Vehicle-Borne Surface Inspection With Image-Guided Tactile Sensing

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Solution Overview

Problem

Conventional surface inspection methods for large-scale components, such as aircraft fuselages, are time-consuming and prone to inconsistency due to human error, and existing sensors lack the accuracy to detect small defects like scratches and gouges efficiently.

Innovation Solution

A two-stage inspection method using image sensors to predict defects and tactile sensors to confirm and measure them, where image sensors provide initial detection and tactile sensors verify defects with high precision, optimizing coverage and accuracy.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Measurement precision

If a sensor with small field of view is used for surface inspection, then measurement precision is improved, but productivity deteriorates due to impracticable sweeping across large surfaces

Engineering Contradiction:
Improvedefect detection accuracyVSAvoidinspection speed
Core Design Contradiction:
Measurement precisionVSProductivity

Solution Approach 1:

The inspection process is divided into two segments: a first sensor (image sensor) performs a first inspection to identify candidate defects, and a second sensor (tactile sensor) performs a second inspection to confirm and characterize them. This segmentation allows the system to efficiently screen large areas while maintaining high measurement precision for confirmed defects.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The first sensor performs a broader, less precise inspection to identify candidate defects, applying partial action to the entire surface. The second sensor then applies excessive action (more precise measurement) only to the candidate defects identified by the first sensor, rather than inspecting every point on the surface with high precision.

Inventive Principle:
Principle #16Partial or excessive action

2Productivity

If a sensor with large field of view is used to cover large surfaces, then productivity is improved, but measurement precision deteriorates due to insufficient accuracy for small defects

Engineering Contradiction:
Improveinspection coverageVSAvoiddefect measurement accuracy
Core Design Contradiction:
ProductivityVSMeasurement precision

Solution Approach 1:

The inspection system uses two different sensors with different field of view characteristics. The first sensor (image sensor) has a larger field of view for efficient coverage, while the second sensor (tactile sensor) has a smaller field of view for precise measurement of candidate defects.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The system replaces a single mechanical scanning approach with a multi-sensor system that combines optical imaging (first sensor) with tactile sensing (second sensor), allowing each sensor to perform its optimized function.

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

3Productivity

If laser-line systems or structured light scanners are used for defect inspection, then productivity is improved through automated scanning, but measurement precision deteriorates due to inability to measure sharp discontinuities with sufficient accuracy

Engineering Contradiction:
Improveautomated inspection capabilityVSAvoidsharp discontinuity measurement accuracy
Core Design Contradiction:
ProductivityVSMeasurement precision

Solution Approach 1:

The system replaces optical scanning methods (laser-line systems, structured light scanners) with tactile sensing (second sensor) for the confirmation and characterization stage, as tactile sensors can directly contact and measure sharp discontinuities with the required precision.

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

Data Source

PatentUS20250388339A1Multimodal inspection of large-scale surfaces using vehicle-borne sensors
Publication Date: 2025.12.25 THE BOEING CO
  • US20250388339A1 patent drawing
  • US20250388339A1 patent drawing
  • US20250388339A1 patent drawing

AI summary

The present disclosure provides a method of inspection of a surface of an aerodynamic structure. The method includes acquiring image(s) of the surface using image sensor(s) disposed adjacent to the surface, and determining, using the image(s) applied to a model, predicted defect(s) of the surface and corresponding location information. The method further includes controlling, using the location information, the position of tactile sensor(s) disposed adjacent to the surface to acquire dimensioning information for at least a first predicted defect of the predicted defect(s). The method further includes characterizing the first predicted defect using the dimensioning information.