WO2017108538A1

WO2017108538A1 - Transport seat device

Info

Publication number: WO2017108538A1
Application number: PCT/EP2016/081031
Authority: WO
Inventors: Christopher TUTE; Alfons Stachel
Original assignee: Recaro Aircraft Seating Gmbh & Co. Kg
Priority date: 2015-12-23
Filing date: 2016-12-14
Publication date: 2017-06-29
Also published as: EP3393908A1; DE102015122808A1

Abstract

The invention relates to a transport seat device, in particular an aircraft seat device, comprising at least one backrest unit (18a; 18b; 18c; 18d; 8e; 18f) having at least one supporting shell (20a; 20b; 20c; 20d; 20e; 20f) formed at least substantially from a fibre composite material, and comprising an armrest device (26a; 26b; 26c; 26d; 26e; 26f) having at least one armrest (28a, 28b; 28b; 28c; 28d, 30d; 28e, 30e; 28f, 30f) connected to the supporting shell (20; 20b; 20c; 20d; 20e; 20f).

Description

Transport seat device

State of the art

The invention relates to a transport seat device according to the preamble of

Patent claim 1.

There have already been proposed transport seat devices.

The object of the invention is in particular to provide a generic device with improved properties in terms of stability. The object is achieved by the features of claim 1, while advantageous embodiments and modifications of the invention can be taken from the dependent claims.

Advantages of the invention

According to the invention, a transport seat device, in particular a

Aircraft seat device, proposed, comprising at least one backrest unit having at least one supporting shell, which is formed at least substantially of a fiber composite material, and with an armrest device having at least one armrest, which is connected to the supporting shell. Under one

Transport seat device "should be understood in particular a device which forms at least a part or an entire seat, wherein the seat is intended to be elevated in a means of transport

Means of transport, for example, as a bus, a ship, a train and preferably designed as an aircraft. Under an aircraft seat device "should be understood in particular a device that at least a part or an entire

Aircraft seat trains. An "aircraft seat" is to be understood in particular as meaning a seat that is raised in an aircraft cabin of an aircraft, wherein the aircraft seat is preferably arranged as part of several side by side , ,

Formed aircraft seats. A "backrest unit" should be understood to mean, in particular, a unit of the aircraft seat which forms a backrest support surface on which a passenger sitting on the aircraft seat can lean his back

Main body and a cushion element, which forms the backrest support surface. The backrest unit is arranged at a rear end of a seat base unit and extends from the seat base unit upwards, from a

Aufständereinheit away. A "supporting shell" is to be understood in particular as meaning a shell-shaped element which is intended to absorb acting forces and to pass them on to a mounting unit

Essentially formed from a fiber composite material, should be understood in this context in particular that the supporting shell at least 50%, preferably 75% and more preferably more than 95% of a

Fiber composite material exists. A "fiber composite material" is to be understood in particular as meaning a multiphase material comprising at least one bedding matrix and reinforcing fibers, The bedding matrix may preferably be made of a plastic, a resin and / or another material which appears expedient to a person skilled in the art The fibers may be formed from synthetic fibers, glass fibers, carbon fibers, natural fibers and / or other fibers that appear appropriate to the person skilled in the art

Device to be understood, which forms an armrest and a connection of the armrest for a seat, in particular an aircraft seat. An "armrest" should be understood to mean, in particular, a unit which forms at least one support surface on which a passenger seated on the aircraft seat can at least partially deposit his arm one

The term "support element" should be understood to mean, in particular, an element which is preferably formed of an elastic, dimensionally stable material and has at least one surface which forms the support surface directly or indirectly.It is conceivable that the support element directly forms the support surface and a passenger directly in Contact with the support element comes or that the armrest unit comprises at least one pad member which covers the support element and thus forms the support surface, whereby the support element forms the support surface indirectly. - -

By "connected", in particular, at least one connecting element is intended to be positively, positively and / or materially coupled to another element, whereby the armrest is preferably connected to the backrest unit laterally A "backbone" of the backrest unit is connected to the back of the backrest unit. "Provided" is to be understood in particular to be specially designed and / or equipped. The fact that an object is intended for a specific function should in particular mean that the object fulfills and / or executes this specific function in at least one application and / or operating state. By means of an embodiment according to the invention, advantageously a particularly advantageous backrest unit with armrests can be provided.

It is further proposed that the armrest device comprises at least one bearing unit, via which the armrest is pivotally mounted in a vertical or horizontal pivot axis to the supporting shell. A "storage unit" should be understood to mean, in particular, a unit by means of which two elements are mounted movably, preferably pivotably, relative to one another In this case, a "vertical pivot axis" is to be understood as meaning, in particular, a vertical plane that is oriented substantially perpendicular to a Aufständerebene

Swivel axis are understood, which is at a right angle on the Aufständerebene. Under a "horizontal pivot axis" is intended in particular a

Swivel axis are understood, which is aligned substantially parallel to the Aufständerebene on which the seat is raised with the armrest device. By "substantially parallel" is meant in particular that the

Pivot axis a maximum of 5 degrees, preferably less than 1 degree of a

Parallels with the insurgent level. As a result, the armrest can be mounted particularly advantageously on the supporting shell and advantageously be adjusted between at least two positions. It is also proposed that the at least one bearing unit has a stop which limits a pivoting range of the armrest. A "stop" should be understood in particular an element that is intended to - -

Limitation of a pivoting range to be contacted by another element, wherein the contacting further pivoting of the two elements is prevented from each other. A "swivel range" should be understood to mean, in particular, an area, in particular an angle range, in which two elements can be pivoted relative to one another

Limited maximum positions of the two mutually pivotable elements.

It is further proposed that the at least one bearing unit has at least one securing module which prevents pivoting of the armrest, at least in one operating state. A "securing module" should be understood to mean, in particular, a module which prevents an adjustment, in particular a pivoting, between a stowed position and a position of use of the armrest

Friction element on which fixes the armrest in a position in at least one operating state by a positive and / or non-positive connection. Under a

In this case, "operating state" is to be understood as meaning, in particular, a state of the security module, wherein the security module preferably has a locking line and an unlocking line as the operating state, whereby the locking module locks the armrest in the locking position, whereby the armrest can not be swiveled Armrest between her

Use position and their stowage be adjusted. This allows the

Armrest can be advantageously secured against adjustment.

