The invention belongs to the field of bionic flying robot equipment, and discloses a bionic butterfly mixed control wing ornithopter which comprises a fuselage, and a transmission mechanism and a control mechanism are mounted in the fuselage; the two groups of wings are connected to the left side and the right side of the fuselage, each group of wings comprises a front wing and a rear wing, and the front wing and the rear wing are partially overlapped; the transmission mechanism is installed in the cavity of the machine body and comprises a reduction gear set frame, a brushless motor installed on the reduction gear set frame, a duplicate gear and a double-crank rocker mechanism, and the brushless motor outputs gear rotation through a motor gear; and each steering mechanism comprises a rear wing connected with the tail wing support in a hinged mode, the tail end of the rear wing is installed on a steering engine arm in a hinged mode, and the steering engine is installed on a rear wing steering engine frame. In each group of wings, the front wing is movably connected to the transmission mechanism, and the rear wing is movably connected to the front wing, so that the rear wing flaps along with the front wing, and the rear wing is movably connected with the steering engine. The aircraft has the advantages of small size, high stability and high performance.

    本发明属于仿生飞行机器人设备领域,公开了一种仿生蝴蝶混控翅扑翼飞行器,包括:机身,所述机身内安装有传动机构和控制机构;两组翅膀,连接在机身的左右两侧,每组翅膀包括前翅和后翅,前翅和后翅部分重叠;传动机构安装在机身腔体内,包括减速齿轮组架、安装在减速齿轮组架上的无刷电机、双联齿轮和双曲柄摇杆机构,无刷电机通过电机齿轮输出齿轮转动;一对转向机构,每个转向机构包括与尾翅支架铰链连接的后翅,且后翅尾端铰链安装在舵机臂上,和安装在后翅舵机架上的舵机。在每组翅膀中,前翅活动连接在传动机构上,后翅活动连接在前翅上,从而使得后翅跟随前翅扑动,且后翅与舵机活动连接。该飞行器具有小体积、高稳定性及高性能的优点。


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    Titel :

    Bionic butterfly mixed control wing ornithopter


    Weitere Titelangaben:

    一种仿生蝴蝶混控翅扑翼飞行器


    Beteiligte:
    WU SHIPING (Autor:in) / WU JIATENG (Autor:in) / LI ZITING (Autor:in) / CHEN WENKAI (Autor:in) / XIE QIAN (Autor:in) / XIAO LIYUN (Autor:in) / WANG ZHENG (Autor:in) / DU SHAOLEI (Autor:in)

    Erscheinungsdatum :

    22.11.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64U / B64C AEROPLANES , Flugzeuge



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