PROBLEM TO BE SOLVED: To protect a structural member from a heating part under the limit of a space and weight of an aircraft.SOLUTION: An aircraft 1 includes: a body 10; an air conditioning pack 21 installed at the outer side of a lower part 10A of the body 10; a fairing 11 covering the air conditioning pack 21; an outer heat insulation material 32 arranged at a region 10R of the body 10, which corresponds to the air conditioning pack 21, from the outer side of the body 10; and an inner heat insulation material 31 disposed at a periphery of the region 10R at the inner side of the body 10.SELECTED DRAWING: Figure 1

    【課題】航空機のスペースや重量に制約がある中で、発熱部から構造部材を保護すること。【解決手段】航空機1は、胴体10と、胴体10の下部10Aの外側に設置される空調パック21と、空調パック21を覆うフェアリング11と、空調パック21に対応する胴体10の領域10Rに胴体10の外側から配置される外側断熱材32と、胴体10の内側で領域10Rの周囲に配置される内側断熱材31とを備える。【選択図】図1


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    Titel :

    AIRCRAFT AND BODY COOLING STRUCTURE


    Weitere Titelangaben:

    航空機、および胴体の冷却構造


    Beteiligte:
    HARA NOBUHIDE (Autor:in) / YAMADA OSAMU (Autor:in)

    Erscheinungsdatum :

    2016-07-25


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Japanisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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