Patent Application
20160200417
This application claims priority to EP 15 150 721.7 filed Jan. 12, 2015, the entire disclosure of which is incorporated by reference herein.
The present disclosure pertains to a floor arrangement for a passenger cabin of an aircraft or spacecraft.
Although applicable to any kind of aircraft or spacecraft or the like, the present disclosure and the problem on which it is based will be explained in greater detail with reference to floor arrangements of commercial aircraft.
On commercial aircraft, mounting rails made from metal or composite materials are installed in the floors of passenger cabins for fastening of cabin outfitting components, like for example seats, galleys, or lavatories. One widely used type of mounting rail is formed with a profile in the shape of an “I”, as it is for example disclosed in document DE 102009039581 A1. This type of mounting rail features horizontal upper and lower flanges that are connected by a vertical web element. On the top of the mounting rail, a crown with a C-like profile is arranged which comprises an opening that points upwards into the passenger cabin between two inward-projecting limbs that comprise holes and slits in alternating succession. Here, the crown forms a slide intended for fixing the cabin outfitting components.
In addition to fixing passenger seats and the like, mounting rails are usually configured to mount and stabilize floor panels that form the floor of the passenger cabin. Hereby, two adjacent mounting rails together support a row of floor panels that are arranged in between the mounting rails one after the other alongside the length of the rails. Typically, each floor panel rests with its side edges on the upper flanges of the mounting rails in such a configuration that floor panels and rail crowns form a flat surface.
Floor panels are usually made of a composite sandwich honeycomb-like structure with a thickness in the order of up to a few centimeters. The floor panels rest on the upper flanges of the mounting rails and are furthermore fixed to the upper flanges by bolts or the like. Due to assembly requirements, a small gap usually remains in between the floor panels and the seat rail crowns. In order to mitigate corrosion phenomena and the like due to liquids entering the gaps, often a sealing is placed into the gaps. For example, a closed-cell foam profile can be glued to the bottom of the floor panel and its lateral surfaces, which is then compressed during installation and thereby becomes impermeable to water and other liquids.
It is an idea of the disclosure herein is to provide a floor for a passenger cabin that is simple to install and deinstall or uninstall.
A first aspect of the disclosure pertains to a floor arrangement for a passenger cabin of an aircraft or spacecraft. The floor arrangement comprises mounting rails for mounting cabin outfitting components, wherein each mounting rail comprises at least one upper support flange for supporting floor panels. The floor arrangement further comprises curved floor panels being inherently formed with a convex top surface and a concave bottom surface, wherein each curved floor panel is mounted to two respective adjacent mounting rails. Here, each curved floor panel is supported by one respective upper support flange of each of the two adjacent mounting rails.
One of the ideas of the present disclosure is to provide an inherently curved floor panel to avoid having to bend a flat floor panel in the installation process of a floor arrangement. The curved floor panel can be directly mounted in between two adjacent mounting rails without any additional efforts, as for example load applications. Hence, the floor arrangement according to the present disclosure is easy to install. The floor panel can then be fastened to the mounting rails in the usual way, e.g. by bolting it to the flanges of the mounting rails from beneath the floor, which then automatically flattens the floor panels. Any remaining curvature of the floor panels is reduced by any cabin component put on top of the floor arrangement. Consequently, also the deinstallation or removal of such floor panels is simple. After having removed the fastening bolts during deinstallation, the floor panel according to the present disclosure by itself resumes its original inherent curved shape and thus automatically bends upwards for easy removal. Hence, damages that might be inflicted on the floor panel by external tools during installation or deinstallation are avoided.
According to an embodiment of the disclosure herein, each curved floor panel is formed with two straight side edges, each of which rests on one respective upper support flange of the two respective adjacent mounting rails. In this embodiment, the curved floor panel has a very convenient shape for facilitating quick and straightforward installation and deinstallation. The curved floor panel simply has to be placed with its side edges on top of the upper flanges of two adjacent mounting rails. Next, it can be fixed by bolts or the like.
According to another embodiment of the disclosure herein, the convex top surface of the curved floor panel or the concave bottom surface or both of them are curved according to a section of a circumferential surface of a circular cylinder. In particular in combination with two straight side edges, the curved floor panels thus has a very simple shape that can be easily installed and produced in various production processes.
According to yet another embodiment of the disclosure herein, each curved floor panel is flattened through fastening of the curved floor panel under tension to the two respective adjacent mounting rails.
According to yet another embodiment of the disclosure herein, each flattened curved floor panel has a vertical rise in between its side edges of less than 10 millimeters. The curvature of the floor panel is thus only very small and hence will not be noticeable in any relevant way after cabin installation, i.e. after the floor panels have been bolted to the flanges and cabin outfitting components have been put on top of the floor arrangement.
The curved floor panels may be formed as a composite lay-up structure. Within the usual production steps of composite lay-up structures, a curved floor panel can be easily ensured by pre-defining a bending through asymmetrical choice of upper and lower layers of the composite structure. For example, the widths, thicknesses and strengths of the individual layers can be chosen so as to achieve a pre-defined deflection of the layers with respect to a flat layer. Usually, common practice teaches to construct composite layers as symmetrical as possible with respect to each other in order to avoid any bending or asymmetries in the final structure. In this embodiment of the disclosure herein, the layers are deliberately chosen in an asymmetric way with respect to each other during production in order to achieve a pre-defined bending of the floor panel.
