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WO2018185109A1 - Dispositif siège d'aéronef - Google Patents

Dispositif siège d'aéronef Download PDF

Info

Publication number
WO2018185109A1
WO2018185109A1 PCT/EP2018/058503 EP2018058503W WO2018185109A1 WO 2018185109 A1 WO2018185109 A1 WO 2018185109A1 EP 2018058503 W EP2018058503 W EP 2018058503W WO 2018185109 A1 WO2018185109 A1 WO 2018185109A1
Authority
WO
WIPO (PCT)
Prior art keywords
armrest
aircraft seat
aircraft
separating element
seat device
Prior art date
Legal status (The legal status 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 status listed.)
Ceased
Application number
PCT/EP2018/058503
Other languages
German (de)
English (en)
Inventor
Andreas Erb
Michael HORLACHER
Christopher TUTE
Jochen Lohrmann
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Recaro Aircraft Seating GmbH and Co KG
Original Assignee
Recaro Aircraft Seating GmbH and Co KG
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
Application filed by Recaro Aircraft Seating GmbH and Co KG filed Critical Recaro Aircraft Seating GmbH and Co KG
Priority to EP18715670.8A priority Critical patent/EP3606824A1/fr
Publication of WO2018185109A1 publication Critical patent/WO2018185109A1/fr
Anticipated expiration legal-status Critical
Ceased legal-status Critical Current

