| 序号 | 专利名 | 申请号 | 申请日 | 公开（公告）号 | 公开（公告）日 | 发明人 |
|---|---|---|---|---|---|---|
| 121 | Lighting system of transport and aircraft | US14319373 | 2014-06-30 | US09415720B2 | 2016-08-16 | Takuya Yoshiguchi; Makoto Goto; Takahiro Tsujinishi |
| To provide a lighting system which can solve the inconvenience experienced by a pilot entering and leaving a control cabin of a transport such as an aircraft. A lighting system LS of an aircraft 1 includes: lights 21 that illuminate a control cabin 15; a lighting power supply system 22 including a main path 22M which supplies power to the lights 21 and a sub path 22S which supplies power to the lights 21; a first switch SW1 that enables and disables power supply through the main path 22M; and a second switch SW2 that enables and disables power supply through the sub path 22S. | ||||||
| 122 | LIGHTING ASSEMBLY FOR INTERIOR CABIN OF A VEHICLE | US14604809 | 2015-01-26 | US20160214529A1 | 2016-07-28 | William Hanson Valentine, JR.; Brock Prince; Matthew Roman Treinen; Alexey Meerov |
| A lighting assembly configured to be positioned within an internal cabin of a vehicle may include a housing defining an internal lighting chamber, a lens secured within the internal lighting chamber, wherein the lens includes a central longitudinal axis, and at least one light-emitting channel secured within the internal lighting chamber. The light-emitting channel(s) is offset in relation to the central longitudinal axis. | ||||||
| 123 | Side emitting glass element | US13903666 | 2013-05-28 | US09329318B2 | 2016-05-03 | Hubertus Russert |
| Side emitting glass elements are provided that include a plurality of light guiding elements, which are inseparably connected to one another at their outer circumferential surfaces, and at least one scattering element. The scattering element is inseparably connected to the outer circumferential surface of at least one light guiding element. The light guiding elements have at least one glass with a refractive index n1, wherein the individual light guiding elements are not enclosed by a cladding. A phase boundary is present between the light guiding elements through which the guided light can pass and to reach the scattering element. | ||||||
| 124 | Lighting | US13348991 | 2012-01-12 | US09302771B2 | 2016-04-05 | Daniel Alan Rust |
| Emergency lighting for an aircraft has a primary power source for light units provided by the normal aircraft power supply and a secondary power source provided by power supply units operable to back-up the primary power source. Each light unit may have its own power supply unit operable to power the light unit in an emergency if the normal aircraft power supply fails or is otherwise unable to power the emergency lighting. Each power supply unit includes one or more electric double layer capacitors that are charged whenever the normal aircraft power supply is operational to provide the primary power source. The useful life of the electric double layer capacitors may be prolonged by reducing the capacitor voltage when the emergency lighting is switched off. | ||||||
| 125 | PIVOT BIN ASSEMBLY WITH MINIMAL FORCE REQUIRED FOR CLOSING | US14924607 | 2015-10-27 | US20160083090A1 | 2016-03-24 | Scott Savian |
| An aircraft storage bin that includes an upper housing, and a bucket pivotally connected to the upper housing that cooperates with the upper housing to define a bin interior. The bucket includes a bottom, a front edge, first and second opposing side walls extending upwardly from the bottom and a center of gravity. The bucket pivots about a pivot axis with respect to the upper housing between an open position and a closed position. The center of gravity of the bucket is positioned below the pivot axis when the bucket is in the closed position. | ||||||
| 126 | Illumination apparatus, use of the illumination apparatus, method for dazzle-free illumination and arrangement comprising the illumination apparatus | US13744653 | 2013-01-18 | US09273849B2 | 2016-03-01 | Frank Schmid |
| It is an object of the invention to provide an improved illumination apparatus for the comfortable illumination of a region monitored by a night vision instrument.To this end, an illumination apparatus 1 having an illumination device 8 is provided, the illumination device 8 comprising at least one LED 9a,b,c and the illumination device 8 being formed in order to emit mixed light with light components in the visible range, and having an optical filter device 10 for filtering the mixed light emitted by the illumination device 8, the optical filter device 10 being formed in order to block light with a cutoff wavelength of more than 610 nm, wherein the illumination device 8 comprises a white LED 9a, a green LED 9b and a red LED 9c, which together produce the mixed light. | ||||||
