• 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:
    Arrangement of seats (6) of a transport means with two parallel corridors (8, 10) oriented in the longitudinal direction of the car (2), two car walls (18, 20) parallel to the corridors (8, 10) ) laterally delimit the cabin (2), a central zone (16) between the corridors (8, 10) and two outer zones (12, 14) adjacent to the central zone (16). Rows of seats (26) have two inner seat modules (28) and two outer seat modules (30) in the central area (16). A plurality of second rows of seats (40) having an inner seat module (62) facing the respective lane (8, 10) and an outer seat module (60) facing the car wall (18, 20) are in outer areas (12, 14). Each seat module (28, 30) has a seat (32, 34) and associated meridian (36, 38). The modules (28, 30) of the central zone (16) have a direction of use parallel to the main direction of the corridor (8, 10), or at a maximum angle (a2) of 4 ° with respect thereto .
    公开号:FR3054525A1
    申请号:FR1757061
    申请日:2017-07-25
    公开日:2018-02-02
    发明作者:Martin Dipl.-Ing.Sieben；Thomas Dipl.-Ing. Sutthoff；Tobias Dipl. -Ing. Schmidt-Schaffer
    申请人:Airbus Operations GmbH；
    IPC主号:
    专利说明:

    054 525
    57061 ® FRENCH REPUBLIC
    NATIONAL INSTITUTE OF INDUSTRIAL PROPERTY © Publication number:
    (only to be used for reproduction orders) © National registration number
    COURBEVOIE © IntCI 8 : B 64 D 11/06 (2017.01)
    PATENT INVENTION APPLICATION
    A1
    ©) Date of filing: 25.07.17. © Applicant (s): AIRBUS OPERATIONS GMBH— DE. © Priority: 29.07.16 DE 102016114124.0. @ Inventor (s): DIPL.-ING.SIEBEN MARTIN, DIPL.- ING. SUTTHOFF THOMAS and DIPL. -ING. SCHMIDT- (43) Date of public availability of the SCHAFFER TOBIAS. request: 02.02.18 Bulletin 18/05. ©) List of documents cited in the report preliminary research: The latter was not established on the date of publication of the request. (© References to other national documents ® Holder (s): AIRBUS OPERATIONS GMBH. related: ©) Extension request (s): © Agent (s): CABINET HERRBURGER.
    FR 3 054 525 - A1 (£ 4) ARRANGEMENT OF SEATS OF A PASSENGER CABIN OF A MEANS OF TRANSPORT.
    ©) Arrangement of seats (6) of a means of transport with two parallel corridors (8, 10), oriented in the longitudinal direction of the cabin (2), two cabin walls (18,20) parallel to the corridors (8 , 10) laterally delimit the cabin (2), a central zone (16) between the corridors (8, 10) and two external zones (12, 14) adjacent to the central zone (16). Seat rows (26) have two interior seat modules (28) and two exterior seat modules (30) in the central area (16). Several second rows of seats (40) comprising an interior seat module (62) facing the respective aisle (8, 10) and an exterior seat module (60) facing the cabin wall (18, 20) are in the outdoor areas (12, 14).
    Each seat module (28, 30) has a seat (32, 34) and an associated chaise longue (36, 38). The modules (28, 30) of the central zone (16) have a direction of use parallel to the main direction of the corridor (8, 10), or making a maximum angle (a2) of 4 ° relative to the latter .

    Field of the invention
    The invention relates to an arrangement of seats in a cabin of a means of transport as well as such a cabin of means of transport and an aircraft equipped with such a cabin.
    State of the art
    In airliner cabins with different seat classes, it is possible, in addition to the simple passenger seats, to also place larger seat modules, consisting of a seat and a chaise longue. Often these seat modules can be configured as needed between a sitting position and a sleeping position. For the seating position, the seating surface of the seat is at a great distance from the meridian, while in the sleeping position, the seating surface, the meridian and possibly an additional seating element form a closed sleeping area. The integration of such seat modules requires, notably due to the length, a significantly larger mounting space than a simple passenger seat.
