EP4126671A1

EP4126671A1 - Aircraft seat assembly

Info

Publication number: EP4126671A1
Application number: EP21715493.9A
Authority: EP
Inventors: Tim Manson; Christophe DUCREUX
Original assignee: Recaro Aircraft Seating GmbH and Co KG
Current assignee: Recaro Aircraft Seating GmbH and Co KG
Priority date: 2020-03-26
Filing date: 2021-03-18
Publication date: 2023-02-08
Also published as: WO2021191056A1; US20230257123A1; DE102020108436A1

Abstract

The invention relates to an aircraft seat assembly (14a; 14b; 14c; 14d) comprising at least one aircraft seat device (46a; 46b; 46c; 46d) and at least one additional aircraft seat device (48a; 48b; 48c; 48d) which are arranged at least partly next to one another in at least one common column of seats(36a; 36b; 36c; 36d) and each of which can be adjusted between a sitting position and a lying position. According to the invention, the lying direction (64a; 64b; 64c; 64d) of the at least one aircraft seat device (46a; 46b; 46c; 46d) is oriented in the opposite direction to another lying direction (96a; 96b; 96c; 96d) of the at least one other aircraft seat device (48a; 48b; 48c; 48d).

Description

Aircraft seating arrangement

State of the art

The invention relates to an aircraft seat arrangement according to the preamble of claim 1.

An aircraft seat arrangement with at least one aircraft seat device and with at least one further aircraft seat device, which are arranged at least partially next to one another in at least one common seat gap and which are each adjustable between a seated position and a reclining position, has already been proposed.

The object of the invention is preferably to provide a generic device with improved properties in terms of compactness and convenience. The object is achieved according to the invention by the features of claim 1, while advantageous configurations and developments of the invention can be found in the subclaims.

Advantages of the invention

The invention is based on an aircraft seat arrangement with at least one aircraft seat device and with at least one further aircraft seat device, which are arranged at least partially next to one another in at least one common seat gap and which are each adjustable between a seated position and a reclining position.

It is proposed that a lying direction of the at least one aircraft seat device is oriented opposite to a further lying direction of the at least one further aircraft seat device. By an inventive Embodiment, an advantageously compact and comfortable arrangement of the at least one aircraft seat device and the at least one further aircraft seat device can be achieved. Furthermore, the at least one aircraft seat device and the at least one further aircraft seat device can be positioned particularly advantageously with respect to one another through the configuration according to the invention. As a result, an available space in an aircraft cabin can advantageously be used efficiently. The aircraft seat arrangement is preferably provided for use in an aircraft cabin of an aircraft. The aircraft cabin is preferably intended for all passengers to stay during a flight, preferably independently of a booked seat class. A seat class is designed, for example, as an economy class, as a premium economy class, as a business class or as a first class. The aircraft cabin preferably has at least one aircraft cabin section, preferably along a longitudinal axis of the aircraft. The aircraft seat arrangement is particularly preferably arranged in the at least one aircraft cabin section. The at least one aircraft cabin section is preferably delimited by at least one partition element, preferably a partition or a curtain, and / or by at least one aircraft cabin module, preferably a kitchen module or a toilet module, along a longitudinal axis of the aircraft. A seat class can preferably be arranged in several aircraft cabin sections. The aircraft cabin preferably has a central axis of the aircraft cabin. The aircraft cabin center axis preferably has the same spacing from opposite aircraft cabin outer walls of the aircraft cabin. The aircraft cabin center axis is preferably aligned parallel to a roll axis of the aircraft. The aircraft cabin center axis is preferably aligned parallel to an aircraft cabin floor of the aircraft cabin. An “aircraft longitudinal axis” should preferably be understood to mean an axis which extends in the direction of the greatest extent of the aircraft cabin and which is arranged within the aircraft cabin. The longitudinal axis of the aircraft is preferably aligned parallel to the central axis of the aircraft cabin. The aircraft preferably has a direction of flight in at least one operating state. Preferably, the direction of flight, preferably in an ideal operating state, is aligned parallel to the aircraft cabin central axis and / or to a longitudinal axis of the aircraft. The aircraft cabin preferably has at least one aircraft cabin aisle. The at least one preferably extends Aircraft cabin aisle at least substantially along a longitudinal axis of the aircraft. The at least one aircraft seat device and the at least one further aircraft seat device are preferably provided to be raised on the aircraft cabin floor of the aircraft cabin. “Provided” should preferably be understood to mean specially designed and / or equipped. The fact that an object is provided for a specific function should preferably be understood to mean that the object fulfills and / or executes this specific function in at least one application and / or operating state. A “seat gap” should preferably be understood to mean an area in the aircraft cabin in which several aircraft seat devices are arranged one behind the other, viewed along an aircraft longitudinal axis, the area being delimited by an aircraft cabin aisle and another aircraft cabin aisle or by an aircraft cabin outer wall of the aircraft cabin. The at least one seat gap preferably extends in the direction of flight. The at least one aircraft seat device and the at least one further aircraft seat device are preferably arranged at least partially next to one another in the at least one common seat gap. Particularly preferably, exactly two aircraft seat devices are arranged directly next to one another in the at least one common seat gap, namely the at least one aircraft seat device and the at least one further aircraft seat device. The at least one aircraft seat device and the at least one further aircraft seat device are preferably arranged, preferably in a single seat column, orthogonally to the longitudinal axis of the aircraft, at least partially overlapping one another. “Arranged next to one another” should preferably be understood to mean that an axis, which is aligned parallel to the aircraft cabin floor and perpendicular to a longitudinal axis of the aircraft, intersects at least one aircraft seat device and the at least one further aircraft seat device. Particularly preferably, the at least one aircraft seat device and the at least one further aircraft seat device are arranged directly adjacent to one another in the at least one seat gap. The at least one aircraft seat device preferably forms an aircraft seat area and the at least one further aircraft seat device forms a further aircraft seat area. An “aircraft seat area” should preferably be understood to mean an area that a passenger in the aircraft cabin has personally available, preferably while the passenger is using the at least one aircraft seat device, preferably all parts of the at least one Aircraft seat device are arranged in the aircraft seat area. The at least one aircraft seat device preferably has an aircraft seat. The aircraft seat is preferably provided to provide a seat for a passenger in the aircraft. The aircraft seat particularly preferably comprises a seat base and a backrest. The aircraft seat preferably comprises at least one armrest. In addition, it would be conceivable that the aircraft seat comprises a leg rest. In principle, the aircraft seat can comprise further add-on parts, such as preferably a headrest. The aircraft seat is preferably adjustable between a sitting position and a lying position, preferably electromechanically. The aircraft seat device preferably comprises at least one adjustment unit which is provided to adjust the aircraft seat between the sitting position and the lying position. The at least one aircraft seat device preferably has at least one housing. The at least one housing is preferably designed as a shell element. The at least one aircraft seat device preferably has at least one console. The at least one aircraft seat device preferably has at least one ottoman. The at least one aircraft seat device preferably has at least one table unit. The at least one aircraft seat device preferably has at least one separating unit which is provided to separate the aircraft seat area from an aircraft cabin aisle and / or from an adjacent aircraft seat area, preferably optically. The at least one further aircraft seat device preferably has a further aircraft seat. The further aircraft seat is preferably provided to provide a further seat for a further passenger in the aircraft. The further aircraft seat particularly preferably comprises a further seat base and a further backrest. The further aircraft seat preferably comprises at least one further armrest. In addition, it would be conceivable that the further aircraft seat comprises a further leg support. In principle, the further aircraft seat can comprise further add-on parts, such as preferably a further headrest. In principle, the aircraft seat and the further aircraft seat can be designed identically. The further aircraft seat is preferably adjustable between a further sitting position and a further lying position, preferably electromechanically. The further aircraft seat device preferably comprises at least one further adjustment unit which is provided to adjust the further aircraft seat between the sitting position and the lying position. The at least one aircraft seat device preferably has at least one further housing on. The at least one further housing is preferably designed as a shell element. The at least one further aircraft seat device preferably has at least one further console. The at least one further aircraft seat device preferably has at least one further ottoman. The at least one further aircraft seat device preferably has at least one further table unit. The at least one further aircraft seat device preferably has at least one further separating unit, which is provided to separate the further aircraft seat area from an aircraft cabin aisle and / or from an adjacent aircraft seat area, preferably optically. A “seat position” should preferably be understood to mean a position of the aircraft seat in which a passenger can sit upright on the aircraft seat. The backrest of the aircraft seat and the seat bottom of the aircraft seat are preferably essentially perpendicular to one another in the seat position, preferably at an angle between 90 degrees and 115 degrees. The seat position preferably forms a first end position of the aircraft seat into which the aircraft seat is maximally adjustable. The seat position is preferably designed as a TTL position. A “TTL position” should preferably be understood to mean an upright position of the aircraft seat which, for safety reasons, must be assumed, preferably in a roll phase, in a take-off phase and in a landing phase of the aircraft. The at least one aircraft seat device preferably has a seat direction. The at least one further aircraft seat device preferably has a further seat direction. The seat direction of the at least one aircraft seat device is particularly preferably oriented opposite to the further seat direction of the at least one further aircraft seat device. A “seat direction” should preferably be understood to mean a direction which is at least substantially parallel to the aircraft cabin floor, preferably with a deviation of 3 degrees from the aircraft cabin floor, and at least substantially perpendicular to a theoretical, flat backrest oriented perpendicular to the aircraft cabin floor wherein the direction corresponds to a normal on a front side of the backrest, the front side of the backrest forming a support surface for a back of a passenger in a normal sitting position. “At least substantially” should preferably be understood to mean that a deviation from a predefined value is preferably less than 25%, preferably less than 10% and particularly preferably less than 5% of the predefined value. Under a "lying position" should preferably a position of the aircraft seat which is provided to provide an at least substantially horizontal lying surface for a passenger, preferably so that the passenger can assume a sleeping position during a flight. In the lying position of the aircraft seat, the passenger preferably lies at least essentially on the aircraft seat, preferably on the seat bottom and on the backrest. The reclining position preferably forms a second end position of the aircraft seat into which the aircraft seat is maximally adjustable. A “lying direction” should preferably be understood to mean a direction which runs at least essentially parallel to the aircraft cabin floor, preferably with a deviation of 3 degrees from the aircraft cabin floor, and in the lying position along a common central axis of the backrest and the seat floor. The lying direction is preferably directed from a head of a passenger to at least one foot of the passenger. The head of the passenger is preferably arranged behind the at least one foot of the passenger, viewed in the lying direction, preferably in a normal sleeping position of the passenger. The fact that an element is arranged “behind” a further element in one direction should preferably be understood to mean that, viewed in that direction, the further element is arranged first and then the element. The fact that an element is arranged “in front of” a further element in one direction should preferably be understood to mean that, viewed in that direction, the element is arranged first and then the further element. The lying direction preferably extends along a seat center axis of the aircraft seat of the at least one aircraft seat device. The lying direction particularly preferably extends along an idealized straight spine of the passenger. The lying direction is particularly preferably defined by the aircraft seat of the at least one aircraft seat device and preferably not by an actual posture of a passenger lying in the lying position on the aircraft seat. The lying direction of the at least one aircraft seat device is preferably formed at least substantially parallel to the further lying direction of the at least one further aircraft seat device. The seat direction of the at least one aircraft seat device is preferably formed at least substantially parallel to the further seat direction of the at least one further aircraft seat device. The sitting direction preferably corresponds to the lying direction. The further sitting direction preferably corresponds to the further lying direction. Basically, you can choose between the sitting position and the lying position further positions can be provided, which preferably form a combined sitting and lying position. The aforementioned definitions for the seat position, the seat direction, the reclining position and the reclining direction are preferably also valid for the at least one further aircraft seat device. The aircraft seat and the further aircraft seat are preferably each designed as a full-flat seat. A “full flat seat” should preferably be understood to mean an aircraft seat which can be transferred from the seated position to the lying position and which forms an at least essentially flat lying surface in the lying position. The flat lying surface is preferably inclined at an angle of 3 degrees to the aircraft cabin floor. In the reclining position, at least the seat bottom of the aircraft seat and the backrest of the aircraft seat are particularly preferably aligned at least substantially parallel to the aircraft cabin floor on which the aircraft seat is raised. In the lying position, the seat bottom of the aircraft seat and the backrest of the aircraft seat preferably have a common support surface which is aligned at least substantially parallel to the aircraft cabin floor.

It is also proposed that the at least one aircraft seat device and the at least one further aircraft seat device each have direct access to an aircraft cabin aisle. This configuration enables advantageously simple and convenient access to an aircraft seat to be achieved. This makes it possible to achieve a particularly advantageously high level of comfort for a passenger. Furthermore, this embodiment can achieve an advantageously high level of comfort for the passenger, since passengers from adjacent aircraft seat areas are not disturbed and / or impaired by direct access to an aircraft cabin aisle. “Direct access” should preferably be understood to mean access from an aircraft cabin aisle to an aircraft seat area, preferably to an aircraft seat, with the access to the aircraft seat area, preferably to the aircraft seat, not running through an adjacent aircraft seat area. Particularly preferably, the passenger can enter the aircraft seat area directly from the aircraft cabin aisle, preferably without crossing another aircraft seat area. The direct access is preferably assigned to only a single aircraft seat device. The direct access can preferably only be used from a single aircraft seat device. It is further proposed that the at least one aircraft seat device and the at least one further aircraft seat device each have direct access to different aircraft cabin aisles. This configuration enables an advantageously uniform distribution of direct access points within the aircraft cabin to be achieved. As a result, an advantageously uniform use of the different aircraft cabin aisles is achieved, as a result of which an advantageously high level of comfort is achieved for a passenger. The aircraft cabin preferably has two aircraft cabin aisles, which are preferably spaced apart from one another by at least one seat gap. The at least one aircraft seat device preferably has direct access to a first aircraft cabin aisle of the two aircraft cabin aisles. The at least one further aircraft seat device preferably has direct access to a second aircraft cabin aisle of the two aircraft cabin aisles.

In addition, it is proposed that the reclining direction of the at least one aircraft seat device has a directional component in the direction of flight and the further reclining direction of the at least one further aircraft seat device has a directional component opposite to the flight direction. This configuration enables an advantageously compact aircraft seat arrangement to be provided. Furthermore, this configuration can achieve an advantageously high level of privacy, which enables an advantageously high level of comfort. A “directional component” should preferably be understood to mean a component of a vector of the lying direction and / or the sitting direction that is aligned parallel to the flight direction. Alternatively, it would also be conceivable that the lying direction of the at least one aircraft seat device has a directional component opposite to the flight direction and the further lying direction of the at least one further aircraft seat device has a directional component in the flight direction.

It is further proposed that the lying direction of the at least one aircraft seat device and the further lying direction of the at least one further aircraft seat device, in particular at least 5 degrees, are oriented at an angle to a longitudinal axis of the aircraft. As a result of this configuration, the at least one aircraft seat device and the at least one further aircraft seat device, viewed in the direction of flight, can advantageously be arranged close together. This can be an advantageous high number of aircraft seat devices are provided in the aircraft cabin section. The lying direction of the at least one aircraft seat device is preferably oriented at an angle of at least 5 degrees, preferably at least 30 degrees and particularly preferably at least 45 degrees to a longitudinal axis of the aircraft. The further lying direction of the at least one further aircraft seat device is preferably oriented at an angle of at least 5 degrees, preferably at least 30 degrees and particularly preferably at least 45 degrees to a longitudinal axis of the aircraft. The lying direction of the at least one aircraft seat device and the further lying direction of the at least one further aircraft seat device are particularly preferably angled at an angle of equal amount to a longitudinal axis of the aircraft. The seat direction of the at least one aircraft seat device and the further seat direction of the at least one further aircraft seat device are particularly preferably oriented at an angle to a longitudinal axis of the aircraft, in particular at least 5 degrees. The seat direction of the at least one aircraft seat device is preferably oriented at an angle of at least 5 degrees, preferably at least 30 degrees and particularly preferably at least 45 degrees to a longitudinal axis of the aircraft. The further seat direction of the at least one further aircraft seat device is preferably oriented at an angle of at least 5 degrees, preferably at least 30 degrees and particularly preferably at least 45 degrees to a longitudinal axis of the aircraft. Particularly preferably, the seat direction of the at least one aircraft seat device and the further seat direction of the at least one further aircraft seat device are angled at an angle of equal amount to a longitudinal axis of the aircraft.

It is further proposed that the lying direction of the at least one aircraft seat device and the further lying direction of the at least one further aircraft seat device are aligned at least essentially parallel to one another. This configuration enables an advantageously compact aircraft seat arrangement to be provided. Furthermore, an advantageously uniform appearance of the aircraft seat arrangement can be achieved through this configuration. Preferably, the lying direction and the further lying direction are ideally aligned with the at least one aircraft seat device and the at least one further aircraft seat device, with an actual lying direction defined by a passenger, io, preferably due to an asymmetrical posture of the passenger, can deviate from the lying direction and the further lying direction.

It is also proposed that the at least one aircraft seat device at least partially intersect an aircraft cabin center plane. This configuration enables an advantageously compact aircraft seat arrangement to be provided. Furthermore, an overhang and / or free space caused by an arrangement of the at least one aircraft seat device and / or the at least one further aircraft seat device can be used advantageously in a space-efficient manner. An “aircraft cabin center plane” should preferably be understood to mean a plane which is oriented perpendicular to the aircraft cabin floor along the aircraft cabin center axis. An outer contour of the at least one aircraft seat device projected onto the aircraft cabin floor preferably at least partially intersects the aircraft cabin center plane. The projected outer contour of the at least one aircraft seat device preferably has a shape which is designed to correspond to an outer contour of at least one adjacent aircraft seat device that is mirrored over an aircraft longitudinal axis.

