An engine (310) of a vertical take-off and landing aircraft (300) is provided, where the engine is configured to be movable relative to an aircraft component (342) of the aircraft (300) between a hovering position for take-off and landing and a cruising position for forward flight, where the engine (310) comprises an aerodynamic component (332), the aerodynamic component (332) has at least one aerodynamic element (334) movable between a first position (336) in accordance with a first operating state of the aircraft and a second position (338) in accordance with a second operating state of the aircraft, the aerodynamic element defining an aerodynamic surface in contact with airflow passing through the engine.

    本发明提供了一种垂直起降飞行器(300)的发动机(310),其中发动机配置成能相对于飞行器(300)的飞行器部件(342)在用于起降的悬停位置与用于向前飞行的巡航位置之间移动,其中发动机(310)包括空气动力学部件(332),空气动力学部件(332)具有至少一个空气动力学元件(334),空气动力学元件(334)能在根据飞行器的第一操作状态的第一位置(336)与根据飞行器的第二操作状态的第二位置(338)之间移动,空气动力学元件限定与穿过发动机的气流接触的空气动力学表面。


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    Titel :

    Aircraft engine including variable area discharge nozzle


    Weitere Titelangaben:

    包括可变面积排放喷嘴的飞行器发动机


    Beteiligte:

    Erscheinungsdatum :

    06.09.2022


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

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



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