Gas Turbine Recontouring Using Section-Wise ML Machining Offsets

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Solution Overview

Problem

The recontouring process for gas turbine engine components is currently iterative and time-consuming, requiring manual intervention due to significant part-to-part variation and uncertainties in the recontouring system, making automation unsuccessful.

Innovation Solution

A system utilizing machine-learned models, such as deep neural networks, to determine machine offsets for each section of the component, allowing for real-time adjustment of the material removal tool path, thereby automating the recontouring process and reducing cycle time.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Manufacturing precision

If manual inspection and iterative machining is used to determine machine offset, then the recontouring process can handle part-to-part variation and system uncertainties, but the process becomes time-consuming and cannot be automated

Engineering Contradiction:
Improverecontouring accuracyVSAvoidregeneration cycle time
Core Design Contradiction:
Manufacturing precisionVSLoss of time

Solution Approach 1:

The system performs preliminary scanning of the component to capture its actual geometry and condition before machining begins. This advance information is used to pre-calculate the machine offset values, eliminating the need for iterative trial-and-error machining and significantly reducing cycle time while maintaining precision

Inventive Principle:
Principle #10Preliminary action

Solution Approach 2:

The patent replaces manual inspection and mechanical measurement methods with automated optical scanning and computer-based calculation systems. This substitution enables rapid data acquisition and processing, allowing the system to determine machine offsets automatically without manual intervention, thus reducing time loss while achieving high manufacturing precision

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

2Manufacturing precision

If manual intervention is used to determine machine offset, then the process can account for significant part-to-part variation and geometrical shape complexities, but the extent of automation is reduced

Engineering Contradiction:
Improvemachine offset accuracyVSAvoidrecontouring automation level
Core Design Contradiction:
Manufacturing precisionVSExtent of automation

Solution Approach 1:

The system enables the recontouring process to be self-sufficient by automatically scanning the component, calculating the appropriate machine offset values based on the scanned data and stored reference geometry, and adjusting the machining operations without requiring manual measurement or intervention. This self-service capability maintains high automation levels while ensuring accurate handling of part variations and geometrical complexities

Inventive Principle:
Principle #25Self-service

3Manufacturing precision

If iterative inspection and machining is performed, then the desired specifications can be achieved, but the productivity is reduced due to repeated cycles

Engineering Contradiction:
Improvecomponent specification complianceVSAvoidrecontouring throughput
Core Design Contradiction:
Manufacturing precisionVSProductivity

Solution Approach 1:

The system performs all necessary measurements and calculations before machining begins. By scanning the component and pre-determining the machine offset values in advance, the system eliminates the need for repeated inspection-machining cycles, thereby maintaining specification compliance while significantly improving productivity through a single-pass machining operation

Inventive Principle:
Principle #10Preliminary action

Data Source

PatentUS10947849B2Systems and methods for recontouring engine components
Publication Date: 2021.03.16 GENERAL ELECTRIC CO
  • US10947849B2 patent drawing
  • US10947849B2 patent drawing
  • US10947849B2 patent drawing

AI summary

Systems and methods that include and/or leverage a cluster of machine-learned models to recontour components of gas turbine engines are provided. In one exemplary aspect, the systems and methods leverage a cluster of machine-learned models to predict repair machining offsets for certain sections of the component that can be used to adjust or set a material removal tool path.