A retractable landing gear assembly for an aircraft, having: a main strut (210) arranged to pivot between a retracted position and an extended position; and a side stay (220) having an unfolded position and a folded position. A telescopic actuator (250) is coupled between the main strut (210) and the side struts (220) such that when the actuator (250) has a first length, the side struts (220) lock the main strut (210) in an extended position, and when the actuator (250) has a second length, the side struts (220) are in a folded position and the main strut (210) are in a retracted position.

    一种用于飞行器的可缩回式起落架组件,其具有:主支柱(210),该主支柱布置成在缩回位置与伸展位置之间枢转;以及侧撑杆(220),该侧撑杆具有展开位置和折叠位置。伸缩式致动器(250)联接在主支柱(210)与侧撑杆(220)之间,使得:当致动器(250)具有第一长度时,侧撑杆(220)将主支柱(210)锁定处于伸展位置,并且当致动器(250)具有第二长度时,侧撑杆(220)处于折叠位置并且主支柱(210)处于缩回位置。


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    Titel :

    Retractable landing gear assembly for aircraft


    Weitere Titelangaben:

    用于飞行器的可缩回式起落架组件


    Beteiligte:

    Erscheinungsdatum :

    2023-11-28


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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