WO2004026688A1 - Support pour dispositifs de divertissement et dispositifs electroniques personnels, monte sur les rails porte-sieges d'un avion - Google Patents

Support pour dispositifs de divertissement et dispositifs electroniques personnels, monte sur les rails porte-sieges d'un avion Download PDF

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Publication number
WO2004026688A1
WO2004026688A1 PCT/CA2003/001455 CA0301455W WO2004026688A1 WO 2004026688 A1 WO2004026688 A1 WO 2004026688A1 CA 0301455 W CA0301455 W CA 0301455W WO 2004026688 A1 WO2004026688 A1 WO 2004026688A1
Authority
WO
WIPO (PCT)
Prior art keywords
arm
support according
post
support
base
Prior art date
Application number
PCT/CA2003/001455
Other languages
English (en)
Inventor
George R. Smallhorn
Original Assignee
Inflight Canada Inc.
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 claimed from US10/247,304 external-priority patent/US6863344B2/en
Priority claimed from CA002404584A external-priority patent/CA2404584A1/fr
Application filed by Inflight Canada Inc. filed Critical Inflight Canada Inc.
Priority to AU2003269648A priority Critical patent/AU2003269648A1/en
Priority to CA002538000A priority patent/CA2538000C/fr
Publication of WO2004026688A1 publication Critical patent/WO2004026688A1/fr

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D11/00—Passenger or crew accommodation; Flight-deck installations not otherwise provided for
    • B64D11/0015—Arrangements for entertainment or communications, e.g. radio, television
    • B64D11/00155—Individual entertainment or communication system remote controls therefor, located in or connected to seat components, e.g. to seat back or arm rest
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D11/00—Passenger or crew accommodation; Flight-deck installations not otherwise provided for
    • B64D11/0015—Arrangements for entertainment or communications, e.g. radio, television
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D11/00—Passenger or crew accommodation; Flight-deck installations not otherwise provided for
    • B64D11/06—Arrangements of seats, or adaptations or details specially adapted for aircraft seats
    • B64D11/0624—Arrangements of electrical connectors, e.g. for earphone, internet or electric supply
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D11/00—Passenger or crew accommodation; Flight-deck installations not otherwise provided for
    • B64D11/06—Arrangements of seats, or adaptations or details specially adapted for aircraft seats
    • B64D11/0627—Seats combined with storage means
    • B64D11/0629—Seats combined with storage means the storage means being specially adapted for emergency equipment
    • B64D11/0631—Seats combined with storage means the storage means being specially adapted for emergency equipment for life vests
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D11/00—Passenger or crew accommodation; Flight-deck installations not otherwise provided for
    • B64D11/06—Arrangements of seats, or adaptations or details specially adapted for aircraft seats
    • B64D11/0638—Arrangements of seats, or adaptations or details specially adapted for aircraft seats with foldable tables, trays or cup holders
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D11/00—Passenger or crew accommodation; Flight-deck installations not otherwise provided for
    • B64D11/06—Arrangements of seats, or adaptations or details specially adapted for aircraft seats
    • B64D11/0696—Means for fastening seats to floors, e.g. to floor rails
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/40—Weight reduction

