EP3990350A1 - Flugzeugkabinenvorrichtung - Google Patents
FlugzeugkabinenvorrichtungInfo
- Publication number
- EP3990350A1 EP3990350A1 EP20736281.5A EP20736281A EP3990350A1 EP 3990350 A1 EP3990350 A1 EP 3990350A1 EP 20736281 A EP20736281 A EP 20736281A EP 3990350 A1 EP3990350 A1 EP 3990350A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- aircraft
- seat
- row
- seats
- backrest
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
Links
- 238000005192 partition Methods 0.000 description 12
- 239000006260 foam Substances 0.000 description 5
- 239000000463 material Substances 0.000 description 5
- 230000001427 coherent effect Effects 0.000 description 4
- 239000004744 fabric Substances 0.000 description 2
- 230000008878 coupling Effects 0.000 description 1
- 238000010168 coupling process Methods 0.000 description 1
- 238000005859 coupling reaction Methods 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 230000018109 developmental process Effects 0.000 description 1
- 230000010354 integration Effects 0.000 description 1
- 239000007779 soft material Substances 0.000 description 1
- 239000004753 textile Substances 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D11/00—Passenger or crew accommodation; Flight-deck installations not otherwise provided for
- B64D11/06—Arrangements of seats, or adaptations or details specially adapted for aircraft seats
- B64D11/0639—Arrangements of seats, or adaptations or details specially adapted for aircraft seats with features for adjustment or converting of seats
- B64D11/0641—Seats convertible into beds
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D11/00—Passenger or crew accommodation; Flight-deck installations not otherwise provided for
- B64D11/06—Arrangements of seats, or adaptations or details specially adapted for aircraft seats
- B64D11/0647—Seats characterised by special upholstery or cushioning features
Definitions
- the invention relates to an aircraft cabin device according to the preamble of
- Aircraft seat row which comprises at least two aircraft seats arranged next to one another, and with at least one, directly in front of the first aircraft seat row
- second row of aircraft seats which comprises at least one aircraft seat, wherein the aircraft seats of the first and second row of aircraft seats have a substantially the same seat direction has been proposed.
- the object of the invention is in particular to provide a generic device with improved properties in terms of variability and comfort.
- the object is achieved according to the invention by the features of
- the invention is based on an aircraft cabin device with at least one first row of aircraft seats, which comprises at least two aircraft seats arranged next to one another, and with at least one, directly in front of the first row of aircraft seats
- second aircraft seat row which comprises at least one aircraft seat, wherein the aircraft seats of the first and second aircraft seat rows have a substantially the same seat direction.
- Aircraft seat row is provided with the first arranged directly behind it Form the aircraft seat of the rear, first row of aircraft seats a common usable area.
- An “aircraft cabin device” should preferably be understood to mean, in particular, a device that is arranged at least in part of an aircraft cabin and / or forms part of an aircraft cabin.
- An “aircraft seat row” should preferably be understood to mean a row of preferably at least two aircraft seats arranged directly next to one another, which are preferably aligned in particular parallel to one another, that is, the seat directions of which are aligned parallel to one another.
- An “aircraft seat” is to be understood as meaning, in particular, a seat which is provided for the purpose of being in an aircraft cabin
- Aircraft to be raised on a cabin floor, and on which a passenger can sit during a flight.
- the aircraft seat has at least one
- a “seat direction” is to be understood in particular as a direction which is aligned parallel to the cabin floor and at least substantially perpendicular to a backrest surface formed by the backrest.
- the aircraft seats of the two aircraft seat rows preferably have the same seat direction, or their seat directions run parallel to one another.
- a “partial area of the aircraft seat row” is to be understood in particular as an area of an aircraft seat row which is arranged between the two lateral ends of the aircraft seat row.
- a partial area of the aircraft seat row is preferably in particular as an aircraft seat or as a
- the sub-area of the aircraft seat row which is provided for forming the common usable area is preferably designed as an aircraft seat with at least one seat bottom and a backrest.
- the partial area of the aircraft seat row that is provided for forming the common usable area is designed as a bench element that has a bench surface that is provided so that a passenger can at least partially sit on it in a flight, with the bench element has at least no full backrest or preferably no backrest at all.
- the sub-area of the aircraft seat row that is provided for forming the common usable area is at least partially designed as a storage area.
- the storage area has at least one recessed storage area, a lockable one Storage compartment and / or electronic connections, for example for charging one
- the sub-area is preferably the
- Row of aircraft seats which is intended to form the common usable area, in a state in which it is not configured as part of a common usable area, usable by the aircraft seat of the same aircraft seat row arranged next to it and by the aircraft seat of the aircraft seat row arranged behind it.
- the sub-area of the aircraft seat row which is provided for forming the common usable area can preferably be used by both passengers in the front and rear aircraft seat rows and can be booked accordingly.
- a “common usable area” should preferably be understood to mean an area which preferably extends over at least two rows of aircraft seats and which is provided for use across rows of aircraft seats by at least one passenger, preferably in particular a child.
- the common usable area is preferably designed in particular as a lying area which is provided so that at least a child or also an adult passenger can lie on it.
- the common usable area is preferably made so large that an adult passenger can also lie stretched out on it.
- “Provided” is to be understood in particular as specifically designed and / or equipped.
- the fact that an object is provided for a specific function should be understood in particular to mean that the object fulfills and / or executes this specific function in at least one application and / or operating state.
- Aircraft cabin device which provides a particularly advantageous space concept, particularly useful for families with children, for aircraft seats of two aircraft seats arranged directly one behind the other.
- the partial area of the front row of aircraft seats can preferably be replaced by a corresponding
- Row of aircraft seats can be booked in addition to your own seat, in particular regardless of whether a common usable area is to be formed in the form of a lying area or whether the sub-area, for example as a storage area or
- Bank area is formed, is used separately.
- the sub-area of the front row of aircraft seats can be used in particular by a passenger of the second aircraft seat of the front row of aircraft seats arranged directly next to it or by a passenger of the first aircraft seat arranged directly behind it in the rear Row of aircraft seats can be booked using the booking system.
- Providing a common usable area can in particular be a convenience for
- the first aircraft seat be the second, front seat
- the aircraft seat row comprises a backrest which, in order to form the common usable area, is provided at least to be moved out of a usable area height.
- a “usable area height” is to be understood in particular as a flea in which the common usable area is arranged and in particular on elements that are provided for providing the usable area, such as in particular a cushion unit for forming the usable area. Under the phrase “from one
- Usable surface height moved out is to be understood in particular that, due to an adjustment, an element, such as in particular the backrest, is no longer arranged in the area of the usable surface height. This allows a common and
- contiguous usable area can be provided particularly easily.
- the backrest for forming the common usable surface is provided to be pivoted backwards so that it is at least partially at least substantially parallel to a seat bottom of the
- Aircraft seat is aligned.
- “Swiveled backwards” should be understood to mean, in particular, rotated or pivoted about an axis of rotation counter to the seat direction.
- “At least essentially parallel” should be understood to mean in particular deviating from a parallel embodiment by a maximum of 10 degrees, preferably a maximum of 5 degrees and particularly preferably less than 1 degree. As a result, the backrest can be moved out of the height of the usable surface particularly easily.
