An aircraft comprising a fuselage, a pair of wings connected to an upper portion of the fuselage, and a pair of wing support struts, each wing support strut being connected between a lower portion of the fuselage and an underside of the adjacent wing, wherein at least one centre landing gear assembly is connected to the fuselage and is configured to be retractable within the fuselage, and a respective outrigger landing gear is connected to each wing support strut, each outrigger landing gear being configured to be retractable within the respective wing support strut.

    一种飞行器,包括:机身;一对机翼,该对机翼连接到机身的上部;以及一对机翼支撑支柱,每个机翼支撑支柱连接在机身的下部与相邻的机翼下侧之间,其中至少一个中央起落架组件连接到机身并构造成在机身内可缩回,并且相应的外伸支架式起落架连接到每个机翼支撑支柱,每个外伸支架式起落架构造成在相应的机翼支撑支柱内可缩回。


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    Titel :

    AIRCRAFT HAVING OUTRIGGER LANDING GEAR


    Weitere Titelangaben:

    具有外伸支架式起落架的飞行器


    Beteiligte:

    Erscheinungsdatum :

    03.12.2021


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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