Furthermore, it is proposed that the security module at least one

Has securing element which engages the blocking of the bearing unit in a guide groove. Under a "fuse element" is intended in particular a

Positive locking element, for example in the form of a safety pin or a

Hatch that are in a Verriegeisteilung of

Locking module engages positively in a corresponding guide groove and so an adjustment of the armrest between the position of use and the

Stowage prevented. As a result, the locking module can be made particularly simple.

Furthermore, it is proposed that the security module at least one

Actuator having to unlock the securing element with the , ,

Secured element is coupled and at least partially protrudes from the armrest. An "actuating element" should be understood to mean, in particular, an element which can be actuated by an operator in order to actuate the securing module, wherein the actuating element can be actuated by pressing, pulling, rotating, axially moving It should be understood in particular that at least one area that must be contacted by an operator for operating the actuating element, is arranged in an area outside the armrest. In principle, it is also conceivable that the actuating element is formed flush with a bearing element and / or an outer side of the armrest, wherein it is easy to operate from the outside by an operator. As a result, the securing element can be operated in a particularly simple manner and the securing module can thereby be adjusted particularly easily by an operator.

In addition, it is proposed that the at least one armrest has at least one base carrier, which is at least partially formed integrally with the supporting shell. A "basic carrier" should be understood to mean, in particular, an element which forms a supporting structure of the armrest, wherein the basic carrier in particular introduces forces acting on the armrest into the supporting shell, wherein the basic carrier is preferably formed of a same material In this case, the base support of the armrest is preferably laminated to the supporting shell, by "at least partially in one piece" being understood to mean that at least one subarea, such as a connection region, is firmly bonded to the supporting shell , Basically, it is also conceivable that a

Base support is formed separately from the supporting structure and is rigidly connected to the supporting shell, for example via a connection plate or connecting bushes which are firmly integrated in the supporting shell. As a result, the armrest can be coupled with the supporting shell in a particularly advantageous manner.

It is further proposed that the armrest has at least one comfort element which is intended to be connected to the base support. A "comfort element" should be understood to mean, in particular, an element which forms a support surface of the armrest and thereby preferably provides a padded support surface , ,

Basic support to be understood connected, wherein the comfort element for a

Use captive tied to the base support. It can do that

Comfort element for replacement, for example, for a cleaning process, non-destructive be solved by the base support. As a result, an advantageously comfortable armrest can be provided.

In addition, it is proposed that the armrest has at least one shell element, which forms a base body of the armrest. In this case, the armrest preferably has at least two shell elements which in a connected state a

Form the body of the armrest. A "shell element" should in particular be understood to mean a thin-walled element which at least partially defines an interior space and preferably together with at least one correspondingly formed element forms a common element, in particular a base body

in particular, be understood a state in which the at least two

Shell elements are connected to each other via a force, form and / or material connection and form a preferably hollow body. As a result, advantageously a particularly lightweight and at the same time advantageously stable base body for the armrest can be provided.

It is further proposed that the armrest has at least one comfort element, which is intended to be mounted on an upper side of the at least one shell element. As a result, the armrest can be made particularly comfortable.

It is also proposed that the armrest has an actuating element which is provided for actuating a locking module. In this context, an "actuating element" should be understood as meaning, in particular, an element which can be operated by a user, in particular a passenger sitting on the aircraft seat Unlocking a seat adjustment is provided, in which a backrest unit and / or a seat bottom unit of the aircraft seat to a Aufständerebene

is pivoted. , ,

A "locking module" should be understood to mean, in particular, a module which fixes two elements to one another at least in one operating state, in which case the locking module is provided in particular to fix the seat base unit and / or the backrest unit in at least one seating position relative to the mounting unit the seat bottom unit and / or the backrest unit can be fixed in at least one sitting position. "Locking" is understood to mean, in particular, firmly fixing in one position. Under a sitting position is intended in particular a

Alignment of the seat bottom unit and / or the backrest unit to the

Revelation level to be understood. In this case, the aircraft seat has at least one sitting position designed as a TTL position and a comfort position. The TTL position is designed as a position of the aircraft seat, which must be taken in a start, landing and turbulence phase of a flight. The TTL position is designed as a taxi, takeoff or landing position. In this case, the TTL position is formed as an upright sitting position in which the seating area of the seat bottom unit in

Substantially parallel to the Aufständerebene and the backrest surface of the

Backrest unit is aligned substantially orthogonal to the Aufständerebene. For seat adjustment, the transport seat device preferably has a storage module, which supports the backrest unit and / or the seat bottom unit pivotally relative to one another. A "storage module" should be understood to mean, in particular, a module via which at least two elements, such as in particular the

Seating unit and / or the backrest unit, to which at least one

Store module movable, in particular pivotally store. The bearing module is preferably designed as a sliding bearing. In principle, it is also conceivable that the bearing module has one or more roller bearings, via which the elements are designed to be pivotable relative to one another. In principle, it is also conceivable that the

Actuator is formed by a rigid rod, which by axial

Move and / or operated by pivoting the locking module. As a result, the actuation of the locking module can advantageously be integrated into the aircraft seat. It is further proposed that the supporting shell at least in one

Connection region of the at least one armrest has a reinforcing element. A "connection area" is to be understood in particular as an area via which the armrest is connected to the supporting shell , ,

Connection region preferably has at least one connection point, via which the armrest is directly connected to the supporting shell. A "reinforcing element" is to be understood in particular as meaning an element which is intended to reinforce the supporting shell for connecting the armrest and in particular to form connection points for the armrest As a result, the armrest can be tied to the supporting shell in a particularly advantageous manner.

Furthermore, it is proposed that the reinforcing element is formed as an insert, which is integrated in the formed of a fiber composite material shell. The term "inserter" is intended in particular to mean a layer of fiberglass layers inserted in a lay-up process prior to a lamination process of the supporting shell

Element to be understood, which is firmly enclosed in the supporting shell and so integral with the lamination process. As a result, the reinforcing element can advantageously be connected to the supporting shell in a particularly simple and advantageous manner.

