SAE ARP4553

Accumulator, Hydraulic, Cylindrical Aircraft, Self-Displacing.

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Standard:
  • ARP4553
Reaffirmed:
  • 2002-07-16
Revised:
  • 1997-10-01
Revision:
  • Historical. Access the latest revision: ARP4553A
Issuing:
  • A-6c6 Power Sources Committee
Scope:

This SAE Aerospace Recommended Practice (ARP) is intended as a guide in defining the requirements for aircraft hydraulic self-displacing accumulators, including details pertinent to the design, fabrication, and performance of the accumulator. This type of accumulator has a piston separator and contains a low pressure chamber and a high pressure chamber for actuating a self-displacing piston. For use in aircraft hydraulic systems of the following types as defined in MIL-H-5440 with rated operating pressures to 8000 psi (55,160 kPa). Type I: -65 to +160 °F (-54 to +71 °C) fluid temperature; Type II: -65 to +275 °F (-54 to +135 °C) fluid temperature. For commercial aircraft applications, the information and guidelines of ARP4752 are considered.

History:
StandardPublishedRevisionStatus
ARP4553A2008-12-19LatestRevised
ARP45531997-10-01HistoricalReaffirmed
AKA:
  • SAE ARP 4553
Sector:
  • Aerospace
Topic:
  • Hydraulic systems

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