Definitions

  • the invention relates to an easily installed and removed support for personal electronic devices for passenger use in an aircraft cabin mounted to the cabin floor, mounted within the seat tracks in the cabin floor and stowed away under the passenger seat or in a free standing pedestal.
  • Aircraft passenger cabins are currently constructed or are being retrofit with a wide assortment of personal electronic devices with entertainment options accessible from the passenger seat.
  • airlines may provide audio and video entertainment, telephone, intercom, television, video games, internet, email and electrical power supply for laptop computers, especially in business class and first class cabins thus permitting passengers to work during the flight, to communicate or to be entertained without leaving their seat or disturbing other passengers.
  • Passenger entertainment systems such as seat mounted flat screen video monitors, and credit card activated cellular telephones are now commonly mounted in the seat backs and seat arm rests of passenger aircraft.
  • Some airlines also distribute compact personal DVD players with a choice of movies, or personal audio CD players in first class and business class cabins. Passengers may carry their own laptop computers or CD players and seek power outlets to preserve batteries and extend use during long flights .
  • passenger seat units are often fitted with power sources, entertainment and personal electronic system units that are mounted in armrests, in consoles, in the seat back or under the seat as an interim measure.
  • the invention provides a support for equipment associated with a passenger seat assembly mounted to a floor in a passenger cabin.
  • the support having a base adapted to anchor to two seat tracks in the cabin floor with a post extending upwardly from the base.
  • Individual support arms each have a proximal end mounted to the base and a distal end with an equipment mount.
  • Each arm has independent deployment transferring the associated arm from a stowed position to a deployed position extending upwardly from the post.
  • the arm can be stowed under an associated passenger seat or in a free-standing pedestal for example.
  • a significant benefit of the invention is that existing seats or existing seat designs need not be changed in order to accommodate newly added services, such as personal video entertainment, laptop computer power, virtual reality video games, email, internet capacity or other such entertainment and personal electronic services complete with keyboards, control pads, display screens and media drives within the very restricted confines of the immediate passenger airline seat area.
  • the invention provides a completely independent stand alone support that is independently supported within the seat tracks of the cabin floor to support various devices such as flat screen video monitors or DVD players as well as accommodating power source cables and receptacles in a compact stow-able unit that stows under the seat or in a pedestal.
  • the invention provides an independent stand-alone support unit for electrical components, which can be modified to support any such entertainment or personal electronic device.
  • a further advantage of the invention is the flexibility of design that aircraft operators can achieve through complete separation of the seating function and the entertainment or personal electronic function within the cabin. More particularly, the seats can be designed for maximum safety, service life and passenger comfort without premature replacement. Seats can be used throughout their entire functional operating life without considering upgrades or modification to accommodate changes to the entertainment or personal electronic systems.
  • the seat function of comfort and safety may be segregated from the entertainment and personal electronic systems provided by the independent support according to the invention. Audio and video signals can be conveyed to the independent support that houses video displays for example and includes receptacles or jacks for headphones completely independently of the seat.
  • the airline operator can quickly reconfigure the cabin (for charters, long haul or short commuter flights) , adding or removing entertainment or personal electronic services by simply installing or removing the independent support unit. Seats need not be modified at all since the support for entertainment and personal electronic systems is independently installed and removed from the cabin floor seat tracks.
  • the invention provides a simple solution enabling retrofitting of existing aircraft or reconfiguring of aircraft with a rapid turn around. For example, entertainment and personal electronic devices are usually more desirable on long haul flights while use of the same aircraft for commuter flights places a premium on cabin space and number of passengers per aircraft.
  • Reconfiguration to provide such services is relatively simple when the invention is used since the independent supports may be installed and removed very quickly to reconfigure the aircraft, whereas conventional reconfiguration involves removing and replacing the entire seat assembly.
  • Figure 1 shows a front perspective view of a three passenger seat assembly with a first "economy class" embodiment of the invention provided spanning between the two seat tracks with an equipment supporting arm extending upwardly on three arms that can be individually folded and rotated downwardly in a stowed position under the seats.
