METHOD OF FORMING AN INTERNAL STRUCTURE WITHIN A HOLLOW COMPONENT

• US 20110002788A1
• Filed: 06/08/2010
• Published: 01/06/2011
• Est. Priority Date: 07/02/2009
• Status: Abandoned Application

• Current Assignee: Rolls-Royce PLC (Rolls-Royce Holdings Plc)
• Original Assignee: Rolls-Royce PLC (Rolls-Royce Holdings Plc)
• Inventors: Mason, John H.
• Application Number:
  US12/796,231
• Publication Number:
  US 20110002788A1
• Time in Patent Office: Days
• US Class Current: 416/223.R
• CPC Class Codes: B21D 26/055 Blanks having super-plastic properties
• CPC Class Codes: B21D 53/78 propeller blades; turbine blades
• CPC Class Codes: F01D 5/005 Repairing methods or devices
• CPC Class Codes: Y02T 50/60 Efficient propulsion technologies, e.g. for aircraft

Abstract

A method of forming an internal structure within a hollow component (2), the component comprising first and second panels (4, 6) and at least one membrane (8; 10) disposed between the first and second panels (4, 6), the method comprising: selectively bonding the at least one membrane (8; 10) to the first and/or second panels (4, 6); inflating the component (2) by passing a pressurised fluid between the first and second panels (4, 6) such that the first and second panels (4, 6) are inflated into contact with a die assembly (38) and such that the membrane (8; 10) forms an internal structure between the first and second panels (4, 6); and deforming the internal structure by applying the pressurised fluid at a first pressure (P1) on one side of the membrane (8; 10) and at a second pressure (P2) on the other side of the membrane (8; 10).

Claims

1. A method of forming an internal structure within a hollow component, the component comprising first and second panels and at least one membrane disposed between the first and second panels, the method comprising:

selectively bonding the at least one membrane to the first and/or second panels;

inflating the component by passing a pressurised fluid between the first and second panels such that the first and second panels are inflated into contact with a die assembly and such that the membrane forms an internal structure between the first and second panels; and

deforming the internal structure by applying the pressurised fluid at a first pressure on one side of the membrane and at a second pressure on the other side of the membrane.

2. A method of forming an internal structure within a hollow component as claimed in claim 1, wherein deforming the internal structure comprises deforming the internal structure in a direction which is substantially parallel to a plane of the first or second panel.

3. A method of forming an internal structure within a hollow component as claimed in claim 1, wherein selectively bonding comprises applying a stop-off material to one or more portions of the at least one membrane and/or the first and second panels and diffusion bonding the component such that the membrane is bonded to the first and second panels except at the one or more portions where the stop-off material is applied.

4. A method of forming an internal structure within a hollow component as claimed in claim 1, wherein the at least one membrane is bonded to only one of the first and second panels.

5. A method of forming an internal structure within a hollow component as claimed in claim 4, wherein either side of the unbonded portion the membrane is bonded to the first or second panel.

6. A method of forming an internal structure within a hollow component as claimed in claim 4, wherein each of the one or more unbonded portions define a cavity between the membrane and the first or second panel.

7. A method of forming an internal structure within a hollow component as claimed in claim 1, wherein during inflation the pressurised fluid inflates the cavity between the membrane and the first or second panel so as to form the internal structure.

8. A method of forming an internal structure within a hollow component as claimed in claim 1, wherein during deformation the first pressure is applied to the cavity between the membrane and the first or second panel and the second pressure is applied between the membrane and the other of the first or second panel.

9. A method of forming an internal structure within a hollow component as claimed in claim 8, wherein the differential between the first pressure and the second pressure causes the internal structure to be deformed.

10. A method of forming an internal structure within a hollow component as claimed in claim 1, wherein the deformed internal structure creates a re-entrant feature.

11. A method of forming an internal structure within a hollow component as claimed in claim 1, wherein the at least one membrane comprises a first membrane and a second membrane and selectively bonding further comprises applying a stop-off material to the one or both of the opposing surfaces of the first and second membranes to prevent bonding of the first membrane to the second membrane.