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
    • B64D11/0606—Arrangements of seats, or adaptations or details specially adapted for aircraft seats with privacy shells, screens, separators or the like
    • 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 invention relates to an aircraft seat device according to the preamble of
  • an aircraft seat device having at least two adjacently arranged aircraft seats and at least one armrest arranged between the two aircraft seats, the armrest being movable between a stowage position and a use position.
  • the object of the invention is in particular to provide a generic device with improved passenger comfort features. The object is achieved by the features of claim 1, while advantageous embodiments and refinements of the invention
  • the aircraft seat device at least one on a
  • an "aircraft seat” is to be understood in particular as a seat which is intended to be raised in an aircraft cabin of an aircraft on a cabin floor, and on which a passenger can sit during a flight.
  • the aircraft seat has at least one seat bottom and a seat back coupled to the backrest, wherein the backrest is preferably pivotally connected to the seat bottom, whereby the aircraft seat is preferably movable into different functional positions.
  • the aircraft seat further has at least one, preferably two
  • the armrest In the stowed position, the armrest is preferably arranged as space-saving as possible on the aircraft seat and can not be used by a passenger to store his arm. In the staging is the
  • Armrest preferably aligned substantially parallel to the backrest. It is conceivable that the armrest has an angle of -10 to +10 degrees to the backrest. In its position of use, the armrest is aligned substantially parallel to the seat bottom, wherein the armrest can have an angle of 0 to 10 degrees to the seat bottom. The armrest is thereby moved from its position of use in particular upwards in its stowed position, in which case preferably a front end of the armrest is pivotable upwards.
  • at least two juxtaposed aircraft seats should be understood in particular two immediately adjacent aircraft seats, which are part of a row of seats, the two adjacent aircraft seats preferably only by a
  • Aircraft seats preferably share an armrest arranged between the two aircraft seats, which is intended for use by passengers of both aircraft seats.
  • a "separating element” should be understood to mean, in particular, an element which, at least in one position, projects into an area between two immediately adjacent aircraft seats, around seating areas of the two
  • a "support element” is to be understood here as meaning, in particular, an element which is provided so that a passenger can partially support himself at least with one body part.
  • the seating areas of two adjacently arranged aircraft seats increase a perceived privacy of the passengers seated on the aircraft seats.
  • the term "provided” is to be understood to mean in particular specially designed and / or equipped.Assuming that an object is intended for a specific function should in particular mean that the object fulfills this specific function in at least one application and / or operating state and / or executes.
  • an aircraft seat device can advantageously be provided in which two adjacently arranged aircraft seats form particularly advantageous support options for passengers seated on the two aircraft seats, and the aircraft seats are thereby designed to be particularly comfortable. It is further proposed that the separating element at least substantially forms a wedge shape. As a result, the separating element can be designed to be particularly ergonomic.
  • the separating element has a width which is smaller, at least in a partial region, by at least 20% than a width of the armrest on its upper side.
  • the term "at least 20% smaller” should be understood to mean, in particular, at least 20% smaller, preferably at least 35% smaller and in a particularly preferred embodiment at least 50% smaller. is smaller, it should be understood in particular that a width of the separating element, in particular in a
  • Connection area to the armrest may be substantially equal to the width of the armrest, and a width of the separating element, in particular in a region remote from the armrest is smaller than the width of the armrest.
  • the separating element can be formed particularly advantageous.
  • the separating element has a height which extends in the position of use of the armrest substantially from a bottom of the armrest to at least 10 cm in front of the seat bottom.
  • a distance between the separating element in a position of use of the armrest is a maximum of 10 cm, preferably a maximum of 5 cm and in a particular preferred embodiment less than 1 cm.
  • the separating element at least one
  • Storage unit having at least one storage space is formed.
  • a “storage unit” is to be understood in particular as meaning a unit which forms a storage space in which a passenger can stow utensils, wherein the storage space can be arranged at least partially in an interior of the separating element or also on a side surface of the storage compartment
  • Storage space of the storage unit at least partially extends into an interior of the armrest and / or is arranged on an outer side surface of the armrest. This makes it particularly easy to provide a storage space for the passenger, in which he can accommodate utensils during a flight.
  • the at least one separating element in a stowed position of the armrest, is movable into a lowered position.
  • a "sinking position of the separating element" in particular a position of the
  • Separating element to be understood in which it does not protrude in the stowed position of the armrest on a backrest surface of the backrest.
  • the separating element In the retracted position, the separating element is arranged completely behind a plane which is formed by front edges of the backrests of the adjacently arranged aircraft seats.
  • the separating element can advantageously be stowed completely in an area behind a backrest surface in order thus to generate a double aircraft seat or to facilitate access to the second aircraft seat.
