A hybrid wing-body aircraft includes a body section having an aerodynamic lift surface. The body section includes an upper body and a lower body. The hybrid wing body aircraft also includes a plurality of hybrid wing sections further defining a body section. The hybrid wing body aircraft includes one or more grooves in the body section. One or more grooves extend from the upper body toward the lower body. The hybrid wing body aircraft also includes one or more open fan engines mounted at least partially within the one or more grooves. One or more open fan engines ingest a portion of a boundary layer of the hybrid wing body aircraft.

    一种混合翼身飞行器,包括具有空气动力学升力表面的本体区段。本体区段包括上本体和下本体。混合翼身飞行器还包括进一步限定本体区段的多个混合机翼区段。混合翼身飞行器在本体区段中包括一个或多个凹槽。一个或多个凹槽从上本体朝向下本体延伸。混合翼身飞行器还包括至少部分地安装在一个或多个凹槽内的一个或多个开式风扇发动机。一个或多个开式风扇发动机摄取混合翼身飞行器的边界层的一部分。


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    Titel :

    Hybrid wing body aircraft


    Weitere Titelangaben:

    混合翼身飞行器


    Beteiligte:

    Erscheinungsdatum :

    2023-10-20


    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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