WO2011077366A1 - Améliorations relatives à des sièges de passagers de véhicule - Google Patents

Améliorations relatives à des sièges de passagers de véhicule Download PDF

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Publication number
WO2011077366A1
WO2011077366A1 PCT/IB2010/055971 IB2010055971W WO2011077366A1 WO 2011077366 A1 WO2011077366 A1 WO 2011077366A1 IB 2010055971 W IB2010055971 W IB 2010055971W WO 2011077366 A1 WO2011077366 A1 WO 2011077366A1
Authority
WO
WIPO (PCT)
Prior art keywords
seats
seat
seating
row
seating arrangement
Prior art date
Application number
PCT/IB2010/055971
Other languages
English (en)
Inventor
Jurgen Brand
David Moodie
Gavin Edward Balasingam
Original Assignee
Air New Zealand Limited
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 AU2009906177A external-priority patent/AU2009906177A0/en
Application filed by Air New Zealand Limited filed Critical Air New Zealand Limited
Publication of WO2011077366A1 publication Critical patent/WO2011077366A1/fr

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B61—RAILWAYS
    • B61D—BODY DETAILS OR KINDS OF RAILWAY VEHICLES
    • B61D1/00—Carriages for ordinary railway passenger traffic
    • B61D1/04—General arrangements of seats
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B61—RAILWAYS
    • B61D—BODY DETAILS OR KINDS OF RAILWAY VEHICLES
    • B61D33/00—Seats
    • 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
    • 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
    • B64D11/0601—Arrangement of seats for non-standard seating layouts, e.g. seats staggered horizontally or vertically, arranged in an angled or fishbone layout, or facing in other directions than the direction of flight
    • 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
    • B64D11/0639—Arrangements of seats, or adaptations or details specially adapted for aircraft seats with features for adjustment or converting of seats
    • B64D11/0644—Adjustable arm rests