It is further proposed that the aircraft seat arrangement comprises at least three seat groupings which are arranged directly one behind the other in the at least one seat column and which are each formed from the at least one aircraft seat device and the at least one further aircraft seat device. With this configuration, an advantageously cost-effective production of the at least one aircraft seat device and the at least one further aircraft seat device can be achieved, wherein a variety of components can advantageously be kept low. Furthermore, this configuration allows a number of seat groupings that is advantageously variable along a longitudinal axis of the aircraft to be arranged. As a result, the aircraft seat arrangement can advantageously be easily implemented in aircraft cabins of different designs. A “seat grouping” should preferably be understood to mean a common arrangement of the at least one aircraft seat device and the at least one further aircraft seat device in an area of the aircraft cabin, preferably in the aircraft cabin section. The at least one aircraft seat device and the at least one further aircraft seat device are preferably directly one behind the other in the at least one seat gap and / or arranged directly next to one another. The at least one aircraft seat device and the at least one further aircraft seat device preferably form one of the at least three seat groupings. Particularly preferably, the at least three seat groupings arranged directly one behind the other in the at least one seat gap are of identical design. The at least three seat groupings preferably form a, preferably periodically, repeatable sequence. Several identical seat groupings can be arranged directly one behind the other, preferably along a longitudinal axis of the aircraft.

It is also proposed that an axis perpendicular to an aircraft longitudinal axis intersects a shoulder area of the at least one aircraft seat device and a further shoulder area of the at least one further aircraft seat device, in particular in the reclining position of the at least one aircraft seat device and the at least one further aircraft seat device. This configuration makes it possible to achieve an advantageously compact arrangement of the at least one aircraft seat arrangement and the at least one further aircraft seat arrangement with respect to one another. Furthermore, this configuration can achieve an advantageously high level of privacy, which enables an advantageously high level of comfort. The axis is preferably aligned parallel to the aircraft cabin floor. Preferably, the axis intersects exactly two shoulder areas in a single seat column. A “shoulder area” is preferably to be understood as an area of an aircraft seat device in which a shoulder of a passenger, which preferably corresponds to the 95th percentile, is preferably arranged in a normal sleeping position in the lying position of the at least one aircraft seat device, with a head of the passenger in the lying position is preferably arranged in an area of an upper edge of the backrest of the aircraft seat, the upper edge preferably being on a side of the backrest facing away from the seat bottom of the aircraft seat. The shoulder area of the at least one aircraft seat device is preferably provided to accommodate the passenger's shoulder, which preferably corresponds to the 95th percentile, in the reclining position of the at least one aircraft seat device. The at least one aircraft seat device and the at least one further aircraft seat device preferably each have direct access to the same aircraft cabin aisle. The lying direction of the at least one aircraft seat device is preferably directed away from an aircraft cabin aisle. Preferably is the further lying direction of the at least one further aircraft seat device is directed towards the aircraft cabin aisle.

It is also proposed that an axis perpendicular to an aircraft longitudinal axis intersects the backrest of the aircraft seat of the at least one aircraft seat device and the further backrest of the further aircraft seat of the at least one further aircraft seat device, in particular in the seat position of the at least one aircraft seat device and the at least one further aircraft seat device. This configuration makes it possible to achieve an advantageously compact arrangement of the at least one aircraft seat arrangement and the at least one further aircraft seat arrangement with respect to one another. Furthermore, this configuration can achieve an advantageously high level of privacy, which enables an advantageously high level of comfort. The axis is preferably aligned parallel to the aircraft cabin floor. Preferably, exactly two backrests are arranged side by side in the at least one common seat gap, namely the backrest of the aircraft seat of the at least one aircraft seat device and the further backrest of the further aircraft seat of the at least one further aircraft seat device.

It is further proposed that the at least one aircraft seat device has at least one housing which, in the lying position of the at least one aircraft seat device, at least substantially covers a head area of the aircraft seat of the at least one aircraft seat device. A particularly comfortable aircraft seat arrangement can be provided by this configuration. Furthermore, this embodiment can advantageously ensure that the aircraft seat of the at least one aircraft seat device is shielded from an environment. As a result, privacy protection can preferably be achieved, which enables an advantageously high level of privacy. Furthermore, an advantageously compact aircraft seat arrangement can be achieved at the same time as a result of this configuration. In the lying position, the head of the passenger is preferably arranged in the head area, the passenger preferably corresponding to the 95th percentile. The head area is preferably located on the upper edge of the backrest of the aircraft seat, the upper edge preferably being located on a side of the backrest facing away from the seat bottom of the aircraft seat. Preferably an axis intersects the is aligned perpendicular to the aircraft cabin floor, the at least one housing of the at least one aircraft seat device and the head region of the aircraft seat of the at least one aircraft seat device, preferably in the lying position. The at least one housing preferably has an upper end, preferably above the head area in the lying position, which at least in sections forms an at least substantially straight edge which is oriented perpendicular to the seating direction of the at least one aircraft seat device, preferably viewed perpendicular to a plane, which is aligned parallel to the aircraft cabin floor. The at least one housing preferably extends from the at least substantially straight edge to at least one storage area of the at least one console of the at least one aircraft seat device, the at least one storage area being arranged between the at least substantially straight edge and the aircraft cabin floor. A length of this extension, measured parallel to the aircraft cabin floor and measured in the seat direction, preferably corresponds to at least 30 cm and particularly preferably at least 40 cm and / or preferably at most 60 cm and particularly preferably at most 50 cm. The at least one housing, viewed in the seat direction, preferably has a slope in front of the aircraft seat. The slope is preferably designed as a flat area of the at least one housing. The slope preferably has an angle of preferably at least 10 degrees, preferably at least 20 degrees and particularly preferably at least 30 degrees with respect to an axis which is oriented perpendicular to the aircraft cabin floor. The slope is preferably inclined towards the aircraft seat of the at least one aircraft seat device. By means of the incline, in particular with a completely lowered separating unit, an advantageously simple and ergonomic view between the aircraft seat of the at least one aircraft seat device and an adjacent aircraft seat of an adjacent aircraft seat device can be made possible. As a result, couples traveling together, who preferably sit opposite one another in the aircraft seat and the adjacent aircraft seat, can advantageously communicate with one another in a simple and convenient manner. Furthermore, by means of the incline, advantageously open aircraft seat areas with an advantageously large spatial effect can be provided. The at least one further aircraft seat device particularly preferably has at least one further housing, which in the lying position of the at least one further aircraft seat device has a further head area of the further aircraft seat which at least substantially covers at least one further aircraft seat device. The at least one housing and the at least one further housing are preferably formed in one piece with one another. “In one piece” should preferably be understood to be at least cohesively connected, for example by a welding process, an adhesive process, an injection molding process and / or another process that appears sensible to a person skilled in the art, and / or advantageously formed in one piece, for example by a Fierstellung from a cast and / or by a Fierstellung in a single or multi-component injection molding process and advantageously from a single blank.

It is further proposed that a seat center axis of an aircraft seat of the at least one aircraft seat device intersects the further seat bottom of the further aircraft seat of the at least one further aircraft seat device, in particular viewed perpendicular to the aircraft cabin floor. As a result of this configuration, component complexity can advantageously be reduced, as a result of which a cost-effective lowering position of the at least one aircraft seat device and of the at least one further aircraft seat device is made possible. Furthermore, an advantageously compact aircraft seat arrangement can be achieved through this configuration. A “seat center axis” should preferably be understood to mean an axis that runs parallel to the seat direction and through a center point of the aircraft seat, preferably the seat bottom and / or the backrest, the center point preferably having the same minimum distance from two armrests of the aircraft seat. The seat center axis of the aircraft seat is preferably aligned parallel to a further seat center axis of the further aircraft seat. The seat center axis and the further seat center axis are preferably spaced apart from one another, preferably viewed perpendicular to the aircraft cabin floor. In principle, it would also be conceivable that the seat center axis of the aircraft seat of the at least one aircraft seat device and the further seat center axis of the further aircraft seat of the at least one further aircraft seat device are arranged in a plane that is oriented perpendicular to the aircraft cabin floor.

It is also proposed that the lying direction of the at least one aircraft seat device and the further lying direction of the at least one further aircraft seat device are directed towards one another. This configuration allows an advantageously compact aircraft seat arrangement can be achieved with a simultaneously advantageously high level of comfort. The lying direction of the at least one aircraft seat device is preferably directed away from an aircraft cabin aisle. The further lying direction of the at least one further aircraft seat device is preferably directed away from a further aircraft cabin aisle.

Furthermore, it is proposed that the at least one aircraft seat device in the reclining position of the at least one aircraft seat device forms a reclining plane that is at a different distance from the aircraft cabin floor than a further reclining plane formed by the at least one further aircraft seat device in the reclining position of the at least one further aircraft seat device is.

As a result of this configuration, the at least one aircraft seat device and the at least one further aircraft seat device can be arranged so as to overlap one another, at least in the lying position. A particularly advantageously compact aircraft seat arrangement can thereby be provided. The lying plane preferably has a greater or smaller minimum distance from the aircraft cabin floor than the further lying plane. A minimum distance between the lying plane and the further lying plane, measured perpendicular to the aircraft cabin floor, is preferably at least 20 cm, preferably at least 25 cm and particularly preferably at least 30 cm. A surface of the backrest of the aircraft seat of the at least one aircraft seat device, a surface of the seat bottom of the aircraft seat of the at least one aircraft seat device and a surface of a foot and / or leg support element of the at least one aircraft seat device preferably form the lying plane. In this context, a “surface” should preferably be understood to mean a surface of an aircraft seat which, in the seated position and / or in the lying position of the aircraft seat, is intended for contact with a passenger, preferably due to the force of weight, the surface preferably having at least one comfort element of the Aircraft seat limited on a passenger facing side of the comfort element. In this context, a “comfort element” should preferably be understood to mean an element that provides padding, such as a foam element and / or a spring core element. The surface of the backrest, the surface of the seat bottom and the surface of the foot and / or leg support element in the lying position are preferably facing away from the aircraft cabin floor. Preferably, a surface of the further backrest of the further aircraft seat of the at least one further aircraft seat device, a surface of the further seat bottom of the further aircraft seat of the at least one further aircraft seat device and a surface of a further foot and / or leg support element of the at least one further aircraft seat device form the further lying level. The surface of the further backrest, the surface of the further seat floor and the surface of the further foot and / or leg support element are preferably facing away from the aircraft cabin floor in the lying position. The seat bottom of the aircraft seat of the at least one aircraft seat device is preferably provided to be raised from the aircraft cabin floor or lowered to the aircraft cabin floor when the seat position is moved from the seated position to the lying position. The further seat floor of the further aircraft seat of the at least one further aircraft seat device is preferably provided to be lowered or raised from the aircraft cabin floor when moving from the seated position to the reclining position. In principle, it would also be conceivable for the seat bottom of the aircraft seat or the further seat bottom of the further aircraft seat to be at the same distance from the aircraft cabin floor in the lying position.

It is further proposed that a footwell of the at least one aircraft seat device and a further footwell of the at least one further aircraft seat device, in particular viewed perpendicular to the aircraft cabin floor, are arranged so as to overlap one another. With this configuration, an available installation space can be used to advantage. As a result, an advantageously compact aircraft seat arrangement can be provided. A “footwell” should preferably be understood to mean a room in which at least one foot of a passenger is placed in the lying position in a normal sleeping position. The footwell of the at least one aircraft seat device is preferably arranged in the at least one console of the at least one aircraft seat device. The foot and / or leg support element of the at least one aircraft seat device is preferably arranged at least substantially in the footwell of the at least one aircraft seat device. The further footwell of the at least one further aircraft seat device is preferably arranged in the at least one further console of the at least one further aircraft seat device. The further foot and / or is preferred Leg support element of the at least one further aircraft seat device is arranged at least substantially in the further footwell of the at least one further aircraft seat device.

It is also proposed that the at least one aircraft seat device and the at least one further aircraft seat device have at least one common console. With this configuration, an available installation space can be used to advantage. As a result, an advantageously compact aircraft seat arrangement can be provided. The at least one common console is preferably arranged between the aircraft seat of the at least one aircraft seat device and the further aircraft seat of the at least one further aircraft seat device. The at least one console of the at least one aircraft seat device and the at least one further console of the at least one further aircraft seat device are preferably designed in one piece. Particularly preferably, the at least one console of the at least one aircraft seat device and the at least one further console of the at least one further aircraft seat device form the at least one common console.

It is further proposed that the aircraft seat arrangement comprises at least one adjacent aircraft seat device which is at least substantially identical to the at least one aircraft seat device, the at least one console being at least partially usable from the at least one adjacent aircraft seat device. As a result of this configuration, an installation space can advantageously be fully utilized. As a result, an advantageously compact aircraft seat arrangement can be provided. In addition, this configuration allows advantageously convenient access by a passenger of the at least one adjacent aircraft seat device to the at least one console. As a result, an advantageously high level of comfort is achieved. “Usable” should preferably be understood to mean that at least one component and / or a space of the at least one console and / or at least one function of the at least one console is accessible, adjustable and / or operable by a passenger in the at least one adjacent aircraft seat device. The at least one common console preferably has at least one storage space. The at least one storage space is preferably accessible only from the at least one adjacent aircraft seat device. Particularly The at least one storage space is preferably arranged above the footwell and the further footwell. An axis that is oriented perpendicular to the aircraft cabin floor preferably intersects the footwell of the at least one aircraft seat device, the footwell of the at least one further aircraft seat device and the at least one stowage space of the at least one console.

It is further proposed that the at least one aircraft seat device and the at least one further aircraft seat device jointly form an at least substantially rectangular base area. With this configuration, an available area of the at least one seat gap can be used advantageously. Furthermore, this configuration allows an advantageously variable number of aircraft seat devices to be arranged along a longitudinal axis of the aircraft.

As a result, the aircraft seat arrangement can advantageously be easily implemented in aircraft cabins of different designs. A “base area” should preferably be understood to mean an area which, viewed perpendicular to the aircraft cabin floor, is enclosed by an outer contour of the at least one aircraft seat device and the at least one further aircraft seat device. It is conceivable that a footwell of the at least one aircraft seat device and / or a further footwell of the at least one further aircraft seat device protrudes into at least one area of at least one adjacent aircraft seat device. The at least substantially rectangular base area is preferably delimited along a longitudinal axis of the aircraft by a partition wall of the at least one aircraft seat device and by a further partition wall of the at least one further aircraft seat device. The partition wall is preferably formed continuously between an aircraft cabin aisle and a further aircraft cabin aisle or an aircraft cabin outer wall of the aircraft cabin. A fluff extension direction of the partition wall is preferably oriented orthogonally to a longitudinal axis of the aircraft.

In addition, it is proposed that the seat direction of the at least one aircraft seat device is aligned at least essentially parallel to a longitudinal axis of the aircraft. This configuration enables an advantageously comfortable aircraft seat arrangement with an advantageously large usable area of the at least one Aircraft seat device are provided. The seat direction of the at least one aircraft seat device preferably deviates from the lying direction of the at least one aircraft seat device by preferably at least 18 degrees, preferably at least 25 degrees and particularly preferably at least 30 degrees. The aircraft seat, preferably the seat base, of the at least one aircraft seat device is preferably arranged in the same position in the sitting position and in the lying position. The seat bottom of the aircraft seat of the at least one aircraft seat device is preferably arranged immovably in one position and / or in one orientation. In principle, however, it is conceivable that the aircraft seat of the at least one aircraft seat device has a backrest that can be pivoted relative to the seat base and / or a seat base articulation. The further seat direction of the at least one further aircraft seat device is particularly preferably oriented at least substantially parallel to a longitudinal axis of the aircraft. The further seat direction of the at least one further aircraft seat device preferably deviates from the further lying direction of the at least one further aircraft seat device by preferably at least 18 degrees, preferably at least 25 degrees and particularly preferably at least 30 degrees. The further aircraft seat, preferably the further seat bottom, of the at least one further aircraft seat device is preferably arranged in the same position in the sitting position and in the lying position. The further seat bottom of the further aircraft seat of the at least one further aircraft seat device is preferably arranged immovably in one position and / or in one orientation. In principle, the further aircraft seat of the at least one further aircraft seat device can have a further backrest that can be pivoted with respect to the further seat base and / or a seat base articulation.

It is also proposed that an axis perpendicular to an aircraft longitudinal axis intersects the seat bottom of the aircraft seat of the at least one aircraft seat device and the further seat bottom of the further aircraft seat of the at least one further aircraft seat device, in particular in the seat position of the at least one aircraft seat device and the at least one further aircraft seat device. This configuration makes it possible to achieve an advantageously compact arrangement of the at least one aircraft seat arrangement and the at least one further aircraft seat arrangement with respect to one another. Furthermore, an advantageously high level of privacy can be achieved through this configuration, as a result of which an advantageously high level of comfort is made possible. The axis is preferably aligned parallel to the aircraft cabin floor. Preferably, exactly two seat bottoms are arranged next to one another in the at least one common seat gap, namely the seat bottom of the aircraft seat of the at least one aircraft seat device and the further seat bottom of the further aircraft seat of the at least one further aircraft seat device.

It is further proposed that the at least one aircraft seat device, in a lying position of the at least one aircraft seat device, form a lying plane that is at most 60% from the aircraft seat of the at least one aircraft seat device. This configuration makes it possible to provide an advantageously comfortable aircraft seat arrangement with an advantageously large usable area of the at least one aircraft seat device. The lying plane is preferably at most 60%, preferably at most 50% and particularly preferably at most 40% of the seat bottom of the aircraft seat of the at least one aircraft seat device. The at least one aircraft seat device preferably has at least one comfort element, which preferably forms a lying surface. The at least one comfort element, viewed in the seat direction, is preferably arranged next to the seat bottom of the aircraft seat. Particularly preferably, the lying plane is formed to preferably at least 30%, preferably at least 40% and particularly preferably at least 60% of the at least one comfort element of the at least one aircraft seat device. The at least one comfort element is preferably designed in one piece with the seat bottom of the aircraft seat of the at least one aircraft seat device. In a reclining position of the at least one further aircraft seat device, the at least one further aircraft seat device preferably forms a further reclining level which is at most 60% of the further aircraft seat of the at least one further aircraft seat device. Preferably, the further lying level is preferably at most 60%, preferably at most 50% and particularly preferably at most 40% of the further seat bottom of the further aircraft seat of the at least one further aircraft seat device. The at least one further aircraft seat device preferably has at least one further comfort element, which preferably forms a further lying surface. The at least one further comfort element, viewed in the further seat direction, is preferably in addition to the further one Arranged seat bottom of the further aircraft seat. Particularly preferably, the further lying plane is formed to preferably at least 30%, preferably at least 40% and particularly preferably at least 60% of the at least one further comfort element of the at least one further aircraft seat device. The at least one further comfort element is preferably designed in one piece with the further seat bottom of the further aircraft seat of the at least one further aircraft seat device.

