Turbine Component Holder With Self-Aligning Notches for X-Ray Imaging

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Solution Overview

Problem

Conventional methods for positioning turbine components for X-ray imaging are labor-intensive and lack precision, making it difficult to ensure uniform orientation and efficient inspection for micro-cracks and other internal damage.

Innovation Solution

A turbine component holder with 3D-printed notches that securely hold and orient turbine components at predefined angles, allowing multiple components to be imaged simultaneously with minimal manual intervention.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Ease of operation

If foam blocks are used to support turbine components, then the components can be held for imaging, but a significant amount of labor is required to ensure correct orientation and prevent movement

Engineering Contradiction:
Improvelabor required for positioningVSAvoidorientation precision
Core Design Contradiction:
Ease of operationVSManufacturing precision

Solution Approach 1:

The holder is designed with notches that automatically secure and orient turbine components through interference fit when inserted, eliminating the need for manual positioning adjustments and ensuring consistent orientation without requiring significant labor

Inventive Principle:
Principle #25Self-service

Solution Approach 2:

The holder uses interference fit—a specific type of mechanical connection where the component is slightly larger than the notch—to automatically secure components in the correct orientation, transforming the positioning process from manual adjustment to automatic self-alignment

Inventive Principle:
Principle #35Parameter changes

2Manufacturing precision

If manual positioning methods are used, then turbine components can be oriented for imaging, but the process is time-consuming and lacks uniformity

Engineering Contradiction:
Improveorientation uniformityVSAvoidimaging speed
Core Design Contradiction:
Manufacturing precisionVSProductivity

Solution Approach 1:

The holder is divided into multiple notches, each designed to hold a turbine component in a specific predefined orientation. This segmentation allows multiple components to be positioned simultaneously with uniform orientation, enabling parallel processing and increasing imaging productivity

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The notches are pre-configured with specific geometries that automatically orient components in the correct position upon insertion, eliminating the need for time-consuming manual adjustment during the imaging process and ensuring uniform orientation across all components

Inventive Principle:
Principle #10Preliminary action

3Reliability

If conventional positioning methods are used, then turbine components can be held for imaging, but precision and consistency in orientation are difficult to ensure

Engineering Contradiction:
Improveorientation consistencyVSAvoidpositioning system complexity
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

Each notch in the holder is designed with specific local geometric features that correspond to the shape of turbine components. These localized features ensure that each component is secured in a precise, repeatable orientation, improving reliability without requiring complex overall system design

Inventive Principle:
Principle #3Local quality

Data Source

PatentEP4592506A1Turbine component holder for imaging
Publication Date: 2025.07.30 CHROMALLOY GAS TURBINE LLC
  • EP4592506A1 patent drawingFigure 1
  • EP4592506A1 patent drawingFigure 2
  • EP4592506A1 patent drawingFigure 3

AI summary

A holder configured to hold a turbine component in position for internal imaging includes a main body configured to support one or more turbine components and one or more holding spaces in in the main body. Each holding space being configured to retain a corresponding turbine component. Each of the one or more holding spaces is configured to automatically secure and orient the corresponding turbine component upon the turbine component being inserted into the holding space.