Method for producing a crossmember for a vehicle and a crossmember for a vehicle

Patent metadata

Field	Value
Publication number	US-11623729-B2
Application number	US-201916424315-A
Country	US
Kind code	B2
Filing date	May 28, 2019
Priority date	Jun 29, 2018
Publication date	Apr 11, 2023
Grant date	Apr 11, 2023

Abstract

A method for producing a crossmember for a vehicle prepares a workpiece having different thicknesses and a preliminary contour from a metal sheet of uniform thickness by flat roll forming to achieve different local thicknesses. The method cuts out the workpiece, and bending roll forms the workpiece to form a crossmember with a cross section having at least two flanges opposite one another, and a web situated between said flanges. The distance between the flanges is not constant along a longitudinal extent of the crossmember, and a thickness profile at least of the web is determined by the flat roll forming. The local thicknesses and the preliminary contour are such that a geometrical shape of the crossmember corresponds to a predetermined geometrical shape with different thicknesses and heights of the web and differently shaped regions of the flanges along the longitudinal extent of the crossmember.

First claim

What is claimed is:

1. A method for producing a crossmember for a vehicle, comprising the steps of: preparing a workpiece having different thicknesses and a preliminary contour from a metal sheet of uniform thickness by flat roll forming to achieve different local thicknesses and cutting out the workpiece; bending roll forming the workpiece to form a crossmember with a cross section which has at least two flanges arranged opposite one another and a web situated between said flanges, wherein the distance between the flanges arranged opposite one another is not constant along a longitudinal extent of the crossmember, and a thickness profile at least of the web is determined by the step of flat roll forming, wherein said at least two flanges each lie in a plane that is not parallel with a plane containing the web, and wherein said at least two flanges each extend away from the web in the same direction wherein the local thicknesses and the preliminary contour are such that that a geometrical shape of the crossmember after the bending roll forming corresponds to a predetermined geometrical shape with different thicknesses and heights of the web and differently shaped regions of the flanges along the longitudinal extent of the crossmember a middle region of the crossmember comprises a C-shaped profile and respective ends of the crossmember comprise a U-shaped profile, and, installing the crossmember in an aircraft, wherein the crossmember forms a supporting structure for a floor of the aircraft.

2. The method according to claim 1 , wherein the flat roll forming is carried out such that the thickness of the workpiece is greatest in a central region of the crossmember.

3. The method according to claim 1 , wherein the flat roll forming is carried out such that a transitional region is arranged between two regions of different sheet-metal thickness, in which region the thickness decreases continuously and which continuously adjoins the two adjacent regions.

4. The method according to claim 1 , wherein two first sections are provided, which are arranged spaced apart off-center on the crossmember.

5. The method according to claim 4 , wherein the flat roll forming is carried out such that the sheet-metal thickness is less in the region of the two first sections than in adjacent regions.

6. The method according to claim 1 , wherein the bending roll forming is carried out in such a way that, in at least one first section, the distance between the flanges arranged opposite one another falls below the distance in the remaining part of the crossmember.

7. The method according to claim 6 , wherein the flat roll forming is carried out such that the sheet-metal thickness is less in the region of the at least one first section than in adjacent regions.

8. The method according to claim 6 , wherein:
during the bending roll forming, at least one first flange and at least one second flange are produced;
the at least one first flange has a continuously flat supporting surface along the longitudinal extent of the crossmember; and
the at least one second flange is spaced apart by different amounts from the at least one first flange along the longitudinal extent of the crossmember.

9. The method according to claim 8 , wherein the preliminary contour is configured to provide a concave arch of the at least one second flange in the direction of the at least one first flange in at least one section of the crossmember.

Assignees

• Airbus Operations Gmbh

Inventors

• Noebel Torsten
• Eilken Wolfgang
• Schulze Wolfgang
• Tiryaki Memis

Classifications

• B21D5/083 Primary

  for obtaining profiles with changing cross-sectional configuration · CPC title

• B21D47/01

  beams or pillars · CPC title

• B21D35/00

  Combined processes according to {or processes combined with} methods covered by groups B21D1/00 - B21D31/00 (B21D21/00 takes precedence) · CPC title

• B64F5/10

  Manufacturing or assembling aircraft, e.g. jigs therefor · CPC title

• B21D53/88

  other parts for vehicles, e.g. cowlings, mudguards · CPC title