Airfoil joining apparatus and methods

Patent metadata

Field	Value
Publication number	US-12312973-B2
Application number	US-202318377508-A
Country	US
Kind code	B2
Filing date	Oct 6, 2023
Priority date	Nov 18, 2021
Publication date	May 27, 2025
Grant date	May 27, 2025

Abstract

An airfoil component for attaching to a cropped airfoil is provided. The cropped airfoil comprises a cropped airfoil attachment section and a cropped first side opposite a cropped second side, which each extend axially between a cropped first edge and a cropped second edge to define a cropped chord length. The airfoil component comprises a body having a component first side opposite a component second side. The body defines an attachment section for attaching the airfoil component to the cropped airfoil at the cropped airfoil attachment section. The attachment section extends axially between a component first edge and a component second edge to define a component chord length, and the attachment section is oversized with respect to the cropped airfoil attachment section such that the component chord length is longer than the cropped chord length. Systems and methods also are provided.

First claim

What is claimed is:

1. A method of repairing an airfoil comprising:
disposing a cropped airfoil in a cropped airfoil electrode;
disposing an airfoil repair component within a repair component electrode, the repair component electrode comprising a repair component electrode insert removably received within a repair component electrode body;
positioning the airfoil repair component with respect to the cropped airfoil;
passing an inert gas to the repair component electrode via an inert gas manifold defined in the repair component electrode; and
conducting a joining process to attach the airfoil repair component to the cropped airfoil and form an airfoil.

2. The method of claim 1 further comprising removing a damaged portion of the airfoil to form the cropped airfoil.

3. The method of claim 1 wherein conducting a joining process comprises passing a current through the cropped airfoil electrode and the repair component electrode.

4. The method of claim 3 wherein passing the current through the cropped airfoil electrode and the repair component electrode includes solid state resistance welding the airfoil repair component received in the repair component electrode to the cropped airfoil received in the cropped airfoil electrode.

5. The method of claim 1 further comprising obtaining a net shape of the airfoil.

6. The method of claim 5 wherein obtaining the net shape of the airfoil comprises machining the airfoil.

7. The method of claim 5 wherein obtaining the net shape of the airfoil comprises deformation processing the airfoil.

8. The method of claim 1 wherein the inert gas manifold includes a plurality of grooves.

9. The method of claim 1 further comprising creating an inert gas shield around the airfoil repair component.

10. A method of airfoil repair comprising:
removing a damaged portion of an original airfoil to form a cropped airfoil, wherein the cropped airfoil comprises a cropped airfoil attachment section and a cropped first side opposite a cropped second side, the cropped first side and the cropped second side each extending axially between a cropped first edge and a cropped second edge to define a cropped chord length;
disposing the cropped airfoil in a cropped airfoil electrode;
disposing an airfoil repair component within a repair component electrode, the repair component electrode comprising a repair component electrode insert removably received within a repair component electrode body, wherein the airfoil repair component comprises a body having a repair first side opposite a repair second side, the body defining a repair attachment section for attaching the airfoil repair component to the cropped airfoil at the cropped airfoil attachment section, the repair attachment section extending axially between a repair first edge and a repair second edge to define a repair chord length, the repair attachment section being oversized with respect to the cropped airfoil attachment section such that the repair chord length is longer than the cropped chord length;
positioning the airfoil repair component with respect to the cropped airfoil;
passing an inert gas to the repair component electrode via an inert gas manifold defined in the repair component electrode; and
passing current through the cropped airfoil electrode and the repair component electrode to attach the airfoil repair component to the cropped airfoil and form a repaired airfoil.

11. The method of claim 10 further comprising coining the cropped airfoil to remove a twist from the cropped airfoil.

12. The method of claim 10 wherein positioning the airfoil repair component with respect to the cropped airfoil comprises locating the repair component electrode through a feedback system to ascertain at least one of a size and a position of the airfoil repair component with respect to the cropped airfoil.

13. The method of claim 10 wherein positioning the airfoil repair component with respect to the cropped airfoil comprises manipulating an alignment assembly to reposition the airfoil repair component along at least one independent axis defined by the cropped airfoil.

14. The method of claim 10 wherein passing current through the cropped airfoil electrode and the repair component electrode comprises welding the airfoil repair component to the cropped airfoil through solid state resistance welding.

15. The method of claim 10 further comprising obtaining a net shape of the original airfoil by processing the repaired airfoil after the repaired airfoil is formed.

16. The method of claim 15 wherein obtaining the net shape of the original airfoil comprises machining the repaired airfoil.

17. The method of claim 10 wherein the inert gas manifold includes a plurality of grooves.

18. The method of claim 10 further comprising creating an inert gas shield around the airfoil repair component.

Assignees

• Gen Electric

Inventors

• Vaze Suhas Prabhakar
• Trapp Timothy
• Campbell Scott Sager
• Firestone Gregory Christopher
• Mast Jonathan David
• Stotler Timothy Vernon

Classifications

• F05D2250/183

  zigzag · CPC title

• F05D2230/233

  Electron beam welding · CPC title

• F05D2230/232

  by welding · CPC title

• F05D2270/80

  Devices generating input signals, e.g. transducers, sensors, cameras or strain gauges · CPC title

• F05D2270/8041

  Cameras · CPC title