49.080 航空航天用流体系统和零部件 标准查询与下载

GSO ISO 6773:2016 航空航天 流体系统 管道和配件的热冲击测试

This International Standard provides an environmental test method for thermal shock testing of fluid system piping and fittings, excluding hose and hose assemblies.

Aerospace -- Fluid systems -- Thermal shock testing of piping and fittings

GSO ISO 14085-5:2016 航空航天系列液压滤芯试验方法 第5部分：抗流动疲劳性能

This part of ISO 14085 specifies a method for determining the resistance of a filter element to flow fatigue caused by varying flow through the filter in various stages of the filter contaminant loading process. The filter is subjected to a uniform varying flow rate for a specified number of cycles, at a number of predetermined differential pressures. Although the number of cycles and differential pressure conditions used in this part of ISO 14085 is meant to simulate possible service conditions, this part of ISO 14085 is not intended to qualify a filter element under replicate conditions of service; this can only be done by a specific test protocol developed for the purpose, including actual conditions of use, for example the operating fluid, contamination, and exact cyclic flow conditions. This part of ISO 14085 establishes a method for verifying the ability of a filter element to withstand the stress caused by cyclic differential pressures induced by a variable flow rate. The test data resulting from application of this part of ISO 14085 can be used to compare the performance of aerospace hydraulic filter elements.

Aerospace series -- Hydraulic filter elements -- Test methods -- Part 5: Resistance to flow fatigue

GSO ISO 14085-4:2016 航空航天系列液压滤芯试验方法 第4部分：塌陷/爆破压力等级验证

This part of ISO 14085 describes a method for verifying the collapse/burst pressure rating of an aerospace hydraulic fluid power filter element. This represents the capability of a filter element to withstand a designated differential pressure in the normal (intended) direction of flow, created by flowing contaminated fluid through the filter element until either collapse/burst occurs or the maximum expected differential pressure is reached without element failure. The collapse/burst pressure test can be conducted in conjunction with an efficiency test performed according to the procedure defined in the ISO 14085-3 by continuing the contaminant injection until the designated filter element differential pressure is reached. This part of ISO 14085 is not intended to qualify a filter element under replicate conditions of service; this can only be done by a specific test protocol developed for the purpose, including actual conditions of use, for example the operating fluid or contamination. The tests data resulting from application of this part of ISO 14085 can be used to compare the performance of aerospace hydraulic filter elements.

Aerospace series -- Hydraulic filter elements -- Test methods -- Part 4: Verification of collapse/burst pressure rating

GSO ISO 8574:2016 航空航天 液压系统管材 弯管的合格试验

This International Standard specifies pressure impulse and burst test procedures for determining and classifying the impulse fatigue strengths of bent tubes used in aerospace hydraulic systems. The procedures are intended for qualification purposes of high- and low-pressure system tubing or for the evaluation of new materials for hydraulic system tubing. NOTE Requirements for tubing used in aerospace hydraulic systems are given in ISO 8575.

Aerospace -- Hydraulic system tubing -- Qualification tests for bent tubes

GSO ISO 8575:2016 航空航天 流体系统 液压系统管

This International Standard specifies the requirements relating to the sizes and material of tubing for use in aerospace hydraulic pressure and return systems. For pressure lines, the requirements apply to the pressure and temperature ranges covered by pressure classes D and E and temperature types II and III as specified in ISO 6771.

Aerospace -- Fluid systems -- Hydraulic system tubing

GSO ISO 7169:2016 航空航天 用于流体系统的可分离管接头 用于 24 度锥体 压力高达 3 000 psi 或 21 000 kPa 采购规格 英寸/公制

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 degree cones, for pressures up to 3 000 psi or 21 000 kPa -- Procurement specification, inch/metric

GSO ISO 1749:2016 飞机—弹性密封圈—包装和标识

This International Standard specifies the requirements for the packaging and the identification, when packaged, of elastomeric sealing rings for aircraft.

Aircraft -- Elastomeric sealing rings -- Packaging and identification

GSO ISO 27996:2016 航空航天流体系统 弹性体密封件 储存和保质期

This International Standard is applicable to the general requirements for data recording procedures, packaging, and storing of elastomeric seals and seal assemblies which include an elastomeric element prior to the seal being assembled into hardware components. The requirements for packaging are an integral part of the controlled storage procedure and provide a means of positive product identity from the time of manufacture to the time of assembly into a component. This International Standard does not establish limitations or storage times for assembled components nor the operating life of these components. The information contained in this International Standard is intended for use by those organizations that do not have specific requirements or recommendations already in place for the control of elastomeric seals and seal assemblies. This International Standard can be specified in control, storage and procurement documents. However, when the requirements of this International Standard are in conflict with the customer's requirements or specifications, the requirements of the customer's detailed specifications take precedence.

Aerospace fluid systems -- Elastomer seals -- Storage and shelf life

GSO ISO 8625-2:2016 航空航天 流体系统 词汇 第2部分：与流量相关的通用术语和定义

This part of ISO 8625 defines general terms relating to flow in fluid systems used in aerospace construction.