- the backrest be formed from at least two backrest elements that are movably mounted relative to one another via a joint device.
- a “backrest element” should in particular be understood to mean a partial element of the backrest which, in at least one normal operating configuration, is provided to form the entire backrest with at least one further backrest element.
- a “joint device” is to be understood in particular as a device which has at least one joint, preferably in particular one
- Rotary joint comprises, and by means of the at least two elements, such as in particular the two backrest elements are movably mounted to one another and can preferably be pivoted in particular relative to one another. This allows the
- the backrest can be brought into an expansion configuration particularly advantageously.
- the backrest of the first aircraft seat of the second aircraft seat row have a lower fleas than an adjacent one
- the backrest wherein the smaller fleas of the backrest is designed so that the backrest, in a folded-back position, connects with an upper end to a seat bottom of the first aircraft seat of the first aircraft seat row.
- the backrest can be designed in a particularly simple manner so that it can be brought into an expansion configuration in a particularly advantageous manner.
- the backrest of the first aircraft seat of the second aircraft seat row is provided to form the common usable area so that it can be removed from the aircraft seat. Under “from the aircraft seat
- the usable area can be provided particularly easily by an aircraft seat with a standard backrest.
- the aircraft cabin device comprises at least one cushion unit which, in order to form the common usable area, is at least one between a seat area of the first aircraft seat and the first rear one
- a “cushion unit” is to be understood in particular as a unit which is provided to form a comfortable, preferably soft surface and for this purpose preferably comprises at least one cushion element.
- a “cushion element” is to be understood as meaning, in particular, a preferably flat element made of a soft material, such as in particular a foam, which preferably has an extension that corresponds to the support surface in the
- the cushion element is preferably formed from a foam core with a removable cover.
- the cushion element is formed by an inflatable element, such as in particular an air mattress.
- the cushion element is formed by a self-filling air mattress, which for this purpose is, for example, a cover comprises foam core surrounding an airtight material.
- the upholstery element it is also conceivable for the upholstery element to be at least partially formed by a covering which has a frame and a textile stretched in the frame. In principle, it is conceivable that a thin cushion is also attached to the covering.
- the upholstery unit designed as a covering is preferably provided in particular to be inserted in an area between the partial area of the front row of aircraft seats and at least one aircraft seat of the rear row of aircraft seats, in order to form a support in this intermediate area.
- the cushion element can be designed as a separate component that can be stowed separately.
- the cushion element can be provided, for example, to be arranged in an overhead bin arranged above the aircraft seat. In particular, it is conceivable that the cushion element can be folded and / or compressed for particularly space-saving stowage. Under
- “Spanning” is to be understood in particular to mean that an element, such as the cushion unit in particular, bridges a defined area. In this way, a particularly advantageous common usable area can be provided.
- the upholstery unit additionally spans a seat area of the second aircraft seat of the first rear aircraft seat row.
- the common usable area can be made particularly advantageously large.
- the upholstery unit also spans an area between the seat area of the second aircraft seat and the backrest of the second aircraft seat of the front, second aircraft seat row arranged in front of it.
- the common usable area can be made particularly advantageously large.
- the aircraft cabin device have at least one
- separating element that at least partially separates the common usable area from a seat area of an adjacent aircraft seat and / or from an aircraft cabin area.
- a “separating element” is to be understood in particular as an element, preferably a flat element, which is provided to separate two areas from one another in at least one partial area.
- a partition element is advantageously formed by a rigid, flat body, which preferably has a padded surface in order to increase comfort.
- at least Partially separate is to be understood in particular to mean that two partial areas, such as in particular the useful area and a further area, are separated from one another at least in a partial area, in particular up to a defined height.
- the common usable area can advantageously be delimited from an environment.
- first aircraft seats of the first and second aircraft seat rows are arranged on the cabin wall side.
- “Cabin wall side” should be understood to mean, in particular, a side wall of the aircraft cabin with at least one side facing.
- the aircraft cabin device can be arranged particularly advantageously in the aircraft cabin.
- first aircraft seats of the first and second aircraft seat rows are arranged in a center area of an aircraft cabin.
- a “center area of an aircraft cabin” should in particular mean an area of
- Aircraft cabin are understood, which is laterally bounded by a cabin aisle.
- the center area preferably has no access to a side wall of the aircraft cabin. This allows the
- the aircraft cabin device can be arranged particularly advantageously in the aircraft cabin.
- the aircraft cabin device according to the invention should not be restricted to the application and embodiment described above.
- the aircraft cabin device according to the invention can be used to fulfill one of these
- Fig. 1 is a schematic representation of an inventive
- Aircraft cabin device in a first exemplary embodiment with two rows of aircraft seats which form a common usable area in a partial area
- FIG. 3 shows a schematic side view of the two rows of aircraft seats, with a backrest of a front aircraft seat which is adjusted backwards into an expansion configuration
- FIG. 4 is a schematic side view with the backrest in FIG.
- Fig. 5 is a schematic side view of an inventive
- Aircraft cabin device in a second embodiment
- Aircraft cabin device in a third embodiment
- Aircraft cabin device in a fourth embodiment
- Fig. 8 is a schematic plan view of an inventive
- Aircraft cabin device in a fifth embodiment
- FIG. 10 a schematic top view of an inventive
- FIG. 11 shows a schematic side view of an inventive
- Figures 1 to 4 show an aircraft cabin device in a first
- the aircraft cabin device is designed as part of an aircraft cabin 10a.
- the aircraft cabin device has a first row of aircraft seats 12a.
- the aircraft seat row 12a is designed as part of a column 14a of aircraft seat rows arranged one behind the other.
- the first row of aircraft seats 12a includes three aircraft seats 16a, 18a, 20a arranged directly next to one another.
- Adjacent aircraft seats 16a, 18a, 20a of the first row of aircraft seats 12a are aligned parallel to one another.
- the aircraft seats 16a, 18a, 20a of the first row of aircraft seats 12a each have a seat direction which runs parallel to one another.
- the aircraft seat row 12a comprises only two aircraft seats 16a, 20a or more than three aircraft seats 16a, 18a, 20a.
- the aircraft cabin device has a second row of aircraft seats 26a.
- the second row of aircraft seats 26a is designed as part of the column 14a. The second
- the aircraft seat row 26a is arranged directly in front of the first aircraft seat row 12a.
- the second row of aircraft seats 26a is arranged at a distance from the first row of aircraft seats 12a.
- a distance between the first row of aircraft seats 12a and the second row of aircraft seats is preferably 76 cm.
- a distance between the first row of aircraft seats 12a and the second row of aircraft seats 26a is between 68 cm and 92 cm.
- the second row of aircraft seats 26a comprises three aircraft seats 28a, 30a, 32a arranged directly next to one another.
- the aircraft seats 28a, 30a, 32a of the second row of aircraft seats 26a, which are arranged next to one another, are, at least essentially, preferably aligned exactly parallel to one another.
- the aircraft seats 28a, 30a, 32a of the second aircraft seat row 26a each have a seat direction which each run at least essentially, preferably exactly parallel to one another.
