Method of manufacturing an article by diffusion bonding

• US 5,284,288 A
• Filed: 06/30/1993
• Issued: 02/08/1994
• Est. Priority Date: 08/15/1992
• Status: Expired due to Term

• Current Assignee: Rolls-Royce PLC (Rolls-Royce Holdings Plc)
• Original Assignee: Rolls-Royce PLC (Rolls-Royce Holdings Plc)
• Inventors: Woodward, James
• Primary Examiner(s): Ramsey, Kenneth J.
• Application Number:
  US08/083,484
• Time in Patent Office: 223 Days
• Field of Search: 228/157, 228/193, 228/221, 228/186
• US Class Current: 228/157
• CPC Class Codes: B23K 20/023 Thermo-compression bonding
• CPC Class Codes: F28F 3/14 by separating portions of a pair of joined sheets to form channels, e.g. by inflation manufacture thereof B23P

Abstract

A plurality of titanium sheets are assembled into a stack. One of the sheets is provided with a stop off material on one surface to prevent diffusion bonding at predetermined positions. The edges of the sheets are welded together and a pipe is welded to the stack to interconnect with the stop off material to form a sealed assembly. The sealed assembly is evacuated. The sealed assembly is heated to evaporate the binder from the stop off and the binder is extracted from the assembly. The pipe is then sealed by two spaced welds. The assembly is heated and externally pressurized to diffusion bond the sheets together. The region of the pipe between the assembly and the first seal and the region of the pipe between both seals collapse to indicate a successful diffusion bond, or one or both regions are uncollapsed to indicate an unsuccessful diffusion bond. An integral structure formed by a successful diffusion bond is then superplastically formed to produce an article.

Claims

1. A method of manufacturing an article by diffusion bonding at least two metal workpieces comprising the steps of

(a) assembling the at least two workpieces into a stack relative to each other so that the surfaces are in mating abutment,

(b) sealing the edges of the at least two workpieces together, except where a pipe is to be inserted, and joining a pipe to the stack to provide a sealed assembly,

(c) sequentially evacuating the interior of the sealed assembly and supplying inert gas to the interior of the sealed assembly through the pipe to remove oxygen from the interior of the sealed assembly,

(d) evacuating the interior of the sealed assembly,

(e) sealing the pipe with a first seal, and sealing the pipe with a second seal which is spaced from the first seal,

(f) applying sufficient heat and pressure across the thickness of the at least two workpieces to diffusion bond the at least two workpieces together to form an integral structure and to collapse the pipe at a first region between the joint between the pipe and the stack and the first seal and to collapse the pipe at a second region between the first seal and the second seal,

(g) observing the first and second regions of the pipe to determine whether a successful diffusion bond has been formed between the workpieces in the stack to form an integral structure.

2. A method as claimed in claim 1 wherein before the workpieces are stacked together, applying a stop off material to preselected areas of at least one of the surfaces of at least one of the at least two metal workpieces to prevent diffusion bonding at the preselected areas, before the pipe is sealed placing the sealed assembly in an oven while the sealed assembly is continuously evacuated, heating the sealed assembly while it is within the oven to evaporate volatile binder from the stop off material while the sealed assembly is continuously evacuated to remove the volatile binder from between the at least two metal workpieces of the sealed assembly, after the integral structure is formed heating and internally pressurising the integral structure to cause some of the preselected areas of at least one of the workpieces to be superplastically formed to produce an article of predetermined shape.

3. A method as claimed in claim 2 comprising heating the stack to a temperature between 250°

C. and 350°

C. to evaporate the volatile binder from the stop off material.

4. A method as claimed in claim 2 wherein, where the workpieces are made of titanium alloy, heating the integral structure to a temperature equal to or greater than 850°

C. to superplastically form the integral structure.

5. A method as claimed in claim 4 comprising heating the integral structure to a temperature between 900°

C. and 950°

C.

6. A method as claimed in claim 1 comprising welding the edges of the workpieces together.

7. A method as claimed in claim 1 wherein before the pipe is sealed, cooling the sealed assembly whilst the sealed assembly is continuously evacuated.

8. A method as claimed in claim 7 comprising cooling the sealed assembly to ambient temperature.

9. A method as claimed in claim 1 comprising welding the pipe to form the first and second seals in the pipe.

10. A method as claimed in claim 9 comprising resistance welding the pipe to form the first and second seals in the pipe.

11. A method as claimed in claim 10 comprising spot welding the pipe to form the first and second seals in the pipe.

12. A method as claimed in claim 1 wherein, where the workpieces are made of a titanium alloy, heating the workpieces to a temperature equal to or greater than 850°

C. and applying pressure equal to or greater than 20×

10⁵ Nm^-2 to diffusion bond the workpieces together to form an integral structure.

13. A method as claimed in claim 12 comprising heating the workpieces to a temperature between 900°

C. and 950°

C. and the pressure applied is between 20×

10⁵ Nm^-2 and 30×

10⁵ Nm^-2.

14. A method as claimed in claim 1 in which the step of sequentially evacuating the interior of the sealed assembly and supplying inert gas to the interior of the sealed assembly through the pipe to remove oxygen from the interior of the sealed assembly is performed a plurality of times.