WO1999039135A1 - Beamformer for a remotely illuminated lighting system and method - Google Patents
Beamformer for a remotely illuminated lighting system and method Download PDFInfo
- Publication number
- WO1999039135A1 WO1999039135A1 PCT/US1999/002756 US9902756W WO9939135A1 WO 1999039135 A1 WO1999039135 A1 WO 1999039135A1 US 9902756 W US9902756 W US 9902756W WO 9939135 A1 WO9939135 A1 WO 9939135A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- light
- reflective element
- source
- transforming
- beamforming device
- Prior art date
Links
Classifications
-
- G—PHYSICS
- G02—OPTICS
- G02B—OPTICAL ELEMENTS, SYSTEMS OR APPARATUS
- G02B6/00—Light guides; Structural details of arrangements comprising light guides and other optical elements, e.g. couplings
- G02B6/0001—Light guides; Structural details of arrangements comprising light guides and other optical elements, e.g. couplings specially adapted for lighting devices or systems
- G02B6/0005—Light guides; Structural details of arrangements comprising light guides and other optical elements, e.g. couplings specially adapted for lighting devices or systems the light guides being of the fibre type
- G02B6/0008—Light guides; Structural details of arrangements comprising light guides and other optical elements, e.g. couplings specially adapted for lighting devices or systems the light guides being of the fibre type the light being emitted at the end of the fibre
Definitions
- the present invention relates generally to lighting systems. More particularly, the present invention relates to remotely illuminated lighting systems, and to a beamforming device, or luminaire, for use in a remotely illuminated lighting system to provide a controlled, precise and dynamic light distribution pattern.
- ALS aircraft approach lighting system
- the conventional aircraft approach lighting system includes groups of incandescent lamps distributed over a field, lighting several thousand feet of the approach to the runway within specific requirements for angular light distribution, color and intensity.
- a major problem with the use of incandescent lamps in the ALS lies with monitoring the many light sources, i.e., each incandescent lamp, for failure.
- the availability of the ALS is dependent on the number and location of failed lamps in the system. Lamp replacement is a significant cost owing to the required human and equipment resources and the cost of the lamps.
- the towers upon which the lamps are mounted must, between the runway threshold and the 1000-foot bar, be of fragile or semi-fragile construction so as to minimize hazards to landing and departing aircraft. Yet, they must also be sufficiently rigid so as to support the lamps under widely varying weather conditions. Additionally, depending on the time of day and weather conditions, the system must be capable of providing up to five illumination intensity levels.
- Existing systems utilizing incandescent lamps include sophisticated control systems to provide and monitor lamp currents to achieve the required illumination intensity levels. System performance is inferred from measured lamp currents, which for several reasons such as lamp type, aging and current loop resistance differences, may not paint an accurate picture of system performance.
- EMI electromagnetic interference
- safety considerations such as reducing and/or eliminating ignition sources, for example, to fuel spilled during an accident.
- RSL remote source lighting
- the system disclosed and described therein incorporates a centralized light source or light engine.
- the light source is coupled via a light pipe system to one or more beamformer s.
- Each beamformer, or luminaire includes a light transformer and holographic diffuser for providing a desired light distribution with minimum intensity loss.
- System performance is directly, optically monitored.
- Centralized lighting sources with enhanced operational life greatly reduce -3-
- spark free beamformers provide safer, reduced cost illumination suitable for use in any number of operating environments.
- Still another object of the present invention is to provide a beamformer having an adaptable light distribution pattern.
- Yet another object of the present invention is to provide a beamformer having a dynamic light distribution pattern.
- An additional object of the present invention is to provide a low cost beamformer having little or no operational maintenance.
- Another object of the present invention is to provide a lighting system including a centralized light source and a fiber optic light distribution system and a plurality of beamformers for achieving a precise system of lighting.
- a further object of the present invention is to provide a method of providing a light distribution pattern.
