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.


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    Title :

    Aircraft/Engine Fuel Pump Two Phase (Slugging Flow) Inlet Performance Test and Evaluation


    Publication date :

    2020-04-29



    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English