Definitions

  • the present invention relates to a seating arrangement and seating configurations in or for a passenger vehicle.
  • the present invention relates to seating arrangement and/ or seating configurations for a passenger aircraft.
  • the present invention may be said to be a seating arrangement in a passenger vehicle said arrangement comprising:
  • each row of seats having at least three juxtaposed seats and each seat including a seat pan and a seat back,
  • all seats in the second row of seats are facing in substantially a second direction opposite to the first direction and configured such that the outermost seats at each end of the second row are angled to face at least in part toward each other, wherein the first and second rows of seats face each other and are spaced apart from each other.
  • angles of the outermost seats of the first and/ or the second row of seats is such that the angle of intersect of the facing direction of the two outermost seats in a row is between 5 and 35 degrees.
  • the intermediate seat or seats in a row are facing parallel or perpendicular to the direction of travel of the vehicle.
  • an arm rest is provided positioned intermediate of each seat.
  • the arm rest can be moved between a stowed condition and a deployed condition.
  • the arm rest can move in a rectilinear manner between the stowed condition and the deployed condition.
  • Preferably outward of at least one of the two outermost seats of a row is a side panel.
  • the side panel includes an arm rest for the occupier of the outermost seat next to the side panel to use.
  • a partition wall is held by the side panel that can move relative the side panel between a stowed condition and an extended condition, the extended condition positioning the panel at least in part to extend beyond the front end of the seat pan of the seat immediately adjacent.
  • the partition wall in the extended condition bridges the gap between the first and second row of seats thereby creating a barrier that at least in part restricts ingress or egress of a passenger into the seats from the side of the seats where the partition wall is positioned.
  • the partition wall includes a table that can be moved from a stowed condition to be presented for use by at least one person occupying the seat immediately adjacent the side panel.
  • the table is configured to allow it to be used by any person occupying a seat in the seating arrangement.
  • the table can be extended to be presented for use by any person occupying a seat in the seating arrangement.
  • the table can be configured to in combination with the seat pan of at least one seat, form a substantially horizontal surface suitable for supporting a person.
  • the table is configured to at least in part occupy the space between the first and second row of seats such that the table surface in combination with the surface of the seat pan's of at least one seat from each of the first and second row of seats forms a support surface for a substantially prostrate person.
  • the vehicle is a passenger aircraft.
  • a platform can be established that together with the seat pans of the two opposed seats can form a bed or recliner.
  • the present invention may be said to be a seating arrangement for a passenger vehicle said arrangement comprising:
  • each seat comprising a seat pan and a seat back
  • outward of at least one of the two distal end seats is a side panel, and wherein a partition wall is held by the side panel that can move relative the side panel between a stored condition and an extended condition, the extended condition positioning the panel to extend beyond the front end of the seat pan of the seat immediately adjacent.
  • an arm rest is provided positioned intermediate of each seat.
  • the arm rest can be moved between a stowed condition and a deployed condition.
  • the arm rest can move in a rectilinear manner between the stowed condition and the deployed condition.
  • the side panel includes an arm rest for the occupier of a distal end seat to use.
  • the partition wall includes a table that can be moved from a stowed condition to be presented for use by at least one person occupying the seat immediately adjacent the side panel.
  • the table is configured to allow it to be used by any person occupying a seat in the seating arrangement.
  • the table can be extended to be presented for use by any person occupying a seat in the seating arrangement.
  • the vehicle is a passenger aircraft.
  • outward of at least one of the two distal end seats is a side panel.
  • a partition wall is held by the side panel that can move relative the side panel between a stored condition and an extended condition, the extended condition positioning the panel to extend beyond the front end of the seat pan of the seat immediately adjacent and past the front end of the seat pan of the seat of the opposite arrangement.
  • the partition wall may include a table that can be moved from a stowed condition to be presented for use by at least one person occupying the seat immediately adjacent the side panel and at least one person occupying corresponding opposite seat of the other seat arrangement.
  • the table is configured to allow it to be used by any person occupying a seat in either of the seating arrangement.
  • the table can be extended to be presented for use by any person occupying a seat in either of the seating arrangements.
  • the seating configuration creates an alcove.
  • one side of the alcove is accessible from an aisle of the vehicle.
  • the other side of the alcove is accessible from an aisle of the vehicle.
  • the other side is positioned adjacent a side of the vehicle.
  • a platform can be established that together with the seat pans of the two opposed seats can form a bed or recliner.
  • the present invention may be said to be an aircraft that includes a seating arrangement or configuration as herein previously described.
  • the present invention may be said to be a seating arrangement for a passenger vehicle said arrangement comprising:
  • each row of seats having at least two juxtaposed seats and each seat including a seat pan and a seat back,
  • all seats in the second row of seats are facing in substantially a second direction opposite to the first direction and configured such that the outermost seats at each end of the second row are angled to face at least in part toward each other, wherein the first and second rows of seats face each other and are spaced apart from each other,
  • the table can be configured to in combination with the seat pan of at least one seat, form a substantially horizontal surface suitable for supporting a person.
  • the table is configured to at least in part occupy the space between the first and second row of seats such that the table surface in combination with the surface of the seat pan's of at least one seat from each of the first and second row of seats forms a support surface for a substantially prostrate person.
  • the present invention may be said to be a seating arrangement as claimed herein with reference to any one or more of the accompanying drawings.
  • This invention may also be said to consist in the parts, elements and features referred to or indicated in the specification of the application, individually or collectively, and any or all combinations of any two or more of said parts, elements or features, and where specific integers are mentioned herein which have known equivalents in the art to which this invention relates, such known equivalents are deemed to be incorporated herein as if individually set forth.
  • the present invention consists in an aircraft that includes a seating configuration as herein described.
