WO2011089558A1 - Agencement de tablette-plateau - Google Patents

Agencement de tablette-plateau Download PDF

Info

Publication number
WO2011089558A1
WO2011089558A1 PCT/IB2011/050249 IB2011050249W WO2011089558A1 WO 2011089558 A1 WO2011089558 A1 WO 2011089558A1 IB 2011050249 W IB2011050249 W IB 2011050249W WO 2011089558 A1 WO2011089558 A1 WO 2011089558A1
Authority
WO
WIPO (PCT)
Prior art keywords
table arrangement
arrangement
tray
fold
passenger
Prior art date
Application number
PCT/IB2011/050249
Other languages
English (en)
Inventor
Glen Wilson Porter
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 AU2010900294A external-priority patent/AU2010900294A0/en
Application filed by Air New Zealand Limited filed Critical Air New Zealand Limited
Publication of WO2011089558A1 publication Critical patent/WO2011089558A1/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
    • B64D11/06—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
    • B60—VEHICLES IN GENERAL
    • B60N—SEATS SPECIALLY ADAPTED FOR VEHICLES; VEHICLE PASSENGER ACCOMMODATION NOT OTHERWISE PROVIDED FOR
    • B60N3/00—Arrangements or adaptations of other passenger fittings, not otherwise provided for
    • B60N3/001—Arrangements or adaptations of other passenger fittings, not otherwise provided for of tables or trays
    • B60N3/002—Arrangements or adaptations of other passenger fittings, not otherwise provided for of tables or trays of trays
    • 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
    • B64D11/0606—Arrangements of seats, or adaptations or details specially adapted for aircraft seats with privacy shells, screens, separators or the like

