Support collar geometry for linear friction welding

Patent metadata

Field	Value
Publication number	US-9694440-B2
Application number	US-90992810-A
Country	US
Kind code	B2
Filing date	Oct 22, 2010
Priority date	Oct 22, 2010
Publication date	Jul 4, 2017
Grant date	Jul 4, 2017

Abstract

An example method of attaching an airfoil for an integrally bladed rotor includes placing a support collar in an installed position around at least a leading edge and trailing edge of an airfoil stub to be repaired in an integrally bladed rotor. The support collar and the airfoil stub together have a midline that is positioned between opposing, laterally outer surfaces of the airfoil stub when the support collar is in the installed position. The method performs linear friction welding to add a replacement airfoil to the airfoil stub.

First claim

We claim:

1. A method of attaching an airfoil for an integrally bladed rotor comprising:
sizing a consumable portion of a support collar assembly such that the consumable portion has a midline that is positioned between opposing, laterally outer surfaces of an airfoil stub for an integrally bladed rotor when the support collar assembly is in an installed position, the support collar assembly placed around at least a leading edge and a trailing edge of the airfoil stub when in the installed position; and
performing linear friction welding to add an airfoil to the airfoil stub.

2. The method of claim 1 , wherein the midline corresponds generally to the circumferential center of a section of the consumable portion, the section taken along a plane that is perpendicular to the first direction.

3. The method of claim 1 , wherein a convex side of the consumable portion is circumferentially spaced from the midline a first distance, and a concave side of the consumable portion is circumferentially spaced from the midline a second distance that is the same as the first distance.

4. The method of claim 3 , wherein a convex side of the consumable portion contains more material or less material than a concave side of the consumable portion.

5. The method of claim 3 , wherein a convex side of the consumable portion contains less material or less material than a concave side of the consumable portion.

6. The method of claim 1 , including consuming the consumable portion of the support collar assembly during the linear friction welding.

7. The method of claim 1 , wherein the support collar assembly and the airfoil stub are formed of the same material.

8. The method of claim 7 , wherein the same material is a titanium material.

9. The method of claim 1 , wherein the support collar assembly is formed of a first sub-collar configured to support the leading edge of the airfoil stub and a second sub-collar configured to support the trailing edge of the airfoil stub, and with unsupported positions between the first sub-collar and the second sub-collar.

10. The method of claim 1 , including consuming a first amount of material from a first lateral side of the midline during the linear friction welding; and
consuming a second amount of material from an opposing, second side of the midline during the linear friction welding, the first amount of material substantially the same as the second amount of material.

11. The method of claim 1 , wherein the integrally bladed rotor comprises a titanium alloy.

12. The method of claim 1 , wherein the support collar assembly comprises a titanium alloy.

13. The method of claim 1 , wherein a convex side of the consumable portion contains more material or less material than a concave side of the consumable portion.

14. The method of claim 1 , wherein the support collar assembly includes a first sub-collar for positioning about the leading edge and a second sub-collar for positioning about the trailing edge.

15. A method of attaching an airfoil for an integrally bladed rotor comprising:
sizing a consumable portion of a support collar assembly such that the consumable portion has a midline that is positioned between opposing, laterally outer surfaces of an airfoil stub when the support collar assembly is in an installed position around at least a leading edge and trailing edge of the airfoil stub for an integrally bladed rotor;
after the sizing, placing the support collar assembly in the installed position; and
performing linear friction welding to add an airfoil to the airfoil stub.

16. The method of claim 15 , including consuming a first amount of material from a first lateral side of the midline during the linear friction welding; and
consuming a second amount of material from an opposing, second side of the support collar assembly during the linear friction welding, the first amount of material substantially the same as the second amount of material.

17. The method of claim 15 , wherein a convex side of the consumable portion is circumferentially spaced from the midline a first distance, and a concave side of the consumable portion is circumferentially spaced from the midline a second distance that is the same as the first distance.

18. The method of claim 17 , wherein a convex side of the consumable portion contains more material than a concave side of the consumable portion.

19. The method of claim 17 , wherein a concave side of the consumable portion contains more material than a convex side of the consumable portion.

20. The method of claim 15 , wherein the support collar assembly includes a first sub-collar for positioning about the leading edge and a second sub-collar for positioning about the trailing edge.

Assignees

• Moor James J
• Chin Herbert A
• Czeladko Greg
• Danko Gene A
• Haynes Andrew L
• Lin Wangen
• Nevins Vincent
• Schaefer Robert P
• Privitzer Eberhardt
• United Technologies Corp

Inventors

• Moor James J
• Chin Herbert A
• Czeladko Greg
• Danko Gene A
• Haynes Andrew L
• Lin Wangen
• Nevins Vincent
• Schaefer Robert P
• Privitzer Eberhardt

Classifications

• F01D25/285

  Temporary support structures, e.g. for testing, assembling, installing, repairing; Assembly methods using such structures · CPC title

• F01D5/34

  Rotor-blade aggregates of unitary construction {, e.g. formed of sheet laminae; (discs formed of sheet laminae F01D5/028; ceramic materials F01D5/284, composite materials F01D5/282)} · CPC title

• B23K2201/001

  Operations & Transport · mapped topic

• F01D5/3061

  by welding, brazing · CPC title

• B23K20/1205 Primary

  using translation movement · CPC title