Table configuration assembly for an aircraft and cabin area

Abstract

The present invention relates to a table configuration assembly (10) comprising a mounting element (12) fastenable to a fastening structural element (102) and defining a mounting plane (E). Furthermore, the table configuration assembly (10) includes a first table element (20) connected to the mounting element (12), wherein the first table element (20) is pivotable relative to the mounting element (12) about a first pivot axis (S1) between a stowed position and a used position, wherein in the stowed position the first table element (20) extends substantially parallel to the mounting plane (E) defined by the mounting element (12), and in the used position the first table element (20) extends substantially perpendicular to the mounting plane (E) defined by the mounting element (12). Finally, the table configuration assembly (10) includes a second table element (22) connected to the first table element (20), wherein the second table element (22) is arranged substantially parallel to the first table element (20) and is rotatable relative to the first table element (20) about a rotation axis (D) arranged parallel to the mounting plane (E) in the used position.

Description

Technical Field

[0001] This invention relates to a table configuration assembly suitable for use in an aircraft cabin. Furthermore, this invention relates to a cabin area equipped with such a table configuration assembly. Background Technology

[0002] In modern transportation, especially in passenger aircraft, the optimal use of available space in the cabin is of great economic significance. Therefore, for tasks such as writing, crew members typically use small, multi-purpose folding tables, which can be placed, for example, in the area of ​​the onboard galley or near the flight attendant's seats. Summary of the Invention

[0003] The object of the present invention is to provide a table configuration assembly suitable for use in the cabin of a vehicle, the table configuration assembly providing a usable workspace for crew members, such as purser, but which can be stowed away to save space when not in use. Furthermore, the object of the present invention is to provide a cabin area equipped with such a table configuration assembly.

[0004] The task is accomplished by having a table configuration assembly according to the invention and a cabin area according to the invention.

[0005] The table configuration assembly includes mounting elements that can be fastened to a fastening structural element. For example, the mounting elements of the table configuration assembly can be configured to fasten to a fastening structural element that is suited for installation on large objects in a passenger cabin, particularly an aircraft cabin. Large objects may be, for example, onboard galleys, lavatory modules, partitions, storage cabinets, or similar large objects. The mounting elements of the table configuration assembly define a mounting plane. With the table configuration assembly fastened to the fastening structural element, the mounting plane defined by the mounting elements can, for example, extend substantially parallel to the wall surface of the fastening structural element facing the mounting element.

[0006] The table configuration assembly also includes a first table element connected to a mounting element. The first table element is pivotable relative to the mounting element about a first pivot axis between a stowed position and a used position. In its stowed position, the first table element extends substantially parallel to the mounting plane defined by the mounting element. Conversely, in its used position, the first table element extends substantially perpendicular to the mounting plane defined by the mounting element. Thus, the first table element can be stowed away to save space or used as a workspace as needed.

[0007] Finally, the table configuration assembly includes a second table element connected to the first table element. The second table element is arranged substantially parallel to the first table element and is rotatable relative to the first table element about a rotation axis that is parallel to the mounting plane in the use position. In the retracted position of the first table element, the rotation axis is arranged perpendicular to the mounting plane. Through its connection to the first table element, the second table element moves together with the first table element as the first table element pivots between its retracted and use positions. Therefore, when the first table element is in its retracted position, the second table element, arranged parallel to the first table element, can also be retracted space-savingly. Conversely, when the first table element is in its use position, the second table element can be positioned relative to the first table element by rotation about the rotation axis, such that both the first and second table elements can be used as a workspace. This achieves a relatively large workspace.

[0008] Preferably, the second table element is connected to the first table element in the region of the end of the first table element opposite to the first pivot axis. This maximizes the working surface provided by the first and second table elements. In particular, the axis of rotation is also arranged in the region of the end of the first table element opposite to the first pivot axis. The end of the first table element opposite to the first pivot axis is preferably constructed to be rounded. Attached here or alternatively, the end of the second table element connected to the first table element can also be constructed to be rounded. Conversely, the free end of the second table element can have straight edges.

[0009] Additionally or alternatively, a friction-generating element may be disposed in the region of the rotation axis, the friction-generating element being configured to minimize undesirable movement of the second table element relative to the first table element about the rotation axis. The friction-generating element is preferably disposed in the region of the rotation axis between the first and second table elements and may be made of, for example, a plastic material, an elastomer material, etc., to resist undesirable rotation of the second table element about the rotation axis.

[0010] In this implementation, the friction-generating element is designed to produce a constant, sustained frictional force. This frictional force can be set once, for example, during the installation of the table configuration assembly, using screws or the like. However, if desired, the friction-generating element can also be designed such that the frictional force it applies is variable and manually set. The user of the table configuration assembly can then, for example, first rotate the second table element about the axis of rotation with the friction-generating element deactivated and then activate the friction-generating element to hold the second table element in its position.