Definitions

  • the present invention relates to a tray table arrangements and in particular but not solely to tray table arrangements for or of seats of commercial passenger aircraft.
  • Traditional economy class seats have comprised of a seat back that defines a seat facing direction parallel to the longitudinal direction of the aircraft. This presents a surface at the back of the seat that is perpendicular to which a tray table can be conveniently mounted to move between a stowed condition flat against the back rest of the seat and a deployed position substantially extending horizontally and presented for use by a passenger in a seat immediately behind.
  • Seats may also not necessarily face in a direction parallel to the longitudinal direction of the aircraft. This has resulted in a need to incorporate tray table arrangements that lend themselves for convenient and compact stowage as well as deployment for use by passengers.
  • the invention may be said to be a tray table arrangement suitable for use by a passenger sitting in an aircraft seat, said tray table arrangement supportable by a support structure to allow it to be presented for use by said passenger, said tray table arrangement comprising:
  • a table arrangement comprising at least one table top member presenting at least one major face
  • a support member mountable on said support structure, for supporting the table arrangement; wherein the table arrangement is rotatably coupleable to said support structure to move between
  • table arrangement in said deployed condition is rotatable about an axis parallel to the normal of at least one major face of the table top member.
  • the support member is rotatably securable or secured to said support structure to enable rotational movement of said table arrangement.
  • the support member is rotatable about a substantially horizontal axis.
  • the table arrangement when the table arrangement is in its stowed condition, it is conveniently disposed for storage out of the way of the passenger.
  • the table arrangement when the table arrangement is in its deployed position, it presents at least part of said major face as a utility surface for said passenger.
  • the table arrangement when the table arrangement is in its stowed condition, it is disposed at a location distal to said passenger, and when the table arrangement is in its deployed position, it is located relatively more proximal said passenger.
  • the support member is a support arm.
  • the major surface of the table top member is disposed substantially horizontally when the table arrangement is in its deployed condition.
  • the table arrangement is rotatable about a substantially vertical axis when the table arrangement is in its deployed condition.
  • the table arrangement is a bi-fold table arrangement.
  • the table arrangement is a bi-fold table arrangement comprising at least two juxtaposable table top members presenting at least one major face each.
  • At least one or more of the tabletop members is a substantially planar member presenting a pair of opposed major faces.
  • the bi-fold table arrangement is movable between
  • the bi-fold table arrangement is movable between its first mode and second mode in its deployed condition.
  • the table top members of the bi-fold table arrangement are co-planar when bi-fold table arrangement is the second mode.
  • At least one of the table top members presents at least part of one major face as a horizontal utility surface for a passenger.
  • the bi-fold table arrangement is rotatable about an axis normal to at least one major face of the table top members when the bi-fold table arrangement is in its deployed condition.
  • the bi-fold table arrangement is rotatable about a substantially vertical axis when the bi-fold table arrangement is in its deployed condition.
  • the bi-fold table arrangement is rotatable about a substantially vertical axis when in its first mode or second mode.
  • the support structure is a seat located in front of the seat in which a passenger may sit.
  • the support structure is a bulkhead, divider or partition of an aircraft.
  • the support member is secured to said support structure in a rotational manner about a rotational axis that is in a plane parallel to the plane of a table top member.
  • the support member is secured to said support structure in a rotational manner about a rotational axis that is in a plane parallel to the plane of the two table top members when in their first or second modes.
  • the support member is secured to said support structure in a rotational manner by a base member that defines a rotational axis.
  • the rotational axis is adjacent said support structure.
  • the rotational axis is at said support structure.
  • the base member limits the rotation of the support arm to a position where the support member is in the deployed condition.
  • the support arm is an articulated arm that includes a first arm portion and a second arm portion that is rotationally supported by said first arm portion about a rotational axis that is parallel to the normal of at least one table top member.
  • the first arm portion is engaged to said support structure.
  • the second arm portion supports said table arrangement.
  • said table arrangement is supported by said second arm portion in a manner to be able to translate relative thereto.
  • said bi-fold table arrangement is supported by said second arm portion in a manner to be able to translate relative thereto in a direction perpendicular to the axis of rotation of the bi-fold table arrangement.
  • said table arrangement is supported by said second arm portion by a cam surface or surfaces and wherein a cam follower of one of the table arrangement and the second support arm can move relative said cam to provided guided translation of the table arrangement relative to said second arm portion in a direction perpendicular to the axis of rotation of the table arrangement.
  • the table arrangement is slidingly engageable with the second arm portion in a linear manner to allow for translative movement of the table arrangement.
  • the invention may be said to consist in an aircraft that includes a tray table arrangement as described.
  • the invention may be said to consist in an aircraft that includes a tray table arrangement as described in this specification and with reference to the accompanying drawings.
  • the invention may be said to consist in a tray table arrangement as described in this specification and with reference to the accompanying drawings.
  • the invention may be said to consist in a tray table arrangement suitable for use by a passenger sitting in an aircraft seat, said tray table arrangement supportable by a support structure to allow it to be presented for use by said passenger, said tray table arrangement comprising:
  • a bi-fold table arrangement comprising at least two juxtaposable table top members, a support member mountable on said support structure, for supporting the bi-fold table arrangement;
  • bi-fold table arrangement is rotatably coupleable or coupled to the support structure by said support member to move between
