共查询到18条相似文献,搜索用时 344 毫秒
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提出一种采用埋入式光纤传感器无损检测复合材料结构状态的新方法。将两种结构简单的新颖光纤传感网络埋入飞机的层状复合材料垂直尾翼试件,对结构内应变、应力以及由于低频部冲击造成的损伤等状态参数进行检测,实验结果显示了该方法的可行性。 相似文献
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针对目前现有视觉传感器标定方法专业性强,靶标制作复杂的现状,以及焊后视觉检测用复合光源视觉传感器的应用环境特点,提出一种简便的利用平面模板与改进型锯齿靶标组合的视觉传感器标定方法。该方法首先利用基于平面模板两步法原理开发的Matlab标定工具箱来完成摄像的内部参数与外部参数标定,然后利用获取的内部参数,结合改进的锯齿靶标方法来实现传感器的结构参数标定。试验结果表明,该方法能够实现对复合光源焊后视觉传感器的精确标定,并且标定过程简单方便。 相似文献
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研究了粘贴式光纤布拉格光栅应变传感器对柔性梁的动态响应特性,并用压电陶瓷加速度传感器作对照。结果表明,粘贴式光纤布拉格光栅传感器具有和压电陶瓷加速度传感器一致的动态响应特性,是一种高灵敏度的用于结构健康监测的新型在线监测技术。论文从应变传感模型的角度分析了光纤光栅应变传感器的轴向应变检测特性的理论基础。 相似文献
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提出了一种磁记忆和涡流集成检测的快速方法,利用磁记忆和涡流检测信号,实现铁磁性材料表面和近表面应力集中和缺陷的检测,同时设计了集成检测系统和传感器,对模拟试块分别进行了四种状态的检测试验。结果表明,集成方法可以实现铁磁性试块应力集中和裂纹的检测,比单一检测能获取更全面的有用信号。 相似文献
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针对煤矿井下液压支架顶梁受外载合力状态监测方面的空缺问题,提出一种新型传感器感知方法,在监测立柱和平衡缸工作状态的前提下,探究不同角度剪切力对顶梁与掩护梁铰接处销轴应变的影响规律。使用多体动力学分析软件ADAMS对特定高度下两柱式液压支架三维模型进行模拟仿真,分析在支架极限载荷区顶梁连接销轴处铰接力、液压缸工作阻力与顶梁外载荷之间的关系,并进一步建立销轴受力三维模型,探索盲孔应变相应的变化规律。结果表明:在顶梁不同承载位置受外载合力达到极限水平时,销轴传感器支撑力角度区间变化规律明显,且剪切力对销轴盲孔应变变化影响较大,依据空间力平衡关系分析各传感器数据即可反解出支架顶梁负载状态。 相似文献
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大型结构件的焊接应力应变测试一直是研究的热点和难点.针对目前大型结构件焊接应力应变在线实时监测手段存在不耐高温和测试精度不高等问题,提出了一种基于光纤Bragg光栅(FBG)传感器的焊接应力应变在线实时监测方法.采用该方法构建了基于FBG传感器的焊接应力应变在线监测系统原理,并对LD10铝合金板材进行了TIG堆焊的温度... 相似文献
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传统的无位置传感器控制通过电机的反电动势来检测电机位置,可以有效降低硬件成本和占用面积,但存在启动困难和启动反向转动等问题。基于此,提出一种施加脉冲电流并检测绕组电感变化量的方法来确定初始转子位置,并配合FOC算法控制BLDC电机平稳高效运行。分析控制超前角优化和电机的抗负载扰动性能,进一步提高整个系统的运行效率和抗干扰能力。最后搭建实验样机对其进行实验验证,实验结果表明该样机能够在无位置传感器的前提下实现无反向转动且高效可靠的启动,同时在FOC闭环控制下实现高效运作。 相似文献
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介绍了在机床上用光纤传感器检测表面粗糙度的原理和一系列试验结果,探讨了检测仪的设计要点以及在线检测技术存在的问题,如光纤探头的结构、传感器的装夹与定位、仪器的元器件选择、仪器的标定、切削液和测量距离变化的影响等,提出了解决或改进的办法,研究结果表明,该检测系统具有结构简单、工作效率高、抗干扰能力强等特点,适用于机床上静态条件下的快速检测和动态条件下的实时监测,有利于提高加工质量和生产效率. 相似文献
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H.N. Jones N. Lagakos S.G. Lambrakos P.P. Trzaskoma-Paulette 《Journal of Materials Engineering and Performance》2008,17(1):64-69
A general method is presented for in situ assessment of mechanical strength degradation of materials or components using an
embedded interferometric fiber-optic strain sensor. This method is based on the analysis of acoustic signature responses resulting
from mechanical excitation of the subject under investigation. Acoustic signature responses are observed by monitoring light
intensity changes resulting from the combination of light signals traveling through the embedded optical fiber (experiencing
dimensional changes through vibrational excitation) and an external optical fiber. This paper discusses the fundamental aspects
of the methodology and its potential investigational pathways and applications. A case study, addressing unobservable corrosion
related degradation of aircraft fuselage lap joints is presented as an example for retrieving information and to demonstrate
the correlations between material properties and fiber-optic interferometric measurements. The application of inverse method
analysis for the interpretation of response signals is also discussed.
