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February 26, 2026Scientific Reports1 citationsOpen Access

High-precision non-destructive blade surface inspection via self learning transformer networks

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PKPriyadharshini KannusamyDGD. GayathriSMS. Mirdula

Key Points

  • The aim is to enhance the accuracy of defect detection in jet engine turbine blades using a deep learning model.
  • Proposed an automated defect detection system utilizing a deep learning model.
  • Captured and pre-processed high-resolution images of turbine blade surfaces.
  • Augmented images to address varying surface conditions.
  • Achieved 98.4% accuracy and 97.9% precision in defect detection.
  • Obtained 98.7% recall and an F1-score of 98.3%.
  • Demonstrated a mean Average Precision (mAP) of 97.6% on 172 blade images.

Abstract

Accurate identification of defects in Jet Engine Turbine and compressor blade surface plays a vital role in ensuring engine efficiency, safety and secure life. Traditional detection techniques were manual and consumed more time, error prone and need of specialized experts. To address these challenges, this work proposes an automated defect detection system using Swin Transformer Based Deep learning model. High resolution blade surface images were captured, pre-processed and augmented to improve robustness with varying surface condition. The novelty of the proposed work is that it adapts the Swin Transformer architecture to the specific challenges of turbine and compressor blade surfaces and it can detect micro-scale defects with high fidelity, by detecting both local and global features. Experimental results demonstrated that the proposed Swin transformer model produces high detection performance compared to the conventional CNN model with an accuracy of 98.4%, precision of 97.9%, recall of 98.7%, F1-score of 98.3% and mean Average Precision (mAP) of 97.6% on a dataset consisting of 172 high-resolution turbine and compressor blade images. The performance of the proposed method indicate that Swin Transformer model is an efficient tool for Non-Destructive Inspection of jet engine turbine and compressor blade surface which can be integrated into automated maintenance systems for better reliability and minimized operational risks.

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Cite This Study

Kannusamy et al. (2026) studied this question.

synapsesocial.com/papers/699f95951bc9fecf3dab371ahttps://doi.org/10.1038/s41598-026-41373-x
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