    Classes of seats are known with in the cabin, two parallel corridors, between which there is a central area for passengers, receiving these seat modules next to each other and several groups of two seat modules one behind others. In such an arrangement, the seat modules often make an angle with respect to each other, so that two seat modules side by side combine in a V-shape. In the laterally outer areas between the cabin wall and the corridor, there are arrangements with individual seating modules one behind the other. In the longitudinal direction of the cabin, often with their meridian, these seats protrude more in the corridor than with the corresponding seat. Each of these seating modules is therefore directly accessible from an adjacent hallway.
    For example, document DE 11 2009 002 229 T5 proposes a system of passenger seats with an integrated multifunctional piece of furniture, showing a compact integrated combination of several following seat modules, which protrude into a corridor with their meridian respectively.
    Document US 2015/0166182 A1 shows a similar variant, in which the seat modules, also with their meridian, are diverted from the corridor.
    Document EP 1 364 874 B1 shows individual modules for airplane passengers, comprising a seat, armrests, a facing element and a side wall spaced from the seat and extending between one side of the seat and one side. the layout element, thereby defining an elongated shape with a first end and a second end; the seat is located at the wide end and the fitting element is located at the narrow end, an access opening is provided opposite the side wall between the ends.
    Document EP 2 303 692 B1 shows a seat module for an airplane passenger, having a seat comprising a horizontal cushion and a backrest as well as a partition wall, which extends along at least one side of the seat ; the seat is designed to be movable between an upright position, in which the seat backrest is approximately vertical, and a pivoted rear position, in which the backrest lies in the plane which extends approximately vertically to the partition wall.
    Document EP 2 783 985 A1 shows an arrangement comprising several seats which, by displacement of the seat cushion and the backrest, can be converted between a sitting configuration and an elongated configuration.
    The use of such seating modules, with seat and chaise longue, undoubtedly considerably increases passenger comfort. However, the comparatively more efficient integration from the point of view of mounting space only allows the installation of a few passengers per unit of area in a given cabin section. This influences the profitability of the means of transport and the costs for each passenger.
    Purpose of the invention
    The object of the invention is to obtain a more efficient use of the mounting space in a cabin section of a means of transport without restricting the comfort of the passengers with such seat modules, but by increasing profitability.
    Presentation and advantages of the invention
    To this end, the subject of the invention is an arrangement of cabin seats of a means of transport, having two corridors spaced apart and parallel to each other, oriented in the longitudinal direction of the cabin, two cabin walls spaced from each other, oriented at least in sections, parallel to the corridors and laterally delimiting the cabin, a central zone for passengers between the corridors, two external zones for passengers, adjacent to the central zone, from which they are separated respectively by one of the corridors and are adjacent to one of the two cabin walls.
    Several first rows of seats respectively comprising two interior seat modules and two exterior seat modules are arranged one behind the other in a longitudinal direction in the central area, several second rows of seats respectively comprising an interior seat module facing the corridor and an exterior seat module facing the cabin wall are arranged one behind the other in a longitudinal direction, in the exterior zones, each seat module has a seat and a meridian associated with the seat, and the seat modules of the central zone have a direction of use parallel to the main direction of the adjacent corridor, or making a maximum angle of 4 ° with respect to this direction, so that the meridian of the respective seat module protrudes more in the corridor than the corresponding seat .
    In other words, the invention provides an arrangement of seats for a cabin of a means of transport; this seating arrangement has two corridors spaced from each other and extending parallel to each other; the corridors are oriented in a longitudinal direction of the cabin and two cabin walls spaced from one another, oriented parallel to the corridors at least in sections, delimit the cabin laterally; a central passenger area is located between the corridors, and two exterior passenger areas, adjacent to the central section, are separated from the central passenger area by one of the corridors respectively and are adjacent to one of the two walls of cabin. Several first rows of seats comprising two central seat modules and two exterior seat modules are arranged one behind the other in the central passenger area in the longitudinal direction; several second rows of seats respectively comprising an interior seat module facing the respective aisle and an exterior seat module facing the respective cabin wall in the exterior passenger areas are arranged one behind the other in longitudinal direction, each module seat has a seat and a chaise longue associated with the seat.
    The seating arrangement is therefore designed for cabins having a relatively large width, so that it can be used for example in "wide body" aircraft. Such cabins are distinguished by the longitudinal corridors crossing practically the entire interior space of the aircraft. For example, this could relate to an aircraft of type A350 or an aircraft with a similar structure and a cabin with a cabin width of about 5.5 m or more.
