To efficiently cool a cooling object in which a heat value is different according to a situation, in a missile.SOLUTION: A missile (10) comprises a cooling facility 40a including independent first cooling circuit 42a and second cooling circuit 42b. The first cooling circuit 42a includes a first circulation channel 44a which sequentially and repeatedly circulates a first cooling medium to cooling objects (34a, 34b), similarly, the second cooling circuit 42b includes a second circulation channel 44b which sequentially and repeatedly circulates a second cooling medium. In the configuration, the first and second circulation channels 44a, 44b do not communicate each other. Therefore, merging of the first and second cooling media, and diversion of the first and second cooling media do not occur.SELECTED DRAWING: Figure 3

    【課題】飛翔体において、状況に応じて発熱量が相違する冷却対象を十分に冷却する。【解決手段】飛翔体(10)には、互いに独立した第1冷却回路42aと第2冷却回路42bを有する冷却設備(40a)が設けられる。第1冷却回路42aは、冷却対象(34a、34b)に第1冷却媒体を順次且つ繰り返し通過させる第1循環流路44aを含む。同様に、第2冷却回路42bは、前記冷却対象に第2冷却媒体を順次且つ繰り返し通過させる第2循環流路44bを含む。ここで、第1循環流路44aと第2循環流路44bは互いに連通しない。従って、第1冷却媒体と第2冷却媒体が合流したり、分流したりすることはない。【選択図】図3


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    Titel :

    MISSILE


    Weitere Titelangaben:

    飛翔体


    Beteiligte:

    Erscheinungsdatum :

    12.10.2022


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Japanisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64C AEROPLANES , Flugzeuge / H01M Verfahren oder Mittel, z.B. Batterien, für die direkte Umwandlung von chemischer in elektrische Energie , PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY



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