The invention relates to an engine (2) for a flying body (1), with an annular vortex guide element (3) which, seen in section, has an air inlet opening (6) arranged centrally with respect to a longitudinal central axis (4) of the engine (2) and, at a distance from the air inlet opening (6), an air outlet opening (7) arranged centrally with respect to the longitudinal central axis (4), which are connected to one another in terms of flow via an intake duct (5) bounded by the vortex guide element (3) and accommodating an air conveying device (8), wherein the air outlet opening (7) is overlapped by an air deflecting element (9) which is arranged geodetically above the vortex guide element (3) during intended operation of the engine (2) and which extends radially outwards from the air outlet opening (7) so that it delimits with the vortex guide element (3) an air exit gap (11) which is in flow connection with the air outlet opening (7). It is provided that the vortex guide element (3) is in the form of a body of rotation which is formed by rotation about an axis of rotation of a closed curve having a continuous course at least on its radially outer side, and in that the air inlet opening (6) opens directly into an outer environment (19) of the engine (2), so that during intended operation of the engine (2) air is conveyed from the side of the engine (2) facing away from the air deflecting element (9) through the air inlet opening (6) into the intake duct (5). The invention further relates to a method for operating an engine (2) for a flying body (1) as well as a flying body (1) with at least one engine (2).


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    Title :

    TRIEBWERK FÜR EINEN FLUGKÖRPER, VERFAHREN ZUM BETREIBEN EINES TRIEBWERKS FÜR EINEN FLUGKÖRPER SOWIE FLUGKÖRPER MIT WENIGSTENS EINEM TRIEBWERK


    Additional title:

    ENGINE FOR AN AIRCRAFT, METHOD FOR OPERATING AN ENGINE FOR AN AIRCRAFT, AND AIRCRAFT HAVING AT LEAST ONE ENGINE
    MOTEUR POUR UN AÉRONEF, PROCÉDÉ DE FONCTIONNEMENT D'UN MOTEUR POUR UN AÉRONEF, ET AÉRONEF COMPORTANT AU MOINS UN MOTEUR


    Contributors:

    Publication date :

    2025-04-30


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    German


    Classification :

    IPC:    B60V Luftkissenfahrzeuge , AIR-CUSHION VEHICLES / B64C AEROPLANES , Flugzeuge




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