  • the term "laterally at least partially coinciding with the armrest” is to be understood in particular as meaning that in a side view, ie orthogonal to a seating direction of the aircraft seats, the separating element is formed overlapping the armrest and, in particular, does not have a seat Outline of the armrest. In this case, the separating element to achieve the
  • the separating element has at least two telescopically adjustable elements. As a result, the separating element can be adjusted particularly easily.
  • the separating element has at least two mutually pivotable elements.
  • the mutually pivotable elements may be formed, for example, as fan elements. Thereby, the separating element can be formed particularly advantageous.
  • the separating element is rigidly connected to the armrest, wherein the armrest is pivotable about a second axis of rotation orthogonal to a pivot axis for adjusting the armrest between the
  • the armrest can be advantageously rotated together with the separating element in a stowed position, whereby the separating element is brought into its lowered position.
  • the separating element is formed separable from the armrest.
  • the term "separable” should be understood to mean, in particular, non-destructive separation, so that the separating element can in particular be repeatedly fixedly mounted on the armrest and disassembled again from the armrest.
  • the aircraft seat device according to the invention is not intended to be the above
  • the aircraft seat device according to the invention may have a number deviating from a number of individual elements, components and units mentioned herein.
  • Fig. 1 is a schematic view of an aircraft seat row with a
  • Aircraft seat device in a first
  • Fig. 2 is a schematic view of an aircraft seat row from above with a
  • Fig. 8 is a schematic representation of an armrest and a
  • FIG. 9 is a schematic representation of an armrest and a
  • Fig. 1 1 is a schematic representation of an armrest and a
  • Fig. 12 is a schematic representation of an armrest and a
  • Figures 1 to 4 show an aircraft seat device in a first
  • the aircraft seat device is part of an aircraft seat row 10a.
  • the aircraft seat row 10a comprises three aircraft seats 12a, 14a, 16a.
  • the aircraft seat row 10a comprises a different number of aircraft seats 12a, 14a, 16a.
  • a seat row is formed only from a single aircraft seat 14a.
  • the aircraft seat 12a, 14a, 16a of the aircraft seat rows Oa are arranged directly next to one another.
  • the first aircraft seat 12a is arranged on a right side of the aircraft seat row 10a.
  • the seat bottom 20a is rigidly connected to the upstand unit 18a. In principle, however, it is also conceivable that the seat bottom 20a is adjustable between a sitting position and a comfort position relative to the Aufmenrritt 18a.
  • the seat bottom 20a forms a seat surface for a passenger seated on the aircraft seat 14a.
  • the aircraft seat 14a comprises a backrest 22a.
  • the backrest 22a is disposed at a rear end of the seat bottom 20a.
  • the backrest 22a is coupled to the upstand unit 18a.
  • the backrest 22a is pivotable between a substantially upright sitting position and an inclined comfort position to the Aufmenmenrmaschine 18a.
  • the backrest 22a is rigidly coupled to the Aufcommunrnati 18a and / or at least partially formed integrally with the seat bottom 20a.
  • the aircraft seat row 10a has a seat divider 24a, which is located between the middle
  • the aircraft seat apparatus includes a second armrest 30a.
  • the second armrest 30a is disposed between the center aircraft seat 14a and the adjacent left aircraft seat 16a.
  • the armrest 30a is intended to be used by a passenger seated on the center aircraft seat 14a and a passenger seated on the adjacent right aircraft seat 12a.
  • the aircraft seat device has two further armrests 32a, 34a, which are respectively arranged on an outer side of the aircraft seats 12a, 16a and terminate the row of aircraft seats 10a towards the outside.
  • the armrests 28a, 30a, 32a, 34a are connected directly to the backrest 22a of the corresponding aircraft seat 12a. It is conceivable that the armrests 28a, 30a, 32a, 34a are connected in particular to a supporting structure of the corresponding backrest 22a.
  • the supporting structure of the backrest 22a, to which the armrests 28a, 30a, 32a, 34a are directly connected, can be formed by way of example of a fiber composite material.
  • the aircraft seat apparatus has another partition member 40a disposed on a lower side of the armrest 30a.
  • the two outer armrests 32a, 34a are shown here without separating elements in the figures and as normal, known from the prior art armrests
  • the separating element 38a designed as a supporting element is provided so that a passenger seated on the lateral aircraft seat 12a can at least laterally support himself at least with a part of his body. In this case, two passengers seated next to one another on the adjacently arranged aircraft seats 12a, 14a can simultaneously be formed on the support element
  • Separator 38a as shown to be concave.
  • the side surfaces 42a, 44a as indicated by dashed lines in Figure 5, may also be convex.
  • the side surfaces 42a, 44a as indicated by dashed lines in Figure 5 may also be convex.
  • the side surfaces 42a, 44a as indicated by dashed lines in Figure 5 may also be convex.
  • the side surfaces 42a, 44a as indicated by dashed lines in Figure 5
  • the aircraft seat apparatus includes a comfort member 46a.
  • the comfort element 46a comprises a padding and a protective cover.
  • the upholstery is included
  • the comfort element 46a spans the side surfaces 42a, 44a of the separating element 38a.
  • the comfort element 46a also spans side surfaces 48a, 50a of the armrest 28a.
  • a particularly advantageously comfortable side support surface for passengers of adjacently arranged aircraft seats 12a, 14a can be provided.
  • FIG. 6 to 13 eight further embodiments of the invention are shown. The following descriptions and the drawings are essentially limited to the differences between the embodiments, with respect to the same components, in particular with respect to components with the same reference numerals, in principle also to the drawings and / or the description of the other
