Method of manufacturing an article by superplastic forming and diffusion bonding

• US 5,479,705 A
• Filed: 06/07/1994
• Issued: 01/02/1996
• Est. Priority Date: 05/01/1992
• Status: Expired due to Term

• Current Assignee: Rolls-Royce PLC (Rolls-Royce Holdings Plc)
• Original Assignee: Rolls-Royce PLC (Rolls-Royce Holdings Plc)
• Inventors: Fowler, John O., Richardson, Brian
• Primary Examiner(s): Ramsey, Kenneth J.
• Application Number:
  US08/255,764
• Time in Patent Office: 574 Days
• Field of Search: 29/889.72, 29/890.42, 228/118, 228/157, 228/172, 228/193, 228/265
• US Class Current: 29/889.72
• CPC Class Codes: B21D 26/055 Blanks having super-plastic properties
• CPC Class Codes: B21D 53/045 by inflating partially united plates
• 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: B23K 2101/001 Turbines
• CPC Class Codes: Y10T 29/49339 Hollow blade

Abstract

A plurality of titanium sheets are assembled into a stack. At least one of the sheets is provided with a stop off material on one of its surfaces 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 assembly is heated and externally pressurized to diffusion bond the sheets together. The integral structure so formed is heated and opposite ends of the integral structure are twisted relatively to contour the integral structure to a predetermined shape. The integral structure is internally pressurized to break the adhesive bonds. The integral structure is heated and internally pressurized to superplastically form one sheet to produce an article, e.g. a fan blade.

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

(d) heating the integral structure and applying loads 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,

(e) heating the twisted integral structure to a temperature at which the metal is plastic and internally pressurising the twisted integral structure to break the adhesive bond between the stop off material and the at least one workpiece in the preselected areas,

(f) heating the twisted 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 predetermined shape.

2. A method as claimed in claim 1 including after internally pressurising the integral structure to break the adhesive bond and before internally pressurising the integral structure to superplastically form at least one workpiece sequentially evacuating and supplying inert gas to the interior of the integral structure to remove oxygen from the interior of the integral structure.

3. A method as claimed in claim 2 in which the step of sequentially evacuating and supplying inert gas to the interior of the integral structure to remove oxygen is performed a plurality of times.

11. A method as claimed in claim 1 or claim 4 wherein, where the workpieces are made of a titanium alloy, heating the workpieces to a temperature equal to or greater than 50°

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

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

16. A method as claimed in claim 1 or claim 4 in which the integral structure is heated to a temperature of 800°

C. for twisting the opposite ends of the integral structure.

17. A method as claimed in any of claims 1 or claim 4 including before the opposite ends of the integral structure are twisted, heating and applying a load to one end of the integral structure to camber said end.

18. A method as claimed in claim 1 or claim 4 including holding a first one of the opposite ends stationary and rotating the other one of the opposite ends to twist the integral structure.

19. A method as claimed in claim 1 or claim 4 in which the article is a fan blade.

20. A method as claimed in claim 1 wherein steps (e) and (f) are performed with the twisted integral structure positioned between superplastic forming dies.

22. A method as claimed in claim 1 or claim 4 wherein the step of breaking the adhesive bond comprises supplying a predetermined volume of pressurised gas into the interior of the integral structure and monitoring the rate of pressure decay in the interior of the integral structure for rates of pressure decay greater than a predetermined value.

4. A method of manufacturing an article by superplastic forming and diffusion bonding at least two metal workpieces, each of the metal workpieces having at least one flat surface, the method comprising the steps of

(a) 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,

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

(c) 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,

(d) 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,

(e) placing the sealed assembly in an oven while continuously evacuating the sealed assembly,

(f) heating the sealed assembly while it is within the oven to evaporate volatile binder from the stop off material while continuously evacuating the sealed assembly to remove the volatile binder from between the at least two metal workpieces of the sealed assembly,

(g) sealing the pipe,

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

(i) heating the integral structure and applying loads 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,

(j) heating the twisted integral structure to a temperature at which the metal is plastic and internally pressurising the twisted integral structure to break the adhesive bond between the stop off material and the at least one workpiece in the preselected areas,

(k) heating the twisted 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 predetermined shape.

5. A method as claimed in claim 4 wherein before the pipe is sealed, the sealed assembly is cooled whilst the sealed assembly is continuously evacuated.

6. A method as claimed in claim 5 in which the sealed assembly is cooled to ambient temperature.

7. A method as claimed in claim 4 or claim 5 including after internally pressurising the integral structure to break the adhesive bond and before internally pressurising the integral structure to superplastically form at least one workpiece sequentially evacuating and supplying inert gas to the interior of the integral structure to remove oxygen from the interior of the integral structure.

