49.080 航空航天用流体系统和零部件 标准查询与下载

GSO ISO 8625-4:2016 航空航天 流体系统 词汇 第4部分：与控制/驱动系统相关的通用术语和定义

This part of ISO 8625 defines general terms relating to control/actuation systems in the field of aerospace fluid systems and components.

Aerospace -- Fluid systems -- Vocabulary -- Part 4: General terms and definitions relating to control/actuation systems

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 9206:2016 航空航天 恒排量液压马达 通用技术条件

This International Standard lays down the general specifications for constant displacement hydraulic motors to be installed in aircraft, which transform hydraulic power into mechanical energy in the form of a rotational torque. Primary and secondary function motors (see clause 3) are covered in this International Standard; actuators with internal rotation angle limits and low-speed motors are not covered in this International Standard. This International Standard shall be used in conjunction with the detail specification particular to each application. NOTE — A schematic summary is provided in annex A for easy reference to the contents of this International Standard.

Aerospace -- Constant displacement hydraulic motors -- General specifications

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 8829-2:2016 航空航天 聚四氟乙烯 (PTFE) 内管软管组件试验方法 第2部分：非金属编织层

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

GSO ISO 9528:2016 航空航天 标准重量聚四氟乙烯 (PTFE) 软管组件 分类 204 摄氏度/21 000 kPa 采购规范

This International Standard specifies requirements for standard-weight 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 21 000 kPa (210 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 can 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 -- Standard-weight polytetrafluoroethylene (PTFE) hose assemblies, classification 204 degrees C/21 000 kPa -- Procurement specification

GSO ISO 17775:2016 飞机 地面服务连接 饮用水、厕所冲水和厕所排水

This International Standard specifies the detail dimensions of the male connector interfaces, fitted to an aircraft, used for servicing of the potable water systems, the toilet-flush water systems, and the toilet drain systems currently in common use. This International Standard is applicable to all commercial aircraft with water and toilet systems and is recommended for military and private aircraft that use water and toilet systems. This International Standard does not include requirements for the ground half (female) couplings or protective caps, but provides sufficient interface details for such items to be designed. It does not include any specified dimensions for the clearance required around the connector on the aircraft body itself for either any protective caps or ground half couplings, although general recommendations are made.

Aircraft -- Ground-service connections -- Potable water, toilet-flush water and toilet drain

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 8625-1:2016 航空航天 流体系统 词汇 第1部分：与压力相关的通用术语和定义

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

Aerospace -- Fluid systems -- Vocabulary -- Part 1: General terms and definitions related to pressure

GSO ISO 23935:2016 飞机—机载流体系统部件的环境试验程序—指定火区的耐火性

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

GSO ISO 6772:2016 航空航天 流体系统 液压软管、管道和配件组件的脉冲测试

This International Standard specifies the requirements and the procedures for impulse testing of hose, tubing, and fitting assemblies for use in aerospace hydraulic systems. Requirements may apply, when appropriate, to components used in other aerospace fluid systems.

Aerospace -- Fluid systems -- Impulse testing of hydraulic hose, tubing and fitting assemblies

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 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 7320:2016 航空航天 流体系统用螺纹密封联轴器 尺寸

This International Standard establishes a system for sealing the port connection of couplings used in the aerospace industry. It specifies dimensions to achieve interchangeability of the port connection, the fitting end and a seal. The seal may be a standard O-ring or a special ring.

Aerospace -- Couplings, threaded and sealed, for fluid systems -- Dimensions

BS ISO 8575:2016 航空航天. 流体系统. 液压系统管路

Aerospace. Fluid systems. Hydraulic system tubing

KS W ISO 7314-2016 航空航天 流体系统 金属软管组件

Aerospace－Fluid systems－Metal hose assemblies

KS W ISO 5887-2016 飞机 机组人员调节面罩与氧气源的连接接头

Aircraft－Joints for connecting crew members'' regulator masks to oxygen sources

KS W ISO 7661-2016 航空航天 流体系统 用于轴向对准的管路的夹具 设计标准和鉴定测试 公制系列

Aerospace－Fluid systems－Clamp blocks for tube lines having axial alignment－Design standard and qualification testing－Metric series

KS W ISO 7315-2016 航空航天 流体系统用“P”型夹具（环形夹具） 外壳尺寸

Aerospace－“P”clamps(loop clamps)for fluid systems－Envelope dimensions