The invention relates to a wing-engine reconstruction type morphing aircraft which comprises an aircraft body, a left wing and a right wing. One end of the left wing is connected with the left side of the fuselage; each of the left wing and the right wing has an extending state and a contracting state which can be switched mutually; when the left wing and the right wing are in the extending state, the left wing extends out of the left side of the fuselage, and the right wing extends out of the right side of the fuselage; when the left wing and the right wing are both in the contraction state, the left wing, the right wing and the bottom plate of the fuselage jointly define a ramjet flow channel of the ramjet. According to the wing-engine reconstruction type variant aircraft, the left wing and the right wing can be switched between the extending state and the contracting state so as to be matched with lifting surfaces required by different flight speeds. Due to the fact that the wing structure and the ramjet engine structure can be shared in a reconfiguration mode, the overall weight of the aircraft can be reduced. And when the low flight speed of the ramjet engine does not need to be used, the dead weight and resistance of the aircraft are reduced.

    本申请涉及一种翼‑发重构型变体飞行器,包括:机身、左机翼、右机翼;左机翼的一端与机身左侧连接,右机翼的一端与机身右侧连接;左机翼和右机翼均具有能相互切换的伸出状态和收缩状态;左机翼和右机翼均处于伸出状态时,左机翼伸出机身的左侧,右机翼伸出机身的右侧;左机翼和右机翼均处于收缩状态时,左机翼和右机翼及机身的底板共同围成冲压发动机的冲压流道。上述翼‑发重构型变体飞行器可通过左机翼和右机翼在伸出状态与收缩状态之间变换,以匹配不同飞行速度所需升力面。由于机翼结构与冲压发动机结构可通过重构的方式共用,从而可以减小飞行器整体的重量。且在不需要使用冲压发动机的较低飞行速度时,减小了飞机的死重和阻力。


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    Title :

    Wing-engine reconstruction type morphing aircraft


    Additional title:

    翼-发重构型变体飞行器


    Contributors:
    CHEN HAIXIN (author) / ZHOU XIAOPENG (author)

    Publication date :

    2023-12-12


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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