Analysis and performance of a large thermoacoustic engine

Analysis and performance of a large thermoacoustic engine
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DOI:
10.1121/1.403896
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发表时间:
1992-09
影响因子:
2.4
通讯作者:
G. Swift
G. Swift
中科院分区:
物理与天体物理3区
文献类型:
--
作者:
G. Swift

文献摘要

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对一台直径为13 cm的热声发动机进行了测量和分析。在其最强大的工作点,使用13.8 bar氦气,发动机提供630 W的外部声负载,将热量转换为所提供的声功率,效率为9%。在低声振幅,其中(线性)热声理论预计将适用,温度差和频率的测量与理论的预测在4%以内,在跨越因素的条件下,平均压力为4,压力振幅为10,频率为6,气体声速为3。但是压力振幅的平方与加热器功率的测量值与理论预测值相差20%,是结果中估计不确定性的两倍。在较高的压力振幅(高达16%的平均压力),甚至更显着偏离现有的热声理论观察。确定了这种振幅依赖性偏差的几个原因,包括声波中的共振增强谐波含量,以及热声热交换器中的新的一阶温度缺陷。这些原因解释了高振幅测量与现有(线性)理论的部分(但不是全部)振幅依赖性偏差。
Measurements and analysis of a 13‐cm‐diam thermoacoustic engine are presented. At its most powerful operating point, using 13.8‐bar helium, the engine delivered 630 W to an external acoustic load, converting heat to delivered acoustic power with an efficiency of 9%. At low acoustic amplitudes, where (linear) thermoacoustic theory is expected to apply, measurements of temperature difference and frequency agree with the predictions of theory to within 4%, over conditions spanning factors of 4 in mean pressure, 10 in pressure amplitude, 6 in frequency, and 3 in gas sound speeds. But measurements of the square of pressure amplitude versus heater power differ from the predictions of theory by 20%, twice the estimated uncertainty in the results. At higher pressure amplitudes (up to 16% of the mean pressure), even more significant deviation from existing thermoacoustic theory is observed. Several causes of this amplitude‐dependent deviation are identified, including resonance‐enhanced harmonic content in the acoustic wave, and a new, first‐order temperature defect in thermoacoustic heat exchangers. These causes explain some, but not all, of the amplitude‐dependent deviation of the high‐amplitude measurements from existing (linear) theory.