    As shown, a seat module can be a unit or a combination of a passenger seat and a chaise longue, which greatly increases individual passenger comfort. In a seat position of the seat module, an intermediate space remains free between the front edge of the seat and the meridian, so that the passenger can sit comfortably on the seat with sufficient freedom of movement of the legs and, if necessary he can put his feet on the meridian. For the sleeping position, it is possible, with pivoting and displacement mechanisms integrated in the seat module, to transform the meridian and the seat into a closed sleeping surface.
    It is understood that, in particular when getting into the means of transport and during the journey, the passenger installed in a seat module must be disturbed as little as possible. For this, when using two seat modules one next to the other, of which only one seat module is adjacent to a corridor, it prevents the crossing of the seat module facing the corridor. This is possible if the gap available on a corridor side between two successive seat modules allows this intermediate space to be crossed. Thus, a passenger can, from the corridor, access a seat module not facing the corridor, without passing through the seat module facing the corridor.
    Implicitly, it is also determined, due to the embodiment defined above, that the two seat modules concerned, arranged side by side, have one with respect to the other a shift in the longitudinal direction. If a passenger crosses the space between two successive seat modules, located on a corridor side, he arrives at an area, diverted from the passenger seat and the meridian, from the diverted seat module from the corridor. A shift in the longitudinal direction makes it possible to reach the corridor between the successive seat modules, located on the side of the corridor, and the intermediate space between the seat and the meridian of the seat module not turned towards the corridor. The use of the mounting space in the means of transport is thus considerably improved, since it is possible to have seat modules not turned towards the corridor that the passenger can reach directly from the corridor without disturbing the passenger installed on a module seat directly connected to the corridor.
    It is preferred that the seat modules of the central passenger area have a direction of use parallel to the main direction of the adjacent corridor or which makes a maximum angle of 4 ° so that the meridian of the respective seat module exceeds more in the hallway than the seat. In particular in combination with a direction of use of the seat modules adjacent to the respective corridor, which essentially coincides with the main direction of the respective corridor, it is possible to decouple the adjacent seat modules in order to improve the private sphere of the passengers concerned. The angle formed between the direction of use and the main direction of the corridor creates a gap between the meridian and the outer seat module, that is to say the seat module facing the corridor, relative to the module of interior seat module seat not facing the corridor.
    It is advantageous to provide a gap of at least 20 cm between the meridian of a seat module facing a corridor and the seat of a seat module located in front, in the longitudinal direction; this gap makes it possible to reach, from the corridor, the seat module not turned towards the corridor. The gap between the successive seat modules must be sufficient to reach the seat module not turned towards the corridor. A 20 cm limit is considered a minimum limit. It is preferable that the distance between the successive seat modules is greater so as not to excessively restrict comfort when the seat module is occupied. For example, consider a gap of 9 inches (approx. 23 cm) or more.
    In an advantageous embodiment, the seats of two neighboring seat modules are offset from one another in the longitudinal direction. The dimension of the offset depends on the design of the space between the seat modules spaced from each other on a corridor side. The passage can be inclined relative to the main extension direction of the corridor; this tilt is different from 90 degrees. The choice of this angle determines the passenger's direction of travel from the corridor through the passage, which consequently determines the advantageous access point to the exterior seat module. This in turn determines the length offset of the seats of the neighboring seat modules.
    In an advantageous embodiment of a seating arrangement, the seats of the outer seating modules of the central area have a maximum offset of 30 cm, preferably a maximum of 25 cm. Such an offset may be the minimum offset which allows access from a corridor to a seat module remote from the corridor.
    The seats of interior seat modules in the exterior areas can however be offset by at least 40 cm, preferably by at least 50 cm. The greater offset than in the central area improves access and service to a seat module oriented towards the cabin wall, or to a window. This optimizes the distance between the corridor and the seat module, available under the storage compartments located above the head, laterally, often placed lower. This can in particular be obtained by a simultaneous enlargement of the V position of the seat modules. The useful oblique position, more marked for this purpose, of the interior seat modules, which are located against the corridor concerned, will be explained below. In addition, in combination with a movable meridian support of the seat modules adjacent to the corridors, it is possible to obtain a wider corridor and also, in all, more usable corridor surface.
