The present invention relates to a hybrid power supply device for an unmanned aerial vehicle (UAV) that can completely maintain the state of the battery regardless of the surrounding temperature. According to the present invention, the hybrid power supply device for a UAV may comprise: a chemical cell unit which generates electricity using chemical fuel; a regenerative battery unit which generates electricity using solar energy and wind energy; a battery unit which stores power produced by the chemical cell unit and the regenerative battery unit; a control unit which controls the supply of power from the chemical cell unit or battery unit to a motor; and a constant temperature maintenance unit which maintains the temperature of the battery unit at an appropriate temperature.

    본 발명은 무인기용 하이브리드 전력 공급장치에 관한 것으로, 화학연료를 이용하여 전기를 발생시키는 화학전지부와, 태양에너지와 풍력에너지를 이용하여 전기를 발생시키는 재생전지부와, 상기 화학전지부와 상기 재생전지부에서 생산된 전력을 저장하는 배터리부와, 상기 화학전지부 또는 배터리부의 전력을 모터에 공급제어하는 제어부와, 상기 배터리부의 온도를 적정온도로 유지하는 항온 유지부를 포함할 수 있다.


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    Titel :

    Hybrid power supply for UAV


    Weitere Titelangaben:

    무인기용 하이브리드 전력 공급장치


    Beteiligte:

    Erscheinungsdatum :

    2023-04-14


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Koreanisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B60L PROPULSION OF ELECTRICALLY-PROPELLED VEHICLES , Antrieb von elektrisch angetriebenen Fahrzeugen / B64C AEROPLANES , Flugzeuge / H02J CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER , Schaltungsanordnungen oder Systeme für die Abgabe oder Verteilung elektrischer Leistung / H02N Elektrische Maschinen, soweit nicht anderweitig vorgesehen , ELECTRIC MACHINES NOT OTHERWISE PROVIDED FOR




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