An airflow disruptor (34, 134, 234) for a gas turbine engine bleed air exhaust port (28) employs a disruptor plate (36) rotatably mounted upstream from an exhaust port (28) of an exhaust duct (26). An actuator is coupled to the disruptor plate (36) and adapted to rotate the disruptor plate (36) into an external airflow (29) responsive to temperature of exhaust flow (31) in the exhaust port (28) whereby the external airflow (29) is turbulated upstream of the exhaust port (28).


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    Title :

    ANTI-ICE SYSTEM EXHAUST AIR DISRUPTOR


    Additional title:

    ANTI-EIS-SYSTEM-ABLUFTDISRUPTOR
    DÉSINTÉGRATEUR D'AIR D'ÉCHAPPEMENT DE SYSTÈME ANTIGIVRE


    Contributors:

    Publication date :

    2023-07-05


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64C AEROPLANES , Flugzeuge



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