  • said bi-fold table in said deployed condition can be presented in a first mode in which the two table tops are in a compacted relationship to each other, and
  • bi-fold table is rotatable about an axis parallel to the normal of the two table tops when in their first mode or second mode.
  • the invention may be said to consist in a tray table arrangement suitable for use by a passenger sitting in an aircraft seat, said tray table arrangement supportable by a support structure to allow it to be presented for use by said passenger, said tray table arrangement comprising:
  • a table arrangement comprising at least one table top member presenting at least one major surface for use as a utility surface;
  • a support member mountable on said support structure, for supporting the table arrangement
  • said support member being rotationally secured to said support structure in a manner to move between
  • the invention may be said to consist in a tray table for use by a passenger sitting in an aircraft seat, said tray table supported by a support structure to allow it to be presented for use by said passenger, and comprising:
  • a bi-fold table comprising at least two juxtaposed table tops
  • a support arm extending between (i) the support structure and (ii) the bi-fold table, to support said bi-fold table
  • said support arm being rotationally secured to said support structure in a manner to move between (a) a stowed condition to position the bi-fold table at a distal more to the passenger location and (b) a deployed condition where the bi-fold table is in at least one proximate more to the passenger position, wherein in said deployed condition said bi-fold table can be presented in at least one mode for use by a passenger sitting in said aircraft seat a first mode where the two table tops are in a compacted relationship to each other and a second mode wherein said two table tops are in an expanded relationship to each other, and
  • bi-fold table in said at least one proximate more to the passenger location is able to rotate about an axis parallel to the normal of the two table tops when in their first or second modes.
  • the support structure is a seat located in front of the seat in which a passenger may sit.
  • the supports structure is a bulkhead, divider or partition of said aircraft.
  • the support arm is secured to said support structure in a rotational manner about a rotational axis that is in a plane parallel to the plane of the two table tops when in their first or second modes.
  • the support arm is secured to said support structure in a rotational manner by a base member that defines a rotational axis.
  • the rotational axis is adjacent said support structure.
  • the rotational axis is at said support structure.
  • the support arm is secured to said support structure in a rotational manner by a base member that limits the rotation of the support arm to a position where the support arm is in the deployed condition.
  • the support arm is an articulated arm that includes a first arm portion and a second arm portion that is rotationally supported by said first arm portion about a rotational axis that is parallel to the normal of the two table tops.
  • the first arm portion is engaged to said support structure.
  • the second arm portion supports said bi-fold table.
  • said bi-fold table is supported by said second arm portion in a manner to be able to translate relative thereto.
  • said bi-fold table is supported by said second arm portion in a manner to be able to translate relative thereto in a direction perpendicular to the axis of rotation of the bi-fold table.
  • said bi-fold table is supported by said second arm portion by a cam surface of surfaces and wherein a cam follower of on of the bi-fold table and the second support arm can move relative said cam to provided guided translation of the bi-fold table relative to said second arm portion in a direction perpendicular to the axis of rotation of the bi-fold table.
  • the present invention broadly may also be said to be an a tray table for use by a passenger sitting in an aircraft seat, said tray table supported by a support structure to allow it to be presented for use by said passenger, and comprising:
  • a table comprising at least one table top
  • a support arm extending between (i) the support structure and (ii) the table, to support said table
  • said support arm being rotationally secured to said support structure in a manner to move between (a) a stowed condition to position the table at a distal more to the passenger location and (b) a deployed condition where the table is in at least one proximate more to the passenger position, and
  • the table in said at least one proximate more to the passenger location is able to rotate about an axis parallel to the normal of the table when in its condition presented for use by said passenger.
  • the support structure is a seat located in front of the seat in which a passenger may sit.
  • the supports structure is a bulkhead, divider or partition of said aircraft.
  • the support arm is secured to said support structure in a rotational manner about a rotational axis that is in a plane parallel to the plane of the table.
  • the support arm is secured to said support structure in a rotational manner by a base member that defines a rotational axis.
  • the rotational axis is adjacent said support structure.
  • the rotational axis is at said support structure.
  • the support arm is secured to said support structure in a rotational manner by a base member that limits the rotation of the support arm to a position where the support arm is in the deployed condition.
  • the support arm is an articulated arm that includes a first arm portion and a second arm portion that is rotationally supported by said first arm portion about a rotational axis that is parallel to the normal of the table.
  • the first arm portion is engaged to said support structure.
  • the second arm portion supports said table.
  • said table is supported by said second arm portion in a manner to be able to translate relative thereto.
  • said table is supported by said second arm portion in a manner to be able to translate relative thereto in a direction perpendicular to the axis of rotation of the table.
  • said table is supported by said second arm portion by a cam surface of surfaces and wherein a cam follower of on of the table and the second support arm can move relative said cam to provided guided translation of the table relative to said second arm portion in a direction perpendicular to the axis of rotation of the table.
  • the present invention broadly may also be said to be an aircraft that includes a tray table as herein above described.
  • the present invention broadly may also be said to be an aircraft that includes a tray table as herein described and with reference to the accompanying drawings.
  • the present invention broadly may also be said to be a tray table as herein described and with reference to the accompanying drawings.
  • Figure 1 is a view of an aircraft onboard which the tray table of the present invention may be carried,
  • Figure 2 shows a layout of a passenger accommodation seating arrangement with which the tray tables of the present invention may be associated
