To provide a multicopter that can perform emergency landing stably from any altitude.SOLUTION: A multicopter 1 includes: an airframe 11; a battery 31 capable of discharging power for flying the airframe 11; and an engine power generation unit 12 for supplying the battery 31 with power for flying the airframe 11. The multicopter includes a PCU (power control unit) 32 for changing a lower limit (SOC lower limit) of a charging rate use range of the battery 31 in accordance with altitude of the airframe 11.SELECTED DRAWING: Figure 2

    【課題】どの高度からでも安定して緊急着陸できるマルチコプタを提供する。【解決手段】本開示の一態様は、機体11と、機体11を飛行させる電力を充放電可能なバッテリ31と、バッテリ31に機体11を飛行させる電力を供給するエンジン発電ユニット12と、を有するマルチコプタ1において、機体11の高度に応じて、バッテリ31の充電率使用範囲の下限値(SOC下限値)を変化させるPCU(パワーコントロールユニット)32を有する。【選択図】図2


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    Title :

    MULTICOPTER


    Additional title:

    マルチコプタ


    Contributors:

    Publication date :

    2022-11-04


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Japanese


    Classification :

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



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