A flow control system on an aircraft engine nacelle incorporates a plurality of flow control devices each having a body. A second plurality of actuators is coupled to the body of an associated one of the flow control devices. The actuator rotates the body about a leading edge of an inlet of a nacelle from a retracted position to an extended position.

    Le système de régulation du flux de nacelle de moteur d'aéronef comprend une pluralité de dispositifs de régulation de débit, chacun ayant un corps. Une deuxième pluralité dactionneurs est couplée au corps de lun de ces derniers associé aux dispositifs de régulation de débit. Lactionneur tourne le corps autour du bord d'attaque dune entrée de nacelle de la position rentrée à la position sortie.


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    Title :

    ROTATING DEVICES FOR MITIGATION OF ADVERSE FLOW CONDITIONS IN AN ULTRA-SHORT NACELLE INLET


    Additional title:

    APPAREILS ROTATIFS SERVANT A ATTENUER LES CONDITIONS DE FLUX NUISIBLES DANS UNE ENTREE DE NACELLE ULTRA COURTE


    Contributors:

    Publication date :

    2022-06-28


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

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



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