    In an advantageous embodiment, a passage area is formed between two successive interior seat modules in an exterior passenger area or two successive exterior seat modules in the central passenger area; this passage area forms, with the main direction of the adjacent corridor, an angle in the range of 45 ° to 135 °. Consequently, the passage can not be crossed perpendicularly from the corridor but at an angle differentiating up to 45 ° in the direction of main extension or vice versa to the direction of main stretch. Preferably, the angle is in a range of 65 ° to 115 °, and particularly preferably in a range of 75 ° to 105 °. An offset between two seat modules, side by side, can be designed so that the outer seat, i.e. the seat not turned towards the corridor, is more offset along the main direction of the corridor or vice versa to the main direction of the corridor, so that a passenger, after crossing the passage, can reach the intermediate space between the seat and the meridian of the exterior seat module. In order to emphasize the orientation of this passage, the shape of the meridians and / or the backrests and / or the covering shell of the passenger seat of the adjacent seat modules is adapted.
    Likewise, the interior seat modules of the exterior passenger area may have a direction of use which makes an angle of at least 4 ° with respect to the main direction of the adjacent corridor. The meridian of the interior seat module of the exterior passenger area may likewise protrude more in the adjacent hallway than the corresponding seat.
    Preferably, the meridians of the seat modules adjacent to a corridor have a mounting depth which decreases from the corridor to the seat module not turned towards the corridor. There is thus a further improvement in the efficiency of the exploitation of the space because the sleeping surface is as large as possible with a diagonal exploitation of the seat module, using in combination both the maximum depth of the meridian and diagonal sleeping. It is not necessary to have a sleeping area if possible large, having continuously the greatest possible length because it would in any case be exploited only by a minimal part of the passengers. This variant is used for the advantageous design of a passage between two seat modules located one behind the other.
    In a particularly advantageous embodiment, the minimum usable width of the corridors is at least 15 inches (approx. 38 cm) and preferably at least 16 inches (approx. 40.6 cm) which allows the passage of a trolley with maximum dimensions according to the Atlas standard, having a width of approximately 31 cm. However, due to the partially oblique direction of use of the seat modules connected to the corridor, there is a clearance space if two people must be able to meet in the corridor. It is then possible to use the passage zones between the seat modules arranged one behind the other.
    In a preferred embodiment, at least the meridians of the seat modules adjacent to the corridor have a base attached to the cabin floor and a support movable relative to the base; in the seating position of the first seat, the support is held on the base in a retracted position, in which the support protrudes as far as possible beyond the base, and, in the sleeping position, the support projects in the adjacent hallway. During the phases of service in the means of transport, during which there is no catering service or without significant passenger traffic in the corridors, the width of the corridors can be reduced without restricting comfort in the means of transport. We can consider bringing the supports for the meridians a distance of up to two inches or more depending on their initial width.
    The support is held on the base, for example, by a passive mechanical device with a spring device and designed to be pressed into an extended position by means of a seat cushion pushed towards the meridian. The making of the chaise longue can thus be very simple, without costly active control.
    As a variant, the support is held on the base by an active mechanical device having at least one actuator and which, when the seat cushion slides, is moved to the extended position or to the retracted position. We can thus obtain more complex movements as well as greater freedom of movement for the sitting position.
    Preferably, in the extended position, the support projects in the first corridor up to a distance of four inches, and more preferably up to a distance of two inches. The initial width of the corridor can be approximately 18 inches. When the media is moved down the hallway, the width of the media is reduced to approximately 16 inches.
    It is advantageous that two neighboring seat modules have a degree of overlap between 25% and 75% in the longitudinal direction. The length offset may be more marked in the outer areas than in the central area. The degree of overlap can therefore be greater in an outdoor area than in the central area.
    The invention further relates to a means of transport having a fuselage with a cabin comprising an arrangement of seats according to the preceding description, the means of transport being in particular an airplane.
    Drawings
    The present invention will be described below in more detail with the aid of exemplary embodiments shown in the accompanying drawings in which:
    FIG. 1 schematically shows an arrangement of seats in an aircraft cabin, FIG. 2 represents a detail of FIG. 1 in a top view, FIG. 3 shows the structure of an arrangement of seats in a three-dimensional representation, ίο Figure 4 shows the combination of a chaise longue and the seat surface of a seat module in the sleeping position, Figure 5 shows an aircraft with a cabin equipped with the arrangement of seats according to invention.