- Figure 1 is a block diagram schematic of a remotely illuminated lighting system incorporating a beamformer in accordance with a preferred embodiment of the present invention
- Figure 2 is a schematic representation in side elevation of a beamformer illustrating the non-imaging light transformer and reflective element thereof in accordance with a preferred embodiment of the present invention
- Figure 3 is a schematic representation of a reflective element suitable for use in the beamformer shown in Figure 2;
- Figure 4 is a schematic representation of a first alternative embodiment of the reflective element shown in Figure 2; -5-
- Figure 5 is a schematic representation of a second alternative embodiment of the reflective element shown in Figure 2;
- Figure 6 is a schematic representation in side elevation of a beamformer illustrating the non-imaging light transformer, holographic diffuser and reflective element thereof in accordance with an alternative preferred embodiment of the present invention
- Figure 7 is a schematic perspective representation of a beamformer illustrating the non-imaging light transformer, holographic diffuser, diffusion mask and reflective element thereof in accordance with an additional alternative preferred embodiment of the present invention
- Figure 8 is a plan view of the diffusion mask shown in Figure 7 and an associated light distribution pattern
- Figure 9 is a schematic perspective representation of a beamformer illustrating the non-imaging light transformer and reflective element thereof in accordance with another alternative preferred embodiment of the present invention.
- Figure 10 is a perspective view of a diffusion mask in accordance with an alternative preferred embodiment of the present invention.
- Figure 11 is a schematic perspective representation of a beamformer illustrating the non-imaging light transformer and reflective element thereof in accordance with yet another alternative preferred embodiment of the present invention.
- a remotely illuminated lighting system distributes from a central illumination source light signals to remote light distribution devices.
- Each remote light distribution device, or beamformer is adaptable to produce a highly precise distribution pattern from the light signals. The distribution pattern may be easily adjusted in both horizontal and vertical directions.
- each beamformer is coupled via a fiber-optic cable to the central light source and includes a non-imaging light transformer -6-
- a holographic diffuser and/or a masking element are incorporated into the beamformer for adapting the shape of the light distribution pattern.
- An electronically controlled masking element may be further incorporated for providing flashing, moving or otherwise dynamic light distribution patterns.
- a remotely illuminated lighting system 10 is adaptable for operation as: 1) an approach lighting system (ALS), 2) a marine navigation lighting system, 3) an aircraft or motor vehicle lighting system 4) an obstruction lighting system or 5) a mine or hazardous area lighting system. Numerous other applications of remotely illuminated lighting system 10 are described in the afore-mentioned U.S. Patent No. 5,629,669, and still many others may be envisioned.
- the remotely illuminated lighting system 10 includes an illuminator 12 (also referred to as a light engine) providing a centralized source of light to beamformers 14 via a light delivery system 16.
- Beamformers 14 may be adapted to: 1) lighting towers (such as in an ALS), 2) aircraft, marine vessels and motor vehicles, or 3) remote and/or hazardous environments (such as mines, explosive manufacturing facilities, refineries, laboratories, and the like).
- Illuminator 12 includes a controlled power supply 20 suitably coupled to a source of electrical energy (not shown) and a direct optical regulator 26.
- Power supply 20 and direct optical regulator are coupled to each other and each are coupled to a lighting system controller 18, including a suitable control processor such as a microprocessor, for the communication of control signals.
- Power supply 26 and direct optical regulator 28 cooperate to control a supply of electrical power to a first light source 22 and a second light source 24.
- the light signals output from first light source 22 and second light source 24 are coupled through optical switch 28 to a high efficiency coupler 30.
- High efficiency coupler 30 couples light output from light sources 22 and 24 via optical switch 28 to light delivery system 16.
- Light delivery system 16 preferably includes an -7-
- optical splitter and a network of fiber-optic bundles for conducting light signals from illuminator 20 to one or more beamformers 14.
- first light source 22 and second light source 24 preferably generate a source of energy in the visible range that is concentrated by an elliptical or parabolic reflector to a focal spot.
- the high efficiency coupler 20 couples the light concentrated in the focal spot into the optical fibers that form light delivery system 22.
- light source 24 is preferably a redundant light source.
- Direct optical regulator 26 is preferably coupled to optical switch 28 to monitor the light output of both first light source 22 and second light source 24. Under normal conditions, only first light source 22 is supplied electrical power and thus is the only source of light signals.
- direct optical regulator 26 which causes signals to be sent to: 1) power supply 20 to cut power to first light source 22 and to provide power to second light source 24 and 2) optical switch 28 to receive light energy from second light source 24 for coupling to high efficiency coupler 30.
