Superplastic forming and diffusion bonding process

Patent metadata

Field	Value
Publication number	US-10850317-B2
Application number	US-201816634927-A
Country	US
Kind code	B2
Filing date	Aug 10, 2018
Priority date	Aug 22, 2017
Publication date	Dec 1, 2020
Grant date	Dec 1, 2020

Abstract

A process and apparatus for forming a structure comprising: a) forming a pack from a skin sheet and a core sheet, wherein venting grooves are formed in a surface of a sheet that is adjacent to the other sheet; b) placing the pack in a mould and heating the pack; c) injecting a first gas between the core and skin sheets to urge the skin sheet against the mould; d) injecting a second gas on the side of the core sheet remote from the skin sheet to urge the core sheet against the skin sheet; e) maintaining gas pressure of the second gas thereby diffusion bonding the sheets; and f) withdrawing some or all of the first gas from the cavity.

First claim

The invention claimed is:

1. A process of forming a structure by diffusion bonding and superplastic forming at least one skin sheet and at least one core sheet, the process comprising:
a) forming a pack from the at least one skin sheet and the at least one core sheet, wherein the pack comprises a first surface of the core sheet positioned adjacent to a second surface of the skin sheet, and wherein one or more venting grooves are formed in at least one surface selected from the group of surfaces consisting of the first surface of the core sheet and the second surface of the skin sheet;
b) placing the pack in a mould and heating the pack to a temperature at which the sheets are capable of superplastic deformation;
c) injecting a first gas between the first surface of the core sheet and the second surface of the skin sheet to urge the skin sheet against an internal face of the mould thereby forming a cavity between the first surface of core sheet and the second surface of the skin sheet;
d) injecting a second gas on the side of the core sheet remote from the skin sheet to urge the core sheet against the skin sheet;
e) maintaining gas pressure of the second gas on the side of the core sheet remote from the skin sheet, thereby forming a diffusion bond between the skin sheet and the core sheet; and
f) withdrawing some or all of the first gas from the cavity between the first surface of core sheet and the second surface of the skin sheet during at least part of step d).

2. The process according to claim 1 , wherein the one or more venting grooves are formed in the second surface of the skin sheet and not in the first surface of the core sheet.

3. The process according to claim 1 , wherein the one or more venting grooves define one or more meandering paths across the surface or surfaces in which the one or more venting grooves are formed.

4. The process according to claim 1 , wherein the one or more venting grooves are formed by machining the surface or surfaces in which the one or more venting grooves are formed.

5. The process according to claim 1 , wherein the one or more venting grooves define a plurality of interconnected loops.

6. The process according to claim 5 , wherein the loops are circles or ellipses.

7. The process according to claim 5 , wherein the process further comprises locating a mechanical fastener through the formed structure at a position that is within a loop defined by the venting grooves.

8. The process according to claim 1 , wherein the one or more venting grooves are located in at least a flange portion of the structure.

9. The process according to claim 1 , wherein the process further comprises injecting a third gas on the side of the skin sheet remote from the core sheet, between the skin sheet and the mould, thereby to force together the skin sheet and the core sheet.

10. The process according to claim 1 , wherein the first gas is the same type of gas as the second gas.

11. The process according to claim 1 , wherein the gases are noble gases.

12. The process according to claim 1 , wherein at least two core sheets are used that have been joined together in selected areas and the second gas injected in step d) is injected between the at least two core sheets.

13. The process according to claim 1 , wherein:
two skin sheets are used;
the pack in step a) is formed by sandwiching one or more core sheets between the skin sheets;
the first gas is injected in step c) between each skin sheet and its adjacent core sheet; and,
in step f), the first gas is withdrawn from the cavity between each skin sheet and its adjacent core sheet.

Assignees

• Bae Systems Plc

Inventors

• Greenhalgh Robert William
• Price Howard James

Classifications

• F05D2230/236

  Diffusion bonding · CPC title

• B21D53/78

  propeller blades; turbine blades · CPC title

• B21D26/055 Primary

  Blanks having super-plastic properties · CPC title

• B21D47/00 Primary

  Making rigid structural elements or units, e.g. honeycomb structures · CPC title

• B23K2103/10

  Aluminium or alloys thereof · CPC title