Furthermore, it is proposed that the at least one armrest is part of a module which is intended to be connected at least to a part of a Aufständereinheit. Under a "module" is in this context in particular a

Merger of several elements are understood, which are preferably integrally formed with each other, but in principle are also firmly coupled together by suitable form, force and / or material connection connections. In this case, the module preferably comprises the armrest, a tread element, a ram protection, a

Display element and / or storage elements. Under a "part of the

Aufständereinheit "should in particular cross member and / or seat divider of a

Airplane seat to be understood. As a result, the armrest can be formed in a particularly advantageous manner together with other elements of the aircraft seat and be connected together therewith.

It is also proposed that the module form at least one tread element. A "tread element" is to be understood as meaning, in particular, an element which provides a tread area for a person, the tread area in particular providing an increased tread from a substrate, in particular from the cabin floor - -

the one person a higher area, in particular over the

appropriate aircraft seat arranged storage compartments, can easily and conveniently reach. As a result, the module can particularly advantageously form a possibility of stepping, in particular a so-called steward step. As a result, the module can be formed with the armrest particularly advantageous.

The transport seat device according to the invention should not be limited to the application and embodiment described above. In particular, in order to fulfill a mode of operation described herein, the inventive transport seat device may have a number deviating from a number of individual elements, components and units mentioned herein.

drawings

Further advantages emerge from the following description of the drawing. In the drawings, six embodiments of the invention are shown. 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 a schematic illustration of a transport seat device in a first exemplary embodiment with a plurality of aircraft seats of an aircraft seat row,

2 shows a schematic detail view of a part of a storage unit for

Storage of an armrest,

3 is a schematic sectional view through an armrest,

4 shows a schematic representation of an armrest of a

Transport seat device in a second embodiment,

5 shows a schematic representation of an aircraft seat with a

Armrest device in a third embodiment,

6 is a schematic representation of an aircraft seat with a

Armrest device in a fourth embodiment, - -

Fig. 7 is a schematic representation of an aircraft seat with a

Armrest device in a fifth embodiment and

Fig. 8 is a schematic representation of an aircraft seat with a

Armrest device in a sixth embodiment.

Description of the embodiments

Figures 1 to 3 show a first embodiment of a transport seat device according to the invention. The transport seat device is designed as an aircraft seat device. In principle, it would also be conceivable that the transport seat device is designed as a device for another motor vehicle, such as for example for a bus, a train, or another, the expert appears reasonable

Mode of Transport. In this case, the transport seat device would one or more

Transport seats, such as bus seats exhibit. The aircraft seat device is part of an aircraft seat 10a. The aircraft seat 10 a is part of a

Aircraft seat row 12a formed. In principle, however, it would also be conceivable that the aircraft seat 10a is designed as a single seat. The aircraft seat row 12a comprises two further aircraft seats 14a, 16a, which are each arranged on one side of the aircraft seat 10a. The aircraft seats 10a, 14a, 16a have an erector unit 120a. By means of the erector unit 120a, the aircraft seats 10a, 14a, 16a are raised on a cabin floor. The aircraft seats 10a, 14a, 16a are in the

Essentially formed identical to each other, which is why in the following only one aircraft seat 10a is described in detail. A description of the aircraft seat 10a can be used to explain the other aircraft seats 14a, 16a. The aircraft seat 10a has a backrest unit 18a. The seatback unit 18a is provided to provide a seatback support surface on which a passenger seated on the aircraft seat 10a can rest with his back. The backrest unit 18a is arranged at a rear end of the aircraft seat 10a. The backrest unit 18a is arranged at a rear end of a seat bottom unit 88a. The backrest unit 18a has a load-bearing

Bowl 20a on. The supporting shell 20a comprises a thin-walled rear wall 22a. The - -

thin-walled rear wall 22a is formed of a fiber composite material. In this case, the rear wall 22a is formed by a molded CFK plate. In principle, it is also conceivable that the rear wall 22a is formed from another fiber composite material that appears appropriate to the person skilled in the art. The thin-walled rear wall 22a closes the backrest unit 18a towards the rear. The rear wall 22 a of

Backrest unit 18a is in this case the area behind the aircraft seat device, in which a further row of aircraft seats is preferably arranged. The supporting shell 20a of the backrest unit 18a comprises a thin-walled front wall 24a. The thin-walled front wall 24a is connected to the thin-walled rear wall 22a. The thin-walled front wall 24a is formed from a fiber composite material. The thin-walled front wall 24a is essentially formed of a same material as the thin-walled rear wall 22a. The thin-walled front wall 24a is disposed on a front side of the backrest unit 18a. Seen in a sitting direction, the thin-walled front wall 24a is arranged in front of the thin-walled rear wall 22a. The thin-walled rear wall 22a and the thin-walled front wall 24a of the backrest unit 18a are connected to each other. The thin-walled front wall 24a and the thin-walled rear wall 22a are connected to one another in a material-locking manner. In principle, it is also conceivable that the thin-walled front wall 24a and the thin-walled rear wall 22a are subsequently firmly connected to one another via a suitable form, force and / or material connection in their connecting regions. The supporting shell 20a of the backrest unit 18a has no closer

shown stiffening element. The stiffening element is made of a

formed foam-like material. The trained as a foam core

Stiffening element is inserted as an insert during a manufacturing process between the thin-walled rear wall 22a and the thin-walled front wall 24a and glued before the thin-walled rear wall 22a and the thin-walled front wall 24a are firmly connected. Basically it is also conceivable that the

Backrest unit 18a is formed only by a front wall 24a and no

Stiffening element or a rear wall 22a has. The seat bottom unit 88a and the backrest unit 18a are provided to be pivotally connected to the upstand unit 120a. Due to the pivotable mounting of the seat bottom unit 88 a and the backrest unit 18 a, the

Aircraft seat 10 a are brought into a TTL position and in a comfort position. - -

In principle, it would also be conceivable for the aircraft seat 10a to be pivotable through the pivotable mounting into further seating positions. For pivotable mounting of the seat bottom unit 88a and the backrest unit 18a, the transport seat device has a bearing module not shown in detail. The storage module is designed as a pivot bearing. The storage module forms a pivot axis over which the

Seat bottom unit 88a and the backrest unit 18a to the Aufständereinheit 120a are pivotable. The pivot axis forms a pivot point around which the

Seat bottom unit 88a and the backrest unit 18a are pivotable together. The pivot axis is arranged below the seat bottom unit 88a. The