- beamformer 14 in accordance with a first preferred embodiment is shown in schematic detail.
- beamformer 14 includes a light-tight housing 100 having a generally cylindrical shape including a closed bottom 102, an open top 104 and a cylindrical cavity 106.
- a flanged aperture 112 is formed in bottom 102 for receiving a fiber-optic cable coupler 108.
- Fiber-optic cable coupler 108 is a suitable fiber-optic cable coupler for coupling beamformer 14 to a fiber-optic cable 110 of light delivery system 16.
- Housing 100 is preferably formed from plastic material using an appropriate molding process.
- a transparent annular window 110 Disposed and secured to top 104 is a transparent annular window 110 preferably constructed from a transparent plastic material. Annular window 110 axially extends -8-
- Reflective element 112 enclosing an end 114 of annular window 110.
- Reflective element 112 is preferably cone shaped with a pinnacle 116 thereof substantially aligned with a centerline of housing 100 and directed inwardly toward cavity 106.
- Reflective element 112 includes an angled reflective surface 118. More particularly, and best seen if Figures 3 - 5, reflective surface 118 is formed to an included angle with respect to the centerline of housing 100.
- Reflective element 112 may be formed using either a dielectric or a metallic configuration for providing reflective surface 118.
- Light transformer 120 includes a body portion 126 having a light entrance 122 and a light exit 124.
- Light entrance 122 is aligned closely adjacent coupler 108, and hence, closely adjacent an end 128 of fiber-optic cable 110 for coupling light signals from fiberoptic cable 110 into light transformer 120.
- Light transformer 120 is preferably of a construction shown and described in the afore-mentioned U.S. Patent No. 5,629,996 for reducing the light flux density per unit area so as to optimize the energy of the light coupled along fiber-optic cable 110 for its intended use in beamformer 14.
- Light transformer 120 may also be of the construction shown and described in the aforementioned United States Patent Application Serial No.
- the distributed light signals 130 exit light transformer 120 at light exit 124 and are directed onto reflective surface 118 and are reflected outwardly through annular window 110 forming light distribution pattern 132.
- light distribution pattern 132 extends radially from beamformer 14 in a 360° horizontal pattern having a vertical distribution angle .
- the vertical elevation of light distribution pattern 132 may be adjusted in beamformer 14 by adjusting the configuration of reflective element 112.
- Figure 3 illustrates reflective element 112 as shown in Figure 2. That is, reflective element 112 is formed with an included angle of 90°. A light ray 134 directed axially along housing 100 and striking reflective element 112 is reflected at an angle to the centerline of housing 100 that is equal to angle or also 90°.
- resulting light distribution pattern 132 for reflective element 112 is one that extends substantially radially outwardly from beamformer 14.
- reflective element 136 is formed with an included angle less than 90°.
- a light ray 134 directed axially along housing 100 and striking reflective element 136 is reflected at an angle to the centerline of housing 100 greater than 90°.
- the resulting light distribution pattern 132 for reflective element 136 is one that is directed upwardly from beamformer 14.
- reflective element 138 is formed with an included angle greater than 90°.
- a light ray 134 directed axially along housing 100 and striking reflective element 138 is reflected at an angle to the centerline of housing 100 less than 90°. In this manner, the resulting light distribution pattern 132 for reflective element 136 is one that is directed downwardly from beamformer 14.
- Beamformer 140 includes positioned between light transformer 110 and reflective element 112, a holographic diffuser 142.
- Holographic diffuser 142 is preferably a volumetric device and is adapted to shape the light signals from light exit 124 prior to striking reflective element 112. In this manner, the light distribution pattern 132, and in particular the vertical distribution angle , can be further controlled.
- holographic diffuser 142 is adapted to direct light rays 144 nearest the centerline of beamformer 140 radially inwardly with respect to the centerline.
- Light rays 144 thus strike reflective element 112 at an incident angle less than 45° and are thus reflected at an angle ⁇ , less than or less than 90°. In this manner, light rays 144 are reflected downwardly.
- Light rays 146 farthest from the centerline of beamformer 140 are directed radially outwardly with respect to the centerline. In this manner, light rays 146 strike reflective element 112 at an incident angle greater than 45° and are thus reflected at an angle 2, greater than or greater than 90°. Light rays 146 are thus reflected upwardly.
