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SAE AIR4002A

8000 psi Hydraulic Systems: Experience and Test Results

Standard by SAE International, 2012-11-15

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  • Language: English
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About This Item

Shortly after World War II, as aircraft became more sophisticated and power-assist, flight-control functions became a requirement, hydraulic system operating pressures rose from the 1000 psi level to the 3000 psi level found on most aircraft today. Since then, 4000 psi systems have been developed for the U.S. Air Force XB-70 and B-1 bombers and a number of European aircraft including the tornado multirole combat aircraft and the Concorde supersonic transport. The V-22 Osprey incorporates a 5000 psi hydraulic system. The power levels of military aircraft hydraulic systems have continued to rise. This is primarily due to higher aerodynamic loading, combined with the increased hydraulic functions and operations of each new aircraft. At the same time, aircraft structures and wings have been getting smaller and thinner as mission requirements expand. Thus, internal physical space available for plumbing and components continues to decrease. This document has been determined to contain basic and stable technology which is not dynamic in nature.
SKU: 3a2ed0555d37

  • Publication Date: 2012-11-15
  • Standard Status: latest
  • Publisher: SAE International
  • Document Type: Aerospace Standard
  • Subject: Fluid power systems, Flight control systems, Military aircraft, Hydraulic systems, Hydraulic fluids, Engine mounts, Pressure, Titanium alloys, Seals and gaskets
  • Official SAE: Doi link

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