发明名称 Power pylon aircraft warning light - uses refractor with two circular segments to concentrate light output from tube source into required viewing angle
摘要 <p>The warning light fixed to the top of power transmission pylons has a luminescent tube (8) enclosed by a transparent cylindrical tube (7). A transparent plexiglass or lexan refractor (9) enclosing the cylinder and tube is shaped so the light output is concentrated in an angle of about 30 degrees which is the vertical visibility angle required by aviation authorities. The refractor (9) has a section essentially comprising two opposed circular arcs centred along the axis of the luminescent tube, a distance 'd' from the centre of the tube (CO). The distance 'd' depends on the index of refraction of the refractor and the required angle of view. For a given light output over the required viewing angle a lower power input is requied, or higher visibility is obtained from a given power input.</p>
申请公布号 FR2471548(A1) 申请公布日期 1981.06.19
申请号 FR19790030365 申请日期 1979.12.11
申请人 CLAUDE 发明人 NHIEP NGUYEN DAT
分类号 F21S8/00;H02G7/00;(IPC1-7):21Q3/00;64F1/20;21V5/08 主分类号 F21S8/00
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