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Aerospace (58)

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Hydraulic fluids (29) Hydraulic systems (29) Electric motors (18) Pumps (17) Environmental testing (16) Pressure (16) Commercial aircraft (14) Identification numbers (12) Stop / start technology (12) Aluminum alloys (9) Hydraulic equipment (9) Hydraulic motors (9) Military aircraft (9) Test procedures (9) Solid propellants (8) Copper alloys (7) Corrosion (7) Compressors (5) Conductivity (5) Failure modes and effects analysis (5) Flight control systems (5) Fuel economy (5) Hydrazines (5) Physical examination (5) Quality control (5) Coatings, colorants, and finishes (4) Combustion chambers (4) Fuel consumption (4) Jet engines (4) Pneumatic systems (4) Radio frequency (4) Test facilities (4) Thrust reversers (4) Air cleaners (3) Aircraft (3) Automatic pilots (3) Batteries (3) Diesel / compression ignition engines (3) Energy conservation (3) Finishing (3) Fuel cells (3) Gas turbines (3) Heat resistant materials (3) Hydraulic control (3) Hydrogen fuel (3) Jet fuel (3) Lead-acid batteries (3) Liquid propellants (3) Plating (3) Spraying (3)

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A-6C4 Power Sources Committee (58)

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TEAA6C4 (58)

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Select Procedure for Inspection of In-Service Airborne Accumulators for Corrosion and Damage

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Procedure for Inspection of In-Service Airborne Accumulators for Corrosion and Damage

A-6C4 Power Sources Committee

Aerospace Standard
ARP4150A
Current

Published 2019-11-12 by SAE International in United States

This SAE Aerospace Recommended Practice (ARP) is a guide in establishing inspection procedures to determine the condition of in-service accumulators. Recommendations are also provided for corrective action if it is determined that the environment is contributing to the deterioration of the surface protection system treatments.

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Select Self-Displacing Hydraulic Accumulator

Self-Displacing Hydraulic Accumulator

A-6C4 Power Sources Committee

Aerospace Standard
ARP4553B
Current

Published 2018-09-04 by SAE International in United States

This SAE Aerospace Recommended Practice (ARP) provides recommendations for design and test requirements for self-displacing hydraulic accumulators.

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Select Motors, Aircraft Hydraulic, Constant Displacement General Specification For

Motors, Aircraft Hydraulic, Constant Displacement General Specification For

A-6C4 Power Sources Committee

Aerospace Standard
AS7997A
Current

Published 2018-08-15 by SAE International in United States

This Specification covers constant displacement hydraulic motors, generally remotely mounted, using hydraulic fluid under pressure as the energy transfer medium for driving various accessories. Hydraulic motors shall be suitable for use in aircraft hydraulic systems conforming to and as defined in MIL-H-5440 and MIL-H-8891 as applicable.

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Select Aerospace Hydraulic Pump Controls

Aerospace Hydraulic Pump Controls

A-6C4 Power Sources Committee

Aerospace Standard
AIR5872A
Current

Published 2017-05-10 by SAE International in United States

This SAE Aerospace Information Report (AIR) presents an overview of the application and control of fixed and variable displacement pumps with the emphasis on the controls most commonly used on variable displacement pumps. It describes various options to control the operation of hydraulic pumps in terms of controlling the pump output pressure and/or flow and assisting in the selection of the pump.

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Select Aerospace – System Integration Factors That Affect Hydraulic Pump Life

Aerospace – System Integration Factors That Affect Hydraulic Pump Life

A-6C4 Power Sources Committee

Aerospace Standard
AIR1922B
Current

Published 2017-02-13 by SAE International in United States

This SAE Aerospace Information Report presents the following factors that affect hydraulic pump life and performance: a The need to supply hydraulic fluid at the correct pressure and quality to the pump inlet port b Considerations for the pump output c Factors to be considered for the pump case drain lines d The mounting of the hydraulic pump e Hydraulic fluid properties, including cleanliness

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Select Accumulator, Hydraulic, Welded Bellows, Factory Pre-Charged

Accumulator, Hydraulic, Welded Bellows, Factory Pre-Charged

A-6C4 Power Sources Committee

Aerospace Standard
ARP4378C
Current

Published 2017-01-09 by SAE International in United States

This SAE Aerospace Recommended Practice (ARP) provides design and test requirements for high pressure, factory pre-charged, welded bellows hydraulic accumulators.

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Select Aerospace – Military Type Variable Delivery, Pressure Compensated Hydraulic Pump

Aerospace – Military Type Variable Delivery, Pressure Compensated Hydraulic Pump

A-6C4 Power Sources Committee

Aerospace Standard
AS19692B
Current

Published 2016-06-22 by SAE International in United States

This SAE Aerospace Standard (AS) establishes the general requirements for the design, construction, acceptance, and qualification testing of flat cut-off pressure compensated, variable delivery hydraulic pumps used in military aircraft hydraulic systems. It also provides parameters for a Procurement Specification to be used in conjunction with this AS. The hydraulic pumps defined by this AS are generally for use in aircraft hydraulic systems conforming to and as defined in AS5440 and MIL-H-8891, as applicable.

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Select Aerospace - Accumulator, Hydraulic, Cylindrical, Piston Separated

Aerospace - Accumulator, Hydraulic, Cylindrical, Piston Separated

A-6C4 Power Sources Committee

Aerospace Standard
ARP4379B
Current

Published 2016-04-20 by SAE International in United States

This SAE Aerospace Recommended Practice (ARP) is a guide for defining the requirements for aerospace piston hydraulic accumulators, including details pertinent to the design, fabrication, performance and testing of the accumulator. This type of accumulator contains a piston which separates pressurized gas and fluid.

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Select Aerospace Auxiliary Power Sources

Aerospace Auxiliary Power Sources

A-6C4 Power Sources Committee

Aerospace Standard
AIR744C
Current

Published 2015-10-26 by SAE International in United States

This SAE Aerospace Information Report (AIR) is a review of the general characteristics of power sources that may be used to provide secondary, auxiliary, or emergency power for use in aircraft, space vehicles, missiles, remotely piloted vehicles, air cushion vehicles, surface effect ships, or other vehicles in which aerospace technology is used. The information contained herein is intended for use in the selection of the power source most appropriate to the needs of a particular vehicle or system. The information may also be used in the preparation of a power source specification. Considerations for use in making a trade study and an evaluation of the several power sources are included. More detailed information relating to specific power sources is available in other SAE Aerospace Information Reports or in Aerospace Recommended Practices.

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Select Aerospace – Civil Type Variable Delivery, Pressure Compensated, Hydraulic Pump

Aerospace – Civil Type Variable Delivery, Pressure Compensated, Hydraulic Pump

A-6C4 Power Sources Committee

Aerospace Standard
AS595D
Current

Published 2015-10-26 by SAE International in United States

This SAE Aerospace Standard (AS) establishes the general requirements for the design, construction, acceptance and qualification testing of flat cut-off pressure compensated, variable delivery hydraulic pumps, used in civil aircraft hydraulic systems. It also provides parameters for a Procurement Specification to be used in conjunction with this AS for each pump. NOTE: Hydraulic pumps may incorporate features such as a clutch in the input drive, which will not be covered by this standard.

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