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首页> 外文期刊>Journal of Engineering for Gas Turbines and Power >On Scaling Down Turbines to Millimeter Size
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On Scaling Down Turbines to Millimeter Size

机译:将涡轮机缩小到毫米尺寸

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摘要

The purpose of this work is to establish the maximum theoretical efficiency that a viscous flow turbine (such as a Tesla turbine) can achieve. This is very much in the spirit of the Betz limit for wind turbines. The scaling down of viscous flow turbines is thought not to alter this result, whereas the scaling down of conventional turbines, whether axial or radial flow, results in an ever lowering of their efficiencies. A semiempirical scaling law is developed for conventional gas turbines using published machine performance data, which is fitted to a simple boundary layer model of turbine efficiency. An analytical model is developed for a viscous flow turbine. This is compared to experimental measurements of the efficiency of a Tesla turbine using compressed air. The semiempirical scaling law predicts that below a rotor diameter of between about 11 mm and 4 mm, a practical Brayton cycle is not possible. Despite that, however, and for rotor diameters less than between about 7 mm and 2 mm, a viscous flow turbine, compressor, or pump will be more efficient than a conventional design. This may have a significant impact on the design of microelectromechanical system devices.
机译:这项工作的目的是确定粘性流动涡轮机(例如Tesla涡轮机)可以达到的最大理论效率。这非常符合风力涡轮机的Betz极限精神。人们认为,按比例缩小粘性流动涡轮机不会改变这种结果,而按常规比例缩小传统涡轮机,无论是轴向流量还是径向流量,都会导致其效率不断降低。使用已公开的机器性能数据为常规燃气轮机开发了半经验定标定律,该定律适用于涡轮机效率的简单边界层模型。开发了用于粘性流动涡轮机的分析模型。这与使用压缩空气的特斯拉涡轮效率的实验测量结果进行了比较。半经验定标定律预测,在转子直径约11mm至4mm之间时,实际的布雷顿循环是不可能的。然而,尽管如此,并且对于小于约7mm至2mm的转子直径,粘性流轮机,压缩机或泵将比常规设计更有效。这可能会对微机电系统设备的设计产生重大影响。

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