49.080 航空航天用流体系统和零部件 标准查询与下载

KS W 1511-2019 飞机用顶针和卸扣

THIMBLE AND SHACKLE FOR AIRCRAFT

KS W 1613-2019 航空航天 滚珠和滚子轴承键止动垫圈

Aerospace－Ball and roller bearings key retaing washer

KS W ISO 8575-2019 航空航天 流体系统 液压系统管材

Aerospace－Fluid systems－Hydraulic system tubing

KS W ISO 7169-2019 航空航天 – 用于流体系统的可分离管接头 用于 24° 锥体 压力高达 3 000 psi 或 21 000 kPa – 采购规格 英寸/公制

Aerospace－Separable tube fittings for fluid systems, for 24° cones, for pressures up to 3 000 psi or 21 000 kPa－Procurement specification, inch/metric

KS W 1617-2019 航空航天 仪表安装片弹簧螺母

Aerospace－Instrument mounting sheet spring nut

BS ISO 18387:2019 航天 线性液压实用执行器 一般规格

What is  ISO 18387- Linear hydraulic utility actuator about ?     ISO 18387 establishes the general requirements for a linear hydraulic utility actuator, herein referred to as a "utility actuator", for use in flight vehicle hydraulic systems at pressures up to 35000 kPa (5000 psi).   These requirements include:   Design requirements   Test requirements.   ISO 18387 is intended to be used in conjunction with the detailed specification that is particular to each application. ...

Aerospace. Linear hydraulic utility actuator. General specifications

ISO 18387:2019 航空航天.线性液压执行机构.一般规范

This document establishes the general requirements for a linear hydraulic utility actuator, herein referred to as a "utility actuator", for use in flight vehicle hydraulic systems at pressures up to 35000 kPa (5000 psi). These requirements include: — design requirements; — test requirements. This document is intended to be used in conjunction with the detail specification that is particular to each application. NOTE Although Brake pistons and Landing Gear Bogie (Truck) Pitch Trimmers are utility actuators, they are outside the scope of this document. This is because these devices are considered to be specialist actuator devices due to their specific duty cycles requiring a separate set of tailored requirements.

Aerospace — Linear hydraulic utility actuator — General specifications

BS EN 3086:2019 航空航天系列 软管组件 名称限制为 15 位数字

What is BS EN 3086 - Hose assemblies about ? BS EN 3086 is a European Standard that specifies the designation method for hose assemblies within 15 digits.   According to BS EN 3086 best practice guidance, you can code hose assemblies in a standardized method based on their metric size, inch size and nominal length. It also outlines codes for coupling configuration, angular orientation, sleeve material of cover, and hose assembly.    Who is BS EN 3086 - Hose assemblies for ? BS EN 3086 on

Aerospace series. Hose assemblies. Designation limited to 15 digits

BS ISO 9206:2018 航天 固定排量液压马达 一般规格

What is this standard about? This document establishes the general requirements for constant displacement hydraulic motors, suitable for use in aircraft hydraulic systems at pressures up to 35 000 kPa (5 000 psi). Primary and secondary function motors (see Clause 4) are covered in this document; however, actuators with internal rotation angle limits and low-speed motors are not covered. This document is to be used in conjunction with the detail specification that is particular to each application.

Aerospace. Fixed displacement hydraulic motors. General specifications

ISO 9206:2018 航空航天系列 - 恒定位液压马达 - 一般规格

This document establishes the general requirements for constant displacement hydraulic motors, suitable for use in aircraft hydraulic systems at pressures up to 35000 kPa (5000 psi). Primary and secondary function motors (see Clause 4) are covered in this document; however, actuators with internal rotation angle limits and low-speed motors are not covered. This document is to be used in conjunction with the detail specification that is particular to each application.

