• 专利附录
  • 专利说明
  • 权利要求
  • 类似技术
  • 同族专利
  • 引用文献
  • 法律状态
  • 优先权
    • 专利摘要:
    The invention relates mainly to a seating arrangement (11), characterized in that it comprises: - at least a first set (E1) of seating units comprising a first seating unit (12.1) and a second seating unit seat (12.2), - at least a second set (E2) of seat units comprising a first seat unit (12.1) and a second seat unit (12.2), - a central space (35) extending between the first set of seat units (E1) and the second set of seat units (E2), - and in that the arrangement of seats (11) comprises closing means (37) at least partially flexible, said closure means (37) being movable between a stowed position in which the closure means (37) are released from the central space (35) and a deployed position in which the closure means (37) seal the central space (35).
    公开号:FR3081835A1
    申请号:FR1870648
    申请日:2018-06-05
    公开日:2019-12-06
    发明作者:Bastien Bonnefoy
    申请人:Zodiac Seats France SA；
    IPC主号:
    专利说明:

    Description
    Title of the invention: ARRANGEMENT OF SEATS, ESPECIALLY AN AIRPLANE The present invention relates to an arrangement of seats, in particular seats for passengers of a transport vehicle, in particular of an airplane.
    The invention aims to provide such an arrangement of seats which ensures both the comfort and safety of passengers, while providing to preserve their privacy. The invention thus finds a particularly advantageous application with airplane seats.
    Business class aircraft seats offer passengers different comfort positions, from a seated position to a berth position, in which the seat defines a substantially horizontal sleeping plane so that the passenger can lengthen.
    Intermediate comfort positions are also proposed, such as the relaxed position in which the backrest is strongly inclined. Generally, these intermediate positions are obtained by tilting the pivoting backrest around a horizontal axis and perpendicular to an extension axis of the seat. The passenger can then remain in the seat during transitions between the different positions.
    The berth is generally made up in particular of the backrest, the seat, a legrest and a footrest, the latter possibly being fixed or linked to the kinematics of the seat.
    The invention aims to improve the privacy of a passenger by allowing him to isolate himself from his immediate neighbor. To this end, the subject of the invention is Arrangement of seats, in particular intended to be installed in an aircraft cabin, characterized in that it comprises:
    - At least a first set of seat units comprising a first seat unit and a second seat unit located one next to the other and respectively comprising a seat capable of moving from a seated position to a berth position ,
    - at least a second set of seat units comprising a first seat unit and a second seat unit situated one next to the other and respectively comprising a seat capable of passing from a seated position to a berth position ,
    - a central space extending between the first set of seat units and the second set of seat units,
    - And in that the seating arrangement comprises closing means at least partially flexible, said closing means being movable between a stowed position in which the closing means are released from the central space and a deployed position in which the closing means seal the central space.
    In one embodiment, the central space is a passage for a person authorizing communication between the first seat unit and the second seat unit of the first set.
    According to one embodiment, the central space extends above a continuous central piece of furniture between the first set of seat units and the second set of seat units.
    In one embodiment, the closure means comprise a curtain, in particular made at least in part of fabric, and a curtain return device in the stowed position.
    In one embodiment, said arrangement comprises means for holding the curtain in the deployed position, such as a handle intended to cooperate with a support and / or a magnetic device.
    In one embodiment, the return device comprises at least one elastic return member, such as a spring.
    In one embodiment, the return device comprises a reel provided with an axis around which at least part of the curtain is wound when the curtain is in the stowed position.
    According to one embodiment, the reel is arranged horizontally in the lower part.
    According to one embodiment, the reel incorporates an electric motor.
    In one embodiment, said arrangement comprises vertical uprights ensuring guiding in translation of the curtain.
    In one embodiment, said arrangement comprises a guide bar connecting the curtain to the vertical uprights.
    In one embodiment, said arrangement comprises a housing in which the curtain is housed in the stowed position.
    In one embodiment, the housing extends projecting relative to a floor of the aircraft.
    In one embodiment, said arrangement comprises means for stiffening the curtain, such as cords or a flexible plate.
    In one embodiment, said arrangement comprises means for generating a light pattern.
    In one embodiment, the means for generating a light pattern comprise a light source and translucent son arranged in a thickness of the curtain.
    According to one embodiment, the means for generating a light pattern comprise a light panel arranged inside the curtain.
    In one embodiment, the means for generating a light pattern comprise an assembly of lamps, in particular of the LED type.