  • Figure 2 is a side elevation view of two passenger seats with supports as shown in Fig. 1, showing in the right side seat the under seat stowed position, the deployed position and the upwardly telescoped deployed position.
  • Figure 3 is a detail sectional view along line 3-3 of Figure 2.
  • Figure 4 is a detail sectional view along line 4-4 of Figure 2.
  • Figure 5 shows an elevation view of a second "first class or business class" embodiment of the invention with a two passenger seat assembly with conventional tray table located at lap height and provided between the two seats an equipment supporting table extending upwardly and laterally on two articulated arms that can be individually folded downwardly in a stowed position within pockets in the support post.
  • Figure 6 is a side elevation view of the arrangement shown in Figure 5.
  • Figure 7 is a top plan view thereof.
  • Figure 8 is a detail view of the table showing the ability to pivot in a horizontal plane and showing four table leaves slidably disposed in the side edges of the table to extend the support surface.
  • Figure 9 is a plan view of a passenger cabin of an aircraft showing six parallel seat supporting tracks that extend longitudinally for connecting seat legs and showing an adapter plate mounted to the seat tracks which is also bolted to the base of the equipment support between the two seats of each two seat assembly.
  • Figure 10 is a front elevation view of the arrangement shown in Figure 9 indicating the location of seat tracks that anchor three pairs of passenger seats to the cabin floor structure.
  • Figure 11 is a detailed frontal view of a support according to the invention showing the base with a life vest storage compartment and two articulated arms with equipment support tables in the stowed position.
  • Figure 12 is a side elevation view of the stowed position shown in Figure 11.
  • Figure 13 is a detailed view of the articulated arms in a stowed position.
  • Figure 14 is a plan view of the equipment support table with extension leaves shown in the extended position.
  • Figure 15 is an exploded elevation view of the equipment support table of Figure 14.
  • Figure 16 is a partial sectional elevation view showing housing of an electrical power source within the base of the support and showing the cable raceway extending cable from the power source to a receptacle in the top portion of the post.
  • Figure 17 is a frontal elevation view of the support with front compartment door removed to show mounting for the power source and storage compartment for the life vests as well showing a spring loaded latch to retain the articulated arms in the stowed position.
  • Figure 18 is a side view of the detail shown in Figure 17.
  • Figure 19 is a sectional view along lines 19-19 of Figure 17.
  • Figure 20 is a top plan view of the spring loaded latch that detains the articulated arms in the stowed position.
  • Figure 21 is a detailed elevation view of the latch.
  • a support 1 for personal electronic devices 2 is shown mounted to seat tracks 3 independently of the associated seat assembly 4.
  • the seat assembly 4 has three passenger seats 5 on a common base with seat legs 6 mounted to the seat tracks 3 in a conventional manner. Two to five or more seats 5 can be accommodated in a like manner.
  • the support 1 Completely independently of the seat assembly 4 and mounting of the seat legs 6 in the seat track 3 is the support 1 which includes a base 7 adapted to anchor to the two seat tracks 3 in the cabin flour of the aircraft cabin.
  • the base 7 includes two mounting brackets 8 each adapted to engage the associated parallel seat track 3.
  • Extending upwardly from the mounting bracket 8 of the base 7 is a post 9.
  • a beam 10 expands between the upward end of each post 9 and rotatably supports three arms 11.
  • Each arm 11 can be independently deployed from the stowed position shown on the left of Figure 1 (under the associated passenger seat 5 and to a deployed position extending upwardly from the post 9.
  • the base 7 is adapted for disposition between the seat legs 6, however depending on the orientation of seat legs 6, the base 7 may be positioned anywhere along the seat track 3.
  • the arm 11 may include a telescoping portion to raise and lower the equipment mount 12 and attached personal electronic device 2 as indicated in arrows on the right side of Figure 1. Further, the equipment mount 12 is rotatably connected at pivot joint 13 to a distal end of the arm 11 so that the personal electronic device 2 can be flipped downwardly as indicated in the left portion of Figure 1 and then rotated about the lower end of the arm 11 on beam 10 to an under seat stowed position.
  • the arm 11 is hollow or includes a cable raceway enclosing cables extending between the base 7 and a top portion of the arm 11.
  • the beam 10 may also be hollow and include a cable raceway. Any wires and cables can extend under the cabin floor or under the carpet in cable raceways within the floor through mounting bracket and up post 9 through the beam 10 and into arms 11.
  • the arms 11 can include a receptacle in communication with cables for providing auxiliary power, headphones jacks or other types of receptacles and consoles.
