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Investigation of microscale dielectric barrier discharge plasma devices.

机译:微型介电势垒放电等离子体装置的研究。

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摘要

This dissertation presents research performed on reduced-scale dielectric barrier discharge (DBD) plasma actuators. A first generation of microscale DBD actuators are designed and manufactured using polymeric dielectric layers, and successfully demonstrate operation at reduced scales. The actuators are 1 cm long and vary in width from tens of microns to several millimeters. A thin-film polymer or ceramic material is used as the dielectric barrier with thicknesses from 5 to 20 microns. The devices are characterized for their electrical, fluidic and mechanical performance. With electrical input of 5 kVpp, 1 kHz, the microscale DBD actuators induce a wall jet with velocity reaching up to 2 m/s and produce 3.5 mN/m of thrust, while consuming an average power of 20 W/m. A 5 mN/m plasma body force was observed, acting on the surrounding air. Failure of the microscale DBD actuators is investigated using thermal measurements of the dielectric surface in addition to both optical and scanning electron microscopy. The cause of device failure is identified as erosion of the dielectric surface due to collisions with ions from the discharge.;A second generation of microscale actuators is then designed and manufactured using a more reliable dielectric material, namely silicon dioxide. These actuators demonstrate a significant improvement in device lifetime compared with first-generation microscale DBD actuators. The increase in actuator lifetime allowed the electrical, fluidic and mechanical characterization to be repeated over several input voltages and frequencies. At 7 kVpp, 1 kHz, the actuators with SiO2 dielectric induced velocities up to 1.5 m/s and demonstrated 1.4 mN/m of thrust while consuming an average power of 41 W/m. The plasma body force reached up to 2.5 mN/m. Depending on electrical input, the induced velocity and thrust span an order of magnitude in range. Comparisons are made with macroscale DBD actuators which relate the actuator's output performance and power consumption with the mass and volume of the actuator design. The small size and of microscale DBD actuators reduces its weight and power requirements, making them attractive for portable or battery-powered applications (e.g., on UAVs).
机译:本文介绍了对减小尺寸的介质阻挡放电(DBD)等离子体致动器的研究。使用聚合物介电层设计和制造了第一代微型DBD执行器,并成功地演示了缩小规模的操作。致动器长1厘米,宽度从数十微米到几毫米不等。薄膜聚合物或陶瓷材料用作电介质阻挡层,厚度为5到20微米。该设备具有电气,流体和机械性能。在5 kVpp,1 kHz的电输入下,微型DBD执行器产生的壁射流的速度高达2 m / s,产生3.5 mN / m的推力,而平均功率为20 W / m。观察到5 mN / m的等离子体体力作用在周围的空气上。除了光学显微镜和扫描电子显微镜外,还使用电介质表面的热测量来研究微米级DBD执行器的故障。器件故障的原因被确定为由于与放电中的离子碰撞而导致的电介质表面腐蚀。然后,使用更可靠的电介质材料(即二氧化硅)设计和制造了第二代微型执行器。与第一代微型DBD执行器相比,这些执行器证明了设备寿命的显着提高。执行器寿命的增加允许在几个输入电压和频率上重复进行电气,流体和机械特性表征。在7 kVpp,1 kHz时,具有SiO2介电层的致动器的速度高达1.5 m / s,推力为1.4 mN / m,同时消耗的平均功率为41 W / m。等离子体力达到2.5 mN / m。取决于电输入,感应速度和推力的范围跨度为一个数量级。大型DBD执行器进行了比较,将执行器的输出性能和功耗与执行器设计的质量和体积联系起来。小巧的微型DBD执行器降低了重量和功率要求,使其对便携式或电池供电的应用(例如,在无人机上)具有吸引力。

著录项

  • 作者

    Zito, Justin C.;

  • 作者单位

    University of Florida.;

  • 授予单位 University of Florida.;
  • 学科 Engineering Electronics and Electrical.;Engineering Mechanical.;Engineering Aerospace.
  • 学位 Ph.D.
  • 年度 2013
  • 页码 178 p.
  • 总页数 178
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

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