To provide a canopy of an unmanned flight body which has a light weight and a rigidity while having a sufficient storage capacity, and further, can reduce an influence of air current.SOLUTION: A canopy 4 of an unmanned flight body is configured from: plural first wall parts 42; plural second wall parts 44 which are formed continuously with the first wall parts 42; and a ceiling part 46 which is formed continuously with the first wall parts 42 and the second wall parts 44. The first wall part 42 and the second wall part 44 are so formed as to have a curve surface in a vertical direction, and has a bottom connected to a main body of an unmanned flight body 1, an intermediate part connected to the bottom, and an upper part which is continuous with the intermediate part, of which at least a part has a curve surface in the vertical direction, and which is formed continuously with the ceiling part 46. The bottom, the intermediate part and the upper part of the second wall part 44 are so formed as to have a curve surface in a direction orthogonal to the vertical direction.SELECTED DRAWING: Figure 4

    【課題】、十分な格納容量を有しつつ、軽量であり、剛性を有し、さらに、気流の影響を低減することができる無人飛行体のキャノピーを提供すること。【解決手段】無人飛行体のキャノピー4は、複数の第一壁部42と、第一壁部42と連続して形成される複数の第二壁部44と、第一壁部42及び第二壁部44と連続して形成される天井部46で構成される。第一壁部42及び第二壁部44は、鉛直方向における曲面を有して形成され、無人飛行体1の本体と接続する底部と、底部と連続する中間部と、中間部と連続し、少なくとも一部が鉛直方向における曲面を有し、天井部46と連続して形成される上部を有し、第二壁部44の底部、中間部及び上部は、鉛直方向と直行する方向における曲面を有して形成されている。【選択図】図4


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    Titel :

    CANOPY OF UNMANNED FLIGHT BODY


    Weitere Titelangaben:

    無人飛行体のキャノピー


    Beteiligte:
    IZU TOMOYUKI (Autor:in)

    Erscheinungsdatum :

    2019-06-20


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Japanisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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