Pivot axis of the bearing module is aligned coaxially with a transverse direction of the Aufständereinheit 120 a. A pivoting of the seat bottom unit 88 a and the

Backrest unit 18a takes place at a point below the seat bottom unit 88a. As a result, a particularly advantageous pivoting of the seat bottom unit 88a and the backrest unit 18a can be achieved. To lock the seat bottom unit 88a and the backrest unit 18a, the transport seat device has a locking module, not shown in more detail. The lock module is provided to seat the seat unit 88a and the

Backrest unit 18a to lock in a sitting position. The locking module fixes the seat bottom unit 88a and the backrest unit 18a in one position only. In this case, the locking module is provided in particular, the

Seat bottom unit 88a and the backrest unit 18a in the TTL position to lock. The locking module is intended to lock the aircraft seat 10a in the TTL position. The lock module does not lock the seat bottom unit 88a and the backrest unit 18a in the comfort position, in particular. The

Locking module is provided for a purely mechanical locking of the aircraft seat 10a.

The transport seat apparatus includes an armrest device 26a. The

Armrest device 26a includes a first armrest 28a and a second armrest 30a. In this case, the first armrest 28a is disposed on a first side of the seat bottom unit 88a of the aircraft seat 10a, and the second armrest 30a is disposed on a first side

opposite side of the seat bottom unit 88a. In principle, it would also be conceivable for the armrest device 26a to have only one armrest 28a on one side - -

Side of the seat bottom unit 88 of the aircraft seat 10 a has. The armrests 28a, 30a are connected to the supporting shell 20a of the backrest unit 18a. The two armrests 28a, 30a are formed substantially the same, which is why only one armrest 28a to be described in more detail below. The armrest 28a includes a first shell member 32a and a second shell member 34a.

In principle, it would also be conceivable that the armrest 28a has only a single shell element, which forms a base body of the armrest. The two shell elements 32a, 34a are formed from a plastic. In principle, it is also conceivable that the shell elements 32a, 34a are formed from a metal, in particular an aluminum or a magnesium. It is particularly conceivable that the shell elements 32a, 34a are formed from a cast aluminum or a magnesium casting. In an assembled state, the two form

Shell elements 32a, 34a together form a base body of the armrest 28a. The shell elements 32a, 34a span an interior in an interconnected state. The shell elements 32a, 34a are over several

Positive locking elements 36a, 38a positively connected to each other. In this case, the one shell element 32a formed as recesses formed, not shown form-fitting elements and the opposite shell element 34a forms a plurality of pins formed as form-fitting elements 36a, 38a, which extend in the direction of the other shell member 32a from. In a connected state, the shell elements 32a, 34a designed as pins engage in the form-fit elements of the shell element 32a which are formed as a recess. As a result, the shell elements 32a, 34a are non-destructively connected to one another.

In principle, it is also conceivable that the two shell elements 32a, 34a are connected to one another via an adhesive connection. The two shell elements 32a, 34a are formed substantially the same. The shell elements 32a, 34a have on sides facing each other a substantially same contour, whereby the shell elements 32a, 34a are formed for connection to each other. The second shell element 34a has a bearing recess 40a in a front region. The bearing recess 40a is provided to support an actuator 1 10a for a locking module. The actuator 1 10a is designed as a rocker arm. To the actuating element 1 10a, a tension member not shown in detail is attached in an assembled state, which connects the actuating element 1 10a with a locking element of the locking module. The - -

Locking element is provided for mechanically locking the backrest unit 18a in at least one sitting position via the locking module. In principle, it is also conceivable that the locking element locks both only the backrest unit 18a and only the seat bottom unit 88a. The tension element is designed as a Bowden cable.

The armrest 28a comprises a comfort element 70a. The comfort element 70a is intended to be mounted on an upper side of the shell elements 32a, 34a. The comfort element 70a is at least partially formed of a soft plastic, which forms a comfortable support surface 72a for a passenger. The

Comfort element 70a has a rigid base body, via which the comfort element 70a is coupled to the shell elements 32a, 34a. The basic body forms downwardly protruding interlocking elements 104a, via which the comfort element 70a can be positively coupled to the shell elements 32a, 34a. About the

Positive locking elements 104a is the comfort element non-destructively separable with the shell elements 32a, 34a connectable.

The armrest device 18a comprises a bearing unit 42a, via which the armrest 28a is pivotably mounted to the supporting shell 20a. The armrest 28a is connected via a connection region 74a with the supporting shell 20a. Of the

Connection region 74a is arranged laterally in the supporting shell 20 of the backrest unit 18a. In this case, a reinforcing element 106a is arranged in the connection region 74a. The reinforcing member 106 a is formed as an insert, which is inserted into the supporting shell 20. The reinforcing member 106 a is as a

Mounting plate formed. The reinforcing element 106a is thereby laminated into the supporting shell 20 during a manufacturing process. The bearing unit 42a forms a horizontal pivot axis 44a. The pivot axis 44a extends in the transverse direction of the aircraft seat 10a. The armrest 28a is pivotable about the bearing unit 42a about the pivot axis 44a between a use position and a stowed position. The bearing unit 42a comprises a bearing pin 46a. The bearing pin 46a forms the pivot axis 44a. The bearing pin 46a is coupled to the supporting shell 20a. The bearing pin 46a is rigidly connected to the supporting shell 20a. The storage unit has a base plate 48a. The base plate 48a is spaced from the supporting shell 20a of the seat back unit 18a. The base plate 48a - -

is connected via screw-formed fasteners 50 a with the supporting shell 20 a. The fastening elements 50a are screwed into the reinforcing element 106a. The base plate 48a is circular. Of the

Bearing pin 46a is guided centrally through the base plate 48a. The bearing pin 46a is rotatably connected to the base plate 48a and the supporting shell 20a. Of the

Bearing pin 46a has a recess 52a, which is provided so that the tension element of the locking module can be guided outwardly from the interior of the armrest 28a. The armrest 28a has a stiffening plate 54a. The stiffening plate 54a is disposed inside the armrest 28a. The