In addition, an aircraft seat device of the aircraft seat arrangement according to the invention is proposed. This configuration enables an advantageously compact aircraft seat arrangement to be achieved.

The aircraft seat arrangement according to the invention should not be restricted to the application and embodiment described above. In particular, the aircraft seat arrangement according to the invention can have a number of individual elements, components and units that differs from a number of individual elements, components and units mentioned herein in order to fulfill a mode of operation described herein.

drawings

Further advantages emerge from the following description of the drawings. Four exemplary embodiments of the invention are shown in the drawing. The drawings, the description and the claims contain numerous features in combination. The person skilled in the art will expediently also consider the features individually and combine them into meaningful further combinations.

Show it:

1 shows an aircraft in a schematic representation in a first exemplary embodiment,

2 shows an aircraft seat arrangement according to the invention in a schematic representation in the first exemplary embodiment, 3 shows a section of the aircraft seat arrangement according to the invention from FIG. 2 in a schematic representation in the first exemplary embodiment,

4 shows a perspective view of the aircraft seat arrangement according to the invention in a schematic representation in the first exemplary embodiment,

5 shows a perspective view of the aircraft seat arrangement according to the invention in a schematic representation in the first exemplary embodiment,

6 shows an aircraft seat arrangement according to the invention in a schematic

Representation in a second embodiment,

7 shows a detail of the aircraft seat arrangement according to the invention

6 in a schematic representation in the second

Embodiment,

8 shows a perspective view of the aircraft seat arrangement according to the invention in a schematic representation in the second exemplary embodiment,

9 shows a perspective sectional view of the aircraft seat arrangement according to the invention in a schematic representation in the second exemplary embodiment,

10 shows a perspective view of an aircraft seat arrangement according to the invention in a schematic representation in a third exemplary embodiment,

11 shows an aircraft seat arrangement according to the invention in a schematic illustration in a fourth exemplary embodiment, FIG. 12 shows a detail of the aircraft seat arrangement according to the invention from FIG. 11 in a schematic illustration in the fourth exemplary embodiment, and FIG

13 shows a perspective view of the aircraft seat arrangement according to the invention from FIG. 11 in a schematic representation in the fourth exemplary embodiment. Description of the exemplary embodiments

FIG. 1 shows an aircraft 10a. The aircraft 10a has an aircraft cabin 12a. The aircraft 10a has an aircraft seat arrangement 14a. Figures 2 to 5 show the aircraft seat arrangement 14a in a first embodiment. The aircraft seat arrangement 14a is intended for use in the aircraft cabin 12a of the aircraft 10a, which is partially shown. The aircraft cabin 12a is intended for all passengers to stay during a flight.

The aircraft cabin 12a has an aircraft cabin central axis 16a. The aircraft cabin center axis 16a is designed as a longitudinal axis of the aircraft. The aircraft cabin center axis 16a is at the same distance from opposite aircraft cabin outer walls 18a, 20a of the aircraft cabin 12a. The aircraft cabin center axis 16a is aligned parallel to a roll axis of the aircraft 10a. The aircraft cabin center axis 16a is aligned parallel to an aircraft cabin floor 22a of the aircraft cabin 12a. The aircraft cabin center axis 16a is preferably arranged on the aircraft cabin floor 22a. The aircraft cabin 12a has an aircraft cabin center plane (not shown in greater detail). The aircraft cabin center plane is oriented perpendicular to the aircraft cabin floor 22a along the aircraft cabin center axis 16a. The aircraft 10a has a flight direction 24a in at least one operating state. In the present case, the flight direction 24a is ideally aligned parallel to the aircraft cabin central axis 16a.

The aircraft cabin 12a has an aircraft cabin section 26a along the aircraft cabin central axis 16a. The aircraft seat arrangement 14a is arranged in the aircraft cabin section 26a. In addition, the aircraft cabin 12a can have at least one further aircraft cabin section, viewed in the direction of flight 24a, preferably in front of or behind the aircraft cabin section 26a. In the present case, the aircraft cabin section 26a is delimited by several aircraft cabin separating elements 28a and by several schematically illustrated aircraft cabin modules 30a along the aircraft cabin central axis 16a. In the present case, the aircraft cabin partition elements 28a are each designed as an aircraft cabin partition wall. In the present case, the aircraft cabin modules 30a are each designed as a kitchen module, as a toilet module, as a wardrobe or as a front-row monument. In the present case, the aircraft cabin 12a has two aircraft cabin aisles 32a, 34a in the aircraft cabin section 26a. Alternatively, it would also be conceivable that the aircraft cabin 12a only has a single aircraft cabin aisle. The aircraft cabin 12a has an aircraft cabin aisle 32a. The aircraft cabin 12a has a further aircraft cabin aisle 34a. The aircraft cabin aisles 32a, 34a each extend at least substantially along an aircraft longitudinal axis, not shown in detail.

In the present case, the aircraft seat arrangement 14a comprises four seat gaps 36a, 38a, 40a, 42a. Alternatively, it would also be conceivable that the aircraft seat arrangement 14a comprises only two or three seat gaps. The four seat gaps 36a, 38a, 40a, 42a each extend in the flight direction 24a. The aircraft seat arrangement 14a comprises a first seat column 36a. The first seat column 36a is designed as a first inner seat column.

The aircraft seat arrangement 14a comprises a second seat column 38a. The second seat column 38a is designed as a second inner seat column. The first seat column 36a and the second seat column 38a are arranged directly next to one another. The aircraft cabin 12a has a central region 44a. The central area 44a is delimited by the two aircraft cabin aisles 32a, 34a. The first seat column 36a and the second seat column 38a are arranged in the central region 44a. A maximum combined extent of the first seat gaps 36a and the second seat gaps 38a measured perpendicular to the aircraft cabin central axis 16a and parallel to the aircraft cabin floor 22a corresponds to a minimum distance between the aircraft cabin aisle 32a and the further aircraft cabin aisle 34a. The first seat column 36a and the second seat column 38a at least substantially completely fill the central region 44a, viewed perpendicular to the aircraft cabin central axis 16a and parallel to the aircraft cabin floor 22a. In principle, it would also be conceivable that only one seat gap is arranged in the central region 44a of the aircraft cabin 12a. The aircraft seat arrangement 14a comprises a third seat column 40a. The third seat column 40a is designed as a first outer seat column. The first seat column 36a and the third seat column 40a are spaced apart from one another by the aircraft cabin aisle 32a. The aircraft seat arrangement 14a comprises a fourth seat column 42a. The fourth seat column 42a is designed as a second outer seat column. The second seat column 38a and the fourth seat column 42a are separated from one another by the further aircraft cabin aisle 34a spaced. In the present case, the fourth seat gap 42a is formed symmetrically to the third seat gap 40a over the aircraft cabin center axis 16a.

The aircraft seat arrangement 14a comprises an aircraft seat device 46a. The aircraft seat device 46a is arranged in the first seat gap 36a. The aircraft seat arrangement 14a comprises a further aircraft seat device 48a. The further aircraft seat device 48a is arranged in the first seat gap 36a. The aircraft seat device 46a and the further aircraft seat device 48a are arranged at least partially next to one another in a common seat gap, namely the first seat gap 36a. In the common first seat gap 36a, exactly two aircraft seat devices are arranged directly next to one another, namely the aircraft seat device 46a and the further aircraft seat device 48a. The aircraft seat device 46a and the further aircraft seat device 48a are arranged in the first seat gap 36a, viewed perpendicular to the aircraft cabin central axis 16a, at least partially overlapping one another. The aircraft seat device 46a and the further aircraft seat device 48a are arranged directly adjacent to one another in the first seat gap 36a. The aircraft seat device 46a and the further aircraft seat device 48a are arranged in the first seat column directly one behind the other and directly next to one another. The aircraft seat device 46a and the further aircraft seat device 48a each have direct access to the same aircraft cabin aisle 32a.

The aircraft seat arrangement 14a comprises an adjacent aircraft seat device 46'a. The adjacent aircraft seat device 46'a is at least essentially identical to the aircraft seat device 46a. The adjacent aircraft seat device 46'a is arranged in the first seat gap 36a. The adjacent aircraft seat device 46'a is arranged adjacent to the further aircraft seat device 48a along a longitudinal axis of the aircraft. The adjacent aircraft seat device 46'a is arranged immediately in front of the further aircraft seat device 48a when viewed in the direction of flight 24a. The adjacent aircraft seat device 46'a is spaced apart from the aircraft seat device 46a by the further aircraft seat device 48a. In principle, it is conceivable that an adjacent aircraft seat device 46'a arranged in the first seat gap 36a and in a first row of seats and / or in a last row of seats in the aircraft cabin section 26a differs from that of the aircraft cabin section 26a Aircraft seat device 46a is formed. As a result, additional space can advantageously be made available in the first row of seats and / or in the last row of seats.

The aircraft seat arrangement 14a comprises an adjacent further aircraft seat device 48’a. The adjacent further aircraft seat device 48’a is at least essentially identical to the further aircraft seat device 48a. The adjacent further aircraft seat device 48’a is arranged in the first seat column 36a. The adjacent further aircraft seat device 48'a is arranged adjacent to the aircraft seat device 46a along a longitudinal axis of the aircraft. The adjacent further aircraft seat device 48’a is arranged immediately behind the further aircraft seat device 48a when viewed in the direction of flight 24a. The adjacent further aircraft seat device 48’a is spaced apart from the further aircraft seat device 48a by the aircraft seat device 46a.

The aircraft seat arrangement 14a comprises another adjacent aircraft seat device 50a. The other adjacent aircraft seat device 50a is arranged in the second seat column 38a. The other adjacent aircraft seat device 50a is arranged at least partially adjacent to the further aircraft seat device 48a along an axis perpendicular to the aircraft cabin central axis 16a. The other adjacent aircraft seat device 50a, viewed in the direction of flight 24a, is arranged at least partially directly next to the aircraft seat device 46a. The other adjacent aircraft seat device 50a, viewed in the direction of flight 24a, is arranged at least partially directly next to the further aircraft seat device 48a. The other adjacent aircraft seat device 50a is designed to be mirrored over the aircraft cabin central axis 16a to the aircraft seat device 46a. The other adjacent aircraft seat device 50a is arranged offset along the aircraft cabin central axis 16a in relation to the aircraft seat device 46a. The other adjacent aircraft seat device 50a is arranged along the aircraft cabin center axis 16a offset from the aircraft seat device 46a by half the maximum aircraft seat device distance between the aircraft seat device 46a and the adjacent aircraft seat device 46'a. The aircraft seat device distance between the aircraft seat device 46a and the adjacent aircraft seat device 46’a is measured along a longitudinal axis of the aircraft. Of the

Aircraft seat assembly distance between the aircraft seat assembly 46a and the adjacent aircraft seat device 46'a is measured between two measuring points arranged identically in the aircraft seat device 46a and the adjacent aircraft seat device 46'a.

The aircraft seat arrangement 14a comprises another adjacent further aircraft seat device 52a. The other adjacent further aircraft seat device 52a is arranged in the second seat gap 38a. The other adjacent further aircraft seat device 52a is arranged adjacent to the other adjacent aircraft seat device 50a along a longitudinal axis of the aircraft. The other adjacent further aircraft seat device 52a is arranged immediately behind the other adjacent aircraft seat device 50a when viewed in the direction of flight 24a. The other adjacent further aircraft seat device 52a is arranged at least partially adjacent to the aircraft seat device 46a along an axis perpendicular to the aircraft cabin central axis 16a. The other, adjacent further aircraft seat device 52a, viewed in the direction of flight 24a, is arranged at least partially directly next to the aircraft seat device 46a. The other adjacent further aircraft seat device 52a is designed to be mirrored over the aircraft cabin central axis 16a to the further aircraft seat device 48a. The other adjacent further aircraft seat device 52a is arranged offset along the aircraft cabin central axis 16a with respect to the further aircraft seat device 48a. The other adjacent further aircraft seat device 52a is arranged along the aircraft cabin center axis 16a offset by half a maximum further aircraft seat device distance between the further aircraft seat device 48a and the neighboring further aircraft seat device 48'a relative to the further aircraft seat device 48a. The further aircraft seat device distance between the further aircraft seat device 48a and the adjacent further aircraft seat device 48'a is measured along a longitudinal axis of the aircraft. The further aircraft seat device distance between the further aircraft seat device 48a and the neighboring further aircraft seat device 48'a is measured between two measuring points which are arranged identically in the further aircraft seat device 48a and the neighboring further aircraft seat device 48'a. The further spacing of the aircraft seat device is identical to the spacing of the aircraft seat device. The aircraft seat device 46a and the further aircraft seat device 48a form a seat grouping 54a of the aircraft seat arrangement 14a. The grouping of seats 54a forms a, preferably periodically, repeatable sequence. In the present case, the aircraft seat arrangement 14a comprises four seat groupings 54a, 54'a, 54 ”a, 54” 'a arranged directly one behind the other in the first seat gap 36a, each of which is formed from the aircraft seat device 46a and the further aircraft seat device 48a. The four seat groupings 54a, 54'a, 54 "a, 54"'a arranged directly one behind the other in the first seat column 36a are of identical design.

The aircraft seat device 46a is provided to be raised on the aircraft cabin floor 22a of the aircraft cabin 12a. The aircraft seat device 46a forms an aircraft seat area. The aircraft seat device 46a has an aircraft seat 56a. The aircraft seat 56a is arranged in the aircraft seat area of the aircraft seat device 46a. The aircraft seat 56a is provided to provide a seat for a passenger in the aircraft 10a. The aircraft seat 56a is designed as a full flat seat. The aircraft seat 56a includes a seat bottom 58a. The aircraft seat 56a includes a backrest 60a. The aircraft seat 56a includes two armrests. In addition, it would be conceivable that the aircraft seat 56a comprises a leg rest. In principle, the aircraft seat 56a can comprise additional add-on parts, such as preferably a headrest. The aircraft seat device 46a is adjustable between a sitting position and a lying position. The aircraft seat 56a is electromechanically adjustable between the sitting position and the lying position. The aircraft seat device 46a comprises at least one adjustment unit, not shown, which is provided to adjust the aircraft seat 56a between the sitting position and the lying position. The aircraft seat 56a of the aircraft seat device 46a is designed to be non-rotatable with regard to a movement about an axis perpendicular to the aircraft cabin floor 22a. In FIGS. 2, 4 and 5, the aircraft seat device 46a is shown in the seated position. In FIG. 3, the aircraft seat device 46a is shown in the lying position. The aircraft seat device 46a has a seat direction 62a. The seat direction 62a of the aircraft seat device 46a has a directional component in the flight direction 24a. The seat direction 62a of the aircraft seat device 46a is oriented at an angle of at least 5 degrees to the aircraft cabin central axis 16a. Alternatively, it would also be conceivable for the seat direction 62a of the aircraft seat device 46a to be parallel to the Is aligned aircraft cabin central axis 16a or at an angle of less than 5 degrees to the aircraft cabin central axis 16a. The seat direction 62a of the aircraft seat device 46a is directed towards the aircraft cabin aisle 32a. The aircraft seat device 46a has a lying direction 64a. The sitting direction 62a corresponds to the lying direction 64a. The lying direction 64a of the aircraft seat device 46a has a directional component in the flight direction 24a. The lying direction 64a of the aircraft seat device 46a is oriented at an angle of at least 5 degrees to the aircraft cabin central axis 16a. Alternatively, it would also be conceivable for the lying direction 64a of the aircraft seat device 46a to be aligned parallel to the aircraft cabin central axis 16a or at an angle of less than 5 degrees to the aircraft cabin central axis 16a. The lying direction 64a of the aircraft seat device 46a is directed towards the aircraft cabin aisle 32a. The aircraft seat device 46a has a housing 66a. The housing 66a is designed as a shell element. The aircraft seat device 46a has a console 68a. The console 68a can be used by two aircraft seat devices arranged directly adjacent to one another, namely the aircraft seat device 46a and the adjacent further aircraft seat device 48'a. The console 68a forms a footwell 76a. The footwell 76a of the console 68a of the aircraft seat device 46a can only be used by a passenger who is staying in a neighboring further aircraft seat area of the neighboring further aircraft seat device 48'a. In addition, the aircraft seat device 46a can also have at least one ottoman. The aircraft seat device 46a has at least one table unit (not shown in more detail). The table unit is arranged on the console 68a of the aircraft seat device 46a. The aircraft seat device 46a has a partition wall 70a. The partition 70a of the aircraft seat device 46a is arranged behind the aircraft seat 56a, viewed in the seat direction 62a. A main direction of extent of the partition wall 70a of the aircraft seat device 46a runs perpendicular to the seat direction 62a. The partition wall 70a of the aircraft seat device 46a has a maximum distance from the aircraft cabin floor 22a which is at least 80% of a maximum distance between the housing 66a and the aircraft cabin floor 22a. The partition wall 70a of the aircraft seat device 46a is provided to permanently optically separate the aircraft seat area of the aircraft seat device 46a from the adjacent further aircraft seat area of the adjacent further aircraft seat device 48'a. The partition wall 70a of the aircraft seat device 46a is in one piece with a partition wall of the adjacent further aircraft seat device 48'a formed. The aircraft seat device 46a has a screen. The screen is arranged on the partition wall 70a. In the present case, the aircraft seat device 46a has two separating units 72a, 74a. A first separating unit 72a of the aircraft seat device 46a is provided to optically separate the aircraft seat area from the aircraft cabin aisle 32a in at least one operating state. The first separating unit 72a of the aircraft seat device 46a is designed to be adjustable. The first separating unit 72a of the aircraft seat device 46a is coupled to the console 68a. A second separating unit 74a of the aircraft seat device 46a is provided to optically separate the aircraft seat area in at least one operating state from another adjacent further aircraft seat area of the other adjacent further aircraft seat device 52a viewed perpendicular to the aircraft cabin central axis 16a. The second separating unit 74a of the aircraft seat device 46a is designed to be adjustable. The second separating unit 74a of the aircraft seat device 46a is coupled to the housing 66a. The second separating unit 74a of the aircraft seat device 46a is formed at least partially in one piece with a second further separating unit of the other adjacent further aircraft seat device 52a. In FIG. 5, the second separating unit 74a of the aircraft seat device 46a is shown fully extended. The aircraft seat device 46a has direct access to the aircraft cabin aisle 32a. A passenger can enter the aircraft seat area of the aircraft seat device 46a directly from the aircraft cabin aisle 32a without crossing another aircraft seat area. The direct access to the aircraft seat device 46a is only assigned to the aircraft seat device 46a. The direct access to the aircraft seat device 46a can only be used from the aircraft seat device 46a.

