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A high frequency cascade thermoacoustic engine

机译:高频级联热声发动机

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摘要

A miniature cascade thermoacoustic engine, which consisted of one standing-wave stage and one traveling-wave stage in series, was built and tested, which length was about 1.2 m, operating at 470 Hz using helium as working gas. The cascade modeling, the simulation and the primary experimental results are described in this paper. Four different configurations of the miniature cascade thermoacoustic engines had been designed and compared. According to the analysis, the diameter ratio of stages was designed to extend the traveling-wave region, which optimized value was about 1.69. The peak-to-peak value of the acoustic pressure was predicted to arrive to 3 bar at the 3 MPa mean pressure of helium when 300 W heating power was the input. The features of the engine were predicted delivering 68 W acoustic power with a thermal efficiency of up to 22.74 percent (the ratio of acoustic power to heater power). Due to careful designing, the engine self-excited the oscillation smoothly from the first experiment. An onset temperature gradient of about 4.5 K/mm was achieved, and the peak-to-peak acoustic pressure was 48 KPa at the 2 MPa mean pressure when 200 W heating power was the input. The design computation and experimental results showed a rather good agreement between the measured and calculated pressure phasor and temperatures distributions in the cascade thermoaoustic engine.
机译:建造并测试了一个微型级联热声发动机,该发动机由一个驻波级和一个行波级串联组成,其长度约为1.2 m,使用氦气作为工作气体以470 Hz的频率运行。本文描述了级联建模,仿真和主要实验结果。设计并比较了微型级联热声发动机的四种不同配置。根据分析,设计了载物台的直径比,以扩展行波区域,优化值约为1.69。当输入300 W加热功率时,预计在3 MPa的氦气平均压力下,声压的峰峰值将达到3 bar。预计该发动机的功能将提供68 W的声功率,热效率高达22.74%(声功率与加热器功率之比)。由于精心设计,发动机从第一次实验起就平稳地自激了振荡。当输入200 W加热功率时,达到约4.5 K / mm的开始温度梯度,并且在2 MPa平均压力下,峰峰声压为48 KPa。设计计算和实验结果表明,在级联热声发动机中,实测和计算的压力相量与温度分布之间有很好的一致性。

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