- beamformer 140 has a vertical distribution angle 2 greater than . It should be appreciated that many other light shaping patterns may be introduced by holographic diffuser for shaping and controlling the light distribution pattern of beamformer 140, and for example, to concentrate the light distribution pattern into a narrow vertical distribution.
- a beamformer 150 provides a horizontal light distribution pattern 158 of less than 360°.
- Beamformer 150 includes positioned between holographic diffuser 142 and reflective element 112 a mask element 152.
- Mask element 152 includes a substantially transparent portion 154 and a substantially opaque portion 156.
- Mask element 152 may be formed from a suitable low loss optically transparent material to which a mask coating is applied in the appropriate configuration.
- the effect of mask element 152 is to block light rays exiting light transformer 120 at light exit 124 from reaching reflective element 112 in predetermined regions.
- the resulting light distribution pattern 158 thus includes a region 162 in which light rays are reflected from reflective element 112 as described, and a region 160 in which no light rays are reflected.
- Beamformer 150 is thus suitable for applications requiring a less than 360° horizontal light distribution pattern, such as marine vessel mast head navigation lights. And, in contrast to the previously noted prior art, a greater than 180° horizontal light distribution pattern is possible with a single beamformer 150.
- Holographic diffuser 142 is shown and is included to provide a desired vertical distribution angle 2; however, it may not be required in every application of beamformer 150. Furthermore, it will be appreciated that holographic diffuser 142 may be coated or otherwise provided with an opaque region to accomplish the function of mask element 152.
- the light distribution pattern 158 may also be achieved utilizing the beamformer 170 shown in Figure 9.
- Beamformer 170 includes light transformer 120 and holographic diffuser 142 and reflective element 172.
- reflective element 172 is identical to reflective elements 112, 136 and 138.
- Reflective element 172 differs in that a portion 174 of reflective surface 118 is made non-reflective. This may be accomplished by a number of methods including 1) not coating portion 174 with reflective material, 2) applying a non-reflective coating to surface 118 in the area of -11-
- portion 174 or 3 applying a mask to reflective element 172.
- the effect is that light rays striking portion 174 are not reflected, and hence a light distribution pattern 158 is achieved.
- a beamformer 180 and associated electronically controlled mask 182 is shown.
- Mask 182 is positioned between light transformer 120 and reflective element 112.
- Mask 182 includes a plurality of liquid crystal cells, individually 201 - 220, respectively coupled to a controller 184 by a plurality of electrical leads 186, and a suitable common ground lead (not shown).
- Each cell 201 - 220 defines an angular portion of mask 182.
- Controller 184 preferably including an appropriate processing device, memory and buffer circuits, provides electrical energy to and selectively energizes cells 201 - 220. Energized cells transition from a substantially transparent state to a substantially opaque state. As seen in Figure 9, cells 201 - 203 are energized and are opaque. The remaining cells 204 - 220 remain transparent.
- mask 182 is operable to form light distribution pattern 158 as seen in Figure 8.
- all cells 201 - 220 but cell 212 are energized and opaque.
- controller 184 Under operation of controller 184, and in accordance with an appropriate sequencing algorithm which may be retained in the memory of controller 184 or hard programmed in, for example, an application specific integrated circuit, adjacent cell 211 is energized as cell 212 is deenergized.
- cell 210 is energized as cell 211 is deenergized. This process repeats progressively for each cell 201 - 220 of mask 182. In this manner, the resulting light distribution pattern will have the effect of a beam of light rotating about beamformer 180. Thus, a rotating beacon effect is created.
- all cells 201 - 220 may be selectively, and concomitantly, energized and deenergized.
- the resulting light distribution pattern is that of a flashing beacon, such as an obstruction-warning beacon.
- a flashing beacon such as an obstruction-warning beacon.
- numerous dynamic light distribution patterns may be achieved through the selective energization and deenergization of cells 201 - 220.
- Beamformer 180 is shown with 20 cells, namely, cells 201 - 220.
- the angular resolution in the horizontal plane is thus approximately 18°.
