发明名称 Aerospace ground maneuver light
摘要 Aerospace ground maneuver light, comprises a reflector (14), the reflector (14) defining a light exit plane (18), an LED light source (26) arranged outside of the area defined by the reflector (14) and its light exit plane (18), and a mounting bar (22) which has a longitudinal extension and at which the LED light source (26) is mounted. The mounting bar (22) extends across the reflector (14) and is spaced apart from the light exit plane (18) of the reflector (14) and comprises a mounting side (24) facing towards the reflector (14) and its light exit plane (18), with the LED light source (26) arranged on the mounting side (24) for emitting light towards the reflector (14). A dividing plane (28) is defined by the mounting bar (22), with the mounting bar (22) extending longitudinally along the dividing plane (28) which in turn extends (i) through the LED light source (26) as well as (ii) perpendicular to the light exit plane (18) and divides the reflector (14) in two reflector halves (30,32) arranged at opposite sides of the dividing plane (28). Each reflector half (30,32) comprises (i) a first reflector surface portion (34) arranged directly adjacent to the dividing plane (28) for reflecting light of the LED light source (26) towards a focal point (40) located outside of the mounting bar (22), and (ii) a second reflector surface portion (36) located directly adjacent to the first reflector surface portion (34) for reflecting light of the LED light source (26) in a direction substantially perpendicular to the light exit plane (18).
申请公布号 EP2667087(B1) 申请公布日期 2014.10.15
申请号 EP20120169322 申请日期 2012.05.24
申请人 GOODRICH LIGHTING SYSTEMS GMBH 发明人 SCHÖN, CHRISTIAN;JHA, ANIL KUMAR;WERNICKE, ALEXANDER;HESSLING, ANDRE
分类号 F21V7/04;B64F1/20;F21V3/04;F21V7/09;F21V29/00;F21W111/06;F21Y101/02 主分类号 F21V7/04
代理机构 代理人
主权项
地址