[0011] In a preferred embodiment of the table configuration assembly, the second table element is rotatable relative to the first table element about a rotation axis between an overlapping position and a working position. When the second table element is in its overlapping position relative to the first table element, the first and second table elements are preferably arranged in a position of maximum overlap, i.e., minimizing the area of ​​one table element protruding from the other. Thus, the longitudinal axis of the first table element, especially the central longitudinal axis, preferably extends parallel to the longitudinal axis of the second table element, especially the central longitudinal axis. When the first table element is in its folded position, the second table element is preferably arranged relative to the first table element in its overlapping position. This minimizes the positional requirements of the table configuration assembly. The rotation axis is perpendicular to the two central longitudinal axes of the first and second table elements, especially at the intersection of the two central longitudinal axes. Therefore, the rotation axis intersects these two central longitudinal axes, particularly at the intersection.

[0012] Conversely, when the second table element is in its working position relative to the first table element, the longitudinal axis of the first table element can form an angle of approximately 80 to 120° with the longitudinal axis of the second table element, particularly an angle of approximately 90 to 110°. When the first table element is in its use position, the longitudinal axis of the first table element can, for example, extend substantially perpendicular to the mounting plane defined by the mounting element.

[0013] This allows for a particularly comfortable workspace with two "table legs".

[0014] Additionally or alternatively, at least when the first table element is positioned in its stowed position, the second table element may be movable relative to the first table element in a direction parallel to the longitudinal axes of the first and second table elements. In particular, the second table element may be connected to the first table element such that, when the first table element is positioned in its stowed position, the second table element is movable relative to the first table element in a direction toward the first pivot axis, parallel to the longitudinal axes of the first and second table elements.

[0015] Preferably, the second table element has a smaller area than the first table element. For example, the second table element may have a shorter dimension in the direction of its longitudinal axis than the first table element in the direction of its longitudinal axis. Additionally or alternatively, the second table element may be constructed identically to a section of the first table element; that is, the second table element may be shaped such that when the second table element is arranged relative to the first table element in its overlapping position, the second table element completely overlaps with a section of the first table element. The section of the first table element constructed identically to the second table element preferably forms a section of the first table element opposite to the first pivot axis.

[0016] The first table element may be provided with a first edge protection profile. The first edge protection profile may extend along at least one segment of the circumferential edge of the first table element, and may be made of, for example, a suitable plastic material. Preferably, the first edge protection profile extends along the entire circumferential edge of the first table element, thereby forming a continuous boundary of the tabletop of the first table element. Additionally or alternatively, the second table element may also be provided with a second edge protection profile, which may be made of, for example, a suitable plastic material and preferably extends along at least one segment of the circumferential edge of the second table element. Preferably, the second edge protection profile extends along the entire circumferential edge of the second table element, thereby forming a continuous boundary of the tabletop of the second table element. The edge protection profile protects the edge areas of the first table element and / or the second table element from damage.

[0017] Preferably, the first edge protection profile protrudes from the tabletop of the first table element in a direction parallel to the axis of rotation. Additionally or alternatively, the second edge protection profile may also protrude from the tabletop of the second table element in a direction parallel to the axis of rotation. This design of the edge protection profile ensures that spilled liquid is contained up to a certain amount and ensures that objects placed on the table configuration assembly do not slip off.

[0018] The tabletop of the first table component can be constructed to be non-slip. Alternatively or additionally, the tabletop of the second table component can also be constructed to be non-slip. For example, the first table component and / or the second table component can be made of non-slip material or have a non-slip coating.

[0019] In a preferred embodiment of the table configuration assembly, the second table element is arranged relative to the first table element such that the lower surface of the second table element faces the tabletop of the first table element. This makes the operation of the table configuration assembly particularly simple, especially when the second table element changes between its overlapping and working positions, and when the first table element changes between its used and stowed positions.

[0020] The first and second table elements are preferably sized such that the user of the table configuration assembly can place three DIN-compliant A4 sheets on the first and second table elements. In particular, the first table element is shaped such that its dimension in its longitudinal axis direction is larger than its dimension in the direction perpendicular to its longitudinal axis. Additionally or alternatively, the second table element may be shaped such that its dimension in its longitudinal axis direction is larger than its dimension in the direction perpendicular to its longitudinal axis. The dimensions of the first table element in both its longitudinal and perpendicular directions are preferably determined such that the user of the table configuration assembly can place two DIN-compliant A4 sheets in a landscape orientation on the first table element. The dimensions of the second table element in both its longitudinal and perpendicular directions are preferably determined such that the user of the table configuration assembly can place one DIN-compliant A4 sheet in a landscape orientation on the second table element.

[0021] Furthermore, a handle can be constructed on the first table element. When the first table element is to pivot between its stowed position and its usable position, the user can grasp the handle. The handle is particularly located in the region at the end of the first table element opposite to the first pivot axis. For example, the handle can be constructed in the form of a groove formed into the underside of the first table element opposite to its tabletop.

