| 序号 | 专利名 | 申请号 | 申请日 | 公开（公告）号 | 公开（公告）日 | 发明人 |
|---|---|---|---|---|---|---|
| 181 | PASSENGER SERVICE UNIT POD ASSEMBLY | US14612044 | 2015-02-02 | US20150166178A1 | 2015-06-18 | Scott Savian |
| A personal service unit pod assembly configured to be positioned in the interior of an aircraft. The personal service unit pod assembly includes a personal service unit pod and a panel positioned directly above and affixed to the personal service unit pod. The pod includes a housing with a lens assembly and a pod interior, a first reading light positioned within the pod interior and configured to shine light below the bottom of the housing, and cabin lighting positioned in the housing and configured to shine light through the lens assembly and above the housing. The panel includes connectors that are configured to secure the personal service unit pod assembly to a component within the aircraft. | ||||||
| 182 | READING LAMP FOR INSTALLATION IN A CABIN TRIM ELEMENT OF A VEHICLE | US14526657 | 2014-10-29 | US20150117040A1 | 2015-04-30 | Matthias HARTMANN; Thomas WENINGER |
| The invention relates to a reading lamp for installation in a cabin trim element (4) of a vehicle, in particular of an aircraft, comprising an installation frame (1) having a ring element (2), a lamp housing (7) having a mating support surface (8), and a clamping ring (9) wherein the clamping ring (9) is connected to the installation frame (1) by means of tension spring elements (10), such that the lamp housing (7) is forced against the support surface (6) of the inner surface of the ring element (2) by means of the clamping ring (9) and may be moved with respect to the installation frame (1) in the manner of a ball and socket joint. | ||||||
| 183 | Display assembly with lighting apparatus | US13311053 | 2011-12-05 | US09004590B2 | 2015-04-14 | Rik Westerink; Timothy W. Terleski; Per Magnus Skold; Alexander Gerard Saucier; Armando Valdes |
| Described are display assemblies having a display coupled to a passenger seat back, a video shroud coupled to the passenger seat back and with an inner opening positioned adjacent the display, wherein a gap is positioned between an outer edge of the display and an edge of the inner opening, and a light apparatus having at least one lighting element coupled to the passenger seat back, wherein the at least one lighting element is positioned to emit light through the gap. The display assembly may also include a diffuser coupled to the video shroud and positioned adjacent the gap. | ||||||
| 184 | OVERHEAD BIN SYSTEM | US14287731 | 2014-05-27 | US20150097081A1 | 2015-04-09 | Amauri PAULINO; Sergio Luiz Abdalla Gomide; Gustavo Selofite De Arruda; Nilmar César Ferreira; Luciano Dos Santos Ribeiro; Demétrio Andrade De Campos; Sergio Augusto Meireles Filho; Frederico Lara De Oliveira; Douglas Gonçalves De Albuquerque; Helio Albino; André Duarte Stein; Paul Priestman; Daniel Macinnes |
| Overhead bin assembly for transport vehicles (e.g., transport category aircraft) are provided with a generally U-shaped bin shell having a bottom wall, an outboard end wall and an upper wall defining an interior stowage space having an inboard opening opposite the end wall. A pair of separated transverse bin supports defining a bin space therebetween may be provided along with a bin door for closing the inboard opening. A cantilever hinge may be provided so as to connect the bin door to the transverse bin support in a cantilever manner to allow for pivotal movement of the bin door between closed and open positions relative to the inboard opening. An arcuate recessed wall may be positioned inboard relative to the upper wall of the bin shell (e.g., as a unitary (one-piece) extension thereof) such that the bin door is received within the recessed wall when in the open position thereof. | ||||||
| 185 | Multi functional supply profile | US12971630 | 2010-12-17 | US08998687B2 | 2015-04-07 | Uwe Schneider |
| A supply system is provided that includes, but is not limited to a profile element. The profile element includes, but is not limited to a front wall, a rear wall, and webs between the front wall and the rear wall so that there are ducts within the profile element. The supply system also includes, but is not limited to at least one functional component integrated in at least one of the plurality of ducts. | ||||||
| 186 | MODULAR OVERHEAD BIN | US14540582 | 2014-11-13 | US20150069182A1 | 2015-03-12 | Sönke JACOBSEN; Marcus GEHM; Steffen ELSTNER; Dieter KRAUSE |
| An overhead bin for an aircraft comprises a base unit that is designed to fasten the overhead bin to a retaining structure of the aircraft, and a mounting unit that is connected to the base unit. By way of the mounting unit, a stowage space of the overhead bin can be accessed. The base unit provides a first stowage space region, and the mounting unit provides a second stowage space region that together with the first stowage space region forms the stowage space of the overhead bin. | ||||||
| 187 | LIGHTING APPARATUS AND VEHICLE | US14450429 | 2014-08-04 | US20150043230A1 | 2015-02-12 | Martin BACHHUBER; Frank SCHMID |