  • Figure 2A is a close-up view of a Figure 2
  • Figure 3 is a plan view of a tray table of the present invention shown in three different positions
  • Figure 4 illustrates a different seating arrangement with which the tray table of the present invention can be associated
  • Figure 5 is a side view of Figure 3
  • Figure 6 is a perspective view of the tray table of the present invention.
  • Figure 7 is a bottom perspective view of the tray table of the present invention.
  • Figure 8 is a bottom view of the tray table of the present invention.
  • the aircraft 1 may have a passenger seating arrangement such as that shown in Figure 2.
  • a partial close-up plan view of part of the seating arrangement is shown in Figure 2A and 4.
  • Each of the seating arrangements is for a passenger.
  • Each of the seating arrangements has a tray table arrangement, also called a tray table 4 in this description, extending from the rear of the seating arrangement.
  • the seating arrangement acts as a support structure for the tray table 4.
  • the tray table 4 comprises a table arrangement, and a support member in the form of a support arm 9.
  • the table arrangement is preferably a bi-fold table.
  • the bi-fold table comprises two table top members (hereinafter called table tops) 5, 6.
  • the bi-fold table is movable between a first mode in which the two table top members are in a compacted relationship to each other, and a second mode wherein said two table top members are in an expanded relationship to each other.
  • the table top members each present at least one major face, and are preferably planar in form, presenting a pair of opposed major faces. It is envisaged that any of the major faces can be used by a passenger as a utility surface.
  • the support member is for supporting the table arrangement from the seating arrangement (or any other suitable support structure such as a divider, bulkhead, partition or similar feature of an aircraft).
  • the table arrangement is rotatably coupleable to a support structure by the support arm 9, to move between a stowed condition in which the table arrangement is folded up against the back of the seating arrangement in front of the passenger, as is conveniently moved out of the passengers way; and a deployed condition in which it presents a utility surface for the passengers use.
  • the table arrangement In the deployed position, is rotatable about an axis parallel to the normal of at least one major face of the table top members, and preferably about a substantially vertical axis.
  • the tray table 4, as shown in Figure 4 is in a partially deployed condition in which a one of the utility surfaces of the bi-fold table arrangement is presented (i.e. in its first mode), and is not presented directly in front of the passenger (i.e. is not fully aligned directly in front of the passenger) but instead has been rotated to the side of the passenger.
  • the tray table 4A shown in Figure 4 is shown in a fully deployed condition (in the bi-fold table is in its second mode in which the two table top members are in an expanded relationship to each other, and in which two major surfaces of the bi-fold table
  • the tray table 4B is shown in a fully stowed position whereas the tray table 4C is in a fully deployed and aligned position.
  • the tray table 4A includes two table tops 5 and 6.
  • the table tops include table top surfaces that can be presented generally upwardly when the tray table is in a fully deployed condition as shown in Figure 4.
  • the table tops 5, 6 lie on top of each other with their major faces being juxtaposed.
  • the table tops 5, 6 are hingingly engaged to each other via hinges 7.
  • the hinges 7 facilitate the folding of the table tops relative to each other.
  • the table tops are preferably supported by a support arm 9 from a seat of the seating arrangement in front of the passenger.
  • the support arm 9 preferably directly supports one of the table top panels such as table top panel 5 of the tray table 4A as shown in Figure 4.
  • the support arm 9 is itself mounted to a seat preferably via a base member 10 to move in a rotational manner around rotational axis XX.
  • the rotational axis XX is aligned substantially horizontally.
  • the support arm 9 is preferably an articulating arm comprising of a first arm portion 11 and a second arm portion 12.
  • the second arm portion 12 is able to rotate relative to the first arm portion 11 about axis Y.
  • axis Y will preferably be aligned substantially vertically.
  • the base portion 12 is rigidly mounted to a seat back of a seat in front and can hold the arm 9 in position. It allows for the arm and table arrangement to rotate about the axis XX between a stowed position as shown with reference to table top 4B in Figure 5 and a deployed position as shown with reference to table top 4C in Figure 5 or partially deployed position as shown in Figure 4 with reference to table top 4.
  • the pivot axis Y allows for the table arrangement to rotate when in a partially deployed position and with reference to table top 4 in Figure 4 through angle A to a position where it can be presented and aligned to the seat 20. Such an aligned position is shown with reference to seat 20A in reference to table of tray table 4A of Figure 4.
  • a sliding arrangement 26 is preferably provided by the second arm 12, that allows for the table to move or translate relative to the second arm 12 in a linear manner.
  • the table may hence move away from and towards the passenger sitting in seat 20A as a result of this sliding motion provision.
  • This may be provided by way of a slot 27 defined by the second arm 12 in which a hub 28 is mounted and can slide between ends of the slot.
  • the mechanism of the tray table of the present invention allows for the table to be moved to a condition where the table tops are folded up and are in a stowed position with reference to 4B of Figure 5.
  • the normal of the tray table tops may extend in a direction parallel to the FWD direction (shown as arrow FWD in figure 3) which is preferably in a direction parallel to the longitudinal direction of the plane or at an angle non-parallel to the FWD direction.
  • the table tops can move to a partially deployed position as shown with reference to tray table 4 in Figure 4 and where the table tops are non-aligned with the seat behind and to a partially deployed position where the tray table is aligned with the seat and a fully deployed position with reference to tray table 4A of Figure 4 where the table tops are unfolded, co-planar and aligned with the seat 20A.
  • the tray table In the fully deployed position the tray table may be moved between a position more distal from the passenger and a position more proximate the passenger in a linear manner.
  • a tray table arrangement is provided that allows for a wide variety of configurations that a passenger may use as utility surfaces, as well as a one that I sable to be folded out of the way when required. It is also inherently suited to use where the seating arrangements are not aligned longitudinally with the aircraft, and allows for flexibility in this regard.