The curved floor panels may further be formed from fiber-reinforced plastic. Fiber-reinforced plastic has many advantages compared to other materials, like for example metal. It is lightweight and can be produced in a relatively cost-efficient way. Complicated stiffened composite structures can be produced without much effort.
The curved floor panels may yet further be preformed into a curved configuration and hardened in an autoclave process. Like this, for example, a floor panel made from a fiber-reinforced plastic can be brought into a curved configuration already “on the assembly line”. The curved configuration is then made permanent in the subsequent autoclave process.
The curved floor panels may be formed with a honeycomb structure between the top surface and the bottom surface. A honeycomb-like structured floor panel has many advantages, like for example a larger stiffness with high break resistance and a high elasticity modulus as well as better sound absorption characteristics than commonly structured floor panels.
According to another embodiment of the disclosure herein, a sealing is located between the upper support flanges of the mounting rails and the curved floor panels. The purpose of the sealing is to close any remaining space in between the curved floor panel and the flanges of the mounting rails. For example, otherwise fluids or moisture could enter any remaining openings and induce long-term corrosion damage to the rails or the floor panels.
The sealing may be formed as a foam profile that has an open-cell or closed-cell structure. Using a foam sealing has the advantage that the foam is compressible during installation of the floor panel. On the one hand, the foam protects both the flanges and the floor panels from any direct damage due to bumping or rattling against each other. On the other hand, the compressed foam functions as an impermeable barrier for any fluid that might enter the space in between the flanges and the floor panels. In addition to these benefits, this solution grants a good relative movement during flight, taking temperature and load deformations into account.
The sealing may be adhesively fixed to the curved floor panels. Thus, for example a foam profile may be glued to the side edges and the bottom surface of a floor panel before installation. The foam is then compressed during installation in order to ensure tightness.
According to another embodiment of the disclosure herein, fasteners fix the curved floor panels to the upper support flanges of the mounting rails. The fasteners may be formed as bolts, screws, rivets, pins or plugs or the like. As soon as the curved floor panels have been mounted in between the mounting rails any relative movement between floor panel and mounting rails is prohibited by the fasteners. In addition, the fastener arrangement may be chosen in such a way that the tension forces applied by the fasteners flatten the floor panels into a flat or nearly flat shape. Hence, the final floor arrangement might retrain only a very slight bending or no curvature at all, so that further cabin installation or passenger convenience is not affected by the inherently curved floor panels.
The disclosure herein will be explained in greater detail with reference to exemplary embodiments depicted in the drawings as appended.
The accompanying drawings are included to provide a further understanding of the present disclosure and are incorporated in and constitute a part of this specification. The drawings illustrate the embodiments of the present disclosure and together with the description serve to explain the principles of the disclosure herein. Other embodiments of the present disclosure and many of the intended advantages of the present disclosure will be readily appreciated as they become better understood by reference to the following detailed description. The elements of the drawings are not necessarily to scale relative to each other. In the figures, like reference numerals denote like or functionally like components, unless indicated otherwise.
Although specific embodiments are illustrated and described herein, it will be appreciated by those of ordinary skill in the art that a variety of alternate and/or equivalent implementations may be substituted for the specific embodiments shown and described without departing from the scope of the present disclosure. Generally, this application is intended to cover any adaptations or variations of the specific embodiments discussed herein.
In the figures, reference sign 1 denotes a floor arrangement for a passenger cabin of an aircraft. The floor arrangement 1 comprises two adjacent mounting rails 2, e.g. for mounting seats to the aircraft floor. Furthermore the floor arrangement 1 comprises a plurality of curved floor panels 4, one of which is shown in the figures. The mounting rails may be made from titanium or cheaper aluminum alloys.
In between top surface 5 and bottom surface 6, a honeycomb structure 8 is formed. The floor panel 4 is formed from fiber-reinforced plastic in a composite lay-up structure, e.g. carbon fiber-reinforced polymer. The curvature is achieved by performing the floor panel 4 into a curved configuration in the assembly and hardening the configuration in a subsequent autoclave process. An alternative way of producing such a curved floor panel 4 would be to deliberately choose the individual layers in an asymmetric way with respect to the layer width, thickness and/or strength. In the present embodiment however, the layers themselves can be inherently symmetric to each other. The bending is achieved by applying a load to the floor panel 4 in the assembly before the autoclave.
Sealings 9 are glued to the straight left and right side edges 7 as well as the bottom surface 6 of the floor panel 4. Each sealing 9 is formed from a closed-cell foam profile. The foam can be made in a flexible, semi-rigid way for example from plastics like extruded Polyethylene, Polypropylene or similar lightweight and cost-effective thermoplastic or other materials with high strength and good shock/vibration absorption properties.
The installation of this kind of curved floor panel 4 is thus possible without having to apply any bending loads to the floor panel 4 and hence is much simpler and failsafe. In addition, also the deinstallation is straightforward. As soon as the fasteners 10 have been removed, the floor panel 4 by itself gets back into its original inherent curved shape with a shortened width. Hence, it can be easily removed from the rails 2 without any additional tooling effort and without risk of damage. This saves maintenance costs and time.
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.
| Number | Date | Country | Kind |
|---|---|---|---|
| 15 150 721.7 | Jan 2015 | EP | regional |
