The invention relates to the technical field of aviation devices, in particular to a descending type integrated external power track electronic floating shoot aviation device. The device comprises an acceleration track gradually changing from vertical transition to transverse transition or upward inclination; in the initial state, an electric bearing vehicle is connected to the upper end of the acceleration track in a suspended mode, and an aircraft is loaded on the electric bearing vehicle; and the electric bearing vehicle is further provided with a power relay mechanism for transmitting advancing power of the electric bearing vehicle to the aircraft. The problems that in the prior art, a device is limited by the weight of an aircraft, and consequently the aircraft needs longer time and acceleration distance to take off are solved; and a large amount of energy is consumed in the early take-off acceleration stage.

    一种下行式集合外动力轨道电子浮射航空装置,涉及航空装置技术领域,包括由竖向过渡渐变为横向或上倾的加速轨道,初始状态下,加速轨道的上端部悬挂连接有电动承载车,电动承载车上装载有飞行器,电动承载车上还设有将其前进的动力传递给飞行器的动力接力机构。本发明解决了传统技术中的装置受限于飞机自身的重量,导致了飞机需要更长的时间和加速距离用以起飞;以及其在前期起飞加速阶段,消耗大量的能源的问题。


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    Titel :

    Downward electronic floating launch aviation device with integrated external power track


    Weitere Titelangaben:

    一种下行式集合外动力轨道电子浮射航空装置


    Beteiligte:
    CHENG LI (Autor:in)

    Erscheinungsdatum :

    2021-07-23


    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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