    In one embodiment, the closure means comprise a semi-flexible curtain having an alternation of blades and folding zones.
    According to one embodiment, means for holding the semi-flexible curtain in the stowed position and in the deployed position, in particular of the magnetic type.
    In one embodiment, the closure means comprise a curtain, in particular made at least in part from sound absorption material.
    Of course, the various characteristics, variants and / or embodiments of the present invention can be combined with one another in various combinations insofar as they are not incompatible or mutually exclusive of each other.
    The present invention will be better understood and other characteristics and advantages will appear on reading the following detailed description comprising embodiments given by way of illustration with reference to the appended figures, presented by way of examples not restrictive, which could serve to complete the understanding of the present invention and the description of its implementation and, if necessary, contribute to its definition, on which:
    - Figures la and 1b are schematic views from above of aircraft cabins incorporating different alternative embodiments of a seating arrangement according to the present invention;
    - Figure 2a is a perspective view illustrating a first embodiment of the closure means according to the invention;
    - Figure 2b is a side view of the closure means comprising a spring return device;
    - Figure 2c is a perspective view of a handle used to pass the curtain according to the invention from a stowed position to a deployed position;
    - Figure 3 is a side view illustrating the structure of a curtain constituting the closure means according to the invention;
    - Figure 4 is a perspective view illustrating a second embodiment of the closure means according to the invention;
    - Figure 5 is a perspective view illustrating a third embodiment of the closure means according to the invention;
    - Figure 6 is a side view of an assembly of two seats showing the integration of stiffening means inside the curtain according to the present invention;
    - Figures 7a, 7b, and 7c are views illustrating three embodiments of means for generating a light pattern in the closure means according to the present invention;
    - Figure 8 is a front view of the various elements making up a semiflexible curtain according to the present invention;
    - Figure 9 is a detailed view of the magnetic holding means of the semi-flexible curtain in the deployed position;
    - Figure 10 is a perspective view of a semi-flexible curtain having an accordion configuration in the stowed position.
    It should be noted that, in the figures, the structural and / or functional elements common to the various embodiments may have the same references. Thus, unless otherwise stated, such elements have identical structural, dimensional and material properties.
    The figure shows an aircraft cabin 10 extending along a longitudinal axis XI comprising a seating arrangement 11. The seating arrangement 11 according to the present invention comprises a plurality of seating units 12 respectively comprising a individual seat 13. Advantageously, the seat 13 is able to pass from a seated position, corresponding to the position used in particular during the stop, take-off and landing phases of the aircraft, and a berth position, in which the seat 13 defines a substantially horizontal sleeping plane for the passenger. In particular, the sitting position and the sleeping position constitute configurations of the seat 13 in two extreme positions. According to alternative embodiments, the seat 13 can also take intermediate positions, called relax positions, between these two extreme positions.
    The plurality of seat units 12 are arranged in at least one row 15a preferably extending along the longitudinal axis XI of the aircraft cabin 10. According to the example presented in Figures la and 1b, the plurality of seat units 12 are arranged in four rows 15a, 15b, 15c, and 15d.
    According to various particular embodiments, inside the row 15a, respectively the rows 15a, 15b, 15c and 15d, the seat unit 12 can be oriented in such a way that the seat 13 is turned towards the front and / or rear of the aircraft. The seats 13 can form a non-zero angle with respect to the longitudinal axis XI as indicated in more detail below.
    It should be noted that the terms front and rear used in connection with the expression seat unit locally define a relative position of the seat 13 inside the row 15a, respectively the rows 15a, 15b, 15c and 15d , and do not refer in any way to an orientation of the seat 13 inside the aircraft cabin 10. In other words, the expression front seat unit means that the seat unit is positioned directly in front of another seat unit inside the row, while the expression rear seat unit means that the seat unit is positioned directly behind another seat unit inside the row.
    According to the embodiment presented, the arrangement of seats 11 comprises two lateral groups 16a, 16b comprising seating units 12. The two lateral groups 16a, 16b each consist respectively of a row 15a, 15b of seat units 12 positioned along a side wall 17 of the fuselage of the aircraft cabin 10. The seating arrangement 11 also includes a central group
    20. The central group 20 is preferably made up of two rows 15c, 15d of seat units 12. In such an arrangement, the two rows 15c, 15d of seat units 12 are placed side by side one with respect to the other.
