The invention relates to a relative motion air kinetic energy aviation aircraft rotating disc type lifting platform. The method is technically characterized in that a plurality of relative movement air kinetic energy recoil thrust generating devices are arranged on the periphery of the lower portion of an aviation aircraft lifting rotating platform arranged on a rotating disc type lifting field, meanwhile, the large-diameter rotating platform is used for doing work for early-stage thrust and normal recoil thrust, and an ultra-long force arm is provided; and the relative motion air kinetic energy of rotating speed high-power amplification of the rotating platform is continuously utilized twice as mechanical kinetic energy, so that the technical effects of large-scale power generation and zero-energy-consumption lifting of aviation aircrafts are achieved.

    本发明涉及一种相对运动空气动能航空飞机转盘式升降平台。其技术特征在于,采用在转盘式升降机场上设置的航空飞机升降转动平台下方周边部位,多具设置相对运动空气动能反冲推力产生装置,同时利用大直径的转动平台为前期推力与正常反冲推力做功、提供超长力臂,两次连续利用转动平台转速高倍扩大相对运动空气动能作为机械动能,由此实现大规模发电与航空飞机的零能耗升降技术效果。


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    Titel :

    Relative motion air kinetic energy aviation aircraft rotating disc type lifting airport


    Weitere Titelangaben:

    相对运动空气动能航空飞机转盘式升降机场


    Beteiligte:
    YI YUANMING (Autor:in)

    Erscheinungsdatum :

    06.02.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen



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