12. A method of forming an internal structure within a hollow component as claimed in claim 1, wherein the die assembly comprises first and second dies each having a forming surface between which the aerofoil structure is placed;

the method further comprising moving the die assembly to a second position and further inflating the component by passing a pressurised fluid between the first and second panels such that the first and second panels are inflated into contact with the die assembly in the second position, wherein the distance between at least a portion of the first and second dies is greater in the second position.

13. A method of forming an internal structure within a hollow component as claimed in claim 12, wherein the forming surface of the first and/or second dies has a section which is movable relative to the rest of the forming surface, and wherein moving the die assembly comprises moving the movable section to the second position.

14. A method of forming an internal structure within a hollow component as claimed in claim 11, wherein selectively bonding comprises selectively bonding the first membrane to the first panel and selectively bonding the second membrane to the second panel.

15. A method of forming an internal structure within a hollow component as claimed in any one of claim 11, wherein the first pressure is applied between the first membrane and the first panel and between the second membrane and the second panel, and the second pressure is applied between the first and second membranes.

16. A method of forming an internal structure within a hollow component as claimed in claim 11, wherein the pressurised fluid when further inflating the component is at a first pressure between the first membrane and the first panel and between the second membrane and the second panel, and at a second pressure between the first and second membranes, wherein the first pressure is lower than the second pressure.

17. A method of forming an internal structure within a hollow component as claimed in claim 11, further comprising providing a damping material between the first and second membranes.

18. A method of forming an internal structure within a hollow component as claimed in claim 1, wherein the hollow component is an aerofoil structure.

19. An aerofoil structure comprising first and second panels and first and second membranes disposed between the first and second panels, wherein the first membrane is selectively bonded to the first panel and the second membrane is selectively bonded to the second panel, wherein unbonded portions of the first and second membranes are formed into re-entrant features, the re-entrant features of the first or second membrane being spaced apart from the other of the first or second membrane.

20. An aerofoil structure as claimed in claim 19, wherein the re-entrant features of the first and second membranes are offset from one another.

21. An aerofoil structure as claimed in claim 19, wherein disposed between the first and second membranes is a damping material.

22. A turbomachine comprising an aerofoil structure as claimed in claims 19.

23. A die assembly for forming an aerofoil structure, the die assembly comprising:

first and second dies each having a forming surface between which the aerofoil structure is placed;

wherein the forming surface of the first and/or second dies has a section which is movable relative to the rest of the forming surface.

24. A die assembly as claimed in claim 23, wherein the movable section is a central section of the forming surface.

25. A die assembly as claimed in claim 23, wherein the movable section is movable toward and away from a central axis between the first and second dies.

26. A die assembly as claimed in claim 23, wherein the movable section has a first and second position.

27. A die assembly as claimed in claim 23, wherein in the first position the aerofoil structure is inflated into contact with the forming surfaces of the first and second dies to form an internal structure and wherein in the second position the aerofoil structure is further inflated into contact with the forming surfaces of the first and second dies to take a final form of the aerofoil structure.

28. A method of forming an internal structure within an aerofoil structure using a die assembly, the aerofoil structure comprising first and second panels and at least one membrane disposed between the first and second panels and the die assembly comprising first and second dies each having a forming surface;

wherein the forming surface of the first and/or second dies has a section which is movable relative to the rest of the forming surface, the method comprising;

selectively bonding the at least one membrane to the first and/or second panels;

locating the aerofoil structure between the forming surfaces of the first and second dies with the movable section in a first position inflating the aerofoil structure by passing a pressurised fluid between the first and second panels such that the first and second panels are inflated into contact with the forming surfaces of the first and second dies and such that the membrane forms an internal structure between the first and second panels;

deforming the internal structure by applying the pressurised fluid at a first pressure on one side of the membrane and at a second pressure on the other side of the membrane;

moving the movable section to a second position and further inflating the aerofoil structure such that the first and second panels are inflated into contact with the forming surfaces of the first and second dies.