The invention belongs to the technical field of airplane static tests, and particularly relates to a multi-point coordinated airplane hoisting device. Comprising a first upper frame, a second upper frame and a third upper frame, a front undercarriage is fixedly installed in the first upper frame, a left main undercarriage is fixedly installed in the second upper frame, and a right main undercarriage is fixedly installed in the third upper frame; the first double-position control actuator cylinder assembly is installed on the first upper frame in the spanwise direction, the second double-position control actuator cylinder assembly is installed on the second upper frame in the heading direction, and the third double-position control actuator cylinder assembly is installed on the third upper frame in the heading direction. The third double-position control actuator cylinder assembly is installed on the third upper frame in the course direction. The full-floating support assembly comprises a first full-floating support assembly, a second full-floating support assembly and a third full-floating support assembly; the coordinated loading control system is used for controlling the double-position control actuator cylinder assembly to achieve airplane hoisting.

    本申请属于飞机静力试验技术领域,特别涉及一种多点协调的飞机起吊装置。包括:第一上框、第二上框以及第三上框,前起落架固定安装在所述第一上框内部,左主起落架固定安装在所述第二上框内部,右主起落架固定安装在所述第三上框内部;第一双位控作动筒组件、第二双位控作动筒组件以及第三双位控作动筒组件,所述第一双位控作动筒组件沿展向安装在所述第一上框上,所述第二双位控作动筒组件沿航向安装在所述第二上框上,所述第三双位控作动筒组件沿航向安装在所述第三上框上;全浮动支持组件包括第一全浮动支持组件、第二全浮动支持组件以及第三全浮动支持组件;协调加载控制系统用于控制所述双位控作动筒组件实现飞机起吊。


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    Titel :

    Multi-point coordinated airplane hoisting device


    Weitere Titelangaben:

    一种多点协调的飞机起吊装置


    Beteiligte:
    TIAN WENPENG (Autor:in) / YIN WEI (Autor:in) / HE YUEZHOU (Autor:in) / LIN JIFENG (Autor:in) / WANG XINTAO (Autor:in) / SONG PENGFEI (Autor:in)

    Erscheinungsdatum :

    2023-05-30


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B66C Krane , CRANES



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