  • Figure 2 shows a side view- illustrating clearly the independent mounting of the support 1 in the seat tracks 3 separate from the mounting of the seats 4 in the same seat tracks 3.
  • Figures 3 and 4 show details of the base 7 for mounting in the seat track 3, where the base 7 includes two gusset plates 14 and four mounting struts 15.
  • the second "first class or business class" embodiment of the invention provides a pedestal support 16 for equipment such as entertainment and personal electronic devices that are associated with a passenger seat 17 mounted to the floor 18 in the passenger cabin.
  • conventional passenger seats 17 include arm rests 19 that may conventionally have hinged compartment doors in their top surface to house foldable articulated arms with flat screen video displays.
  • Most armrests also conventionally include jacks for head phones to access the aircraft audio system as well as other personal electronic devices to page a cabin attendant, light switches etc. built in to conventional passenger seats 17.
  • the invention however provides a stand alone support 16 that has upwardly extending articulated arms 19 that fold downwardly into a stowed position within the post 21 of the support 16 and optionally include an equipment mount table 22.
  • the embodiment shown includes a flat table 22 as a means to mount entertainment and personal electronic equipment with extension leaves 23 slidably disposed on lateral edges of the table to accommodate a personal DVD player or CD player for example.
  • the invention is not limited to provision of a table 22, but also includes other means to mount various types of equipment such as a flat screen video monitor, LED display or even a 3-D virtual reality helmet for playing video games for example.
  • the base 24 of the support 16 is large enough to house a life vest storage compartment and to house electrical components such as power supply units 37 or other electronic components.
  • the support 16 includes a base 24 anchored to the tracks 27 in the cabin floor 18 with an adapter plate 26.
  • the base 24 is disposed laterally adjacent and forward to the passenger seats 17 that are served by the support 16.
  • each support arm 20 Extending upwardly from the base 24 is a post 21, • 25 which includes two elongate pockets 29 within which the articulated support arms 20 are shown (in Figures 11 and 12) in the stowed position.
  • a proximal end of each support arm 20 is pivotally mounted to a top portion of the post 21 with a T-bracket 30.
  • the distal end of the arm 20 includes the equipment support table 22, which is also shown in the stowed position.
  • FIG 13 shows an improved detailed view of the articulated arms 20-. It can be appreciated that each arm 20 is independently deployable and pivotally mounted to an associated T-bracket 30 to rotate about the shoulder bolt 31.
  • a gas spring 32 resiliently biases the articulated arm 20 to the deployed position (shown in Figure 5) .
  • a lower end 33 of the gas spring 32 is pivotally mounted to the post 21 on a small bracket while the upper end 34 is pivotally connected to the arm 20 at a short distance from the shoulder bolt 31.
  • the gas spring 32 exerts a rotary force to resiliently bias the arm 20 toward the deployed position.
  • each arm 20 has independent deployment means for transferring the associated arm 20 from the stowed position (shown in Figures 11, 12 and 13) housed • within the associated pocket 29 of the post 21 to the deployed position (shown in Figures 1 , 2 and 3) extending upwardly and laterally from the post 21 toward a central portion of the associated seat 17.
  • the post 21 preferably includes a cable raceway 35 housing at least one cable 36 extending between the base 24 and the top portion of the post 21.
  • the base 24 houses an electrical power supply unit 37 held in place with a bracket 38 that is provided with a power receptacle 39 in communication with the cable 36 to provide power for laptop computers for example. Cables from the base 24 to the aircraft services can be hidden beneath the carpet, under the floor or in floor mounted raceways .
  • the pocket 29 also preferably includes a latch 40 for releasably detaining the arm 20 in the stowed position (shown in Figure 11 and 12) .
  • the latch 40 includes a manual button 41 which is spring loaded to the catch position shown in Figure 20 to resiliently detain the arm 20. Depressing the button 41 against the force of spring 42 releases the arm 20 from dog 43. The arm 20 is resiliently biased by the gas spring 32 to the deployed position and when free of the latch 40 rotates upwardly.
  • an equipment support table 22 is constructed of an upper plate 44 and a lower plate 45 which sandwich together the sliding table leaves 23. As well, the table 22 can rotate about a bolt 46 (shown in Figure 8) that rotatably connects the table 22 to the distal end of the articulated arm 20.
  • the arm 20 can telescope longitudinally by means of a carriage 47 with pins 48 and 49 sliding in tracks 50 of a first arm segment 51.
  • Carriage release dog 52 holds the carriage 47 in the stowed position until sufficient rotation occurs about bolt 31 when the latch 10 is released to release the carriage release dog 52. Under the biased force of the gas spring 32, rotation occurs and the arm 20 rotates upwardly about the shoulder bolt 31.
  • the carriage release dog 52 releases the carriage 47 and the carriage 47 can manually slide on pins 48 and 49 in the tracks 50.

