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Aircraft/Engine Fuel Pump Two Phase (Slugging Flow) Inlet Performance Test and Evaluation
- Aerospace Standard
Published April 29, 2020 by SAE International in United States
Downloadable datasets availableAnnotation ability available
This procedure is intended to apply to all engine or airframe mounted fuel pumps and controls when required by the applicable specification. The procedure recommends a recirculation system similar to ARP492 to control the fuel properties affecting the fluid and its ability to "release" fuel vapors and dissolved air and have these "re-entrained or dissolved" during the fluid recovery process back to the tank and the original starting conditions.
ARP4028 has been reaffirmed to comply with the SAE five-year review policy.
|Aerospace Standard||Aircraft Engine Fuel Pump Cavitation Endurance Test|
|Technical Paper||Designing for V/L Performance in an Aircraft Engine Fuel Pump|
|Aerospace Standard||Aircraft/Engine Fuel Pump Net Positive Suction Pressure Performance Test and Evaluation|
Data Sets - Support Documents
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