- the aircraft seat row 12a and the aircraft seats 28a, 30a, 34a of the second aircraft seat row 26a have essentially the same seat directions.
- the seating directions of the aircraft seats 16a, 18a, 20a of the first aircraft seat row 12a and the seating directions of the aircraft seats 28a, 30a, 32a of the second aircraft seat row preferably run parallel to one another.
- the seat directions of aircraft seats 16a, 18a, 20a, 28a, 30a, 32a of the two aircraft seat rows 12a, 24a arranged directly one behind the other preferably run in alignment with one another.
- the aircraft seats 16a, 18a, 20a, 28a, 30a, 32a of the two rows of aircraft seats 12a, 24a arranged directly one behind the other have a small offset to one another.
- Aircraft seats 28a, 30a, 32a of the second row of aircraft seats 26a are preferably aligned in alignment with the aircraft seats 16a, 18a, 20a of the first row of aircraft seats 12a.
- the first aircraft seat 16a of the first aircraft seat row 12a is preferably behind the first aircraft seat 28a of the second aircraft seat row 26a, the second aircraft seat 18a of the first aircraft seat row 12a behind the second aircraft seat 30a the second row of aircraft seats 26a and the third aircraft seat 20a of the first
- Aircraft seat row 12a arranged behind the third aircraft seat 32a of the second aircraft seat row 26a.
- the second row of aircraft seats 26a is designed here, for example, as a front row of the column 14a. In principle, it is also conceivable for the second row of aircraft seats 26a to be designed as any row in the column 14a.
- the rows of aircraft seats 12, 26 are designed here by way of example on the side wall.
- Rows of aircraft seats 12a, 26a are arranged between a side wall 22a and a cabin aisle 24a of the aircraft cabin 10a.
- the aircraft seat rows 12a, 26a may be designed as a middle row of seats which are arranged between two cabin aisles 24a.
- the aircraft seats 16a, 18a, 20a, 28a, 30a, 32a are designed as economy class aircraft seats.
- the aircraft seats 16a, 18a, 20a, 28a, 30a, 32a are designed as premium economy class aircraft seats.
- the aircraft seats 16a, 18a, 20a of the first row of aircraft seats 12a are preferably designed essentially the same.
- the first aircraft seat 16a is arranged on the side wall.
- the second aircraft seat 18a is designed as a center seat of the first row of aircraft seats 12a.
- the third aircraft seat 20a is designed as an aisle-side seat which faces the cabin aisle 24a.
- the aircraft seats 16a, 18a, 20a are raised together on the cabin floor via a stand unit 34a. Since the
- aircraft seats 16a, 18a, 20a are designed essentially the same, only the aircraft seat 16a will be briefly described in more detail below.
- a configuration of the aircraft seats 18a, 20a of the first row of aircraft seats can be found in the description of the one aircraft seat 16a.
- the aircraft seat 16a has a seat bottom 36a.
- the seat bottom 36a is coupled to the stand unit 34a.
- the seat bottom 36a forms a seat surface of the aircraft seat 16a.
- the aircraft seat includes a
- the backrest 38a is coupled to the stand unit 34a.
- the backrest 38a is arranged at a rear end of the seat bottom 36a of the aircraft seat 16a.
- the aircraft seat 16a is provided to be adjusted between an essentially upright sitting position and a comfort position.
- the backrest 38a is preferably pivotably connected to the stand unit 24a. In the comfort position, the backrest 38a of the aircraft seat 16a is pivoted backwards out of the seat position with an upper end. In principle, it is also conceivable that the seat bottom when adjusted between the seat position and the Comfort position is also adjusted.
- the aircraft seat 16a can be locked in the upright sitting position, the comfort position and possible positions in between.
- the aircraft seats 28a, 30a, 32a of the second row of aircraft seats 26a are raised together on the cabin floor via a stand unit 56a.
- the two aircraft seats 30a, 32a of the second row of aircraft seats 26a are designed essentially the same.
- the second aircraft seat 30a of the second aircraft seat row 26a is designed as a central seat.
- the third aircraft seat 32a of the second row of aircraft seats 26a is designed as an aisle-side seat which faces the cabin aisle 24a.
- the second aircraft seat 30a and the third aircraft seat 32a of the second aircraft seat row 26a are preferably designed in the same way as the aircraft seats 18a, 20a of the first aircraft seat row 12a arranged immediately behind them, i.e. in particular like the aircraft seat 16a of the first aircraft seat row 12a described above.
- the second and third aircraft seats 30a, 32a of the second aircraft seat row 26a are designed differently than the aircraft seats 16a, 18a, 20a of the first aircraft row 12a, in particular have minor differences, for example when the second aircraft seat row 26a is a front row Column 14a is formed.
- the first aircraft seat 28a of the second aircraft seat row 26a is preferably designed differently from the two other aircraft seats 30a, 32a.
- the first aircraft seat 28a of the second aircraft seat row 26a is provided in particular to be adjusted between a normal operating configuration and an expansion configuration. In the normal operating configuration, the first aircraft seat 28a is the second
- the aircraft seat row 26a can preferably be used in exactly the same way as the others
- Airplane seats 30a, 32a Airplane seats 30a, 32a.
- the first aircraft seat 28a is preferably in the
- the first aircraft seat 26a of the second aircraft seat row 26a is provided so that a passenger can sit on it quite normally.
- the first aircraft seat 28a is arranged on the side wall.
- the first aircraft seat 30a also has a seat bottom 40a.
- the seat bottom 40a is in the
- the aircraft seat 28a includes a backrest 42a.
- the backrest 40a is in the normal operating configuration of the aircraft seat 28a provided to provide a back support surface for a passenger sitting on the aircraft seat 28a.
- the backrest 42a is in the
- a partial area 44a of the second front row of aircraft seats 26a is provided for this purpose, with the first aircraft seat 16a arranged directly behind it, the first
- Form aircraft seat row 12a a common usable area 46a.
- the sub-area 44a of the second front row of aircraft seats 26a is preferably formed in particular by the first aircraft seat 28a of the second row of aircraft seats 26a.
- the second row of aircraft seats 26a instead of the first aircraft seat 26a, forms a bench element which forms the sub-area 44a of the second row of aircraft seats.
- the common usable area 46a in particular forms a coherent area which extends over partial areas of both rows of aircraft seats 12a, 26a arranged one behind the other.
- the common usable surface 46a extends in particular from a rear end of the seat area of the first aircraft seat 16a of the first aircraft seat row 12a to a front end of the seat area of the first aircraft seat 28a of the second aircraft seat row 26a.
- the common usable surface 46a is in particular formed continuously from the seat area of the first aircraft seat 16a of the first aircraft seat row 12a to the seat area of the first aircraft seat 28a of the second aircraft seat row 26a.
- no elements of the aircraft seats 16a, 28a are arranged in the area directly above the usable surface 46a. In principle, it is of course conceivable that elements of the
- Aircraft seat 16a, 28a such as a seat divider or an armrest, for example, can be arranged above the usable surface 46a, but not directly above, but in an area to the side of it.
- the usable area 46a is designed in particular as an essentially flat lying area.
