The invention discloses an aircraft morphing nose cone and a morphing aircraft, and belongs to the field of morphing aircrafts. Comprising a plurality of nose cone shells, the nose cone shells are sequentially arranged in the first direction, and every two adjacent nose cone shells can move relatively; any two adjacent nose cone shells are connected through the first driving chain groups and the second driving chain groups, and the first driving chain groups and the second driving chain groups are distributed at intervals in the second direction; when the first driving chain group and the second driving chain group are switched from an unlocking state to a locking state, the two adjacent nose cone shells are far away from each other, so that the aircraft variant nose cone extends; when the first driving chain group and the second driving chain group are switched from a locking state to an unlocking state, the two adjacent nose cone shells are close to each other, so that the aircraft variant nose cone is shortened; and when the running speed of the first driving chain group is higher than that of the second driving chain group, the aircraft variant nose cone is bent.

    本申请公开了一种飞行器变体头锥及变体飞行器,属于变体飞行器领域。包括:多个头锥外壳,多个头锥外壳沿第一方向依次设置,相邻两个头锥外壳之间可相对移动;多个第一驱动链组和多个第二驱动链组,任意相邻的两个头锥外壳通过第一驱动链组以及第二驱动链组连接,且第一驱动链组与第二驱动链组沿第二方向间隔分布;在第一驱动链组以及第二驱动链组均由解锁状态向锁紧状态切换时,相邻两个头锥外壳之间相互远离,以使飞行器变体头锥伸长;在第一驱动链组与第二驱动链组均由锁紧状态向解锁状态切换时,相邻两个头锥外壳之间相互靠近,以使飞行器变体头锥缩短;在第一驱动链组的运行速度大于第二驱动链组的运行速度时,飞行器变体头锥弯曲。


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    Title :

    Aircraft variant nose cone and variant aircraft


    Additional title:

    飞行器变体头锥及变体飞行器


    Contributors:
    YAN SHAOZE (author) / ZHANG YULING (author) / GU YONGXIA (author) / WU HONGYU (author) / HAO YUXING (author) / TIAN JINGYI (author) / YANG JIAWEN (author)

    Publication date :

    2024-05-28


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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