittings are covered in the procurement specification. This part of ISO 8829 is applicable when reference is made to it in a procurement specification or other definition document. NOTE Fluids used for the tests are listed in Annex A.

Aerospace - Test methods for polytetrafluoroethylene (PTFE) inner-tube hose assemblies - Part 2: Non-metallic braid

ISO 9679:2006 航空航天.流体系统用夹具

This International Standard specifies the test methods and procedures to be used for the qualification and comparison of support or retention devices used in the installation of aerospace fluid systems. It is applicable when reference is made to parts standards, procurement specifications, or other definition documents.

Aerospace - Clamps for fluid systems - Test methods

DLA QPL-AS1339-30-2006 金属加固3000PSI 400华氏度重量轻液压与气动聚四氟乙烯软管装配

This list has been prepared for use by or for the Government in the acquisition of products covered by SAE-AS1339. Listing of a product is not intended to and does not connote endorsement of the product by the Department of Defense. All products listed herein have been qualified under the requirements for the product as specified in the latest effective issue of the applicable specification. This list is subject to change without notice;revision or amendment of this list will be issued as necessary. The listing of a product does not release the supplier from compliance with the specification requirements.

HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE, METALLIC REINFORCED, 3000 PSI, 400 DEGREES F, LIGHTWEIGHT, HYDRAULIC AND PNEUMATIC

ISO 23935:2006 飞行器.机载流体体系部件的环境试验程序.指定防火区内的耐火性

This International Standard specifies the requirements for tests which may be applied to all fluid system components located in zones designated as "fire zones" and built to satisfy the minimum level specified for withstanding fire. This International Standard does not relate to withstanding fire outside designated fire zones, nor to flammability requirements, or to those conditions induced by the flame coming from the combustion chamber.

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

SAE AS21922B-2006 非扩口耦合管套

SLEEVE, COUPLING, FLARELESS FSC 4730FIGURE 1 - SLEEVE, COUPLING, FLARELESSTABLE 1A - DIMENSIONS A-ETABLE 1B - DIMENSIONS F-S

SLEEVE, COUPLING, FLARELESS FSC 4730

SAE AS5235A-2006 非扩口耦合管套配件

FITTING, SLEEVE, COUPLING, FLARELESS FSC 4730TABLE 1A - DIMENSIONSTABLE 1B - DIMENSIONS AND WEIGHTS

Fitting, Sleeve, Coupling, Flareless

BS EN 4610:2005 航空航天系列.8°30'钛合金管接头.带推进线螺母的45°弯头

This standard specifies the characteristics of elbows 45°, with thrust wire nut, for pipe couplings 8°30', in titanium alloy, for aerospace applications. Nominal pressure: up to 28 000 kPa. Temperature range: – 55 °C to 135 °C.

Pipe coupling 8°30' in titanium alloy — Elbows 45°, with thrust wire nut

SAE AS5959-2006 辅助压模配件安装和检验方法

This procedure establishes the instructions to prepare tube ends and install and inspect axially swaged permanent tube fittings qualified to AS 5958. This procedure is applicable when specified on the engineering drawing or in the procurement document.

Axially Swaged Fittings, Installation and Inspection Procedure

DIN EN 3269:2006 航空航天系列.8°30'钛合金管接头.带动态梁密封端的单头卡套.德文和英文版本EN 3269-2001

This standard specifies the characteristics of blind ferrules with dynamic beam seal end for pipe couplings 8?0', in titanium alloy, for aerospace applications.

Aerospace series - Pipe coupling 8°30' in titanium alloy - Ferrules, blind, with dynamic beam seal end; German and English version EN 3269:2001

DLA QPL-AS604-17-2006 金属加固3000PSI 400华氏度重量级液压聚四氟乙烯软管装配

This amendment forms a part of MI L-W-81822/5A, dated 3 March 1982, and is approved for use by all Departments and Agencies of the Department of Defense.

HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE, METALLIC REINFORCED, 3000 PSI, 400 DEGREES F, HEAVYWEIGHT, HYDRAULIC