IP Library Granted Patent US 11,828,190
Granted Patent B2
US 11,828,190 · App. 17/529,656 · Granted Nov 28, 2023

Airfoil joining apparatus and methods

Inventors: Suhas Prabhakar Vaze (Loveland, OH); Timothy Trapp (Cincinnati, OH); Scott Sager Campbell (Columbus, OH); Gregory Christopher Firestone (Pickerington, OH); Jonathan David Mast (Lebanon, OH); Timothy Vernon Stotler (Columbus, OH)
Assignee: General Electric Company
F01D5/005B23K11/0026B23K11/16B23K15/0006B23K15/006B23K15/0093B23P6/002F01D5/02F01D5/34F04D29/324B23K2101/001B23K2103/26B23P2700/13F05D2230/233F05D2230/234F05D2230/235F05D2230/40F05D2230/80
View Patent ↗
Loading inventors, assignments & file history…
Monitor This Case
Get email alerts when status or documents change.
Order Certified Copies
Most orders are placed with the USPTO same day — all within 24 business hours.
Order via The Patent Place →
Pre-filled with this patent's details
Quick Facts
Patent No.
US 11,828,190
App. No.
17/529,656
Granted
Nov 28, 2023
Kind
B2
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.

Claims (20)

1. An airfoil repair system, comprising:

a cropped airfoil comprising 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;

an airfoil repair component comprising 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;

a repair component electrode for receipt of the airfoil repair component, the repair component electrode comprising a repair component electrode insert removable with respect to a repair component electrode body, the repair component electrode insert surrounding at least a portion of the airfoil repair component; and

a retention assembly for positioning the airfoil repair component with respect to the cropped airfoil,

wherein the repair component electrode insert defines an inert gas manifold for receipt of an inert gas and a plurality of grooves extending from the inert gas manifold along the repair component electrode insert.

2. The airfoil repair system of claim 1 , wherein the repair component electrode insert comprises a first half and a second half, each of the first half and the second half defining a portion of the inert gas manifold for receipt of the inert gas and each of the first half and the second half defining the plurality of grooves extending from the inert gas manifold along the respective half of the repair component electrode insert.

3. The airfoil repair system of claim 1 , further comprising a cropped airfoil electrode for receipt of the cropped airfoil, wherein the cropped airfoil electrode comprises a dovetail block, a cropped airfoil electrode body, and the retention assembly, wherein the cropped airfoil comprises a dovetail receivable within the dovetail block, and wherein the dovetail block is removably secured to the cropped airfoil electrode body by one-handed manipulation of the retention assembly.

4. The airfoil repair system of claim 1 , wherein the repair component electrode body defines a plurality of serrations, each serration having a change in direction.

5. The airfoil repair system of claim 1 , wherein a blisk comprises the cropped airfoil, and wherein the retention assembly comprises a cropped airfoil portion for positioning the airfoil repair component with respect to the blisk.

6. The airfoil repair system of claim 1 , wherein the retention assembly comprises a feedback system including at least one feedback device located to determine at least one of a size and a position of the airfoil repair component with respect to the cropped airfoil.

7. The airfoil repair system of claim 1 , wherein the retention assembly comprises an alignment assembly, wherein the alignment assembly is configured to adjust the position of the airfoil repair component with respect to the cropped airfoil along one or more independent axes defined by the cropped airfoil.

8. The airfoil repair system of claim 1 , wherein the repair component electrode comprises a point constraint, a line constraint, and a planar restraint with respect to the airfoil repair component, and wherein the point constraint is configured to be manipulated to release the airfoil repair component for removal from the repair component electrode.

9. An electrode assembly, comprising:

a repair component electrode;

a cropped airfoil electrode; and

a retention assembly and a dovetail block for positioning a cropped airfoil relative to an airfoil repair component to provide a stabilization force,

wherein the repair component electrode receives the airfoil repair component, and the cropped airfoil electrode receives the cropped airfoil, and

wherein an electrical current and a compressive axial force are passed through the repair component electrode, with the airfoil repair component positioned therein, and the cropped airfoil electrode, with the cropped airfoil positioned therein, to join the airfoil repair component to the cropped airfoil,

wherein the repair component electrode defines an inert gas manifold for receipt of an inert gas and a plurality of grooves extending from the inert gas manifold along the repair component electrode.

Assignments (3)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jun 7, 2023
From: EWI
To: GENERAL ELECTRIC COMPANY
Reel/Frame 063883/0066 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Nov 18, 2021
From: VAZE, SUHAS PRABHAKAR; TRAPP, TIMOTHY; CAMPBELL, SCOTT SAGER; MAST, JONATHAN DAVID
To: GENERAL ELECTRIC COMPANY
Reel/Frame 058152/0067 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Nov 18, 2021
From: FIRESTONE, GREGORY CHRISTOPHER; STOTLER, TIMOTHY VERNON
To: EWI
Reel/Frame 058152/0135 →
Continuity (1)
Related Publication 20230151735A1 · May 18, 2023