A pressure relief system (400) is provided and a corresponding method (600) for relieving pressure from a duct (402) routing a gas from a compressor (103) to a load utilizing the same. According to one aspect, a pressure relief assembly (104), located near the load, and independent of the primary load compressor pressure relief valve (104), for use with the duct includes a cover (222), first and second chambers (212, 214), and a piston (220). The piston provides a moveable wall between the chambers and is coupled to the cover. As gas from the duct enters the two chambers, the configuration of the chambers provides for a pressure differential that moves the piston and the corresponding cover. This movement transitions the cover from a closed configuration that seals the duct to an open configuration that allows gas within the duct to escape.


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    Title :

    COMPRESSOR SURGE PROTECTION


    Additional title:

    VERDICHTERPUMPSCHUTZ
    PROTECTION CONTRE LE POMPAGE DU COMPRESSEUR


    Contributors:

    Publication date :

    2019-12-04


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    F16K VALVES , Ventile / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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