| 127 | High brightness light emitting diode luminaire | US13366520 | 2012-02-06 | US09261258B2 | 2016-02-16 | Storm S. Sears |
| A light emitting diode (LED) luminaire that produces a uniform light pattern at close distances is provided. The LED luminaire includes a housing, a printed circuit board assembly thermally coupled to the housing, a plurality of high brightness (HB) LED emitters, thermally coupled to the printed circuit board assembly to form a linear array, and a linear reflector assembly, attached to the housing, to concentrate the light generated by the LED emitters over a beam angle formed by the upper surface of the housing and the linear reflector assembly. | ||||||
| 128 | Lighting system | US14250908 | 2014-04-11 | US09227727B2 | 2016-01-05 | Tadasi Nisimura; Youji Tachino; Atsushi Motoya; Takashi Ohta; Hiroshi Kido; Junichi Hasegawa; Shigeo Gotoh; Nobuyuki Matsui; Tadashi Murakami |
| A lighting system includes a lighting apparatus provided along one side of an aisle and a specular reflection plate provided along the other side of the aisle to reflect the light emitted from the lighting apparatus toward a region where the lighting apparatus is provided. According to the above configuration, the lighting apparatus can illuminate the region where the lighting apparatus is provided. Therefore, it is possible to effectively illuminate a cabin of an aircraft with less lighting apparatuses as compared to conventional lighting apparatuses which are provided along both sides of the aisle. Moreover, since the number of the lighting apparatuses can be reduced, it is possible to improve fuel efficiency of the aircraft by reducing the total weight of the aircraft. | ||||||
| 129 | Method and system for determination of performance and response to electromagnetic radiation | US13874638 | 2013-05-01 | US09205932B2 | 2015-12-08 | Melanie L. Kimsey-Lin; Taylor A. Chaintreuil |
| A method of selecting a lighting pattern of an aircraft is disclosed herein. The method comprises exposing a photoluminescent element to electromagnetic radiation emitted from a light source of the aircraft. The light source has (a) a spectral power distribution and (b) an illumination level. The method also comprises calculating a total energy absorbed by the photoluminescent element based on (a) the spectral power distribution, (b) the illumination level, and (c) an exposure duration. The method comprises correlating the total energy absorbed to a discharge duration based on a normalized photoluminescent response function of the photoluminescent element. And the method also comprises verifying that the (a) spectral power distribution, (b) illumination level, and (c) exposure duration of the light source are in compliance with operational guidelines for the light source and the photoluminescent element based on the discharge duration. | ||||||
| 130 | LIGHTING DEVICE FOR THE INTERIOR FURNISHING OF AN AIRCRAFT CABIN | US14700690 | 2015-04-30 | US20150314873A1 | 2015-11-05 | Sylvain Mariat; Jean-Cyrille Destieu; Beranger Chantal; Jean-Luc Legros; Nicolas Ferrere; Pascal Taffarello |
| An aircraft fuselage comprising a structural wall and a floor delimiting a cabin for passengers, said wall being covered by a plurality of adjacent trim panels arranged in succession in the longitudinal direction of the fuselage and spaced from one another with a gap between two adjacent panels. Each panel is also fixed to the wall and has a concave shape adapted to the shape of the fuselage. At least one lighting device is disposed at the level of at least one of the gaps and is arranged perpendicularly to a longitudinal axis of the fuselage. The lighting device comprises a housing fixed to the wall. The housing is provided with an opening on a face oriented toward the interior of said cabin. The housing further comprises at least one lighting element making it possible to light the cabin through the gap. | ||||||
| 131 | Pivot bin assembly | US14622377 | 2015-02-13 | US09174734B2 | 2015-11-03 | Scott Savian; Corey Williams |
