共找到 2366 条与 航空航天用流体系统和零部件 相关的标准,共 158 页
Aerospace. Cleanliness classification for hydraulic fluids
Aerospace - Cleanliness classification for hydraulic fluids
Aviation equipment. Hydraulic system. Equal flange tees and transitive branches bulkhead on run for tube connections on internal cone 24°
Aviation equipment. Hydraulic system. Equal tees and transitive branches for tube connections on internal cone 24° with an inner connection on run
Aviation equipment. Hydraulic systems. Fittings, pipes, for pumping systems for environments for external crimping. Technical specifications
Aviation equipment. Hydraulic system. Equal flange tees and transitive branches bulkhead on side for tube connections on internal cone 24°
Aviation equipment. Hydraulic systems. Branch pipes, tips with outer cone, for internal expansion
Aviation equipment. Hydraulic systems. The order of handling of products containing hoses, and their installation in aircraft products
Aviation equipment. Hydraulic systems. Pass-through and transitional connectors, under axial pressure fitting for pressure 35 MPa. Angle connector, coupling - nipple with nut
Aviation equipment. Hydraulic system. Assembly, installation and torque for flareless and straight thread fluid fittings and tube assemblies
Aviation equipment. Hydraulic system. Union and reducing elbows 90° for tube connections on internal cone 24°
Aviation equipment. Hydraulic systems. Straight, cross, triple, transitional and transitional connectors, under axial pressing for a pressure of 35 MPa. Specifications
Aviation equipment. Hydraulic system. Straight and transient crosses for tube connections on internal cone 24°
Limited-movable connections of pipelines of a fuel system of the aircraft equipment. Metric series
Aviationequipment. Hydraulic system. Unions and adapters for tube connections on internal cone 24°
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
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
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
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