The invention belongs to the technical field of propulsion, and particularly relates to an aerospace thruster. The aerospace thruster comprises an air compressor, a wind tunnel pipe and a plurality of wing-shaped modules, the two ends of the wind tunnel pipe are connected with an air inlet and an air outlet of the air compressor respectively, and the wing-shaped modules are arranged in the wind tunnel pipe. According to the requirement of the size of an aircraft, a wing is divided into a plurality of wing-shaped modules, the wing-shaped modules are installed and fixed in a closed circulating wind tunnel pipe one by one, high-speed airflow in the wind tunnel pipe impacts the wing-shaped modules to generate lift force, and the wing-shaped modules lift the first wind tunnel pipe to take off. The generation of the lift force is not related to wind in any direction of the outside of the wind tunnel pipe and is not related to whether air exists in the outside or not, so that the safety performance of the aircraft is improved; the thruster is also a'media-free thruster '.

    本发明属于推进技术领域,具体涉及一种空天推力器。空天推力器,包括空压机、风洞管和若干翼型模块,风洞管的两端分别连接空压机的进气口和出气口,翼型模块设置在风洞管内。本发明按飞机大小的需求、把机翼分解成若干个翼型模块、一个个安装固定在密闭循环的风洞管内,由风洞管内的高速气流冲击翼型模块产生升力,由翼型模块抬着风洞管一起飞。这种升力的产生与风洞管外界刮什么方向的风都没有关系,与外界有无空气也没有关系,提高了飞行器的安全性能;本发明还是“无介质推力器”。


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    Title :

    Aerospace thruster


    Additional title:

    空天推力器


    Contributors:
    WANG JINHAI (author)

    Publication date :

    2023-05-12


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64G Raumfahrt , COSMONAUTICS / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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