| A pivot bin assembly configured to receive luggage and be positioned in the interior of an aircraft. The pivot bin assembly includes an upper housing that includes a strongback and first and second side panels, a bucket that cooperates with the upper housing to define a bin interior, a first pivot mechanism operatively associated with the first side panel and the bucket, and a second pivot mechanism operatively associated with the second side panel and the bucket. The first and second pivot mechanisms are axially aligned along a pivot axis such that the bucket pivots about the pivot axis with respect to the upper housing between an open position and a closed position. | ||||||
| 132 | PIVOT BIN ASSEMBLY | US14796829 | 2015-07-10 | US20150307192A1 | 2015-10-29 | Scott Savian |
| An aircraft storage bin that includes an upper housing, and a bucket pivotally connected to the upper housing that cooperates with the upper housing to define a bin interior. The bucket includes a bottom, a front edge and first and second opposing side walls extending upwardly from the bottom and pivots about a pivot axis with respect to the upper housing between an open position and a closed position. When the storage bin is installed in an aircraft, a first horizontal distance is defined between a first vertical line that extends through the pivot axis and the front edge of the bucket when the bucket is in the closed position, and a second horizontal distance is defined between the first vertical line and the front edge of the bucket when the bucket is in the open position. The first horizontal distance is greater than the second horizontal distance. | ||||||
| 133 | Pivot bin assembly | US13765652 | 2013-02-12 | US09162617B2 | 2015-10-20 | Scott Savian; Stephen Kearsey |
| A pivot bin assembly configured to receive luggage and be positioned in the interior of an aircraft. The pivot bin assembly includes an upper housing that includes a strongback and first and second side panels, a bucket that cooperates with the upper housing to define a bin interior, a first pivot mechanism operatively associated with the first side panel and the bucket, and a second pivot mechanism operatively associated with the second side panel and the bucket. The first and second pivot mechanisms are axially aligned along and are rotatable about a pivot axis such that the bucket pivots about the pivot axis with respect to the upper housing between an open position and a closed position. | ||||||
| 134 | LED STRIP LIGHTING DEVICE FOR A CABIN OF A PASSENGER AIRCRAFT | US14640419 | 2015-03-06 | US20150257224A1 | 2015-09-10 | Birger Timm; Volker Antonczyk; Henrik Heine |
| The invention relates to a LED strip lighting device for a cabin of a passenger aircraft, the device comprising at least one LED strip, comprising a plurality of N independently controllable LED segments (S), wherein each LED segment (S) comprises at least four LED selected from red, green, blue, ice blue, warm white and cold white or another type of LED; a plurality of M driver units, wherein each LED section (S) is connected to a driver unit for providing a control signal to the respective LED section (S); and a bus system connecting all M driver units. The device further comprises a micro controller connected to the bus system for providing control signals for each driver unit, such that each LED segment (S) emits light in intensity and color according to a predetermined illumination pattern. | ||||||
| 135 | AIRCRAFT CABIN LIGHT SYSTEM | US14640400 | 2015-03-06 | US20150251594A1 | 2015-09-10 | Birger Timm; Volker Antonczyk; Henrik Heine |
| The invention relates to an interior lighting device for mounting at a ceiling portion of a cabin interior of a passenger aircraft. The invention further relates to a lighting arrangement of two or more of such interior lighting devices and a passenger aircraft comprising a passenger cabin, wherein the cabin has such a lighting arrangement. The transparent area light source and the reading lights are highly integrated and the reading light is placed behind the transparent area light source. Both together are mounted preferably in a ceiling portion of the cabin interior, for example within a PSU, which is placed above the head of a passenger. | ||||||
| 136 | Lighting apparatus | US14250900 | 2014-04-11 | US09127815B2 | 2015-09-08 | Youji Tachino; Atsushi Motoya; Takashi Ohta; Hiroshi Kido; Junichi Hasegawa; Shigeo Gotoh; Nobuyuki Matsui; Tadashi Murakami; Tadasi Nisimura |
