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A non-invasive capacitive sensor strip for aerodynamic pressure measurement

机译:用于空气动力压力测量的无创电容式传感器条带

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摘要

This paper presents a capacitive pressure sensor strip implemented in general purpose printed circuit board (PCB) technology based on a thin 3D structure composed of polyimide, woven glass reinforced epoxy resin (FR4) and metal layers. Multiphysics finite elements method (FEM) simulations have been performed over the proposed structure in order to develop a time-dependent electrical and mechanical model that can be easily used to tailor the characteristics to the application. The device targets a wide class of fluid dynamics applications, being non-invasive, comformable and smart for placement. The device simulations are herein validated by experimental wind tunnel measurements and compared with figures obtained on a wing profile by conventional electromechanical pressure transducers. This approach is one of the first example of fully embedding and electronically controlled fluid flow monitoring apparatus that could be used in replacement of state of the art mechanical systems.
机译:本文介绍了一种基于通用印刷电路板(PCB)技术的电容式压力传感器条,该条基于由聚酰亚胺,玻璃纤维增​​强环氧树脂(FR4)和金属层组成的薄3D结构。为了开发出随时间变化的电气和机械模型,可以轻松地使用多物理场有限元方法(FEM)模拟该结构,该模型可以轻松地用于为应用程序定制特性。该设备针对广泛的流体动力学应用,具有非侵入性,适形性和放置智能性。装置仿真在此通过实验风洞测量得到验证,并与通过常规机电压力传感器在机翼轮廓上获得的数字进行比较。这种方法是完全嵌入和电子控制的流体流量监控设备的第一个示例,该设备可用于替代现有技术的机械系统。

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