  • Aircraft seat device is part of an aircraft seat row, not shown here.
  • the aircraft seat row includes, as in the first embodiment, a plurality of juxtaposed aircraft seats arranged between the aircraft seats armrests 28b.
  • the aircraft seat apparatus has a partition member 38b disposed on a lower side of the armrest 28b. In contrast to the first embodiment, the armrest 28b and the
  • the partition 38b has a storage unit 52b.
  • Storage unit 52b has a storage space 54b on each side surface 42b, 44b of the separating element 38b. In the figure 6 is only one
  • Pocket member 56b formed, which is firmly connected to the side surface 44b of the partition member 38b.
  • the pocket element 56b is formed by an elastically extensible material. It is also conceivable that the pocket element 56b of a
  • Utensils can be stored in the storage space 54b, which is spanned by the pocket member 56b and the divider 38b. Utensils can between the bag member 56b and the
  • Separator 38b are clamped.
  • the storage unit 52b is arranged at least partially in the area of the armrest 38b.
  • the aircraft seat apparatus includes a fastener 98b. The fastener 98b is attached to the armrest 28b and the separator 38b.
  • Fastener 98b is provided so that a passenger can tie a personal item to the armrest 28b and the partition member 38b.
  • the fastener 98b is in a front portion of the armrest 28b and the
  • Aircraft seat device a plurality and / or arranged at another location
  • Attachment 98b has.
  • Fastening means 98b wraps around the armrest 28b and the partition member 38b in the circumferential direction.
  • the fastener 98b is formed as an elastic band.
  • the fastening means 98b is designed to be elastically extensible.
  • a passenger can elastically elongate the fastener 98b by pulling on the fastener 98b, thereby interposing between the armrest 28b, divider 38b, and fastener 98b Space is created in which the passenger can introduce the object. After the passenger has withdrawn the force on the fastener 98b, the fastener 98b pulls by its internal tension, which by the elastic
  • the aircraft seat device has an operating module 100b.
  • the control module 100b includes a plurality of controls provided for controlling the aircraft seat or other peripheral devices, such as a display screen.
  • Operating module 100b is arranged on side surfaces 42b, 48b of the armrest 28b and of the separating element 38b. Due to the increased area provided by the side surfaces 42b, 48b of the armrest 28b and the separating element 38b, an operating module 100b may preferably have many and / or larger operating elements than in the prior art.
  • Figure 7 shows a third embodiment of an inventive
  • Aircraft seat device is part of one not closer illustrated aircraft seat row.
  • the aircraft seat row includes as in the first
  • Embodiment a plurality of juxtaposed aircraft seats arranged between the aircraft seats armrests 28c.
  • the aircraft seat apparatus has a partition member 38c disposed on a lower side of the armrest 28c.
  • the partition 38c is intended to be movable to a sinking position. In the retractable position, the partition 38c is intended not to protrude beyond a backrest surface of a seat back in the stowed position of the armrest 28c.
  • the separating element 38c is brought laterally in a sinking position in coincidence with the armrest 28c. In the lowered position, the separating element 38c thereby does not protrude beyond the armrest 28c in a side view.
  • the partition 38c is intended to be located in the lowered position within the armrest 28c.
  • the armrest 28c has a recess in which the separating element 38c in the
  • the armrest 28c has an adjusting mechanism 58c.
  • the adjusting mechanism 58c supports the partition member 38c movably to the armrest 28c.
  • the adjusting mechanism 58c is formed by a bearing element 60c.
  • the bearing member 60c is rotatably connected to the armrest 28c and the partition member 38c.
  • the bearing member 60c is formed as a bearing rod.
  • the bearing member 60c is rotatably supported at a first end in a rear portion of the armrest 28c.
  • the bearing member 60c is rotatably supported at a second end to a front portion of the partition member 38c.
  • the bearing element 60c is arranged obliquely to the armrest 28c and protrudes down from the recess in the armrest 28c out.
  • the partition member 38c attached to the bearing member 60c protrudes from the armrest 28c at the bottom and is disposed in its use position.
  • the bearing element 60 c is pivoted into a position aligned substantially parallel to the armrest 28 c and completely in the
  • Figure 8 shows a fourth embodiment of an inventive
  • Aircraft seat device is part of an aircraft seat row, not shown here.
  • the aircraft seat row includes as in the first
  • Embodiment a plurality of juxtaposed aircraft seats arranged between the aircraft seats armrests 28d.
  • the aircraft seat apparatus has a partition member 38d disposed on an underside of the armrest 28d.
  • the separator 38d is intended to be movable to a sinking position. In the retracted position, the divider 38d is intended not to protrude beyond a backrest surface of a seat back in the stowed position of the armrest 28d. In the retractable position, the separating element 38d on the underside of the armrest 28d is formed so small that the separating element 38d does not extend beyond a plane of the
  • the armrest 28d is here formed in FIG. 8 as a thin plate compared to the other embodiments. In principle, it is also conceivable that the armrest 28d is formed by a thicker element.
  • the separating element 38d is formed by five articulated elements 62d, 64d, 66d, 68d, 70d.
  • the elements 62d, 64d, 66d, 68d, 70d are formed as plates.
  • the two first elements 62d, 64d are spaced apart from each other with a first end hinged to the underside of the armrest 28d.
  • the two second elements 66d, 68d are each hingedly connected at their first end to a second end of the first elements 62d, 64d.
  • the second elements 66d, 68d are hinged together at their second ends.
