Interior (e.g., Instrument, Cockpit) Patents (Class 362/471)
  • Publication number: 20040090787
    Abstract: Provided herein are methods and systems for illuminating environments, including aircraft environments. The methods and systems include facilities for providing both white and non-white illumination, with color and color temperature control, in programmed response to inputs. Methods and systems are also provided for improving the addressing of light systems in a network lighting configuration.
    Type: Application
    Filed: August 28, 2003
    Publication date: May 13, 2004
    Applicant: Color Kinetics, Inc.
    Inventors: Kevin J. Dowling, Frederick M. Morgan, Michael K. Blackwell
  • Publication number: 20030235055
    Abstract: An LED light bulb has a bulb base having an electrical contact, an outer sidewall, an insulator between the electrical contact and the outer sidewall. The LED light bulb further includes a bulb circuit board mounted upon the bulb base and extending upwardly therefrom. The bulb circuit board has a first side and a second side. A plurality of LEDs are mounted on the first and second sides of the bulb circuit board such that the plurality of LEDs are in electrical communication with the electrical contact through a resistor. A flange extending outwardly from the outer sidewall adjacent a bottom edge of the outer sidewall.
    Type: Application
    Filed: June 2, 2003
    Publication date: December 25, 2003
    Inventor: Pervaiz Lodhie
  • Publication number: 20030210554
    Abstract: The lamp (10) for a vehicle is provided with a housing (12), an illuminant (18) arranged in the housing (12) and a plug element (24) for electrically contacting the illuminant (18). Further, the lamp (10) comprises a pull-off-assisting element (30) for pulling the plug element (24) off the housing (12) in a pull-off direction (32). The pull-off-assisting element (30) comprises a first end (38) arranged at the plug element (24) such that it is pivotable about a pivoting axis (28) which extends transversely to the pull off direction (32), and a second end (40) configured for being manually gripped and pulling the pull-off-assisting element (30). This pull-off-assisting element (30) is pivotable between a parking position in which it rests against the housing (12), and a pull-off position in which it extends from the housing (12) for pulling off the plug element (24).
    Type: Application
    Filed: May 9, 2003
    Publication date: November 13, 2003
    Inventor: Rolf Broelemann
  • Patent number: 6568833
    Abstract: A light is disclosed which may be an aircraft light, comprising a base 2 for mounting the light, a chassis 8 upstanding from the base, a circuit board 10 mounted upon an outer face of the chassis and at least one solid state emitter—and more preferably an aray of LEDs 24, 26—mounted upon the circuit board. The invention provides a light which is constructionally convenient but can provide a clean beam pattern.
    Type: Grant
    Filed: June 27, 2001
    Date of Patent: May 27, 2003
    Assignee: Oxley Developments Company Limited
    Inventors: Michael Christopher Worgan, Timothy George Bushell
  • Patent number: 6520666
    Abstract: An apparatus for lighting or illuminating spaces, bodies or surfaces, which is formed from a plurality of light emitting diodes (1). The light emitting diodes (1) are radially enclosed by a casing body (14) which is adjoined at the end by a tubular element (15) which bears against a lens (4). A set spacing is thereby established between the light emitting diode (1) and the lens (4). All light spots issuing from the light emitting diode (1) are projected to form a single light spot of a high level of brightness by virtue of the superimposed relationship at a spacing in front of the lens (4).
    Type: Grant
    Filed: February 1, 2000
    Date of Patent: February 18, 2003
    Assignee: Diehl Luftfahrt Elektronik GmbH
    Inventors: Wolfgang Beyerlein, Thomas Krummer
  • Patent number: 6494587
    Abstract: A method of backlighting a flat panel display over an expanded dimming range includes providing a backlight including multiple cold cathode fluorescent lamps positionable directly behind a diffuser. Each of multiple drive circuits is adapted to independently adjust arc current of at least one of the multiple cold cathode fluorescent lamps in order to change the luminance output of the at least one of the cold cathode fluorescent lamps. Control signals are provided to each of the multiple drive circuits to separately control luminance output of different cold cathode fluorescent lamps such that at the same instant the different cold cathode fluorescent lamps are driven to substantially different luminance intensities, thereby allowing a reduction of an overall minimum luminance provided by the backlight and expanding the dimmable range of the backlight. A backlight implementing the methods of the invention is also disclosed.
    Type: Grant
    Filed: August 24, 2000
    Date of Patent: December 17, 2002
    Assignee: Rockwell Collins, Inc.
    Inventors: James E. Shaw, William G. Perreault
  • Patent number: 6454209
    Abstract: A comfort and illumination unit especially for a passenger space in an aircraft is constructed for cooperation with a straight wall panel that can be integrated in or secured to a vertical straight wall and/or a horizontal straight ceiling wall. The unit has a mounting base and a cover with passenger convenience elements mounted to the base under the cover which is provided with cut-outs for access to the convenience elements. Fluorescent bulbs form a frame around the convenience elements.