[0022] Preferably, the first pivot axis (about which the first table element is pivotable between its stowed position and its used position) is movable relative to the mounting element between a rest position and an operating position when the first table element switches between its stowed position and its used position. The movement of the first pivot axis relative to the mounting element can be a translational movement of the first pivot axis within a mounting plane defined by the mounting element. Therefore, when the first table element switches between its stowed position and its used position, the end of the first table element facing the first pivot axis performs not only a pivotal movement about the first pivot axis but also a translational movement within the mounting plane.

[0023] When the table configuration assembly is operationally ready and mounted on a fastening structural element in the aircraft cabin, the first pivot axis preferably moves upward relative to the mounting element in the mounting plane defined by the mounting element when the first table element is transitioned from its stowed position to its used position. Conversely, the first pivot axis preferably moves downward relative to the mounting element in the mounting plane defined by the mounting element when the first table element is transitioned from its used position to its stowed position. This movable design of the first pivot axis enables a particularly space-saving implementation of the table configuration assembly, as the first table element thus protrudes significantly less from the mounting element in its longitudinal direction in its stowed position compared to an arrangement with a rigid first pivot axis.

[0024] The table configuration assembly may also include a guiding device for guiding the movement of the first pivot axis between its rest position and its operating position. For example, the guiding device may include at least one guide rail in which the end of the first pivot axis is movably received. Preferably, the guiding device includes two substantially parallel guide rails, each movably receiving an end of the first pivot axis. The guiding device, i.e., one or more guide rails of the guiding device, is preferably secured to the mounting element.

[0025] In a preferred embodiment, the mounting element of the table configuration assembly includes two sidewalls. The sidewalls of the mounting element may extend substantially perpendicular to the mounting plane defined by the mounting element. Additionally or alternatively, the sidewalls of the mounting element may extend substantially parallel to each other. Additionally or alternatively, the mounting element may include a rear wall. The rear wall preferably extends within the mounting plane defined by the mounting element.

[0026] Preferably, the table configuration assembly further includes a locking mechanism for locking the first table element in its usage position. For example, the locking mechanism may include a first locking element connected to a mounting element and a second locking element complementary to the first locking element and connected to the first table element. The locking element may, for example, be positioned on the first table element in a region of the end of the first table element facing the first pivot axis.

[0027] In a particularly preferred embodiment, the locking mechanism is designed such that it is activated by applying pressure to the tabletop of a first table element positioned in its use location. For example, the first and / or second locking elements of the locking mechanism can be arranged and configured such that the first and second locking elements automatically engage with each other whenever the user applies a corresponding pressure to the tabletop of the first table element positioned in its use location.

[0028] Additionally or alternatively, the locking mechanism can be designed such that its activation is associated with an audible sound. For example, the first and / or second locking elements of the locking mechanism can be designed such that a click is heard when the two locking elements engage. The user of the table configuration component then receives an audible signal indicating to the user that the first table component is securely in its usage position.

[0029] Furthermore, the table configuration assembly may include a manually operable release mechanism for releasing the locking mechanism. The release mechanism may be fastened to the mounting element. For example, the release mechanism may include an operating button connected to a first locking element of the locking mechanism via a connecting element. The operating button may, for example, be fastened to a retaining element extending between two sidewalls of the mounting element. Manual operation of the operating button, such as pressing, may be transmitted to the first locking element via the connecting element, thereby releasing the first locking element from the second locking element.

[0030] The table configuration assembly preferably further includes a support element, the first end of which is pivotally connected to the mounting element about a second pivot axis. Conversely, the second end of the support element is preferably pivotally connected to the first table element about a third pivot axis. In particular, the second end of the support element is connected to the underside of the first table element. Thus, the support element is pivotable relative to the mounting element and the first table element between a rest position and a supported position. In its rest position, occupied by the support element when the first table element is in its folded position, the support element is arranged substantially parallel to the first table element. Conversely, in its supported position, occupied by the support element, when the first table element is in its used position, the longitudinal axis of the first table element forms an angle of about 30 to 60°, particularly about 40 to 50°, and particularly preferably about 45° with the longitudinal axis of the support element.

[0031] The support element provides increased load-bearing capacity to the first table element, making it more load-bearing than the second table element. Preferably, the support element is sized so that the first table element can bear a load of 5 kg. This allows users of the table configuration assembly to place electronic devices, such as tablets or lightweight laptops, on the first table element.

[0032] Furthermore, the table configuration assembly may include a locking mechanism for locking the first table element in its retracted position. For example, the locking mechanism may include at least one locking lever rotatably mounted on the mounting element about a rotation axis. When the locking lever is in the locked position, it preferably rests against the underside of the first table element opposite to its tabletop or against a support element, thereby holding the first table element in its retracted position. Conversely, when the locking lever is in the released position, it releases the first table element or support element, allowing the first table element to move from its retracted position to its usable position. To ensure particularly reliable locking of the first table element in its retracted position, the locking mechanism may have two locking levers. The locking mechanism then meets aircraft-permitted requirements. The two locking levers are preferably fastened to the mounting element such that, in their locked position, they rest against the underside of the first table element in the region of two opposing edge areas of the first table element or in the region of two opposing edge areas of the support element.

