发明名称 WINDSHIELD OF AIRCRAFT
摘要 PROBLEM TO BE SOLVED: To avoid making an excessive electric current flow into a controller and the like which applies the electric current to a heater, by an induction current flowing into the heater of a windshield when it is struck by lightning.SOLUTION: A windshield 10 of an aircraft includes a plurality of conductive layers 21, 22 and 23 that are arranged along an in-plane direction of the windshield 10 and wire-connected to one another. The plurality of conductive layers 21, 22 and 23 are heaters that are supplied with a three-phase alternating current to generate heat, and wire-connected so that each induction current Iinduced by a magnetic field H associated with a lightning current Ican be circulated among the conductive layers 21, 22 and 23.SELECTED DRAWING: Figure 2
申请公布号 JP2016150642(A) 申请公布日期 2016.08.22
申请号 JP20150028544 申请日期 2015.02.17
申请人 MITSUBISHI AIRCRAFT CORP 发明人 YAMAURA TSUYOTOSHI;KITAZUME KATSUYA;HASHIMOTO TAKEKI
分类号 B64C1/14;B64D45/02 主分类号 B64C1/14
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