    Description of embodiments
    Figure 1 shows the cabin 2 of an aircraft fuselage 4 having a seating arrangement 6. The seating arrangement 6 has a first corridor 8, a second corridor 10, a first exterior passenger area 12 (hereinafter first external zone 12), a second external passenger zone 14 (hereinafter second external zone 14) as well as a central passenger zone 16 (hereinafter central zone 16). The two corridors 8 and 10 extend parallel to the longitudinal direction x of the cabin 2, are spaced from each other on either side of the central zone 16. The first external zone 12 is between the cabin wall 18 left, in the direction of flight, and the first aisle 8. Similarly, the second exterior zone 14 is between the second aisle 10 and the cabin wall 20 right in the direction of flight. For example, the seating arrangement 6 has two seating arrangement sections 22 and 24, separated from each other in the longitudinal direction x, which are, for example, identical. They can be separated from each other by partitions or fixed elements.
    The central area 16 has several first rows of seats 26 one behind the other, having respectively two interior seat modules 28 and two exterior seat modules 30. Each of the seat modules 28, 30 has a seat 32, 34 and a meridian 36, 38 associated with the seat 32, 34. A seat module 28, 30 thus provides a comfortable seat with the possibility of placing the feet on the support of a meridian 36, 38. For better comfort, it is also possible to provide a sleeping surface in combination with seat elements 32, 34.
    The outer zone 12, 14 has several second rows of seats 40 which also consist of a seat 32, 34 and a meridian 36, 38, forming an interior seat module 62 adjacent to the corridor 8, 10 and a module outer seat 60 turned in the other direction. The practical arrangement of these components with respect to each other is illustrated on an enlarged scale in the following figures.
    The second rows of seats 40 are characterized in that the seat module 60 disposed against the cabin wall 18, 20 is turned only slightly outward relative to the longitudinal direction x or parallel to this direction. The direction of use of the seat module 62 connecting to the corridor 8 10 is turned inwards by an angle al towards the respective corridor 8, 10. The angle al is at least 4 °. Consequently, two neighboring seat modules 60 and 62 of an external zone 12, 14 form a slightly V-shaped position between them; this widening of the V is towards the longitudinal direction x.
    This is also the case for the left half and the right half of the central zone 16, that is to say that the directions of use of the seat modules 28 and 30 of each of these two halves widen slightly to their direction of use, that is to say that they form a slightly V-shaped position. While the interior seat modules 28 are preferably parallel to the longitudinal direction, the exterior seat modules 30 make an angle a2 with respect to the longitudinal direction; this angle is at most 4 °, preferably at most 2 °.
    In addition, the seat modules connecting to a corridor 8, 10 are separated from the seat module placed in front in the longitudinal direction x; this gap, between two seat modules adjacent to a corridor, gives access to a seat module located outside or in the middle of the cabin. The seats 32 and 34 are offset from each other in the longitudinal direction so that the space between the seat and the chaise longue is easily accessible from the corridor.
    Figure 2 shows a detail of Figure 1 in top view, in the direction of flight, for only the left half of the seating arrangement 6, which is symmetrical with respect to the central axis C. A first module interior seat 42 directly adjacent to the central axis C has a seat 32 parallel to the central axis C or only slightly turned. The seat surface of the first seat 32 has, for example, a seat width of 20 inches (approx. 50.8 cm) and is protected rearward, on a rear side, by a seat shell 44 .
    A first meridian 36 is associated with the seat 32, the first seat 32 and the first meridian 36 can be configured between a sitting position (as shown in FIG. 2) and a sleeping position (not shown). In the sitting position, there is a free space between the first seat 32 and the first meridian 36.
    The first meridian 36 has, for example, a support 48 housed in a manner movable by the passenger of the first seat 32. The support 48 may have a variable deviation from the central axis C.
    Adjacent to the first interior seat module 42 is disposed a first exterior seat module 50, having a second seat 34 with which is associated a meridian 38. The second seat 34 offset from the first seat 32 by a minimum distance in the longitudinal direction is directly adjacent to the first corridor 8. The second seat 34 can have a shape essentially symmetrical to that of the first seat 32; it is also protected by a seat shell 52 surrounding the second seat 34 and transforming into a lateral shell 54 extending to the second meridian 38. The first lateral shell 44 surrounds the first seat 32 and arrives in a first shell lateral 45 rectilinear, extending to the first meridian 36. Thus, the two seat modules 42 and 50 provide good protection and create an intimate sphere, the best possible.