    The lateral groups 16a, 16b are respectively separated from the central group 20 by a circulation corridor 21. According to the configuration presented in FIG. La, two circulation corridors 21 are therefore provided in the aircraft cabin 10, specifically between each lateral group 16a, 16b and the central group 20. As a variant, the two lateral groups 16a, 16b may each be formed by several rows of seat units 12.
    Each seat 13 has an extension axis X2 corresponding substantially to a direction of longitudinal extension of the seat 13. In particular, the extension axis X2 corresponds to the longitudinal extension direction of the seat 13 in the berth position . In this case, the axis X2 is substantially parallel to the longitudinal axis XI of the aircraft cabin, that is to say it forms an angle less than 10 degrees relative to the axis XI.
    Alternatively, as shown in Figure 1b, the extension axis X2 of a seat forms a non-zero angle greater than 10 degrees with the longitudinal axis XI of the aircraft cabin 10. We can then define chevron seat configurations in which the two seat units 12 form a "V". The seat units 12 can be turned towards the inside of the assembly as is the case in FIG. 1b, so that the point of the “V” shape is located in front of the seat units. Alternatively, the seat units 12 are turned towards an adjacent circulation corridor 21 so that the point of the “V” shape is located behind the backs 24 of the seats 13 (configuration in reverse chevron or reverse herringbone in English). Thus arranged, each passenger has direct access to the circulation corridor 21 from the seat 13.
    Optimizing the density of aircraft cabin 10 relative to a width of the latter is in particular possible by modifying the angle of the extension axis X2 of the seats 13 relative to the longitudinal axis XI from the aircraft cabin 10.
    According to various embodiments, the extension axes X2 of the seats 13 can form substantially the same angle relative to the longitudinal axis XI of the aircraft cabin 10. In addition, the extension axes X2 of two adjacent seats 13 of the central group 20 can cut the longitudinal axis XI of the aircraft cabin 10 substantially at the same point. Alternatively, the two laterally adjacent seats 13 can be offset relative to each other along the longitudinal axis XI, so that the extension axes X2 of the two laterally adjacent seats 13 intersect the longitudinal axis
    XI at different points.
    As is particularly illustrated in Figure 2a, each seat unit 12 comprises a seat 13 having a backrest 24, in particular adjustable in inclination, and a seat 25, in particular potentially adjustable in inclination. In addition, the seat 13 may include a leg rest (not shown), in particular adjustable in inclination. In addition, the seat unit 12 may include a footrest 27.
    The footrest 27 may consist of a fixed cushion, in particular arranged in a housing 29 dedicated to receive the feet of the passenger. Preferably, the footrest 27 is located in the extension of the seat 13 when the latter is in the berth position.
    The seat unit 12 may also include a side cabinet 32, which can in particular be used as a fixed shelf and / or as a storage for a meal shelf.
    The seat unit 12 may also include a fixed shell 33 capable of ensuring separation. Such a fixed shell 33 therefore makes it possible to guarantee the privacy of each passenger. Advantageously, in order to fulfill such a privacy guarantee function, the fixed shell 33 extends around the backrest 24 of the seat 13 in order to create an interior space, partially closed, in which the seat 13 is arranged.
    When two seat units 12 are arranged one behind the other, advantageously, the two seat units 12 are arranged so as to define a vertical overlap, at least partial, between them. The vertical overlap between the two seat units 12 may consist, as shown, in positioning the housing 29 of the footrest 27 of the rear seat unit 12 under the side cabinet 32 of the corresponding front seat unit 12 .
    There is also a seat unit 12 left in which the side cabinet 32 is disposed to the left of the seat 13 and a seat unit 12 right in which the side cabinet 32 is disposed to the right of the seat 13. A row 15a , 15b, 15c, 15d is formed by alternating seat units 12 left and seat units 12 right, so that each seat 13 of a rear seat unit 12 is located in front of a side cabinet 32 of the front seat unit 12 comprising the housing 29 of the corresponding footrest 27.
    As shown in particular in Figures 2a, 4, and 5, the arrangement 11 comprises at least a first set El of rear seat units comprising a first seat unit 12.1 and a second seat unit 12.2 located l 'next to each other. The seat units 12.1 and 12.2 of the assembly El belong to two different rows 15c, 15d. The seat units 12.1, 12.2 of the El assembly are joined laterally to one another by being contiguous or separated from each other by a maximum of a few centimeters.
