Rotationally symmetrical LED-based anti-collision light for aircraft
원문보기
IPC분류정보
국가/구분
United States(US) Patent
등록
국제특허분류(IPC7판)
F21V-001/00
B64D-047/06
출원번호
UP-0035365
(2005-01-13)
등록번호
US-7645053
(2010-02-22)
발명자
/ 주소
Machi, Nicolo F.
Singer, Jeffrey M.
Barnhart, Brian J.
출원인 / 주소
Honeywell International Inc.
대리인 / 주소
Black Lowe & Graham PLLC
인용정보
피인용 횟수 :
19인용 특허 :
19
초록▼
A rotationally symmetrical anti-collision light (100, 200) for an aircraft utilizing light-emitting diodes (LEDs) is mounted to the fuselage of an aircraft. The LEDs (10, 10′, 20, 20′) may be configured in one or more concentric rings. The anti-collision light includes a reflector (30,
A rotationally symmetrical anti-collision light (100, 200) for an aircraft utilizing light-emitting diodes (LEDs) is mounted to the fuselage of an aircraft. The LEDs (10, 10′, 20, 20′) may be configured in one or more concentric rings. The anti-collision light includes a reflector (30, 30′) configured to redirect the light emitted by at least one of the rings, so that the light pattern satisfies predetermined specifications.
대표청구항▼
What is claimed is: 1. A fuselage-mounted anti-collision light comprising: a base platform on which a first plurality of light-emitting diodes (LEDs) are arranged, the first plurality of LEDs being arranged in a symmetrical manner about a vertical axis; a top platform on which a second plurality of
What is claimed is: 1. A fuselage-mounted anti-collision light comprising: a base platform on which a first plurality of light-emitting diodes (LEDs) are arranged, the first plurality of LEDs being arranged in a symmetrical manner about a vertical axis; a top platform on which a second plurality of LEDs are arranged, the second plurality of LEDs being inverted with respect to the first plurality of LEDs; and a reflector coupling the top platform and base platform, the reflector having first and second portions that redistribute light from the first and second pluralities of LEDs, respectively, wherein, during operation, the anti-collision light is mounted to the exterior of an aircraft fuselage such that the first and second pluralities of LEDs are operationally arranged in a symmetrical manner about a common vertical axis of the aircraft, and wherein the diameter of the base platform is larger than the height of the mounted anti-collision light. 2. The anti-collision light of claim 1, wherein the first and second pluralities of LEDs are controlled to flash according to a rate of substantially 46 flashes per minute at a duty cycle of substantially 23%. 3. The anti-collision light of claim 1, wherein the diameter of the base platform is larger than the diameter of the top platform. 4. The anti-collision light of claim 1, wherein the second portion of the reflector redistributes the light from the second plurality of LEDs within a coverage area extending above the base plane, the coverage area being substantially symmetrical about the vertical axis. 5. The anti-collision light of claim 4, wherein the coverage area extends to substantially 40 degrees above the base plane, and the anti-collision light is configured to satisfy minimum intensity requirements corresponding to the coverage area. 6. The anti-collision light of claim 1, wherein at least one of the first and second LEDs are grouped into strings, each string comprising two or more LEDs electrically connected in series. 7. The anti-collision light of claim 6, further comprising: one or more current regulators, each electrically connected to a corresponding string of LEDs, wherein the current regulator is configured to maintain the current flowing through the corresponding string of LEDs at a predetermined level. 8. The anti-collision light of claim 1, wherein the anti-collision light is configured for at least two modes of operation, each of the modes corresponding to a particular type of light to be emitted in a flashing manner. 9. The anti-collision light of claim 8, wherein at least a portion of the first and second pluralities of LEDs are red LEDs, and another portion of the first and second pluralities of LEDs are white LEDs, and the anti-collision light is configured to be switchable between the following operating modes: a red-light mode, and a white-light mode. 10. The anti-collision light of claim 1, wherein the diameter of the top platform is smaller than the diameter of the base platform, the anti-collision light further comprising: a lens, which projects from the base to the top platform at an angle that reduces a drag coefficient. 11. The anti-collision light of claim 10, wherein the angle of the lens with respect to the base is substantially within the range of 35-40 degrees. 