The invention discloses a subsonic stealth unmanned aerial vehicle. The subsonic stealth unmanned aerial vehicle comprises a nose; the machine body comprises a front part, a middle part, a rear part and a tail part, and an air inlet channel with an opening facing the machine head direction is arranged below the rear part of the machine body; the balance wings are positioned at the rear part of the fuselage and comprise a left balance wing and a right balance wing which are symmetrically arranged on the left side and the right side of the fuselage; the empennage and the engine are arranged at the tail part of the fuselage, and the empennage is a Y-shaped empennage; the variable infrared enhancement system and the wingtip of the balance wing are integrally arranged, the variable infrared enhancement system comprises a front infrared radiation cabin, a rear infrared radiation cabin and a control cabin, the front infrared radiation cabin and the rear infrared radiation cabin are integrally arranged, the control cabin is arranged between the front infrared radiation cabin and the rear infrared radiation cabin, and the variable infrared enhancement system is used for carrying out front-back bidirectional radiation. According to the subsonic stealth unmanned aerial vehicle provided by the invention, the variable infrared enhancement system with variable infrared characteristics is integrated on the aerial vehicle, so that the effectiveness of training and testing is improved, and the problem that functions and performance are difficult to consider at the same time is solved.

    本发明公开了一种亚音速隐身无人飞行器,包括:机头;机身,所述机身包括前部、中部、后部和尾部,所述机身后部下方设置有开口朝向机头方向的进气道;平衡翼,所述平衡翼位于机身后部,包括对称构置于机身左、右两侧的左平衡翼和右平衡翼;构置于机身尾部的尾翼及发动机,所述尾翼为Y型尾翼;可变红外增强系统,所述可变红外增强系统与平衡翼的翼尖一体化构置,包括一体化构置的前红外辐射舱、后红外辐射舱和设置在两者之间的控制舱,所述可变红外增强系统用于进行前后双向辐射。本发明提供的亚音速隐身无人飞行器,通过将具备可变红外特性的可变红外增强系统整合在飞行器上,提高了训练和测试的实效性,解决了功能与性能之间难以兼顾的问题。


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    Title :

    Subsonic stealth unmanned aerial vehicle


    Additional title:

    一种亚音速隐身无人飞行器


    Contributors:
    LI YAN (author) / YANG HONG (author) / BAO SIYU (author) / HAN XU (author) / MIAO YUHANG (author)

    Publication date :

    2025-03-28


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64U / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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