- the usable area 46a has a
- the usable area height corresponds approximately to a seat height of the aircraft seats 16a, 18a, 20a, 28a, 30a, 32a, which is formed by an upper side of the seat bottoms 36a, 40a.
- the usable area height is preferably arranged in particular directly above the seat height of the aircraft seats 16a, 28a.
- the usable area 46a is preferably provided in particular to be used by a passenger,
- the common usable area 46a is preferably provided to provide a reclining area for a child is provided, while another passenger, for example a parent, can sit on the aircraft seat 18a of the first aircraft seat row 12a arranged immediately next to it and can at least stretch out his legs on the usable surface 46a.
- the common usable surface 46a is provided, in particular, to extend the area of the first aircraft seat 16a of the rear, first aircraft seat row 12a to the seat area of the first aircraft seat 28a of the second, front aircraft seat row 26a.
- the first aircraft seat 28a of the front, second row of aircraft seats 26a is provided to be adjusted into its extended configuration.
- the first aircraft seat 28a of the second aircraft seat row 26a is preferably configured in such a way that, in the usable area height, a continuous area between the backrest 38a of the rear aircraft seat 16a of the first aircraft seat row 12a and a front end of the seat bottom 40a of the first aircraft seat 28a of the second aircraft seat row 26a is created.
- the extended configuration of the aircraft seat 28a in particular its backrest 42a is preferably adjusted.
- the backrest 42a of the first aircraft seat 28a of the second, front row of aircraft seats 26a is provided to form the common usable surface 46a to be moved out of the usable surface height.
- Backrest 42a is provided in particular to be moved out of an area above seat bottoms 36a, 40a of the first aircraft seats 16a, 28a of the two rows of aircraft seats 12a, 16a.
- the backrest 38a is provided, in particular, to be moved out of the usable area height in an extended configuration.
- the backrest 42a for forming the common usable surface is provided, in particular, to be pivoted backwards in such a way that it is at least partially aligned essentially parallel to the seat bottom 40a of the aircraft seat 28a.
- the backrest 42a is to form the
- the backrest 42a of the first aircraft seat 28a of the second aircraft seat row 26a has two mutually movably mounted via a joint device 48a
- the backrest elements 50a, 52a together form the entire backrest 42a.
- the first backrest element 50a forms a lower part of the backrest 42a.
- the second backrest element 52a forms an upper part of the backrest 42a.
- each of the Backrest elements 50a, 52a each comprise one half of the backrests 42a.
- the two backrest elements 50a, 52a are connected to one another via the joint device 48a.
- the joint device 48a forms a rotation or pivot axis about which the two backrest elements 50a, 52a can be moved relative to one another, in particular can be pivoted relative to one another.
- the joint device 48a preferably comprises at least one rotation bearing, not shown in detail.
- the joint device 48a comprises a coupling gear that movably couples the two backrest elements 50a, 52a to one another.
- the upper, second backrest element 52a can preferably be pivoted by at least 90 degrees to the lower, first backrest element 50a.
- the lower backrest element 50a is coupled to the stand unit 56a.
- the aircraft seat 28a has a bearing unit 54a.
- the lower backrest element 50a is pivotably connected to the stand unit 56a by means of the bearing unit 54a.
- the backrest element can preferably be rotated backwards by at least 90 degrees from an upright sitting position.
- the backrest element 50a can preferably be brought into at least one position in which the backrest element 50a is oriented essentially parallel to the cabin floor.
- the backrest element 50a is preferably in the expansion configuration
- Backrest 42a from the normal operating configuration into the extended configuration is preferably first of all the upper, second backrest element 52a pivoted backwards relative to the first backrest element 50a. Furthermore, the two backrest elements 50a, 52a are relative to the bearing unit 54a
- the first backrest element 50a preferably extends from the seat bottom 40a of the front aircraft seat 38a to a front end of the seat bottom 36a of the rear aircraft seat 16a of the rear aircraft seat row 12a.
- the backrest 42a of the first aircraft seat 28a is arranged in the expansion configuration in an intermediate space between the two first aircraft seats 16a, 28a of the two aircraft seat rows 12a, 26a.
- the backrest 42a, in particular the first, lower backrest element 50a preferably spans the gap in the expansion configuration between the seat bottom 40a of the front first aircraft seat 28a and the
- the backrest 42a preferably rests against the rear first aircraft seat 16a, in particular its seat bottom 36a. In principle, it would also be conceivable for the backrest 42a to be coupled to the rear first aircraft seat 16a in the expansion configuration.
- the second backrest element 52a preferably extends in the direction of the cabin floor or is on the first
- Backrest element 50a folded in and locked on this.
- the second backrest element 52a in the expanded configuration forms a support element for the backrest 42a and stands on the cabin floor.
- Extension configuration does not stand directly on the first rear aircraft seat 16a, but rather that there is a gap between the backrest 42a and the seat bottom 36a, which in particular preferably results in a transfer to the
- Expansion configuration can be facilitated.
- the aircraft cabin device comprises a cushion unit 58a.
- the cushion unit 58a is designed to form the common usable surface 46a.
- the cushion unit 58a is provided in particular to form a surface, in particular a lying surface, of the common usable area.
- the cushion unit 58a is preferably formed from a cushion element 60a. In principle, it is also conceivable that the cushion unit 58a is formed from a plurality of cushion elements 60a.
- the cushion element 60a is preferably formed from a foam.
- the cushion element 60a preferably has a cover (not shown in detail) which has a foam core of the
- the cushion element 60a is formed from another material that appears useful to a person skilled in the art.
- the cushion element 60a forms the complete cushion unit 58a.
- the cushion unit 58a is designed in particular in such a way that it at least substantially, preferably completely, fills the common usable area 46a.
- the upholstery unit 58a preferably extends from the backrest 38a of the rear first aircraft seat 16a to a front end of the seat bottom 40a of the front first aircraft seat 28a.
- the cushion unit 58a preferably has a width which corresponds to a width of the seat bottoms 36a, 40a. In an assembled state, the cushion unit spans the Seating areas of both seat bottoms and those between the seating area of the first
- the aircraft cabin device does not have a cushion unit 58a, but only a blanket which is placed over the seat bottoms 36a, 40a of the two aircraft seats 16a, 28a and the folded backrest 42a.
- a cushion unit 58a In principle, it is also conceivable that no element at all is designed to form the common usable area 46a, but rather the common usable area 46a is formed directly from the surfaces of the seat bottoms 36a, 40a of the two aircraft seats 16a, 28a and the folded backrest 42a.
- FIG. 4 an embodiment without a cushion unit 58a is shown as an example.
- the aircraft cabin device comprises a first separating element 62a.
- Separating element 62a is provided in particular to at least partially delimit common usable area 46a.
- the first separating element 62a delimits the useful surface 46a in particular laterally and on a front side.
- the separating element 62a extends to the side of the first aircraft seats 16a, 28a.
- the separating element 62a separates the usable area from the side wall 22a.
- the separating element 62a extends from the backrest 38a of the rear first aircraft seat 16a to the front end of the seat bottom 40a of the front first aircraft seat 28a.
- the separating element 62a extends over an entire length of the common usable surface 46a.
- Separating element 62a preferably extends at the front end of seat bottom 40a of front first aircraft seat 28a transversely to the seat direction and separates common usable surface 46a towards the front.
