| 发明名称 |
LIGHTING DEVICE FOR AIRCRAFT ALLOWING THE INTEGRATION OF ADDITIONAL FUNCTIONS AT ITS CENTER |
| 摘要 |
A Light Emitting Diode (LED) light for an aircraft includes a hollow cylindrical body, a plurality of LEDs mounted in the hollow body, and at least one reflector to receive light beams emitted by the LEDs and configured to direct the light beams in a lighting direction of the LED light. The LEDs are mounted on a cylindrical support and disposed radially in the cylindrical body, and the cylindrical support has a polygonal contour. |
| 申请公布号 |
US2016347474(A1) |
申请公布日期 |
2016.12.01 |
| 申请号 |
US201615167575 |
申请日期 |
2016.05.27 |
| 申请人 |
ZODIAC AERO ELECTRIC |
发明人 |
Millet Philippe;Doule Claude |
| 分类号 |
B64D47/04;G08G5/02;F21V7/06;F21V7/22;F21V3/04;F21V29/70 |
主分类号 |
B64D47/04 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A Light Emitting Diode (LED) light for an aircraft, comprising:
a hollow cylindrical body: a plurality of LEDs mounted in the hollow body; and at least one reflector to receive light beams emitted by the LEDs and configured to direct the light beams in a lighting direction of the LED light, wherein the LEDs are mounted on a cylindrical support and disposed radially in the cylindrical body, the cylindrical support having a polygonal contour. |
| 地址 |
Montreuil FR |