| The invention relates to a lighting apparatus (3), in particular reading lamp, for recessing in a trim (1) of a passenger cab of a vehicle, in particular a land vehicle, aircraft, or watercraft, in which a first light-emitting device (4) is held pivotably on a recess-mounting frame (2) so that a light-emitting direction of the first light-emitting device (4) with respect to the recess-mounting frame (2) is changeable. In order to simplify the design of a lighting apparatus (3) for illuminating a passenger cab, the invention proposes that the recess-mounting frame (2) has, on its visible side (S), a second light-emitting device (5) which at least sectionally surrounds the first light-emitting device (4) and which is fitted invariably in respect of its light-emitting direction on the recess-mounting frame (2). | ||||||
| 188 | AIRCRAFT SEATING UNIT WITH FIXTURE MEMBER | US14321855 | 2014-07-02 | US20150008283A1 | 2015-01-08 | Wolfgang Rittner; Günter Boomgaarden |
| The invention relates to an aircraft passenger service arrangement comprising one or more passenger service units for arrangement above a passenger seat, and a fixture member. The passenger service arrangement is characterized in that the fixture member is adapted for directly fixing the passenger service unit to a passenger seat in a defined relationship to each other. Further the invention relates to a seating device comprising an aircraft passenger service arrangement. | ||||||
| 189 | PASSENGER SUPPLY SYSTEM FOR INSTALLATION IN A PASSENGER SUPPLY CHANNEL | US14269715 | 2014-05-05 | US20140329452A1 | 2014-11-06 | Tobias Wirth; Sebastian Umlauft |
| A passenger supply system installed in a passenger supply channel (PSC) on board a vehicle, such as an aircraft. The supply system comprises a rail track configured to be mounted along the PSC. The supply system further comprises an indiv panel mounted on the rail track and connectable to the PSC for supplying a passenger with conditioned air, medical outlet and/or oxygen. The indiv panel comprises a crossover area. The supply system further comprises a passenger supply unit mounted on the rail track and connectable to the PSC for supplying the passenger with light, visual information and/or sound information. The supply unit comprises an overlapping area. The supply unit and the indiv panel are configured such that in a mounted state of the supply unit and of the indiv panel the overlapping area of the supply unit at least partially overlaps with the crossover area of the indiv panel. | ||||||
| 190 | Direction Controlled Service Apparatus | US13863360 | 2013-04-15 | US20140306059A1 | 2014-10-16 | Douglas A. Brown; Kwun-Wing W. Cheung |
| A direction controlled service apparatus may include a mounting assembly, a housing assembly configured to operably connect to the mounting assembly, the housing assembly being movable with respect to the mounting assembly, and a plurality of actuators connected between the mounting assembly and the housing assembly, each actuator of the plurality of actuators being configured to contract upon a current being applied to the actuator to rotate the housing assembly with respect to the mounting assembly. | ||||||
| 191 | Retractable passenger seat | US13287158 | 2011-11-02 | US08851568B2 | 2014-10-07 | Robert Funk; Rebeca Rubio Trevizo; Fernando Luis Bencomo Arvizo; Gabriela Alejandra Gonzalez Gonzalez; Raul Daniel Flores Aguirre |
| Described are passenger seat assemblies having at least one seat back support pivotally coupled to an overhead support structure, at least one seat pan pivotally coupled to the at least one seat back support, and at least one foot rest support may be pivotally coupled to the seat pan. The seat back support may be configured to rotate into a retracted position adjacent the overhead support structure. The seat pan may be configured to rotate into a retracted position adjacent the seat back support. Finally, the foot rest support may be configured to rotate into a retracted position adjacent the seat pan. | ||||||
| 192 | Integration of supply functions in a storage compartment | US13244442 | 2011-09-24 | US08851420B2 | 2014-10-07 | Ralf Schliwa; Martin Frey; René Stoll; Andreas Tolksdorf; Uwe Schneider |
| Integration of supply functions is provided in a storage compartment. In particular, an integrated module is provided, which can be mounted in the overhead area of a passenger cabin, and exhibits different system components, which are automatically hooked up to the supply system of the transport (e.g., an aircraft) during the mechanical installation of the module on the load-bearing structure of the cabin. | ||||||
| 193 | READING LIGHT | US14150603 | 2014-01-08 | US20140192544A1 | 2014-07-10 | Ben Orson; Zhao Jin; Christian Mecke |
| A lighting assembly that includes an outer housing defining an outer housing axis, an inner housing defining an inner housing axis and a light member positioned in the inner housing. The outer housing includes a front surface having a front opening and an inner surface that defines an adjustment cavity having a truncated spherical shape. The inner housing has a truncated spherical shape and is at least partially received within the adjustment cavity. The inner housing defines a light recess therein and includes a front cover having an aperture defined therein. The front cover at least partially defines the light recess. The light member defines a light axis. The light axis and the inner housing axis are not co-axial and not parallel and form an angle therebetween. The inner housing is adjustable between a home position and a plurality of adjustment positions. | ||||||
