Fastener Joint Modeling for Fatigue Cracking Prevention

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Solution Overview

Problem

Existing modeling solutions for joints with fasteners are either manual or of low fidelity, failing to accurately capture three-dimensional contact interactions and prevent costly cracking during full-scale fatigue tests.

Innovation Solution

A method and system for modeling joints with fasteners that involves receiving input parameters, calculating second-level parameters, building component models, subtracting fastener bores, generating an assembly model, applying boundary conditions and loads, and generating an input file suitable for finite element analysis.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Ease of manufacture

If manual modeling methods are used, then flexibility in model building is maintained, but modeling time increases and productivity decreases

Engineering Contradiction:
Improvemodeling flexibilityVSAvoidmodeling speed
Core Design Contradiction:
Ease of manufactureVSProductivity

Solution Approach 1:

The system enables automated self-modeling of joint assemblies by automatically generating component models, fastener models, and assembly models from input parameters without requiring manual intervention for each modeling step

Inventive Principle:
Principle #25Self-service

Solution Approach 2:

The system uses parameter-driven modeling where changing input parameters automatically updates the entire model including geometry, material properties, boundary conditions, and analysis settings, allowing rapid exploration of design variations

Inventive Principle:
Principle #35Parameter changes

2Device complexity

If low fidelity modeling is used, then modeling complexity is reduced, but stress prediction accuracy deteriorates

Engineering Contradiction:
Improvemodeling complexityVSAvoidstress prediction accuracy
Core Design Contradiction:
Device complexityVSMeasurement precision

Solution Approach 1:

The system segments the joint assembly into distinct component models and fastener models that can be independently defined and assembled, allowing detailed representation of complex three-dimensional contact interactions while maintaining organized model structure

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The system transitions from two-dimensional simplifications to three-dimensional modeling, capturing the full spatial complexity of fastener-structure contact interactions and enabling accurate stress predictions at fastener locations

Inventive Principle:
Principle #17Another dimension (Dimensionality change)

3Reliability

If designs are changed during certification testing, then cracking problems can be addressed, but program time and costs increase

Engineering Contradiction:
Improvecracking mitigationVSAvoidprogram schedule
Core Design Contradiction:
ReliabilityVSLoss of time

Solution Approach 1:

The system performs preliminary virtual testing and stress analysis before physical certification tests, identifying potential cracking issues and optimizing designs in advance to prevent problems during actual testing

Inventive Principle:
Principle #10Preliminary action

Solution Approach 2:

The system uses finite element analysis results to provide feedback on stress concentrations and potential failure points, enabling iterative design optimization that prevents cracking issues before they manifest in physical testing

Inventive Principle:
Principle #23Feedback

Data Source

PatentUS20250068780A1Modeling joints with fasteners
Publication Date: 2025.02.27 THE BOEING CO
  • US20250068780A1 patent drawing
  • US20250068780A1 patent drawing
  • US20250068780A1 patent drawing

AI summary

A method for modeling joints with fasteners includes receiving multiple input parameters of multiple components connectable with one or more fasteners; calculating multiple second level parameters with a computer based on the input parameters; building multiple component models of the components absent the one or more fasteners based on the second level parameters; subtracting multiple bolt bores from the component models; and generating an assembly model by combining the component models with one or more fastener models of the one or more fasteners in the bolt bores. The method further includes applying multiple boundary conditions to the assembly model; applying multiple loads to the assembly model under the boundary conditions to generate multiple analysis key words; and generating an input file based on the analysis key words. The input file is suitable for a finite element analysis.