In the lying position of the aircraft seat device 46a, the housing 66a of the aircraft seat device 46a at least substantially covers a head region 78a of the aircraft seat 56a of the aircraft seat device 46a. An axis, not shown in more detail, which is oriented perpendicular to the aircraft cabin floor 22a, intersects the housing 66a of the aircraft seat device 46a and the head region 78a of the aircraft seat 56a of the aircraft seat device 46a in the lying position. The housing 66a has an upper end above the head region 78a in the lying position, which at least in sections forms an at least substantially straight edge 80a, which is oriented at least substantially perpendicular to the seat direction 62a of the aircraft seat device 46a, preferably viewed perpendicular to a plane which is oriented parallel to the aircraft cabin floor 22a. The housing 66a extends from the at least substantially straight edge 80a to a storage surface 82a of the aircraft seat device 46a, the storage surface 82a being arranged between the at least substantially straight edge 80a and the aircraft cabin floor 22a. A length of this extension corresponds to, parallel to the aircraft cabin floor 22a and measured in the seat direction 62a, at least 30 cm and at most 50 cm. The housing 66a has a bevel 84a in front of the aircraft seat 56a when viewed in the seat direction 62a. The slope 84a is designed as a flat area of the housing 66a. The slope 84a has an angle of at least 10 degrees with respect to an axis which is oriented perpendicular to the aircraft cabin floor 22a. The slope 84a is inclined towards the aircraft seat 56a of the aircraft seat device 46a. A space behind the backrest 60a can advantageously be optimized for a passenger by means of the incline 84a. The incline 84a can advantageously increase privacy and comfort. Furthermore, an improved view between the further aircraft seat 88a of the further aircraft seat device 48a and another neighboring aircraft seat of the other neighboring aircraft seat device 50a can be made possible by means of the bevel 84a (see FIGS. 3 to 5). As a result, couples traveling together can advantageously communicate easily and conveniently with one another. By means of the incline 84a, open aircraft seat areas with an advantageously large spatial effect can advantageously be provided. The housing 66a has a noise-reducing material on a side facing the aircraft seat 56a. On the side facing the aircraft seat 56a, the housing 66a has a lighting unit (not shown in greater detail) which is provided to illuminate the aircraft seat 56a, preferably selectively. In the present case, the aircraft seat device 46a can have a storage element 86a arranged on the housing 66a (FIG. 4). The storage element 86a is arranged on the slope 84a of the housing 66a. The storage element 86a is designed to be foldable. The storage element 86a has an additional storage surface which is semicircular. In a folded-out position of the storage element 86a, the additional storage surface is aligned at least essentially parallel to the aircraft cabin floor 22a. The additional storage area is in a folded-in position of the storage element 86a aligned at least substantially parallel to the slope 84a. Additionally or alternatively, it would also be conceivable for the storage element 86a to have a display element which can preferably be viewed at least in the lying position. Additionally or alternatively, it would also be conceivable for the storage element 86a to have a flap and / or a holder, for example for a tablet PC.

The further aircraft seat device 48a is provided to be raised on the aircraft cabin floor 22a of the aircraft cabin 12a. The further aircraft seat device 48a forms a further aircraft seat area. The further aircraft seat device 48a has a further aircraft seat 88a. The further aircraft seat 88a is arranged in the further aircraft seat area. The further aircraft seat 88a is provided to provide a seat for a passenger in the aircraft 10a. A maximum spacing of the aircraft seat 56a of the aircraft seat device 46a has a greater spacing from the aircraft cabin aisle 32a than a maximum further spacing of the further aircraft seat 88a of the further aircraft seat device 48a from the aircraft cabin aisle 32a. The further aircraft seat 88a is designed as a full-flat seat. The further aircraft seat 88a comprises a further seat bottom 90a. The further aircraft seat 88a comprises a further backrest 92a. The further aircraft seat 88a comprises two further armrests. In addition, it would be conceivable that the further aircraft seat 88a comprises a further leg support. In principle, the further aircraft seat 88a can comprise further additional add-on parts, such as preferably a further headrest. The further aircraft seat device 48a is adjustable between a sitting position and a lying position. The further aircraft seat 88a is electromechanically adjustable between the sitting position and the lying position. The further aircraft seat device 48a comprises at least one further adjustment unit, not shown in detail, which is provided to adjust the further aircraft seat 88a between the sitting position and the lying position. The further aircraft seat 88a of the further aircraft seat device 48a is designed to be non-rotatable with regard to a movement about an axis perpendicular to the aircraft cabin floor 22a. In Figures 2 and 4, the further aircraft seat device 48a is shown in the seated position. In Figures 3 and 5, the further aircraft seat device 48a is shown in the lying position. The further aircraft seat device 48a has a further seat direction 94a. The seat direction 62a of the aircraft seat device 46a is opposite to the further seat direction 94a of the further aircraft seat device 48a aligned. The further seat direction 94a of the further aircraft seat device 48a has a directional component opposite to the flight direction 24a. The further seat direction 94a of the further aircraft seat device 48a is oriented at an angle of at least 5 degrees to the aircraft cabin central axis 16a. The further seat direction 94a of the further aircraft seat device 48a is directed away from the aircraft cabin aisle 32a. Alternatively, it would also be conceivable for the further seat direction 94a of the further aircraft seat device 48a to be aligned parallel to the aircraft cabin central axis 16a or at an angle of less than 5 degrees to the aircraft cabin central axis 16a. The further aircraft seat device 48a has a further lying direction 96a. The lying direction 64a of the aircraft seat device 46a is oriented opposite to the further lying direction 96a of the further aircraft seat device 48a. The further sitting direction 94a corresponds to the further lying direction 96a. The further lying direction 96a of the further aircraft seat device 48a has a directional component opposite to the flight direction 24a. The further lying direction 96a of the further aircraft seat device 48a is oriented at an angle of at least 5 degrees to the aircraft cabin central axis 16a. The further lying direction 96a of the further aircraft seat device 48a is directed away from the aircraft cabin aisle 32a. Alternatively, it would also be conceivable for the further lying direction 96a of the further aircraft seat device 48a to be aligned parallel to the aircraft cabin central axis 16a or at an angle of less than 5 degrees to the aircraft cabin central axis 16a. The further aircraft seat device 48a has a further housing 98a. The further housing 98a is designed as a shell element. The further housing 98a of the further aircraft seat device 48a is formed in one piece with the housing 66a of the aircraft seat device 46a. The further aircraft seat device 48a has a further console 100a. A maximum distance of the console 68a of the aircraft seat device 46a has a smaller distance to the aircraft cabin aisle 32a than a maximum further distance of the further console 100a of the further aircraft seat device 48a to the aircraft cabin aisle 32a. The further console 100a can be used by two aircraft seat devices arranged directly adjacent to one another, namely the adjacent aircraft seat device 46'a and the further aircraft seat device 48a. The further console 100a forms a further footwell 108a. The further footwell 108a of the further console 100a of the further aircraft seat device 48a can only be used by a passenger, which is located in an adjacent aircraft seat area of the adjacent aircraft seat device 46'a. In addition, the further aircraft seat device 48a can also have at least one further ottoman. The further aircraft seat device 48a has at least one further table unit (not shown in more detail). The further table unit is arranged on the further console 100a of the further aircraft seat device 48a. The further aircraft seat device 48a has a further partition wall 102a. The further partition wall 102a of the further aircraft seat device 48a is arranged behind the further aircraft seat 88a, viewed in the further seat direction 94a. A fluff extension direction of the further partition wall 102a of the further aircraft seat device 48a runs perpendicular to the further seat direction 94a. The further partition wall 102a of the further aircraft seat device 48a has a maximum distance from the aircraft cabin floor 22a which is at least 80% of a maximum distance between the further housing 98a and the aircraft cabin floor 22a. The further partition 102a of the further aircraft seat device 48a is provided to permanently optically separate the further aircraft seat area of the further aircraft seat device 48a from the adjacent aircraft seat area of the adjacent aircraft seat device 46'a. The further partition 102a of the further aircraft seat device 48a is designed in one piece with a partition wall of the adjacent aircraft seat device 46'a. The further aircraft seat device 48a has a further screen. The further screen is arranged on the further partition wall 102a. In the present case, the further aircraft seat device 48a has two further separating units 104a, 106a. A first further separating unit 104a of the further aircraft seat device 48a is provided to optically separate the further aircraft seat area from the aircraft cabin aisle 32a in at least one operating state. The first further separating unit 104a of the further aircraft seat device 48a is designed to be adjustable. The first further separating unit 104a of the further aircraft seat device 48a is coupled to the further separating wall 102a. A second further separating unit 106a of the further aircraft seat device 48a is provided to optically separate the further aircraft seat area in at least one operating state from another adjacent aircraft seat area of the other adjacent aircraft seat device 50a viewed perpendicular to the aircraft cabin central axis 16a. The second further separating unit 106a of the further aircraft seat device 48a is designed to be adjustable. The second further separation unit 106a of the further The aircraft seat device 48a is coupled to the further housing 98a. The second further separating unit 106a of the further aircraft seat device 48a is formed at least partially in one piece with a second separating unit of the other adjacent aircraft seat device 50a. In FIG. 5, the second further separating unit 106a of the further aircraft seat device 48a is shown fully extended. The further aircraft seat device 48a has direct access to the aircraft cabin aisle 32a. A passenger can enter the further aircraft seat area of the further aircraft seat device 48a directly from the aircraft cabin aisle 32a without crossing another aircraft seat area. The direct access to the further aircraft seat device 48a is only assigned to the further aircraft seat device 48a. The direct access to the further aircraft seat device 48a can only be used from the further aircraft seat device 48a.

The further housing 98a of the further aircraft seat device 48a at least essentially covers a further head region 110a of the further aircraft seat 88a of the further aircraft seat device 48a in the lying position of the further aircraft seat device 48a. An axis, not shown in more detail, which is oriented perpendicular to the aircraft cabin floor 22a, intersects the further housing 98a of the further aircraft seat device 48a and the further head region 110a of the further aircraft seat 88a of the further aircraft seat device 48a in the lying position. The further housing 98a has a further upper end above the further head region 110a in the lying position, which at least in sections forms a further at least substantially straight edge 112a which is oriented perpendicular to the seat direction 94a of the further aircraft seat device 48a, preferably perpendicular to a plane considered, which is aligned parallel to the aircraft cabin floor 22a. The further housing 98a extends from the further at least substantially straight edge 112a to a further storage surface 114a of the further aircraft seat device 48a, the further storage surface 114a being arranged between the at least substantially straight edge 112a and the aircraft cabin floor 22a. A length of this extension corresponds, parallel to the aircraft cabin floor 22a and measured in the seat direction 94a, to at least 30 cm and at most 50 cm. The further storage surface 114a is part of the further console 100a. The further housing 98a, viewed in the further seat direction 94a, points in front of the further aircraft seat 88a on a further slope 116a. The further slope 116a is designed as a flat area of the further housing 98a. The further incline 116a has an angle of at least 10 degrees with respect to an axis which is oriented perpendicular to the aircraft cabin floor 22a. The further slope 116a is inclined towards the further aircraft seat 88a of the further aircraft seat device 48a. A space behind the further backrest 92a can advantageously be optimized for a passenger by means of the further incline 116a. The further incline 116a can advantageously increase privacy and comfort. Furthermore, an advantageously convenient passage between the aircraft seat 56a of the aircraft seat device 46a and the aircraft cabin aisle 32a can be provided by means of the further bevel 118a. Furthermore, by means of the further incline 118a, service in the aircraft seat area of the aircraft seat device 46a can advantageously be carried out simply and safely by a crew. An advantageously open aircraft seat area with an advantageously large spatial effect can be provided by means of the further incline 118a. Furthermore, a passage from the aircraft cabin aisle 32a to the aircraft seat 56a of the aircraft seat device 46a can advantageously be widened by the further slope 116a of the further housing 98a of the further aircraft seat device 48a. The further housing 98a has a noise-reducing material on a side facing the further aircraft seat 88a. The further housing 98a has, on the side facing the further aircraft seat 88a, a further lighting unit (not shown in more detail) which is provided to illuminate the further aircraft seat 88a, preferably selectively. In the present case, the further aircraft seat device 48a can have a further storage element 118a arranged on the further housing 98a (FIG. 4). The further storage element 118a is arranged on the further incline 116a of the further housing 98a. The further storage element 118a is designed to be foldable. The further storage element 118a has an additional further storage surface which is semicircular. In a folded-out position of the further storage element 118a, the additional further storage surface is aligned at least essentially parallel to the aircraft cabin floor 22a. In a folded-in position of the further storage element 118a, the additional further storage surface is aligned at least essentially parallel to the further incline 116a. Additionally or alternatively, it would also be conceivable that the further storage element 118a has a further display element, which is preferably visible at least in the lying position. Additionally or alternatively would be it is also conceivable that the further storage element 118a has a further flap and / or a further holder, for example for a tablet PC.

The seat direction 62a of the aircraft seat device 46a is formed at least essentially parallel to the further seat direction 94a of the further aircraft seat device 48a. The lying direction 64a of the aircraft seat device 46a is formed at least essentially parallel to the further lying direction 96a of the further aircraft seat device 48a. The lying direction 64a of the aircraft seat device 46a and the further lying direction 96a of the further aircraft seat device 48a are angled at the same angle to the aircraft cabin central axis 16a. The lying direction 64a of the aircraft seat device 46a and the further lying direction 96a of the further aircraft seat device 48a are aligned at least essentially parallel to one another. The reclining direction 64a and the further reclining direction 96a are ideally aligned with the aircraft seat device 46a and the further aircraft seat device 48a, an actual reclining direction defined by a passenger deviating from the reclining direction 64a and / or the further reclining direction 96a, preferably due to an asymmetrical posture of the passenger can.

The aircraft seat device 46a at least partially intersects the aircraft cabin center plane. An outer contour of the aircraft seat device 46a projected onto the aircraft cabin floor 22a at least partially intersects the aircraft cabin center plane. The projected outer contour of the aircraft seat device 46a has a shape that is designed to correspond to an outer contour of the other adjacent aircraft seat device 50a and the other adjacent further aircraft seat device 52a that is mirrored over the aircraft cabin center axis 16a. The further aircraft seat device 48a is spaced apart from the aircraft cabin center plane. The further aircraft seat device 48a does not intersect the aircraft cabin center plane.

An axis not shown in more detail perpendicular to the aircraft cabin central axis 16a intersects the aircraft seat 56a of the aircraft seat device 46a and the further aircraft seat 88a of the further aircraft seat device 48a in the seat position of the aircraft seat device 46a and the further aircraft seat device 48a in the first seat gap 36a. The axis perpendicular to the aircraft cabin center axis 16a intersects the first Seat column 36a and the second seat column 38a the aircraft seat 56a of the aircraft seat device 46a and the further aircraft seat 88a of the further aircraft seat device 48a in the seat position of the aircraft seat device 46a and the further aircraft seat device 48a. The axis perpendicular to the aircraft cabin central axis 16a intersects the backrest 60a of the aircraft seat 56a of the aircraft seat device 46a and the further backrest 92a of the further aircraft seat 88a of the further aircraft seat device 48a in the seat position of the aircraft seat device 46a and the further aircraft seat device 48a. The axis is aligned parallel to the aircraft cabin floor 22a. In the common first seat gap 36a, exactly two backrests are arranged side by side, namely the backrest 60a of the aircraft seat 56a of the aircraft seat device 46a and the further backrest 92a of the further aircraft seat 88a of the further aircraft seat device 48a. The axis intersects exactly two backrests in the first seat column 36a and the second seat column 38a, namely the backrest 60a of the aircraft seat 56a of the aircraft seat device 46a and the further backrest 92a of the further aircraft seat 88a of the further aircraft seat device 48a.

An axis not shown in more detail perpendicular to the aircraft cabin central axis 16a intersects a shoulder region 120a of the aircraft seat device 46a and a further shoulder region 122a of the further aircraft seat device 48a in the lying position of the aircraft seat device 46a and the further aircraft seat device 48a. The axis is aligned parallel to the aircraft cabin floor 22a. The axis intersects exactly two shoulder areas 120a, 122a in the first seat gap 36a. The axis intersects exactly two shoulder areas 120a, 122a in the first seat column 36a and in the second seat column 38a.

An axis not shown in more detail perpendicular to the aircraft cabin central axis 16a and parallel to the aircraft cabin floor 22a intersects the console 68a of the aircraft seat device 46a and another adjacent further aircraft seat of the other neighboring further aircraft seat device 52a in the seat position.

An axis not shown in more detail perpendicular to the aircraft cabin central axis 16a and parallel to the aircraft cabin floor 22a intersects the further aircraft seat 88a of the further aircraft seat device 48a in the seat position and another adjacent console of the other adjacent aircraft seat device 50a. An axis not shown in more detail perpendicular to the aircraft cabin central axis 16a intersects the seat bottom 58a of the aircraft seat 56a of the aircraft seat device 46a and another adjacent further seat bottom of the other adjacent further aircraft seat of the other adjacent further aircraft seat device 52a in the seat position of the aircraft seat device 46a and the other neighboring further aircraft seat device 52a .

