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MWCNT/EPOXY Composite Film as a Structural Strain Sensor for Micro Air Vehiclesud

机译:MWCNT / EPOXY复合膜作为微型飞机的结构应变传感器 ud

摘要

Peizo resistive Multiwall Carbon Nano Tubes (MWCNT) /Epoxy based composites film sensors with varying percentage of MWCNTs were developed and the percolation behaviour was studied by electrical conductivity measurements. These films exhibited percolation thresh hold at 2% MWCNT loading. Further, the composite film sensors were characterized in quasi static tensile mode in the range 0-1300 micro strain using a custom designed electrical circuit. The sensitivity of the various composite sensors, estimated in terms of gauge factor was found to be in the range of 40-140 for different percentage loading of MWCNT. To explore the feasibility of these sensors for Micro Air Vehicles (MAVs), static test was carried out by mounting the composite film sensors on MAV wing. The response of the film sensor for bending induced tensile and compressive strains was investigated. Gauge factors of 90 and 80 were realized for tensile and compressive strains respectively. These studies indicated that MWCNT/ Epoxy based composite films are found to be promising candidate for structural strain sensing on MAV.
机译:开发了具有可变百分比的CNT的Peizo电阻多壁碳纳米管(MWCNT)/环氧树脂基复合膜传感器,并通过电导率测量研究了其渗透行为。这些薄膜在2%MWCNT负载下表现出渗滤脱粒率。此外,使用定制设计的电路以准静态拉伸模式在0-1300微应变范围内对复合膜传感器进行了表征。对于不同的MWCNT百分比负载,各种复合传感器的灵敏度(以规格系数估算)在40-140范围内。为了探索这些传感器在微型飞行器(MAV)上的可行性,通过将复合膜传感器安装在MAV机翼上进行了静态测试。研究了薄膜传感器对弯曲引起的拉伸和压缩应变的响应。分别针对拉伸应变和压缩应变实现了90和80的应变系数。这些研究表明,发现基于MWCNT /环氧树脂的复合膜有望在MAV上用于结构应变传感。

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