- the partition element 62a is
- the separating element 62a preferably has a flea which corresponds to an armrest height.
- the separating element is firmly connected to the first aircraft seats 16a, 28a of the two rows of aircraft seats 12a, 26a.
- the separating element 62a in particular in the area of the seat bottom 40a of the front first aircraft seat 28a, to be U-shaped and thereby separate the common usable surface 46a in particular from the middle aircraft seat 30a of the front aircraft seat row 26a, which the common usable surface 46a from at least partially separates a seat area of an adjacent aircraft seat and / or from an aircraft cabin area.
- the separating element 62a is formed in one piece with the cushion unit 58a.
- the aircraft cabin device can preferably comprise a second separating element 76a.
- the second separating element 76a is shown schematically in FIG. 1 and in FIG.
- the second separating element 76a is provided to separate the common usable surface 46a in the area of the partial area 44a of the front row of aircraft seats 26a and the second aircraft seat 30a of the front row of aircraft seats 26a.
- the second separating element 76a is provided to separate the common usable surface 46a from a remainder of the front row of aircraft seats 26a, in particular the directly adjacent aircraft seat 30a.
- the second partition member 76a preferably extends from the front end of the seat bottom 40a of the front first
- the second separating element 76a can preferably have a flea which corresponds to the flea of an armrest.
- the separating element 76a can preferably also have a height that corresponds to a backrest height, so that the second separating element 76a extends up to an upper edge of the backrest of the second aircraft seat 30a of the front in an assembled state
- the second separating element 76a is preferably formed from a padded plate. In principle, it is also conceivable that the second separating element 76a is formed by a covering. The second separating element 76a preferably forms a privacy protection.
- the second separating element 76a is preferably shown schematically in FIG. 1, at least two different fleas of the second separating element 76a being indicated. In principle, it is of course also conceivable that the second separating element 76a has a different flea.
- FIGS. 5 to 10 Five further exemplary embodiments of the invention are shown in FIGS. 5 to 10.
- the following descriptions and the drawings are essentially limited to the differences between the exemplary embodiments, with regard to components with the same designation, in particular with regard to components with the same reference symbols, in principle also to the drawings and / or the description of the others
- Embodiments in particular FIGS. 1 to 4, can be referred to.
- the letter a is the reference number of Embodiment in Fig. 1 to 4 adjusted.
- the letter a is replaced by the letters b to g.
- the aircraft cabin device is designed as part of an aircraft cabin 10b.
- the aircraft cabin device has a first row of aircraft seats 12b.
- Row of aircraft seats 12b is designed as part of a column 14b of rows of aircraft seats arranged one behind the other.
- the first row of aircraft seats 12b comprises three aircraft seats 16b arranged directly next to one another.
- the aircraft seats 16b of the first aircraft seat row 12b, which are arranged next to one another, are designed essentially the same as the aircraft seats of the first aircraft seat row of the first
- the aircraft cabin device has a second row of aircraft seats 26b.
- the second row of aircraft seats 26b is designed as part of the column 14b.
- the aircraft seat row 26b is arranged directly in front of the first aircraft seat row 12b.
- the second row of aircraft seats 26b is arranged at a distance from the first row of aircraft seats 12b.
- the second row of aircraft seats 26b comprises three aircraft seats 28b, 30b arranged directly next to one another.
- the second and third aircraft seats 30b of the second aircraft seat row 26b are designed essentially the same as the second and third aircraft seats of the second aircraft seat row of the first exemplary embodiment and are therefore not to be described in more detail here.
- the first aircraft seat 28b of the second aircraft seat row 26b is provided in particular to be adjusted between a normal operating configuration and an expansion configuration.
- a partial area 44b of the second front row of aircraft seats 26b is provided with the first aircraft seat 16b arranged directly behind it, the first
- Form aircraft seat row 12b a common usable area 46b.
- the sub-area 44b of the second front row of aircraft seats 26b is preferably formed in particular by the first aircraft seat 28b of the second row of aircraft seats 26b.
- the common usable area 46b in particular forms a coherent area which extends over partial areas of both rows of aircraft seats 12b, 26b arranged one behind the other.
- the usable area 46b essentially corresponds to that in the first
- the first aircraft seat 28b of the front, second aircraft seat row 26b is provided to be placed in its
- the first aircraft seat 28b of the second aircraft seat row 26b is configured differently in order to form the expansion configuration.
- the aircraft seat 28b has a backrest 42b.
- the backrest 42b is designed differently than the backrest of the first
- the backrest 42b of the first aircraft seat 28b of the second aircraft seat row 26b is provided to form the common usable surface 46b so that it can be removed from the aircraft seat 28b.
- the backrest 42b is designed in particular essentially the same as the backrests of the remaining aircraft seats 16b, 30b of the aircraft seat rows 12b, 26b.
- the backrest 42b of the first front aircraft seat 42b is in particular designed to be manually separable from a stand unit 56b of the aircraft seat row 26b.
- the backrest 42b is preferably connected to the stand unit 56b by means of a quick-release fastener, not shown in detail. To form the common usable surface 46b, the backrest 42b can simply be detached from the stand unit 56b and thus from a
- usageable area height between the two aircraft seats 16b, 28b are removed.
- the backrest 42b can be stowed in a cargo area of the aircraft.
- the first aircraft seat 28b does not have a backrest 42b at all and the aircraft seat 28b is basically designed as a bench element which only has a seat surface without a back support surface.
- the aircraft seat 28b could be used as a bench element on which at least one passenger can sit both in the seat direction of the other aircraft seats and against a seat direction of the other aircraft seats.
- the first aircraft seat 16b of the first rear aircraft seat row 12b comprises an expansion device 78b.
- the expansion device 78b is provided for expanding a seat surface of a seat bottom of the rear aircraft seat 16b.
- Extension device 78b is designed as a seat bottom extension.
- Extension device 78b has a seat bottom extension element 80b which is adjustable between a stowed position and a use position.
- the seat bottom extension element 80b is preferably arranged at a front end of a seat bottom 36b of the rear aircraft seat 16b.
- the seat bottom extension element 80b is preferably attached to a stand unit of the aircraft seat 16b.
- the seat bottom extension element 80b is preferably pivotably connected to the aircraft seat 16b.
- the seat bottom extension element 80b is preferably in the stowed position
- the seat bottom extension element 80b is preferably aligned horizontally and expands the seat surface of the seat bottom 36b. In the position of use this is
- Seat bottom extension element 80b is preferably aligned essentially parallel to seat bottom 36b of aircraft seat 16b. In the position of use, the seat bottom extension element 80b preferably extends over a portion of the distance between the seat bottom 36b of the rear aircraft seat 16b and the front aircraft seat 28b. In principle, it would also be conceivable that
- the position of use extends as far as the front aircraft seat 28b and completely bridges a gap between the rear aircraft seat 16b and the front aircraft seat 28b.
- the aircraft cabin device comprises a cushion unit 58b for forming the common usable area 46b.
- the cushion unit 58b can in particular have a cushion element 60b equivalent to the first exemplary embodiment.
