Fastening System For Passenger Seats In A Cabin Of A Vehicle
20190308736 ยท 2019-10-10
Assignee
Inventors
Cpc classification
B64D11/0639
PERFORMING OPERATIONS; TRANSPORTING
International classification
Abstract
A fastening system for passenger seats in a vehicle cabin has two or more guide rails to be integrated into or onto a cabin floor, and a plurality of slides, to be brought into engagement with the guide rails and having a flange for connection to a passenger seat to retain the passenger seat on a guide rail. Each guide rail has a profile cross section, perpendicularly to a main axis of extent (x), having a base region, a supporting region and an undercut situated therebetween. Each slide has a cavity, of complementary design with the profile cross section, and a necked region, to be brought into engagement with the undercut, thus enabling the supporting region to be enclosed by the cavity of the slide. Each slide has a rotatably mounted roller projecting into the necked region and can be brought into surface contact with a guide rail surface.
Claims
1. A fastening system for passenger seats in a cabin of a vehicle, comprising: two or more guide rails configured to be integrated into or onto a floor of the cabin; and a plurality of slides configured to be brought into engagement with the guide rails and having a flange for connection to a passenger seat in order to retain the relevant passenger seat on a guide rail, wherein each guide rail has a profile cross section, perpendicularly to a main axis of extent, each guide rail having a base region, a supporting region and at least one undercut situated therebetween, wherein each slide has a cavity of a complementary design with the profile cross section of the guide rail, and a necked region configured to be brought into engagement with the undercut, thus enabling the supporting region to be enclosed by the cavity of the slide, and wherein each slide has at least one rotatably mounted roller projecting into the necked region and configured to be brought into surface contact with a surface of the guide rail.
2. The fastening system according to claim 1, further comprising a flat cover element fixed on the supporting region.
3. The fastening system according to claim 1, wherein the at least one undercut comprises two mutually opposite undercuts.
4. The fastening system according to claim 1, wherein the slide has two mutually spaced rollers for each undercut, the two mutually spaced rollers each configured to be brought into surface contact with the surface of the guide rail.
5. The fastening system according to claim 4, wherein the at least one undercut comprises two mutually opposite undercuts, and wherein the slide has at least one pair of mutually opposite rollers for engagement in two mutually opposite regions of the profile cross section.
6. The fastening system according to claim 4, wherein all the rollers are arranged in a common plane and are mounted so as to be rotatable about a respective axis perpendicular to the common plane.
7. The fastening system according to claim 1, wherein at least one slide has a movably mounted retaining body configured to be moved into the cavity and out of the cavity, and wherein the guide rail has latching openings configured to be brought into engagement with the retaining body when the slide is in engagement with the guide rail.
8. The fastening system according to claim 7, wherein the retaining body is a sprung pin urged by a spring force into a neutral position, in which the retaining body is in the cavity.
9. The fastening system according to claim 8, wherein the retaining body is arranged in a guide and ends flush with an outer surface of the guide when the retaining body is in the neutral position.
10. The fastening system according to claim 1, wherein the roller has a circumferential groove matched to a contour of the surface of the guide rail.
11. The fastening system according to claim 1, wherein the slide has at least one projection projecting into the necked region and forming a clearance fit with the undercut.
12. A passenger seat system for a cabin of a vehicle, comprising: at least one passenger seat device having a seat frame, and a fastening system according to claim 1, wherein the fastening system has two mutually spaced guide rails extending parallel to one another, wherein the seat frame of the at least one passenger seat device has two pairs of mutually spaced seat legs, which are each connected to one slide, and wherein the slides are in engagement with the guide rails.
13. The passenger seat system according to claim 12, wherein the guide rails are configured to be fastened on seat rails arranged in a floor of a cabin of the vehicle.