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  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Transportation (AREA)
  • Mechanical Engineering (AREA)
  • Passenger Equipment (AREA)

Abstract

L'invention concerne un agencement de tablette-plateau à des fins d'utilisation par un passager assis dans un siège d'avion, l'agencement de tablette-plateau étant supporté par une structure de support qui lui permet d'être présenté à des fins d'utilisation par le passager, et comportant une tablette à deux battants comportant au moins deux éléments supérieurs de tablette juxtaposés, un bras de support s'étendant entre (i) la structure de support et (ii) la tablette à deux battants, pour supporter la tablette à deux battants, le bras de support étant assujetti de manière rotative à la structure de support de manière à permettre un déplacement entre (a) une condition escamotée positionnant la tablette à deux battants dans une position plus distale par rapport au passager et (b) une condition déployée dans laquelle la tablette à deux battants se trouve dans une position au moins plus proche par rapport au passager. Dans la condition déployée, la tablette à deux battants peut être présentée dans au moins un mode à des fins d'utilisation par un passager assis dans le siège d'avion parmi un premier mode selon lequel les deux éléments supérieurs de la tablette sont en une relation compacte l'un par rapport à l'autre et un second mode selon lequel les deux éléments supérieurs de la tablette sont en une relation étendue l'un par rapport à l'autre, et la tablette à deux battants se trouvant dans ladite au moins une position plus proche par rapport au passager étant en mesure de pivoter autour d'un axe parallèle au plan normal des deux éléments supérieurs de la tablette quand elle est dans le premier mode ou le second mode.
PCT/IB2011/050249 2010-01-20 2011-01-20 Agencement de tablette-plateau WO2011089558A1 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
AU2010900294A AU2010900294A0 (en) 2010-01-20 A tray table
AU2010900294 2010-01-20

Publications (1)

Publication Number Publication Date
WO2011089558A1 true WO2011089558A1 (fr) 2011-07-28

