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材料导报  2020, Vol. 34 Issue (Z1): 581-584    
  高分子与聚合物基复合材料 |
直升机复合材料结构基于振动健康监测的研究进展
朱洪艳, 吴宝昌, 林长亮, 王金亮, 王刚
哈尔滨飞机工业集团有限责任公司,哈尔滨 150066
Research Progress on Vibration Based Structural Health Monitoring onHelicopter Composite Material Structures
ZHU Hongyan, WU Baochang, LIN Changliang, WANG Jinliang, WANG Gang
Harbin Aircraft Industry(group) Co., Ltd., of AVIC, Harbin 150066, China
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摘要 直升机纤维增强树脂基复合材料结构对冲击、疲劳应力等引起的内部分层、裂纹缺陷非常敏感,它会使复合材料结构在没有预警的情况下发生灾难性的失效。因此,对能够及时检测出复合材料内部分层损伤、裂纹方法的需求愈益急迫。而结构健康监测能够实现对复合材料结构的实时原位监测,其中基于振动的健康监测技术使用了振动特性(阻尼、模态、固有频率),它可以很容易地连续从直升机结构的振动中提取,是一种非常有应用前景的结构健康监测方法。本文综述了直升机复合材料结构基于振动特性的健康监测技术的研究进展。
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朱洪艳
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王金亮
王刚
关键词:  复合材料  直升机  振动损伤  健康监测    
Abstract: Helicopterfiber reinforced resin composite material structures are quite sensible to the internal delamination and cracks induced by impact and fatigue stress. It can make composite material structure damage catastrophically without any prewarning. Therefore, the requirement for the method that can detect delamination and cracks in the composite material structures in time is more and more imperative. And that structural health monitoring(SHM) can implement monitoring on compo-site material structures in real time and in-situ. Vibration based SHM utilizes vibration properties, such as damping, modal and natural frequency, which can be easily and continuously extract from the vibration of helicopter composite material structures. It is a SHM method which will hold application foreground greatly. The vibration based SHM technologies of helicopter composite material structures are reviewed.
Key words:  composite material    helicopter    vibration    failure    health monitoring
                    发布日期:  2020-07-01
ZTFLH:  TB33  
作者简介:  朱洪艳,哈尔滨飞机工业集团有限责任公司设计员,高级工程师,博士。2010年毕业于哈尔滨工业大学材料科学与工程学院,现在专业为航空结构强度分析。
引用本文:    
朱洪艳, 吴宝昌, 林长亮, 王金亮, 王刚. 直升机复合材料结构基于振动健康监测的研究进展[J]. 材料导报, 2020, 34(Z1): 581-584.
ZHU Hongyan, WU Baochang, LIN Changliang, WANG Jinliang, WANG Gang. Research Progress on Vibration Based Structural Health Monitoring onHelicopter Composite Material Structures. Materials Reports, 2020, 34(Z1): 581-584.
链接本文:  
http://www.mater-rep.com/CN/  或          http://www.mater-rep.com/CN/Y2020/V34/IZ1/581
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