| 194 | Light for an aircraft | US13475127 | 2012-05-18 | US08740424B2 | 2014-06-03 | Andre Hessling; Enrico Beier |
| A light for an aircraft comprises a holder for carrying a plurality of light emitting diodes arranged along a curvilinear line and a first optical unit comprising an elliptic reflective partial surface defining a plurality of focal points forming a first curvilinear focal line extending along the light emitting sites of the light emitting diodes, and a plurality of second focal points. The light further includes a second optical unit comprising a single further focal point or a plurality of further focal points forming a further curvilinear focal line. The plurality of the second focal points of the first optical unit coincide and are identical to the single further focal point of the second optical unit or are located along the further curvilinear focal line of the second optical unit. | ||||||
| 195 | Reading lamp | US12586251 | 2009-09-17 | US08687977B2 | 2014-04-01 | Wolfgang Niehoff |
| There is provided a reading lamp having a lighting unit (BE) which has at least first light emitting diodes (LEDs) and/or second light emitting diodes (IR-LEDs) for the emission of IR radiation. The reading lamp further has a modulation unit (ME) for modulation of the light emission of the first and/or second light emitting diodes in dependence on an input signal (IN). | ||||||
| 196 | INDIVIDUAL LIGHTING DEVICE FOR A VEHICLE SEAT | US13923074 | 2013-06-20 | US20130343072A1 | 2013-12-26 | Charles EHRMANN; Philippe ROY; Pascal GORDIET |
| The invention relates to an individual lighting device (20) for a vehicle seat including: a plurality of light sources (S1, S2, S3) having an adjustable light intensity and each emitting in a favored direction (D1, D2, D3), at least two sources being arranged so that the directions (D1, D2, D3) of those two sources are not parallel. | ||||||
| 197 | Lighting apparatus, especially a reading lamp | US13252313 | 2011-10-04 | US08602614B2 | 2013-12-10 | Bernd Schultheis; Achim Weil; Andreas Dietrich; Dirk Vogel |
| The lighting apparatus, especially a reading lamp, has a light source (48), a movable cover (24) to which the light source (48) is fastened, an adjusting element (21) that cooperates with the cover (24), a bearing unit (26) for supporting the cover (24) and an adjusting ring (21). The cover (24) and light source (48) are movable around a longitudinal axis (L) of the lighting apparatus (10) by actuating the adjusting element (21) and the cover (24) and light source (48) are moveable around a transverse axis (Q) extending perpendicular to the longitudinal axis (L) by actuating the cover (24). The lighting apparatus in the form of the reading lamp is particularly useful aboard aircraft, ships, trains, automobiles, or other vehicles. | ||||||
| 198 | PASSENGER SERVICE SYSTEM WITH IMPROVED AIR GUIDANCE | US13868692 | 2013-04-23 | US20130286673A1 | 2013-10-31 | Sebastian UMLAUFT; Robert Thomas |
| A passenger service system includes an individual ventilation arrangement and/or a lighting arrangement, wherein at least one air nozzle of the individual ventilation arrangement and/or at least one reading lamp of the lighting arrangement is/are disposed in the region of a service surface of the passenger service system, The service surface of the passenger service system includes a substantially flat portion as well as a buckled portion, which is curved convexly relative to the substantially flat portion and extends along a longitudinal axis (LP) of the passenger service system. | ||||||
| 199 | Device for supplying loads in the overhead area of a passenger cabin, in particular in commercial aircraft | US13179794 | 2011-07-11 | US08500065B2 | 2013-08-06 | Frank Schmid; Marc Renz; Norbert Knopp; Juergen Grabmann; Dietmar Voelkle; Markus Klingseis; Wolf-Dieter Kuhnla |
| Corresponding to reducing the number of components that need to be separately installed, in addition to a weight reduction and a reduction in the cable loom volume, improved system reliability is obtained if the loads relating to a seating space in a passenger cabin (12), in particular in an aircraft, are combined on an overhead panel (17) which is connected, via line connections which are now only short, to a spatially associated supply module (19), which is operated in cutouts (20) in a stub frame (13), in order to anchor a hat rack (11) in the fuselage structure (16) of the cabin (12). | ||||||
| 200 | Supply unit for flexible supply channels | US13130433 | 2009-10-26 | US08474755B2 | 2013-07-02 | Uwe Schneider |
| According to one exemplary embodiment of the invention, a service unit for being installed on a service channel of an aircraft is disclosed, wherein said service unit features a mounting device and a connecting device. These two devices cooperate in such a way that the mounting and the automatic connecting are realized in one step when the service unit is moved into the installation position. | ||||||
QQ群二维码
意见反馈
意见反馈