The invention discloses an aircraft power device which comprises a shell, a first power structure is arranged in the middle of the shell, second power structures are symmetrically arranged on the two sides of the shell, and the first power structure comprises a first eruption device, a first fuel chamber and a first oxidizing agent chamber. The first power structure comprises an engine, a mixing chamber, a first fuel chamber and a first oxidant chamber, two first sprayers are arranged in the middle of the shell and communicated with the first fuel chamber and the first oxidant chamber through pipelines, two second sprayers are further arranged in the middle of the shell and communicated with the first fuel chamber and the first oxidant chamber through pipelines, and the second power structure comprises an engine, a mixing chamber, a second fuel chamber and a second oxidant chamber. The power device is provided with the oxidizing agent and the fuel, the oxidizing agent and the fuel react to provide power for the aircraft in the high altitude, and the flight height of the aircraft is guaranteed.

    本发明公开了一种飞机动力装置,包括壳体,所述壳体中部设置有一号动力结构,所述壳体两侧对称设置有二号动力结构,所述一号动力结构包括一号喷发器、一号燃料室和一号氧化剂室,所述一号喷发器通过管路和一号燃料室、一号氧化剂室连通,所述壳体中部还设置有两个二号喷发器,所述二号喷发器通过管路和一号燃料室、一号氧化剂室连通,所述二号动力结构包括发动机、混合室、二号燃料室和二号氧化剂室。本发明中的动力装置设置有氧化剂和燃料,通过氧化剂和燃料反应提供飞机在高空是的动力,保证飞机的飞行高度。


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    Title :

    Airplane power device


    Additional title:

    一种飞机动力装置


    Contributors:

    Publication date :

    2024-05-03


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    F02K JET-PROPULSION PLANTS , Strahltriebwerke / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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