- the upholstery unit has an integrated stiffening element which is provided to support the upholstery element 60b in particular in an intermediate area between the two first aircraft seats 16b, 28b.
- an additional support means which bridges the intermediate area between the first aircraft seats 16b, 28b, could be dispensed with.
- the upholstery unit 58b it would also be conceivable for the upholstery unit 58b to have a covering that is stretched in a space between the front aircraft seat 28b and the rear aircraft seat 16b. In principle, it is conceivable that a cushion element 60 can be dispensed with.
- the aircraft cabin device is designed as part of an aircraft cabin 10c.
- the aircraft cabin device has a first row of aircraft seats 12c.
- Row of aircraft seats 12c is designed as part of a column 14c of rows of aircraft seats arranged one behind the other.
- the first row of aircraft seats 12c comprises three aircraft seats 16c arranged directly next to one another.
- the aircraft seats 16c of the first aircraft seat row 12c, which are arranged next to one another, are designed essentially the same as the aircraft seats of the first aircraft seat row of the first
- the aircraft cabin device has a second row of aircraft seats 26c.
- the second row of aircraft seats 26c is designed as part of the column 14c.
- the aircraft seat row 26c is arranged directly in front of the first aircraft seat row 12c.
- the second row of aircraft seats 26c is arranged at a distance from the first row of aircraft seats 12c.
- the second row of aircraft seats 26c comprises three aircraft seats 28c, 30c arranged directly next to one another.
- the second and third aircraft seats 30c of the second aircraft seat row 26c are designed essentially the same as the second and third aircraft seats of the second aircraft seat row of the first exemplary embodiment and are therefore not to be described in more detail here.
- the first aircraft seat 28c of the second aircraft seat row 26c is provided in particular to be adjusted between a normal operating configuration and an expansion configuration.
- a partial area 44c of the second front row of aircraft seats 26c is provided for this purpose, with the first aircraft seat 16c arranged immediately behind it, the first
- Form aircraft seat row 12c a common usable area 46c.
- the sub-area 44c of the second front row of aircraft seats 26c is preferably formed in particular by the first aircraft seat 28c of the second row of aircraft seats 26c.
- the common usable area 46c in particular forms a coherent area which extends over partial areas of both rows of aircraft seats 12c, 26c arranged one behind the other.
- the usable area 46c essentially corresponds to that in the first
- the first aircraft seat 28c of the front, second aircraft seat row 26c is provided to be placed in its
- the first aircraft seat 28c of the second aircraft seat row 26c is designed differently in order to form the expansion configuration.
- the aircraft seat 28c has a backrest 42c.
- the backrest 42c is different designed as the backrest of the first embodiment.
- the backrest 42c of the first aircraft seat 28c of the second aircraft seat row 26c has fewer fleas than an adjacent backrest 64c of the second aircraft seat 30c of the front, second aircraft seat row 26c.
- the aircraft seat 28c with the backrest 42c which has a smaller fleas, is designed in particular as a seat for smaller passengers up to a certain size and a certain weight and is approved accordingly.
- the smaller fleas of the backrest 42c is preferably designed so that the backrest 42c in a folded-back position with an upper end on a seat bottom 36c of the first aircraft seat 16c of the first
- the backrest 42c preferably has in particular a flea which corresponds to a distance between the two rows of aircraft seats 12c, 26c.
- the backrest 42c in particular has a flea of approximately 300 cm to 400 cm.
- the backrest 42c is mounted pivotably via a bearing unit 54c to a stand unit 56c of the second row of aircraft seats 26c.
- the aircraft cabin device comprises a cushion unit 58c.
- the cushion unit 58c is designed to form the common usable surface 46c.
- the cushion unit 58c is preferably equivalent to one of the preceding exemplary embodiments
- the aircraft cabin device is designed as part of an aircraft cabin 10d.
- the aircraft cabin device has a first row of aircraft seats 12d.
- Row of aircraft seats 12d is designed as part of a column 14d of rows of aircraft seats arranged one behind the other.
- the first row of aircraft seats 12d comprises three aircraft seats 16d arranged directly next to one another.
- the aircraft seats 16d of the first aircraft seat row 12d, which are arranged next to one another, are designed essentially the same as the aircraft seats of the first aircraft seat row of the first
- the aircraft cabin device has a second row of aircraft seats 26d.
- the second row of aircraft seats 26d is designed as part of the column 14d.
- the aircraft seat row 26d is arranged directly in front of the first aircraft seat row 12d.
- the second row of aircraft seats 26d is arranged at a distance from the first row of aircraft seats 12d.
- the second row of aircraft seats 26d comprises three aircraft seats 28d, 30d arranged directly next to one another.
- the second and third aircraft seats 30d of the The second row of aircraft seats 26d are designed essentially the same as the second and third aircraft seats of the second row of aircraft seats of the first exemplary embodiment and are therefore not to be described in more detail here.
- the first aircraft seat 28d of the second aircraft seat row 26d is provided in particular to be adjusted between a normal operating configuration and an expansion configuration.
- a partial area 44d of the second front row of aircraft seats 26d is provided for this purpose, with the first aircraft seat 16d arranged directly behind it, the first
- Form aircraft seat row 12d a common usable surface 46d.
- the sub-area 44d of the second front row of aircraft seats 26d is preferably formed in particular by the first aircraft seat 28d of the second row of aircraft seats 26d.
- the common usable surface 46d in particular forms a coherent area which extends over partial areas of both rows of aircraft seats 12d, 26d arranged one behind the other.
- the usable area 46d essentially corresponds to that in the first
- the first aircraft seat 28d of the front, second row of aircraft seats 26d is intended to be placed in its
- the first aircraft seat 28d of the second aircraft seat row 26d is configured differently in order to form the expansion configuration.
- the aircraft seat 28d has a backrest 42d.
- the backrest 42d is designed differently than the backrest of the first
- the backrest 42d of the first aircraft seat 28d of the second aircraft seat row 26d has two backrest elements 50d, 52d which are mounted so as to be movable relative to one another via a bearing device 66d.
- the backrest elements 50d, 52d together form the entire backrest 42d.
- the first backrest element 50d forms a lower part of the backrest 42d.
- the second backrest element 52d forms an upper part of the backrest 42d.
- Backrest elements 50d, 52d can be moved linearly to one another by means of the bearing device 66d.
- the upper backrest member 52d is in the lower one
- the backrest 42d is designed to be telescopically retractable or extendable. In principle, it is also conceivable that the second upper backrest element is linearly in front of or behind the lower backrest element 50d is proceeded.
- the bearing device 66d preferably has at least one linear bearing, not shown in detail.
- the second backrest element 52d can preferably be locked on the first backrest element both in a retracted position and in an extended position.
- the aircraft seat 28d has a bearing unit 54d. By means of the storage unit 54d is the lower
- the backrest element 50d is pivotably connected to the stand unit 56d.
- the backrest element can preferably be rotated backwards by at least 90 degrees from an upright sitting position.
- the backrest element 50d can preferably be brought at least into a position in which the backrest element 50d is oriented essentially parallel to the cabin floor.
- FIG. 8 shows an aircraft cabin device in a fifth exemplary embodiment.
