Seat rail for supporting seats in an aircraft and a method of manufacturing a seat rail

Patent metadata

Field	Value
Publication number	US-10035600-B2
Application number	US-201514938532-A
Country	US
Kind code	B2
Filing date	Nov 11, 2015
Priority date	Nov 11, 2014
Publication date	Jul 31, 2018
Grant date	Jul 31, 2018

Abstract

A seat rail for supporting seats in an aircraft comprises a support portion for connection with the cabin floor and a seat receiving portion having a groove for receiving the end portions of connector elements coupled with the support frame of a seat. The support portion comprises a profile arrangement of a fiber-reinforced polymer, preferably carbon fiber-reinforced polymer, having a central main portion and flanges which extend outwardly from and perpendicular with respect so the main portion to form a support surface for the seat rail. The main portion comprises a slot open at least at its end remote from the flanges. At least one metal element comprising the groove for receiving the end portions of the connector elements has a leg which is inserted into the slot of the main portion and is secured therein. The seat rail may be manufactured in a continuous process.

First claim

The invention claimed is:

1. A method of manufacturing a seat rail for supporting seats in an aircraft, the method comprising:
pre-forming a profile arrangement of fiber material and a polymer to obtain a support portion comprising a central main portion and flanges which extend outwardly from and perpendicular with respect to the central main portion to form a support surface for the seat rail, wherein the central main portion comprises a slot at least open at its end remote from the flanges;
providing the seat rail comprising the support portion for connection with a cabin floor and a seat receiving portion comprising a groove for receiving end portions of connector elements coupled with a seat support frame;
inserting at least one metal element, which comprises the groove for receiving the end portions of connector elements, into the slot prior to curing of the profile arrangement; and
pressing material of the central main portion into engagement with the at least one metal element during curing of the profile arrangement.

2. The method according to claim 1 , wherein the at least one metal element comprises lateral flanges for engagement with the profile arrangement adjacent to the slot and a leg projecting perpendicular with respect to the lateral flanges which leg is inserted into the slot of the profile arrangement.

3. The method according to claim 1 , wherein to obtain a fixed connection of the at least one metal element with the profile arrangement, ribs or recesses are provided in an area of the at least one metal element which engages with the central main portion.

4. The method according to claim 1 , wherein the profile arrangement is formed of two profile rails with a space between them forming the slot.

5. The method according to claim 4 , wherein the profile rails are each U-shaped in cross-section, wherein the profile rails are formed such that the slot is arranged between their bases.

6. The method according to claim 4 , wherein the profile rails are L-shaped in cross-section.

7. The method according to claim 1 , wherein during pre-forming of the profile arrangement the at least one metal element is inserted.

8. The method according to claim 1 , wherein a plurality of metal elements is inserted into the slot to form a continuous track.

9. The method according to claim 1 , comprising a post-curing step of cutting the seat rail to length.

Assignees

• Airbus Operations Gmbh

Inventors

• Vichniakov Alexei
• Gillessen Alexander

Classifications

• Y02T50/46

  Cross-Sectional Technologies · mapped topic

• B64C1/20

  specially adapted for freight · CPC title

• B64D11/0696 Primary

  Means for fastening seats to floors, e.g. to floor rails · CPC title

• Y02T50/40

  Weight reduction · CPC title