ARRANGEMENT IN A VEHICLE CABIN WITH CABIN MONUMENTS PLACEABLE IN ROWS WITH LAMINAR CONTACT OF THE LATERAL SURFACES THEREOF

Abstract

An arrangement in a cabin of a vehicle has a plurality of cabin monuments, placeable in rows, of which the lateral surfaces are in laminar contact, said cabin monuments having a front side and a rear side and a wall surface of the aircraft fuselage, at least sections of which face toward the cabin of the vehicle and are not aligned parallel with a lengthwise axis of the cabin. The cabin monuments are arranged in rows parallel to the lengthwise axis of the cabin, so that the front sides and the rear sides are each aligned parallel to the lengthwise axis of the cabin. The rear sides of at least two cabin monuments, each of which include storage space for cabin trolleys, are positioned with an offset relative to each other in a direction transverse to the lengthwise axis of the cabin.

Claims

1. An arrangement in a cabin of a vehicle, the arrangement comprising: a plurality of cabin monuments that are placeable in rows and are in laminar contact with each other via the lateral surfaces thereof, each of which having a front side and a rear side; and a surface of a fuselage wall of the vehicle, at least portions of which extend in a non-parallel manner to a lengthwise axis of the cabin and face the cabin; wherein the cabin monuments are arranged in rows parallel to the lengthwise axis of the cabin, so that the front sides and rear sides extend parallel to the lengthwise axis of the cabin; and wherein the rear sides and/or the front sides of at least two cabin monuments, each of which has at least one storage space for cabin trolleys, have an offset in a direction extending transversely to the lengthwise axis of the cabin.

2. The arrangement of claim 1, wherein the cabin monuments have the same construction depth, and at least portions of the rear sides are arranged flush against the surface of the fuselage wall facing toward the cabin.

3. The arrangement of claim 2, wherein at least two front sides are offset relative to each other in a direction extending transversely to the lengthwise axis of the cabin.

4. The arrangement of claim 1, wherein at least two cabin monuments have different construction depths, and the rear sides at least portions of the cabin monuments are arranged flush against the surface of the fuselage wall facing toward the cabin, and wherein the front sides of the cabin monuments extend in a common plane.

5. The arrangement of claim 1, wherein the fuselage wall extends at an angle to the lengthwise axis of the cabin.

6. The arrangement of claim 1, wherein the surface of the fuselage wall includes reinforcing elements, which protrude into the cabin.

7. The arrangement of claim 1, wherein die construction depths of the cabin monuments are graduated in a stepped pattern, graduated in a grid pattern, which is formed by available sizes of transportable cabin trolleys.

8. A vehicle including a cabin with at least one arrangement comprising: a plurality of cabin monuments that are placeable in rows and are in laminar contact with each other via the lateral surfaces thereof, each of which having a front side and a rear side; and a surface of a fuselage wall of the vehicle, at least portions of which extend in a non-parallel manner to a lengthwise axis of the cabin and face the cabin, wherein the cabin monuments are arranged in rows parallel to the lengthwise axis of the cabin, so that the front sides and rear sides extend parallel to the lengthwise axis of the cabin, and wherein the rear sides and/or the front sides of at least two cabin monuments, each of which has at least one storage space for cabin trolleys, have an offset in a direction extending transversely to the lengthwise axis of the cabin.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

[0020] Further features, advantages and application options of the disclosed subject matter will be evident from the following description of embodiments and the figures. Identical or similar objects are also designated by the same reference signs in all of the figures.

[0021] FIGS. 1 to 4 each show diagrammatic representations of an arrangement in plan view.

DETAILED DESCRIPTION

[0022] The following detailed description is merely illustrative in nature and is not intended to limit the embodiments of the subject matter or the application and uses of such embodiments. As used herein, the word “exemplary” means “serving as an example, instance, or illustration.” Any implementation described herein as exemplary is not necessarily to be construed as preferred or advantageous over other implementations. Furthermore, there is no intention to be bound by any expressed or implied theory presented in the preceding technical field, background, brief summary or the following detailed description.

[0023] FIG. 1 shows a first embodiment of an arrangement 2 in an aircraft cabin 4, more precisely in a rear area, in which a pressure bulkhead 6 is positioned to seal a pressurized fuselage. In this area, a fuselage wall 8 is arranged and extends at an angle to a lengthwise axis of the cabin 10. In a lengthwise direction x defined thereby, the distance between fuselage wall 8 and the lengthwise axis of the cabin 10 thus increases continually until a purely cylindrical area of the fuselage is reached, at which point the distance remains constant. However, discontinuities can exist over the length of fuselage wall 8, caused by reinforcing elements and the like.