    The second meridian 38 can also have a mobile support 56 with a variable deviation from the first corridor 8.
    As can be seen from the example, several first seat modules 42, several second seat modules are arranged one behind the other in the longitudinal direction. Between a seat shell 52 and the front edge 58 of the second meridian 38, there is a gap, for example 9 inches (approx. 22.9 cm) which allows a passenger to arrive at the first seat module 42 from the first corridor 8. The front edge 58 of the second meridian 38 is coupled so as not to extend perpendicular to a main direction of extension of the first corridor 8 but with an angle, for example 15 degrees in the opposite direction from the direction of flight. The second seat shell 52 is adapted and therefore extends asymmetrically.
    Thanks to the interval not perpendicular to the corridor 8, the offset between the first seat 32 and the second seat 34 allows direct access to the intermediate space 46 between the first seat 32 and the first meridian 36 from the corridor 8. Thus a passenger occupying the second seat module 50 will not be disturbed and the cabin crew can also very easily reach the passenger of the first seat module 42.
    A similar organization is that of the side passenger area 12, in which a third seat module 60 is placed against a cabin wall 18 not shown here. This third seat module 60 also has a first seat 34 and a first meridian 38, corresponding to those of the first seat module 50. A fourth seat module 62 is placed directly adjacent to the third seat module 60 and it is adjacent at the first corridor 8. Here, a seat 32 is used as well as an exemplary symmetrical meridian 56 plane, in the form of a meridian 64. The seats 32 and 34 are offset approximately by the depth of a seating surface. The direction of use of the fourth seat module 62 is offset, for example, by 7 ° from the longitudinal direction x, so that the meridian 64 projects more into the corridor 8 than the seat 32.
    To delimit the fourth seat module 62 and the third seat module 60, a shell 44 surrounds the seat 32 and arrives at the back shell 42 of the seat 34. The latter surrounds the seat 34 and is transformed into an additional shell part 66 extending to the meridian 64 of the fourth seat module 62. The direction of use of the third seat module 60 is slightly turned towards the cabin wall 18.
    Due to the movable support 56, 68, which can be pulled out, the meridians 38 and 64 adjacent to the corridor, the width of the corridor 8 can be reduced, for example from 18 inches to 16 inches. However, this does not restrict passenger comfort. If it should be necessary, in the corridor, to avoid a person coming in front, a service trolley or the like, it is possible to wait in the intermediate spaces between two seat modules until the other person or the service cart has passed.
    FIG. 3 shows a three-dimensional representation of the total structure, highlighting in particular the extension in height of the meridians 36, 38 and 63. In particular the supports 48, 56, 68 are at a certain distance above the cabin floor 70, which considerably reduces any discomfort for passengers or on-board staff moving in corridor 8.
    FIG. 4 shows an example of the combination of a support 72 with a meridian 74 and a seating surface 76, together forming a sleeping surface with the backrest (not shown). The support 72 is movable between a rest position (shown in dashes) 78 and a use position 80. The movement can be carried out either actively by mechanical drive means or passively by pushing the support 72 to pass from the rest position 78 to the use position 80 using the front edge 82 of the seat part 76. The particular advantage lies in the fact that in the seated position, the support 72 protrudes as little as possible in the corridor 8, but that in a position of use, it can offer a maximum sleeping length. The height of the support 72 adjacent to the corridor preferably has a height, for example, of a maximum of 25 inches (approximately 63.5 cm). If this is met, there will be a minimum lane width of 15 inches (approximately 38 cm) based on the relevant admission provisions.
    Figure 5 shows an aircraft 84 with a fuselage 86 and a cabin 88 having a seating arrangement as described above.
