Method of making an airfoil

• US 4,472,866 A
• Filed: 03/01/1982
• Issued: 09/25/1984
• Est. Priority Date: 03/01/1982
• Status: Expired due to Fees

• Current Assignee: Ex-Cell-O Corporation
• Original Assignee: TRW Limited (Zeppelin - Stiftung der Stadt Friedrichshafen)
• Inventors: Moracz, Donald J., Cook, Charles R., Toth, Istvan J.
• Primary Examiner(s): Moon, Charlie T.
• Assistant Examiner(s): Wallace, Ronald S.
• Application Number:
  US06/353,403
• Time in Patent Office: 939 Days
• Field of Search: 29/156.8 B, 29/156.8 H, 29/156.8 T, 29/423, 29/463, 29/469, 228/193, 228/190, 228/243, 228/182, 416/233, 416/229 R
• US Class Current: 29/889.6
• CPC Class Codes: B23P 15/04 turbine or like blades from several pieces
• CPC Class Codes: Y10T 29/49332 Propeller making
• CPC Class Codes: Y10T 29/4981 Utilizing transitory attached element or associated separate material
• CPC Class Codes: Y10T 29/49893 Peripheral joining of opposed mirror image parts to form a hollow body
• CPC Class Codes: Y10T 29/49904 Assembling a subassembly, then assembling with a second subassembly

Abstract

An improved method of making an airfoil includes stacking plies in two groups. A separator ply is positioned between the two groups of plies. The groups of plies and the separator ply are interconnected to form an airfoil blank. The airfoil blank is shaped, by forging or other methods, to have a desired configuration. The material of the separator ply is then dissolved or otherwise removed from between the two sections of the airfoil blank to provide access to the interior of the airfoil blank. Material is removed from inner sides of the two separated sections to form core receiving cavities. After cores have been placed in the cavities, the two sections of the airfoil blank are interconnected and the shaping of the airfoil is completed. The cores are subsequently removed from the completed airfoil.

Claims

1. A method of making an airfoil, said method comprising the steps of providing first and second groups of metal plies, providing a separator ply, positioning the two groups of plies with the separator ply between them, forming an airfoil blank by interconnecting and deforming the two groups of plies and the separator ply to form an airfoil blank having first and second sections with the separator ply between the sections, separating the two sections of the airfoil blank to provide access to the interior of the airfoil blank by dissolving the material of the separator ply, and, after performing the step of dissolving the material of the separator ply, removing material from one of the sections to provide a cavity in the one section, and interconnecting the two sections of the airfoil blank with the cavity in the one section facing toward the other section.

2. A method as set forth in claim 1 further including the step of removing material from the other section to provide a cavity in the other section after having performed the step of dissolving the material of the separator ply and prior to performance to said step of interconnecting the two sections, said step of interconnecting the two sections including interconnecting the two sections with the cavity in the other section facing toward the one section.

3. A method as set forth in claim 1 wherein said step of providing first and second groups of plies includes the step of providing first and second groups of plies formed of a first metal, said step of providing a separator ply including the step of providing a separator ply formed of a second metal which is different than the first metal.

4. A method as set forth in claim 3 wherein said step of dissolving the material of the separator ply includes the step of exposing the material of the separator ply to a corrosive material which is effective to chemically attack the second metal and is ineffective to chemically attack the first metal.

5. A method as set forth in claim 3 wherein said step of interconnecting the two groups of plies and the separator ply includes the step of bonding the plies together.

6. A method as set forth in claim 1 wherein said step of deforming the two groups of plies and the separator ply is performed after said step of interconnecting the two groups of plies and the separator ply and prior to performance of said step of dissolving the material of the separator ply.

7. A method as set forth in claim 6 wherein said step of interconnecting the two sections includes the step of diffusion bonding the two sections together with the cavity in the one section facing toward the other section.

8. A method as set forth in claim 6 further including the step of placing a core in the cavity prior to performing said step of interconnecting the two sections, said step of interconnecting the two sections including interconnecting the two sections with the core in abutting engagement with the two sections, said method further including the step of removing the core from the cavity after having performed said step of interconnecting the two sections.

9. A method of making an airfoil, said method comprising the steps of providing metal material for first and second longitudinally extending sections of the airfoil, positioning a longitudinally extending separator piece between the material for the first and second airfoil sections, interconnecting the separator piece and the material for the first and second airfoil sections, shaping the separator piece and the first and second airfoil sections after having performed said interconnecting step, subsequently removing the material of the separator piece from between the first and second airfoil sections to separate them, removing material from at least one of the airfoil sections after having separated them, and thereafter interconnecting the first and second airfoil sections.

10. A method as set forth in claim 9 further including the step of placing a core between the first and second airfoil sections before interconnecting them, said step of interconnecting the first and second airfoil sections including interconnecting the airfoil sections with the core in engagement with both sections, said method further including the step of shaping the first and second airfoil sections with the core between them and then removing the core.

11. A method as set forth in claim 9 wherein said step of shaping the separator piece and the first and second airfoil sections includes the step of deforming the first and second airfoil sections to have an arcuate configuration corresponding to the chamber of the airfoil.

12. A method as set forth in claim 9 wherein said step of shaping the separator piece and the first and second airfoil sections includes the step of deforming the first and second airfoil sections to have a twist corresponding to the twist of the airfoil.

13. A method as set forth in claim 9 wherein said step of providing material for first and second longitudinally extending sections of the airfoil includes the step of providing first and second groups of plies.

14. A method as set forth in claim 9 wherein said step of removing the material of the separator piece from between the first and second airfoil section includes the step of dissolving the material of the separator piece.