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
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