Stiffening plate 54a is rigidly connected to the shell elements 32a, 34a of the armrest 28a. The stiffening plate 54a is formed of a metal. In principle, it is also conceivable that the stiffening plate 54a is formed from a fiber composite material, such as a CFRP or a GRP. The stiffening plate 54a extends from a portion of the base plate 48a to a front end of the armrest 28a. The stiffening plate 54a has a receiving hole 56a through which the bearing pin 46a is guided in an assembled state. The stiffening plate 54a forms a guide groove 58a. The guide groove 58a is formed as a continuous groove penetrating the stiffening plate 54a. The guide groove 58a forms a circular path. The guide groove 58a is arranged circumferentially about the bearing pin 46a. The bearing pin 46a forms in a mounted state a center of the circular path, which forms the guide groove 58a. The bearing unit 42a has a guide pin 60a. The guide pin 60a is disposed in the assembled state in the guide groove 58a. The guide pin 60a is fixed to the base plate 48a of

Storage unit 42 a connected. The guide groove 58a forms two stops for the guide pin 60a. At a first, upper end, the guide groove 58a forms a stop for a position of use of the armrest 28a. At a lower end, the guide groove 58a forms a stop for a stowage position of the armrest 28a. By the stops, which forms the guide groove 58 a at their ends, is a

Pivoting range of the armrest 28a limited. The storage unit 42a has a

Securing module 62a on. The securing module 62a is provided to prevent a pivoting of the armrest 28a in at least one operating state. For this purpose, the securing module 62a has a securing element 64a. The securing element 64a is movably mounted. The securing element 64a is designed as a securing pin. In this case, the securing element 64a is coaxial with the pivot axis via a linear bearing - -

44a displaceable. The securing element 64a is through the base plate 48a of

Bearing unit 42 a guided. In this case, the securing element 64a extends into the guide groove 58a. When the armrest is in the use position, the securing element 64a abuts against the stop which forms the lower end of the guide groove 58a. If the armrest 28a locked in the use position, that is

Secured element 64a arranged in the guide groove 58a. By an axial

Displacement of the securing element 64a is movable from the guide groove 58a. When the securing member 64a is moved out of the guide groove 58a, the armrest 28a with the stiffening plate 54a into which the guide groove 58a is inserted can be turned to the guide pin 60a about the bearing pin 46a and thus brought into the stowed position. For actuating the securing element 64a, the bearing unit 42a has an actuating element 66a. The actuator 66a is connected to the

Secured element 64a firmly connected. The actuator 66a is provided for unlocking the fuse element 64a. The actuator 66a is formed as a handle member that is intended to be gripped by an operator. About the actuator 66a let the fuse element 64a move axially. The bearing unit 42 a has a spring element 68 a, which has a

Restoring force on the securing element 64a exerts. The securing element 64 a must against the restoring force of the spring element 68 a from its rest position in the

Guide groove 58a are deflected. If the armrest 28a is pivoted back out of the storage position into the use position, the securing element 64a is automatically pressed back into the guide groove 58a by the restoring force of the spring element 68a and thus locks the armrest 28a in the position of use again.

The further aircraft seats 14a, 16a of the aircraft seat row 12a, which are respectively arranged on one side of the aircraft seat 10a, each have a backrest unit 1 12a, 1 14a and an armrest 1 16a, 1 18a connected to the backrest unit 1 12a, 1 14a. The aircraft seats 14a, 16a each have only one armrest 16a, 118a. The armrests 1 16a, 1 18a are each arranged on a side facing away from the aircraft seat 10a side of the backrest unit 1 12a, 1 14a of the aircraft seat 14a, 16a. The armrests 28a, 30a of the middle aircraft seat 10a of

Aircraft seat row 12a are provided for the respectively facing outer aircraft seat 14a, 16a. The armrests 1 16a, 1 18a of the aircraft seats 14a, 16a are in the

Essentially formed equal to the armrests 28a, 30a of the aircraft seat 10a. - -

Even with an adjustment of one of the aircraft seats 10a, 14a, 16a in a comfort position can from the adjacent aircraft seat 10a, 14a, 16a, which is arranged in a TTL position, of the two adjacent aircraft seats 10a, 14a, 16a common armrest 16a 16a , 1 18a can be used comfortably. FIGS. 4 to 8 show five further exemplary embodiments of the invention. The following descriptions and the drawings are essentially limited to the differences between the embodiments, with respect to the same components, in particular with respect to components with the same reference numerals, in principle also to the drawings and / or the description of the other

Embodiments, in particular of Figures 1 to 3, can be referenced. To distinguish the embodiments of the letter a is the reference numerals of the embodiment in the figures 1 to 3 adjusted. In the exemplary embodiments of FIGS. 4 to 8, the letter a is replaced by the letters b to f

FIG. 4 shows a second exemplary embodiment of the invention

Transport seat device shown. The transport seat device is as one

Aircraft seat device formed. The aircraft seat device is part of a

Aircraft seat 10b. The aircraft seat 10b has a backrest unit 18b. The backrest unit 18b is intended to provide a backrest support surface on which a passenger sitting on the aircraft seat 10b can rest with his back. The backrest unit 18b has a supporting shell 20b. The supporting shell 20b is formed substantially identically to the supporting shell of the preceding embodiment. The transport seat apparatus includes an armrest device 26b. The armrest device 26b includes a first armrest 28b and a second armrest, not shown. The armrest 28b has a main body 108b. The main body 108b of the armrest 28b is formed from a plastic. In principle, it is also conceivable that the main body 108b of the armrest 28b is formed from another material that appears appropriate to a person skilled in the art. The armrest 28b comprises a comfort element 70b. The

Comfort element 70b is arranged on an upper side of the armrest 28b and forms a support surface 72b for a passenger. In this case, the comfort element 70b is formed upholstered. The comfort element 70b is formed, for example, from a soft plastic. In principle, it is also conceivable that the comfort element 70b - -

at least partially formed by a foam. In principle, it is also conceivable that the comfort element 70b has a cover, which is preferably replaceable. In principle, it is also conceivable that the comfort element 70b is formed from a silicone. The armrest 28b is connected to the supporting shell 20b. In this case, the

Armrest device 26b for pivotally mounting the armrest 28b a

Storage unit 42b. About the bearing unit 42b, the armrest 28b is pivotable between a stowage position and a use position. In this case, the