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  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Fittings On The Vehicle Exterior For Carrying Loads, And Devices For Holding Or Mounting Articles (AREA)

Abstract

L'invention porte sur un support d'équipements associé à un siège de passager fixé au sol de la cabine d'un avion. Un tel support comporte une base s'ancrant dans les rails porte-sièges, un montant s'étendant de la base vers le haut, et des bras supports individuels dont l'extrémité proximale est fixée à la base, et l'extrémité distale comporte une monture pour des équipements. Chacun de ces bras est mobile indépendamment entre une position repliée sous le siège associé, et une position déployée dans le montant, s'étendant vers le haut à partir du montant.
PCT/CA2003/001455 2002-09-20 2003-09-18 Support pour dispositifs de divertissement et dispositifs electroniques personnels, monte sur les rails porte-sieges d'un avion WO2004026688A1 (fr)

Priority Applications (2)

Application Number Priority Date Filing Date Title
AU2003269648A AU2003269648A1 (en) 2002-09-20 2003-09-18 Support for passenger entertainment and personal electronic devices mounted in aircraft seat tracks
CA002538000A CA2538000C (fr) 2002-09-20 2003-09-18 Support pour dispositifs de divertissement et dispositifs electroniques personnels, monte sur les rails porte-sieges d'un avion

Applications Claiming Priority (4)

Application Number Priority Date Filing Date Title
US10/247,304 US6863344B2 (en) 2002-09-20 2002-09-20 Support for passenger entertainment and personal electronic devices mounted in aircraft seat tracks
US10/247,304 2002-09-20
CA2,404,584 2002-09-23
CA002404584A CA2404584A1 (fr) 2002-09-23 2002-09-23 Dispositif de rangement sous le siege pour appareils electroniques personnels

Publications (1)

Publication Number Publication Date
WO2004026688A1 true WO2004026688A1 (fr) 2004-04-01

Family

ID=32031349

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/CA2003/001455 WO2004026688A1 (fr) 2002-09-20 2003-09-18 Support pour dispositifs de divertissement et dispositifs electroniques personnels, monte sur les rails porte-sieges d'un avion

Country Status (2)

Country Link
AU (1) AU2003269648A1 (fr)
WO (1) WO2004026688A1 (fr)

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7168674B2 (en) * 2004-12-14 2007-01-30 Mcfarlane Daniel S Aircraft seat track repair device
EP1774997A2 (fr) * 2005-09-14 2007-04-18 Aruze Corporation Machine de jeu
DE102006052536A1 (de) * 2006-11-06 2008-05-08 Poggenpohl Möbelwerke GmbH Bestuhlung einer Fahrzeugkabine
DE102007045731A1 (de) * 2007-09-25 2009-07-30 Esg Elektroniksystem- Und Logistik-Gmbh Arbeitsstation zur Integration in ein Luftfahrzeug, insbesondere Helikopter
EP2106141A2 (fr) * 2008-03-25 2009-09-30 Inflight Investments Inc. Système de contrôle d'accès pour services en vol au siège du passager
WO2015154076A1 (fr) * 2014-04-04 2015-10-08 B/E Aerospace, Inc. Ossature d'embase de siège d'avion
US9919803B2 (en) 2014-04-04 2018-03-20 B/E Aerospace, Inc. Aircraft seat base frame
NO344012B1 (en) * 2018-04-13 2019-08-12 Norwegian Special Mission As Portable and foldable aeronautical workstation