Aerospace — Fixed displacement hydraulic motors — General specifications

ASTM D2155-18 用自燃温度测定飞机液压液耐火性的标准试验方法

1.1 This test method is used for assessing the fire resistance of hydraulic fluids used for aircraft applications by determination of the autoignition temperature of the hydraulic fluid in air at one atmosphere pressure using hypodermic syringe injection. 1.2 The values stated in inch-pound units are to be regarded as standard. The values given in parentheses are mathematical conversions to SI units that are provided for information only and are not considered standard. 1.3 This standard is used to measure and describe the response of materials, products, or assemblies to heat and flame under controlled conditions, but does not by itself incorporate all factors required for fire hazard or fire risk assessment of the materials, products, or assemblies under actual fire conditions. 1.4 This standard does not purport to address all of the safety concerns, if any, associated with its use. It is the responsibility of the user of this standard to establish appropriate safety, health, and environmental practices and determine the applicability of regulatory limitations prior to use. 1.5 This international standard was developed in accordance with internationally recognized principles on standardization established in the Decision on Principles for the Development of International Standards, Guides and Recommendations issued by the World Trade Organization Technical Barriers to Trade (TBT) Committee.

Standard Test Method for Determination of Fire Resistance of Aircraft Hydraulic Fluids by Autoignition Temperature

ASTM F309-18 非压缩性航空推进剂液体取样标准实践

1.1 This practice covers procedures for obtaining a sample of noncryogenic aerospace propellant. Two procedures are covered as follows: Procedure 1—Closed System (Section 6), and Procedure 2—Open-End Procedure (Section 7). 1.2 This standard does not purport to address all of the safety concerns, if any, associated with its use. It is the responsibility of the user of this standard to establish appropriate safety, health, and environmental practices and determine the applicability of regulatory limitations prior to use. For hazard statements see Sections 4 and 5. 1.3 This international standard was developed in accordance with internationally recognized principles on standardization established in the Decision on Principles for the Development of International Standards, Guides and Recommendations issued by the World Trade Organization Technical Barriers to Trade (TBT) Committee.

Standard Practice for Liquid Sampling of Noncryogenic Aerospace Propellants

BS EN 4834:2018 航空航天系列 适配器 管接头 24° 锥体 压力高达 35 000 kPa (5 080 psi) 用于环锁定接头的端口 英制系列 几何配置

What is BS EN 4834 - Pipe coupling about?      BS EN 4834 is a European Standard that specifies the dimensions, tolerances, and requirements of a port for a fluid connection with ring locked fitting, for use in aircraft systems at a nominal operating pressure of 35 000 kPa (5 080 psi) maximum and temperature range of −54 to +135 °C (−65 to +275 °F).   Who is BS EN 4834 - Pipe coupling for?     BS EN 4834 on pipe coupling is useful for:     Aerospace hydraulic systems, fluids, and components  

Aerospace series. Adaptor, Pipe coupling 24° Cone up to 35 000 kPa (5 080 psi) Port for Ring locked fitting. Inch Series. Geometric configuration

BS EN 4835:2018 航空航天系列 环锁接头和异径管、24° 锥体压力高达 35 000 kPa (5 080 psi) 的安装和拆卸要求 英制系列

What is BS EN 4835 - Adaptors and reducers about?      BS EN 4835 is a European Standard that specifies the installation and removal requirements for adaptors and reducers, threaded, with a lockring for pipe couplings 24° according to EN 4833 and EN 4836 .   BS EN 4835 establishes an accurate procedure of adaptor installation, removal, and reinstallation to ensure the repeatability of the installation operation and to ensure effective compliance to sealing and locking requirements.   The adaptor shown on all Figures of BS EN 4835 is given as an example for the 24° internal cone interface according to EN 6123 .   This ...

