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Detection and measurement of impacts in composite structures using a self-powered triboelectric sensor

机译:使用自动摩擦摩擦传感器检测和测量复合结构中的冲击

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摘要

Composite structures as e.g. aircrafts, wind turbines or racing cars are frequently subjected to numerous impacts. For example, aircrafts may collide with birds during take-off and landing or get damaged due to the impact of hailstones. These impacts harm the integrity of the composite laminates used in their structures which results in delamination and other failures which are usually very difficult to detect by visual inspections. Hence, the detection and quantification of impacts is of vital importance for monitoring the health state of composite structures. Recently, triboelectric sensors have been demonstrated to detect touches, pressures, vibrations and other mechanical motions with the advantages of being self-powered, maintenance-free and easy to fabricate. However, there is no research focusing on the potential of triboelectric sensors to detect impacts in a wide energy range. In this paper, a self-powered triboelectric sensor is developed to measure impacts at high energy in structures made of composite materials. This could be particularly beneficial for the detection of bird strikes, hailstones and other high energy impacts in aircraft composite structures. For that purpose, composite plates are subjected to various energy impacts using a drop weight impact machine and the electric responses provided by the developed triboelectric sensor are measured in terms of voltage and current. The idea is to evaluate the sensitivity of the electrical signals provided by the sensor to changes in the impact energy. The results prove that the generated electric responses are affected by the energy of the impact and their amplitude increases linearly with the impact energy. The voltage and current sensor responses demonstrate a very good impact sensitivity of 160 mV/J and a strong linear relationship to the impact energy (R = 0.999) in a wide energy range from 2 to 30 J. This work suggests a novel approach to measure the magnitude of the impacts in composite structures
机译:复合结构如例如。飞机,风力涡轮机或赛车经常受到许多影响。例如,飞机可能在起飞和降落时与鸟类碰撞或由于冰雹的影响而损坏。这些影响损害了它们结构中使用的复合层压板的完整性,这导致分层和其他故障通常很难通过目视检查检测。因此,对监测复合结构的健康状况至关重要的影响是至关重要的。最近,已经证明了摩擦电传感器以检测触摸,压力,振动和其他机械运动,具有自动的,免维护,易于制造的优点。然而,没有研究专注于摩擦电传感器的潜力,以检测宽能量范围内的影响。在本文中,开发了一种自给自足的摩擦电传感器,以测量由复合材料制成的结构中的高能量的影响。这对于检测飞机复合结构中的鸟类撞击,冰雹和其他高能量影响特别有益。为此目的,复合板使用下落重量冲击机进行各种能量冲击,并且由开发的摩擦传感器提供的电响应在电压和电流方面测量。该想法是评估传感器提供的电信号的灵敏度,以改变冲击能量。结果证明,所产生的电反应受到冲击能量的影响,并且它们的幅度随冲击能量线性增加。电压和电流传感器响应表现出160 mV / j的非常好的冲击灵敏度和与冲击能量(r = 0.999)的强烈线性关系在宽的能量范围内,从2到30 J.这项工作表明了一种新的衡量方法复合结构中的影响的大小

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