WO2002028711A8 - Dual mode light source for aircraft external lighting - Google Patents

Dual mode light source for aircraft external lighting

Info

Publication number
WO2002028711A8
WO2002028711A8 PCT/US2001/029110 US0129110W WO0228711A8 WO 2002028711 A8 WO2002028711 A8 WO 2002028711A8 US 0129110 W US0129110 W US 0129110W WO 0228711 A8 WO0228711 A8 WO 0228711A8
Authority
WO
WIPO (PCT)
Prior art keywords
light source
mode
dual mode
aircraft
current
Prior art date
Application number
PCT/US2001/029110
Other languages
French (fr)
Other versions
WO2002028711A2 (en
WO2002028711A3 (en
Inventor
John J Martin
Cary H Leach
Original Assignee
L 3 Comm Corp
John J Martin
Cary H Leach
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Priority to AU3038302A priority Critical patent/AU3038302A/en
Application filed by L 3 Comm Corp, John J Martin, Cary H Leach filed Critical L 3 Comm Corp
Priority to EP01986287A priority patent/EP1319324A4/en
Priority to AU2002230383A priority patent/AU2002230383A1/en
Priority to CA002422826A priority patent/CA2422826A1/en
Publication of WO2002028711A2 publication Critical patent/WO2002028711A2/en
Publication of WO2002028711A3 publication Critical patent/WO2002028711A3/en
Publication of WO2002028711A8 publication Critical patent/WO2002028711A8/en

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D47/00Equipment not otherwise provided for
    • B64D47/02Arrangements or adaptations of signal or lighting devices
    • B64D47/06Arrangements or adaptations of signal or lighting devices for indicating aircraft presence
    • HELECTRICITY
    • H05ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
    • H05BELECTRIC HEATING; ELECTRIC LIGHT SOURCES NOT OTHERWISE PROVIDED FOR; CIRCUIT ARRANGEMENTS FOR ELECTRIC LIGHT SOURCES, IN GENERAL
    • H05B45/00Circuit arrangements for operating light-emitting diodes [LED]
    • H05B45/10Controlling the intensity of the light
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D2203/00Aircraft or airfield lights using LEDs
    • HELECTRICITY
    • H05ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
    • H05KPRINTED CIRCUITS; CASINGS OR CONSTRUCTIONAL DETAILS OF ELECTRIC APPARATUS; MANUFACTURE OF ASSEMBLAGES OF ELECTRICAL COMPONENTS
    • H05K1/00Printed circuits
    • H05K1/02Details
    • H05K1/14Structural association of two or more printed circuits
    • HELECTRICITY
    • H05ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
    • H05KPRINTED CIRCUITS; CASINGS OR CONSTRUCTIONAL DETAILS OF ELECTRIC APPARATUS; MANUFACTURE OF ASSEMBLAGES OF ELECTRICAL COMPONENTS
    • H05K1/00Printed circuits
    • H05K1/18Printed circuits structurally associated with non-printed electric components
    • H05K1/189Printed circuits structurally associated with non-printed electric components characterised by the use of a flexible or folded printed circuit

Abstract

A dual mode light source unit (3) for an aircraft is configured to be secured into a socket for an incandescent navigation light bulb. The unit has electric circuitry configured to process the input current from the socket and based thereon operate in either civilian, visible mode or covert IR mode. When the current is in one electrical state, or a certain voltage level, the circuitry sends power to the visible light source (13). When the current is in a different state, the circuitry sends power only to the IR source (15). All control may be accomplished over a single pair of wires, as in existing systems that do not have IR mode capability. To upgrade existing aircraft, light source units (3) according to the invention are inserted into the existing navigational light sockets.
PCT/US2001/029110 2000-09-19 2001-09-17 Dual mode light source for aircraft external lighting WO2002028711A2 (en)

Priority Applications (4)

Application Number Priority Date Filing Date Title
AU3038302A AU3038302A (en) 2000-09-19 2001-09-12 Dual mode light source for aircraft external lighting
EP01986287A EP1319324A4 (en) 2000-09-19 2001-09-17 Dual mode light source for aircraft external lighting
AU2002230383A AU2002230383A1 (en) 2000-09-19 2001-09-17 Dual mode light source for aircraft external lighting
CA002422826A CA2422826A1 (en) 2000-09-19 2001-09-17 Dual mode light source for aircraft external lighting

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US09/665,600 US6559777B1 (en) 2000-09-19 2000-09-19 Dual mode light source for aircraft external lighting
US09/665,600 2000-09-19

Publications (3)

Publication Number Publication Date
WO2002028711A2 WO2002028711A2 (en) 2002-04-11
WO2002028711A3 WO2002028711A3 (en) 2002-06-13
WO2002028711A8 true WO2002028711A8 (en) 2003-07-03

Family

ID=24670761

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/US2001/029110 WO2002028711A2 (en) 2000-09-19 2001-09-17 Dual mode light source for aircraft external lighting

Country Status (4)

Country Link
US (1) US6559777B1 (en)
EP (1) EP1319324A4 (en)
AU (2) AU3038302A (en)
WO (1) WO2002028711A2 (en)