    Type: Grant
    Filed: June 12, 2000
    Date of Patent: September 24, 2002
    Assignee: Airbus Deutschland GmbH
    Inventors: Thomas Bock, Andrew Muin, Markus Schumacher
  • Patent number: 6422723
    Abstract: A portable cockpit illumination device for the purpose of supplementing existing cockpit illumination from an overhead type lamp assembly provides for an even illumination of all cockpit panel instruments. A portable design allows installation or removal from the cockpit in seconds without using any tools. Two modes of operation insure cockpit illumination under any flight conditions. An accessory power receptacle internal to an aircraft cockpit provides power during normal operation, and a self contained battery source provides cockpit illumination during emergency situations when no external power source is available. During normal operation, a charging circuit insures optimal battery performance. A plurality of light emitting diodes (LED's) wired in a series-parallel array receives power from a DC to DC buck converter, whereby an input source voltage is reduced to a lower output voltage. A rheostat controlled feedback voltage loop provides for load current and illumination control.
    Type: Grant
    Filed: June 9, 2000
    Date of Patent: July 23, 2002
    Inventor: Robert Charles Walters
  • Publication number: 20020015309
    Abstract: An emergency lighting system for an aircraft has photoluminescent material arranged to define an escape path to the exits. The photoluminescent material is encapsulated within a track of predetermined length for securing to the floor of the aircraft. The track comprises a one piece housing formed with a longitudinally extending slot and the photoluminescent material is provided by an insert that is a push-fit in the slot from one end of the housing. The housing is closed at both ends to seal the slot and prevent ingress of dirt or fluid. In a modification the housing is compressed with the insert in place to reduce the height of the track and optionally to provide the track with anti-slip characteristics.
    Type: Application
    Filed: July 23, 2001
    Publication date: February 7, 2002
    Inventors: Peter David Stokes, Peter Winstanley Bodle
  • Publication number: 20010053071
    Abstract: An indication lamp for, for instance, aircraft passenger cabins comprising light sources housed in lamp chambers defined by a housing and a front cover. Translucent indication portions of the shapes indicative of non-smoking and fasten-seatbelt signs in red, for instance, are formed in the front cover; and the light sources, each comprising a set of light emitting diodes of different colors, such as green and red, are installed behind the translucent indication portions so that each light source emits a mixture of colors that is similar to an incandescent light, thus illuminating the sings with an enhanced visibility.
    Type: Application
    Filed: June 7, 2001
    Publication date: December 20, 2001
    Applicant: KOITO MANUFACTURING CO., LTD.
    Inventors: Takashi Yoda, Kunio Toyota
  • Patent number: 6283621
    Abstract: A vehicle interior lamp assembly comprises a light assembly carried within a housing. A cover is snap fit to the housing and carries a lens in registration with the light assembly. The light assembly includes a dome shape reflector, into which a light bulb is positioned, and a light switch slidingly positioned within a slotted flange attached to the housing. A light switch actuator, in operational connection with the light switch, is captured by the cover. The lens is formed with a double convex middle region and a pair of outer regions formed with a plurality of serrations which reflect light toward the light reflector to thereby provide a uniform pattern of illumination about a preselected area. In one preferred embodiment, the housing supports a pair of lighting assemblies to permit selective illumination of a passenger's seat, table, or the like.
    Type: Grant
    Filed: June 4, 1999
    Date of Patent: September 4, 2001
    Assignee: ASC Industries, Inc.
    Inventor: Gregory G. Macri
  • Patent number: 6247825
    Abstract: A vehicle lighting system providing lighting for an instrument panel generating light having a wave length, such as white light, which does not interfere with night goggle vision systems. The system comprises a portable housing, a battery pack, and an plurality of cables extending outwardly from the housing to a plurality of light-emitting elements providing white light proximate each of the plurality of vehicle instruments.
    Type: Grant
    Filed: October 30, 1999
    Date of Patent: June 19, 2001
    Inventor: Richard E. Borkowski
  • Patent number: 6203180
    Abstract: Proposed is a lighting arrangement which is mounted at or in the ceiling (4) preferably of an aeroplane cabin (2), comprising a plurality of punctiform light sources (8), wherein the punctiform light sources (8) have at least one light emitting diode (LED) (9) and are at least partially connected together in parallel or in series and are connected to at least one power supply unit (14). A Zener diode (15) is connected in parallel in the reverse direction in relation to each light emitting diode or light emitting diode group. The power supply unit (14) is such that it provides for a constant current flow. The light emitting diodes used are preferably white light emitting diodes.
    Type: Grant
    Filed: August 11, 1999
    Date of Patent: March 20, 2001
    Assignee: Diehl Striftung & Co.
    Inventor: Walter Fleischmann
  • Patent number: 6158882
    Abstract: An LED semiconductor lighting system that comprises a lighting apparatus for illuminating vehicle interiors and powered by a source of electrical power provided by or on the vehicle. The lighting apparatus comprises a light tube with an interior space and has a plurality of light emitting diodes and current limiting resistors contained within such interior space of the light tube. The illumination intensity of the light emitting diodes is controlled by a dimming module in electrical contact with the LEDs and electrically connected to the vehicle source of power. An alternative embodiment of the lighting apparatus includes a flexible light tube.
