The invention relates to a thrust group (300) for a propulsion device (10), comprising a thrust engine (302), arranged to provide a thrust force (F1, F2) oriented in a direction so as to provide substantially vertical take-off and landing capability, a deflector assembly (304) comprising a pair of deflecting elements (306a, 306b) arranged to selectively divert the ejected fluid and movably mounted in the fluid outlet path. In order to reduce the bulk of the thrust group and improve reliability and responsiveness, the invention relates more particularly to the positioning of the deflecting elements opposite the ejected fluid.


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    Title :

    Thrust group for a propulsion device and associated propulsion device


    Contributors:

    Publication date :

    2024-02-01


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    F02K JET-PROPULSION PLANTS , Strahltriebwerke / B64C AEROPLANES , Flugzeuge



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