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航空多层铆接结构内层裂纹的远场涡流检测

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多层铆接结构是飞机机身蒙皮与型材的主要结构.由于周期性载荷作用,其内部型材等承力部位易产生疲劳裂纹,该位置隐蔽性强,采用目视或常规无损检测技术难以检测出这些缺陷.而远场涡流检测技术可检测埋藏深度大的缺陷,采用该技术对飞机多层铆接结构的内层裂纹进行检测.结果表明:选择合适的检测频率时,检测信号阻抗的幅值与裂纹深度、检测信号阻抗的相位角与裂纹埋藏深度均呈良好的线性关系,对于确定的被检材料和检测传感器,得出的拟合公式可为裂纹损伤的定位、定量检测提供理论参考依据,从而获得裂纹的准确信息,实现裂纹损伤的准确定位和定量检测.
The far-field eddy current detection of inner layer crack of aviation multilayer riveted structures
The multilayer riveted structure is the main structure of aircraft fuselage skin and profiles.Due to periodic loading,fatigue cracks are prone to occur in load-bearing parts such as internal profiles,which are highly concealed and difficult to detect using visual and conventional nondestructive testing techniques.The far-field eddy current detection technology can detect defects with a large burial depth,so it was applied to the inner layer crack detection of aircraft multilayer riveted structures.The results indicated that the amplitude of the detection signal impedance had a good linear relationship with the crack depth,and the phase angle of the detection signal impedance had a good linear relationship with the crack burial depth by selecting an appropriate detection frequency.For the determined tested material and detection sensor,the fitting formula obtained can provide a theoretical reference for the localization and quantitative detection of crack damage,thus obtaining accurate information of cracks and achieving accurate localization and quantitative detection of crack damage.

multilayered structureinner layer crackfar field eddy current testingimpedance amplitudeimpedance phase angle

李小丽、陈新波、王正、王泽帅、宋凯

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海军航空大学青岛校区航空机械工程与指挥系,青岛 266041

中国海洋大学信息科学与工程学部,青岛 266100

92329部队,葫芦岛 125100

南昌航空大学无损检测技术教育部重点实验室,南昌 330063

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多层结构 内层裂纹 远场涡流检测 阻抗幅值 阻抗相位角

2024

无损检测
中国机械工程学会 上海材料研究所

无损检测

CSTPCD
影响因子:0.558
ISSN:1000-6656
年,卷(期):2024.46(3)
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