Method of manufacturing an article by superplastic forming and diffusion bonding

• US 6,418,619 B1
• Filed: 10/02/2000
• Issued: 07/16/2002
• Est. Priority Date: 10/14/1999
• Status: Expired due to Term

• Current Assignee: Rolls-Royce PLC (Rolls-Royce Holdings Plc)
• Original Assignee: Rolls-Royce PLC (Rolls-Royce Holdings Plc)
• Inventors: Launders, Paul D
• Primary Examiner(s): ROSENBAUM, IRENE CUDA
• Application Number:
  US09/678,370
• Time in Patent Office: 652 Days
• Field of Search: 298/897, 298/891, 298/897.2, 294/28, 228/118
• US Class Current: 29/889.7
• CPC Class Codes: B21D 53/78 propeller blades; turbine blades
• CPC Class Codes: B23K 20/023 Thermo-compression bonding
• CPC Class Codes: B23K 20/18 Zonal welding by interposing weld-preventing substances between zones not to be welded
• CPC Class Codes: B23P 15/04 turbine or like blades from several pieces
• CPC Class Codes: Y10T 29/49318 Repairing or disassembling
• CPC Class Codes: Y10T 29/49336 Blade making
• CPC Class Codes: Y10T 29/49339 Hollow blade

Abstract

A method of manufacturing an article (10) from two metal workpieces (30,32), the first and second metal workpieces (30,32) define the outer profile of the article (10). The second workpiece (32) is thicker than the first workpiece (30). The first workpiece (30) has two flat surfaces (34,36) and the second workpiece has one flat surface (38) and one machined (42) surface (40). Stop of is applied to surface (34) to prevent diffusion bonding at preselected areas. The workpieces (30,32) are assembled into a stack (58) so that the flat surfaces (34,38) are in abutment. Heat and pressure are applied to diffusion bond the workpieces (30,32) together to form an integral structure (60). The integral structure (60) is placed in a die such that the first workpiece (30) faces a convex surface of the die. The integral structure (60) is heated to cause the integral structure (60) to be hot creep formed on the convex surface of the die. The integral structure (62) is hot formed in a superplastic forming die by heating and internally pressurising the integral structure (62) to cause a preselected area of the second workpiece to be hot formed to produce the article (10).

Claims

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

(a) forming a first metal workpiece which has a first flat surface and a second flat surface,

(b) forming a second metal workpiece which has a first flat surface, the second metal workpiece being thicker than the first metal workpiece, the first and second metal workpieces defining the outer profile of the article,

(c) machining the second metal workpiece on a second surface opposite to the first flat surface to give a predetermined mass distribution in the second metal workpiece,

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

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

(f) applying heat and pressure across the thickness of the at least two metal workpieces to diffusion bond the at least two metal workpieces together in areas other than the preselected areas to form an integral structure,

(g) placing the integral structure in a hot creep forming die, the die having a convex surface, the integral structure being placed in the die such that the second flat surface of the first metal workpiece faces the convex surface of the die, heating the integral structure while it is within the die to cause the integral structure to be hot creep formed on the convex surface of the die,

(h) placing the integral structure in a superplastic forming dies heating the integral structure and internally pressurising the integral structure while it is within the die to cause the preselected area of at least the second metal workpiece to be hot formed to produce a hollow article of predetermined shape.

2. A method as claimed in claim 1 wherein step (c) comprises machining the second metal workpiece to varying depths up to a maximum depth, the maximum depth of machining is such that the remaining thickness of the second metal workpiece is equal to the thickness of the first metal workpiece.

3. A method a claimed in claim 1 wherein the hollow article is a fan outlet guide vane.

4. A method as claimed in claim 1 comprising a superplastically forming and diffusion bonding three metal workpieces, the third metal workpiece having flat surfaces, wherein in step (e) the three metal workpieces are assembled into the stack relative to each other so that the third metal workpiece is between the first and second metal workpieces and the flat surfaces are in mating abutment, said stack having opposite ends.

5. A method as claimed in claim 4 wherein the hollow article is a fan blade.

6. A method as claimed in claim 1 wherein the hot creep forming die used in step (g) is the superplastic forming die used in step (h).

7. A method as claimed in claim 4 wherein after diffusion bonding the stack of workpieces and before superplastically forming the integral structure, the integral structure is heated and loads are applied to opposite ends of the integral structure to twist one end relative to the other end to contour the integral structure to a predetermined shape.

8. A method as claimed in claim 7 wherein after twisting the integral structure and before superplastic forming the integral structure, the contoured integral structure is internally pressurised to break the adhesive bond between the stop off material and the at least one workpiece in the preselected area.

9. A method as claimed in claim 8 wherein after internally pressurising the integral structure to break the adhesive bond and before internally pressurising the integral structure to superplastically form at least one metal workpiece, the interior of the integral structure is sequentially evacuated and supplied with inert gas to remove oxygen from the interior of the integral structure.

10. A method as claimed in claim 1 wherein after diffusion bonding the stack of workpieces and before superplastically forming the integral structure, the integral structure is internally pressurised to break the adhesive bond between the stop off material and the at least one workpiece in the preselected area.

11. A method as claimed in claim 10 wherein after internally pressurising the integral structure to break the adhesive bond and before internally pressurising the integral structure to superplastically form at least one metal workpiece, the interior of the integral structure is sequentially evacuated and supplied with inert gas to remove oxygen from the interior of the integral structure.

12. A method as claimed in claim 1 wherein the metal workpieces have edges and after the metal workpieces are arranged in a stack and before the metal workpieces are diffusion bonded together to form an integral structure, the edges of the metal workpieces are sealed.

13. A method as claimed in claim 12 wherein the edges of the metal workpieces are welded together.

14. A method as claimed in claim 1 wherein where the metal workpieces are made of a titanium alloy, the metal 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<sup>−

2</sup> to diffusion bond the workpieces together to form an integral structure.

15. A method as claimed in claim 14 wherein the metal workpieces are heated to a temperature between 900°

C. 950°

C. and the pressure applied is between 20×

10⁵ Nm<sup>−

2</sup> and 30×

10⁵ Nm<sup>−

2</sup>.

16. A method as claimed in claim 1 wherein the integral structure is heated to a temperature equal to, or greater than, 850°

C. to superplastically form the integral structure.

17. A method as claimed in claim 16 wherein integral structure is heated to a temperature between 900°

and 950°

C.

18. A method as claimed in claim 1 wherein the integral structure is hot creep formed at a temperature equal to, or greater than, 740°

C.

19. A method as claimed in claim 1 wherein in step (c), the machining comprises one of milling, electrochemical machining, chemical machining, or the electrodischarge machining.

20. A method as claimed in claim 1 wherein the thickness of the first metal workpiece is substantially the same as the thickness required for the finished hollow article.