  • the present invention consists in an aircraft that includes a plurality of seating configurations as herein described positioned in a row formation wherein the back rests of two adjacent configurations are positioned back to back.
  • the present invention consist in a seating arrangement as herein described and with reference to the accompanying drawings. In a further aspect the present invention consist in a seating arrangement as shown in the accompanying drawings.
  • Figure 1 illustrates a seating configuration consisting of two seat arrangements each comprising of 3 seats
  • Figure 2 is a plan view of the seating configuration of Figure 1 ,
  • Figure 3 is a front view of one of the seating arrangements of Figure 1,
  • Figure 4 is a side view of Figure 1 .
  • Figure 5 is a side view of a seating arrangement
  • Figure 6 is a cutaway perspective view illustrating a plurality of seating arrangements in pairs defining a preferred seating configuration within the body of an aircraft
  • Figure 7 is a front view of that of Figure 6,
  • Figure 8 is a perspective view of a seating configuration consisting of two seating arrangements
  • Figure 9 is an alternative perspective view of a seating configuration consisting of two seating arrangements.
  • Figure 10 is a perspective view of an aircraft.
  • each seating arrangement includes 3 seats, 4, 5, 6, as shown with reference to the seating arrangement 3.
  • Each seat is of a size and shape to allow for a passenger to be sedentary in at least an upright condition and preferably also in a partially reclined condition.
  • Figure 5 shows a side view of a seat wherein the seat is shown in profile, in both an upright condition and a partially reclined condition.
  • the seating arrangement is mounted within an aircraft 999 to provide a variety of seating and accommodation for passengers. It will be appreciated that whilst the preferred embodiment of the seating arrangement is mounted within an aircraft, the seating arrangement could be mounted in any other vehicle such as a cruise ship, train or bus.
  • the seating arrangement could be mounted in any other vehicle such as a cruise ship, train or bus.
  • Intermediate of each of the seats is preferably an arm rest 7, 8.
  • Each arm rest can preferably be held in a stored condition wherein it does not substantially interfere with a cross seat direction of the seating arrangement 3.
  • each arm rest 7, 8 moves rectilinear between the stored condition as shown in Figure 1, 2 and in used condition where an arm rest surface is more elevated than in the stored condition.
  • each of the seats 4, 5, 6 are in close juxtaposition relative to each other. They preferably form a seat unit.
  • each seat effectively defines part of a single bench seat of the seating arrangement 3. This can allow for a passenger to recline across at least 2 of the seats of the arrangement as shown in Figure 1.
  • the arm rest may move in a rotational manner between its stored condition where it may be located within a space between the seat backs of each of the seats and in use condition extending substantially horizontally.
  • each seating arrangement 2, 3 of a seating configuration consists of 3 seats.
  • each seating arrangement may only include 2 seats.
  • each seating arrangement will have two distal end most seats.
  • the seating arrangement 3 has distal end most seats 4, 6 with a seat 5 intermediate thereof.
  • the design of the seat arrangement (whether it is in a configuration as shown in Figure 1 or whether the seating arrangement does not have a corresponding seating arrangement facing it and providing an alcove like arrangement) has the distal end most seats designed, with a bias inwardly.
  • the bias may be as a result of a slight flaring forward of the back rest at the peripheral edges of the distal end most seats.
  • the wings 10, 11 may project in a forward direction (relative to the seating arrangement 3) so as to create a feeling of enclosure encouraging those passengers sitting in the distal end most seats to have a bias towards facing each other.
  • the intermediate seat 5 has a face direction that is non- parallel to the slight biased faced direction of the distal end most seats. This bias induced on passengers by the distal end most seats may also be encouraged as a result of the free end 20 of the seat pans of the distal end most seats being generally non- perpendicular or non-symmetrical and effectively non-perpendicular to the facing direction of the intermediate seat 5 as shown in Figure 2.
  • each seating arrangement 2 or 3 is positioned proximate another seating arrangement.
  • the pair of seating arrangements are position to define a seating configuration 1 where in the seating arrangements face each other. That is, the seat directions are substantially parallel and in opposing directions to each other.
  • the space between the facing seating arrangement of a seating configuration is sufficient to allow for a person to walk between the 2 seating
  • a platform 35 may span between the 2 seating arrangements 2, 3 to cooperate with one or each of the seats in a seating arrangement and the corresponding opposite seats of the opposite seating arrangement to define a bed or recline surface.
  • the platform 35 can be positioned at a level commensurate with the height of the seat pans of the seats of the seating arrangements.
  • the platform 35 may be supported by part of the seating arrangements or by an alternative structure.
  • Adjacent 1 or both of the distal end most seats of a seating arrangement is a side wall 40.
  • the side wall 40 includes an arm rest surface 41.
  • the side wall 40 defines a side wall to the seating arrangement or partial side wall to the seating arrangement and also encourages passengers in a manner to facilitate their interaction.
  • the side wall 40 may include a cavity 42.
  • the cavity 42 may include a partition 43.
  • the partition may be movably located in the cavity 42 to move between a stored condition where it is substantially concealed within the cavity and an extended position where it extends across at least part of the entrance to the alcove defined between the 2 seating arrangements.
  • the partition 43 when in the extended position extends beyond the free end of the seat pan of the seat adjacent the end wall 40 is in a forward direction therefrom.
  • the partition 43 can extend all the way to an opposite end wall of an opposite seating arrangement of the seating configuration. That way the alcove, at that end of the seating configuration can be closed.
  • a like partition wall 43 may be provided at the opposite end of the seating configuration to also enclose that entrance to the alcove.
  • the opposite end of the alcove may sit against the side of the aircraft body and therefore be closed by the aircraft body. Carried by the partition 43 may also be a tray table as shown in Figure 8.
  • the tray table 44 may be movably configured in a manner so as to extend in a substantially horizontal condition as shown in Figure 8 for use at least by those passengers in the distal end seat proximate most the partition wall 43 but preferably also by the other passengers sitting in the other seats.
  • the tray table 44 may be hingeably engaged so as to fold between a horizontal condition and a vertical condition. In the vertical condition it may also end up being capable of storage within the cavity 42 of a side wall of a seating arrangement.
  • tray table 44 may be stored in the side wall of 1 of the seating
  • partition wall 43 may be stored in a side wall of the opposite seating arrangement.
  • the tray table 44 may also be configured and positioned for use as the platform