P.P. Trzaskoma-Paulette is presently working as an Independent Consultant 相似文献
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Monitoring of fibre reinforced composites with embedded optical fibre Bragg sensors, with application to filament wound pressure vessels 总被引:1,自引:0,他引:1
Tests carried out on bare optical fibres with a Bragg sensor show the feasibility of using these sensors for strain sensing. They have been embedded into simple composite laminates and have been subjected to static loading in bending tests. The measured strain from the Bragg sensor is perfectly linear with the applied force. Optical fibres with a Bragg sensor have also been embedded into filament wound pressure vessels. Tests carried out on such a pressure vessel include both static and slowly varying load schemes. The Bragg signal is nearly perfectly linear with the applied pressure. The results demonstrate the applicability of Bragg sensors for continuous monitoring of composite materials. 相似文献
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基于渤海冰区某真实导管架结构,首先进行结构数值计算,确定光纤应变布点位置及其与冰荷载的确定关系,其次进行结构光纤安装和现场监测,最后进行结构的极值冰荷载确认。由原型结构应变测量得到的冰荷载可以对传统的冰力计算公式进行有效的校核。 相似文献
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Composites are promising alternatives for space structures because of their versatile characteristics such as high specific stiffness and strength. When composite structures are exposed to the space environments (low Earth orbit, LEO), however, they are known to undergo considerable temperature change induced by the direct sunlight and the Earth's shadow in addition to ultraviolet, high vacuum, atomic oxygen and so forth. Therefore, for the successful completion of their missions, it is important for the structures to maintain the consistent dimensional stability in such a thermal cycling condition. The coefficient of thermal expansion (CTE) of the structures is suitable to express the dimensional stability, and it is needed to be monitored throughout the mission. For this purpose, fiber optic sensors, which have many advantages, were investigated to check their suitability in this paper.Two fiber Bragg grating (FBG) sensors have been adopted for the simultaneous measurement of thermal strain and temperature to get the CTE change of a carbon/epoxy composite laminate. LEO conditions with high vacuum, ultraviolet and thermal cycling environments were simulated in a thermal vacuum chamber. As a pre-test, a FBG temperature sensor was calibrated and a FBG strain sensor was evaluated through the comparison with the electric strain gauge (ESG) attached on an aluminum specimen in the same temperature range as the thermal cycling. The change of the transverse CTE in a composite laminate exposed to the space environment was measured for intervals of aging cycles in real time. As a whole, there was no abrupt change of the CTE after 1000 aging cycles. After aging, however, the CTE decreased a little all over the test temperature range. These changes are thought to have been caused by outgassing, moisture desorption, matrix cracking, etc. In this paper, embedding application of FBG sensors to composites operated under space environment and their successful real-time monitoring of thermal deformations over a long time was shown. 相似文献