- the aircraft cabin device is designed as part of an aircraft cabin 10e.
- the aircraft cabin device has a first row of aircraft seats 12e and a second row of aircraft seats 26e.
- the aircraft seat rows 12e, 26e are designed in accordance with one of the preceding exemplary embodiments.
- the aircraft cabin device is provided, equivalent to one of the preceding exemplary embodiments, to form a common usable area 46e.
- the common usable area 46e extends, as in the previous exemplary embodiments, in particular in the area of two first aircraft seats 16e, 28e of the two one behind the other
- the aircraft cabin device comprises a cushion unit 58e.
- the cushion unit 58e spans the seat surface of the first two aircraft seats 16e, 28e of the two rows of aircraft seats 12e, 26e.
- the cushion unit 58e also spans a seat area of the second aircraft seat 18e of the first, rear aircraft seat row 12e.
- the cushion unit 58e is in particular L-shaped.
- the first has anterior
- Extension device 68e which is attached to a front end of a seat bottom 40e of the aircraft seat 28e.
- the expansion device 68e is provided to expand the seat area of the seat bottom 40e forwards, preferably up to just before another aircraft seat, not shown in detail.
- the expansion device 68e can for example be formed by an additional element which is pivotably arranged at the front end of the seat bottom 40e and which can be pivoted between a stowed position and a use position running essentially parallel to the seat bottom.
- the cushion unit 58e preferably extends to a front end of the expansion device 68e.
- the cushion unit 58e extends beyond a front end of the seat bottom 40e of the front aircraft seat 28e of the second
- Airplane seat row 26e Airplane seat row 26e.
- the common usable area can advantageously be made larger in contrast to the first exemplary embodiment.
- the aircraft cabin device comprises a first belt device 84e.
- Belt device 84e is provided to secure a passenger seated on cushion unit 58e in the area of aircraft seat 16e.
- the belt device 84e has a belt 86e designed as a two-point belt.
- the belt 86e is preferably designed as a lap belt.
- the belt 86e is particularly preferred as the belt of the
- Aircraft seat 16e formed.
- the belt device 84e has a belt extension element, not shown, which is attached to the
- the belt tongue of the belt 86e of the aircraft seat 16e is connected and has a belt tongue which is arranged in an area above the cushion unit 58e.
- the belt 86e of the belt device 84e which is the belt 86e of the aircraft seat 16e, is provided with a
- the aircraft cabin device comprises a second belt device 88e.
- Belt device 88e is to secure an aircraft seat 28e of the front row of aircraft seats 26e arranged in front of the aircraft seat 16e on the
- the belt device 88e is designed as a three-point belt.
- the belt device 88e has a shoulder belt 90e.
- the shoulder strap 90e is preferably attached to a fastening device Tied to the support structure of the aircraft seat 28e.
- the shoulder strap 90e is preferably detachably connected to the support structure of the aircraft seat 28e by means of the fastening device.
- the shoulder strap 90e it would also be conceivable for the shoulder strap 90e to be fixed to a support structure of the further aircraft seat 92e arranged in front of it by means of a fastening device.
- parts of the belt device 88e to be firmly integrated into the aircraft seat 92e arranged in front of it.
- parts of the belt device 88e are integrated into the backrest 70e of the aircraft seat 92e. Integration into one side as well as into a rear side of the backrest 70e is conceivable. For example, it is conceivable that a pulley or the complete shoulder strap 90e including one
- Roll-up device is firmly integrated into the backrest 70e of the aircraft seat 92e.
- the parts of the belt device 88e are preferably coupled to a load-bearing structure of the aircraft seat 92e.
- the second belt device 88e comprises a lap belt 94e.
- the lap belt 94e is at a first end on a support structure of the
- Aircraft seat 28e attached. In principle, it would also be conceivable that the
- the lap belt 94e is connected directly to a belt of the aircraft seat 28e via a belt extension 96e. Due to the connection to the support structure of the aircraft seat 28e, forces acting on the belts 90e, 94e of the second belt device can advantageously be introduced into a rigid and load-bearing structure of the aircraft seat 28e or the aircraft seat 92e. As a result, a passenger sitting on the cushion unit 58e in the area of the aircraft seat 16e can advantageously also during a TTL phase of a flight, i.e. in particular also during a take-off or landing phase,
- the cushion unit 58e can advantageously be used by a passenger during an entire stay in the aircraft cabin 10e.
- the aircraft cabin device comprises a partition element 98e.
- the separating element 98e is provided to separate the usable surface 46e from at least aircraft seats 30e, 32e of the front row of aircraft seats 26e.
- the separating element 98e preferably extends on a rear side of the front aircraft seats 30e, 32e of the
- the separating element 98e has a U-shaped profile in an assembled state.
- the partition member 98e is preferably formed from a thin, rigid material.
- the separating element 98e is formed by a fabric element that is guided along a frame.
- FIG. 9 shows an aircraft cabin device in a sixth exemplary embodiment.
- the aircraft cabin device is designed as part of an aircraft cabin 10f.
- the aircraft cabin device has a first aircraft seat row 12f and a second aircraft seat row 26f.
- the aircraft seat rows 12f, 26f are designed in accordance with one of the preceding exemplary embodiments.
- the aircraft cabin device is provided, equivalent to one of the preceding exemplary embodiments, to form a common usable area 46f.
- the common usable area 46f extends, as in the previous exemplary embodiments, in particular in the area of two first aircraft seats 16f, 28f of the two one behind the other
- the aircraft cabin device comprises a cushion unit 58f. As in the first exemplary embodiment, the cushion unit 58f spans the
- the cushion unit 58f also spans a seating area of the second aircraft seat 18f of the first, rear aircraft seat row 12f.
- the cushion unit 58f is, in particular, L-shaped.
- the upholstery unit 58f also extends into an area between a seat area of the second aircraft seat 18f and one in front of it
- the common usable area 46f in contrast to the other exemplary embodiments, can advantageously be enlarged further.
- the aircraft cabin device shows an aircraft cabin device in a seventh exemplary embodiment.
- the aircraft cabin device is designed as part of an aircraft cabin 10g.
- the aircraft cabin device has a first row of aircraft seats 12g and a second row of aircraft seats 26g.
- the two rows of aircraft seats 12g, 26g are arranged in a center area of the aircraft cabin 10g.
- the two rows of aircraft seats 12g, 26g are each side of one
- the aircraft seat rows 12g, 26g each have four Airplane seats 16g, 18g, 20g, 28g, 30g, 32g, 72g, 74g.
- a configuration of a common usable area 46g can correspond to one of the preceding
- Embodiments correspond.
- the aircraft cabin device comprises a belt device 88g.
- the belt device 88g is provided for securing a passenger seated on the cushion unit 58g in the area of the aircraft seat 28g arranged in front of the aircraft seat 16g, the front row of aircraft seats 26g.
- the belt device 88g is designed as a multi-point belt.
- the belt device 88g is preferably designed as a three-point belt or a five-point belt.
- the belt device 88g has a first shoulder belt 90g and a second shoulder belt 100g.
- the shoulder straps 90g, 100g are preferably connected to a support structure of the aircraft seat 28g via a fastening device.
