V21 管件、卡箍、密封件 标准查询与下载

SAE AS4319B-2006 密封环的扩口管至凸起的接合器、扩展器配件

FITTING, EXPANDER, ADAPTER, FLARED TUBE TO BOSS FOR SEAL RING FSC 4730

FITTING, EXPANDER, ADAPTER, FLARED TUBE TO BOSS FOR SEAL RING FSC 4730

SAE AS18280/2A-2006 套管、内或外冲模或焊接、24度锥形非扩口配件、3000 psi

This SAE Aerospace Standard (AS) establishes the requirements for internally or externally swaged or welded sleeves or tube end adapters for use with 24?cone flareless fluid connection fittings per AS18280.

(R) Sleeves, Internally or Externally Swaged or Welded, 24 Degrees Cone Flareless Fitting, 3000 psi

GJB 5554-2006 飞机地面供风接口和接头类型和尺寸

本标准规定了飞机机上地面供风接口和地面空调设备地面供风接头的类型和尺寸。 本标准适用于总容积为50m以下的飞机设备舱、货舱和驾驶舱的飞机机上地面供风接口和空调设备地面供风接头、也适用于直升机的地面供风接口和空调设备地面供风接头。

Type and size of ground supply air inlet and adapter for aircraft

SAE AMS5580K-2006 74Ni、15.5Cr、和8.0Fe 退货的耐腐蚀耐热镍合金密封管

This specification covers a corrosion and heat resistant nickel alloy in the form of seamless tubing. This tubing has been used typically for parts requiring corrosion and oxidation resistance, up to 2000 °F (1093 °C), particularly where such parts may require welding during fabrication, but usage is not limited to such applications.

Nickel Alloy, Corrosion and Heat Resistant, Seamless Tubing 74Ni - 15.5Cr - 8.0Fe Annealed UNS N06600

BS EN 2608:2005 航空航天系列.8°30'带锁环的螺纹适配器的安装和移除要求

This standard specifies the installation and removal requirements for adaptors, threaded, with lockring for pipe couplings 8°30' 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°30' interface according to EN 2604. This procedure is used for adaptors 8°30', for nominal pressure up to 28 000 kPa to install the adapters according to EN 3248, EN 3270 and EN 3566.

Aerospace series - Installation and removal requirements for 8 ° 30' adaptors, threaded, with lockring

BS ISO 23933:2006 航空航天.等级为135℃/20.684 kPa(275℉/3000 psi)和135℃/21000 kPa(275℉/3046 psi)的芳族聚酰胺增强的轻型聚四氟乙烯(PTFE)软管组件.采购规范

ISO 23933:2006 specifies requirements for aramid reinforced lightweight polytetrafluoroethylene (PTFE) hose assemblies for use in aircraft hydraulic, oil and fuel systems at temperatures between -55 °C and 135 °C (-65 °F and 275 °F) and at a nominal pressure of 21 000 kPa (210 bar) (3 046 psi) or 20 684 kPa (3 000 psi). The hose assemblies are also suitable for use within the same temperature and pressure limitations in aircraft pneumatic systems where some gaseous diffusion through the wall of the PTFE liner may be tolerated.

Aerospace series. Aramid reinforced lightweight polytetrafluoroethylene (PTFE) hose assemblies, classification 135°C/20 684 kPa (275°F/3 000 psi) and 135°C/21 000 kPa (275°F/3 046 psi). Procurement specification

SAE AS5620A-2006 Ti-3Al-2.5V冷处理和应力释放的、达到35,000 kPa (5080 psi)合格试验和控制要求的钛液压管

This SAE Aerospace Standard (AS) shall be used in conjunction with AMS 4946 to provide requirements for qualification testing and for Qualified Products Listing (QPL) and Qualified Manufacturer Listing (QML) for Ti-3Al-2.5V cold worked and stress relieved hydraulic system tubing. The basic tubing shall comply with the requirements of SAE AMS 4946.

Titanium Hydraulic Tubing, Ti-3Al-2.5V Cold Worked and Stress Relieved, Up to 35,000 kPa (5080 psi), Requirements for Qualification Testing and Control

SAE AS4088C-2006 航空杆铲运机密封管设计标准

This SAE Aerospace Standard (AS) defines gland details for rod diameters from 1/4 to 15-1/2 in. inclusive corresponding to O-Ring Dash No. sizes -108/-111, -206/-222, -325/-349 and -425/-460. The gland details herein provide more space than MS33675 and sufficient to fit more efficient and reliable exclusion devices.

Aerospace Rod Scraper Gland Design Standard

DIN EN 3272:2006 航空航天系列.8°30'管接头.焊接箍用动态梁密封端.几何构型.德文和英文版本EN 3272-2001

This standard specifies the dimensions of the dynamic beam seal end for welded ferrules for pipe couplings 8?0', nominal pressure up to 28000 kPa, for aerospace applications.

Aerospace series - Pipe coupling 8°30' - Dynamic beam seal end for ferrule, welded - Geometric configuration; German and English version EN 3272:2001

AECMA PREN 3545-009-2006 航空航天系列. 尾部密封和无密封塑料护套、锁紧装置、工作温度操作温度-55°C至175°C的矩形电接点.第009部分;插头和插座防护罩.产品标准

This draft is now available for public comment and your views and technical comments on it would be appreciated. If you have no specific comments to make hut find it generally acceptable it would be helpful if you would notify US accordingly. Suggestions entailing revision of the text should indicate the preferred wording. Please quote the relevant clause number against any comment.