    A second set E2 of front seat units comprises a first seat unit 12.1 and a second seat unit 12.2 located one next to the other. The seat units 12.1 and 12.2 of the assembly E2 belong to two different rows 15c, 15d. The seat units 12.1, 12.2 of the E2 assembly are joined laterally to one another by being contiguous or separated from each other by a maximum of a few centimeters.
    The seat units 12.1 and 12.2 of a given set El, E2 are of the same type, left or right.
    A central space 35 extends between the first set El of seat units and the second set E2 of seat units. This central space 35 extends along an axis X3 of the assembly El, in particular an axis of symmetry of the assembly El.
    In the embodiment of Figure la, the central space 35 is a passage for a person authorizing communication between the first seat unit 12.1 and the second seat unit 12.2 of the first set El. The central passage 35 extends between the shells 33 of the seat units of the assembly El and of the seat units 12 of the assembly E2. In this case, closing means 37 described in more detail below extend along a height of the seat in the deployed position.
    Alternatively, in the embodiment of Figure 1b, the central space 35 extends above a central piece of furniture 32 'continuous between the first set of El seat units and the second set of 'E2 seating units. In this case, the closure means 37 are arranged above the central cabinet 32 '.
    The closing means 37 arranged along the central space 35 are capable of ensuring the closing of the central space 35. Said closing means 37 at least partially flexible are movable between a stowed position in which the closing means 37 are released from the central space 35 and a deployed position in which the closing means 37 close off the central space 35. The closing means 37 then extend along the axis X3 of the assembly El. Consequently, the passenger seated in a seat 13 of the assembly El is separated from its immediate neighbor by the closing means 37. The passenger thus finds himself seated in an area of intimacy defined by the enclosed space thus created by the shell 33 and the closing means 37.
    In the embodiment of Figures 2a, 4, and 5, the closure means 37 comprise a curtain 39, in particular made of fabric, and a return device 40 of the curtain 39 in the stowed position. As can be seen in Figure 3, the curtain 39 may include a first part 39.1 made of a fine fabric, called the technical part, and a second part 39.2 made of thick material fixed on the first part
    39.1 by being, for example, sewn on this first part 39.1. The second part
    39.2 is thicker than the first part 39.1, this is the reason why the terms thin and thick must be understood relative to the thickness of these two parts 39.1 and 39.2. The second part 39.2 is called the aesthetic part because it may have patterns, such as the logo of an airline company. The second part
    39.2 could for example be made of fabric, alcantara, or leather to increase the perceived quality of the whole. The curtain 39 can be made at least in part from sound absorption material.
    In the embodiment of Figure 2a, the return device 40 comprises at least one elastic return member 41, such as a spring. In the example shown in FIG. 2b, two springs 41 are used, each fixed on the one hand to a set of seats E1 or E2 and on the other hand to the curtain 39. The curtain 39 can be deployed horizontally along the arrow FL [ The curtain 39 further comprises means 43 for holding said curtain 39 in the deployed position. As shown in FIG. 2c, these holding means 43 comprise for example a handle 44 forming a hook intended to cooperate with a fixed support, in particular in the form of a square. It is also possible to use one or more magnetic holding devices 45 in combination. The holding means 43 may comprise a mechanical fuse making it possible to release the central space 35 when a limit force is applied to the holding means 43. Alternatively, curtain 39 may include fusible seams.
    In the embodiment of Figure 4, the return device 40 comprises a reel 46 provided with an axis around which at least part of the curtain 39 is wound when the curtain 39 is in the stowed position.
    The reel 46 is arranged horizontally at the bottom, in particular on the floor. The reel 46 makes it possible to free up maximum space between the central passengers when the curtain 39 is down in the stowed position. Alternatively, the reel 46 extends over a central unit 32 'separating the seat units 12.1, 12.2 from the assembly El (cf. FIG. 1b).
    The reel 46 can integrate an electric motor 47 associated with a belt system.
    Vertical uprights 50 provide translational guidance of the curtain 39 from top to bottom and vice versa. The connection between the uprights 50 and the curtain 39 is of the male / female type, or is a slide connection, or is a toothed belt connection with pinion in the case of an electric motorization.
    A guide bar 51 can connect the curtain 39 to the uprights 50. The guide bar 51 extends horizontally at one end of the curtain 39. The curtain 39 can be deployed vertically in the direction of arrow F2.
    In the embodiment of Figure 5, the return device 40 comprises a reel 53. The reel 53 is arranged horizontally in the lower part. The roller 53 opens up a maximum of space between the central passengers when the curtain 39 is down in the stowed position.