Bearing unit 42b on a bearing shell 20b connected to the bearing element 76b. The bearing member 76b is fixedly connected to the supporting shell 20b. For this purpose, the bearing unit 42 has three fastening elements 50b, which are designed as screw elements. The fastening elements 50b are arranged in a connection region 74b of the supporting shell 20b. It is conceivable that in the

Attachment 74b one or more reinforcing elements are arranged, which reinforce the connection region 74b. The reinforcing elements may be formed as sockets, each trained as a screw member

Fastener 50b a socket is inserted into the supporting shell 20b. It is also conceivable that the reinforcing element is formed as a single plate, which is formed in the connection region 74b, for example, by lamination firmly connected to the supporting shell 20b. The bearing member 76b has a circular support portion 78b provided for supporting the armrest 28b thereon. A center of the circular support portion 78b forms a pivot axis 44b of the bearing unit 42b. The bearing member 76b has a different from the

Supporting region 78b rising stop 86b. The stopper 86b is as a

Formed elevation, which rises radially on the circular support portion 78b to the outside. For connection to the bearing element 76b, the armrest 28b has a bearing receptacle 80b. The bearing receptacle 80b has a recess which is so large that the bearing element 76b can be arranged centrally with the stop 86b. The bearing receptacle 80b forms two bearing elevations 82b, 84b protruding inward from an edge of the recess. The bearing elevations 82b, 84b extend in an assembled state except for the circular support region 78b of the

Bearing element 76b. As a result, the armrest 28b is mounted via the bearing elevations 82b, 84b via a slide bearing to the circular support region 78b. The - -

Bearing bosses 82b, 84b together with the stopper 86b respectively

Maximum stops, which limit a pivoting range of the armrest 28b between the position of use and the stowed position. In the position of use of the armrest 28b, the stop 86b of the bearing element 76b bears against the bearing elevation 82b. In the stowed position, the stopper 86b bears against the bearing elevation 84b.

FIG. 5 shows a third exemplary embodiment of the invention

Transport seat device. The transport seat device is designed as an aircraft seat device. The aircraft seat device is part of an aircraft seat 10c. Of the

Aircraft seat 10c has a backrest unit 18c. The seatback unit 18c is provided to provide a seatback support surface on which a passenger seated on the aircraft seat 10c can rest with his back. The backrest unit 18c has a supporting shell 20c. The supporting shell 20c is formed of a fiber composite material. In this case, the supporting shell 20c on a front wall 24c, which is formed of a plurality of fiber composite layers. It is conceivable that the front wall 24 c, which forms the supporting shell 20 c, from

different fiber composite layers, in particular CFK layers and / or fiberglass layers, is formed. The aircraft seat 10c includes a seat bottom unit 88c. The

Seat bottom unit 88c is provided to seat a passenger

provide. The seat bottom unit 88c is partially integral with the

Backrest unit 18c formed. The seat bottom unit 88c is of the load-bearing

Shell 20c, which forms the backrest unit 18c formed. The seat bottom unit 88c and the backrest unit 18c are formed together by a common shell 20c. The seat bottom unit 88c and the backrest unit 18c are common on a cabin floor of an aircraft cabin via an erector unit

elevated.

The transport seat apparatus includes an armrest device 26c. The

Armrest device 26c has a first armrest 28c. The armrest 28c is connected to the seatback unit 18c on a first side of the seat bottom unit 88c. The armrest 28c has a base support 90c. The base support 90c of the armrest 28c is integral with the supporting shell 20c of the seat back unit 18c

educated. The armrest 28c is at least partially formed on the supporting shell 20c. In this case, the base support 90c of the armrest 28c is made of a , -

Fiber composite formed. It is conceivable that the base support 90c is formed of a same fiber composite material as the supporting shell 20c. The base support 90c of the armrest 28c and the supporting shell 20c are made together in a lamination process. In principle, it would also be conceivable that the base support 90c is subsequently connected via a material connection, for example by gluing, or by a screw connection with the supporting shell 20c. The armrest 28c has a comfort element 70c. The comfort element 70c is connected to the base support 90c of the armrest 28c. The comfort element 70c forms a support surface for a passenger and is formed from a padded material. Here, the comfort element 70c is non-destructively separable connected to the base support 90c. Thereby, the comfort element 70c can be easily exchanged. The comfort element 70 c is not shown in detail locking elements with the

Base support 90c connected. In principle, it is also conceivable that the comfort element 70c is connected to the base support 90c by means of a material connection or via other form and / or adhesion elements that appear appropriate to the person skilled in the art. The armrest 28c is rigidly and immovably connected to the supporting shell 20c. The armrest device 26c has only the armrest 28c integrally formed on one side with the supporting shell 20c. In principle, it would be conceivable for the armrest device 26c to have an armrest that can be attached to the supporting shell 20c on the opposite side of the armrest 28c. An armrest for the opposite side of the aircraft seat 10c is attached, for example, to a non-illustrated, arranged next to the aircraft seat 10c aircraft seat, which is part of a same row of aircraft seats as the aircraft seat 10c. This further armrest is preferably formed the same as the armrest 28c described above which is partially formed integrally with the supporting shell 20c.

FIG. 6 shows a fourth exemplary embodiment of the invention

Transport seat device. The transport seat device is designed as an aircraft seat device. The aircraft seat apparatus is part of an aircraft seat 10d. Of the

Aircraft seat 10d has a backrest unit 18d. The backrest unit 18d is intended to provide a backrest support surface on which a passenger sitting on the aircraft seat 10d can rest with his back. The backrest unit 18d has a supporting shell 20d. The supporting shell 20d is formed of a fiber composite material. In this case, the supporting shell 20d has a - -

Front wall 24d, which is formed of several fiber composite layers. It is conceivable that the front wall 24d, which forms the supporting shell 20d, from

different fiber composite layers, in particular CFK layers and / or fiberglass layers is formed. The aircraft seat 10d includes a seat bottom unit 88d. The

Seat bottom unit 88d is intended to provide a seating surface for a passenger. The seat bottom unit 88d is partially integral with the

Backrest unit 18d formed. The seat bottom unit 88d is formed by the supporting shell 20d constituting the seat back unit 18d. The seat bottom unit 88d and the backrest unit 18d are formed together by a common shell 20d. The seat bottom unit 88d and the backrest unit 18d are common on a cabin floor of an aircraft cabin via an erector unit

elevated.