    权利要求:
    Claims (15)
    [1" id="c-fr-0001]
    1 °) Arrangement of cabin seats (6) (2) of a means of transport, having:
    two lanes (8, 10) spaced apart and parallel to each other, oriented in the longitudinal direction of the cabin (2), two cabin walls (18, 20) spaced from each other, oriented to the less in sections, parallel to the corridors (8, 10) and laterally delimiting the cabin (2), a central zone for passengers (16) between the corridors (8, 10), two exterior zones for passengers (12, 14), adjacent to the central area (16), from which they are separated respectively by one of the corridors (8, 10) and are adjacent to one of the two cabin walls (18, 20), arrangement in which several first rows of seats (26 ) comprising respectively two interior seat modules (28, 42) and two exterior seat modules (30, 50) are arranged one behind the other in a longitudinal direction in the central area (16), several second rows of seats (40) comprising respectively an interior seat module (62) turned towards the corridor (8, 10) and an external seat module (60) facing the cabin wall (18, 20) are arranged one behind the other in a longitudinal direction, in the external zones (12, 14), each seat module (28, 30, 42, 50, 60, 62) has a seat (32, 34) and a meridian (36, 38) associated with the seat (32, 34), and the seat modules (28, 30 , 42, 50) of the central zone (16) have a direction of use parallel to the main direction of the adjacent corridor (8, 10), or making a maximum angle (a2) of 4 ° relative to this direction, of so that the meridian (36, 38) of the respective seat module (28, 30, 60, 62) protrudes more in the corridor (8, 10) than the corresponding seat (32, 34).
    [2" id="c-fr-0002]
    2 °) arrangement of seats according to claim 1, wherein a gap of at least 20 cm is formed between a meridian (36, 38) of a seat module (30, 50, 62) facing the corridor (8 , 10) and the seat (32, 34) of a seat module (30, 50, 62) lying in front in the longitudinal direction, this gap making it accessible from the corridor (8, 10), the seat module (28 , 60) not facing the corridor (8, 10).
    [3" id="c-fr-0003]
    3 °) arrangement of seats (6) according to claim 1 or 2, wherein the seats (32, 34) of two adjacent seat modules (28, 30, 42, 50, 60, 62) are offset one by relative to each other in the longitudinal direction.
    [4" id="c-fr-0004]
    4 °) arrangement of seats (6) according to any one of claims 1 to 3, wherein the seats (32, 34) of an outer seat module (30, 50) of the central area (16) have a maximum offset of 30 cm, preferably maximum of 25 cm.
    [5" id="c-fr-0005]
    5 °) arrangement of seats (6) according to any one of the preceding claims, in which the seats (32, 34) of an interior seat module (62) of the exterior zones (12, 14) have an offset of at least 40 cm, preferably at least 50 cm.
    [6" id="c-fr-0006]
    6 °) arrangement of seats (6) according to any one of the preceding claims, in which a passage is formed between two interior seat modules (62) succeeding one another in an exterior area (12, 14) or two exterior seat modules (30, 50) succeeding each other in the central zone (16), this passage forming with the main direction of the adjacent corridor (8, 10), an angle in a range of 45 ° to 135 °.
    [7" id="c-fr-0007]
    7 °) arrangement of seats (6) according to any one of the preceding claims, in which the interior seat modules (62) of the exterior zones (12, 14) respectively have a direction of use which forms an angle (a 1) at least 4 ° from the main direction of the corridor (8,
    10).
    [8" id="c-fr-0008]
    8 °) arrangement of seats (6) according to any one of the preceding claims, in which the meridians (36, 38) of the seat modules (30, 50, 62) adjacent to a corridor (8, 10) have a depth mounting which decreases from the corridor (8, 10) towards the seat module (28, 42, 60) not turned towards the corridor (8, 10).
    [9" id="c-fr-0009]
    9 °) arrangement of seats (6) according to any one of the preceding claims, in which the minimum usable width of the corridors (8, 10) is at least 15 inches (approx. 38 cm) and preferably at least minus 16 inches (approx. 40.6 cm).
    [10" id="c-fr-0010]
    10 °) arrangement of seats (6) according to any preceding claim wherein the meridians (36, 38) at least seat modules (30, 50, 62) adjacent to one of the corridors (8, 10 ) have a base which can be attached to the cabin floor (70) and a support (48, 56, 68, 72) movable relative to the base, the support (48, 56, 68, 72), in a position d seat of the corresponding seat (32, 34) is held on the base in a retracted position, the support (48, 56, 68, 72) protrudes as far as possible beyond the base, and the support (48, 56 , 68, 72), in a sleeping position, projects into the adjacent corridor (8, 10).