| This lighting apparatus includes three or more LEDs arranged in a row. Each of the LEDs emits light of a color different from that of an LED adjacent to itself, and the LEDs include an LED having a relatively wide light distribution angle and others of the three or more LEDs each having a relatively narrow light distribution angle. The one LED is arranged in an inner portion in the row of the other LEDs. In this configuration, light emitted from the one LED is mixed well with lights emitted from the respective other LEDs adjacent to the one LED, and thus, color unevenness of illuminating light can be reduced. | ||||||
| 137 | CEILING TRIM ELEMENT FOR AN INTERIOR TRIM ARRANGEMENT OF AN AIRCRAFT CABIN | US14619723 | 2015-02-11 | US20150232168A1 | 2015-08-20 | Benedikt Kircher; Paul Edwards |
| A ceiling trim element for a passenger cabin of a vehicle, in particular for an aircraft cabin of an aircraft which has a planar panel element with a front side and a rear side, wherein the front side is provided to point towards the interior of the passenger cabin, and the rear side is provided to point away from the interior of the passenger cabin, wherein an image surface is provided in the panel element, wherein the image surface is assigned a varying pattern generator in order to illuminate the image surface with varying patterns, and having an illuminating ring generator to generate an illuminating ring which surrounds the image surface. | ||||||
| 138 | PSU pod assembly and method for using same | US13765646 | 2013-02-12 | US09079528B2 | 2015-07-14 | Scott Savian |
| A PSU pod assembly that is configured to be positioned in the interior of an aircraft. The PSU pod assembly includes a PSU pod that includes a housing that includes a top, a bottom and first, second, third and fourth sides that cooperate to define a pod interior and a panel positioned above and connected to the PSU pod. The PSU pod includes at least first and second reading lights positioned within the pod interior that are configured to shine light below the housing and cabin lights positioned on or in the housing that are configured to shine light above the housing. The panel includes connectors that are configured to secure the PSU pod assembly to a component within the aircraft. | ||||||
| 139 | PIVOT BIN ASSEMBLY | US14622377 | 2015-02-13 | US20150151839A1 | 2015-06-04 | Scott Savian; Corey Williams |
| A pivot bin assembly configured to receive luggage and be positioned in the interior of an aircraft. The pivot bin assembly includes an upper housing that includes a strongback and first and second side panels, a bucket that cooperates with the upper housing to define a bin interior, a first pivot mechanism operatively associated with the first side panel and the bucket, and a second pivot mechanism operatively associated with the second side panel and the bucket. The first and second pivot mechanisms are axially aligned along a pivot axis such that the bucket pivots about the pivot axis with respect to the upper housing between an open position and a closed position. | ||||||
| 140 | Calibration method for LED lighting systems | US13035329 | 2011-02-25 | US09018858B2 | 2015-04-28 | Gannon T. Gambeski; David P. Eckel; Seckin K. Secilmis; Andrew B. Walsh; Richard Waring, Jr.; Rand Lee; David Jenkins; Maciej Adam Jakuc; Jeffrey Reeder |
| A method of operating a lighting fixture comprising a plurality of discrete illumination sources of distinguishably different color coordinates comprises determining target color coordinates and luminous flux at which to operate the lighting fixture, determining input electrical power values for each of the plurality of discrete illumination sources that substantially produce the target color coordinates and luminous flux by referencing a calibration data lookup table having calibration data based on measurements of the plurality of discrete illumination sources, determining a color mixing zone defined by three distinguishably different color coordinates of the plurality of discrete illumination sources within which the target color coordinates lie according to the calibration data, determining luminous flux ratios for each of the plurality of discrete illumination sources having one of the three distinguishably different color coordinates defining the color mixing zone that substantially produces the target color coordinates, and determining input electrical power levels for each of the plurality of discrete illumination sources that generate the determined luminous flux ratios. | ||||||
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