    Type: Grant
    Filed: June 30, 1998
    Date of Patent: December 12, 2000
    Assignee: Emteq, Inc.
    Inventor: A. John Bischoff, Jr.
  • Patent number: 6106140
    Abstract: A lighting arrangement for a space or compartment (2) which can be closed off, with a fire-proofing ceiling (3), in particular for receiving freight in passenger aircraft, comprising lighting units (6) arranged in the fire-proofing ceiling (3), which for the purposes of static load relief of the fire-proofing ceiling (3) and at the same time for a better lighting effect for the space or compartment (2), has the following features: a plurality of through openings (19) are arranged in distributed fashion in the fire-proofing ceiling (3), fire-resistant light coupling-out elements (16) are arranged in the through openings (19) in such a way that their light cones (9) intersect in the space or compartment (2) and the light coupling-out elements (16) are connected by way of optical waveguides (14) to at least one common light source (15).
    Type: Grant
    Filed: January 29, 1999
    Date of Patent: August 22, 2000
    Assignee: Diehl Stiftung & Co.
    Inventors: Thomas Krummer, Otmar Kruppa
  • Patent number: 6092915
    Abstract: The present invention provides a decorative lighting laminate that can be made to glow or illuminate while shielding the laminate's light source components from view. The decorative lighting laminate is made from a decorative laminate that includes a transparent base layer and a thin translucent decorative covering layer. In a preferred embodiment, the base layer is made from a clear polycarbonate material and the decorative covering layer is made from an organic fluoropolymeric, such as a polyvinyl fluoride or a polyvinylidene fluoride polymeric material.
    Type: Grant
    Filed: January 30, 1998
    Date of Patent: July 25, 2000
    Assignee: The Boeing Company
    Inventor: Gregory James Rensch
  • Patent number: 6039451
    Abstract: Disclosed are a backlight and avionics display using the same to provide light to a liquid crystal display (LCD) device. In the backlight, a day mode light source positioned on a first side of the LCD device and adapted to provide a first source of light for use by the LCD device during day mode operations. A night mode light source positioned on the first side of the LCD device is adapted to provide a second source of light for use by the LCD device during night mode operations. A sculptured transflector positioned between the day mode light source and the night mode light source has, at a first side adjacent the day mode light source, a transflective material and a plurality of arcuate or parabolic surfaces in order to maximize a percentage of light from the day mode light source which is reflected toward the LCD device.
    Type: Grant
    Filed: June 4, 1998
    Date of Patent: March 21, 2000
    Assignee: Rockwell Science Center, Inc.
    Inventor: Duane A. Grave
  • Patent number: 5984494
    Abstract: The Dual Spectrum Illumination System (DSIS) is a modular light source having two independent emitters of optical radiation. A halogen bulb provides a high intensity visible beam. The second source of emissions is a ring of light emitting diodes (LED). The LED ring can be configured to supply area illumination, beam illumination, or a combination of area and beam illumination. The spectrum emitted by the LED is selectable from the wide range of commercially available diodes. The illumination system provides a beam and infrared area lighting using 21 high power, 6 watt, LEDs emitting at 880 nanometers mounted on the ring. Illumination control electronics are provided on a printed circuit assembly to provide the diodes with the correct current and voltage. A second embodiment of the invention is as a direct replacement for aircraft landing lights, mobile vehicle head lights, and any other situation requiring beam illumination.
    Type: Grant
    Filed: April 2, 1997
    Date of Patent: November 16, 1999
    Assignee: Jimmy G. Cook
    Inventors: Mark Garland Chapman, Laurence Hastings Bloxham
  • Patent number: 5921670
    Abstract: A lighting system for passenger cabins, particularly aircraft passenger cabins, is equipped with at least one central light source cooperating with hollow light guides for distributing light in the passenger cabin. The light sources may be positioned in fixed locations within the aircraft or in fixed locations in the ceiling or in mobile locations within the hollow light guides. Light extractors are positioned where needed. The light guides are hollow preferably tubular light guides which may cooperate with optical light conductor fibers, and with lenses and mirrors where needed.
    Type: Grant
    Filed: March 14, 1997
    Date of Patent: July 13, 1999
    Assignee: Daimler-Benz Aerospace Airbus GmbH
    Inventors: Markus Schumacher, Andrew Muin, Michael Lau
  • Patent number: RE36642
    Abstract: A fiber-optic lighting system is powered by a power supply connected to a high intensity light source which generates a beam of light. A first elongate light guide extends between a first end positioned within the beam of light and a second end positioned adjacent a lamp reflector. A second elongate light guide which is configured to emit light from a side also extends from a first end positioned within the beam of light. An elongate light fixture is positioned along the second light guide for directing light emitted from the side of the light guide.
    Type: Grant
    Filed: July 9, 1999
    Date of Patent: April 4, 2000
    Inventor: Bouchaib Ziadi