Abstract
Carbon Fibre Reinforced Polymers (CFRPs) are lightweight materials that make up 50% of the structural weight in aircraft like Airbus A350XWB and Boeing 787 Dreamliner [1]. Non-Destructive Evaluation (NDE) procedures are crucial during and after manufacturing to ensure the highest quality of important structures made from CFRPs such as wing covers, stabilizers, fuselage, and engine covers. Common NDE techniques include radiographic and eddy current testing, visual inspection, and Ultrasonic Testing (UT). Manual UT inspections using single ultrasonic transducers or Phased Array Ultrasonic Testing (PAUT) arrays are laborious and heavily influenced by human operators [2]. Automated NDE using industrial manipulators has accelerated the acquisition of ultrasonic data, but manual data interpretation still presents a bottleneck. An automated approach to data processing and interpretation would be beneficial, as data acquisition can take a few hours while data interpretation and quality report generation can take up to 6-8 hours. This paper proposes an automated Deep Learning (DL) algorithm based on autoencoder architectures that processes ultrasonic Bscan images. An unsupervised training approach was adopted to train the model to recognize anomalies in the data in the form of surface and subsurface defects. Data was captured from series of CFRP coupons of various thicknesses, ply orientation configurations, and surface finishes. Flat bottom holes of sizes 3,4,6,7, and 9 mm at depths of 1.5, 3, 4.5, 6, 7.5 mm were introduced in some of the CFRP samples. Training/testing data was acquired with an experimental setup that mimics the industrial process, with KUKA KR90 industrial manipulator delivering an Olympus RollerFORM-5L64 to the surface of the test piece. The array was excited in linear mode with unfocused 4 element sub-aperture, operating at frequency of 5 MHz. The roller probe was controlled by PEAK NDT MP6 ultrasonic controller, while vertical movement of KUKA KR90 was controlled with force-torque unit. This resulted in acquisition of 7500 individual B-scans. Several convolutional autoencoder models with varying latent space sizes were tested. Due to the nature of B-scans and the domain representation, hyperbolic tangent function was used as activation to retain pixel values between –1 and 1. Furthermore, different dimensionality reductions were explored such us max pooling with various square kernel sizes, max pooling with rectangular kernels, and standard convolutional layers. The combination of L1 and L2 losses was used to evaluate image reconstruction performance of the decoder. To prevent overfitting and improve convergence, we used the combination of batch normalisation layers, learning rate schedulers, momentum, and weight decays for the ADAM optimizer. This automated NDT scanning combined with DL algorithm enabled swift and accurate analysis of ultrasonic B-scans. The algorithm completes analysis of single B-scan frame of 1024 by 64 pixels in 13.6 ms. This approach is showing a major improvement in the data interpretation time and defect detection success rate. [1] Slayton R, Spinardi G. Radical innovation in scaling up: Boeing’s Dreamliner and the challenge of socio-technical transitions. Technovation. 2016 [2] Ali et al. The reliability of defect sentencing in the manual ultrasonic inspection. NDT and E International. 2012
Original language | English |
---|---|
Publication status | Published - 12 Sept 2023 |
Event | 60th Annual British Conference on NDT - Northampton Town Centre Hotel, Northampton, UK , Northampton, United Kingdom Duration: 12 Sept 2023 → 14 Sept 2023 https://www.bindt.org/events-and-awards/ndt-2023/ |
Conference
Conference | 60th Annual British Conference on NDT |
---|---|
Abbreviated title | BINDT 2023 |
Country/Territory | United Kingdom |
City | Northampton |
Period | 12/09/23 → 14/09/23 |
Internet address |
Keywords
- anomaly detection
- Machine Learning
- NDT
- composite materials
- deep learning