[0033] The cabin area, particularly the aircraft cabin area, includes fastening structural elements and the aforementioned table configuration components. The fastening structural elements are constructed, in particular, in the form of large objects (e.g., galleys, lavatory modules, storage compartment partitions, or similar large objects). The mounting elements for the table configuration components are fastened to the fastening structural elements.

[0034] In a preferred embodiment of the cabin area, seats, particularly crew seats, are fastened to a fastening structural element adjacent to a table configuration assembly. The table configuration assembly can then be optimally used by the person sitting in the seat. Attached Figure Description

[0035] Preferred embodiments of the invention will now be described in more detail with the aid of the accompanying drawings, wherein...

[0036] Figure 1 The front view shows a table configuration assembly suitable for use in passenger cabins, particularly aircraft cabins, wherein the first table element of the table configuration assembly is in a stowed position.

[0037] Figure 2 The following view shows the results based on Figure 1 Desktop configuration components,

[0038] Figure 3 Shown in 3D view according to Figure 1 Desktop configuration components,

[0039] Figure 4 The diagram illustrates the process of the first table element in the table configuration assembly transitioning from its stowed position to its used position. Figure 3 Desktop configuration components,

[0040] Figure 5 Showing according to Figure 3 and Figure 4 A table configuration component, wherein a first table element occupies its usage position, while a second table element is arranged in an overlapping position relative to the first table element.

[0041] Figure 6a and Figure 6b Showing according to Figure 5 The table configuration components, wherein the second table element is arranged in a working position relative to the first table element.

[0042] Figure 7 The second table element, drawn with "transparency", is shown according to... Figure 6a Desktop configuration components,

[0043] Figure 8 Shown in side view according to Figure 6a and Figure 6b Desktop configuration components,

[0044] Figure 9 Shown from top view according to Figure 8 The desktop configuration components, and

[0045] Figure 10 Showing equipped with according to Figures 1 to 9 The table configuration components are located in the aircraft cabin area. Detailed Implementation

[0046] exist Figures 1 to 9 The table configuration component 10 is shown in different operating states. For example, especially in… Figure 10 As can be seen, the table configuration assembly 10 is configured to be installed in a cabin area, particularly in the aircraft cabin area 100. The table configuration assembly 10 includes a mounting element 12 that can be fastened to a fastening structural element 102 installed in the aircraft cabin area 100. Figure 10 In the aircraft cabin area 100 shown, the fastening structural element 102 is configured as an aircraft galley, meaning that the mounting element 12 is fastened to the side wall of the aircraft galley. Alternatively, however, it is also possible that the mounting element 12 and the table configuration assembly 10 therefrom are fixed to the fastening structural element 102 as a partition wall, a lavatory module, a storage cabinet, or a similar large object. Adjacent to the table configuration assembly 10, the flight attendant seat 104 is fastened to the fastening structural element 102.

[0047] like Figure 2 and Figures 4 to 7 As best shown, mounting element 12 includes two sidewalls 14, 16 that extend substantially parallel to each other. Sidewalls 14, 16 are interconnected by a rear wall 18. To secure mounting element 12 to fastening structural element 102, the rear wall 18 of mounting element 12 is fixed to fastening structural element 102, for example, by screws, rivets, or similar fastening elements. Mounting element 12 thus defines a mounting plane E that extends substantially perpendicular to the sidewalls 14, 16 of mounting element 12. Conversely, the rear wall 18 of mounting element 12 extends within the mounting plane E.

[0048] Furthermore, the table configuration assembly 10 includes a first table element 20 connected to the mounting element 12. The first table element 20 is positioned relative to the mounting element 12 about a first pivot axis S1. Figures 1 to 3 The collapsible position shown is the same as Figures 5 to 9 The positions shown are pivotable. The first pivot axis S1 extends substantially parallel to the mounting plane E defined by the mounting element 10.

[0049] In its folded position, the first table element 20 is arranged substantially parallel to the mounting plane E defined by the mounting element 12. Conversely, in its used position, the first table element 20 extends substantially perpendicular to the mounting plane E defined by the mounting element 12.

[0050] The first table element 20 is formed such that its dimension in the direction of its central longitudinal axis L1 is larger than its dimension in the direction perpendicular to its central longitudinal axis L1. When the first table element 20 is arranged in its folded position, the central longitudinal axis L1 of the first table element extends substantially parallel to the mounting plane E defined by the mounting element 12. Conversely, when the first table element 20 is arranged in its used position, the central longitudinal axis L1 of the first table element 20 extends substantially perpendicular to the mounting plane E defined by the mounting element 12.

[0051] The table configuration assembly 10 also includes a second table element 22 connected to the first table element 20. Specifically, the second table element 22 is connected to the first table element 20 in the region of the end of the first table element 20 opposite to the first pivot axis S1. The rotation axis D is also arranged in the region of the end of the first table element 20 opposite to the first pivot axis S1. In the embodiment of the table configuration assembly 10 shown in the figures, the end of the first table element 20 opposite to the first pivot axis S1 and connected to the second table element 22 is rounded. The end of the second table element 22 connected to the first table element 20 is also rounded. Conversely, the free end of the second table element 22 has a straight edge.

