Aircraft landing light unit, exterior aircraft lighting system and method of operating an aircraft landing light unit
IPC분류정보
국가/구분
United States(US) Patent
등록
국제특허분류(IPC7판)
B64D-047/04
H05B-033/08
B60Q-001/14
B64D-047/06
F21V-005/04
H05B-037/02
F21Y-101/02
출원번호
US-0158874
(2016-05-19)
등록번호
US-9723677
(2017-08-01)
우선권정보
EP-15168342 (2015-05-20)
발명자
/ 주소
Hessling-Von Heimendahl, Andre
Schoen, Christian
Jha, Anil Kumar
출원인 / 주소
GOODRICH LIGHTING SYSTEMS GMBH
대리인 / 주소
Cantor Colburn LLP
인용정보
피인용 횟수 :
0인용 특허 :
11
초록▼
An aircraft landing light unit includes a plurality of LEDs, an optical system associated with the plurality of LEDs for shaping a light output of the aircraft landing light unit for illuminating an aircraft environment, a control unit for controlling the plurality of LEDs, and a photo detector arra
An aircraft landing light unit includes a plurality of LEDs, an optical system associated with the plurality of LEDs for shaping a light output of the aircraft landing light unit for illuminating an aircraft environment, a control unit for controlling the plurality of LEDs, and a photo detector arranged for detecting light, emitted by the plurality of LEDs, output via the optical system and reflected by atmospheric haze, such as clouds, fog, rain and snow, wherein the control unit is coupled to the photo detector and is configured to control the plurality of LEDs on the basis of the light detected by the photo detector, thereby adjusting the light output of the aircraft landing light unit to the atmospheric haze.
대표청구항▼
1. An aircraft landing light unit, comprising: a plurality of LEDs,an optical system associated with the plurality of LEDs for shaping a light output of the aircraft landing light unit for illuminating an aircraft environment,a control unit for controlling the plurality of LEDs, anda photo detector
1. An aircraft landing light unit, comprising: a plurality of LEDs,an optical system associated with the plurality of LEDs for shaping a light output of the aircraft landing light unit for illuminating an aircraft environment,a control unit for controlling the plurality of LEDs, anda photo detector arranged for detecting light, emitted by the plurality of LEDs, output via the optical system and reflected by atmospheric haze, such as clouds, fog, rain and snow,wherein the control unit is coupled to the photo detector and is configured to control the plurality of LEDs on the basis of the light detected by the photo detector, thereby adjusting the light output of the aircraft landing light unit to the atmospheric haze. 2. An aircraft landing light unit according to claim 1, wherein the control unit is configured to compare the light detected by the photo detector to a reflection threshold value and to decrease the light output of the aircraft landing light unit as a response to the light detected by the photo detector being above the reflection threshold value. 3. An aircraft landing light unit according to claim 2, wherein the control unit is configured to dim all of the plurality of LEDs as a response to the light detected by the photo detector being above the reflection threshold value. 4. An aircraft landing light unit according to claim 2, wherein the plurality of LEDs comprises a first subset of LEDs and a second subset of LEDs, with the first and second subsets of LEDs being separately controllable, and wherein the control unit is configured to dim the first subset of LEDs as a response to the light detected by the photo detector being above the reflection threshold value. 5. An aircraft landing light unit according to claim 2, wherein the plurality of LEDs comprises a first subset of LEDs and a second subset of LEDs, with the first and second subsets of LEDs being separately controllable, and wherein the control unit is configured to switch off the first subset of LEDs as a response to the light detected by the photo detector being above the reflection threshold value. 6. An aircraft landing light unit according to claim 4, wherein the first subset of LEDs provides for more illumination in a pilot forward vision direction than the second subset of LEDs. 7. An aircraft landing light unit according to claim 4, wherein the second subset of LEDs provides for a broader field of illumination than the first subset of LEDs. 8. An aircraft landing light unit according to claim 2, wherein the reflection threshold value is a fixed threshold value. 9. An aircraft landing light unit according to claim 2, wherein the reflection threshold value is a variable threshold value, set depending on an ambient light level around the aircraft landing light unit. 10. An aircraft landing light unit according to claim 2, wherein the reflection threshold value is at least 10 times as high as an expected reflection value, corresponding to a light reflection from an airport runway in clear sky conditions. 11. An aircraft landing light unit according to claim 1, further comprising a photo detector lens, associated with the photo detector for condensing reflected light towards the photo detector. 12. An exterior aircraft lighting system, comprising: an aircraft landing light unit according to claim 1, andat least one further exterior aircraft light unit, the at least one further exterior aircraft light unit being coupled to the photo detector of the aircraft landing light unit and being configured to control its respective light output on the basis of the light detected by the photo detector of the aircraft landing light unit. 13. The exterior aircraft lighting system according to claim 12, wherein the at least one further exterior aircraft light unit is at least one anti-collision light unit. 14. A method of operating an aircraft landing light unit, comprising a plurality of LEDs, an optical system associated with the plurality of LEDs, and a photo detector, the method comprising the steps of: operating the plurality of LEDs in a nominal operating mode, thereby providing a light output of the aircraft landing light unit for illuminating an aircraft environment,detecting light, emitted by the plurality of LEDs, output via the optical system and reflected by atmospheric haze, such as clouds, fog, rain and snow,controlling the plurality of LEDs on the basis of the light detected by the photo detector, thereby adjusting the light output of the aircraft landing light unit to the atmospheric haze. 15. The method of operating an aircraft landing light unit according to claim 14, further comprising the step of: comparing the light detected by the photo detector to a reflection threshold value,wherein the step of controlling the plurality of LEDs comprises dimming a subset of the plurality of LEDs as a response to the light detected by the photo detector being above the reflection threshold value.
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이 특허에 인용된 특허 (11)
Calvin, Nathan Howard; Wilkinson, Dean Andrew, Aircraft external lighting system and method.
Hagan, Riley, Apparatus and method for preventing night blindness and/or vertigo among pilots caused by the reflection of an aircraft's anti-collision warning lights from clouds or other light reflecting conditions into the cockpit.
Stam, Joseph S.; Walstra, Eric J.; Berends, Keith H.; Rycenga, Brock R.; Longworth, Kevin J.; Meekhof, David A., Automatic vehicle exterior light control systems.
Rizkin Alexander ; Durets Yevgeniy Y. ; Oberg Carl E. ; Ruiz David ; Tudhope Robert H., Remote illumination system having a light output modifying apparatus.
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