An axis not shown in more detail perpendicular to the aircraft cabin central axis 16a intersects the further seat bottom 90a of the further aircraft seat 88a of the further aircraft seat device 48a and another adjacent seat bottom of another adjacent aircraft seat of the other adjacent aircraft seat device 50a in the seat position of the further aircraft seat device 48a and the other adjacent aircraft seat device 50a .

The previously described features for the aircraft seat device 46a and the further aircraft seat device 48a in the first seat column 36a are basically also valid for the second seat column 38a, with all elements of the second seat column 38a mirrored over the aircraft cabin central axis 16a, but offset along a longitudinal axis of the aircraft relative to the first seat column 36a are formed. For the third seat column 40a, the description of the aircraft seat device 46a and the further aircraft seat device 48a from the first seat column 36a can in principle be used. In principle, the description of the second seat column 38a can be used for the fourth seat column 42a.

In principle, the aircraft seat arrangement 14a shown in FIG. 2 is not limited to the number of aircraft seat devices shown. The aircraft seat arrangement 14a can have fewer or more than the aircraft seat devices shown. In principle, it would also be conceivable for the aircraft seat arrangement 14a shown in FIG. 2 to be arranged in whole or in part, preferably at least one of the seat gaps 36a, 38a, 40a, 42a, mirrored about an axis in the aircraft cabin 12a, the axis being perpendicular to the aircraft cabin central axis 16a and is aligned parallel to the aircraft cabin floor 22a.

In the figures 6 to 13 three further embodiments of the invention are shown. The following descriptions and drawings are essentially limited to the differences between the exemplary embodiments, with reference to the drawings and / or the description of the other exemplary embodiments, in particular FIGS. 1 to 5, in principle also with regard to components with the same designation, in particular with regard to components with the same reference numerals. To distinguish the exemplary embodiments, the letter a is placed after the reference numerals of the exemplary embodiment in FIGS. 1 to 5. In the exemplary embodiments of FIGS. 6 to 13, the letter a is replaced by the letters b to d.

Figures 6 to 9 show an aircraft seat arrangement 14b in a second embodiment. The aircraft seat arrangement 14b is provided for use in a partially illustrated aircraft cabin 12b of an aircraft. The aircraft cabin 12b has an aircraft cabin central axis 16b. The aircraft cabin center axis 16b is designed as a longitudinal axis of the aircraft. The aircraft cabin center axis 16b is at the same distance from opposite aircraft cabin outer walls 18b, 20b of the aircraft cabin 12b. The aircraft cabin central axis 16b is aligned parallel to an aircraft cabin floor 22b of the aircraft cabin 12b. The aircraft cabin 12b has an aircraft cabin center plane (not shown in greater detail). The aircraft has a flight direction 24b in at least one operating state. In the present case, the flight direction 24b is ideally aligned parallel to the aircraft cabin central axis 16b. The aircraft cabin 12b has an aircraft cabin section 26b along the aircraft cabin central axis 16b. In the present case, the aircraft cabin section 26b is delimited by several aircraft cabin separating elements 28b and by several schematically illustrated aircraft cabin modules 30b along the aircraft cabin central axis 16b. The aircraft cabin 12b has two aircraft cabin aisles 32b, 34b in the aircraft cabin section 26b. The aircraft cabin 12b has an aircraft cabin aisle 32b. The aircraft cabin 12b has a further aircraft cabin aisle 34b.

In the present case, the aircraft seat arrangement 14b comprises three seat gaps 36b, 40b, 42b. The three seat gaps 36b, 40b, 42b each extend in the flight direction 24b.

The aircraft seat arrangement 14b comprises a first seat column 36b. The first seat column 36b is designed as an inner seat column. The aircraft cabin 12b has a central region 44b. The central area 44b is of the two aircraft cabin aisles 32b, 34b limited. The first seat column 36b is arranged in the central region 44b. A maximum extent of the first seat gaps 36b measured perpendicular to the aircraft cabin central axis 16b and parallel to the aircraft cabin floor 22b corresponds to a minimum distance between the aircraft cabin aisle 32b and the further aircraft cabin aisle 34b. The first seat gap 36b at least substantially completely fills the central region 44b, viewed perpendicular to the aircraft cabin central axis 16b and parallel to the aircraft cabin floor 22b. The aircraft seat arrangement 14b comprises a second seat column 40b. The second seat column 40b is designed as a first outer seat column. The first seat gaps 36b and the second seat gaps 40b are spaced apart from one another by the aircraft cabin aisle 32b. The aircraft seat arrangement 14b comprises a third seat column 42b. The third seat column 42b is designed as a second outer seat column. The first seat column 36b and the third seat column 42b are spaced apart from one another by the further aircraft cabin aisle 34b. In the present case, the third seat gap 42b is formed symmetrically to the second seat gap 40b over the aircraft cabin center axis 16b.

The aircraft seat arrangement 14b comprises an aircraft seat device 46b. The aircraft seat device 46b is arranged in the first seat gap 36b. The aircraft seat device 46b intersects the aircraft cabin center plane. The aircraft seat arrangement 14b comprises a further aircraft seat device 48b. The further aircraft seat device 48b is arranged in the first seat gap 36b. The further aircraft seat device 48b intersects the aircraft cabin center plane. The aircraft seat device 46b and the further aircraft seat device 48b are arranged at least partially next to one another in a common seat gap, namely the first seat gap 36b. The aircraft seat device 46b and the further aircraft seat device 48b are arranged in the first seat gap 36b, viewed perpendicular to the aircraft cabin central axis 16b, at least partially overlapping one another. The aircraft seat device 46b and the further aircraft seat device 48b are arranged directly adjacent to one another in the first seat gap 36b. The aircraft seat device 46b and the further aircraft seat device 48b are arranged in the first seat column directly one behind the other and directly next to one another. The aircraft seat device 46b and the further aircraft seat device 48b each have direct access to different aircraft cabin aisles 32b, 34b. The aircraft seat arrangement 14b comprises an adjacent aircraft seat device 46'b. The adjacent aircraft seat device 46'b is at least essentially identical to the aircraft seat device 46b. The adjacent aircraft seat device 46'b is arranged in the first seat gap 36b. The adjacent aircraft seat device 46'b is arranged adjacent to the aircraft seat device 46b along a longitudinal axis of the aircraft. The adjacent aircraft seat device 46'b is arranged immediately behind the aircraft seat device 46b when viewed in the direction of flight 24b.

The aircraft seat arrangement 14b comprises an adjacent further aircraft seat device 48'b. The adjacent further aircraft seat device 48'b is at least essentially identical to the further aircraft seat device 48b. The adjacent further aircraft seat device 48'b is arranged in the first seat column 36b. The adjacent further aircraft seat device 48'b is arranged adjacent to the further aircraft seat device 48b along a longitudinal axis of the aircraft. The adjacent further aircraft seat device 48'b is arranged immediately in front of the further aircraft seat device 48b when viewed in the direction of flight 24b.

The aircraft seat device 46b and the further aircraft seat device 48b form a seat grouping 54b of the aircraft seat arrangement 14b. The grouping of seats 54b forms a, preferably periodically, repeatable sequence. In the present case, the aircraft seat arrangement 14b comprises six seat groupings 54b, 54'b, 54 ”b, 54” '”b, 54” ”b, 54”' ”b, which are arranged directly one behind the other in the first seat column 36b, each consisting of the aircraft seat device 46b and the further aircraft seat device 48b are formed. The six seat groupings 54b, 54'b, 54 "b, 54" "b, 54" "b, 54" "b, which are arranged directly one behind the other in the first seat column 36b, are designed identically.

The aircraft seat device 46b forms an aircraft seat area. The aircraft seat device 46b has an aircraft seat 56b. The aircraft seat 56b is designed as a full flat seat. The aircraft seat 56b includes a seat bottom 58b. The aircraft seat 56b includes a backrest 60b. The aircraft seat 56b includes two armrests. The aircraft seat device 46b is adjustable between a sitting position and a lying position. The aircraft seat 56b is electromechanically adjustable between the sitting position and the lying position. In FIGS. 6 to 8, the aircraft seat device 46b is shown in the seated position. In FIG. 9, the aircraft seat device 46b is shown in the lying position. The aircraft seat assembly 46b has a seat direction 62b. The aircraft seat device 46b has a lying direction 64b. The sitting direction 62b corresponds to the lying direction 64b. The lying direction 64b of the aircraft seat device 46b has a directional component in the flight direction 24b. The lying direction 64b of the aircraft seat device 46b is oriented at an angle of at least 30 degrees to the aircraft cabin central axis 16b. The lying direction 64b of the aircraft seat device 46b is directed away from the aircraft cabin aisle 32b. The aircraft seat device 46b has a housing 66b. The housing 66b is designed as a shell element. The housing 66b of the aircraft seat device 46b is preferably formed in one piece with an adjacent further housing of the adjacent further aircraft seat device 48'b. The aircraft seat device 46b has a console 68b. The console 68b can be used by at least two aircraft seat devices arranged directly adjacent to one another, namely the aircraft seat device 46b and the further aircraft seat device 48b. The console 68b intersects the aircraft cabin midplane. The aircraft seat device 46b has a screen. The screen is arranged on the console 68b. The aircraft seat device 46b has a table unit 124b. The table unit 124b is arranged on the housing 66b of the aircraft seat device 46b. In the present case, the aircraft seat device 46b has a separating unit 72b. The separating unit 72b of the aircraft seat device 46b is provided to optically separate the aircraft seat area from the aircraft cabin aisle 32b in at least one operating state. The separating unit 72b of the aircraft seat device 46b is designed to be adjustable. The separating unit 72b of the aircraft seat device 46b is coupled to the housing 66b. The aircraft seat device 46b has direct access to the aircraft cabin aisle 32b. A passenger can enter the aircraft seat area of the aircraft seat device 46b directly from the aircraft cabin aisle 32b without crossing another aircraft seat area. The direct access to the aircraft seat device 46b is only assigned to the aircraft seat device 46b. The direct access to the aircraft seat device 46b can only be used from the aircraft seat device 46b.

The further aircraft seat device 48b forms a further aircraft seat area. The further aircraft seat device 48b has a further aircraft seat 88b. The further aircraft seat 88b is designed as a full-flat seat. A maximum further distance between the further aircraft seat 88b and the further aircraft seat device 48b has a greater distance from the aircraft cabin aisle 32b than a maximum distance from the aircraft seat 56b of the aircraft seat device 46b to the aircraft cabin aisle 32b. The further aircraft seat 88b comprises a further seat bottom 90b. The further aircraft seat 88b comprises a further backrest 92b. The further aircraft seat 88b comprises two further armrests. The further aircraft seat device 48b can be adjusted between a sitting position and a lying position. The further aircraft seat 88b is electromechanically adjustable between the sitting position and the lying position. In FIGS. 6 to 8, the further aircraft seat device 48b is shown in the seated position. In the figure 9, the further aircraft seat device 48b is shown in the lying position. The further aircraft seat device 48b has a further seat direction 94b. The seat direction 62b of the aircraft seat device 46b is oriented opposite to the further seat direction 94b of the further aircraft seat device 48b. The further aircraft seat device 48b has a further lying direction 96b. The lying direction 64b of the aircraft seat device 46b is oriented opposite to the further lying direction 96b of the further aircraft seat device 48b. The further sitting direction 94b corresponds to the further lying direction 96b. The further lying direction 96b of the further aircraft seat device 48b has a directional component opposite to the flight direction 24b. The further lying direction 96b of the further aircraft seat device 48b is oriented at an angle of at least 30 degrees to the aircraft cabin central axis 16b. The further lying direction 96b of the further aircraft seat device 48b is directed away from the further aircraft cabin aisle 34b. The further aircraft seat device 48b has a further housing 98b. The further housing 98b is designed as a shell element. The further housing 98b of the further aircraft seat device 48b is preferably formed in one piece with an adjacent housing of the adjacent aircraft seat device 46'b. The further aircraft seat device 48b has a further console 100b. The further console 100b intersects the aircraft cabin center plane. A minimal distance between the console 68b of the aircraft seat device 46b and the aircraft cabin aisle 32b is the same as a minimal further distance between the further console 100b of the further aircraft seat device 48b and the further aircraft cabin aisle 34b. The further console 100b can be used by at least two aircraft seat devices arranged directly adjacent to one another, namely the aircraft seat device 46b and the further aircraft seat device 48b. The further aircraft seat device 48b has another screen. The further screen is arranged on the further console 100b. The further screen is preferably designed to be displaceable towards the aircraft cabin floor 22b. The further screen can in principle also be designed to be pivotable about an axis parallel to the aircraft cabin floor 22b. This makes it possible to provide an advantageously optimal viewability of the further screen in the lying position of the further aircraft seat device 48b. The further aircraft seat device 48b has a further table unit 126b. The further table unit 126b is arranged on the further console 100b of the further aircraft seat device 48b. In the present case, the further aircraft seat device 48b has a further separating unit 104b. The further separating unit 104b of the further aircraft seat device 48b is provided to optically separate the further aircraft seat area from the further aircraft cabin aisle 34b in at least one operating state. The further separating unit 104b of the further aircraft seat device 48b is designed to be adjustable. The further separating unit 104b of the further aircraft seat device 48b is coupled to the further housing 98b. The further aircraft seat device 48b has direct access to the further aircraft cabin aisle 34b. A passenger can enter the further aircraft seat area of the further aircraft seat device 48b directly from the further aircraft cabin aisle 34b without crossing another aircraft seat area. The direct access to the further aircraft seat device 48b is only assigned to the further aircraft seat device 48b. The direct access to the further aircraft seat device 48b can only be used from the further aircraft seat device 48b.

The seat direction 62b of the aircraft seat device 46b is formed at least essentially parallel to the further seat direction 94b of the further aircraft seat device 48b. The seat direction 62b of the aircraft seat device 46b and the further seat direction 94b of the further aircraft seat device 48b are directed towards one another. The reclining direction 64b of the aircraft seat device 46b is formed at least substantially parallel to the further reclining direction 96b of the further aircraft seat device 48b. The lying direction 64b of the aircraft seat device 46b and the further lying direction 96b of the further aircraft seat device 48b are directed towards one another. The lying direction 64b of the aircraft seat device 46b and the further lying direction 96b of the further aircraft seat device 48b are at the same angle to the Aircraft cabin center axis 16b angled. The lying direction 64b of the aircraft seat device 46b and the further lying direction 96b of the further aircraft seat device 48b are aligned at least essentially parallel to one another. The reclining direction 64b and the further reclining direction 96b are ideally aligned with the aircraft seat device 46b and the further aircraft seat device 48b, an actual reclining direction defined by a passenger deviating from the reclining direction 64b and / or the further lying direction 96b, preferably due to an asymmetrical posture of the passenger can.

A seat center axis 128b of the aircraft seat 56b of the aircraft seat device 46b intersects the further seat bottom 90b of the further aircraft seat 88b of the further aircraft seat device 48b, viewed perpendicular to the aircraft cabin floor 22b (FIG. 7). The seat center axis 128b of the aircraft seat 56b is aligned parallel to a further seat center axis 130b of the further aircraft seat 88b of the further aircraft seat device 48b. The seat center axis 128b and the further seat center axis 130b are spaced apart from one another in the present case, viewed perpendicular to the aircraft cabin floor 22b. In principle, it would also be conceivable that the seat center axis 128b of the aircraft seat 56b of the aircraft seat device 46b and the further seat center axis 130b of the further aircraft seat 88b of the further aircraft seat device 48b are arranged in a plane which is oriented perpendicular to the aircraft cabin floor 22b. The seat center axis 128b of the aircraft seat 56b of the aircraft seat device 46b intersects the aircraft cabin center axis 16b at an intersection which, viewed in the direction of flight 24b, lies behind an intersection point of the further seat center axis 130b of the further aircraft seat 88b of the further aircraft seat device 48b with the aircraft cabin center axis 16b.

The aircraft seat device 46b has a footwell 132b (FIG. 9). The footwell 132b is provided for placing at least one foot in the lying position of the aircraft seat device 46b. The footwell 132b of the aircraft seat device 46b is arranged in the console 68b of the aircraft seat device 46b. The console 68b forms the footwell 132b. The footwell 132b of the aircraft seat device 46b can only be used by a passenger who is in the aircraft seat area of the aircraft seat device 46b. The aircraft seat device 46b has a foot and / or legrest element 134b. The foot and / or leg support element 134b of the aircraft seat device 46b is arranged at least substantially in the footwell 132b of the aircraft seat device 46b.

The further aircraft seat device 48b has a further footwell 136b (FIG. 9). The further footwell 136b is provided for placing at least one foot in the lying position of the further aircraft seat device 48b. The further footwell 136b of the further aircraft seat device 48b is arranged in the further console 100b of the further aircraft seat device 48b. The further console 100b forms the further footwell 136b. The further footwell 136b of the further aircraft seat device 48b can only be used by a passenger who is in the further aircraft seat area of the further aircraft seat device 48b. The further aircraft seat device 48b has a further foot and / or leg support element 138b. The further foot and / or leg support element 138b of the further aircraft seat device 48b is arranged at least essentially in the further footwell 136b of the further aircraft seat device 48b. The footwell 132b of the aircraft seat device 46b and the further footwell 136b of the further aircraft seat device 48b, viewed perpendicular to the aircraft cabin floor 22b, are arranged so as to overlap one another. The footwell 132b of the aircraft seat device 46b is arranged between the aircraft cabin floor 22b and the further footwell 136b of the further aircraft seat device 48b.