[0052] The second table element 22 extends substantially parallel to the first table element 20 and is arranged such that the lower side 24 of the second table element 22 faces the tabletop 26 of the first table element 20. Similar to the first table element 20, the second table element 22 is also configured such that its dimension in the direction of its central longitudinal axis L2 is greater than its dimension in the direction perpendicular to its central longitudinal axis L2.

[0053] The second table element 22 is pivotable together with the first table element 20 about the first pivot axis S1. That is, when the first table element 20 is in its retracted position (in which the first table element 20 extends substantially parallel to the mounting plane E defined by the mounting element 12), the second table element 22 also extends substantially parallel to the mounting plane E. Thus, the central longitudinal axis L2 of the second table element 22 extends substantially parallel to the mounting plane E, just like the central longitudinal axis L1 of the first table element 20. Conversely, when the first table element 20 is in its used position (in which the first table element 20 extends substantially perpendicular to the mounting plane E defined by the mounting element 12), the second table element 22 also extends substantially perpendicular to the mounting plane E.

[0054] As from Figure 5 With Figure 6 to Figure 9As best shown in the comparison, the second table element 22 is rotatable relative to the first element 20 about a rotation axis D. The rotation axis D is arranged parallel to the mounting plane (E) in the usage positions of the table elements 20 and 22. The rotation axis intersects and is perpendicular to the two central longitudinal axes L1 and L2 at the intersection point. In particular, the second table element 22 can rotate relative to the first table element 20 about the rotation axis D. Figure 5 The overlapping positions shown in Figures 6 to 7 are as follows: Figure 9 Rotate between the indicated working positions.

[0055] Furthermore, at least when the first table element 20 is positioned in its folded position, the second table element 22 is movable relative to the first table element 20 in a direction parallel to the longitudinal axis L1 of the first table element 20 and the longitudinal axis L2 of the second table element 20. Specifically, the second table element 22 is connected to the first table element 20 such that when the first table element 20 is positioned in its folded position, the second table element is movable relative to the first table element 20 in a direction toward the first pivot axis S1, parallel to the longitudinal axis L1 of the first table element 20 and the longitudinal axis L2 of the second table element 22. Thus, the first table element 20, positioned in its folded position, extends upward from the mounting element 12 more than the second table element 22, see [reference needed]. Figure 2 and Figure 3 .

[0056] When the second table element 22 is arranged relative to the first table element 20 in its overlapping position, the first and second table elements 20, 22 are arranged in a position of maximum overlap with each other, that is, minimizing the area of ​​one table element protruding from the other. In the embodiment of the table configuration assembly 10 shown in the figures, the second table element 22 has a smaller area than the first table element 20. In particular, the second table element 22 has a shorter dimension in the direction of its central longitudinal axis L2 than the first table element 20 in the direction of its central longitudinal axis L1.

[0057] Furthermore, the second table element 22 is constructed identically to the first table element 20 in terms of its sections. That is, the second table element 22 is shaped such that when the second table element is arranged in its overlapping position relative to the first table element 20, the second table element completely overlaps with a section of the first table element 20. The sections of the first table element 20 that are identically constructed to the second table element 22 form the sections of the first table element 20 that are away from the first pivot axis S1, such that when the second table element 22 is arranged in its overlapping position relative to the first table element 20, only the section of the first table element 20 adjacent to the first pivot axis S1 is not covered by the second table element 22.

[0058] When the first table component 20 is in its folded position, the second table component 22 is always arranged in its overlapping position relative to the first table component 20 in order to minimize the positional requirements of the table configuration assembly 10. See [link to documentation]. Figures 1 to 3 Conversely, when the first table element 20 is in its usage position, the second table element 22 can remain in its... Figure 5 In the overlapping position shown, the central longitudinal axis L2 of the second table element 22 extends substantially parallel to the central longitudinal axis L1 of the first table element 20 and substantially perpendicular to the mounting plane E. However, the second table element 22 can also be rotated about the rotation axis D relative to the first table element 20 to its working position shown in Figures 6 to 9.

[0059] When the second table element 22 is in its working position, the central longitudinal axis L1 of the first table element 20 and the central longitudinal axis L2 of the second table element 22 form an angle of approximately 80 to 120°, especially approximately 90 to 110°. This creates a comfortable working space with two "table legs" for the person sitting in the crew seat 104.

[0060] In the embodiment of the table configuration assembly 10 shown in the accompanying drawings, the first table element 20 and the second table element 22 are sized such that the user of the table configuration assembly 10 can place three DIN-formatted A4 pages on the first table element 20 and the second table element 22. The tabletop 26 of the first table element 20 is specifically configured to be non-slip and adapted to accommodate two DIN-formatted A4 pages in landscape orientation, while the similarly non-slip tabletop 30 of the second table element 22 is adapted to accommodate one DIN-formatted A4 page in landscape orientation.

