Blade-Reinforcement Pairing to Minimize Assembly Defects

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Solution Overview

Problem

The assembly of composite material blades with titanium leading edge reinforcements is a time-consuming process often requiring manual sanding to correct production defects, which can degrade the mechanical performance of the final part and may not fully address assembly issues.

Innovation Solution

A method that estimates a defect indicator for each pair of parts to minimize the need for machining operations by optimizing the pairing of blades and leading edge reinforcements, using geometric characteristics and predictive models to identify feasible assemblies without sanding, and implementing a linear assignment problem to assign parts that minimize total defects.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Ease of manufacture

If manual sanding is performed to correct production defects, then assembly feasibility is improved, but mechanical performance is degraded and time is increased

Engineering Contradiction:
Improveassembly feasibilityVSAvoidmechanical performance
Core Design Contradiction:
Ease of manufactureVSStrength

Solution Approach 1:

The patent performs preliminary actions by measuring geometric characteristics of parts before assembly and using predictive models to estimate defect indicators. This allows identification of parts that can be assembled without sanding, preventing the need for subsequent machining operations that would degrade mechanical performance.

Inventive Principle:
Principle #10Preliminary action

Solution Approach 2:

The patent replaces the mechanical sanding process with a computational approach using predictive models and optimization algorithms. By calculating defect indicators and optimizing part pairing, the system substitutes manual machining with automated selection, eliminating material removal and preserving mechanical integrity.

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

2Ease of manufacture

If manual sanding is performed to correct production defects, then assembly feasibility is improved, but production time is increased

Engineering Contradiction:
Improveassembly feasibilityVSAvoidproduction time
Core Design Contradiction:
Ease of manufactureVSLoss of time

Solution Approach 1:

The patent performs preliminary measurements of geometric characteristics and predictive estimations of defect indicators before assembly. This advance preparation enables direct assembly without time-consuming sanding operations, significantly reducing production time while ensuring assembly feasibility.

Inventive Principle:
Principle #10Preliminary action

Solution Approach 2:

The patent substitutes the time-consuming manual sanding process with automated computational methods including predictive models and optimization algorithms. This replacement eliminates the need for iterative trial-and-error sanding, dramatically reducing production time.

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

3Device complexity

If parts are selected without optimization, then assembly process is simple, but machining operations are required to enable assembly

Engineering Contradiction:
Improveassembly process complexityVSAvoidassembly feasibility
Core Design Contradiction:
Device complexityVSEase of manufacture

Solution Approach 1:

The patent implements a self-service system where the optimization algorithm automatically selects part pairs with minimal defect indicators. The system uses measured geometric characteristics and predictive models to autonomously identify compatible parts, eliminating the need for manual intervention or complex trial-and-error assembly processes.

Inventive Principle:
Principle #25Self-service

Solution Approach 2:

The patent replaces manual part selection and assembly trial-and-error processes with automated computational optimization. The system uses algorithms to calculate defect indicators and determine optimal part pairings, substituting human judgment and manual adjustment with automated intelligent selection.

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

4Ease of manufacture

If sanding is performed to correct production anomalies, then assembly possibility is improved, but material is removed and quality is degraded

Engineering Contradiction:
Improveassembly possibilityVSAvoidassembly quality
Core Design Contradiction:
Ease of manufactureVSManufacturing precision

Solution Approach 1:

The patent performs preliminary measurements and predictive estimations to identify parts with compatible geometric characteristics before assembly. By selecting parts with low defect indicators, the system ensures high assembly quality without requiring material removal through sanding, thus preserving manufacturing precision.

Inventive Principle:
Principle #10Preliminary action

Solution Approach 2:

The patent substitutes the material-removing sanding process with a selection-based approach using predictive models. By calculating defect indicators and optimizing part pairing computationally, the system achieves high assembly quality without physical material removal, maintaining original part dimensions and surface integrity.

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

Data Source

PatentEP3555776B1Method, system and computer program for the selection of assembly parts
Publication Date: 2024.07.03 SAFRAN AIRCRAFT ENGINES SAS
  • EP3555776B1 patent drawingFigure 1
  • EP3555776B1 patent drawing
  • EP3555776B1 patent drawing

AI summary

The invention relates to a method for assembling parts (A, B) chosen respectively among a plurality of first parts and a plurality of second parts. The method comprises: - for each first part and each second part among the plurality of first parts and the plurality of second parts, estimating (CST) a defectiveness indicator of the assembly of the first part with the second part;- for a batch of N assemblies to be produced, assigning (AFF) N first parts among the plurality of first parts to N second parts among the plurality of second parts, in order to constitute N pairs ({Ai, Bj}) of a first part and a second part, said assignment being carried out so that said N pairs minimise a total assembly defectiveness. Application to the assembly of a blade and a leading edge reinforcement.