Aerospace series. Installation and removal requirements for Ring locked fitting and reducer, 24° Cone up to 35 000 kPa (5 080 psi). Inch Series

BS EN 4833:2018 航空航天系列 管接头 24° 锥体 压力高达 35 000 kPa (5 080 psi) 环锁接头 不耀眼的结局 英制系列 超细牙螺纹

What is BS EN 4833 - Pipe coupling about?      BS EN 4833 is a European Standard that specifies the dimensions, tolerances, required characteristics, and the mass of an adaptor, flareless tube end EN 6123, ring locked type, for use in 35 000 kPa (5 080 psi) working pressure systems.   BS EN 4833 covers the requirements, quality assurance, designation, marking, preparation for delivery, technical specifications.    Who is BS EN

Aerospace series. Pipe coupling 24° Cone up to 35 000 kPa (5 080 psi) Ring-locked fitting. Flareless End. Inch Series. Extra Fine Thread Pitch

BS EN 4836:2018 航空航天系列 适配器 管接头 24° 锥体 压力高达 35 000 kPa (5 080 psi) 环锁接头 减速器 不耀眼的结局 英制系列 超细牙螺纹

What is BS EN 4836 - Pipe coupling about?      BS EN 4836 is a European Standard that specifies the dimensions, tolerances, required characteristics and the mass of a reducer, flareless tube end EN 6123 , ring locked type, for use in 35 000 kPa (5 080 psi) working pressure systems.   BS EN 4836 covers the requirements, quality assurance, designation, marking, packaging and technical specification. Who is BS EN 4836 - Pipe coupling for?     BS EN 4836 on pipe coupling is useful for:  

Aerospace series. Adaptor, Pipe coupling 24° Cone up to 35 000 kPa (5 080 psi) Ring-locked fitting. Reducer. Flareless End. Inch Series. Extra Fine Thread Pitch

DIN EN 6126:2018 航空航天系列-接头端，24°内锥，外螺纹，无扩口型，尺寸-32管径D=2英寸（D=50,8 mm）超细螺纹螺距英制系列-英制系列-设计标准

This standard specifies the dimensions, tolerances and the required characteristics of a fitting end, 24° cone, external thread, flareless type, size -32 for use in hydraulic and fluid systems at 220 psi, diameter D = 2 inches (D = 50,8 mm) for aerospace applications. This is a design standard, not valid for order. This fitting can not be used for plug in union.

Aerospace series - Fitting end, 24° internal cone, external thread, flareless type, size -32 tube diameter D=2 inches (D=50,8 mm) extra fine thread pitch inch series - Inch series - Design standard; German and English version EN 6126:2018

DIN EN 4833:2018 航空航天系列 管接头 24° 锥形高达 35 000 kPa（5 080 psi）环锁接头 扩口端 英制系列 超细螺纹螺距

This European Standard specifies the dimensions, tolerances, required characteristics and the mass of an adaptor, flareless tube end EN 6123, ring locked type, for use in 35000 kPa (5080 psi) working pressure systems.

Aerospace series - Pipe coupling 24° Cone up to 35 000 kPa (5 080 psi) Ring-locked fitting - Flareless End - Inch Series - Extra Fine Thread Pitch; German and English version EN 4833:2018

ASTM F309-04(2018) 非压缩性航空推进剂液体取样标准实践

Standard Practice for Liquid Sampling of Noncryogenic Aerospace Propellants

DIN EN 4510:2018 航空航天系列 管接头，60°，球形，钛合金 TI-P64001，适配器，直型，双端，带锁紧环

This European standard specifies the characteristics of the pipe coupling adapter, 60° spherical sealing face manufactured in titanium alloy with locking ring, for installing in a boss for aerospace applications. These adapters shall be installed into port connections manufactured in accordance with EN 2602 using ISO 3601-1 sealing O-rings selected sizes. O-ring material depends on the system fluid and operation conditions. The installation shall be performed in accordance with EN 2608. Nominal working pressure: up to 28000 kPa. Temperature range: limited by elastomeric sealing ring, -54 °C to +135 °C.

Aerospace series - Pipe couplings, 60°, spherical, in titanium alloy TI-P64001, adapters, straight, double end, with locking ring; German and English version EN 4510:2018