    [11" id="c-fr-0011]
    11 °) arrangement of seats (6) according to claim 10, wherein the support (48, 56, 68, 72) is held on the base by means of a passive mechanical device having a spring arrangement and it is adapted to be pressed into an extended position by means of a seat cushion (32, 34) moved to the meridian (36, 38).
    [12" id="c-fr-0012]
    12 °) arrangement of seats according to claim 10 or 11, wherein the support (48, 56, 68, 72) is held on the base by means of an active mechanical device having at least actuator, movable in a position exit or return when moving the cushion of the seat concerned (32, 34).
    [13" id="c-fr-0013]
    13 °) arrangement of seats according to any one of claims 10 to 12, wherein the support (48, 56, 68, 72), in the extended position, protrudes up to a distance of four inches and preferably up to a disîo tance of two inches in an adjacent corridor (8, 10).
    [14" id="c-fr-0014]
    14 °) means of transport (84) having a fuselage with a cabin comprising an arrangement of seats (6) according to any one of claims 1 to 13.
    [15" id="c-fr-0015]
    15 °) means of transport (84) according to claim 14 which is an airplane.
    30 10 28/34 30
    CD
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    同族专利:
    公开号 | 公开日
    US10899455B2|2021-01-26|
    FR3054525B1|2021-05-14|
    DE102016114124A1|2018-02-01|
    US20180029712A1|2018-02-01|
    引用文献:
    公开号 | 申请日 | 公开日 | 申请人 | 专利标题
    DE19983643T1|1998-10-15|2002-01-31|British Airways Plc Harmondswo|seating unit|
    FR2839947B1|2002-05-22|2004-11-26|Airbus|INDIVIDUAL MODULE FOR AIRCRAFT PASSENGER|
    FR2934564B1|2008-08-01|2011-05-06|Airbus|SEAT MODULE FOR PASSENGER AIRCRAFT|
    FR2935684B1|2008-09-10|2011-05-13|Airbus|PASSENGER SEAT SYSTEM INTEGRATING MULTI-FUNCTIONAL FURNITURE, AND AIRCRAFT COMPRISING SUCH A SYSTEM|
    US8944379B2|2011-10-28|2015-02-03|Zodiac Seat Shells Us Llc|Aircraft seating configuration|
    US9527592B2|2012-07-06|2016-12-27|Zodiac Seats France|High end business class cabin arrangement|
    GB201217319D0|2012-09-27|2012-11-14|Acumen Design Associates Ltd|Aircraft passenger seating arrangement|
    FR3003540B1|2013-03-25|2015-05-29|Eads Sogerma|ARRANGEMENT OF CONVERTIBLE SEATS IN LAYERS|
    EP2974961B1|2014-07-15|2017-04-26|Airbus Defence and Space GmbH|Seat assembly, seat arrangement and passenger cabin for an aircraft|
    US10569884B2|2015-11-11|2020-02-25|Rockwell Collins, Inc.|Aircraft passenger seat with enhanced lie flat position spacing|DE102015105540A1|2015-04-10|2016-10-13|Airbus Operations Gmbh|Space-optimized passenger seat arrangement for a vehicle cabin|
    DE102015105539A1|2015-04-10|2016-10-13|Airbus Operations Gmbh|Space-optimized passenger seat arrangement for a vehicle cabin|
    US20190308730A1|2018-04-06|2019-10-10|B/E Aerospace, Inc.|Aircraft passenger seating unit and passenger seating arrangement|
    DE102018133541A1|2018-12-21|2020-06-25|Recaro Aircraft Seating Gmbh & Co. Kg|Airplane seat assembly|
    法律状态:
    2018-07-25| PLFP| Fee payment|Year of fee payment: 2 |
    2019-07-19| PLFP| Fee payment|Year of fee payment: 3 |
    2020-07-21| PLFP| Fee payment|Year of fee payment: 4 |
    2020-10-16| PLSC| Search report ready|Effective date: 20201016 |
    2021-07-28| PLFP| Fee payment|Year of fee payment: 5 |
    优先权:
    申请号 | 申请日 | 专利标题
    DE102016114124.0A|DE102016114124A1|2016-07-29|2016-07-29|Seat arrangement for an interior or a passenger cabin of a means of transport and a corresponding means of transport|
    DE102016114124.0|2016-07-29|
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