To provide a suspension structure applied to a drone, which comprises a hook body and at least one hook claw.SOLUTION: The hook body includes a bottom, at least one pivot end, an abutment, and a hook port between the pivot end and the abutment, and the hook port is at a position facing the bottom. The hook claw includes a pivot part and first and second claws extending from the pivot part, and the pivot part comes into contact with the pivot end. The weight of the second claw is larger than that of the first claw. When the suspended structure is in a suspended state, the first tail end of the first claw abuts against the abutment to close the hook port. A drone suspension system including the suspension structure is also provided.SELECTED DRAWING: Figure 1A

    【課題】無人機に適用される吊り構造であって、フック状本体と少なくとも1つのフック爪を含む。【解決手段】フック状本体は底部、少なくとも1つの樞接端と当接部を有し、少なくとも1つの樞接端と当接部の間にフック口を有し、かつ、フック口は底部と対向する位置にある。また、少なくとも一つのフック爪は樞接部及び樞接部からそれぞれ延出する第1の爪部と第2の爪部を有する、樞接部は少なくとも一つの樞接端に樞接する。第2の爪部の重さは第1の爪部の重さより大きい。吊り構造が吊り状態にある場合、第1の爪部の第1の末端が当接部に当接して、フック口を閉鎖する。本発明はさらに前記吊り構造を含む無人機吊りシステムを提供する。【選択図】図1A


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    Title :

    SUSPENSION STRUCTURE AND DRONE SUSPENSION SYSTEM


    Additional title:

    吊り構造と無人機吊りシステム


    Contributors:

    Publication date :

    2024-05-17


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Japanese


    Classification :

    IPC:    B66C Krane , CRANES / B64U / B66D Haspeln , CAPSTANS



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