PROBLEM TO BE SOLVED: To save a weight of an aircraft which is electrically driven.SOLUTION: Provided is a device having a driving-motor 202 connected to a generator 204 which is electrically and directly connected to electric motors 210a, 210b. A propeller or fans 212a, 212b are connected to the electric motor and are driven by the electric motor. A bidirectional power source converter 208 is connected to the generator 204, and further connected to an energy accumulation device 214. Further, provided is a method with use of the device in which the energy accumulation device 214 is selectively connected to the electric motor.SELECTED DRAWING: Figure 2

    【課題】電気的に駆動される航空機の軽量化を図る。【解決手段】電気モータ210a,210bに電気的に直接結合されるジェネレータ204に結合される原動機202を有する装置を提供する。プロペラまたはファン212a,212bが電気モータに結合され、また電気モータによって駆動される。双方向電源変換器208がジェネレータ204に結合され、エネルギ蓄積デバイス214に更に結合される。エネルギ蓄積デバイス214は電気モータに選択的に結合される当該装置を使用する方法がまた提供される。【選択図】図2


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    Titel :

    ELECTRIC DIRECT CONNECTION DRIVING DEVICE FOR PROPELLING AND LIFTING AIRCRAFT


    Weitere Titelangaben:

    航空機の推進およびリフトのための電気直結駆動装置


    Beteiligte:

    Erscheinungsdatum :

    2017-01-05


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Japanisch


    Klassifikation :

    IPC:    B60L PROPULSION OF ELECTRICALLY-PROPELLED VEHICLES , Antrieb von elektrisch angetriebenen Fahrzeugen / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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