BD-YOLO:一个基于深度学习的航空发动机孔探图像叶片损伤检测模型OA
BD-YOLO:A Deep Learning-Based Model for Blade Damage Detection in Aero-engine Borescope Images
针对航空发动机孔探图像叶片损伤方向任意且细长损伤易引入过多背景干扰、导致定位精度下降的问题,本文提出一种基于改进You only look once version 8(YOLOv8)的旋转目标检测模型BD-YOLO.首先,设计融合跨阶段连接(Cross stage partial,CSP)与密集连接扩张卷积模块(Receptive field enhancement module,RFEM)的小目标检测跨阶段局部感受野增强模块(Cross stage partial receptive field enhancement module,CSRFEM),增强对细小损伤的特征提取能力.其次,在颈部网络引入改进的双向特征金字塔网络SimBiFPN,实现多尺度特征的高效融合.最后,在头部网络增设专用小目标检测头,提升小尺寸损伤的识别精度.实验结果表明,BD-YOLO的平均精度均值(Mean average precision,mAP)50、mAP75和mAP50~95分别达到98.6%、84.3%和63.3%,检测速度为34帧/s,能够实现叶片损伤的高精度实时检测.
To address the issues in aero-engine borescope images,such as the arbitrary orientation of blade damage and the tendency for slender damage to introduce excessive background interference,leading to reduced localization accuracy,this paper proposes a rotated object detection model,BD-YOLO,based on an improved You Only Look Once version 8(YOLOv8).Firstly,a small object detection module named cross stage partial receptive field enhancement module(CSRFEM),which integrates the cross stage partial(CSP)and receptive field enhancement module(RFEM),is designed to enhance feature extraction capabilities for minor damages.Secondly,an improved bidirectional feature pyramid network,SimBiFPN,is introduced into the neck network to achieve efficient multi-scale feature fusion.Finally,a dedicated small object detection head is added to the head network to improve the recognition accuracy of small-sized damages.Experimental results demonstrate that BD-YOLO achieves mean average precision(mAP)50,mAP75,and mAP50-95 values of 98.6%,84.3%,and 63.3%,respectively,with a detection speed of 34 frames per second,enabling high-precision real-time detection of blade damage.
徐超;王文哲;蒋增华;冷晟;王静秋
南京航空航天大学机电学院,南京 210016南京航空航天大学机电学院,南京 210016中国航发湖南动力机械研究所,株洲 412002南京航空航天大学机电学院,南京 210016南京航空航天大学机电学院,南京 210016
航空航天
航空发动机孔探检测YOLOv8叶片损伤目标检测
aeroengineborescope detectionyou only look once version 8(YOLOv8)blade damageobject detection
《南京航空航天大学学报(自然科学版)》 2026 (2)
372-379,8
直升机动力学全国重点实验室2024年度科技创新基金(KY-1003-2024-0027).
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