- the cells need not be formed as angular sections of mask 182, but may be formed in various configurations providing a wide variety of light distribution patterns. In certain applications it may be necessary to provide a colored light. For example, navigation lights are colored red for port, blue for starboard and white for stern, respectively. Obstruction lights are typically colored red.
- beamformers 14, 140, 150 170 and 180 may include a suitable colored filter disposed between light transformer 120 and reflective element 112. In the alternative, colored filters or colored light sources may be employed in illuminator 20.
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- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Optics & Photonics (AREA)
- Non-Portable Lighting Devices Or Systems Thereof (AREA)
Abstract
Description
Claims
Priority Applications (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EP99906831A EP1060342A4 (en) | 1998-02-03 | 1999-02-03 | Beamformer for a remotely illuminated lighting system and method |
CA002319324A CA2319324A1 (en) | 1998-02-03 | 1999-02-03 | Beamformer for a remotely illuminated lighting system and method |
JP2000529562A JP4439113B2 (en) | 1998-02-03 | 1999-02-03 | Remote lighting device |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US1754398A | 1998-02-03 | 1998-02-03 | |
US09/017,543 | 1998-02-03 |
Publications (1)
Publication Number | Publication Date |
---|---|
WO1999039135A1 true WO1999039135A1 (en) | 1999-08-05 |
Family
ID=21783183
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/US1999/002756 WO1999039135A1 (en) | 1998-02-03 | 1999-02-03 | Beamformer for a remotely illuminated lighting system and method |
Country Status (4)
Country | Link |
---|---|
EP (1) | EP1060342A4 (en) |
JP (2) | JP4439113B2 (en) |
CA (1) | CA2319324A1 (en) |
WO (1) | WO1999039135A1 (en) |
Cited By (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2381065A (en) * | 2001-10-05 | 2003-04-23 | Nicotech Ltd | Optical systems including conical or pyramidal reflectors |
US6582114B1 (en) * | 2001-12-11 | 2003-06-24 | The Boeing Company | Rotating fiber flasher system |
US6778729B1 (en) | 2000-04-17 | 2004-08-17 | The Boeing Company | Device and method for optical signal switching |
US6980715B2 (en) | 2003-09-29 | 2005-12-27 | The Boeing Company | Fiber optic rotary joint and method therefor |
EP2230179A1 (en) * | 2009-03-18 | 2010-09-22 | EADS Construcciones Aeronauticas, S.A. | Illuminating system for in-flight refuelling operations |
EP2263519A2 (en) * | 2009-06-17 | 2010-12-22 | Karl Storz GmbH & Co. KG | Endoscope tube |
CN105700156A (en) * | 2014-12-16 | 2016-06-22 | 赛洛米克斯股份有限公司 | Optic homogenizer |
RU2600121C1 (en) * | 2015-05-12 | 2016-10-20 | Федеральное государственное казенное военное образовательное учреждение высшего профессионального образования "Военный учебно-научный центр Военно-Морского Флота "Военно-морская академия имени Адмирала Флота Советского Союза Н.Г. Кузнецова" | Automated ship system for lighting communication |
RU2638057C2 (en) * | 2016-05-11 | 2017-12-11 | Федеральное государственное казенное военное образовательное учреждение высшего образования "Военный учебно-научный центр Военно-Морского Флота "Военно-морская академия имени Адмирала флота Советского Союза Н.Г. Кузнецова" | Automated shipboard complex of light-signal communication |
US12007097B2 (en) | 2022-10-11 | 2024-06-11 | Japan Display Inc. | Lighting device |
Citations (1)
Publication number | Priority date | Publication date | Assignee | Title |
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US5134550A (en) * | 1991-06-28 | 1992-07-28 | Young Richard A | Indirect lighting fixture |
Family Cites Families (5)
Publication number | Priority date | Publication date | Assignee | Title |
