发明名称 |
WARNING LAMP FOR AN AIRCRAFT |
摘要 |
The lamp (1) has LEDs (42, 46, 58, 60) arranged within an area delimited by a light permeable cover (12), which has a frontal cover area and a rear cover area formed by a frontal cover element (22) and a rear cover element (28) that are made of two different light permeable materials. A cooling body (18) is arranged between the cover elements for separating the cover elements. The cooling body has a cooling surface (32), which is a part of external contours of the cover, formed by the cover elements and possesses an upper region (38) and adjacent, opposing side areas (40). |
申请公布号 |
EP2296973(A1) |
申请公布日期 |
2011.03.23 |
申请号 |
EP20090769198 |
申请日期 |
2009.06.19 |
申请人 |
GOODRICH LIGHTING SYSTEMS GMBH;AIRBUS DEUTSCHLAND GMBH |
发明人 |
KOHLMEIER-BECKMANN, CARSTEN;GRIESBACH, MARTIN;MUELLER, BERNHARD;FERLING, SONJA;HESSLING, ANDRE;LUEDER, SASCHA |
分类号 |
F21V29/00;B64C27/82;B64D47/06;F21S8/10;F21W101/06;F21W111/00;F21Y101/02 |
主分类号 |
F21V29/00 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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