Method of mitigating wrinkles during the manufacture of super-plastically formed parts

Patent metadata

Field	Value
Publication number	US-2025249496-A1
Application number	US-202418430471-A
Country	US
Kind code	A1
Filing date	Feb 1, 2024
Priority date	Feb 1, 2024
Publication date	Aug 7, 2025
Grant date	—

Abstract

A method including arranging a plurality of flat sheets into a part assembly, consisting of a first outer sheet and a second outer sheet. A friction-modifying layer is applied to the first outer sheet, where the first outer sheet has a first portion and a second portion. The friction-modifying layer is applied at a first thickness in the first portion and a second thickness in the second portion. The first thickness and the second thickness are different thicknesses. The method also includes placing the part assembly on a lower die of a die system with the first outer sheet facing the lower die. The method further includes moving an upper die of the die system in a forming direction toward the lower die to stretch and compress the part assembly between the upper die and the lower die and to super-plastically form the part assembly into the formed part.

First claim

What is claimed is:

1 . A method of mitigating wrinkles during a manufacture of a super-plastically formed part, the method comprising:
arranging a plurality of flat sheets into a part assembly, the plurality of flat sheets comprising a first outer sheet and a second outer sheet; applying a friction-modifying layer to the first outer sheet of the part assembly, wherein:
the first outer sheet comprises a first portion having a first percentage of coverage and a second portion having a second percentage of coverage;
the friction-modifying layer is applied at a first thickness in the first portion and a second thickness in the second portion; and
the first thickness and the second thickness are different thicknesses;
placing the part assembly on a lower die of a die system such that the first outer sheet is facing the lower die; and moving an upper die of the die system in a forming direction toward the lower die to stretch and compress the part assembly between the upper die and the lower die and to super-plastically form the part assembly into a formed part.

2 . The method of claim 1 , further comprising simulating a super-plastic formation of a simulated part assembly into a simulated formed part to predict at least one wrinkle-prone location within the simulated formed part.

3 . The method of claim 2 , wherein:
the first portion of the first outer sheet corresponds with the at least one wrinkle-prone location within the simulated formed part; the second portion of the first outer sheet corresponds with locations other than the at least one wrinkle-prone location within the simulated formed part; and the step of applying the friction-modifying layer to the first outer sheet comprises applying the friction-modifying layer to the first portion at the first thickness to mitigate wrinkles at the at least one wrinkle-prone location while super plastically forming the part assembly into the formed part.

4 . The method of claim 1 , wherein the step of applying the friction-modifying layer to the first outer sheet comprises applying the friction-modifying layer to the first outer sheet using a mask comprising at least one aperture corresponding with the first portion.

5 . The method of claim 4 , wherein a location of the at least one aperture of the mask, a shape of the at least one aperture, and a size of the at least one aperture are predetermined based on a simulation of a super-plastic formation of a simulated formed part.

6 . The method of claim 1 , further comprising:
forming a corner cutout at each corner of the part assembly to define a plurality of flanges, wherein each one of the plurality of flanges extends between adjacent ones of the corner cutouts; and the step of moving the upper die of the die system in the forming direction comprises trapping each one of the plurality of flanges between die-blocks, coupled to the upper die, and the lower die, as the upper die of the die system is moved in the forming direction toward the lower die.

7 . The method of claim 1 , further comprising, prior to applying the friction-modifying layer, increasing a surface irregularity in an irregular portion of the first outer sheet of the part assembly.

8 . The method of claim 1 , wherein the friction-modifying layer is configured to precisely control a state of stress within the part assembly when super-plastically forming the part assembly into the formed part.

9 . The method of claim 1 , wherein:
the first outer sheet further comprises a third portion having a third percentage of coverage; the friction-modifying layer is applied at a third thickness in the third portion; and the third thickness is different than the first thickness and the second thickness.

10 . The method of claim 1 , wherein the first thickness is less than the second thickness.

11 . The method of claim 1 , wherein the plurality of flat sheets further comprises at least one inner sheet disposed between the first outer sheet and the second outer sheet.

12 . A method of mitigating wrinkles during a manufacture of a super-plastically formed part, the method comprising:
subjecting a part assembly to a super-plastic forming process; and controlling a state of stress within the part assembly during the super-plastic forming process by non-uniformly applying a friction-modifying layer to an outer sheet of the part assembly prior to the super-plastic forming process, such that a thickness of the friction-modifying layer at least one wrinkle-prone location of the outer sheet is different than a thickness of the friction-modifying layer at other locations of the outer sheet.

13 . The method of claim 12 , wherein the thickness of the friction-modifying layer at the at least one wrinkle-prone location is less than the thickness of the friction-modifying layer at other locations of the outer sheet.

14 . The method of claim 12 , further comprising simulating a super-plastic formation of a simulated part assembly into a simulated formed part to predict the at least one wrinkle-prone location within the simulated formed part.

15 . A formed part produced by a process comprising:
arranging a plurality of flat sheets into a part assembly, the plurality of flat sheets comprising a first outer sheet and a second outer sheet; applying a friction-modifying layer to the first outer sheet of the part assembly, wherein:
the first outer sheet comprises a first portion having a first percentage of coverage and a second portion having a second percentage of coverage;
the friction-modifying layer is applied at a first thickness in the first portion and a second thickness in the second portion; and
the first thickness and the second thickness are different thicknesses;
placing the part assembly on a lower die of a die system such that the first outer sheet is facing the lower die; and moving an upper die of the die system in a forming direction toward the lower die to stretch and compress the part assembly between the upper die and the lower die and to super-plastically form the part assembly into the formed part.

16 . The formed part of claim 15 , wherein the part assembly further comprises at least one inner sheet disposed between the first outer sheet and the second outer sheet.

17 . The formed part of claim 16 , wherein the at least one inner sheet is formed into a network of cells between the first outer sheet and the second outer sheet when the part assembly is super-plastically formed into the formed part.

18 . The formed part of claim 15 , wherein at least one of the plurality of flat sheets comprises at least one of a size, a shape, or a thickness that is different from the size, the shape, or the thickness of others of the plurality of flat sheets.

19 . The formed part of claim 15 , further comprising:
forming a corner cutout at each corner of the part assembly to define a plurality of flanges, wherein each one of the plurality of flanges extends between adjacent ones of the corner cutouts; and the step of moving the upper die of the die system in the forming direction comprises trapping each one of the plurality of flanges between die-blocks, coupled to the upper die, and the lower die, as the upper die of the die system is moved in the forming direction toward the lower die.

20 . The formed part of claim 15 , wherein each one of the plurality of flat sheets comprises a titanium material.

Assignees

• Boeing Co

Inventors

• Henson Landon
• Spurgers Jacob
• Jenny Craig

Classifications

• F05D2240/14

  Casings or housings protecting or supporting assemblies within · CPC title

• B21D53/92 Primary

  other parts for aircraft · CPC title

• G06F30/20

  Design optimisation, verification or simulation (optimisation, verification or simulation of circuit designs G06F30/30) · CPC title

• B21D22/022

  by heating the blank or stamping associated with heat treatment (C21D takes precedence) · CPC title

• B32B2311/18

  Titanium · CPC title