To provide a technology that allows an air vehicle to maintain its attitude when flying with water pressure.SOLUTION: A nozzle 110 includes a first cylindrical part 160, a second cylindrical part 162, and a bending part 164. The first cylindrical part 160 includes a first end part 150 and extends in a first direction as an extension from a hose 200. The second cylindrical part 162 includes a second end part 152 and extends in a second direction different from the first direction. The bending part 164 connects the first cylindrical part 160 with the second cylindrical part 162. An inertia rotor 120 is disposed at a position where a servo motor rotation axis 170 of a servo motor 122 and a first cylindrical part rotation axis 172 in a first direction of the first cylindrical part 160 correspond with each other.SELECTED DRAWING: Figure 3

    【課題】水圧により飛行する場合であっても姿勢を維持する技術を提供する。【解決手段】ノズル110は、第1筒部160、第2筒部162、屈曲部164を含む。第1筒部160は、第1端部150を含み、かつホース200からの延長で第1方向に延びる。第2筒部162は、第2端部152を含み、かつ第1方向とは異なった第2方向に延びる。屈曲部164は、第1筒部160と第2筒部162とを接続する。慣性ロータ120は、サーボモータ122のサーボモータ回転軸170と第1筒部160の第1方向の第1筒部回転軸172とが合わされる位置に配置される。【選択図】図3


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    Title :

    FLIGHT EXTINCTION DEVICE AND EXTINCTION SYSTEM


    Additional title:

    飛行消火装置、消火システム


    Contributors:

    Publication date :

    2021-11-01


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Japanese


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / A62C FIRE-FIGHTING , Feuerbekämpfung / B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen



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