8. A method as claimed in claim 7 in which the step of sequentially evacuating and supplying inert gas to the interior of the integral structure to remove oxygen is performed a plurality of times.

9. A method as claimed in claim 4 comprising welding the edges of the workpieces together.

10. A method as claimed in claim 4 including heating the stack to a temperature between 250°

C. and 350°

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

12. A method as claimed in claim 10 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.

13. A method as claimed in claim 10 wherein the integral structure is heated to a temperature equal to or greater than 850°

C. to superplastically form the integral structure.

14. A method as claimed in claim 13 wherein the integral structure is heated to a temperature between 900°

C. and 950°

C.

15. A method as claimed in claim 4 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.

21. A method as claimed in claim 4 wherein steps (j) and (k) are performed with the twisted integral structure positioned between the superplastic forming dies.

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

(d) heating the integral structure and applying loads 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,

(e) heating the twisted integral structure to a temperature at which the metal is plastic and internally pressurizing the twisted integral structure to break the adhesive bond between the stop off material and the at least one workpiece in the preselected areas,

(f) heating the twisted integral structure and internally pressurizing it to cause the preselected areas of at least one of the workpieces to be superplastically formed to produce an article of predetermined shape,

wherein the step of breaking the adhesive bond comprises supplying a predetermined volume of pressurized gas into the interior of the integral structure and monitoring the rate of pressure decay in the interior of the integral structure for rates of pressure decay greater than a predetermined value.

25. The method as claimed in claim 23 wherein step (e) and (f) are performed with the twisted integral structure positioned between superplastic forming dies.

24. A method of manufacturing an article by superplastic forming and diffusion bonding at least two metal workpieces, each of the metal workpieces having at least one flat surface, the method comprising the steps of

(a) 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,

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

(c) 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,

(d) 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,

(e) placing the sealed assembly in an oven while continuously evacuating the sealed assembly,

(f) heating the sealed assembly while it is within the oven to evaporate volatile binder from the stop off material while continuously evacuating the sealed assembly to remove the volatile binder from between the at least two metal workpieces of the sealed assembly,

(g) sealing the pipe,

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

(i) heating the integral structure and applying loads 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,

(j) heating the twisted integral structure to a temperature at which the metal is plastic and internally pressurizing the twisted integral structure to break the adhesive bond between the stop material and the at least one workpiece in the preselected areas,

(k) heating the twisted integral structure and internally pressurizing it to cause the preselected areas of at least one of the workpieces to be superplastically formed to produce an article of predetermined shape,

wherein the step of breaking the adhesive bond comprises supplying a predetermined volume of pressurized gas into the interior of the integral structure and monitoring the rate of pressure decay in the interior of the integral structure for rates of pressure decay greater than a predetermined value.

26. The method as claimed in claim 24 wherein step (j) and (k) are performed with the twisted integral structure positioned between superplastic forming dies.

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

(d) heating the integral structure and applying loads to opposite ends of the integral structure to twist one and relative to the other end to contour the integral structure to a predetermined shape,

(e) heating the twisted integral structure to a temperature at which the metal is plastic and internally pressurizing the twisted integral structure to break the adhesive bond between the stop off material and the at least one workpiece in the preselected areas without support from any die structure,

(f) heating the twisted integral structure and internally pressurizing it to cause the preselected areas of at least one of the workpieces to be superplastically formed to produce an article of predetermined shape,

wherein the step of breaking the adhesive bond comprises supplying a predetermined volume of pressurized gas into the interior of the integral structure and monitoring the rate of pressure decay in the interior of the integral structure for rates of pressure decay greater than a predetermined value.

28. A method of manufacturing an article by superplastic forming and diffusion bonding at least two metal workpieces, each of the metal workpieces having at least one flat surface, the method comprising the steps of

(a) 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,

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

(c) 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,

(d) 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,

(e) placing the sealed assembly in an oven while continuously evacuating the sealed assembly,

(f) heating the sealed assembly while it is within the oven to evaporate volatile binder from the stop off material while continuously evacuating the sealed assembly to remove the volatile binder from between the at least two metal workpieces of the sealed assembly,

(g) sealing the pipe,

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

(i) heating the integral structure and applying loads 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,

(j) heating the twisted integral structure to a temperature at which the metal is plastic and internally pressurizing the twisted integral structure to break the adhesive bond between the stop material and the at least one workpiece in the preselected areas without support from any die structure,

(k) heating the twisted integral structure and internally pressurizing it to cause the preselected areas of at least one of the workpieces to be superplastically formed to produce an article of predetermined shape.