The transport seat apparatus includes an armrest device 26d. The

Armrest device 26d has a first armrest 28d and a second armrest 30d. The armrest 28d is on a first side of the seat bottom unit 88d at the

Backrest unit 18ad tethered. The second armrest 30d is connected to the backrest unit 18d on an opposite side. The armrests 28d, 30d are substantially the same design as those in the preceding third embodiment. The armrests 28d, 30d each include a base support 90d formed integrally with the supporting shell 20d. The

Armrest device 26d thereby forms two armrests 28d, 30d integrally formed on the supporting shell 20d. The armrests 28d, 30d are rigidly and non-movably connected to the backrest unit 18d.

FIG. 7 shows a fifth exemplary embodiment of the invention

Transport seat device. The transport seat device is designed as an aircraft seat device. The aircraft seat device is part of an aircraft seat 10e. Of the

Aircraft seat 10e is formed as part of an aircraft seat row 12e. In principle, however, it would also be conceivable that the aircraft seat 10e is designed as a single seat. The aircraft seat row 12e comprises two further aircraft seats 14e, 16e, which are arranged next to the aircraft seat 10e. The aircraft seat 10e is designed as a seat-side seat. The aircraft seat 14e is designed as a middle seat and the third aircraft seat 16e as an outer seat. The aircraft seats 10a, 14a, 16a have a , -

Aufständereinheit 120e on. By means of the erector unit 120e, the aircraft seats 10e, 14e, 16e are raised on a cabin floor. The two other aircraft seats 14e, 16e are identical. The two aircraft seats 14e, 16e are formed like the corresponding aircraft seat from the third embodiment disclosed in FIG. The aircraft seats 14e, 16e also each have one

Backrest unit 1 12e, 1 14e with a supporting shell and in each case an integrally formed armrest 1 16e, 1 18e. To explain the aircraft seats 14e, 16e, the description of the aircraft seat of the third Ausführungsbeis can be used. By the same configuration of the aircraft seats 14e, 16e, identical parts can advantageously be used to form the row of aircraft seats 12e, which in particular can save costs.

The aircraft seat 10e has a backrest unit 18e. The seat back unit 18e is provided to provide a seat back support surface on which a passenger sitting on the airplane seat 10e can rest with his back. The backrest unit 18e has a supporting shell 20e. The supporting shell 20e is formed of a fiber composite material. In this case, the supporting shell 20e on a front wall 24e, which is formed of a plurality of fiber composite layers. It is conceivable that the front wall 24e, which forms the supporting shell 20e, made

different fiber composite layers, in particular CFK layers and / or fiberglass layers, is formed. The aircraft seat 10e includes a seat bottom unit 88e. The

Seat bottom unit 88e is provided to seat a passenger

provide. The seat bottom unit 88e is partially integral with the

Backrest unit 18e formed. The seat bottom unit 88e is formed by the supporting shell 20e that constitutes the seat back unit 18e. The seat bottom unit 88e and the backrest unit 18e are formed together by a common shell 20e. The seat bottom unit 88e and the backrest unit 18e are raised together on an elevator unit 120e on a cabin floor of an aircraft cabin.

The transport seat apparatus includes an armrest device 26e. The

Armrest device 26e has a first armrest 28e and a second armrest 30e. The first armrest 28e is formed on the supporting shell 20e equivalent to the previous embodiments. The second armrest 30e also has one , -

Base support 92e on. The base support 92e is formed on the supporting shell 20e. In this case, the base support 92e is shorter than the base support 90e of the armrest 28e. The armrest 30e has a second base support 94e which is connected to the first base support 92e. The two basic carriers 92e, 94e form one

Basic body of the armrest 30e. The armrest 30e includes a storage unit 42e. Via the bearing unit 42e, the armrest 30e is designed to be pivotable relative to the supporting shell 20e. The bearing unit 42e pivotally supports the second base bracket 94e to the first base bracket 92e of the armrest 30e. In this case, the bearing unit 42e bearing elements not shown in detail. The bearing elements are designed as bearing pins and bearing mounts, which are coupled together in a known manner to achieve a pivotal connection. The storage unit 42e forms a

Pivot axis 44e, about which the armrest 30e is pivotable to the supporting shell 20e. About the pivot axis 44e of the second base support 94e is pivotable to the first base support 92e of the armrest 30e. The bearing unit 42e has a securing module, not shown in more detail, by means of which the bearing unit 42e can be fixed in the position of use. By pivoting the armrest 30e, an improved access to the aircraft seat 10e can preferably be achieved.

Figure 8 shows a sixth embodiment of an inventive

Transport seat device. The aircraft seat 10f has a backrest unit 18f. The seat back unit 18f is provided to provide a seat back support surface on which a passenger seated on the aircraft seat 10f can rest with his back. The backrest unit 18f has a supporting shell 20f. The supporting shell 20f is formed of a fiber composite material. The

Transposing seat apparatus includes a seat bottom unit 88f. The seat bottom unit 88f and the seat back unit 18f are connected to each other. To raise the

Seat bottom unit 88f and the backrest unit 18f, the aircraft seat 10f on a Aufständereinheit. The Aufständereinheit comprises seat feet, by means of which

Aufständereinheit is coupled to a floor. The Aufständereinheit further has two cross members 96f, 98f. The cross members 96f, 98f extend transversely to a seat direction of the aircraft seat 10f and are rigidly connected to the seat feet. The cross members 96f, 98f extend over an entire width of an aircraft seat row 12f, part of which is the aircraft seat 10f. The cross members 96f, 98f are formed as tubular elements. In this case, a first cross member 96 f is formed as a front support tube, which in a , -

front area of the Aufständereinheit is arranged. The second cross member 98f is formed as a rear support tube disposed in a rear portion of the stand unit. The aircraft seat 10 f is as a gangseitiger seat of

Aircraft seat row 12f formed. The aircraft seat 10f is formed as a seat facing a cabin passage. The aircraft seat 10f is designed in particular like the corresponding aircraft seat from the third exemplary embodiment of FIG. The aircraft seat row 12 f comprises at least two further aircraft seats, not shown in greater detail, which are of the same design as the aircraft seat 10 f. As a result, it is particularly advantageous to provide an aircraft seat row 12f which has many identical seats and thus identical parts. As a result, a particularly advantageous cost-effective row of aircraft seats can be provided.