Aerospace series Connectors, electrical, rectangular, with sealed and non-sealed rear, plastic housing, locking device, operating temperatures - 55 癈 to 175 癈 Part 009: Protective cover for plug and receptacle Product standard Edition P 1

AECMA PREN 6120-2006 航空航天系列.栓紧公差铁模锁凸出头修剪类铝合金7050化学薄膜英尺系列.P1版

This standard specifies the characteristics of close tolerance pins, swage locking, protruding head, shear type, in aluminium alloy 7050-T73 with chemical film, inch series, with a maximum operating temperature of 80 °C for aerospace application. Pins with diameter code 040 shall be used in combination with collars as per EN 6051 only. Pins with diameter code 050, 060 and 080 shall be used in combination with collars as per EN 6054 only.

Aerospace series Pins, close tolerance, swage locking, protruding head, shear type, in aluminium alloy 7050, chemical film Inch series Edition P 1

AECMA PREN 3545-002-2006 航空航天系列. 尾部密封和无密封塑料护套、锁紧装置、工作温度操作温度-55°C至175°C的矩形电接点.第002部分;技术规范和触点组合

It is essential that products defined by European Aerospace Series Standards (EN) conform with the requirements of these standards, and that the quality of the products be consistently maintained. To this effect, a qualification system, AECMA-CERT, for manufacturer and product is implemented. It is based upon :

Aerospace series Connectors, electrical, rectangular, with sealed and non-sealed rear, plastic housing, locking device, operating temperatures - 55 癈 to 175 癈 Part 002: Specification of performance and contact arrangements Edition P 5

AECMA PREN 3545-001-2006 航空航天系列. 尾部密封和无密封塑料护套、锁紧装置、工作温度操作温度-55°C至175°C的矩形电接点.第001部分;技术规范

The text of this standard, which exists in three equivalent versions (English, French, German) has been drawn up under the responsibility of AECMA (Association Européenne des Constructeurs de Matériel Aérospatial) and has been circulated to Official Services. Any reservations expressed by Official Services and not resolved in this issue, have been incorporated in the history sheet which has accompanied this prEN to CEN.

Aerospace series Connectors, electrical, rectangular, with sealed and non-sealed rear, plastic housing, locking device, operating temperatures - 55 癈 to 175 癈 Part 001: Technical specification Edition P 4

SAE AS5868A-2006 5080 Psi液压的轴向陷型的无扩口闷头的接头配件

FITTING ASSEMBLY, ADAPTER, BULKHEAD FLARELESS, AXIALLY SWAGED, HYDRAULIC, 5080 PSI FSC 4730

FITTING ASSEMBLY, ADAPTER, BULKHEAD FLARELESS, AXIALLY SWAGED, HYDRAULIC, 5080 PSI FSC 4730

AECMA PREN 6117-2006 航空航天系列.润滑规范扣件鲸蜡醇.P1版

This specification defines the process applicable to the lubrication of threaded bolts, nuts, lock bolt pins and collars with cetyl alcohol. It defines the product application methods and the relevant quality assurance requirements for the lubrication of the commonly used fastener materials: Aluminium alloys, alloy steels, stainless steels, titanium alloys and nickel base alloys.

Aerospace series Specification for lubrication of fasteners with cetyl alcohol Edition P 1

AECMA PREN 6095-2006 航空航天系列.旋转扣件结构和非结构应用技术规范.P1版

This standard specifies the required characteristics, inspections, tests, quality assurance requirements, conditions for qualification acceptance and delivery of rotary fasteners for structural and non-structural applications. This standard applies to all rotary fasteners for structural and non structural applications. It may be applied when referred to in the product standard or in a design specification.

Aerospace series Rotary fasteners Structural and non-structural applications Technical specification Edition P 1

GJB 5424-2005 3.5吨级军用越野汽车规范

本规范规定了飞船结构用橡胶静密封材料的要求、质量保证规定、交货准备和说明事项。 本规范适用于载人飞船结构静密封用硅橡胶材料的制备、检验和验收。卫星及其它空间飞行器结构密封材料可以参照使用。

Specification for static seal rubber materials used in the structure system of spacecraft

AECMA PREN 3545-008-2005 航空航天系列. 尾部密封和无密封塑料护套、锁紧装置、工作温度操作温度-55°C至175°C的矩形电接点.第008部分;装配工具/编码去除和附件系统产品

This standard is part of the series of EN metallic material standards for aerospace applications. The general organization of this series is described in EN 4258.

Aerospace Series Connectors, electrical, rectangular, with sealed and non-sealed rear, plastic housing, locking device, operating temperatures - 55 degrees C to 175 degrees C Part 008: Tools for assembly/removal of coding and attachment system Product st

NF L46-611*NF EN 4167:2005 航空航天系列.三部分弹簧张力夹具.耐热钢FE-PA2601(A286)制内夹具

Aerospace series - Clips, spring tension, three parts - Inner clips in heat resisting steel FE-PA2601 (A286).

NF L46-613*NF EN 4166:2005 航空航天系列.三部分弹簧张力夹具.聚四氟乙烯轴衬

Aerospace series - Clips, spring tension, three parts - PTFE bushes.