复合材料科学与工程 ›› 2020, Vol. 0 ›› Issue (9): 74-78.

• 应用研究 • 上一篇    下一篇

航空复合材料多层蜂窝夹芯结构的空气耦合式超声检测技术研究

张继敏, 周晖, 刘奎   

  1. 中国商用飞机有限责任公司复合材料中心,上海200436
  • 收稿日期:2019-11-11 出版日期:2020-09-25 发布日期:2020-09-28
  • 作者简介:张继敏(1988-),男,硕士,工程师,主要从事复合材料结构无损检测技术方面的研究, zhangjimin@comac.cc。

STUDY ON MULTI-LAYER HONEYCOMB SANDWICH STRUCTURE OF AERONAUTICAL COMPOSITE BY AIR-COUPLED ULTRASONIC INSPECTION TECHNIQUE

ZHANG Ji-min, ZHOU Hui, LIU Kui   

  1. Commercial Aircraft Corporation of China Ltd., Composite Centre, Shanghai 200436, China
  • Received:2019-11-11 Online:2020-09-25 Published:2020-09-28

摘要: 采用基于穿透式异侧检测模式的空气耦合超声C扫描检测技术,对复合材料多层蜂窝夹芯结构进行无损检测研究。研究三层蜂窝垂直拼接固化后,蜂窝表面裸露状态下的空气耦合超声检测结果;同时研究三层蜂窝垂直拼接且粘接了表面蒙皮后的空气耦合超声检测结果,并与常规超声喷水穿透C扫描检测结果进行了对比分析。通过声束传播路径分析以及传统射线和CR检测,验证了空气耦合超声C扫描检测结果的适用性和可靠性。结果表明,在蜂窝表面裸露状态下的空气耦合超声检测无法实现全部粘接界面的脱粘检测,而在有表面蒙皮粘接的情况下,空气耦合超声检测方法相比于常规超声喷水穿透C扫描检测,可以不受蜂窝格拼接无法对齐影响,实现快速、有效地检测。

关键词: 复合材料, 多层蜂窝夹芯结构, 拼接界面, 空气耦合式超声检测

Abstract: The air-coupled ultrasonic C scan technique based on the penetrative opposite side detection mode was utilized to study the inspection of composite multi-layer honeycomb sandwich structure. The result of air-coupled ultrasonic inspection on the triple-layer honeycomb structure was study under the exposed state of honeycomb surface. Meanwhile, the result of air-coupled ultrasonic inspection on the triple-layer honeycomb structure was studied when the honeycomb surface was skinned and compared with the conventional water jet TTU result. The adaptation and reliability of the air-coupled ultrasonic C scan results were proved through the analysis of ultrasonic path and the detection of traditional rays and CR. It was shown that not all bonding interface defects could be detected by the air-coupled ultrasonic technique under the exposed state of honeycomb surface. However, when the honeycomb surface was skinned, compared with conventional water jet TTU, the air-coupled ultrasonic result was not affected by the honeycomb cell being not aligned. And the fast and effective inspection was realized.

Key words: composites, multi-layer honeycomb sandwich structure, bonding interface, air-coupled ultrasonic inspection

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