PROBLEM TO BE SOLVED: To provide a windshield of aircraft capable of suppressing induction current running through a heater of the windshield when a lightning strikes.SOLUTION: A windshield 10 of aircraft comprises: conductive layers 21, 22, 23, which generate heat when an electric current is supplied. The conductive layers 21, 22, 23 are oriented toward a lateral direction DH, which is a horizontal direction included in in-plane directions of the windshield 10. An induction current running to a direction opposing a change in a magnetic flux due to a lightning current striking an aircraft from above is hardly induced in the conductive layers 21, 22, 23.SELECTED DRAWING: Figure 2

    【課題】被雷時に風防のヒータに流れる誘導電流を抑制する。【解決手段】航空機の風防10は、電流が供給されることで発熱する導電層21,22,23を備えている。導電層21,22,23は、風防10の面内方向に含まれる水平な方向である横方向DHを指向している。航空機に向けて上方から落雷する雷電流に伴う磁束の変化を妨げる向きで流れる誘導電流は、導電層21,22,23には殆ど誘起されない。【選択図】図2


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    Titel :

    WINDSHIELD OF AIRCRAFT


    Weitere Titelangaben:

    航空機の風防


    Beteiligte:

    Erscheinungsdatum :

    2016-08-08


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Japanisch


    Klassifikation :

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



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