[0061] As best in Figure 6b As can be seen, the first table element 20 has a first edge protection profile 31a, which extends along the entire circumferential edge of the first table element 20 and thus forms a continuous boundary of the tabletop 26 of the first table element 20. Correspondingly, the second table element 22 has a second edge protection profile 31b, which extends along the entire circumferential edge of the second table element 22 and thus forms a continuous boundary of the tabletop 30 of the second table element 22. The edge protection profiles 31a and 31b are each made of a suitable plastic material and protect the edge areas of the table elements 20 and 22 from damage.

[0062] Furthermore, the first edge protection profile 31a protrudes beyond the tabletop 26 of the first table element 20 in a direction parallel to the rotation axis D, while the second edge protection profile 31b protrudes beyond the tabletop 30 of the second table element 22 in a direction parallel to the rotation axis D. The edge protection profiles 31a and 31b thus prevent spilled liquids from dripping unimpeded from the tabletops 26 and 30 of the table elements 20 and 22 and protect objects placed on the tabletops 26 and 30, such as paper, from slipping at least to some extent.

[0063] A feature is provided in the region of the rotation axis D. Figure 7 The friction generating element 28 shown is configured to minimize undesirable movement of the second table element 22 relative to the first table element 20 about the rotation axis D. When the table configuration assembly 10 is as described... Figure 10 This is especially important when the device is installed in the aircraft cabin and used in flight. In particular, the friction generating element 28 is arranged in the region of the rotation axis D between the first table element 20 and the second table element 22 and can be made of, for example, plastic material, elastomer material, etc.

[0064] Here, the friction generating element 28 is designed to generate a constant frictional force, set by screws or the like, during the installation of the table configuration assembly 10. However, the friction generating element 28 can also be designed such that the frictional force applied by it is variable and manually set. For example, a user of the table configuration assembly 10 can first rotate the second table element 22 from its overlapping position about the rotation axis D to its working position with the friction generating element 28 deactivated, and then activate the friction generating element 28 to hold the second table element 22 relative to the first table element 20 in its working position.

[0065] As best in Figure 1 , 3 As shown in Figure 4, a handle 32 is constructed on the first table element 20. Specifically, the handle 32 is arranged in the region of the end of the first table element 20 opposite to the first pivot axis S1 and is constructed in the form of a groove formed into the underside 34 of the first table element 20 opposite to the tabletop 26 of the first table element 20. When the first table element 20 pivots together with the second table element 22 between its stowed position and its used position, the user can grip the handle 32.

[0066] The table configuration assembly 10 also includes a support element 36, the first end of which is pivotally connected to the mounting element 12 about a second pivot axis S2. The second pivot axis S2 extends substantially parallel to the first pivot axis S1 and parallel to the mounting plane E defined by the mounting element 12. Figure 10As shown, when the table configuration assembly 10 is installed in the aircraft cabin area 100, the second pivot axis S2 is fixed to the mounting element 12 in the area of ​​the mounting element 12 near the ground.

[0067] Conversely, the second end of the support element 36 is pivotally connected to the first table element 20 about a third pivot axis S3. Specifically, the second end of the support element 36 is connected to the lower side 34 of the first table element 20, allowing the support element 36 to be positioned relative to the mounting element 12 and the first table element 20. Figure 1 and Figure 3 The rest position shown and Figures 5 to 9 The support element 36 pivots between the shown support positions. In its rest position, occupied by the first table element 20 when it is in its stowed position, the support element 36 is arranged substantially parallel to the first table element 20. Conversely, in its support position, occupied by the support element 36 when the first table element 20 is in its used position, the longitudinal axis L1 of the first table element 20 forms an angle of approximately 45° with the longitudinal axis L3 of the support element 36.

[0068] The support element 36 provides the first table element 20 with increased load-bearing capacity, making the first table element 20 more load-bearing than the second table element 22. In the embodiment shown here, the table configuration assembly 10 is typically capable of loading 5 kg.

[0069] The table configuration assembly 10 includes a locking mechanism 38 for locking the first table element 20 in its stowed position. The locking mechanism 38 includes two locking levers 40 and 42, which are rotatably mounted on the side walls 14 and 16 of the mounting element 12 about a rotation axis. When the locking levers 40 and 42 are in the locked position, they abut against opposing edge sections of the support element 36 arranged in its rest position, thereby holding the support element 36 in its rest position, see in particular... Figure 1 Specifically, the first table element 20 is also held in its retracted position. Conversely, when the locking levers 40 and 42 are in the released position, the locking levers release the support element 36 and thus the first table element 20, allowing the support element 36 to move into its supported position and the first table element 20 to move into its used position, as detailed in the following figure. Figures 3 to 5 .