Aerospace -- Fluid systems -- Vocabulary -- Part 2: General terms and definitions relating to flow

GSO ISO 5859:2016 航空航天系列液压气动系统及元件原理图图形符号

This International Standard establishes a system of graphic symbols of hydraulic and pneumatic circuits and components for all types of aerospace systems.

Aerospace series -- Graphic symbols for schematic drawings of hydraulic and pneumatic systems and components

GSO ISO 8829-1:2016 航空航天 聚四氟乙烯（PTFE）内管软管组件的试验方法 第1部分：金属（不锈钢）编织层

This part of ISO 8829 specifies test methods for flexible polytetrafluoroethylene (PTFE) inner tubes with metallic (stainless steel) 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. If performance requirements are not defined in this part of ISO 8829, they are defined in the performance 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. The requirements for non-metallic braid hose assemblies are given in ISO 8829-2.

Aerospace -- Test methods for polytetrafluoroethylene (PTFE) inner-tube hose assemblies -- Part 1: Metallic (stainless steel) braid

GSO ISO 9538:2016 航空航天 液压管接头和配件 平面弯曲试验

This International Standard specifies a flexure test procedure for reconnectable and permanent hydraulic tube joints. This procedure is intended for conducting flexure tests on fittings with high-strength hydraulic tubes made of corrosion-resisting steel, nimonic, titanium and aluminium for use on commercial and military aircraft.

Aerospace -- Hydraulic tubing joints and fittings -- Planar flexure test

GSO ISO 8177:2016 航空航天 用于流体系统的 Omega 夹具（鞍形夹具） 尺寸

This International Standard specifies maximum and minimum dimensions for omega clamps (saddle clamps) installed by means of two bolts with nominal diameters of 5 mm. The specified dimensions define a dimensional envelope. This international Standard shall not be considered as an interchangeability standard. The tolerances for each type of clamp are to be defined in the parts standards drawings.

Aerospace -- Omega clamps (saddle clamps) for fluid systems -- Dimensions

GSO ISO 9938:2016 航空航天 聚四氟乙烯 (PTFE) 软管组件 分类 204 摄氏度/28 000 kPa 采购规范

This International Standard specifies requirements for polytetrafluoroethylene (PTFE) hose assemblies for use in aircraft hydraulic systems at temperatures between − 55 °C and + 204 °C and at a nominal pressure up to 28 000 kPa (280 bar). 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. The use of these hose assemblies in high-pressure pneumatic storage systems is not recommended. In addition, installations in which the limits specified in this International Standard are exceeded, or in which the application is not covered specifically by this International Standard, for example for oxygen, shall be subject to the approval of the purchaser.

Aerospace -- Polytetrafluoroethylene (PTFE) hose assemblies, classification 204 degrees C/28 000 kPa -- Procurement specification

GSO ISO 7257:2016 飞机—液压管接头和配件—旋转弯曲试验

This International Standard specifies flexure test procedures to determine and classify the fatigue strengths of reconnectable or permanent hydraulic tube joints. The procedure is intended for conducting flexure tests of fittings and joints with high strength hydraulic tubes of various alloys such as corrosion resistant steel, Nimonic, titanium and aluminum alloy hydraulic tube for use on commercial and military aircraft. A mean stress is applied by holding system pressure in the specimens and then flexing in a rotary bending test machine.

Aircraft -- Hydraulic tubing joints and fittings -- Rotary flexure test

GSO ISO 6771:2016 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

GSO ISO 8775:2016 航空航天 流体系统用气态氧补充连接件（新型） 尺寸（英制系列）

This International Standard specifies the mating dimensions and access clearance for a gaseous oxygen replenishment coupling for aircraft.

Aerospace -- Gaseous oxygen replenishment connection for use in fluid systems (new type) -- Dimensions (Inch series)

GSO ISO 8153-1:2016 航空航天流体系统和部件 词汇 第1部分：软管组件

This part of ISO 8153 defines terms used for all types of hose assemblies. General terms can be made more precise through the addition of supplementary terminology relating to the design, range of application and/or the material of the hose/hose assembly. Terms and definitions specific to metallic hose assemblies are given in ISO 7369. NOTE Certain concepts used in this part of ISO 8153 are not applicable to all types of hose assemblies, but only to specific types, e.g. the term “insert” does not apply to a flexible metal hose without an insert as defined by this part of ISO 8153.

Aerospace fluid systems and components -- Vocabulary -- Part 1: Hose assemblies

GSO ISO 22072:2016 航空航天 电动静压执行器（EHA） 采购规范中定义的特性

This International Standard defines the general characteristics, requirements and design data to be included in the procurement technical specification of an electrohydrostatic actuator (EHA) to be used to power aircraft control surfaces or other moving parts of an aerospace vehicle. This type of actuator is an alternative to the hydraulically powered servo-control actuators that are currently used. It is intended that this International Standard cover the unique requirements of EHAs.

Aerospace -- Electrohydrostatic actuator (EHA) -- Characteristics to be defined in procurement specifications

GSO ISO 8625-3:2016 航空航天 流体系统 词汇 第3部分：与温度有关的通用术语和定义

This part of ISO 8625 defines general terms relating to temperature in fluid systems used in aerospace construction.

Aerospace -- Fluid systems -- Vocabulary -- Part 3: General terms and definitions relating to temperature