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ID=44306440

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/IB2011/050249 WO2011089558A1 (fr) 2010-01-20 2011-01-20 Agencement de tablette-plateau

Country Status (1)

Country Link
WO (1) WO2011089558A1 (fr)

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2015002609A1 (fr) 2013-07-04 2015-01-08 Singapore Technologies Aerospace Ltd Dossier de siège pour un siège de passager
USD732310S1 (en) 2013-12-06 2015-06-23 Zodiac Seats Uk Limited Table
EP2930109A1 (fr) * 2014-04-07 2015-10-14 Zodiac Seats UK Limited Agencement de table
WO2015156926A1 (fr) * 2014-04-07 2015-10-15 B/E Aerospace, Inc. Table à plateau extensible latéralement
WO2016165978A1 (fr) * 2015-04-13 2016-10-20 Zodiac Seats France Module de sieges muni d'une tablette a configuration optimisee
US9919802B2 (en) 2014-04-07 2018-03-20 B/E Aerospace, Inc. Laterally-expanding tray table
WO2022067119A1 (fr) * 2020-09-25 2022-03-31 Adient Aerospace, Llc Tablette coulissante pourvue d'un ensemble de verrouillage

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5547247A (en) * 1994-08-16 1996-08-20 Burns Aerospace Corporation Passenger tray table with ingress/egress position
US20050012375A1 (en) * 2003-04-30 2005-01-20 3861589 Canada Inc. Seat for aircraft
US20060109257A1 (en) * 2004-10-18 2006-05-25 Emilio Ambasz Writing tablet

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5547247A (en) * 1994-08-16 1996-08-20 Burns Aerospace Corporation Passenger tray table with ingress/egress position
US20050012375A1 (en) * 2003-04-30 2005-01-20 3861589 Canada Inc. Seat for aircraft
US20060109257A1 (en) * 2004-10-18 2006-05-25 Emilio Ambasz Writing tablet

Cited By (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2015002609A1 (fr) 2013-07-04 2015-01-08 Singapore Technologies Aerospace Ltd Dossier de siège pour un siège de passager
EP3016550A4 (fr) * 2013-07-04 2017-03-22 Singapore Technologies Aerospace Ltd Dossier de siège pour un siège de passager
USD732310S1 (en) 2013-12-06 2015-06-23 Zodiac Seats Uk Limited Table
WO2015156926A1 (fr) * 2014-04-07 2015-10-15 B/E Aerospace, Inc. Table à plateau extensible latéralement
US9573687B2 (en) 2014-04-07 2017-02-21 B/E Aerospace, Inc. Laterally-expanding tray table
EP2930109A1 (fr) * 2014-04-07 2015-10-14 Zodiac Seats UK Limited Agencement de table
EP3128873A4 (fr) * 2014-04-07 2017-09-27 B/E Aerospace, Inc. Table à plateau extensible latéralement
US9776723B2 (en) 2014-04-07 2017-10-03 Zodiac Seats Uk Limited Table arrangement
US9919802B2 (en) 2014-04-07 2018-03-20 B/E Aerospace, Inc. Laterally-expanding tray table
WO2016165978A1 (fr) * 2015-04-13 2016-10-20 Zodiac Seats France Module de sieges muni d'une tablette a configuration optimisee
US20180127099A1 (en) * 2015-04-13 2018-05-10 Zodiac Seats France Seat module comprising a tray table with an optimised design
JP2018512335A (ja) * 2015-04-13 2018-05-17 ゾディアック シーツ フランス 最適化された構成のテーブル付き座席モジュール
US10494102B2 (en) 2015-04-13 2019-12-03 Safran Seats Seat module comprising a tray table with an optimised design
WO2022067119A1 (fr) * 2020-09-25 2022-03-31 Adient Aerospace, Llc Tablette coulissante pourvue d'un ensemble de verrouillage
US11827360B2 (en) 2020-09-25 2023-11-28 S & S Numerical Control, Inc. Slide-out tray table with interlock assembly

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