The invention discloses a novel intelligent deformable aircraft, and particularly relates to the technical field of aerodynamic configuration design of aircrafts. The novel intelligent deformable aircraft comprises a fuselage and engines symmetrically arranged on the rear side of the fuselage, an inverted-V-shaped empennage is further arranged at the tail of the fuselage, morphing wings are arranged on the fuselage, and the morphing wings can adjust the sweepback angle within 0-90 degrees. A front undercarriage located at the head of the fuselage and two main undercarriages below the engine are further arranged at the bottom of the fuselage. By the adoption of the technical scheme, the problem that an existing aircraft cannot achieve sweepback flexible deformation is solved, and the aerodynamic performance of the aircraft can be improved.

    本发明专利公开了一种新型智能变体飞行器,具体涉及飞行器气动外形设计的技术领域。一种新型智能变体飞行器,包括机身和对称设置在机身后侧的发动机,所述机身的尾部还设有倒V尾翼,所述机身上设有变体机翼,所述变体机翼可实现后掠角在0‑90°内调节,所述机身的底部还设有位于机身头部的前起落架和发动机下方的两个主起落架。采用本发明技术方案解决了现有的飞行器无法实现后掠角灵巧变形的问题,可提高飞行器的气动性能。


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    Title :

    Novel intelligent deformable aircraft


    Additional title:

    一种新型智能变体飞行器


    Contributors:
    MA XIAOYONG (author) / MIAO SHUAI (author) / LEI PENGXUAN (author) / HUANG YONG (author) / ZHOU WEIQUN (author) / QIAN FENGXUE (author) / CHEN LILI (author) / XIAO YUNLEI (author) / TANG JIGANG (author)

    Publication date :

    2021-07-23


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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