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Transportation (AREA)
  • Seats For Vehicles (AREA)

Abstract

L'invention porte sur un agencement de sièges pour véhicule à passagers, l'agencement comprenant au moins deux sièges juxtaposés tournés dans la même direction, les sièges d'extrémité distale étant tournés face à face. Les sièges d'extrémité distale ont également un panneau latéral portant une paroi de séparation pouvant s'étendre au-delà de l'avant de la cuvette du siège adjacent pour former une barrière ou un écran qui empêche l'accès depuis l'aile à la zone située à l'avant des sièges. Cet agencement de sièges peut aussi comprendre deux rangées de sièges opposés, dont les cuvettes de siège peuvent être combinées à la table/plateforme située entre les rangées des sièges pour former un lit.
PCT/IB2010/055971 2009-12-21 2010-12-21 Améliorations relatives à des sièges de passagers de véhicule WO2011077366A1 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
AU2009906177A AU2009906177A0 (en) 2009-12-21 Improvements Relating To Passenger Vehicle Seating
AU2009906177 2009-12-21

Publications (1)

Publication Number Publication Date
WO2011077366A1 true WO2011077366A1 (fr) 2011-06-30

Family

ID=44195021

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/IB2010/055971 WO2011077366A1 (fr) 2009-12-21 2010-12-21 Améliorations relatives à des sièges de passagers de véhicule

Country Status (1)

Country Link
WO (1) WO2011077366A1 (fr)

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2899125A1 (fr) * 2014-01-28 2015-07-29 Airbus Defence and Space GmbH Agencement de siège, cabine d'avion et accoudoir et siège ou groupe de sièges destiné à être utilisé pour celui-ci
EP3348479A1 (fr) * 2017-01-12 2018-07-18 Bell Helicopter Textron Inc. Configurations de siège d'avion flexible
US10625866B2 (en) 2017-01-12 2020-04-21 Bell Helicopter Textron Inc. Flexible foldover seat configurations for emergency egress of aircraft
WO2020112659A1 (fr) * 2018-11-29 2020-06-04 Safran Seats Usa Llc Sièges de classe affaires pour un véhicule de transport de passagers
US10926861B2 (en) 2018-06-04 2021-02-23 Textron Innovations Inc. Puck cover
US10933969B2 (en) 2017-01-12 2021-03-02 Bell Helicopter Textron Inc. Puck attachment mechanism for flexible aircraft configuration
JP2021094354A (ja) * 2019-12-19 2021-06-24 ヤマハ発動機株式会社 車両