  • Separator 38d is connected to the second ends of the second elements 66d, 68d. As a result, a foldable separating element 38d is formed. In a use position, the interconnected elements 62d, 64d, 66d, 68d, 70d substantially form a wedge shape, with the fifth element 70d forming a point. The four others
  • Elements 62d, 64d, 66d, 68d each form two side surfaces of the separating element 38d.
  • the elements 62d, 64d, 66d, 68d for a sinking position can be folded into one another as shown in FIG. 8 by folding the second elements 66d, 68d inwardly into an area between the two first elements 62d, 64d.
  • the fifth element 70d is arranged centrally between the two second elements 66d, 68d and does not protrude beyond the first elements 62d, 64d in the lowered position.
  • Figure 9 shows a fifth embodiment of an inventive
  • Aircraft seat device is part of an aircraft seat row, not shown here.
  • the aircraft seat row includes as in the first
  • Embodiment a plurality of juxtaposed aircraft seats arranged between the aircraft seats armrests 28e.
  • the aircraft seat apparatus has a partition member 38e disposed on a lower side of the armrest 28e.
  • the separating element 38e is formed by two mutually pivotable elements 72e, 74e.
  • the elements 72e, 74e are designed as fan elements.
  • the separating element 38e is formed by a different number of elements 72e, 74e.
  • the embodiment with exactly two elements 72e, 74e is intended to be only an example here.
  • the elements 72e, 74e are pivotally connected to the armrest 28e via a common axis of rotation 76e.
  • the axis of rotation 76e is arranged at a first, rear end of the armrest 28e.
  • the elements 72e, 74e are preferably U-shaped.
  • the outer element 74e is preferably made smaller, so that the inner element 72e can enclose the outer element 74e.
  • the armrest 28e has on its underside a recess in which the elements 72e, 74e in a
  • the aircraft seat device has a locking unit, not shown, which fixes the elements 72e, 74e in the lowered position and in a position of use relative to the armrest 28e.
  • Figure 10 shows a sixth embodiment of an inventive
  • Aircraft seat device is part of one not closer illustrated aircraft seat row.
  • the aircraft seat row includes as in the first
  • the aircraft seat apparatus has a partition member 38f disposed on a lower side of the armrest 28f.
  • the partition 38f is intended to be movable to a sinking position. In the retractable position, the divider 38f is intended not to protrude beyond a backrest surface of a seat back in the stowed position of the armrest 28f.
  • the separating element 38f is brought laterally in a sinking position into coincidence with the armrest 28f. In the lowered position, the separating element 38f thus does not protrude beyond the armrest 28f in a side view.
  • the partition 38f is intended to be located in the lowered position within the armrest 28f.
  • the armrest 28f has a recess in which the separating element 38f in the
  • Reverse position is arranged.
  • the recess is attached to a lower end of the armrest 28f.
  • the armrest 28f has an adjusting mechanism 58f.
  • the adjustment mechanism 58f supports this
  • the adjusting mechanism 58f is formed as a scissors mechanism.
  • the adjustment mechanism 58f has two
  • Bearing elements 78f, 80f which are pivotally connected at a first end to the armrest 28f.
  • the bearing elements 78f, 80f are formed as rods. With a second end, the bearing elements 78f, 80f are rotatable and each along one
  • Figure 1 1 shows a seventh embodiment of an inventive
  • Aircraft seat device is part of an aircraft seat row, not shown here.
  • the aircraft seat row includes as in the first
  • the aircraft seat apparatus has a partition member 38g disposed on an underside of the armrest 28g.
  • the armrest 28g and the Separator 38g designed differently. In FIG. 11, therefore, only the armrest 28g and the separating element 38g are shown.
  • the partition 38g is rigidly connected to the armrest 28g.
  • the partition 38g is integrally formed with the armrest 28g.
  • the armrest 28g has a bearing block 86g. Via the bearing block 86g, the armrest 28g is pivotable between its position of use and its stowed position.
  • the bearing block 86g forms a first axis of rotation 88g, which is formed transversely to a seating direction.
  • the bearing block 86g has a second axis of rotation 90g.
  • the second axis of rotation 90g is orthogonal on the axis of rotation 88g for adjusting the armrest 28g between the stowed position and the
  • Figure 12 shows an eighth embodiment of an inventive
  • Aircraft seat device is part of an aircraft seat row, not shown here.
  • the aircraft seat row includes, as in the first embodiment, a plurality of juxtaposed aircraft seats arranged between the aircraft seats armrests 28h.
  • the aircraft seat apparatus has a partition member 38h disposed on an underside of the armrest 28h. In contrast to the first embodiment, the armrest 28h and the
  • FIG. 13 shows a ninth embodiment of an aircraft seat device according to the invention.
  • the aircraft seat device is part of an aircraft seat row, not shown here.
  • the aircraft seat row includes as in the first
  • Embodiment a plurality of juxtaposed aircraft seats arranged between the aircraft seats armrests 28i.
  • the aircraft seat apparatus has a partition member 38i disposed on a lower side of the armrest 28i.
  • the armrest 28i forms a U-shaped main body.
  • the armrest 28i in this case has a recess 102i in the transverse direction, between the side by side
  • the separating element 38i is formed by an element 72i, which can be pivoted to the armrest 28i.
  • the pivotable element 72i is pivotally mounted at a front end of the armrest 28i via a rotation axis 76i.
  • the axis of rotation 76i is disposed in a lower third of the armrest 28i.
  • the pivotable element 72i forming the separating element 38i is arranged in the recess 102i of the U-shaped main body of the armrest 28i.
  • the separating element 38i forming
  • pivotable element 72i pivoted by substantially 180 degrees, whereby the partition element 38i forming pivotable element 72i swings under the U-shaped main body of the armrest 28i out.

