The invention discloses a flap retracting and releasing device and an aircraft, the aircraft comprises a wing and flaps, the flap retracting and releasing device comprises retracting and releasing mechanisms, the retracting and releasing mechanisms are arranged on the wing, each flap is correspondingly provided with one retracting and releasing mechanism, and each retracting and releasing mechanism comprises a first retracting and releasing assembly and a second retracting and releasing assembly which are in driving connection with the corresponding flap; the first folding and unfolding assembly and the second folding and unfolding assembly are symmetrically arranged about the length center line of the flap; the driving mechanism is arranged between the first folding and unfolding assembly and the second folding and unfolding assembly; the driving mechanism is in driving connection with the retracting and releasing mechanism through the transmission mechanism, the transmission mechanism comprises a first transmission assembly and a second transmission assembly, and the driving mechanism is in driving connection with the first retracting and releasing assembly through the first transmission assembly and is in driving connection with the second retracting and releasing assembly through the second transmission assembly; and the first folding and unfolding assembly and the second folding and unfolding assembly are driven to synchronously drive the flap to fold and unfold. According to the technical scheme, the problem that the flap is prone to clamping stagnation in the folding and unfolding process is solved.

    本发明公开一种襟翼收放装置和飞行器,其中,飞行器包括机翼和襟翼,襟翼收放装置包括:收放机构,设于机翼,每一襟翼对应设置一收放机构,收放机构包括与襟翼驱动连接的第一收放组件和第二收放组件,第一收放组件和第二收放组件关于襟翼的长度中心线对称设置;驱动机构,设于第一收放组件和第二收放组件之间;以及传动机构,驱动机构通过传动机构与收放机构驱动连接,传动机构包括第一传动组件和第二传动组件,驱动机构通过第一传动组件与第一收放组件驱动连接且通过第二传动组件与第二收放组件驱动连接,以驱使第一收放组件和第二收放组件同步驱动襟翼收放。本发明技术方案解决了襟翼在收放过程中易卡滞的问题。


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    Title :

    Flap folding and unfolding device and aircraft


    Additional title:

    襟翼收放装置和飞行器


    Contributors:
    WU WEI (author) / QU HUMIN (author) / ZHANG ZIQIAN (author) / WANG CHAO (author) / YU XIN (author)

    Publication date :

    2023-06-30


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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