Citations (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4936620A (en) * 1983-05-16 1990-06-26 S.A. Seatco N.V. Arrangement or organization of seats inside the passenger area of vehicle
FR2671530A1 (fr) * 1991-01-16 1992-07-17 Minhonnac Hubert Siege, pour vehicule de chemin de fer, orientable indifferemment dans le sens de la marche du train ou dans le sens inverse.
JPH1120680A (ja) * 1997-07-04 1999-01-26 Koito Ind Ltd 座席装置
WO2001030639A1 (fr) * 1999-10-22 2001-05-03 Mack Trucks, Inc. Compartiment de couchage modulaire pour camions
WO2005080196A1 (fr) * 2004-02-20 2005-09-01 Leadearn Investments Limited Soute d'aeronef
US7108226B2 (en) * 2003-10-10 2006-09-19 The Boeing Company Interior seating architecture for aircraft
US7185849B2 (en) * 2001-08-09 2007-03-06 Virgin Atlantic Airways Limited Passenger accommodation cabin for a vehicle
US7399031B2 (en) * 2005-10-11 2008-07-15 R-N-R International, Inc. Dinette having a collapsible table assembly
WO2009009005A1 (fr) * 2007-07-09 2009-01-15 Gerald Bosstick Lit formé de fauteuils en vis-à-vis
US7578470B2 (en) * 2006-04-21 2009-08-25 Be Aerospace, Inc. Passenger seating arrangement

Patent Citations (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4936620A (en) * 1983-05-16 1990-06-26 S.A. Seatco N.V. Arrangement or organization of seats inside the passenger area of vehicle
FR2671530A1 (fr) * 1991-01-16 1992-07-17 Minhonnac Hubert Siege, pour vehicule de chemin de fer, orientable indifferemment dans le sens de la marche du train ou dans le sens inverse.
JPH1120680A (ja) * 1997-07-04 1999-01-26 Koito Ind Ltd 座席装置
WO2001030639A1 (fr) * 1999-10-22 2001-05-03 Mack Trucks, Inc. Compartiment de couchage modulaire pour camions
US7185849B2 (en) * 2001-08-09 2007-03-06 Virgin Atlantic Airways Limited Passenger accommodation cabin for a vehicle
US7108226B2 (en) * 2003-10-10 2006-09-19 The Boeing Company Interior seating architecture for aircraft
WO2005080196A1 (fr) * 2004-02-20 2005-09-01 Leadearn Investments Limited Soute d'aeronef
US7399031B2 (en) * 2005-10-11 2008-07-15 R-N-R International, Inc. Dinette having a collapsible table assembly
US7578470B2 (en) * 2006-04-21 2009-08-25 Be Aerospace, Inc. Passenger seating arrangement
WO2009009005A1 (fr) * 2007-07-09 2009-01-15 Gerald Bosstick Lit formé de fauteuils en vis-à-vis

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2899125A1 (fr) * 2014-01-28 2015-07-29 Airbus Defence and Space GmbH Agencement de siège, cabine d'avion et accoudoir et siège ou groupe de sièges destiné à être utilisé pour celui-ci
EP3348479A1 (fr) * 2017-01-12 2018-07-18 Bell Helicopter Textron Inc. Configurations de siège d'avion flexible
US10604262B2 (en) 2017-01-12 2020-03-31 Bell Helicopter Textron Inc. Flexible aircraft seat configurations
US10625866B2 (en) 2017-01-12 2020-04-21 Bell Helicopter Textron Inc. Flexible foldover seat configurations for emergency egress of aircraft
US10933969B2 (en) 2017-01-12 2021-03-02 Bell Helicopter Textron Inc. Puck attachment mechanism for flexible aircraft configuration
US11155353B2 (en) 2017-01-12 2021-10-26 Textron Innovations Inc. Flexible aircraft seat configurations
US10926861B2 (en) 2018-06-04 2021-02-23 Textron Innovations Inc. Puck cover
WO2020112659A1 (fr) * 2018-11-29 2020-06-04 Safran Seats Usa Llc Sièges de classe affaires pour un véhicule de transport de passagers
US11702207B2 (en) 2018-11-29 2023-07-18 Safran Seats Usa Llc Business class seats for a passenger vehicle
JP2021094354A (ja) * 2019-12-19 2021-06-24 ヤマハ発動機株式会社 車両
JP7382819B2 (ja) 2019-12-19 2023-11-17 ヤマハ発動機株式会社 車両

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