Method of producing a high-energy hydroformed structure from a 2XXX-series alloy

Patent metadata

Field	Value
Publication number	US-12152292-B2
Application number	US-202017599661-A
Country	US
Kind code	B2
Filing date	Mar 23, 2020
Priority date	Apr 3, 2019
Publication date	Nov 26, 2024
Grant date	Nov 26, 2024

Abstract

A method of producing an integrated monolithic aluminum structure, comprising: providing an aluminum alloy plate with a thickness of at least 38.1 mm, wherein the plate is a 2xxx-series alloy in a T3-temper and has a composition comprising, in wt. %: Cu 3.8-4.5, Mn 0.3-0.8, Mg 1.1-1.6, Si up to 0.15, Fe up to 0.20, Cr up to 0.10, Zn up to 0.25, Ti up to 0.15, Ag up to 0.10, balance aluminum; optionally pre-machining the plate to an intermediate machined structure; high-energy hydroforming the plate or intermediate structure against a rigid die forming surface having a desired curvature contour of the integrated monolithic aluminum structure, causing the plate or the intermediate structure to conform to the forming surface contour; machining or mechanical milling the high-energy formed structure to a near-final or final machined integrated monolithic aluminum structure; ageing the final integrated monolithic aluminum structure to a desired temper.

First claim

The invention claimed is:

1. A method of producing an integrated monolithic aluminum structure, the method comprising the steps of:
providing an aluminum alloy plate with a predetermined thickness of at least 31.75 mm, wherein the aluminum alloy plate is a 2xxx-series alloy provided in a T3-temper, and wherein the 2xxx-series alloy has a composition comprising, in wt. %: Cu 3.8% to 4.5%, Mn 0.3% to 0.8%, Mg 0.9% to 1.6%, Si up to 0.15%, Fe up to 0.20%, Cr up to 0.10%, Zn up to 0.25%, Ti up to 0.15%, Ag up to 0.10%, impurities and balance aluminum;
optionally pre-machining of the aluminum alloy plate to an intermediate machined structure;
high-energy hydroforming of the plate or optional intermediate machined structure against a forming surface of a rigid die having a contour in accordance with a desired curvature of the integrated monolithic aluminum structure, the high-energy forming causing the plate or the intermediate machined structure to conform to the contour of the forming surface to at least one of a uniaxial curvature and a biaxial curvature as a high-energy formed structure;
machining or mechanical milling of the high-energy formed structure to a near-final or final machined integrated monolithic aluminum structure; and
ageing of the final integrated monolithic aluminum structure to a desired temper.

2. The method according to claim 1 , wherein the high-energy hydroforming step is by explosive forming.

3. The method according to claim 1 , wherein the high-energy hydroforming step is by electrohydraulic forming.

4. The method according to claim 1 , wherein following the high-energy forming operation, in that order, the high-energy formed structure is machined to a final machined integrated monolithic aluminum structure and then aged to a desired temper.

5. The method according to claim 1 , wherein the high-energy hydroforming operation, in that order, the high-energy formed structure is aged to a desired temper and then machined to a final machined integrated monolithic aluminum structure.

6. The method according to claim 1 , wherein following the high-energy hydroforming operation, the high-energy formed structure is stress-relieved, preferably by compressive forming, followed by machining and ageing to a desired temper of the integrated monolithic aluminum structure.

7. The method according to claim 1 , wherein following high-energy hydroforming operation, the high-energy formed structure is stress-relieved, followed by machining and ageing to a desired temper of the integrated monolithic aluminum structure.

8. The method according to claim 7 , wherein the high-energy formed structure is stress-relieved by compressive forming in a next high-energy hydroforming step.

9. The method according to claim 1 , wherein the predetermined thickness of the aluminum alloy plate is at least 50.8 mm.

10. The method according to claim 1 , wherein the predetermined thickness of the aluminum alloy plate is at least 63.5 mm.

11. The method according to claim 1 , wherein the predetermined thickness of the aluminum alloy plate is at most 127 mm.

12. The method according to claim 11 , wherein the predetermined thickness of the aluminum alloy plate is at most 114.3 mm.

13. The method according to claim 1 , wherein the ageing of the integrated monolithic aluminum structure is to a desired temper selected from the group of: T3, T4, T6, and T8.

14. The method according to claim 1 , wherein the ageing of the integrated monolithic aluminum structure is to a T8 temper.

15. The method according to claim 14 , wherein the ageing of the integrated monolithic aluminum structure is to a T852, T87 or T89 temper.

16. The method according to claim 1 , wherein the 2xxx-series aluminum alloy has a Cu-content of 3.8% to 4.3%.

17. The method according to claim 16 , wherein the 2xxx-series aluminum alloy has a CU-content of 3.8% to 4.1%.

18. The method according to claim 1 , wherein the pre-machining and final machining comprises numerically-controlled machining.

Assignees

• Airbus Sas

Inventors

• BüRGER ACHIM
• Bach Andreas Harald
• Spangel Sabine Maria
• Meyer Philippe

Classifications

• C22F1/057

  of alloys with copper as the next major constituent · CPC title

• C22C21/16

  with magnesium · CPC title

• C22C21/14

  with silicon · CPC title

• C21D9/46

  for sheet metals · CPC title

• B21D53/92

  other parts for aircraft · CPC title