    The reel 53 can integrate an electric motor 54 associated with a belt system.
    Vertical uprights 55 provide guiding in translation of the curtain 39 from top to bottom and vice versa.
    The connection between the uprights 55 and the curtain 39 is of the male / female type, or is a slide connection, or is a toothed belt connection with pinion in the case of an electric motor.
    Advantageously, the curtain 39 is housed in the stowed position in a rigid housing 57. This housing 57 extends horizontally along the axis X3 of the assembly El. This housing 57 extends projecting relative to the floor of the 'aircraft to form a wall of separation between passengers. This avoids interference between the feet of neighboring passengers. Unlike the embodiment of Figure 4, the curtain 39 is not wound in the stowed position but extends in a plane. The curtain 39 can be deployed vertically along arrow E3.
    As can be seen in Figure 6, the curtain 39 may include stiffening means 60, such as cords and / or rigid edges and / or a rigid or semi-rigid plate. These means 60 may extend along a contour of the curtain 39.
    In the embodiment of Figures 7a, 7b, and 7c, the curtain 39 incorporates means 61 for generating a light pattern. These means 61 may include a light source 62 and translucent wires 63 arranged in a thickness of the curtain 39, as illustrated in FIG. 7a, or a light panel 64, preferably flexible, placed inside or on the curtain 39, as illustrated in FIG. 7b. Alternatively, an assembly of lamps 65, in particular of the LED type, may be used, as illustrated in FIG. 7c. A configuration of perforations 66 made in the curtain 39 may allow the desired pattern to appear.
    In the embodiment of Figures 8 to 10, the closure means 37 comprise a semi-flexible curtain 39 having an alternation of vertical blades 67 and folding zones 68. The semi-flexible curtain 39 is foldable at least partly along zones 68.
    The semi-flexible curtain 39 is formed by a plurality of blades 67 spaced regularly between them and covered by fabric 69, the portions of the fabric extending between two adjacent blades 67 forming the folding zones 68. Glue 70 may be arranged between the blades 67 and over the entire contour of the fabric to ensure the assembly of two layers of fabric between which the blades 67 are held. The blades 67 may be made of a rigid or semi-rigid plastic material.
    As can be seen in Figure 9, we can use holding means 71 of the curtain 39 in the stowed position and in the deployed position, in particular of the magnetic type. It is thus possible to use a magnet 72 to make a magnetic bonding of the free end edge of the curtain 39 against a fixed metal support secured to a seat unit 12.
    The semi-flexible curtain 39 can be configured so that the vertical blades 67 are folded over one another in the stowed position, as shown in FIG. 10. The curtain 39 then has an accordion structure in which the blades 67 are superimposed on each other over the majority of their surface. As a variant, the blades 67 could be oriented horizontally.
    A closing device 37 'similar to the device 37 can be installed to removably close the passage on the side of the corridor 21, as shown in FIG. 2a.
    The invention may also be implemented with seats installed in other means of transport, such as for example bus, train, or boat seats.
    Obviously, the invention is not limited to the embodiments described above and provided only by way of example. It encompasses various modifications, alternative forms and other variants which a person skilled in the art may envisage within the framework of the present invention and in particular any combination of the different operating modes described above, which can be taken separately or in combination.