12. The anti-collision light of claim 10, wherein the top platform includes cooling fins, which are configured to further reduce the drag coefficient. 13. The anti-collision light of claim 1, wherein the first plurality of LEDs on the base platform are arranged as a first ring of LEDs, and the second plurality of LEDs on the top platform are arranged as a second ring of LEDs. 14. The anti-collision light of claim 13, wherein at least one of the first and second rings of LEDs flashes its LEDs in a rotational pattern, such that only a subset of its LEDs flash at any given time. 15. The anti-collision light of claim 13, wherein the first portion of the reflector is configured to redistribute the light from the first ring of LEDs in a coverage area, which extends from substantially 0 to 40 degrees above a base plane of the anti-collision light, and the second portion of the reflector is configured to redistribute the light from the second ring of LEDs in a supplemental coverage area, which extends at least up to substantially 75 degrees above the base plane. 16. The anti-collision light of claim 15, wherein the anti-collision light is configured to satisfy minimum intensity requirements corresponding to the coverage area and the supplemental coverage area. 17. A device comprising: a plurality of light-emitting diodes (LEDs) on a base, which are arranged in a symmetrical manner about a vertical axis, wherein the LEDs are grouped into strings, each string comprising two or more LEDs electrically connected in series; a reflector configured to redistribute light from LEDs on the base; and monitor circuitry for each string of LEDs, the monitor circuitry being configured to monitor the operating status of LEDs in each string, the monitor circuitry being operable to shut off the anti-collision light if a predetermined number of LEDs fail in any string. 18. The anti-collision light of claim 17, wherein the reflector operably couples the base to a top platform, a plurality of LEDs are arranged on the top platform, the LEDs on the top platform being inverted with respect to the LEDs on the base, each string of LEDs includes a plurality of the LEDs on the base and a plurality of the LEDs on the top platform, and each monitor circuitry is configured to shut down the anti-collision light if at least one of the following occurs with respect to the corresponding string: more than a pre-determined number of the LEDs on the base fail; and more than a pre-determined number of the LEDs on the top platform fail. 19. The anti-collision light of claim 17, wherein the monitor circuitry includes an LED sensing circuit configured to monitor potential voltage drops across the LEDs in a given string, the monitor circuitry being operable to determine a failure in a LED in response to a voltage drop. 20. The anti-collision light of claim 19, wherein the monitor circuitry provides an alternate current path for LEDs in the given string in response to an LED failure. 21. A device comprising: a plurality of light-emitting diodes (LEDs) on a base, which are arranged in a symmetrical manner about a vertical axis; and a reflector configured to redistribute light from LEDs on the base, wherein at least a portion of the LEDs on the base are visible LEDs, which are configured to emit light at a visible wavelength, the anti-collision light includes a plurality of infrared (IR) LEDs configured to emit light at substantially an IR wavelength, and the anti-collision light is configured to be switchable between the following operating modes: a visible mode, and an IR mode. 22. The anti-collision light of claim 21, wherein the visible LEDs include both red and white LEDs, and the anti-collision light is configured to be switchable between the following operating modes: a visible red-light mode, a visible white-light mode, and an IR mode. 23. The anti-collision light of claim 21, wherein the visible LEDs are grouped into strings, each comprising two or more visible LEDs electrically connected in series, and the IR LEDs are grouped into strings, each comprising two or more IR LEDs electrically connected in series. 24. The anti-collision light of claim 23, further comprising: a first set of one or more current regulators, each electrically connected to a corresponding string of LEDs; and a second set of one or more current regulators, each electrically connected to a corresponding string of IR LEDs, wherein each current regulator in the first and second sets is configured to maintain the current flowing through the corresponding string of LEDs at a predetermined level.
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이 특허에 인용된 특허 (19)
Runnels Russell W. (528 Greene Rd. Martinsville OH 45146), Aircraft collision pilot warning indicating system.
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