In FIG. 9, the aircraft seat 56b and the further aircraft seat 88b are shown in the lying position, the aircraft seat 56b and the further aircraft seat 88b being shown in dashed lines in the seated position. In the lying position of the aircraft seat device 46b, the aircraft seat device 46b forms a lying plane 140b, which has a different distance from the aircraft cabin floor 22b than a further lying plane 142b, which is formed by the further aircraft seat device 48b in the lying position of the further aircraft seat device 48b. In the present case, the further lying plane 142b has a smaller minimum distance from the aircraft cabin floor 22b than the lying plane 140b. Alternatively, it would be conceivable that the further lying plane 142b has a greater minimum distance from the aircraft cabin floor 22b than the lying plane 140b. A minimum distance between the lying plane 140b and the further lying plane 142b is perpendicular to measured from the aircraft cabin floor 22b, at least 25 cm. A surface of the backrest 60b of the aircraft seat 56b of the aircraft seat device 46b, a surface of the seat bottom 58b of the aircraft seat 56b of the aircraft seat device 46b and a surface of the foot and / or leg support element 134b of the aircraft seat device 46b form the lying plane 140b. The surface of the backrest 60b, the surface of the seat bottom 58b and the surface of the foot and / or leg support element 134b face away from the aircraft cabin floor 22b in the lying position. The seat bottom 58b of the aircraft seat 56b of the aircraft seat device 46b is provided to be lowered to the aircraft cabin floor 22b when moving from the seated position to the lying position. Alternatively, it would be conceivable that the seat bottom 58b of the aircraft seat 56b of the aircraft seat device 46b is provided to be raised from the aircraft cabin floor 22b during a transfer from the seated position to the lying position. A surface of the further backrest 92b of the further aircraft seat 88b of the further aircraft seat device 48b, a surface of the further seat bottom 90b of the further aircraft seat 88b of the further aircraft seat device 48b and a surface of the further foot and / or leg support element 138b of the further aircraft seat device 48b form the further lying level 142b the end. The surface of the further backrest 92b, the surface of the further seat bottom 90b and the surface of the further foot and / or leg support element 138b face away from the aircraft cabin floor 22b in the lying position. The further seat floor 90b of the further aircraft seat 88b of the further aircraft seat device 48b is provided to be raised from the aircraft cabin floor 22b when the seat position is transferred to the lying position. Alternatively, it would be conceivable that the further seat bottom 90b of the further aircraft seat 88b of the further aircraft seat device 48b is provided to be lowered to the aircraft cabin floor 22b when moving from the seated position to the lying position.

The aircraft seat device 46b and the further aircraft seat device 48b comprise a common console 144b. The console 68b of the aircraft seat device 46b and the further console 100b of the further aircraft seat device 48b are designed in one piece. The console 68b of the aircraft seat device 46b and the further console 100b of the further aircraft seat device 48b are perpendicular to the Aircraft cabin floor 22b viewed, arranged at least partially overlapping one another. The console 68b of the aircraft seat device 46b and the further console 100b of the further aircraft seat device 48b form the common console 144b. The common bracket 144b is cuboid. The common console 144b intersects the aircraft cabin midplane. The common console 144b is arranged between the aircraft seat 56b of the aircraft seat device 46b and the further aircraft seat 88b of the further aircraft seat device 48b. The common console 144b is arranged between an adjacent aircraft seat of the adjacent aircraft seat device 46'b and an adjacent further aircraft seat of the adjacent further aircraft seat device 48'b. The common console 144b is at a maximum distance from the aircraft cabin floor 22b, which is at least 90% of a maximum distance between the housing 66b and / or the further housing 98b and the aircraft cabin floor 22b.

The common console 144b can be partially used from the adjacent aircraft seat device 46'b. The common console 144b can be partially used from the adjacent further aircraft seat device 48'b. The common console 144b can be used by the neighboring aircraft seat device 46'b and the neighboring further aircraft seat device 48'b. An axis not shown in more detail perpendicular to the aircraft cabin central axis 16b and parallel to the aircraft cabin floor 22b intersects the common console 144b, the adjacent aircraft seat of the adjacent aircraft seat device 46'b in the seat position and the adjacent further aircraft seat of the neighboring further aircraft seat device 48 'in the first seat column 36b. b in the sitting position.

In the common first seat gap 36b, the adjacent aircraft seat device 46‘b and the adjacent further aircraft seat device 48‘b are arranged next to one another.

In the present case, the common bracket 144b has two storage spaces 146b, 148b. The common console 144b has a storage space 146b. The stowage space 146b is only accessible from the adjacent aircraft seat device 46'b. The stowage space 146b is arranged above the footwell 132b and the further footwell 136b. An axis which is oriented perpendicular to the aircraft cabin floor 22b intersects the footwell 132b of the aircraft seat device 46b, the further footwell 136b of the further aircraft seat device 48b and the stowage space 146b of the common console 144b. The common console 144b has a further storage space 148b. The further stowage space 148b is only accessible from the neighboring further aircraft seat device 48'b. The further storage space 148b is arranged above the footwell 132b and the further footwell 136b. An axis which is oriented perpendicular to the aircraft cabin floor 22b intersects the footwell 132b of the aircraft seat device 46b, the further footwell 136b of the further aircraft seat device 48b and the further stowage space 148b of the common console 144b. Between the stowage space 146b and the further stowage space 148b, a partition, not shown in detail, of the common console 144b is arranged.

A plurality of alternative aircraft seat devices are arranged in the second seat column 40b, which are at least substantially identical, but are designed to be mirrored to the aircraft seat device 46b over a longitudinal axis of the aircraft. The multiple alternative aircraft seat devices in the second seat column 40b each have direct access to the same aircraft cabin aisle 32b. In the third seat column 42b, several other aircraft seat devices are arranged, which are at least substantially identical to the aircraft seat device 46b. The previously described features for the aircraft seat device 46b in the first seat column 36b also apply in principle to the third seat column 42b. The several other aircraft seat devices in the third seat column 42b each have direct access to the same further aircraft cabin aisle 34b.

In principle, the aircraft seat arrangement 14b shown in FIG. 6 is not limited to the number of aircraft seat devices shown. The aircraft seat arrangement 14b can have fewer or more than the illustrated aircraft seat devices. In principle, it would also be conceivable that the aircraft seat arrangement 14b shown in FIG is aligned parallel to the aircraft cabin floor 22b.

In the figure 10 an aircraft seat arrangement 14c is shown in a third embodiment. The third embodiment is similar to the second embodiment. the Aircraft seat arrangement 14c is provided for use in a partially illustrated aircraft cabin 12c of an aircraft. The aircraft cabin 12c has an aircraft cabin central axis 16c. The aircraft cabin 12c has an aircraft cabin floor 22c. The aircraft cabin 12c has an aircraft cabin center plane (not shown in greater detail). In at least one operating state, the aircraft has a flight direction 24c. In the present case, the flight direction 24c is ideally aligned parallel to the aircraft cabin central axis 16c. The aircraft cabin 12c has an aircraft cabin aisle 32c. The aircraft cabin 12c has a further aircraft cabin aisle 34c. In the present case, the aircraft seat arrangement 14c comprises three seat columns. The aircraft seat arrangement 14c comprises a first seat column 36c. The first seat column 36c is designed as an inner seat column. The aircraft cabin 12c has a central region 44c. The first seat column 36c is arranged in the central region 44c. The aircraft seat arrangement 14c comprises a second seat column, not shown in detail. The second seat column can be embodied identically to the second seat column 40b from the second exemplary embodiment. The aircraft seat arrangement 14c comprises a third seat column (not shown in greater detail). The third seat column can be designed identically to the third seat column 42b from the second exemplary embodiment.

The aircraft seat arrangement 14c comprises an aircraft seat device 46c. The aircraft seat device 46c is arranged in the first seat gap 36c. The aircraft seat arrangement 14c comprises a further aircraft seat device 48c. The further aircraft seat device 48c is arranged in the first seat gap 36c. The aircraft seat device 46c and the further aircraft seat device 48c are arranged at least partially next to one another in a common seat column, namely the first seat column 36c. The aircraft seat arrangement 14c comprises an adjacent aircraft seat device 46'c. The adjacent aircraft seat device 46'c is at least essentially identical to the aircraft seat device 46c. The adjacent aircraft seat device 46'c is arranged in the first seat gap 36c. The aircraft seat arrangement 14c comprises an adjacent further aircraft seat device 48'c. The adjacent further aircraft seat device 48'c is at least essentially identical to the further aircraft seat device 48c. The adjacent further aircraft seat device 48'c is arranged in the first seat gap 36c. The aircraft seat device 46c and the further aircraft seat device 48c form one Seat grouping 54c of the aircraft seat arrangement 14c. In the present case, the aircraft seat arrangement 14c comprises at least three seat groupings 54c, 54'c, 54'c, which are arranged directly one behind the other in the first seat column 36c and which are each formed from the aircraft seat device 46c and the further aircraft seat device 48c. The aircraft seat device 46c forms an aircraft seat area. The aircraft seat device 46c has an aircraft seat 56c. The aircraft seat 56c is designed as a full flat seat. The aircraft seat 56c includes a seat bottom 58c. The aircraft seat 56c includes a backrest 60c. The aircraft seat device 46c is adjustable between a sitting position and a lying position. In FIG. 10, the aircraft seat device 46c is shown in the seated position. The aircraft seat device 46c has a seat direction 62c. The aircraft seat device 46c has a lying direction 64c. The sitting direction 62c corresponds to the lying direction 64c. The lying direction 64c of the aircraft seat device 46c has a directional component in the flight direction 24c. The lying direction 64c of the aircraft seat device 46c is oriented at an angle of at least 25 degrees to the aircraft cabin central axis 16c. The aircraft seat device 46c has a housing 66c. The aircraft seat device 46c has a console 68c. The console 68c can be used by two aircraft seat devices arranged directly adjacent to one another, namely the aircraft seat device 46c and the further aircraft seat device 48c. The console 68c intersects the aircraft cabin midplane. In the present case, the aircraft seat device 46c has two separating units 72c, 74c. A first separating unit 72c of the aircraft seat device 46c is provided to optically separate the aircraft seat area from the aircraft cabin aisle 32c in at least one operating state. The aircraft seat device 46c has direct access to the aircraft cabin aisle 32c. The further aircraft seat device 48c forms a further aircraft seat area. The further aircraft seat device 48c has a further aircraft seat 88c. The further aircraft seat 88c is designed as a full flat seat. The further aircraft seat 88c comprises a further seat bottom 90c. The further aircraft seat 88c comprises a further backrest 92c. The further aircraft seat device 48c can be adjusted between a sitting position and a lying position. In the figure 10, the further aircraft seat device 48c is shown in the seat position. The further aircraft seat device 48c has a further seat direction 94c. The seat direction 62c of the aircraft seat device 46c is oriented opposite to the further seat direction 94c of the further aircraft seat device 48c. The other The aircraft seat device 48c has a further lying direction 96c. The lying direction 64c of the aircraft seat device 46c is oriented opposite to the further lying direction 96c of the further aircraft seat device 48c. The further sitting direction 94c corresponds to the further lying direction 96c. The further lying direction 96c of the further aircraft seat device 48c has a directional component opposite to the flight direction 24c. The further lying direction 96c of the further aircraft seat device 48c is oriented at an angle of at least 25 degrees to the aircraft cabin central axis 16c. The further aircraft seat device 48c has a further housing 98c. The further aircraft seat device 48c has a further console 100c. The further console 100c intersects the aircraft cabin center plane. The further console 100c can be used by two aircraft seat devices arranged directly adjacent to one another, namely the aircraft seat device 46c and the further aircraft seat device 48c. In the present case, the further aircraft seat device 48c has two further separating units 104b, 106c. A first further separating unit 104c of the further aircraft seat device 48c is provided to optically separate the further aircraft seat area from the further aircraft cabin aisle 34c in at least one operating state. The further aircraft seat device 48c has direct access to the further aircraft cabin aisle 34c.

The aircraft seat device 46c and the further aircraft seat device 48c comprise a common console 144c. The console 68c of the aircraft seat device 46c and the further console 100c of the further aircraft seat device 48c are designed in one piece. The console 68c of the aircraft seat device 46c and the further console 100c of the further aircraft seat device 48c, viewed perpendicular to the aircraft cabin floor 22c, are arranged at least partially overlapping one another. The console 68c of the aircraft seat device 46c and the further console 100c of the further aircraft seat device 48c form the common console 144c. An axis not shown in more detail perpendicular to the aircraft cabin central axis 16c and parallel to the aircraft cabin floor 22c intersects the common console 144c, an adjacent aircraft seat of the adjacent aircraft seat device 46'c in the seat position and an adjacent further aircraft seat of the neighboring further aircraft seat device 48 'in the first seat column 36c. c in the sitting position. The aircraft seat device 46c has a footwell 132c. The further aircraft seat device 48c has a further footwell 136c. The footwell 132c of the aircraft seat device 46c and the further footwell 136c of the further aircraft seat device 48c, viewed perpendicular to the aircraft cabin floor 22c, are arranged so as to overlap one another. In the lying position of the aircraft seat device 46c, the aircraft seat device 46c forms a lying plane, not shown, which has a different distance from the aircraft cabin floor 22c than a further lying plane, not shown, which is formed by the further aircraft seat device 48c in the lying position of the further aircraft seat device 48c. The seat bottom 58c of the aircraft seat 56c of the aircraft seat device 46c is provided to be lowered to the aircraft cabin floor 22c when moving from the seated position to the lying position. The further seat floor 90c of the further aircraft seat 88c of the further aircraft seat device 48c is provided to be raised from the aircraft cabin floor 22c when the seat position is transferred to the lying position.

The seat direction 62c of the aircraft seat device 46c is formed at least essentially parallel to the further seat direction 94c of the further aircraft seat device 48c. The reclining direction 64c of the aircraft seat device 46c is formed at least substantially parallel to the further reclining direction 96c of the further aircraft seat device 48c. The lying direction 64c and the further lying direction 96c are ideally aligned with the aircraft seat device 46c and the further aircraft seat device 48c, with an actual lying direction defined by a passenger, preferably due to an asymmetrical posture of the passenger, deviating from the lying direction 64c and / or the further lying direction 96c can.

A seat center axis, not shown, of the aircraft seat 56c of the aircraft seat device 46c and a further seat center axis, not shown, of the further aircraft seat 88c of the further aircraft seat device 48c are spaced apart in the present case, viewed perpendicular to the aircraft cabin floor 22c. The seat center axis of the aircraft seat 56c of the aircraft seat device 46c and the further seat center axis of the further aircraft seat 88c of the further aircraft seat device 48c are aligned parallel to one another. In contrast to the second embodiment, a distance between the seat center axis of the aircraft seat 56c of the aircraft seat device 46c and the further seat center axis of the further aircraft seat 88c of the further aircraft seat device 48c is greater than in the second embodiment. In the present case, an axis not shown in more detail, which is aligned parallel to the seat direction 62c and / or the reclining direction 64c of the aircraft seat device 46c, intersects the aircraft seat 56c of the aircraft seat device 46c and the further aircraft seat 88c of the further aircraft seat device 48c. Alternatively, it would be conceivable that the aircraft seat 56c of the aircraft seat device 46c and the further aircraft seat 88c of the further aircraft seat device 48c do not have a common cutting axis that is oriented parallel to the seat direction 62c and / or the lying direction 64c of the aircraft seat device 46c.

In the present case, the common console 144c is cuboid, with two opposite corners of the common console 144c each having a radius of at least 10 cm when viewed perpendicular to the aircraft cabin floor 22c. The radius of the rounding extends parallel to the aircraft cabin floor 22c. Viewed perpendicularly to the aircraft cabin floor 22c, the common console 144c, a housing for the adjacent aircraft seat device 46'c and a further housing for the adjacent further aircraft seat device 48'c form a shape that essentially corresponds to the shape of a paragraph symbol.

The common console 144c can be partially used from the adjacent aircraft seat device 46'c. The common console 144c can be partially used from the adjacent further aircraft seat device 48'c. An axis not shown in more detail perpendicular to the aircraft cabin central axis 16c and parallel to the aircraft cabin floor 22c intersects the common console 144c, the adjacent aircraft seat of the adjacent aircraft seat device 46'c in the seat position and the adjacent further aircraft seat of the neighboring further aircraft seat device 48 'in the first seat gap 36c. c in the sitting position. In the present case, the common bracket 144c has two storage spaces 146c, 148c. The two stowage spaces 146c, 148c are designed similarly to the stowage spaces 146b, 148b from the second exemplary embodiment. The two storage spaces 146c, 148c are each means a closure element closable. In this way, objects can advantageously be prevented from falling out. The closure elements can be designed, for example, as a flap, as a sliding door, as a pleated blind or as a curtain. Between the stowage space 146c and the further stowage space 148c, a partition, not shown in detail, of the common console 144c is arranged.

A second separating unit 74c of the aircraft seat device 46c is provided to optically separate the aircraft seat area in at least one operating state from a further adjacent aircraft seat area of the adjacent further aircraft seat device 48'c, viewed perpendicular to the aircraft cabin central axis 16c. The second separating unit 74c of the aircraft seat device 46c is designed to be adjustable. The second separating unit 74c is provided to fill a free space between the housing 66c and the console 68c. The second separating unit 74c of the aircraft seat device 46c is coupled to the console 68c. The second separating unit 74c of the aircraft seat device 46c is at least partially designed in one piece with a second further separating unit of the adjacent further aircraft seat device 48'c.

A second further separating unit 106c of the further aircraft seat device 48c is provided to optically separate the further aircraft seat area in at least one operating state from an adjacent aircraft seat area of the adjacent aircraft seat device 46'c, viewed perpendicular to the aircraft cabin central axis 16c. The second further separating unit 106c of the further aircraft seat device 48c is designed to be adjustable. The second further separating unit 106c is provided to fill up a further free space between the further housing 98c and the further console 100c. The second further separating unit 106c of the further aircraft seat device 48c is coupled to the further console 100c. The second further separation unit 106c of the further aircraft seat device 48c is at least partially designed in one piece with a second separation unit of the adjacent aircraft seat device 46'c.