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5984415A (en) * 1995-09-14 1999-11-16 Daimlerchrysler Aerospace Airbus Gmbh Passenger service unit especially for a passenger aircraft cabin
DE19901858A1 (de) * 1999-01-19 2000-07-20 Gerhard Mueller Variable Halteanordnung zur Positionierung von Zubehörteilen in insbesondere einem Kraftfahrzeug
US6179263B1 (en) * 1997-10-14 2001-01-30 Rosen Products Llc Stowable support apparatus
US6427957B1 (en) * 2000-07-28 2002-08-06 Rosen Products Llc Stowable support system

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5984415A (en) * 1995-09-14 1999-11-16 Daimlerchrysler Aerospace Airbus Gmbh Passenger service unit especially for a passenger aircraft cabin
US6179263B1 (en) * 1997-10-14 2001-01-30 Rosen Products Llc Stowable support apparatus
DE19901858A1 (de) * 1999-01-19 2000-07-20 Gerhard Mueller Variable Halteanordnung zur Positionierung von Zubehörteilen in insbesondere einem Kraftfahrzeug
US6427957B1 (en) * 2000-07-28 2002-08-06 Rosen Products Llc Stowable support system

Cited By (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7168674B2 (en) * 2004-12-14 2007-01-30 Mcfarlane Daniel S Aircraft seat track repair device
EP1920803A3 (fr) * 2005-09-14 2012-12-19 Universal Entertainment Corporation Machine de jeu
EP1774997A2 (fr) * 2005-09-14 2007-04-18 Aruze Corporation Machine de jeu
EP1920803A2 (fr) * 2005-09-14 2008-05-14 Aruze Corporation Machine de jeu
EP1774997A3 (fr) * 2005-09-14 2007-07-11 Aruze Corporation Machine de jeu
DE102006052536A1 (de) * 2006-11-06 2008-05-08 Poggenpohl Möbelwerke GmbH Bestuhlung einer Fahrzeugkabine
US8342450B2 (en) 2006-11-06 2013-01-01 Airbus Operations Gmbh Seating arrangement of a vehicle compartment
DE102007045731A1 (de) * 2007-09-25 2009-07-30 Esg Elektroniksystem- Und Logistik-Gmbh Arbeitsstation zur Integration in ein Luftfahrzeug, insbesondere Helikopter
EP2106141A3 (fr) * 2008-03-25 2010-01-06 Inflight Investments Inc. Système de contrôle d'accès pour services en vol au siège du passager
EP2106141A2 (fr) * 2008-03-25 2009-09-30 Inflight Investments Inc. Système de contrôle d'accès pour services en vol au siège du passager
WO2015154076A1 (fr) * 2014-04-04 2015-10-08 B/E Aerospace, Inc. Ossature d'embase de siège d'avion
US20150284095A1 (en) * 2014-04-04 2015-10-08 B/E Aerospace, Inc. Aircraft seat base frame
US9573688B2 (en) 2014-04-04 2017-02-21 B/E Aerospace, Inc. Aircraft seat base frame
CN106458326A (zh) * 2014-04-04 2017-02-22 Be航天公司 飞行器座椅基部框架
US9919803B2 (en) 2014-04-04 2018-03-20 B/E Aerospace, Inc. Aircraft seat base frame
NO344012B1 (en) * 2018-04-13 2019-08-12 Norwegian Special Mission As Portable and foldable aeronautical workstation
NO20180508A1 (en) * 2018-04-13 2019-08-12 Norwegian Special Mission As Portable and foldable aeronautical workstation

Also Published As

Publication number Publication date
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