The invention discloses a propulsion device and a flight carrier, the propulsion device comprises a compressor assembly, a synchronous propulsion assembly, an air inlet baffle disc and a centrifugal machine assembly, the synchronous propulsion assembly is located between the compressor assembly and the centrifugal machine assembly, and the air inlet baffle disc is arranged between the synchronous propulsion assembly and the centrifugal machine assembly. The working process of the propelling device comprises the steps that the air compressor assembly sucks air and compressed air, the synchronous propelling machine assembly and the centrifugal machine assembly rotate synchronously and propel the air into the centrifugal machine assembly, and a centrifugal machine paddle wheel rotates to generate centrifugal force and exhaust the air. As the propelling device does not adopt hot oil, no high-temperature fuel gas is discharged, and the potential safety hazard is small. In addition, the opening is formed in the local area of the air inlet baffle disc, the air quality difference can be generated through asymmetric air inlet, and therefore the centrifugal force difference is caused, large lift force is generated, and the low-altitude flight requirement is met.

    本发明公开一种推进装置和飞行载具,其中,推进装置包括压气机组件、同步推进机组件、进气挡盘和离心机组件,同步推进机组件位于压气机组件和离心机组件之间,进气挡盘设于同步推进机组件与离心机组件之间。该推进装置工作过程:压气机组件吸入空气和压缩空气,同步推进机组件与离心机组件同步转动,并将空气推进离心机组件,离心机浆轮旋转产生离心力并排出空气。由于本发明的推进装置不采用燃热油,没有高温燃气排出,安全隐患小。再加上进气挡盘的局部区域开设开口,能够通过不对称式进气产生空气的质量差,从而引起离心力差,以产生较大的升力,进而满足低空飞行需要。


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    Titel :

    Propulsion device and flying vehicle


    Weitere Titelangaben:

    一种推进装置和飞行载具


    Beteiligte:
    GAO HONGSHENG (Autor:in)

    Erscheinungsdatum :

    2023-12-26


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

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



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