Non-destructive Inspection Model Generation for Composite Parts

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Solution Overview

Problem

Generating a non-destructive inspection model for composite parts is a complex and resource-intensive process, especially in aerospace applications, where physical internal inspection often requires destruction of the part, and existing methods struggle to efficiently utilize design model data for predicting acoustic wave responses.

Innovation Solution

A method and system that analyze design model files to determine properties of composite parts, such as ply and interply descriptions, to generate a non-destructive inspection model, using a computing platform with a processor and memory, including modules for design model file analysis and non-destructive inspection model generation, which enables the creation of accurate models for simulating acoustic wave propagation without physical testing.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If physical internal inspection methods are used on composite parts, then inspection can be performed, but the part must be destroyed

Engineering Contradiction:
Improveinspection capabilityVSAvoidpart integrity
Core Design Contradiction:
ReliabilityVSStrength

Solution Approach 1:

The patent creates a digital copy (virtual model) of the composite part from its design model, which can be inspected repeatedly without affecting the physical part. This virtual model replicates the acoustic wave propagation characteristics, allowing non-destructive inspection simulation and eliminating the need for destructive physical testing.

Inventive Principle:
Principle #26Copying

2Reliability

If traditional non-destructive inspection model generation methods are used, then inspection models can be created, but the process is complex and resource intensive

Engineering Contradiction:
Improveinspection model accuracyVSAvoidmodel generation efficiency
Core Design Contradiction:
ReliabilityVSProductivity

Solution Approach 1:

The patent performs preliminary actions by utilizing the design model data that already exists from the manufacturing process. By extracting material properties, geometry, and layup information from the pre-existing design model, the system eliminates the need for time-consuming physical measurements and setup, significantly accelerating the inspection model generation process while maintaining accuracy.

Inventive Principle:
Principle #10Preliminary action

3Loss of information

If design model data is not utilized for inspection model generation, then inspection models can be created using physical testing, but rich design data is wasted

Engineering Contradiction:
Improvedesign data utilizationVSAvoidinspection process complexity
Core Design Contradiction:
Loss of informationVSDevice complexity

Solution Approach 1:

The patent makes the design model serve multiple functions: it is used both for manufacturing the composite part and for generating the non-destructive inspection model. By extracting relevant information (material properties, geometry, layup sequence) from the design model, the system eliminates the need for separate physical characterization processes, reducing complexity while maximizing the utility of existing design data.

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

Data Source

PatentUS9152744B2Methods, systems, and computer readable media for generating a non-destructive inspection model for a composite part from a design model of the composite part
Publication Date: 2015.10.06 AIRBUS OPERATIONS (SAS)
  • US9152744B2 patent drawing
  • US9152744B2 patent drawing
  • US9152744B2 patent drawing

AI summary

Methods, systems, and computer readable media for generating a nondestructive inspection model are provided, where such methods, systems and computer readable media are particularly suitable for use with aerospace parts or components. The method can include occurring at a computing platform with a memory and a processor, and analyzing, by the processor, a design model file stored in the memory to determine one or more properties of a composite part, the design model file describing one or more physical characteristics of the composite part. The method also can include generating, by the processor, a non-destructive inspection model for the composite part based on the one or more properties of the composite part determined by analyzing the design model file.