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

Abstract

L'invention concerne un dispositif siège d'aéronef comprenant au moins deux sièges d'aéronef (12a, 14a, 16a) disposés l'un à côté de l'autre et au moins un accoudoir (28a, 30a ; 28b ; 28c ; 28d ; 28e ; 28f ; 28g ; 28h, 28i) disposé entre les deux sièges d'aéronef, l'accoudoir (28a, 30a ; 28b ; 28c ; 28d ; 28e ; 28f ; 28g ; 28h, 28i) étant déplaçable entre une position de rangement et une position d'utilisation. Selon l'invention, au moins un élément de séparation (38a, 40a ; 38b ; 38c ; 38d ; 38e ; 38f ; 38g ; 38h, 38i) est prévu, qui est disposé sur un côté inférieur de l'accoudoir (28a, 30a ; 28b ; 28c ; 28d ; 28e ; 28f ; 28g ; 28h, 28i), qui forme, au moins dans une position de rangement de l'accoudoir (28a, 30a ; 28b ; 28c ; 28d ; 28e ; 28f ; 28g ; 28h, 28i), un élément d'appui et/ou d'espace privé, et qui sépare les zones d'assise des deux sièges d'aéronef (12a, 14a, 16a) l'une de l'autre.
PCT/EP2018/058503 2017-04-03 2018-04-03 Dispositif siège d'aéronef Ceased WO2018185109A1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
EP18715670.8A EP3606824A1 (fr) 2017-04-03 2018-04-03 Dispositif siège d'aéronef

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE102017107139.3 2017-04-03
DE102017107139.3A DE102017107139A1 (de) 2017-04-03 2017-04-03 Flugzeugsitzvorrichtung

Publications (1)

Publication Number Publication Date
WO2018185109A1 true WO2018185109A1 (fr) 2018-10-11

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PCT/EP2018/058503 Ceased WO2018185109A1 (fr) 2017-04-03 2018-04-03 Dispositif siège d'aéronef

Country Status (3)

Country Link
EP (1) EP3606824A1 (fr)
DE (1) DE102017107139A1 (fr)
WO (1) WO2018185109A1 (fr)

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GB2614031A (en) * 2021-10-07 2023-06-28 New Territory Design Ltd Vehicle seating

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US10737790B1 (en) * 2018-11-06 2020-08-11 Pedro Cabrita Safety barrier for aircraft seats
WO2021262215A1 (fr) * 2020-06-22 2021-12-30 Safran Seats Usa Llc Séparateur rétractable pour siège de passager
FR3119806B1 (fr) * 2021-02-17 2024-06-14 Speedinnov Siège d’un véhicule de transport et véhicule de transport associé

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DE102004061471A1 (de) * 2004-12-21 2006-07-06 Recaro Aircraft Seating Gmbh & Co. Kg Passagiersitz, insbesondere Fluggastsitz, sowie Passagier-Sitzgruppe, insbesondere Fluggast-Sitzgruppe
DE102005017879A1 (de) * 2005-04-19 2006-10-26 Recaro Aircraft Seating Gmbh & Co. Kg Passagiersitz, insbesondere Fluggastsitz

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