Airfoil Repair Joining Using Oversized Weld Attachment Sections

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Solution Overview

Problem

Current methods for repairing airfoil components in gas turbine engines are time-consuming, expensive, and have low yield rates, especially when dealing with damaged blades or blisks, as they often require replacing entire components rather than just the damaged portion, which can be costly and complex.

Innovation Solution

An airfoil repair system that includes a locally or wholly oversized airfoil repair component with a repair attachment section designed to align and secure to a cropped airfoil using an electrode assembly for precise positioning and welding, reducing the need for hand tools and enhancing the quality and speed of the repair process through features like inert gas shielding and adaptive current control.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If traditional repair methods are used to repair airfoil components, then the repair process can handle complex damaged configurations, but the repair time increases and productivity decreases

Engineering Contradiction:
Improverepair success rateVSAvoidrepair speed
Core Design Contradiction:
ReliabilityVSProductivity

Solution Approach 1:

The airfoil repair component is divided into a body portion and a separate attachment section that can be independently positioned and joined to the cropped airfoil, allowing for modular repair that reduces complexity and time

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The attachment section is pre-configured with alignment features and positioning elements that enable direct attachment to the cropped airfoil without requiring extensive manual alignment or preparation work during the repair process

Inventive Principle:
Principle #10Preliminary action

2Adaptability or versatility

If traditional repair methods are used to repair airfoil components, then the repair can be performed on various damaged configurations, but the cost increases and resource consumption increases

Engineering Contradiction:
Improverepair capabilityVSAvoidmaterial waste
Core Design Contradiction:
Adaptability or versatilityVSLoss of substance

Solution Approach 1:

Instead of replacing entire airfoil components, the invention applies a localized attachment section only to the cropped portion of the airfoil where damage occurred, preserving the majority of the original component and reducing material waste

Inventive Principle:
Principle #3Local quality

Solution Approach 2:

The invention recovers value from cropped airfoils that would otherwise be discarded by providing a repair component that can be attached to the remaining viable portion, thereby reducing material waste and resource consumption

Inventive Principle:
Principle #34Discarding and recovering

3Ease of manufacture

If manual alignment and positioning methods are used, then the repair process can be performed with simple equipment, but the manufacturing precision decreases and alignment accuracy is poor

Engineering Contradiction:
Improveprocess simplicityVSAvoidalignment accuracy
Core Design Contradiction:
Ease of manufactureVSManufacturing precision

Solution Approach 1:

The attachment section incorporates pre-configured alignment features such as positioning protrusions or registration elements that automatically guide correct alignment with the cropped airfoil, eliminating the need for complex manual alignment procedures while maintaining high precision

Inventive Principle:
Principle #10Preliminary action

Solution Approach 2:

The invention replaces manual mechanical alignment methods with built-in geometric alignment features and positioning mechanisms that provide automatic, precise alignment through the attachment section's design

Inventive Principle:
Principle #28Mechanics substitution (Replace mechanical system)

4Strength

If complex joining procedures are used to attach repair components, then the joint strength can be ensured, but the device complexity increases and operation becomes difficult

Engineering Contradiction:
Improvejoint strengthVSAvoidjoining ease
Core Design Contradiction:
StrengthVSEase of operation

Solution Approach 1:

The joining process is segmented into simplified steps facilitated by the attachment section's design, which may include pre-drilled holes, built-in fastening features, or localized welding zones that reduce the complexity of the joining procedure while maintaining joint strength

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The attachment section incorporates self-aligning or self-securing features that reduce the need for complex external joining equipment or procedures, allowing for simpler operation while ensuring adequate joint strength through its design

Inventive Principle:
Principle #25Self-service

Applied Scientific Principles

This section explains which scientific principles are used to turn an abstract innovation direction into a practical engineering solution.

Function Achieved in This Case

The system improves the alignment and joining process, reducing repair time and costs while increasing the success rate of airfoil repairs by allowing for more accurate positioning and higher quality welds, even in complex configurations like blisks, and facilitates easier extraction of the repaired airfoil.

Implementation Method 1

passing current through the cropped airfoil electrode and the repair component electrode to join the airfoil repair component to the cropped airfoil

Methodology Applied
Scientific EffectResistive heating: Joule Heating

Implementation Method 2

US 2011/005075 relates to solid state resistance welding for airfoil repair

Methodology Applied
Scientific EffectSolid state resistance welding: Welding

Data Source

PatentEP4183977B1Airfoil joining apparatus
Publication Date: 2024.07.03 GENERAL ELECTRIC CO
  • EP4183977B1 patent drawingFigure 1
  • EP4183977B1 patent drawingFigure 2
  • EP4183977B1 patent drawingFigure 3A~3B

AI summary

Repair components, systems, and methods are provided. For example, an airfoil repair component (200) for attaching to a cropped airfoil (140) comprises a body (205) and a repair attachment section (242) for attaching the airfoil repair component (200) to the cropped airfoil (140) at a cropped airfoil attachment section (142), the repair attachment section (242) being oversized with respect to the cropped airfoil attachment section (142) such that the repair attachment section (242) has a repair chord length (cr) longer than a cropped chord length (cc) of the cropped airfoil attachment section (142) and a repair width (wr) wider than a cropped width (wc) of the cropped airfoil attachment section (142). An airfoil repair system (300) comprises the airfoil repair component (200), a repair component electrode (304) for receipt of the airfoil repair component (200), and a tooling assembly (344) for positioning the airfoil repair component (200) with respect to the cropped airfoil (140). The repair component electrode (304) comprises a removable insert (330) surrounding at least a portion of the airfoil repair component (200).