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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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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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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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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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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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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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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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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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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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Aerospace - Application Guide for Hydraulic Power Transfer Units

A-6C4 Power Sources Committee
  • Aerospace Standard
  • ARP1280B
  • Current
Published 2014-11-13 by SAE International in United States
This SAE Aerospace Recommended Practice (ARP) is an application guide for hydraulic power transfer units and describes: The various types Typical design approaches Their operational characteristics and limitations Circuit recommendations Typical applications The scope of this ARP is limited to devices that transfer power between hydraulic systems and do so by means of rotary subassemblies such as hydraulic motors and pumps.
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