In principle, the aircraft seat arrangement 14c shown in FIG. 10 is not limited to the number of aircraft seat devices shown. The aircraft seat arrangement 14c can have fewer or more than the aircraft seat devices shown. In principle, it would also be conceivable that the aircraft seat arrangement 14c shown in FIG. 10 is arranged in the aircraft cabin 12c in the first seat column 36c, mirrored about the aircraft cabin central axis 16c. FIGS. 11 to 13 show an aircraft seat arrangement 14d in a fourth exemplary embodiment. The aircraft seat arrangement 14d is provided for use in a partially illustrated aircraft cabin 12d of an aircraft. The aircraft cabin 12d has an aircraft cabin central axis 16d. The aircraft cabin center axis 16d is designed as a longitudinal axis of the aircraft. The aircraft cabin central axis 16d is at the same distance from opposite aircraft cabin outer walls 18d, 20d of the aircraft cabin 12d. The aircraft cabin center axis 16d is aligned parallel to an aircraft cabin floor 22d of the aircraft cabin 12d. The aircraft cabin 12d has an aircraft cabin center plane (not shown in greater detail). In at least one operating state, the aircraft has a flight direction 24d. In the present case, the flight direction 24d is ideally aligned parallel to the aircraft cabin central axis 16d. The aircraft cabin 12d has an aircraft cabin section 26d along the aircraft cabin central axis 16d. In the present case, the aircraft cabin section 26d is delimited by several aircraft cabin separating elements 28d and by several schematically illustrated aircraft cabin modules 30d along the aircraft cabin central axis 16d. The aircraft cabin 12d has two aircraft cabin aisles 32d, 34d in the aircraft cabin section 26d. The aircraft cabin 12d has an aircraft cabin aisle 32d. The aircraft cabin 12d has a further aircraft cabin aisle 34d.

In the present case, the aircraft seat arrangement 14d comprises three seat gaps 36d, 40d, 42d. The aircraft seat arrangement 14d includes a first seat column 36d. The first seat column 36d is designed as an inner seat column. The aircraft cabin 12d has a central region 44d. The central area 44d is delimited by the two aircraft cabin aisles 32d, 34d. The first seat column 36d is arranged in the central region 44d. A maximum extension of the first seat gaps 36d measured perpendicular to the aircraft cabin central axis 16d and parallel to the aircraft cabin floor 22d corresponds to a minimum distance between the aircraft cabin aisle 32d and the further aircraft cabin aisle 34d. The first seat gap 36d at least substantially completely fills the central region 44d, viewed perpendicular to the aircraft cabin central axis 16d and parallel to the aircraft cabin floor 22d. The aircraft seat arrangement 14d comprises a second seat column 40d. The second seat column 40d is designed as a first outer seat column. The aircraft seat arrangement 14d comprises a third seat column 42d. The third seat column 42d is designed as a second outer seat column. In the present case, the third seat gap 42d is formed symmetrically to the second seat gap 40d over the aircraft cabin center axis 16d. In principle, the third seat column 42d could also be embodied identically to the second seat column 40d.

The aircraft seat arrangement 14d comprises an aircraft seat device 46d. The aircraft seat device 46d is arranged in the first seat gap 36d. The aircraft seat device 46d intersects the aircraft cabin center plane. The aircraft seat arrangement 14d comprises a further aircraft seat device 48d. The further aircraft seat device 48d is arranged in the first seat gap 36d. The further aircraft seat device 48d intersects the aircraft cabin center plane. The aircraft seat device 46d and the further aircraft seat device 48d are arranged at least partially next to one another in a common seat gap, namely the first seat gap 36d. In the common first seat gap 36d, exactly two aircraft seat devices are arranged directly next to one another, namely the aircraft seat device 46d and the further aircraft seat device 48d. The aircraft seat device 46d and the further aircraft seat device 48d are arranged in the first seat gap 36d, viewed perpendicular to the aircraft cabin central axis 16d, at least partially overlapping one another. The aircraft seat device 46d and the further aircraft seat device 48d are arranged directly adjacent to one another in the first seat gap 36d. The aircraft seat device 46d and the further aircraft seat device 48d are arranged in the first seat gap 36d directly one behind the other and directly next to one another. The aircraft seat device 46d and the further aircraft seat device 48d each have direct access to different aircraft cabin aisles 32d, 34d.

The aircraft seat arrangement 14d comprises an adjacent aircraft seat device 46'd. The adjacent aircraft seat device 46'd is at least essentially identical to the aircraft seat device 46d. The adjacent aircraft seat device 46'd is arranged in the first seat column 36d. The adjacent aircraft seat device 46'd is arranged adjacent to the further aircraft seat device 48d along a longitudinal axis of the aircraft. The adjacent aircraft seat device 46'd, viewed in the direction of flight 24d, is immediately in front of the further aircraft seat device 48d arranged. The adjacent aircraft seat device 46'd is spaced apart from the aircraft seat device 46d by the further aircraft seat device 48d.

The aircraft seat arrangement 14d comprises an adjacent further aircraft seat device 48'd. The adjacent further aircraft seat device 48'd is at least essentially identical to the further aircraft seat device 48d. The adjacent further aircraft seat device 48'd is arranged in the first seat column 36d. The adjacent further aircraft seat device 48'd is arranged adjacent to the aircraft seat device 46d along a longitudinal axis of the aircraft. The adjacent further aircraft seat device 48'd is arranged immediately behind the aircraft seat device 46d when viewed in the direction of flight 24d. The adjacent further aircraft seat device 48'd is spaced apart from the further aircraft seat device 48d by the aircraft seat device 46d.

The aircraft seat device 46d and the further aircraft seat device 48d form a seat grouping 54d of the aircraft seat arrangement 14d. The grouping of seats 54d forms a, preferably periodically, repeatable sequence. In the present case, the aircraft seat arrangement 14d comprises four seat groupings 54d, 54'd, 54 "d, 54" 'd arranged directly one behind the other in the first seat column 36d, which are each formed from the aircraft seat device 46d and the further aircraft seat device 48d. The four seat groupings 54d, 54'd, 54 "d, 54" 'd arranged directly one behind the other in the first seat column 36d are designed identically. The aircraft seat device 46d and the further aircraft seat device 48d together form an at least substantially rectangular base area, preferably viewed perpendicular to the aircraft cabin floor 22d. The at least substantially rectangular base area defines the seat grouping 54d.

The aircraft seat device 46d forms an aircraft seat area. The aircraft seat device 46d has an aircraft seat 56d. In the present case, the aircraft seat 56d is not designed as a full flat seat. The aircraft seat 56d includes a seat bottom 58d. The aircraft seat 56d includes a backrest 60d. In principle, the aircraft seat 56d can comprise additional add-on parts, such as preferably a headrest, a legrest and / or at least one armrest. The aircraft seat device 46d is adjustable between a sitting position and a lying position. In FIGS. 11 and 12, the aircraft seat device 46d is shown in FIG Lying position shown. In FIG. 11, the adjacent aircraft seat device 46'd is shown in the seated position. The aircraft seat 56d of the aircraft seat device 46d is arranged in the same position in the sitting position and in the lying position. The aircraft seat 56d of the aircraft seat device 46d is designed to be non-adjustable in one orientation. The aircraft seat 56d of the aircraft seat device 46d is designed to be rotatable with respect to a movement about an axis perpendicular to the aircraft cabin floor 22d. The seat bottom 58d of the aircraft seat 56d of the aircraft seat device 46d is arranged in the same position in the sitting position and in the lying position.

The seat bottom 58d of the aircraft seat 56d is arranged in a stationary manner in the aircraft seat area of the aircraft seat device 46d. In the seated position and in the lying position of the aircraft seat device 46d, the seat bottom 58d of the aircraft seat 56d of the aircraft seat device 46d is arranged at the same point. The seat bottom 58d of the aircraft seat 56d of the aircraft seat device 46d is designed to be non-adjustable in one position. In principle, it is conceivable that the backrest 60d of the aircraft seat 56d is movably supported with respect to the seat bottom 58d of the aircraft seat 56d. The aircraft seat device 46d has a seat direction 62d. The seat direction 62d of the aircraft seat device 46d is oriented at least essentially parallel to the aircraft cabin central axis 16d. The seat direction 62d corresponds to the flight direction 24d. The aircraft seat device 46d has a lying direction 64d. The lying direction 64d differs from the seating direction 62d, viewed perpendicular to the aircraft cabin floor 22d, at an angle of at least 30 degrees. In the present case, the seat direction 62d of the aircraft seat device 46d deviates from the lying direction 64d of the aircraft seat device 46d by at least 30 degrees. The lying direction 64d of the aircraft seat device 46d has a directional component in the flight direction 24d. The lying direction 64d of the aircraft seat device 46d is oriented at an angle of at least 30 degrees to the aircraft cabin central axis 16d.

The lying direction 64d of the aircraft seat device 46d is directed away from the further aircraft cabin aisle 34d. The aircraft seat device 46d has a housing 66d. The housing 66d is designed as a shell element. The aircraft seat device 46d has a console 68d. The console 68d can be used by two aircraft seat devices arranged directly adjacent to one another, namely the aircraft seat device 46d and the adjacent further aircraft seat device 48'd. The console 68d intersects the aircraft cabin midplane. The aircraft seat device 46d has a partition wall 70d. The partition wall 70d of the The aircraft seat device 46d is arranged behind the aircraft seat 56d when viewed in the seat direction 62d. A downward direction of extent of the partition wall 70d of the aircraft seat device 46d runs perpendicular to the aircraft cabin central axis 16d. The partition wall 70d is formed continuously between the aircraft cabin aisle 32d and the further aircraft cabin aisle 34d. The partition wall 70d of the aircraft seat device 46d is provided to permanently optically separate the aircraft seat area of the aircraft seat device 46d from the adjacent further aircraft seat area of the adjacent further aircraft seat device 48'd. In principle, it would be conceivable for the partition wall 70d to be designed to be adjustable and, for example, to be movable towards the aircraft cabin floor 22d. The partition wall 70d of the aircraft seat device 46d is formed in one piece with a partition wall of the adjacent further aircraft seat device 48'd. The aircraft seat device 46d has a screen. The screen is arranged on the partition wall 70d. The aircraft seat device 46d has a footwell 76d. The footwell 76d is provided for placing at least one foot in the lying position of the adjacent further aircraft seat device 48'd. The footwell 76d of the aircraft seat device 46d is arranged in the console 68d of the aircraft seat device 46d. The console 68d forms the footwell 76d. The footwell 76d of the console 68d of the aircraft seat device 46d can only be used by a passenger who is staying in a neighboring further aircraft seat area of the neighboring further aircraft seat device 48'd. The console 68d is designed to be cantilevered starting from the partition wall 70d in the direction of the aircraft seat 56d. Between the aircraft cabin floor 22d and the console 68d, a footwell (not shown in more detail) of the aircraft seat device 46d is formed, in which the passenger's feet can be positioned in the seated position. In the present case, the aircraft seat device 46d has two separating units 72d, 74d. A first separating unit 72d of the aircraft seat device 46d is provided to optically separate the aircraft seat area from the further aircraft cabin aisle 34d in at least one operating state. The first separating unit 72d of the aircraft seat device 46d is designed to be adjustable. The first separating unit 72d of the aircraft seat device 46d is coupled to the housing 66d. A second separating unit 74d of the aircraft seat device 46d is provided to optically separate the aircraft seat area from the aircraft cabin aisle 32d in at least one operating state. The second separating unit 72d of the aircraft seat device 46d is designed to be adjustable. The aircraft seat assembly 46d has direct access to the further aircraft cabin aisle 34d. A passenger can enter the aircraft seat area of the aircraft seat device 46d directly from the further aircraft cabin aisle 34d without crossing another aircraft seat area. The direct access to the aircraft seat device 46d is only assigned to the aircraft seat device 46d. The direct access to the aircraft seat device 46d can only be used from the aircraft seat device 46d.

In a lying position of the aircraft seat device 46d, the aircraft seat device 46d forms a lying plane 140d which is at most 60% formed by the aircraft seat 56d of the aircraft seat device 46d. In the present case, at most 40% of the lying plane 140d is formed from the seat bottom 58d of the aircraft seat 56d of the aircraft seat device 46d. The aircraft seat device 46d has two comfort elements 150d, 152d. A first comfort element 150d of the aircraft seat device 46d partially forms a lying surface. The first comfort element 150d, viewed in the seat direction 62d, is arranged next to the seat bottom 58d of the aircraft seat 56d. At least 50% of the lying plane 140d is formed by the first comfort element 150d of the aircraft seat device 46d. The first comfort element 150d is formed in one piece with the seat bottom 58d of the aircraft seat 56d of the aircraft seat device 46d. In the present case, the first comfort element 150d of the aircraft seat device 46d is arranged non-adjustable in the aircraft seat area of the aircraft seat device 46d. In principle, it is conceivable that the first comfort element 150d of the aircraft seat device 46d protrudes beyond the at least substantially rectangular base area. A second comfort element 152d of the aircraft seat device 46d partially forms the lying surface in the lying position. In the lying position, the second comfort element 152d, viewed in the seat direction 62d, is arranged directly behind the seat bottom 58d of the aircraft seat 56d. The second comfort element 152d is arranged in the lying position between the seat bottom 58d of the aircraft seat 56d and the console 68d. At least 20% of the lying plane 140d is formed by the second comfort element 152d of the aircraft seat device 46d. The second comfort element 152d is designed to be movable with respect to the seat bottom 58d of the aircraft seat 56d. The second comfort element 152d is designed to be movable with respect to the first comfort element 150d. In principle, it is conceivable that the second comfort element 152d in the seat position between the aircraft cabin floor 22d and the first comfort element 150d is stowed. Alternatively or additionally, it would be conceivable that the second comfort element 152d is stowed in the seat position between the aircraft cabin floor 22d and the seat floor 58d of the aircraft seat 56d. In principle, it would also be conceivable for the second comfort element 152d to be stored in the seated position of the aircraft seat device 46d at a different location in the aircraft cabin 12d. A surface of the seat bottom 58d of the aircraft seat 56d of the aircraft seat device 46d, a surface of the first comfort element 150d of the aircraft seat device 46d and a surface of the second comfort element 152d of the aircraft seat device 46d form the lying plane 140d. The surface of the seat bottom 58d of the aircraft seat 56d, the surface of the first comfort element 150d and the surface of the second comfort element 152d face away from the aircraft cabin floor 22d in the lying position of the aircraft seat device 46d.

The further aircraft seat device 48d forms a further aircraft seat area. The further aircraft seat device 48d has a further aircraft seat 88d. In the present case, the further aircraft seat 88d is not designed as a full-flat seat. A minimum distance between the aircraft seat 56d of the aircraft seat device 46d and the further aircraft cabin aisle 34d is the same as a minimum further distance between the further aircraft seat 88d of the further aircraft seat device 48d and the aircraft cabin aisle 32d. The further aircraft seat 88d comprises a further seat bottom 90d. The further aircraft seat 88d comprises a further backrest 92d. In principle, the further aircraft seat 88d can comprise additional further add-on parts, such as preferably a further headrest, a further leg support and / or at least one further armrest. The further aircraft seat device 48d can be adjusted between a sitting position and a lying position. In FIGS. 11 and 12, the further aircraft seat device 48d is shown in the lying position. In FIG. 11, the adjacent further aircraft seat device 48'd is shown in the seated position. The further aircraft seat 88d of the further aircraft seat device 48d is arranged in the same position in the sitting position and in the lying position. The further aircraft seat 88d of the further aircraft seat device 48d is designed to be non-adjustable in one orientation. The further aircraft seat 88d of the further aircraft seat device 48d is designed to be non-rotatable with regard to a movement about an axis perpendicular to the aircraft cabin floor 22d. The further seat bottom 90d of the further aircraft seat 88d of the further aircraft seat device 48d is in the sitting position and in the lying position in FIG arranged in the same position. The further seat bottom 90d of the further aircraft seat 88d is arranged in a stationary manner in the further aircraft seat area of the further aircraft seat device 48d. In the seated position and in the lying position of the further aircraft seat device 48d, the further seat bottom 90d of the further aircraft seat 88d of the further aircraft seat device 48d is arranged at the same point. The further seat bottom 90d of the further aircraft seat 88d of the further aircraft seat device 48d is designed to be non-adjustable in one position. In principle, it is conceivable that the further backrest 92d of the further aircraft seat 88d is movably supported with respect to the further seat bottom 90d of the further aircraft seat 88d. The further aircraft seat device 48d has a further seat direction 94d. The further seat direction 94d of the further aircraft seat device 48d is oriented at least essentially parallel to the aircraft cabin central axis 16d. The further seat direction 94d corresponds to the flight direction 24d. The further aircraft seat device 48d has a further lying direction 96d. The further lying direction 96d differs from the further seating direction 94d, viewed perpendicular to the aircraft cabin floor 22d, at an angle of at least 30 degrees. In the present case, the further seat direction 94d of the further aircraft seat device 48d deviates from the further lying direction 96d of the further aircraft seat device 48d by at least 30 degrees. The further lying direction 96d of the further aircraft seat device 48d has a directional component in the flight direction 24d. The further lying direction 96d of the further aircraft seat device 48d is oriented at an angle of at least 30 degrees to the aircraft cabin central axis 16d.

