Illumination – Supported by vehicle structure – Aircraft
Reexamination Certificate
2004-08-18
2008-10-14
Sawhney, Hargobind S (Department: 2885)
Illumination
Supported by vehicle structure
Aircraft
C362S539000
Reexamination Certificate
active
07434970
ABSTRACT:
An aircraft rear position light device (1) has a modular configuration. The device utilizes solid-state light sources. In an exemplary embodiment, the light sources are side-emitting light-emitting diodes (LEDs) (40), which are attached to a heat sink (30). A reflector (200) is positioned next to each of the LEDs. The device further includes an outer lens (10) with an integrated cut-off shield (110) and optical treatments (120). The configuration of LEDs and reflectors, in conjunction with the cut-off shield and optical treatments, allows the emitted light to satisfy predetermined minimum and maximum angular intensity requirements. An electronics module (50) is also attached to the heat sink to connect the LEDs to a power source in the aircraft. Electronic updates may be made by replacing the electronics module.
REFERENCES:
patent: 4663627 (1987-05-01), Dennis
patent: 6354714 (2002-03-01), Rhodes
patent: 6461029 (2002-10-01), Gronemeier et al.
patent: 6462669 (2002-10-01), Pederson
patent: 6483439 (2002-11-01), Vukosic
patent: 6507290 (2003-01-01), Lodhie et al.
patent: 6559777 (2003-05-01), Martin et al.
patent: 6568833 (2003-05-01), Worgan et al.
patent: 6578986 (2003-06-01), Swaris et al.
patent: 6598998 (2003-07-01), West et al.
patent: 6641284 (2003-11-01), Stopa et al.
patent: 6669357 (2003-12-01), Konicke et al.
patent: 6674096 (2004-01-01), Sommers
patent: 6679621 (2004-01-01), West et al.
patent: 6799870 (2004-10-01), Lin
patent: 6866394 (2005-03-01), Hutchins et al.
patent: 6964507 (2005-11-01), Mohacsi
patent: 6994459 (2006-02-01), Worsdell et al.
patent: 7021801 (2006-04-01), Mohacsi
patent: 2002/0018009 (2002-02-01), Rast
patent: 2002/0048174 (2002-04-01), Pederson
patent: 2002/0196637 (2002-12-01), Dubin et al.
patent: 2003/0048641 (2003-03-01), Alexanderson et al.
patent: 2003/0107885 (2003-06-01), Galli
patent: 2003/0174499 (2003-09-01), Bohlander
patent: 2004/0208018 (2004-10-01), Sayers et al.
patent: 2005/0068777 (2005-03-01), Popovic
patent: 2005/0093718 (2005-05-01), Martin
patent: 2005/0110649 (2005-05-01), Fredericks et al.
patent: 2005/0111220 (2005-05-01), Smith
patent: 2005/0128759 (2005-06-01), Fredericks et al.
patent: 1168902 (2002-01-01), None
patent: WO-03/068599 (2003-08-01), None
Honeywell: “Introducing Honeywell Astreon Solid State Lighting for Business Aircraft,” Oct. 2003. URL: http://honeywellaes.com/lighting/index.jsp>.
Machi Nicolo F.
McKenzie Mark A.
Singer Jeffrey M.
Black Lowe & Graham PLLC
Honeywell International , Inc.
Sawhney Hargobind S
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