Method of manufacturing an article by diffusion bonding

• US 6,871,398 B2
• Filed: 09/10/2001
• Issued: 03/29/2005
• Est. Priority Date: 09/14/2000
• Status: Expired due to Term

• Current Assignee: Rolls-Royce PLC (Rolls-Royce Holdings Plc)
• Original Assignee: Rolls-Royce PLC (Rolls-Royce Holdings Plc)
• Inventors: Richardson, Brian, Green, Michael
• Primary Examiner(s): EDMONDSON, LYNNE RENEE
• Application Number:
  US09/948,878
• Publication Number:
  US 20040118903A1
• Time in Patent Office: 1,296 Days
• Field of Search: 228/118, 228/157, 228/190, 228/193, 298/897, 298/897.2, 298/897.21
• US Class Current: 29/889.72
• CPC Class Codes: B21D 26/055 Blanks having super-plastic properties
• CPC Class Codes: B23K 20/021 Isostatic pressure welding
• CPC Class Codes: B23K 20/18 Zonal welding by interposing weld-preventing substances between zones not to be welded
• CPC Class Codes: B23K 20/233 without ferrous layer
• CPC Class Codes: B23K 2101/001 Turbines
• CPC Class Codes: B23K 2103/14 Titanium or alloys thereof
• CPC Class Codes: B23P 15/04 turbine or like blades from several pieces
• CPC Class Codes: F01D 5/147 Construction, i.e. structural features, e.g. of weight-saving hollow blades F01D5/148, F01D5/16 and F01D5/20 take precedence; blade shape F01D5/141; blades with cooling or heating channels or cavities F01D5/18; heating, heat-insulating or cooling means on blades F01D5/18
• CPC Class Codes: F04D 29/324 Blades
• CPC Class Codes: F04D 29/384 characterised by form
• CPC Class Codes: F05D 2230/10 by removing material
• CPC Class Codes: F05D 2230/23 by permanently joining parts together
• CPC Class Codes: Y10T 29/49318 Repairing or disassembling
• CPC Class Codes: Y10T 29/49339 Hollow blade
• CPC Class Codes: Y10T 29/49341 with cooling passage

Abstract

A method of diffusion bonding three metal work pieces to form a fan blade, where each workpiece has a flat surface and an excess portion larger than a predetermined size needed to produce a finished fan blade; longitudinally extending slots are provided to interconnect the flat surfaces of the excess portions of the work pieces; the work pieces are assembled into a stack with the flat surfaces in mating abutment and the stack is evacuated from one end of the stack through the slots; heat and pressure are applied across the thickness of the work pieces to diffusion bond the work pieces together to form an integral structure; the excess portions with the slots are then removed.

Claims

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

(a) forming at least two metal workpieces, each metal workpiece has at least one flat surface, each metal workpiece is larger than a predetermined size in at least one direction parallel to the flat surface to form at least one excess portion, the predetermined size is that required to produce the outer profile of the finished article, the at least one excess portion being located outside the outer profile of the finished article,

(b) forming at least one groove in the flat surface of the at least one excess portion of the at least one of the least two metal workpieces,

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

(d) evacuating the stack such that the at least one groove enables at least more of the gases in the stack to be removed from the stack, and

(e) applying heat and pressure across the thickness of the at least two metal workpieces to diffusion bond the at least two metal workpieces together to form an integral structure,

(f) cutting the integral structure such as to remove the excess portions of the at least two metal workpieces and the at least one groove.

2. A method as claimed in claim 1 wherein the at least two metal workpieces have first and second longitudinally spaced ends, each metal workpiece is larger than a predetermined size in a lateral direction perpendicular to the longitudinal direction between the first and second longitudinally spaced ends to form at least one excess portion, the at least one groove extends longitudinally between the first and second longitudinally spaced ends, evacuating the stack from the first end of the stack such that the at least one groove enables at least more of the gases at the second end of the stack to be removed from the stack.

3. A method as claimed in claim 1 comprising before step (d) additional step (g) 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 metal workpieces and after step (f) additional step (h) placing the integral structure in a superplastic forming die 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.

4. A method as claimed in claim 3 comprising after step (f) and before step (h) placing the integral structure in a hot creep forming 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.

5. A method as claimed in claim 1 wherein step (a) comprises forming a first metallic workpiece, a second metallic workpiece and a third metallic workpiece, the third metallic workpiece having two flat surfaces, and step (c) comprises assembling the three metal workpieces into the stack relative to each other so that third metal workpiece is between the first and second metal workpieces and the flat surfaces are in mating abutment.

6. A method as claimed in claim 5 wherein step (a) comprises forming two excess portions on each of the first, second and third metallic workpieces.

7. A method as claimed in claim 6 wherein step (b) comprises forming longitudinally extending slots through the third metallic workpiece to interconnect the flat surfaces of both excess portions of the third metal workpiece.

8. A method as claimed in claim 1 wherein the article is a fan blade.

9. A method as claimed in claim 1 wherein step (a) comprises forming a first metallic workpiece and a second metallic workpiece.

10. A method as claimed in claim 9 wherein step (a) comprises forming two excess portions on each of the first and second metallic workpieces.

11. A method as claimed in claim 10 wherein step (b) comprises forming at least one longitudinally extending groove in the flat surface of both excess portions of the first metal workpiece.

12. A method as claimed in claim 10 wherein step (b) comprises forming at least one longitudinally extending groove in the flat surface of both excess portions of the first metal workpiece and forming at least one longitudinally extending groove in the flat surface of both excess portions of the second metal workpiece.

13. A method as claimed in claim 10 wherein step (b) comprises forming at least one longitudinally extending groove in the flat surface of one excess portion of the first metal workpiece and forming at least one longitudinally extending groove in the flat surface of one excess portion of the second metal workpiece.

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

15. A method as claimed in claim 1 wherein step (a) comprises forming at least one aperture through a first end of the first metallic sheet, step (b) comprises forming the at least one longitudinally extending slot such that it interconnects with the at least one aperture and step (c) comprises stacking at least one additional metallic member on the first end of the first metallic sheet.

16. A method as claimed in claim 1 wherein the at least one longitudinally extending groove extends substantially the full length of the at least one of the at least two metal workpieces.

17. A method as claimed in claim 3 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.

18. A method as claimed in claim 17 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.

19. A method as claimed in claim 18 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.

20. A method as claimed in claim 3 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.

21. A method as claimed in claim 20 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.

22. A method as claimed in claim 1 wherein 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.

23. A method as claimed in claim 22 wherein the edges of the metal workpieces are welded together.

24. 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.

25. A method as claimed in claim 24 wherein the metal workpieces are heated to a temperature between 900°

C. and 950°

C. and the pressure applied is between 20×

10⁵ Nm<sup>−

2</sup> and 30×

10⁵ Nm<sup>−

2</sup>.

26. A method as claimed in claim 3 wherein the integral structure is heated to a temperature equal to, or greater than, 850°

C. to superplastically form the integral structure.

27. A method as claimed in claim 26 wherein the integral structure is heated to a temperature between 900°

and 950°

C.

28. A method as claimed in claim 4 wherein the integral structure is hot creep formed at a temperature equal to, or greater than, 740°

C.

29. A method as claimed in claim 1 wherein step (f) comprises water jet cutting.