共找到 272 条与 液压、冷气系统及其附件 相关的标准,共 19 页
General specification for aircraft constant pressure variable hydraulic pump
General specification for variable displacement hydraulic pumps driven by AC induction motors for aircraft
General requirements of braking antiskid system for civil aircraft
Aerospace series. Hydraulic tubing joints and fittings. Planar flexure test
Aerospace series. AC induction electric motor driven, variable delivery, hydraulic pumps. General requirements
Aerospace. Cleanliness classification for hydraulic fluids
Aerospace - Cleanliness classification for hydraulic fluids
Aerospace. Fluid systems. Hydraulic system tubing
Aircraft. Hydraulic tubing joints and fittings. Rotary flexure test
Aircraft - Hydraulic tubing joints and fittings - Rotary flexure test
Aerospace series. Constant displacement hydraulic motors. General specifications
Aerospace series. Hydraulic, pressure compensated, variable delivery pumps. General requirements
This International Standard establishes the general requirements for pressure compensated, variable delivery hydraulic pumps, suitable for use in aircraft hydraulic systems at pressures up to 35000 kPa (5000 psi). This International Standard is to be used in conjunction with detail specifications that is particular to each application.
Aerospace series - Hydraulic, pressure compensated, variable delivery pumps - General requirements
Aerospace series - Constant displacement hydraulic motors - General specifications
Aerospace series. Fluid, hydraulic, phosphate ester-base, fire resistant. Technical specification
Aerospace series. Pipe coupling 8
Each engine, with all icing protection systems operating, must
Aeronautics and space. Part33:Airworthiness standards: aircraft engines. SubpartE:Design and construction;turbine aircraft engines. Section33.68:Induction system icing.
(a)–(b) [Reserved] (c) Ingestion of ice under the conditions of paragraph (e) of this section may not
Aeronautics and space. Part33:Airworthiness standards: aircraft engines. SubpartE:Design and construction;turbine aircraft engines. Section33.77:Foreign object ingestion-ice.
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
Aerospace - Separable tube fittings for fluid systems, for 24° cones, for pressures up to 3000 psi or 21000 kPa - Procurement specification, inch/metric
本标准规定了液压脉冲试验台的关键部件组成、要求和操作方法。 本标准适用于液压软管组件、硬管、盘旋管、接头、作动筒、阀、压力容器及类似液压系统部件的标准液压脉冲试验台的研制。
General requirement for hydraulic impulse test stand
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