发明名称 AIRCRAFT BEACON LIGHT
摘要 PROBLEM TO BE SOLVED: To provide a ground type aircraft beacon light in which the mounting and dismounting workability of the aircraft beacon light lamp body can be enhanced, the number of parts can be reduced, and a space needed at the time of arrangement can be made smaller. SOLUTION: The fixing of a lamp body 2 and a support body 3 is made also by a magnetic coupling of a primary side transformer 33 and a secondary side transformer 10 in addition to the screw connection of a screw 21 and a female screw 35. This means that when assembling the aircraft beacon light 1, it can be assembled with only the screw connection, and also that when a power source 4 is supplied with electric power, it is arranged so that the screw connection between the screw 21 and the female screw 35 is not released improperly by the magnetic coupling action of the primary transformer 33 and the secondary transformer 10. Then, since by only stopping the electric power supply to the power source 4, the lamp body 2 and the support body 3 can become in a state that they can be dismounted, workability in the maintenance and replacement works of the lamp body 2 can be enhanced. COPYRIGHT: (C)2007,JPO&INPIT
申请公布号 JP2006286379(A) 申请公布日期 2006.10.19
申请号 JP20050104268 申请日期 2005.03.31
申请人 TOSHIBA LIGHTING & TECHNOLOGY CORP 发明人 SHINNO SHINGO;SUZUKI KIYOSHI;IDE KATSUYUKI;KATO TOSHIYA
分类号 F21S2/00;F21W101/06;F21Y101/00 主分类号 F21S2/00
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