航空计算技术2024,Vol.54Issue(2) :32-36.

飞机线束装配螺栓螺距数量图像测量方法研究

Research on Image Measurement Method of Bolt Pitch Quantity in Aircraft Wire Harness Assembly

闫静 陆珊珊 张忆鑫
航空计算技术2024,Vol.54Issue(2) :32-36.

飞机线束装配螺栓螺距数量图像测量方法研究

Research on Image Measurement Method of Bolt Pitch Quantity in Aircraft Wire Harness Assembly

闫静 1陆珊珊 1张忆鑫1
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作者信息

  • 1. 南京航空航天大学,江苏 南京 210000
  • 折叠

摘要

飞机线束是电气线路互联系统(EWIS)的装配单元,重要的飞机线束常以线束捆的方式用P型金属带垫卡箍固定在飞机上.卡箍固定线束的装配质量检测要求之一是卡箍螺栓与螺母拧紧后,螺栓应露出螺母螺距数量大于规定值.为实现飞机线束装配检测智能化,提出一种基于图像自动识别P型卡箍螺栓伸出螺母螺距数量的方法.分析确立螺栓伸出螺母单侧牙顶中点为需要识别的图像特征点,并建立利用牙顶特征点计算螺距数量的公式;通过对图像进行预处理、边缘检测、轮廓提取及拟合、极值点检测等得到牙顶特征点个数;针对不同具体图像实例进行了实验验证.

Abstract

The aircraft wiring harness is the assembly unit of the Electrical Wiring Interconnection Sys-tems(EWIS).The important harnesses are often secured by P-type metal cushion clamps in bundles.One of the quality inspection requirements for assembly of clamped wire harnesses is that after tightening the clamp bolt and nut,the bolt should expose the nut by more than specified pitches.To achieve intelli-gent inspection of aircraft wiring harness assembly,a method was proposed for automatically identifying the number of pitches of the bolt protruding the nut in a P-type clamp based on image recognition.First-ly,the midpoints of the unilateral crests of the bolt extending the nut were built up as the image crest fea-ture points,and the formula for calculating the number of pitches using the crest feature points was estab-lished.Secondly,the number of crest feature points was obtained through image preprocessing,edge detec-tion,contour extraction and fitting,and extremum point detection.Finally,the two concrete image exam-ples were experimentally verified.

关键词

飞机线束/卡箍装配质量/螺纹螺距/数字化检测/图像处理

Key words

aircraft wiring harness/clamp assembly quality/pitch of thread/digital detection/image pro-cessing

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基金项目

国家商用飞机制造工程技术研究中心创新基金(SAMC13-JS-15-024)

出版年

2024
航空计算技术
中国航空工业西安航空计算技术研究所

航空计算技术

CSTPCD
影响因子:0.316
ISSN:1671-654X
参考文献量15
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