The invention relates to a long-endurance flight backpack based on eddy current hybrid power. The long-endurance flight backpack comprises a power system, an electric propulsion system, a skeleton part, a manned part and a flight control system, the power system comprises an energy storage part and an energy conversion part. The efficient power utilization rate is achieved, long-endurance flight can be achieved, the optimal flight performance is met through flexible power distribution performance, meanwhile, the advantages of being environmentally friendly, good in economic performance and the like are achieved, low-altitude flight is met, and wide development prospects are achieved.

    本发明涉及一种基于涡电混合动力的长续航飞行背包,包括动力系统、电力推进系统、骨架部分、载人部分、飞行控制系统;所述动力系统包括储能部分和能量转化部分。本发明实现了高效的动力利用率可实现长续航飞行,灵活的动力分配性能满足了最佳的飞行性能,同时具有环保、经济性能好等优势,满足低空飞行,具有开阔的发展前景。


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    Titel :

    Long-endurance flying backpack based on eddy current hybrid power


    Weitere Titelangaben:

    一种基于涡电混合动力的长续航飞行背包


    Beteiligte:
    XUE ZHAOYUN (Autor:in) / HU XIAO'AN (Autor:in) / WAN YIXING (Autor:in) / SONG XUAN (Autor:in) / SHAN ZHIYANG (Autor:in) / LI JIATONG (Autor:in) / DONG LEQI (Autor:in) / WANG XINYUE (Autor:in) / XIANG XULU (Autor:in) / WANG ZIHUAI (Autor:in) ... [mehr]

    Erscheinungsdatum :

    15.04.2025


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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