[0070] As best from comparison Figures 3 to 5 As can be seen from the comparison, when the first table element 20 changes between its stowed position and its used position relative to the mounting element 12, the first pivot axis S1 is in Figure 3 The rest position shown and Figure 5The operating positions shown are movable. The movement of the first pivot axis S1 relative to the mounting element 12 is a translational movement of the first pivot axis S1 within the mounting plane E defined by the mounting element 12. Therefore, when the first table element 20 switches between its stowed position and its used position, the end of the first table element 20 facing the first pivot axis S1 performs not only a pivotal movement around the first pivot axis S1, but also a translational movement within the mounting plane E.

[0071] The translational movement of the first pivot axis S1 in the mounting plane E is guided by the guide device 44. The guide device 44 includes two substantially parallel guide rails, in which the ends of the first pivot axis S1 are movably accommodated. The guide device 44, i.e., the guide rails of the guide device 44, is fastened to the mounting element 12.

[0072] The table is equipped with 10 components, such as... Figure 10 When the table element 20 is mounted on the fastening structural element 102 in operation-ready position, the first pivot axis S1 moves upward relative to the mounting element 12 in the mounting plane E as the table element 20 is switched from its retracted position to its used position. Conversely, the first pivot axis S1 moves downward relative to the mounting element 12 in the mounting plane E as the table element 20 is switched from its used position to its retracted position.

[0073] Furthermore, the table configuration assembly 10 includes a locking mechanism 46 for securing the first table element 20 in its usage position. The locking mechanism 46 includes a first locking element 48 connected to the mounting element 12, see in particular... Figure 4 Furthermore, the locking mechanism 46 includes a second locking element (not visible in the figure) that is complementary to the first locking element 48 and connected to the first table element 20. The second locking element is disposed on the first table element 20 in the region of the end of the first table element 20 facing the first pivot axis S1.

[0074] Locking mechanism 46 is designed to allow the pressing force (by...) Figure 5 (The arrow in the diagram) Applying pressure to the tabletop 26 of the first table element 20, which is positioned in its use location, activates the locking mechanism. Specifically, the first and second locking elements 48 of the locking mechanism 46 are arranged and configured such that they automatically engage with each other whenever the user applies a corresponding pressing force to the tabletop 26 of the first table element 20, which is positioned in its use location. Figure 5 In the arrangement shown, the first table element 20 still overlaps with the second table element 20, and the pressing force for activating the locking mechanism 46 is transmitted through the tabletop 30 of the second table element 22 to the tabletop 26 of the first table element 20.

[0075] Furthermore, the locking mechanism 46 is designed to associate its activation with an audible sound. In particular, the first and second locking elements 48 of the locking mechanism 46 are designed such that a clicking sound can be heard when the two locking elements 48 engage with each other.

[0076] Finally, the table configuration assembly 10 includes a manually operable release mechanism 50 for releasing the locking mechanism 46. The release mechanism 50 is fastened to the mounting element and includes an operating button 52 connected via a connecting element 54 to a first locking element 48 of the locking mechanism 46. The operating button 52 is fastened to a retaining element 56 extending between the two sidewalls 14, 16 of the mounting element 12. When manual pressure is applied to the operating button 52, the pressure is transmitted via the connecting element 54 to the first locking element 48. This releases the first locking element 48 from the second locking element, allowing the first table element 20 to pivot from its used position to its stowed position.

Claims

1. A table configuration assembly (10) for an aircraft, the table configuration assembly comprising: - Mounting element (12), which can be fastened to the fastening structural element (102) and defines the mounting plane (E), - A first table element (20) connected to the mounting element (12), wherein the first table element (20) is pivotable relative to the mounting element (12) about a first pivot axis (S1) between a stowed position and a used position, wherein in the stowed position the longitudinal axis (L1) of the first table element (20) and its center extends substantially parallel to the mounting plane (E) defined by the mounting element (12), and in the used position the longitudinal axis (L1) of the first table element (20) and its center extends substantially perpendicular to the mounting plane (E) defined by the mounting element (12), and - A second table element (22) connected to the first table element (20), wherein the second table element (22) is arranged substantially parallel to the first table element (20) and is capable of rotating relative to the first table element (20) about a rotation axis (D) arranged parallel to the mounting plane (E) in the use position. The first pivot axis (S1) is movable relative to the mounting element (12) between a stationary position and an operating position when the first table element (20) switches between its stowed position and its used position. Its features are, The rotation axis (D) is arranged perpendicular to the mounting plane (E) in the retracted position, and At least when the first table element (20) is in its stowed position, the second table element (22) is able to move relative to the first table element (20) in the direction of the longitudinal axis (L1) parallel to the center of the first table element (20) and the longitudinal axis (L2) of the second table element (22).

2. The table configuration assembly (10) according to claim 1, wherein, The second table element (22) is connected to the first table element (20) in the region of the end of the first table element (20) away from the first pivot axis (S1), and / or a friction generating element (28) is provided in the region of the rotation axis (D), the friction generating element being configured to minimize undesirable movement of the second table element (22) relative to the first table element (20) about the rotation axis (D).