    权利要求:
    Claims (1)
    [1" id="c-fr-0001]
    claims [Claim 1] Seat arrangement (11), in particular intended to be installed in an aircraft cabin (10), characterized in that it comprises:- at least a first set (El) of seat units comprising a first seat unit (12.1) and a second seat unit (12.2) located one next to the other and respectively comprising a seat (13) able to move from a seated position to a berth position,- at least a second set (E2) of seat units comprising a first seat unit (12.1) and a second seat unit (12.2) located one next to the other and respectively comprising a seat (13) able to move from a seated position to a berth position,- a central space (35) extending between the first set of seat units (El) and the second set of seat units (E2),- And in that the arrangement of seats (11) comprises closing means (37) at least partially flexible, said closing means (37) being movable between a stowed position in which the closing means (37) are released from the central space (35) and a deployed position in which the closing means (37) close the central space (35). [Claim 2] Seat arrangement according to claim 1, characterized in that the central space (35) is a passage for a person authorizing communication between the first seat unit (12.1) and the second seat unit (12.2) of the first set ( El). [Claim 3] Seat arrangement according to claim 1, characterized in that the central space extends over a continuous central unit (32 ') between the first set of seat units (El) and the second set of seating units (E2). [Claim 4] Seat arrangement according to any one of claims 1 to 3, characterized in that the closing means (37) comprise a curtain (39), in particular made at least partly of fabric, and a return device (40) of the curtain (39) in the stowed position. [Claim 5] Seat arrangement according to claim 4, characterized in that it comprises means (43) for holding the curtain (39) in the deployed position, such as a handle (44) intended to cooperate with a support and / or a device magnetic (45). [Claim 6] Seat arrangement according to claim 4 or 5, characterized in that the return device (40) comprises at least one elastic member
    return (41), such as a spring. [Claim 7] Seat arrangement according to claim 4 or 5, characterized in that the return device (40) comprises a reel (46) provided with an axis around which at least part of the curtain (39) is wound when the curtain (39 ) is in the stowed position. [Claim 8] Arrangement according to claim 7, characterized in that the reel (46) is arranged horizontally in the lower part. [Claim 9] Arrangement according to claim 7 or 8, characterized in that the reel (46) incorporates an electric motor (47). [Claim 10] Arrangement according to any one of claims 7 to 9, characterized in that it comprises vertical uprights (50) ensuring guiding in translation of the curtain (39). [Claim 11] Arrangement according to claim 10, characterized in that it comprises a guide bar (51) connecting the curtain (39) to the vertical uprights (50). [Claim 12] Arrangement according to any one of claims 4 to 11, characterized in that it comprises a housing (57) in which the curtain (39) is housed in the stowed position. [Claim 13] Arrangement according to claim 12, characterized in that the housing (57) projects in relation to a floor of the aircraft. [Claim 14] Seat arrangement according to any one of claims 4 to13, characterized in that it comprises stiffening means (60) of the curtain (39), such as cords or a flexible plate. [Claim 15] Seat arrangement according to any one of claims 4 to 14, characterized in that it comprises means (61) for generating a light pattern. [Claim 16] Seat arrangement according to claim 15, characterized in that the means for generating (61) a light pattern comprise a light source (62) and translucent wires (63) arranged in a thickness of the curtain (39). [Claim 17] Seat arrangement according to claim 15 or 16, characterized in that the means for generating (61) a light pattern comprise a light panel (64) disposed inside the curtain (39). [Claim 18] Seat arrangement according to any one of claims 15 to 17, characterized in that the means for generating (61) a light pattern comprise an assembly of lamps (65), in particular of the LED type. [Claim 19] Seat arrangement according to any one of claims 1 to
    18, characterized in that the closing means (37) comprise a semi-flexible curtain (39) having alternating blades (67) and folding zones (68).
    [Claim 20] Seat arrangement according to claim 19, characterized in that it comprises means (71) for holding the curtain (39) semi-flexible in the stowed position and in the deployed position, in particular of the magnetic type.
    类似技术:
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    同族专利:
    公开号 | 公开日
    EP3802321A1|2021-04-14|
    FR3081835B1|2021-04-09|
    CN112236362A|2021-01-15|
    WO2019234041A1|2019-12-12|
    US20210221516A1|2021-07-22|
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    法律状态:
    2019-07-01| PLFP| Fee payment|Year of fee payment: 3 |
    2019-12-06| PLSC| Search report ready|Effective date: 20191206 |
    2021-05-19| PLFP| Fee payment|Year of fee payment: 4 |
    2021-09-03| CA| Change of address|Effective date: 20210730 |
    2021-09-03| CD| Change of name or company name|Owner name: SAFRAN SEATS, FR Effective date: 20210730 |
    优先权:
    申请号 | 申请日 | 专利标题
    FR1870648A|FR3081835B1|2018-06-05|2018-06-05|SEATING ARRANGEMENT, ESPECIALLY OF AN AIRCRAFT|FR1870648A| FR3081835B1|2018-06-05|2018-06-05|SEATING ARRANGEMENT, ESPECIALLY OF AN AIRCRAFT|
    US15/734,438| US20210221516A1|2018-06-05|2019-06-04|Device for closing a space within an airplane|
    EP19728070.4A| EP3802321A1|2018-06-05|2019-06-04|Device for closing a space within an airplane|
    CN201980037839.3A| CN112236362A|2018-06-05|2019-06-04|Device for closing a space in an aircraft|
    PCT/EP2019/064522| WO2019234041A1|2018-06-05|2019-06-04|Device for closing a space within an airplane|
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