Aircraft Engine Part Machining with 3D Reference Alignment

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Solution Overview

Problem

Existing methods for manufacturing aircraft engine parts face challenges in establishing a common coordinate system for complex parts with multiple precision features, particularly when machining reference features are obstructed by fixtures, leading to high costs and imprecision.

Innovation Solution

A method involving the creation of a tri-dimensional model to determine the geometrical relationship between machining and setup reference features, using a computer measurement machine to measure and compute the position and orientation of the machining reference feature, and applying a coordinate transformation to correct the CNC machine's coordinate system.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Manufacturing precision

If a common coordinate system is established for complex parts with multiple precision features, then manufacturing precision is improved, but device complexity increases due to the need for multiple fixtures and coordinate transformations

Engineering Contradiction:
Improveprecision featuresVSAvoidfixture and coordinate system complexity
Core Design Contradiction:
Manufacturing precisionVSDevice complexity

Solution Approach 1:

A reference feature is introduced as an intermediary element that connects the machining feature and setup feature. The reference feature serves as a common coordinate system basis, allowing precise transformation between different feature coordinate systems without requiring complex multi-fixture arrangements. The reference feature acts as a mediator that simplifies the coordinate transformation process while maintaining manufacturing precision.

Inventive Principle:
Principle #24Intermediary (Mediator)

Solution Approach 2:

The invention creates a digital model (copy) of the part containing all features including the reference feature. This digital representation allows virtual establishment of coordinate systems and transformations before actual machining, reducing the need for physical trial-and-error with complex fixtures. The digital copy enables precise calculation of coordinate transformations without physical complexity.

Inventive Principle:
Principle #26Copying

2Manufacturing precision

If high-precision fixtures are used to maintain coordinate accuracy, then manufacturing precision is improved, but manufacturing cost increases

Engineering Contradiction:
Improvecoordinate system accuracyVSAvoidmanufacturing cost
Core Design Contradiction:
Manufacturing precisionVSEase of manufacture

Solution Approach 1:

The invention replaces expensive high-precision physical fixtures with a digital model containing all geometric information. The coordinate transformations are calculated mathematically from the digital model rather than being physically enforced by costly precision fixtures. This digital copying approach maintains coordinate accuracy while significantly reducing manufacturing costs.

Inventive Principle:
Principle #26Copying

Solution Approach 2:

The invention changes the approach from physical parameter control (fixture precision) to digital parameter control (coordinate transformation calculations). By transforming the problem from a physical precision maintenance issue to a computational geometry issue, the need for expensive high-precision fixtures is eliminated while maintaining the required coordinate accuracy.

Inventive Principle:
Principle #35Parameter changes

3Ease of manufacture

If multiple machining operations are performed on different fixtures, then ease of manufacture is improved, but measurement precision deteriorates due to difficulty in establishing common coordinate system

Engineering Contradiction:
Improvemachining operabilityVSAvoidcoordinate system alignment
Core Design Contradiction:
Ease of manufactureVSMeasurement precision

Solution Approach 1:

The reference feature serves as a persistent intermediary that remains consistent across multiple machining operations and fixtures. All coordinate transformations are referenced to this common reference feature, ensuring that measurements and machining on different fixtures can be accurately correlated. This mediator approach maintains measurement precision while allowing operational flexibility.

Inventive Principle:
Principle #24Intermediary (Mediator)

Solution Approach 2:

The reference feature and its associated coordinate system serve multiple functions across different machining operations and fixtures. Rather than requiring separate coordinate systems for each fixture or operation, the universal reference feature enables a single coordinated approach to multiple machining tasks, maintaining measurement precision while improving ease of manufacture.

Inventive Principle:
Principle #6Universality (Multi-functionality)

Data Source

PatentEP4660726A1Method of manufacturing a part of an aircraft engine, and system therefor
Publication Date: 2025.12.10 PRATT & WHITNEY CANADA CORP
  • EP4660726A1 patent drawingFigure 1
  • EP4660726A1 patent drawingFigure 2
  • EP4660726A1 patent drawingFigure 3

AI summary

The method can include mounting the part (34) on a machining fixture (46), obtaining a geometrical relationship between a machining reference feature (42) of the part (34) and a setup reference feature (40) of the part (34), such as via a 3D model acquired by scanning, measuring a position and orientation of the setup reference feature (40) relative the machining fixture (46), computing a position and orientation of the machining reference feature (42) based on the geometrical relationship and on the measured position and orientation; and machining the target feature (44) of the part (34) relative to the computed position and orientation of the machining feature (42).