共找到 272 條與 液壓、冷氣系統(tǒng)及其附件 相關(guān)的標(biāo)準(zhǔn),共 19 頁
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
Aerospace series - Constant displacement hydraulic motors - General specifications
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. Fluid, hydraulic, phosphate ester-base, fire resistant. Technical specification
Aerospace series. Pipe coupling 8
(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.
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.
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
本標(biāo)準(zhǔn)規(guī)定了民用飛機(jī)氣動系統(tǒng)的設(shè)計要求(包括設(shè)計依據(jù)、設(shè)計準(zhǔn)則、一般要求、詳細(xì)要求、設(shè)計程序及設(shè)計驗證)和安裝要求。 本標(biāo)準(zhǔn)適用于民用飛機(jī)氣動系統(tǒng)設(shè)計和安裝。
Design and installation requirements for pneumatic system of civil aircraft
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