To reduce the number of necessary actuators, improve reliability and redundancy, as well as reducing weight and fuel consumption, a thrust reverser assembly configured for reversing thrust of an aircraft engine is proposed. The thrust reverser assembly comprises flaps and linkage arrangements, wherein the flaps are driven between a stowed position and a deployed position by the linkage arrangement due to an axial movement of a part of the engine nacelle. The linkage arrangement is configured as a four bar linkage, in particular, a double rocker bar linkage.


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    Title :

    Thrust reverser assembly for an engine nacelle of an aircraft


    Contributors:

    Publication date :

    2022-05-03


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    F02K JET-PROPULSION PLANTS , Strahltriebwerke / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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