3. Table configuration assembly (10) according to claim 1 or 2, wherein The second table element (22) is rotatable relative to the first table element (20) about a rotation axis (D) between an overlapping position and a working position, in which the first table element and the second table element (22) are arranged in a position of maximum overlap with each other, and in the working position, the longitudinal axis (L1) of the first table element (20) and the longitudinal axis (L2) of the second table element (22) form an angle of 80 to 120°.

4. The table configuration assembly (10) according to claim 3, wherein In the working position, the longitudinal axis (L1) of the first table element (20) forms an angle of 90 to 110° with the longitudinal axis (L2) of the second table element (22).

5. The table configuration component (10) according to claim 1 or 2, wherein: - The second table element (22) has a smaller area than the first table element (20), and / or - the second table element (22) is constructed congruently to one section of the first table element (20), and / or - the first table element (20) is provided with a first edge protection profile (31a) which extends along at least one section of the circumferential edge of the first table element (20) and / or protrudes in a direction parallel to the axis of rotation (D) beyond the tabletop (26) of the first table element (20); and / or - the second table element (22) is provided with a second edge protection profile (31b) which extends along at least one section of the circumferential edge of the second table element (22) and / or protrudes in a direction parallel to the axis of rotation (D) beyond the tabletop (30) of the second table element (22); and / or - the tabletop (26) of the first table element (20) is constructed to be slip-resistant; and / or - the tabletop (30) of the second table element (22) is constructed to be slip-resistant.

6. The table configuration assembly (10) according to claim 1 or 2, wherein - the second table element (22) is arranged relative to the first table element (20) such that the underside (24) of the second table element (22) faces the tabletop (26) of the first table element (20), and / or the first table element (20) and the second table element (22) are dimensioned such that a user of the table arrangement assembly (10) is able to place three DIN A4 pages on the first table element (20) and the second table element (22), and / or the first table element (20) is shaped such that the dimension of the first table element in the direction of the longitudinal axis (LI) of the first table element is greater than the dimension of the first table element in a direction perpendicular to the longitudinal axis (LI) of the first table element, and / or the second table element (22) is shaped such that the dimension of the second table element in the direction of the longitudinal axis (L2) of the second table element is greater than the dimension of the second table element in a direction perpendicular to the longitudinal axis (L2) of the second table element, and / or a handle (32) is constructed on the first table element (20).

7. The table arrangement assembly (10) according to claim 1 or 2, further comprising a guide device (44) for guiding the movement of the first pivot axis (SI) between a rest position of the first pivot axis and an operating position of the first pivot axis.

8. The table configuration assembly (10) according to claim 1 or 2, wherein, The mounting element (12) comprises two side walls (14, 16) which extend substantially perpendicularly to the mounting plane (E) defined by the mounting element (12) and / or substantially parallel to one another, and / or the mounting element (12) comprises a rear wall (18) which extends substantially in the mounting plane (E) defined by the mounting element (12).

9. The table arrangement assembly (10) according to claim 1 or 2, further comprising a locking mechanism (46) for locking the first table element (20) in a use position of the first table element.

10. The table configuration assembly (10) according to claim 9, wherein, The locking mechanism (46) is designed such that it can be activated by applying a pressing force to the tabletop (26) of the first table element (20) arranged in the use position of the first table element, and / or the locking mechanism (46) is designed such that the activation of the locking mechanism is associated with an audible sound.

11. The table configuration assembly (10) according to claim 9, wherein, The table configuration assembly further comprises a manually operable release mechanism (50) for releasing the locking mechanism (46).

12. The table configuration assembly (10) according to claim 1 or 2, wherein, The table configuration assembly further comprises a support element (36) whose first end portion is pivotably connected with the mounting element (12) about a second pivot axis (S2) and whose second end portion is pivotably connected with the first table element (20) about a third pivot axis (S3) such that the support element (36) can be pivoted relative to the mounting element (12) and the first table element (20) between a rest position in which the support element (36) is arranged essentially parallel to the first table element (20) and a support position in which the longitudinal axis (L1) of the first table element (20) forms an angle of 30 to 60° with the longitudinal axis (L3) of the support element (36).

13. The table configuration assembly (10) according to claim 12, wherein, In the support position the longitudinal axis (L1) of the first table element (20) forms an angle of 40 to 50° with the longitudinal axis (L3) of the support element (36).

14. The table configuration assembly (10) according to claim 13, wherein, In the support position the longitudinal axis (L1) of the first table element (20) forms an angle of 45° with the longitudinal axis (L3) of the support element (36).

15. The table configuration assembly (10) according to claim 1 or 2, wherein, The table configuration assembly further comprises a locking mechanism (38) for locking the first table element (20) in the stowed position of the first table element.

16. A passenger cabin area (100) comprising: - a fastening structure element (102), and - a table configuration assembly (10) according to any one of claims 1 to 15, wherein the mounting element (12) of the table configuration assembly (10) is fastened on the fastening structure element (102).

17. The cabin region (100) according to claim 16, wherein Adjacent to the table configuration assembly (10) on the fastening structure element (102) a crew seat (104) is fastened.

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