SAE ARP4553 Accumulator, Hydraulic, Cylindrical Aircraft, Self-Displacing
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Product Code:SAE ARP4553
Title:Accumulator, Hydraulic, Cylindrical Aircraft, Self-Displacing
Issuing Committee: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掳F (-54 to +71掳C) fluid temperature; Type II: -65 to +275掳F (-54 to +135掳C) fluid temperature. For commercial aircraft applications, the information and guidelines of ARP4752 are considered.
Title:Accumulator, Hydraulic, Cylindrical Aircraft, Self-Displacing
Issuing Committee: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掳F (-54 to +71掳C) fluid temperature; Type II: -65 to +275掳F (-54 to +135掳C) fluid temperature. For commercial aircraft applications, the information and guidelines of ARP4752 are considered.
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