The invention discloses a flapping-gliding combined type bionic aircraft with low energy consumption. The bionic aircraft comprises a flapping-wing aircraft body, a first driving mechanism and a transmission structure, the flapping-wing aircraft body comprises a fuselage and flapping wings, and the wings can be driven by the first driving mechanism to perform flapping action; and a wing locking mechanism, the wing locking mechanism is connected with the fuselage, and the wing locking mechanism can also be separably matched with the transmission structure and/or the wing. When the wing locking mechanism is separated from the transmission structure and/or the wings, the wings are in a flapping state, and the bionic aircraft flies in a flapping wing mode; when the wing locking mechanism is fixedly matched with the transmission structure and/or the wings, the wings are in a fixed state, and the bionic aircraft flies in a fixed wing gliding mode. The aircraft has two flight modes of flapping wing flight and gliding, free switching can be achieved in the flight process according to requirements, and the adaptability to the environment is higher.

    本发明公开了一种低能耗的扑动‑滑翔复合式的仿生飞行器。该仿生飞行器包括扑翼飞行器主体、第一驱动机构和传动结构,扑翼飞行器主体包括机身以及可扑动的机翼,机翼能够在第一驱动机构的驱使下执行扑动动作;以及,机翼锁定机构,机翼锁定机构与机身连接,机翼锁定机构还能够与传动结构和/或机翼可分离地配合;当机翼锁定机构与传动结构和/或机翼彼此分离时,机翼处于可扑动状态,仿生飞行器通过扑翼模式飞行;而当机翼锁定机构与传动结构和/或机翼固定配合时,机翼处于固定状态,仿生飞行器通过固定翼滑翔模式飞行。本发明具有扑翼飞行和滑翔两个飞行模式,可以根据需求在飞行过程中自由切换,对于环境的适应性更强。


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    Title :

    Flapping-gliding combined type bionic aircraft with low energy consumption


    Additional title:

    低能耗的扑动-滑翔复合式的仿生飞行器


    Contributors:
    GUO YAFEI (author) / LI JIADONG (author) / LIU KUN (author) / WANG MENGSHUO (author) / HU YIMIN (author) / LIU XINHAO (author)

    Publication date :

    2024-03-12


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64U / B64C AEROPLANES , Flugzeuge



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