Accumulator, Hydraulic, Cylindrical Aircraft, Self-Displacing
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Product Code: ARP4553
Date Published: 1997-10-01 - A newer version of this standard is available.
Date Reaffirmed: July 2002
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°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.
Product Status: In Stock
File Size:
235K
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| Current & Historical versions of this standard |
|---|
| Standard |
Date published |
?Status |
| ARP4553A |
2008-12-19 |
Revised |
| ARP4553 |
1997-10-01 |
Reaffirmed |
|
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