14. A vehicle having a cabin, a floor and at least one passenger seat system according to claim 12.
15. The vehicle according to claim 14, wherein the vehicle is an aircraft.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
[0029] Further features, advantages and possible uses of the present invention will be found in the following description of the embodiment examples and the figures. Here, all the features described and/or depicted, in themselves and in any desired combination, form the subject matter of the invention, even when considered independently of their combination in the individual claims or the dependency references thereof. In the figures, the same reference signs furthermore stand for identical or similar objects.
[0030]
[0031]
[0032]
[0033]
[0034]
DETAILED DESCRIPTION
[0035]
[0036] By way of example, the flange 6 has a ring shape and is attached rigidly on one side to the slide 2. Of course, the flange 6 can also be attached to the slide 2 on both sides. This can depend, in particular, on the type and embodiment of the seat foot to be fastened, and neither of the two versions is excluded. An opening 10 of the flange 6 extends in a transverse direction y and is complemented by recesses 12 on the upper side 4. The recesses 12 are shaped and positioned in such a way that an elongate element, e.g. a cylindrical element, could rest in both recesses 12 and, at the same time, extends through the opening 10 in the flange 6. This ensures that a connecting means extending through the flange can be reached by means of a suitable tool. Of course, other versions are also conceivable, and this illustration should be understood only as one possible example.
[0037] Behind the flange 6 in the x direction there is a guide 14, which receives a retaining body 16. This body can be moved along a z direction, which is perpendicular to a plane defined by the x axis and the y axis. The retaining body 16 can be moved into and out of the cavity 8. In the position shown, the retaining body 16 is in a neutral position and ends approximately flush with an outer surface 18 of the guide 14. Also visible on the surface 4 are four axles 20, which are provided for mounting rollers, which can be seen in subsequent figures.
[0038]
[0039]
[0040]
[0041] Based on the above illustrations,
[0042] To illustrate the relative positions of the projections 24 and of receiving spaces 44 for the rollers 22,
[0043] Meanwhile, the attachment of a passenger seat to a slide 2 is illustrated in
[0044] In the illustration shown, the guide rail 34 is furthermore covered by a flat cover element 50 in order to prevent damage and contamination. By way of example, the cover element 50 can be implemented in the form of a strip-shaped carpet section, which can correspond to the surrounding carpet 52 on both sides of the guide rail 34. Embodiment of the cavity 8 to implement a mechanically simple and low-cost cover 50 of this kind is readily possible by allowing a sufficient vertical clearance with respect to the guide rail.
[0045] The same illustration is shown in
[0046]
[0047] As shown in the partially transparent illustration in
[0048] To release the retention, there can be an actuating mechanism 62, which is illustrated as a linear motion element in
[0049] As is shown in a partially transparent illustration in
[0050]
[0051] The aircraft 70 has a cabin 72, which is equipped with a plurality of such guide rails 34, which extend parallel to the longitudinal axis X of the aircraft 70. By means of such a construction, it is possible to enable seat spacings to be changed between individual flights and, at the same time, to enable cabin crew to carry out this themselves. Neither expensive tools nor great force are required to move the relevant passenger seats 68 along the longitudinal axis x.
[0052] For the sake of completeness, it should be noted that having does not exclude any other elements or steps and a or an does not exclude a multiplicity. It should furthermore be noted that features which have been described with reference to one of the above embodiment examples can also be used in combination with other features of other embodiment examples described above. Reference signs in the claims should not be regarded as restrictive.
[0053] While at least one exemplary embodiment of the present invention(s) is disclosed herein, it should be understood that modifications, substitutions and alternatives may be apparent to one of ordinary skill in the art and can be made without departing from the scope of this disclosure. This disclosure is intended to cover any adaptations or variations of the exemplary embodiment(s). In addition, in this disclosure, the terms comprise or comprising do not exclude other elements or steps, the terms a or one do not exclude a plural number, and the term or means either or both. Furthermore, characteristics or steps which have been described may also be used in combination with other characteristics or steps and in any order unless the disclosure or context suggests otherwise. This disclosure hereby incorporates by reference the complete disclosure of any patent or application from which it claims benefit or priority.