PROBLEM TO BE SOLVED: To create a load hook understructure which does not need maintenance, achieves high cost efficiency, is simple, and aerodynamically achieves high efficiency.SOLUTION: A load hook understructure 1 is attached onto a cabin structure of a helicopter or into the cabin structure and includes a housing 10. A shaft 12 having hook attachment means 121 is attached into the housing so as to be connected with a load hook and thereby be connected with the load hook understructure.SELECTED DRAWING: Figure 3a

    【課題】メンテナンスがいらない、費用効率が高い、簡単な、空気力学的に効率の良い荷重フック下部構造体を創出する。【解決手段】ヘリコプターのキャビン構造体上に或いはキャビン構造体中に取り付くための荷重フック下部構造体1であって、ハウジング10を備え、該ハウジング内には、フック取り付け手段121を有するシャフト12が、荷重フックと接続でき、それにより、荷重フック下部構造体と接続できるように装着される。【選択図】図3a


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    Titel :

    LOAD HOOK UNDERSTRUCTURE


    Weitere Titelangaben:

    荷重フック下部構造体


    Beteiligte:
    MARTIN STUCKI (Autor:in) / COSIMO DONNO (Autor:in)

    Erscheinungsdatum :

    2017-02-23


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Japanisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64C AEROPLANES , Flugzeuge / F16F SPRINGS , Federn



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