[0024] Arrangement 2 includes a plurality of cabin monuments 12, 14, 16, 18 and 20, which are arranged in rows in 1 in lengthwise direction x, so that the lateral surfaces thereof touch each other. Arrangement 2 is also replicated symmetrically, meaning that such an arrangement 2 can be found on both sides of the lengthwise axis of cabin 10.

[0025] Each cabin monument 12 to 20 has a front side 12a, 14a, 16a, 18a and 20a as well as a rear side 12b, 14b, 16b, 18b and 20b facing toward fuselage wall 8. As hinted in FIG. 1, rear sides 20b are arranged as closely as possible to fuselage wall 8. In this way, for example, enough storage spaces are created in cabin monument 12 to accommodate two full-size cabin trolleys 22, while in cabin monuments 14 and 16 two storage spaces for full-size cabin trolleys 22 and two storage spaces for half-size cabin trolleys 24 are provided. Cabin monument 18 may include storage spaces for two full-size cabin trolleys 22, cabin monument 20 may have a storage space for one half-size cabin trolley 24. The groups of cabin monuments 12, 14 and 16, 18 and 20 are used with graduated construction depths, which is adapted to an installation space that is dictated by the fuselage wall 8 in order to maintain an even, flat front of arrangement 2.

[0026] FIG. 2 shows a modified arrangement 26 with cabin monuments 28, 30 and 32, which are arranged side by side in lengthwise direction x. One special feature consists in the cabin monuments 28 and 30 have the same construction depth, while cabin monument 32 is offset in the y-direction, i.e., transversely to the lengthwise direction x. A work surface 34 facing away from fuselage wall 8 forms a continuous transition from cabin monument 30 to cabin monument 32. In this arrangement 26, a gap 36 may form between rear sides 28b and 30b and the fuselage wall 8, and this might be obscured by a covering (not shown) or filled with smaller, lockable storage compartments. FIG. 2 also shows a configuration in which only the front sides 30a, 32a of the cabin monuments 30, 32 are offset with respect to each other and the rear sides 30b, 32c of the cabin monuments 30, 32 are not offset to each other. This configuration is shown by the dashed line in FIG. 2. In other words, it is possible that only front sides 28a, 30a, 32a of the cabin monuments 28, 30, 32 comprise offsets with respect to each other whereas rear sides 28b, 30b, 32b are aligned with each other. This configuration provides advantages concerning force introduction and transmission. However, in case of an alignment of the rear sides 28b, 30b, 32b of the monuments 28, 30, 32, there is still enough space for system connections.

[0027] A further refinement of this design is shown in FIG. 3 with the arrangement 38 illustrated there. In this case, three cabin monuments 40, 42 and 44 of the same type are offset in the y-direction with respect to each other and are positioned at the smallest possible distance from fuselage wall 8. Thus, two transition areas 46 and 48 are created so that the differences in width can be managed as smoothly as possible.

[0028] Finally, FIG. 4 shows an arrangement 50 in an essentially cylindrical area of a fuselage wall 52, with a plurality of cabin monuments 54, 56, 58 and 60 arranged in rows, that is to say consecutively in the x-direction, and which have alternating depths. The depth can vary, as indicated by the dashed lines, in order to increase space available for electric equipment/wiring. The widths of the cabin monuments are selected so they are correlated with a frame distance 62 in such a way that deeper cabin monuments 56 and 60 extend as reinforcing components 64 produced in the form of a framework and intended to stiffen the fuselage, whereas a little lower down cabin monuments 54 and 58 are set apart from the framework.

[0029] It should be noted in addition that the term “include” does not exclude other elements or steps, and “one” does not preclude a plurality. It should further be noted that features which have been described with reference to one of the aforementioned embodiments can also be used in combination with other features of other embodiments that have also been described in the preceding text. Reference signs in the claims are not to be construed as a limitation thereof.

[0030] While at least one exemplary embodiment has been presented in the foregoing detailed description, it should be appreciated that a vast number of variations exist. It should also be appreciated that the exemplary embodiment or embodiments described herein are not intended to limit the scope, applicability, or configuration of the claimed subject matter in any way. Rather, the foregoing detailed description will provide those skilled in the art with a convenient road map for implementing the described embodiment or embodiments. It should be understood that various changes can be made in the function and arrangement of elements without departing from the scope defined by the claims, which includes known equivalents and foreseeable equivalents at the time of filing this patent application.