Metal fusion bonding – Process – With shaping
Patent
1994-05-12
1995-07-11
Heinrich, Samuel M.
Metal fusion bonding
Process
With shaping
228190, B21D 2602, B23K 2000
Patent
active
054313279
DESCRIPTION:
BRIEF SUMMARY
BACKGROUND OF THE INVENTION
1. Field of the Invention
This invention is concerned with superplastic forming and in particular with an improved method of superplastic forming sandwich structures from a plurality of aluminum alloy sheets.
2. Discussion of Prior Art
The formation of sheet metal into useful configurations is usually achieved by forces applied to the material by hard tooling, such as in press forming. By contrast, in superplastic forming processes, the required deformation of the workpiece is accomplished by application of gas pressure. A die cavity delimits expansion of the workpiece, but intimate contact between the die and the deforming sheet does not occur until the desired configuration has been achieved in the vicinity of the contact zone.
Many aluminum alloys have the potential to undergo superplastic forming and consequently there is a desire amongst aerospace manufacturers to produce aluminum alloy structures using combined diffusion bonding/superplastic forming processes (DB/SPF) similar to those currently used for titanium components.
However, the propensity of titanium alloys to undergo diffusion bonding is superior to that of the majority of structural aluminum alloys and in many cases strengths of titanium diffusion bonds are comparable to that of the bulk metal. By contrast, the bond interface in joints between aluminum alloys may be much weaker than the parent material. This is especially true at the elevated temperatures required for superplastic forming. As a result of this, when a stress is applied normal to the diffusion bond, the joint is susceptible to peeling under a relatively low peel force.
Low peel strength precludes or limits the use of diffusion bonds in multiple sheet structures with the result that manufacturers are actively seeking alternatives to superplastic forming of aluminum structures lest peel fracture should occur before stresses in the sheet assembly reach the levels required to effect superplastic deformation.
In our earlier patent application GB 2 241 914 A we disclose a method for diffusion bonding aluminum-lithium alloys which gives rise to materials having improved properties compared with previously-known methods. The resultant materials are capable of withstanding high shear stresses, but they have insufficient peel strengths to undergo superplastic forming except in the case of very thin sheet sections of 1 mm thickness or less.
This is in marked contrast to the high peel strengths observed in diffusion bonded titanium alloy joints and it is therefore an object of the present invention to effect an increase in the peel resistance of diffusion bonded aluminum alloys to the extent that such materials are rendered suitable for processing by superplastic forming.
SUMMARY OF THE INVENTION
The invention is a method of superplastically forming a sandwich structure from a plurality of aluminum alloy sheets, the method comprising: said stack comprising a pair of outer sheets and at least one core sheet; pattern to create a workpiece having internal cavities; sheets, and the workpiece, to the diffusion bonding step in the zones where diffusion bonding is to be carried out, said reinforcing material thereby serving to prevent the tensile stresses exerted during subsequent superplastic forming from causing peel fracture of the diffusion bonds such that superplastic strain occurs selectively in those regions of the workpiece between the diffusion bonded zones.
The reinforcing material may take the form of separate pieces such as strips or patches which are bonded in a predetermined pattern on the parent sheets from which the workpiece is to be formed. Conveniently, these separate pieces are diffusion bonded to the parent sheets in the same diffusion bonding operation which joins the sheets together.
Alternatively, the reinforcing material may be integrally formed with the parent sheet material. This is achieved by machining or chemically milling thicker sheets in selected regions to create a predetermined pattern of stepped areas, the raised portions of w
REFERENCES:
patent: 2983993 (1961-05-01), Johnson
patent: 4043498 (1977-08-01), Conn, Jr.
patent: 4304821 (1981-12-01), Hayase et al.
patent: 4351470 (1982-09-01), Swadling et al.
patent: 4530197 (1985-07-01), Rainville
patent: 4632296 (1986-12-01), Mansbridge et al.
Dunford David V.
Partridge Peter G.
Heinrich Samuel M.
The Secretary of State for Defence in Her Brittanic Majesty's Go
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