The further lying direction 96d of the further aircraft seat device 48d is directed away from the aircraft cabin aisle 32d. The further aircraft seat device 48d has a further housing 98d. The further housing 98d is designed as a shell element. The further housing 98d of the further aircraft seat device 48d is preferably formed in one piece with the housing 66d of the aircraft seat device 46d. The further aircraft seat device 48d has a further console 100d. The further console 100d can be used by two aircraft seat devices arranged directly adjacent to one another, namely the further aircraft seat device 48d and the adjacent aircraft seat device 46'd. The further console 100d intersects the aircraft cabin center plane. The further aircraft seat device 48d has a further partition wall 102d. The further partition 102d of the further aircraft seat device 48d is behind the further one, viewed in the seat direction 94d Arranged aircraft seat 88d. A main direction of extent of the further partition 102d of the further aircraft seat device 48d runs perpendicular to the aircraft cabin central axis 16d. The further partition wall 102d is formed continuously between the aircraft cabin aisle 32d and the further aircraft cabin aisle 34d. The further partition 102d of the further aircraft seat device 48d is provided to permanently optically separate the aircraft seat area of the further aircraft seat device 48d from the adjacent aircraft seat area of the adjacent aircraft seat device 46'd. In principle, it would be conceivable for the further partition wall 102d to be designed to be adjustable and, for example, to be movable towards the aircraft cabin floor 22d. The further partition 102d of the further aircraft seat device 48d is formed in one piece with a partition wall of the adjacent aircraft seat device 46'd. The further aircraft seat device 48d has a further screen. The further screen is arranged on the further partition wall 102d. The further aircraft seat device 48d has a further footwell 108d. The further footwell 108d is provided for placing at least one foot in the lying position of the adjacent aircraft seat device 46'd. The further footwell 108d of the adjacent aircraft seat device 46'd is arranged in the further console 100d of the further aircraft seat device 48d. The further console 100d forms the further footwell 108d. The further footwell 108d of the further console 100d of the further aircraft seat device 48d can only be used by a passenger who is in an adjacent aircraft seat area of the adjacent aircraft seat device 46'd. The footwell 76d of the aircraft seat device 46d and the further footwell 108d of the further aircraft seat device 48d are arranged next to one another, viewed along the aircraft cabin central axis 16d. The further console 100d is designed to be cantilevered starting from the further partition wall 102d in the direction of the further aircraft seat 88d. Between the aircraft cabin floor 22d and the further console 100d, a further footwell (not shown) of the further aircraft seat device 48d is formed, in which the passenger's feet can be positioned in the seated position. In the present case, the further aircraft seat device 48d has two further separating units 104d, 106d. A first further separating unit 104d of the further aircraft seat device 48d is provided to optically separate the further aircraft seat area from the aircraft cabin aisle 32d in at least one operating state. The first further separating unit 104d of the further aircraft seat device 48d is designed to be adjustable. The first more Separation unit 104d of the further aircraft seat device 48d is coupled to the further housing 98d. A second further separating unit 106d of the further aircraft seat device 48d is provided to optically separate the further aircraft seat area from the further aircraft cabin aisle 34d in at least one operating state. The second further separating unit 106d of the further aircraft seat device 48d is designed to be adjustable. The further aircraft seat device 48d has direct access to the aircraft cabin aisle 32d. A passenger can enter the further aircraft seat area of the further aircraft seat device 48d directly from the aircraft cabin aisle 32d without crossing another aircraft seat area. The direct access to the further aircraft seat device 48d is only assigned to the further aircraft seat device 48d. The direct access to the further aircraft seat device 48d can only be used by the further aircraft seat device 48d.

In a reclining position of the further aircraft seat device 48d, the further aircraft seat device 48d forms a further reclining plane 142d, which is at most 60% formed by the further aircraft seat 88d of the further aircraft seat device 48d. In the present case, the further lying plane 142d is formed to a maximum of 40% from the further seat bottom 90d of the further aircraft seat 88d of the further aircraft seat device 48d. The lying plane 140d of the aircraft seat device 46d is at the same distance from the aircraft cabin floor 22d as the further lying plane 142d of the further aircraft seat device 48d. The further aircraft seat device 48d has two further comfort elements 154d, 156d. A first further comfort element 154d of the further aircraft seat device 48d partially forms a further lying surface. The first further comfort element 154d, viewed in the further seat direction 94d, is arranged next to the further seat bottom 90d of the further aircraft seat 88d. At least 50% of the further lying plane 142d is formed by the first further comfort element 154d of the further aircraft seat device 48d. The first further comfort element 154d is designed in one piece with the further seat bottom 90d of the further aircraft seat 88d of the further aircraft seat device 48d. In the present case, the first further comfort element 154d of the further aircraft seat device 48d is arranged in a non-adjustable manner in the further aircraft seat area of the further aircraft seat device 48d. In principle, it is conceivable that the first further comfort element 154d of the further Aircraft seat device 48d protrudes beyond the at least substantially rectangular base area. A second additional comfort element 156d of the additional aircraft seat device 48d partially forms the additional lying surface in the lying position. In the lying position, the second further comfort element 156d, viewed in the further seat direction 94d, is arranged directly behind the further seat bottom 90d of the further aircraft seat 88d. The second further comfort element 156d is arranged in the lying position between the further seat bottom 90d of the further aircraft seat 88d and the further console 100d. At least 20% of the further lying plane 142d is formed by the second further comfort element 156d of the further aircraft seat device 48d. The second further comfort element 156d is designed to be movable with respect to the further seat bottom 90d of the further aircraft seat 88d. The second further comfort element 156d is designed to be movable with respect to the first further comfort element 154d. In principle, it is conceivable that the second further comfort element 156d is stowed in the seat position between the aircraft cabin floor 22d and the first further comfort element 154d. Alternatively or additionally, it would be conceivable that the second further comfort element 156d is stowed in the seat position between the aircraft cabin floor 22d and the further seat floor 90d of the further aircraft seat 88d. In principle, it would also be conceivable that the second further comfort element 156d is stored in the seat position of the further aircraft seat device 48d at a different location in the aircraft cabin 12d. A surface of the further seat bottom 90d of the further aircraft seat 88d of the further aircraft seat device 48d, a surface of the first further comfort element 154d of the further aircraft seat device 48d and a surface of the second further comfort element 156d of the further aircraft seat device 48d form the further lying plane 142d. The surface of the further seat bottom 90d of the further aircraft seat 88d, the surface of the first further comfort element 154d and the surface of the second further comfort element 156d face away from the aircraft cabin floor 22d in the lying position of the further aircraft seat device 48d.

The seat direction 62d of the aircraft seat device 46d is oriented opposite to the further seat direction 94d of the further aircraft seat device 48d. The seat direction 62d of the aircraft seat device 46d is formed at least essentially parallel to the further seat direction 94d of the further aircraft seat device 48d. the Lying direction 64d of the aircraft seat device 46d is oriented opposite to the further lying direction 96d of the further aircraft seat device 48d. The lying direction 64d of the aircraft seat device 46d is formed at least essentially parallel to the further lying direction 96d of the further aircraft seat device 48d. The lying direction 64d of the aircraft seat device 46d and the further lying direction 96d of the further aircraft seat device 48d are angled at the same angle to the aircraft cabin central axis 16d. The lying direction 64d of the aircraft seat device 46d and the further lying direction 96d of the further aircraft seat device 48d are aligned at least essentially parallel to one another. The lying direction 64d and the further lying direction 96d are ideally aligned with the aircraft seat device 46d and the further aircraft seat device 48d, with an actual lying direction defined by a passenger, preferably due to an asymmetrical posture of the passenger, deviating from the lying direction 64d and / or the further lying direction 96d can.

A seat center axis, not shown in detail, of the aircraft seat 56d of the aircraft seat device 46d is identical to a seat center axis, not shown in detail, of an adjacent aircraft seat of the adjacent aircraft seat device 46'd. A further seat center axis, not shown in detail, of the further aircraft seat 88d of the further aircraft seat device 48d is designed identically to a further seat center axis, not shown in detail, of an adjacent further aircraft seat of the neighboring further aircraft seat device 48'd.

An axis not shown in more detail perpendicular to the aircraft cabin central axis 16d intersects the seat bottom 58d of the aircraft seat 56d of the aircraft seat device 46d and the further seat bottom 90d of the further aircraft seat 88d of the further aircraft seat device 48d. The axis is aligned parallel to the aircraft cabin floor 22d. In the first seat gap 36d, exactly two seat bottoms are arranged side by side, namely the seat bottom 58d of the aircraft seat 56d of the aircraft seat device 46d and the further seat bottom 90d of the further aircraft seat 88d of the further aircraft seat device 48d.

The third seat column 42d is partially shown in FIG. The aircraft seat arrangement 14d comprises an alternative aircraft seat device 158d. the The alternative aircraft seat device 158d is arranged in the third seat column 42d. The alternative aircraft seat device 158d is designed essentially identically to the aircraft seat device 46d. In contrast to the aircraft seat device 46d in the first seat column 36d, the aircraft seat device 158d in the third seat column 42d is adapted to a shape of the aircraft cabin outer wall 20d. The alternative aircraft seat device 158d has an aircraft seat 160d. The aircraft seat 160d includes a seat bottom 162d. The aircraft seat 160d includes a backrest that is not visible. In FIGS. 11 and 13, the alternative aircraft seat device 158d is shown in the seat position. The alternative aircraft seat device 158d has a seat direction 164d. The alternative aircraft seat device 158d has a reclining direction 166d which, for the sake of clarity, is shown in an adjacent alternative aircraft seat device. The alternative aircraft seat device 158d has a housing 168d. The alternative aircraft seat device 158d has a console 170d. The alternative aircraft seat device 158d has a partition wall 172d. The alternative aircraft seat device 158d has at least one alternative comfort element (not shown in more detail). The alternative comfort element has a different shape than the comfort element of the aircraft seat device 46d. The at least one alternative comfort element is designed to be movable with respect to the seat bottom 162d of the aircraft seat 160d. The alternative aircraft seat device 158d has a footwell not shown in detail. The aircraft seat arrangement 14d comprises an alternative further aircraft seat device 174d. The alternative further aircraft seat device 174d is arranged in the third seat column 42d. The alternative further aircraft seat device 174d is designed essentially identically to the further aircraft seat device 48d. In contrast to the further aircraft seat device 48d in the first seat column 36d, the alternative further aircraft seat device 174d in the third seat column 42d is adapted to the aircraft cabin outer wall 20d. The alternative further aircraft seat device 174d has a further aircraft seat 176d. The further aircraft seat 176d comprises a further seat bottom 178d. The further aircraft seat 176d comprises a backrest 180d. In FIGS. 11 and 13, the alternative further aircraft seat device 174d is shown in the seated position. The alternative further aircraft seat device 174d has a further seat direction 182d. The alternative further aircraft seat device 174d has a further lying direction 184d from For the sake of clarity, is shown in a neighboring alternative further aircraft seat device. The alternative further aircraft seat device 174d has a further housing 186d. In the present case, the at least one alternative comfort element of the alternative aircraft seat device 158d can be slidable and / or foldable on the further housing 186d of the alternative further aircraft seat device 174d or on the partition 172d of the alternative aircraft seat device 158d. The alternative further aircraft seat device 174d has a further console 188d. The alternative further aircraft seat device 174d has a further partition wall 190d. The alternative further aircraft seat device 174d has a first further comfort element 192d. The first further comfort element 192d is at least essentially identical to the first further comfort element 154d of the further aircraft seat device 48d. The alternative further aircraft seat device 174d has a second further comfort element, not shown in detail. The second further comfort element is at least essentially identical to the second further comfort element 156d of the further aircraft seat device 48d. The alternative further aircraft seat device 174d has a footwell 194d. The alternative aircraft seat device 158d and the alternative further aircraft seat device 174d each have direct access to the same further aircraft cabin aisle 34d.

The second seat column 40d is mirrored over the aircraft cabin center axis 16d to the third seat column 42d. In principle, the aircraft seat arrangement 14d shown in FIG. 11 is not limited to the number of aircraft seat devices shown. The aircraft seat arrangement 14d can have fewer or more than the aircraft seat devices shown. In principle, it would also be conceivable that the aircraft seat arrangement 14d shown in FIG is aligned parallel to the aircraft cabin floor 22d.

Claims

3/16/2021 claims

1 . Aircraft seat arrangement with at least one aircraft seat device (46a; 46b; 46c; 46d) and with at least one further aircraft seat device (48a; 48b; 48c; 48d), which are arranged at least partially next to one another in at least one common seat gap (36a; 36b; 36c; 36d) and which are each adjustable between a sitting position and a lying position, characterized in that a lying direction (64a; 64b; 64c; 64d) of the at least one aircraft seat device (46a; 46b; 46c; 46d) is opposite to a further lying direction (96a; 96b; 96c; 96d) of the at least one further

Aircraft seat device (48a; 48b; 48c; 48d) is aligned.

2. Aircraft seat arrangement according to claim 1, characterized in that the at least one aircraft seat device (46a; 46b; 46c; 46d) and the at least one further aircraft seat device (48a; 48b; 48c; 48d) each have direct access to an aircraft cabin aisle (32a, 34a ; 32b, 34b; 32c, 34c; 32d, 34d).

3. Aircraft seat arrangement according to claim 1 or 2, characterized in that the at least one aircraft seat device (46b; 46c; 46d) and the at least one further aircraft seat device (48b; 48c; 48d) each have direct access to different aircraft cabin aisles (32b, 34b; 32c ,

34c; 32d, 34d).

4. Aircraft seat arrangement according to one of the preceding claims, characterized in that the lying direction (64a; 64b; 64c; 64d) of the at least one aircraft seat device (46a; 46b; 46c; 46d) has a directional component in a flight direction (24a; 24b; 24c; 24d ) and the further lying direction (96a; 96b; 96c; 96d) of the at least one further aircraft seat device (48a; 48b; 48c; 48d) has a directional component opposite to the flight direction (24a; 24b; 24c; 24d).

5. Aircraft seat arrangement according to one of the preceding claims, characterized in that the lying direction (64a; 64b; 64c; 64d) of the at least one aircraft seat device (46a; 46b; 46c; 46d) and the further lying direction (96a; 96b; 96c; 96d) the at least one further aircraft seat device (48a; 48b; 48c; 48d), in particular angled by at least 5 degrees, are oriented to a longitudinal axis of the aircraft.

6. Aircraft seat arrangement according to one of the preceding claims, characterized in that the lying direction (64a; 64b; 64c; 64d) of the at least one aircraft seat device (46a; 46b; 46c; 46d) and the further lying direction (96a; 96b; 96c; 96d) the at least one further aircraft seat device (48a; 48b; 48c; 48d) are aligned at least substantially parallel to one another.

7. Aircraft seat arrangement according to one of the preceding claims, characterized in that the at least one aircraft seat device (46a; 46b; 46c; 46d) at least partially intersects an aircraft cabin center plane.

8. Aircraft seat arrangement according to one of the preceding claims, characterized by at least three seat groupings (54a, 54'a, 54 ”a, 54” 'a; 54b, 54 arranged one behind the other directly in the at least one seat gap (36a; 36b; 36c; 36d) 'b, 54 "b, 54"' b, 54 "" b, 54 ""'b; 54c, 54'c, 54 "c; 54d, 54'd, 54" d, 54 "' d), the are each formed from the at least one aircraft seat device (46a; 46b; 46c; 46d) and the at least one further aircraft seat device (48a; 48b; 48c; 48d).

9. Aircraft seat arrangement according to one of the preceding claims, characterized in that an axis perpendicular to a longitudinal axis of the aircraft intersects a shoulder region (120a) of the at least one aircraft seat device (46a) and a further shoulder region (122a) of the at least one further aircraft seat device (48a), in particular in the reclining position of the at least one aircraft seat device (46a) and the at least one further aircraft seat device (48a).

10. Aircraft seat arrangement according to one of the preceding claims, characterized in that an axis perpendicular to an aircraft longitudinal axis has a backrest (60a) of an aircraft seat (56a) of the at least one aircraft seat device (46a) and a further backrest (92a) of a further aircraft seat (88a) at least one further aircraft seat device (48a) intersects, in particular in the seat position of the at least one aircraft seat device (46a) and the at least one further aircraft seat device (48a).

11. Aircraft seat arrangement according to one of the preceding claims, characterized in that the at least one aircraft seat device (46a) has at least one housing (66a) which, in the lying position of the at least one aircraft seat device (46a), has a head region (78a) of an aircraft seat (56a) at least substantially covers at least one aircraft seat device (46a).

12. Aircraft seat arrangement according to one of claims 1 to 8, characterized in that a seat center axis (128b) of an aircraft seat (56b) of the at least one aircraft seat device (46b) has a seat bottom (90b) of a further aircraft seat (88b) of the at least one further aircraft seat device (48b ), in particular viewed perpendicular to an aircraft cabin floor (22b), intersects.

13. Aircraft seat arrangement according to one of claims 1 to 8 or 12, characterized in that the lying direction (64b; 64c) of the at least one aircraft seat device (46b; 46c) and the further lying direction (96b; 96c) of the at least one further aircraft seat device (48b; 48c) are directed towards each other.

14. Aircraft seat arrangement according to one of claims 1 to 8, 12 or 13, characterized in that the at least one aircraft seat device (46b; 46c) in the lying position of the at least one aircraft seat device (46b; 46c) forms a lying plane (140b) that forms another Distance to an aircraft cabin floor (22b; 22c) as a further lying plane (142b) which is formed by the at least one further aircraft seat device (48b; 48c) in the lying position of the at least one further aircraft seat device (48b; 48c).

15. Aircraft seat arrangement according to one of claims 1 to 8 or 12 to 14, characterized in that a footwell (132b; 132c) of the at least one aircraft seat device (46b; 46c) and a further footwell (136b; 136c) of the at least one further aircraft seat device ( 48b; 48c), in particular viewed perpendicular to an aircraft cabin floor (22b; 22c), are arranged so as to overlap one another.

16. Aircraft seat arrangement according to one of claims 1 to 8 or 12 to 15, characterized in that the at least one aircraft seat device (46b; 46c) and the at least one further aircraft seat device (48b; 48c) have at least one common console (144b; 144c).

17. Aircraft seat arrangement according to claim 16, characterized by at least one adjacent aircraft seat device (46'b) which is at least substantially identical to the at least one aircraft seat device (46b), the at least one console (144b) at least partially from the at least one adjacent Aircraft seat device (46'b) can be used.

18. Aircraft seat arrangement according to one of claims 1 to 8, characterized in that the at least one aircraft seat device (46d) and the at least one further aircraft seat device (48d) together form an at least substantially rectangular base area.

19. Aircraft seat arrangement according to one of claims 1 to 8 or 18, characterized in that a seat direction (62d) of the at least one aircraft seat device (46d) is aligned at least substantially parallel to a longitudinal axis of the aircraft.

20. Aircraft seat arrangement according to one of claims 1 to 8, 18 or 19, characterized in that an axis perpendicular to an aircraft longitudinal axis has a seat base (58d) of an aircraft seat (56d) of the at least one aircraft seat device (46d) and a further seat base (90d) further aircraft seat (88d) which intersects at least one further aircraft seat device (48d), in particular in the seat position of the at least one aircraft seat device (46d) and the at least one further aircraft seat device (48d).

21. Aircraft seat arrangement according to one of claims 1 to 8 or 18 to 20, characterized in that the at least one aircraft seat device (46d) in a lying position of the at least one aircraft seat device (46d) forms a lying plane (140d) which is at most 60% of a Aircraft seat (56d) of the at least one aircraft seat device (46d) is formed.

22. Aircraft seat device (46a, 48a; 46b, 48b; 46c, 48c; 46d, 48d) of an aircraft seat arrangement (14a; 14b; 14c; 14d) according to one of the preceding claims.