To provide systems and methods for powering an electric aerial vehicle.SOLUTION: A power source 100 for an electric propulsion system 118 of an aerial vehicle 110 includes a body having an electrical energy storage device 138 configured to store electrical energy. The power source also includes a plurality of terminals 242 coupled to an electrical energy storage device for supplying electrical energy from an electrical energy storage device to an electric propulsion system of the aerial vehicle. The power source further includes a plurality of flight control surfaces 126 extending outwardly from the body. The flight control surfaces are actuatable to adjust a flight attitude of the power source. Additionally, the power source includes a flight control system 256 including a processor and the flight control system is configured to actuate a plurality of flight control surfaces to fly the power source to a target location when the power source is dropped from the aerial vehicle.SELECTED DRAWING: Figure 2

    【課題】電動航空ビークルに電力を供給するためのシステムおよび方法を提供する。【解決手段】航空ビークル110の電気推進システム118用の電力源100が、電気エネルギーを蓄えるように構成された電気エネルギー貯蔵装置138を有する本体を含む。さらに、電力源は、電気エネルギー貯蔵装置から航空ビークルの電気推進システムに電気エネルギーを供給するための電気エネルギー貯蔵装置に接続された複数の端子242を含む。電力源は、本体から外へ延びる複数の飛行制御面126をさらに含む。飛行制御面を、電力源の飛行姿勢を調整するように作動させることができる。さらに、電力源は、プロセッサを含む飛行制御システム256を含み、飛行制御システムは、電力源が航空ビークルから投下されたときに電力源を目標位置へ飛行させるべく複数の飛行制御面を作動させるように構成される。【選択図】図2


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    Title :

    SYSTEMS AND METHODS FOR POWERING ELECTRIC AERIAL VEHICLE


    Additional title:

    電動航空ビークルに電力を供給するためのシステムおよび方法


    Contributors:

    Publication date :

    2019-06-20


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Japanese


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64C AEROPLANES , Flugzeuge / H02J CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER , Schaltungsanordnungen oder Systeme für die Abgabe oder Verteilung elektrischer Leistung



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