Method of manufacturing an article, a method of diffusion bonding and a vacuum chamber

• US 5,226,578 A
• Filed: 08/27/1992
• Issued: 07/13/1993
• Est. Priority Date: 10/29/1991
• Status: Expired due to Fees

• Current Assignee: Rolls-Royce PLC (Rolls-Royce Holdings Plc)
• Original Assignee: Rolls-Royce PLC (Rolls-Royce Holdings Plc)
• Inventors: Douglas, Joseph
• Primary Examiner(s): Heinrich, Samuel M.
• Application Number:
  US07/935,250
• Time in Patent Office: 320 Days
• Field of Search: 228/118, 228/157, 228/193, 228/214, 228/242
• US Class Current: 228/157
• CPC Class Codes: B21D 26/055 Blanks having super-plastic properties
• CPC Class Codes: B23K 20/14 Preventing or minimising gas access, or using protective gases or vacuum during welding formed by material interposed between workpieces B23K20/18
• CPC Class Codes: B23K 20/18 Zonal welding by interposing weld-preventing substances between zones not to be welded

Abstract

A stack of titanium sheets are placed between a pair of pressurisable chambers in a vacuum chamber. One of the mating surfaces of each pair of mating surfaces has had a stop off material applied in a desired pattern to prevent diffusion bonding. A pump evacuates the vacuum chamber and heaters heat the stack to evaporate volatile binders from the stop off. When all the binder has been removed the stack is heated and the pressure in the pressurisable chambers is increased to cause a pair of resilient members to apply pressure on the stack to diffusion bond the sheets together. The volatile binder is removed quickly and oxidation of the titanium is prevented during baking out of the binder. The integral structure is then heated and internally pressurised to superplastically form one of the sheets to produce an article of predetermined shape. No welding of the sheets before bonding is required.

Claims

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

(a) applying a stop off material to prevent diffusion bonding to preselected areas of at least one of the surfaces of at least one of the at least two metal workpieces,

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

(c) placing the stack in pressing means positioned within a vacuum chamber,

(d) evacuating the vacuum chamber,

(e) minimising the pressure applied across the thickness of the at least two workpieces, by the pressing means, to allow the flow of volatile binders and gases from between the at least two workpieces into the vacuum chamber,

(f) heating the stack while it is within the vacuum chamber to evaporate volatile binder from the stop off material, while continuously evacuating the vacuum chamber to remove the volatile binder from between the at least two workpieces and the vacuum chamber,

(g) applying heat and increasing the pressure applied across the thickness of the at least two workpieces, by the pressing means, to diffusion bond the at least two workpieces together in areas other than the preselected areas to form an integral structure,

(h) removing the integral structure from the vacuum chamber,

(i) heating the integral structure and internally pressurising it to cause the preselected areas of at least one of the workpieces to be superplastically formed to produce an article of pre-determined shape.

2. A method of manufacturing an article as claimed in claim 1 wherein the stack is placed between a first selective pressing means and a second selective pressing means in the vacuum chamber, the pressure applied across the thickness of the at least two workpieces is minimised by minimising the pressure applied by the first and second selective pressing means, the pressure applied across the thickness of the at least two workpieces is increased by increasing the pressure applied by the first and second selective pressing means.

3. A method of manufacturing an article as claimed in claim 2 wherein the first selective pressing means is a first selectively pressurisable chamber and the second selective pressing means is a second selectively pressurisable chamber.

4. A method of manufacturing an article as claimed in claim 1 wherein the stack is heated to a temperature between 250°

C. and 350°

to evaporate the volatile binder form the stop off material.

5. A method of manufacturing an article as claimed in claim 1 wherein the workpieces are made of a titanium alloy, the workpieces are heated to a temperature equal to or greater than 850°

C. and the pressure applied is equal to or greater than 20×

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

6. A method of manufacturing an article as claimed in claim 5 wherein the workpieces are heated to a temperature between 900°

C. and 950°

C. and the pressure applied is between 20×

10⁵ Nm^-2 and 30×

10⁵ Nm^-2.

7. A method of manufacturing an article as claimed in claim 5 wherein the integral structure is heated to a temperature equal to or greater than 850°

C. to superplastically form the integral structure.

8. A method of manufacturing an article as claimed in claim 7 wherein the integral structure is heated to a temperature between 900°

C. and 950°

C.

9. A method of manufacturing an article as claimed in claim 1 wherein during the assembling of the at least two workpieces into a stack a pipe is arranged to extend from the stack, one end of the pipe is adjacent a preselected area of at least one of the surfaces of at least one of the at least two metal workpieces.

10. A method of diffusion bonding together at least two metal workpieces comprising the steps of:

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

(b) placing the stack between a first selectively pressurisable chamber and a second selectively pressurisable chamber disposed in a vacuum chamber,

(c) evacuating the vacuum chamber,

(d) applying heat and increasing the pressure in the first and second selectively pressurisable chambers simultaneously to apply a pressure across the thickness of the at least two workpieces, thereby diffusion bonding the workpieces together.

11. A method of diffusion bonding as claimed in claim 10 wherein, where the workpieces are made of titanium alloy, the workpieces are heated to a temperature equal to or greater than 850°

C. and the pressure applied is equal to or greater than 20×

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

12. A method of diffusion bonding as claimed in claim 11 wherein the workpieces are heated to a temperature between 900°

C. and 950°

C. and the pressure applied is between 20×

10⁵ Nm^-2 and 30×

10⁵ Nm^-2.