The invention belongs to the technical field of aircraft aerodynamic configuration design, and discloses a combined aircraft layout and connecting mechanism which comprises a main aircraft and two subaircrafts, and the main aircraft and the sub aircrafts adopt flying wing layout; the main aircraft and the sub aircrafts are consistent in plane shape and are each provided with a single front edge and a single rear edge; the two sub aircrafts are arranged at the two sides of the rear edge of the main machine, and the front edges of the sub aircrafts are connected with the rear edge of the main aircraft; and the main aircraft and the sub aircrafts have the same front edge sweepback angle. A combined aircraft has the characteristics of being good in aerodynamic performance, high in invisibility and high in lift-drag ratio, the combat functions of remote throwing, sub-aircraft aerial networking and the like can be achieved, the functions of the aircraft are effectively expanded, and the combat effect of the aircraft is improved.

    本发明属于飞行器气动外形设计技术领域,公开了一种组合飞行器布局及连接机构,包括主机和两个子机,主机和子机均采用飞翼布局;主机和子机的平面形状一致,且均具有单前缘和单后缘;两个子机布置在主机后缘两侧,且子机的前缘与主机的后缘衔接;主机和子机的前缘后掠角相同。本发明的组合飞行器兼具气动性能好、高隐身和高升阻比的特性,可以实现远程投放、子机空中组网等作战功能,有效拓展了飞行器的功能,提高了飞行器的作战效果。


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    Title :

    Combined aircraft layout and connecting mechanism


    Additional title:

    一种组合飞行器布局及连接机构


    Contributors:
    MA XIAOYONG (author) / HUANG JIANGTAO (author) / CHEN LILI (author) / ZHONG SHIDONG (author) / XIAO YUNLEI (author) / DU XIN (author) / ZHANG SHENG (author)

    Publication date :

    2020-12-18


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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