The transport seat apparatus has an armrest unit 26f. The armrest unit 26f includes a first armrest 28f and a second armrest 30f. The second armrest 30f should not be described in detail. The second armrest 30f may be formed according to one of the armrests from the preceding embodiments. The armrest 28f is disposed on a corridor side of the aircraft seat 10f. In this case, the armrest 28f is formed as a part of a module 10Of which is intended to be connected to a part of the stand-up unit. The module 10Of is intended to be connected to the cross members 96f, 98f of the stand-up unit. The module 10Of forms a main body 122f. Via the main body 122f, the module 10Of is connected to the cross members 96f, 98f. In this case, the module 10Of is connected via connecting elements, not shown, to the cross members 96f, 98f. The connecting elements can be designed as form-fitting elements, such as receiving holes. It is conceivable that the module is secured by further fastening elements, such as screws, on the Aufständereinheit. The module 10Of is formed from a fiber composite material. In principle, it is also conceivable that the module is formed of a metal, such as an aluminum or a magnesium. In this case, the module 10Of is formed, for example, from an aluminum casting or a magnesium casting. At an upper end, the module 10Of forms the armrest 28f. In this case, the armrest 28f comprises a comfort element 70f which is coupled to the module 10Of in order to form a support surface. The armrest 28f includes a storage unit 42f. The armrest 28f can be pivoted via the bearing unit 42f to the base body 122f of the module 10Of - -

educated. In this case, the bearing unit 42f bearing elements not shown in detail. The bearing elements are designed as bearing pins and bearing mounts, which are coupled together in a known manner to achieve a pivotal connection. The bearing unit 42f forms a pivot axis 44f about which the armrest 28f is pivotable towards the main body 122f of the module 10Of. At a lower end, the module forms a tread element 102f. The tread element is designed as a stewardstep. The tread 102f is integrally formed with the module 10Of. The

Tread element 102f is formed from a fiber composite material. In principle, it is also conceivable that the tread element 102f is formed from a different material, such as a metal. It is also conceivable that the tread element 102f is formed separately from the module 10Of and is connected to the module 10Of via a suitable connection method. The module 10Of further forms a crash protection, which protects the aircraft seat 10f laterally. In this case, the base body 122f of the module 10Of is designed as a ramming protection. The module 10Of further functions as a cover member.

, -

airplane seat

Aircraft seat row

airplane seat

Backrest unit

carrying shell

rear wall

front wall

armrests device

armrest

shell element

Form-fitting element

bearing recess

storage unit

swivel axis

bearing bolt

baseplate

fastener

recess

stiffening plate

receiving hole

guide

guide pin

security module

fuse element

actuator , -

spring element

comfort element

bearing surface

connecting region

bearing element

support area

bearing seat

camp survey

attack

Seat bottom unit

base support

crossbeam

module

Step element

Form-fitting element

reinforcing element

body

actuator

Backrest unit

armrest

riots purity

body

Claims

claims

A transport seat device, in particular an aircraft seat device, having at least one backrest unit (18a; 18b; 18c; 18d; 18e; 18f) which has at least one supporting shell (20a; 20b; 20c; 20d; 20e; 20f) which consists at least substantially of a fiber composite material and an armrest device (26a; 26b; 26c; 26d; 26e; 26f) comprising at least one

An armrest (28a, 28b; 28b; 28c; 28d, 30d; 28e, 30e; 28f, 30f) connected to the supporting shell (20a; 20b; 20c; 20d; 20e; 20f). The transport seat apparatus according to claim 1, characterized in that the armrest device (26a; 26b; 26e) comprises at least one bearing unit (42a; 42b; 42e) over which the armrest (28a, 30a; 28b; 28e) is mounted in a vertical or horizontal pivotal axis (44a; 44b; 44e) is pivotally mounted to the supporting shell (20a; 20b; 20e). A transport seat apparatus according to claim 2, characterized in that the at least one bearing unit (42a; 42b) has a stopper which limits a pivoting range of the armrest (28a, 30a; 28b). 4, the transport seat device according to claim 2 or 3, characterized in that the at least one bearing unit (42a) at least one securing module (62a), which prevents pivoting of the armrest (28a) at least in one operating state.

Transport seat device according to claim 4, characterized in that the securing module (62a) at least one securing element (64a) which engages to block the bearing unit (42a) in a guide groove (58a).

6. Transport seat device according to claim 4, characterized in that the securing module (62a) has at least one actuating element (66a) which is for unlocking the securing element (64a) with the securing element (64a) coupled and at least partially protruding from the armrest (28a) ,

The transport seat apparatus according to one of the preceding claims, characterized in that the at least one armrest (28c; 28d, 30d; 28e) comprises at least one base support (90c; 90d; 92e, 94e) at least partially integral with the supporting shell (20c 20d, 20e) is formed.

8. Transport seat device according to claim 7, characterized in that the armrest (28c) has at least one comfort element (70c) which is intended to be connected to the base support (90c).

9. Transport seat device according to one of the preceding claims, characterized in that the armrest (28 a) at least one shell element (32 a, 34 a), which forms a base body of the armrest (28 a).

10. Transport seat device according to claim 9, characterized in that the armrest (28 a) has at least one comfort element (70 a), which is intended to be mounted on an upper side of the at least one shell element (32 a, 34 a).

1 1. Transport seat device according to one of the preceding claims, characterized in that the armrest (28a) has an actuating element (1 10a) which is provided for actuating a locking module.

12. Transport seat device according to one of the preceding claims, characterized in that the supporting shell (20 a) at least in one

Connection region (74a) of the at least one armrest (28a)

Reinforcing element (106a).

13. Transport seat device according to claim 12, characterized in that the reinforcing element (106a) is formed as an insert, which is integrated in the formed of a fiber composite material shell (20a).

14. Transport device according to one of the preceding claims, characterized

characterized in that the at least one armrest (28f) is part of a module

(1 OOf), which is intended, at least with a part of a

Aufständereinheit to be connected.

15. Transport device according to claim 14, characterized in that the module (1 OOf) at least one tread element (102f) is formed.

16. Aircraft seat with a transport seat device according to one of the preceding claims.