The invention discloses a symmetrical multi-connecting-rod electrically-driven aircraft landing gear structure which comprises a main driving mechanism, a follow-up mechanism and a main supporting column. The driving end of the main driving mechanism is hinged to the main supporting column, the top of the main supporting column is hinged to the machine body, and the bottom of the main supporting column is connected with tires. The follow-up mechanism comprises a first four-bar mechanism, a second four-bar mechanism, a right supporting column rocker and a left supporting column rocker, the first four-bar mechanism and the second four-bar mechanism are symmetrically arranged, one end of the first four-bar mechanism and one end of the second four-bar mechanism are hinged to the machine body, and the other end of the first four-bar mechanism and the other end of the second four-bar mechanism are hinged to a fixed support on the main supporting column. End connecting rods, close to the machine body, of the first four-bar mechanism and the second four-bar mechanism are hinged to the main supporting column through a right supporting column rocker and a left supporting column rocker respectively. The structure is light and compact, reliability, stability and safety are guaranteed, the requirement of an electric drive mode for high power is lowered, the stable, reliable and light supporting requirements of the aircraft landing gear are met, and good practicability is achieved.

    本发明公开了一种对称式多连杆电驱飞机起落架结构,包括主驱动机构、随动机构、主支柱;所述主驱动机构的驱动端与主支柱铰接,所述主支柱的顶部与机体铰接,且底部连接有轮胎;所述随动机构包括对称设置的第一四连杆机构、第二四连杆机构以及右支柱摇杆、左支柱摇杆,所述第一四连杆机构、第二四连杆机构的一端分别与机体铰接,且另一端分别与主支柱上的固定支座铰接;所述第一四连杆机构、第二四连杆机构靠近机体的端部连杆分别通过右支柱摇杆、左支柱摇杆与主支柱铰接。本发明结构轻巧、紧凑,保证了可靠性、稳定性和安全性,降低了电驱方式对高功率的要求,实现了飞机起落架稳定、可靠、轻便的支撑需求,具有较好的实用性。


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    Titel :

    Symmetrical multi-connecting-rod electrically-driven aircraft landing gear structure


    Weitere Titelangaben:

    一种对称式多连杆电驱飞机起落架结构


    Beteiligte:
    ZHONG XUEMIN (Autor:in) / YE BO (Autor:in) / ZHOU JIA (Autor:in) / WANG DANYANG (Autor:in) / HE LEI (Autor:in) / CAO HU (Autor:in) / PU HAILONG (Autor:in) / TAN YULONG (Autor:in) / LI ZHUOLONG (Autor:in)

    Erscheinungsdatum :

    28.06.2022


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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