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JPS6179156A (en) * | 1984-09-26 | 1986-04-22 | Yamazato Erekutoronaito Kk | Needle type oxygen concentration detecting element |
JPH03173004A (en) * | 1989-11-30 | 1991-07-26 | Toshiba Lighting & Technol Corp | Lighting equipment |
JPH08106805A (en) * | 1990-04-23 | 1996-04-23 | Takeshi Namiki | Reflector structure projecting geometrical pattern |
JPH0414303A (en) * | 1990-05-08 | 1992-01-20 | Asahi Glass Co Ltd | Obstruction marking light |
US5629996A (en) * | 1995-11-29 | 1997-05-13 | Physical Optics Corporation | Universal remote lighting system with nonimaging total internal reflection beam transformer |
-
1999
- 1999-02-03 CA CA002319324A patent/CA2319324A1/en not_active Abandoned
- 1999-02-03 WO PCT/US1999/002756 patent/WO1999039135A1/en not_active Application Discontinuation
- 1999-02-03 EP EP99906831A patent/EP1060342A4/en not_active Withdrawn
- 1999-02-03 JP JP2000529562A patent/JP4439113B2/en not_active Expired - Fee Related
-
2009
- 2009-08-28 JP JP2009197728A patent/JP2009302063A/en active Pending
Patent Citations (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5134550A (en) * | 1991-06-28 | 1992-07-28 | Young Richard A | Indirect lighting fixture |
Non-Patent Citations (1)
Title |
---|
See also references of EP1060342A4 * |
Cited By (17)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6778729B1 (en) | 2000-04-17 | 2004-08-17 | The Boeing Company | Device and method for optical signal switching |
GB2381065A (en) * | 2001-10-05 | 2003-04-23 | Nicotech Ltd | Optical systems including conical or pyramidal reflectors |
GB2381065B (en) * | 2001-10-05 | 2004-03-03 | Nicotech Ltd | Optical systems including reflectors |
US6582114B1 (en) * | 2001-12-11 | 2003-06-24 | The Boeing Company | Rotating fiber flasher system |
US6980715B2 (en) | 2003-09-29 | 2005-12-27 | The Boeing Company | Fiber optic rotary joint and method therefor |
EP2230179A1 (en) * | 2009-03-18 | 2010-09-22 | EADS Construcciones Aeronauticas, S.A. | Illuminating system for in-flight refuelling operations |
WO2010106213A1 (en) * | 2009-03-18 | 2010-09-23 | Eads Construcciones Aeronáuticas, S.A. | Lighting system for in-flight refuelling operations |
EP2263519A3 (en) * | 2009-06-17 | 2011-04-20 | Karl Storz GmbH & Co. KG | Endoscope tube |
EP2263519A2 (en) * | 2009-06-17 | 2010-12-22 | Karl Storz GmbH & Co. KG | Endoscope tube |
EP3064123A1 (en) * | 2009-06-17 | 2016-09-07 | Karl Storz GmbH & Co. KG | Endoscope tube |
US10624526B2 (en) | 2009-06-17 | 2020-04-21 | Karl Storz Se & Co. Kg | Endoscope-pipe |
CN105700156A (en) * | 2014-12-16 | 2016-06-22 | 赛洛米克斯股份有限公司 | Optic homogenizer |
WO2016100013A1 (en) * | 2014-12-16 | 2016-06-23 | Cellomics, Inc. | Optic homogenizer |
US10353130B2 (en) | 2014-12-16 | 2019-07-16 | Cellomics, Inc. | Optic homogenizer |
RU2600121C1 (en) * | 2015-05-12 | 2016-10-20 | Федеральное государственное казенное военное образовательное учреждение высшего профессионального образования "Военный учебно-научный центр Военно-Морского Флота "Военно-морская академия имени Адмирала Флота Советского Союза Н.Г. Кузнецова" | Automated ship system for lighting communication |
RU2638057C2 (en) * | 2016-05-11 | 2017-12-11 | Федеральное государственное казенное военное образовательное учреждение высшего образования "Военный учебно-научный центр Военно-Морского Флота "Военно-морская академия имени Адмирала флота Советского Союза Н.Г. Кузнецова" | Automated shipboard complex of light-signal communication |
US12007097B2 (en) | 2022-10-11 | 2024-06-11 | Japan Display Inc. | Lighting device |
Also Published As
Publication number | Publication date |
---|---|
JP4439113B2 (en) | 2010-03-24 |
EP1060342A4 (en) | 2003-03-19 |
EP1060342A1 (en) | 2000-12-20 |
JP2009302063A (en) | 2009-12-24 |
JP2002502091A (en) | 2002-01-22 |
CA2319324A1 (en) | 1999-08-05 |
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