Rail for the fastening of equipment elements in aircraft, in particular seats, and method for production

Patent metadata

Field	Value
Publication number	US-12377953-B2
Application number	US-202318296644-A
Country	US
Kind code	B2
Filing date	Apr 6, 2023
Priority date	Apr 8, 2019
Publication date	Aug 5, 2025
Grant date	Aug 5, 2025

Abstract

A rail for the fastening of equipment elements, such as, in particular, seats, in aircraft, includes a holding region for connection to an equipment element of an aircraft, and a support region to fasten the rail to a carrier element of the aircraft. The rail has a metallic shell which is, for example, made of titanium and which is filled with a fiber-reinforced thermoplastic filler material which is reinforced by short fibers. To produce the rail, a metallic molded part is used as a casting mold and is filled, for example by injection, with the filler material and, after the rail has been produced, forms the metallic shell for the filler material.

First claim

The invention claimed is:

1. A method for producing a rail for fastening equipment elements in an aircraft, comprising the steps:
molding a rail part, being for the fastening of equipment elements of the aircraft, from metal with a holding region and a support region for fastening to a carrier element of the aircraft,
filling the holding region of the rail part with a filler material and,
wherein, after the rail part has been produced, the rail part forms a metallic shell for the filler material,
wherein the metallic shell defines a cavity having a first end separated from a second end by an intermediate portion, the first end having a cross-sectional area greater than a cross-sectional area of the of the intermediate portion taken parallel to the cross-sectional area of the first end,
wherein the filler material is located within the first end of the cavity and the intermediate portion of the cavity.

2. The method as claimed in claim 1 , wherein the filler material used comprises at least one of:
a plastic;
a polymer; or
a thermoplastic.

3. The method as claimed in claim 1 , further including a step of adding fibers to the filler material for reinforcing purposes, said fibers comprising at least one of:
short fibers;
carbon fibers.

4. The method as claimed in claim 1 , wherein the metallic shell comprises at least one of:
titanium,
aluminum, or
a metal alloy.

5. The method as claimed in claim 1 , wherein the rail is produced by means of injection molding, the metallic shell being used as a casting mold and being filled with the filler material, in order to, together with the filler material after hardening thereof, form the rail.

6. The method as claimed in claim 1 , wherein the metallic shell is filled with the filler material by thermoplastic injection, and comprises at least one of:
short fibers added to the filler material;
the injection being carried out at both end regions of the molded rail part;
the injection being carried out as a thermal injection; or
the rail being produced for the fastening of equipment elements in the aircraft comprising the holding region for connection to the equipment element of the aircraft, and the support region to fasten the rail to the carrier element of the aircraft, wherein the rail comprises the metallic shell which is filled with the filler material.

Assignees

• Airbus Operations Gmbh

Inventors

• Tiryaki Memis
• Eilken Wolfgang
• Werner Sven Hardy
• Zybala André

Classifications

• B32B15/14

  next to a fibrous or filamentary layer · CPC title

• B32B2605/18

  Aircraft · CPC title

• B32B2311/18

  Titanium · CPC title

• B32B15/20

  comprising aluminium or copper {(B32B15/016 and B32B15/017 take precedence)} · CPC title

• B29C2045/0008

  the fibres being oriented randomly · CPC title