- the shoulder straps 90g, 100g are preferably detachably connected to the support structure of the aircraft seat 28g by means of the fastening device.
- the belt device 88g preferably has one or three not shown in detail
- Lap belts which can be connected to the shoulder belts 90g, 100g via a belt lock.
- the lap belts are preferably firmly coupled to a support structure of the aircraft seat 28g. In principle, it is also conceivable that the lap belts are coupled to the belt 86g of the aircraft seat 28g.
- a passenger in particular a child, can be secured particularly securely on the cushion unit 58g of the usable area 46g.
- the aircraft cabin device comprises a first separating element 98g.
- Separating element 98g is provided to separate the usable area 46g from at least one aircraft seat 30g of the front row of aircraft seats 26g.
- the separating element 98g preferably extends on a rear side of the front aircraft seat 30g of the aircraft seat row 26g and laterally between the aircraft seat 30g and the area of the aircraft seat 28g which is covered by the cushion unit 58g.
- the partition member 98g is preferably formed from a thin, rigid material. In principle, it is also conceivable that the separating element 98g is formed by a fabric element that is guided along a frame.
- the aircraft cabin device comprises a second separating element 102g.
- the separating element 102g is provided to separate the usable area 46g at least from the aircraft seats 72g, 74g of the two rows of aircraft seats 12g, 26g.
- the separating element 102g can also consist of a thin, rigid one Be formed material.
- the partition elements 98g, 102g can preferably increase the privacy of the usable area 46g.
- Fig. 1 1 shows an aircraft cabin device in an eighth embodiment.
- the aircraft cabin device is designed as part of an aircraft cabin 10h.
- the aircraft cabin device has a first row of aircraft seats 12h.
- Row of aircraft seats 12h is designed as part of a column 14h of rows of aircraft seats arranged one behind the other.
- the first row of aircraft seats 12h comprises three aircraft seats 16h arranged directly next to one another.
- the aircraft seats 16h of the first aircraft seat row 12h, which are arranged next to one another, are designed essentially the same as the aircraft seats of the first aircraft seat row of the first
- the aircraft cabin device has a second row of aircraft seats 26h.
- the second row of aircraft seats 26h is designed as part of the column 14h.
- the aircraft seat row 26h is arranged directly in front of the first aircraft seat row 12h.
- the second row of aircraft seats 26h is arranged at a distance from the first row of aircraft seats 12h.
- the second row of aircraft seats 26h comprises two aircraft seats 30h arranged directly next to one another.
- the two aircraft seats 30h correspond to the second and third aircraft seats of the second aircraft seat row of the first
- the second row of aircraft seats 26h has a partial area 44h which is provided to form a common usable surface 46h with the first aircraft seat 16h of the first row of aircraft seats 12h arranged directly behind it.
- the partial area 44h is not formed by a first aircraft seat of the front, second aircraft seat row 26h.
- the second, front row of aircraft seats 26h does not have a first aircraft seat. Instead of the first
- the front, second row of aircraft seats 26h has a useful area 82h.
- the useful area 82a can for example be designed as a bench element which forms a bench surface for sitting, preferably in different directions.
- the usable area 82h can preferably also be designed as a storage area which has at least one storage area and / or a lockable storage compartment in which a passenger can store personal items during a flight. Reference number
- Extension device for seat base extension element usable area
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Seats For Vehicles (AREA)
Abstract
Description
Claims
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
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DE102019117429.5A DE102019117429A1 (de) | 2019-06-27 | 2019-06-27 | Flugzeugkabinenvorrichtung |
PCT/EP2020/068114 WO2020260644A1 (de) | 2019-06-27 | 2020-06-26 | Flugzeugkabinenvorrichtung |
Publications (1)
Publication Number | Publication Date |
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EP3990350A1 true EP3990350A1 (de) | 2022-05-04 |
Family
ID=71452205
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EP20736281.5A Pending EP3990350A1 (de) | 2019-06-27 | 2020-06-26 | Flugzeugkabinenvorrichtung |
Country Status (3)
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EP (1) | EP3990350A1 (de) |
DE (1) | DE102019117429A1 (de) |
WO (1) | WO2020260644A1 (de) |
Family Cites Families (17)
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US1977520A (en) * | 1932-11-25 | 1934-10-16 | Louis Dubin | Automobile combined seat and bed |
US2332841A (en) * | 1937-12-17 | 1943-10-26 | Douglas Aircraft Co Inc | Berth and chair arrangement |
US2926951A (en) * | 1958-09-11 | 1960-03-01 | Gen Motors Corp | Vehicle seat |
DE3842733C2 (de) * | 1988-12-19 | 1995-06-22 | Opel Adam Ag | Kraftfahrzeugsitz |
JPH11276295A (ja) * | 1998-03-30 | 1999-10-12 | Nissan Shatai Co Ltd | シートバック構造 |
WO2000023298A1 (en) * | 1998-10-16 | 2000-04-27 | Lear Corporation | Seat structure for vehicle |
US6715716B1 (en) * | 2002-09-17 | 2004-04-06 | The Boeing Company | Economy aircraft sleeper seat |
KR100509672B1 (ko) * | 2003-05-19 | 2005-08-24 | 용 현 문 | 간이침대 겸용 운송수단 시트 |
DE102005025544A1 (de) * | 2005-06-01 | 2006-12-07 | Johnson Controls Gmbh | Sitzanlage und damit ausgestattetes Fahrzeug |
CN2878127Y (zh) * | 2006-02-10 | 2007-03-14 | 吴星星 | 轿车用组合式坐卧两用椅 |
DE102006031361B4 (de) * | 2006-07-06 | 2011-03-10 | Airbus Operations Gmbh | Flugzeug mit einer darin installierbaren Liegevorrichtung zur notfallmedizinischen Versorgung von Patienten |
DE102007004830B4 (de) * | 2007-01-31 | 2015-09-10 | Airbus Operations Gmbh | Flugzeug mit einer für einen Patiententransport umkonfigurierbaren Sitzanordnung |
FR2912700B1 (fr) * | 2007-02-20 | 2009-04-03 | Peugeot Citroen Automobiles Sa | Dispositif de commande d'un siege arriere a partie de dossier rabattable integrant un appui-tete amovible. |
CN101357605A (zh) * | 2008-10-06 | 2009-02-04 | 邵金山 | 改进的汽车座椅组合床 |
WO2012006941A1 (zh) * | 2010-07-12 | 2012-01-19 | Zhang Xingliang | 乘客座椅和组合坐卧两用座椅单元、多用座椅单元 |
CN105291900B (zh) * | 2015-11-25 | 2018-04-20 | 重庆工商大学 | 汽车座椅总成及其靠背伸缩式汽车座椅 |
CN111295333A (zh) * | 2017-10-31 | 2020-06-16 | 赛峰座椅美国有限责任公司 | 用于经济舱座椅的斜倚沙发系统 |
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2019
- 2019-06-27 DE DE102019117429.5A patent/DE102019117429A1/de active Pending
-
2020
- 2020-06-26 EP EP20736281.5A patent/EP3990350A1/de active Pending
- 2020-06-26 WO PCT/EP2020/068114 patent/WO2020260644A1/de active Application Filing
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