Families Citing this family (21)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7055994B2 (en) * 2000-09-19 2006-06-06 L-3 Communications Corporation Light source assembly and methods for aircraft external lighting
US6984061B1 (en) 2003-03-05 2006-01-10 Soderberg Manufacturing Co., Inc. Covert infrared landing light
US7314296B2 (en) * 2003-12-08 2008-01-01 Honeywell International Inc. Multi-platform aircraft forward position light utilizing LED-based light source
US7126290B2 (en) * 2004-02-02 2006-10-24 Radiant Power Corp. Light dimmer for LED and incandescent lamps
US7434970B2 (en) * 2004-03-12 2008-10-14 Honeywell International Inc. Multi-platform LED-based aircraft rear position light
US7414546B2 (en) * 2004-07-08 2008-08-19 Honeywell International Inc. White anti-collision light utilizing light-emitting diode (LED) technology
AT500892B1 (en) * 2004-09-01 2008-01-15 Pollmann Austria Ohg LIGHT-BEARING UNIT
US20060098448A1 (en) * 2004-11-06 2006-05-11 Mark Coast Multiple spectrum marker and light assembly for vehicles
FR2880406B1 (en) * 2005-01-06 2008-06-13 Ece Soc Par Actions Simplifiee LIGHT SIGNALING DEVICE
US7651054B2 (en) * 2006-04-13 2010-01-26 The Boeing Company Device, method, and aircraft for illuminating in-flight operations
US20080225547A1 (en) * 2006-10-02 2008-09-18 Rogers Thomas W LED vehicle lamp
US7701078B1 (en) 2007-08-06 2010-04-20 The United States Of America As Represented By The Secretary Of The Air Force Common bus aircraft retrofit load control
EP2157556B1 (en) * 2008-08-22 2011-04-06 Goodrich Lighting Systems GmbH Navigational lighting system for an airplane, in particular for military aircraft
US8289739B2 (en) * 2009-12-10 2012-10-16 Emerson Electric Co. Power supply continuous input voltage extender
US8284580B2 (en) * 2009-12-10 2012-10-09 Emerson Electric Co. Power supply discontinuous input voltage extender
US8890411B2 (en) 2011-10-14 2014-11-18 Control Solutions LLC Computer controlled configurable lighting system for modular vehicle lights
US9061772B1 (en) * 2012-06-11 2015-06-23 The Boeing Company Dual mode lights automatic intensity control
JP6017913B2 (en) * 2012-10-10 2016-11-02 株式会社東芝 Electronic apparatus and operation control method
US9868546B2 (en) 2015-06-22 2018-01-16 Goodrich Lighting Systems, Inc. Dual-mode vehicle light system
US10472089B2 (en) * 2016-03-01 2019-11-12 Goodrich Lighting Systems, Inc. Dual mode aft light with a first light emitter and a plurality of second light emitters
US10040575B2 (en) 2016-07-15 2018-08-07 Goodrich Lighting Systems, Inc. Dual mode aircraft light assembly

Family Cites Families (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4495549A (en) 1982-09-28 1985-01-22 The Boeing Company Infrared radiation filter lens for aircraft lights
US4733335A (en) 1984-12-28 1988-03-22 Koito Manufacturing Co., Ltd. Vehicular lamp
US5101326A (en) * 1990-09-27 1992-03-31 The Grote Manufacturing Co. Lamp assembly for motor vehicle
US5632551A (en) 1994-07-18 1997-05-27 Grote Industries, Inc. LED vehicle lamp assembly
GB9603350D0 (en) 1995-04-05 1996-04-17 Oxley Dev Co Ltd Aircraft lighting system
US5685637A (en) 1995-09-08 1997-11-11 Jimmy G. Cook Dual spectrum illumination system
US5984494A (en) 1995-09-08 1999-11-16 Jimmy G. Cook Light shield for an illumination system
US6045240A (en) 1996-06-27 2000-04-04 Relume Corporation LED lamp assembly with means to conduct heat away from the LEDS
KR20000053229A (en) 1996-11-12 2000-08-25 플렉 레오나르드 Lamp
GB2337645A (en) * 1998-05-21 1999-11-24 Avimo Ltd Warning light with overdriven LEDs
DE19931689A1 (en) 1999-07-08 2001-01-11 Patent Treuhand Ges Fuer Elektrische Gluehlampen Mbh Planar LED assembly on thermally-conductive board, increases cooling, component packing density and life, whilst permitting active device integration to form display- or illumination panel in or on e.g. vehicle
US6367949B1 (en) 1999-08-04 2002-04-09 911 Emergency Products, Inc. Par 36 LED utility lamp
US6244728B1 (en) 1999-12-13 2001-06-12 The Boeing Company Light emitting diode assembly for use as an aircraft position light
US6517218B2 (en) 2000-03-31 2003-02-11 Relume Corporation LED integrated heat sink
DE10034767A1 (en) 2000-07-18 2002-05-02 Hella Kg Hueck & Co lamp

Also Published As

Publication number Publication date
AU2002230383A1 (en) 2002-04-15
AU3038302A (en) 2002-04-15
US6559777B1 (en) 2003-05-06
WO2002028711A2 (en) 2002-04-11
WO2002028711A3 (en) 2002-06-13
EP1319324A4 (en) 2005-04-06
EP1319324A2 (en) 2003-06-18

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