共查询到20条相似文献,搜索用时 93 毫秒
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《工程热物理学报》2010,(6)
设计搭建了太阳能热声发动机实验系统,它由双轴全自动跟踪菲涅尔透镜聚焦型集热器和小型化驻波热声发动机两大组件构成。分别对充注不同压力N_2、He、Ar三种工质的太阳能热声发动机的起振温度、起振时热声核温度分布、压力振幅进行了实验研究。结果表明,氮气、氦气和氩气在相同充气压力下,He起振温度最高,N_2起振温度最低;N_2在充气压力1.0 MPa时达到最低起振温度394.8℃,且其压力振幅对充气压力变化不敏感;Ar在充气压力1.0 MPa时达到最低起振温度418.2℃,且其压力振幅随着充气压力的升高而逐渐增加。实验结果为优化太阳能热声发动机系统的热力性能提供了实验依据。 相似文献
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《工程热物理学报》2017,(12)
最近我们研究小组提出了一种声学共振行波热声发电机,它由三个相同的热声发动机核心单元,三台直线电机通过细长的谐振管连接起来。为了考察单个热声发动机核心单元的热功转换性能,我们搭建了热声发动机核心单元热功转换性能测试实验台。该实验台由两台压缩电机,热声发动机核心单元和两台膨胀电机组成。通过改变膨胀电机的电容和电阻,可以改变膨胀电机的阻抗,从而改变热声发动机核心单元的热功转换性能。经过模拟,我们确定了核心单元最佳工作阻抗范围.实验中当负载阻抗幅值为1.19×10~7 Pa·s/m~3,相位为60°时,获得最高净声功1046W和最高热声效率25.52%。由于热声发动机核心单元的漏热,实验结果和模拟结果在热声效率上相差较大。 相似文献
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针对热声发动机中复杂的起振、消振行为,在自行研制的"驻波型热声发动机试验平台"上,开展了工质类型、加热功率、充气压力等参数对热声发动机起振、消振行为的影响规律研究.试验结果表明:当采用纯氦气和90%氦气+10%氩气的混合气体时,系统存在一最佳的充气压力值,使起振温度和消振温度达到最低;而其余工质,其起振温度与消振温度均随着充气压力增加而逐渐提高;与此同时,由于加热功率对板叠热端温度影响较小,故采用板叠热端温度作为行为特性参数更为合理. 相似文献
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热声发动机用加热器的设计与实验验证 总被引:4,自引:0,他引:4
热声发动机利用热声效应将热能转换为机械能,热能由核心部件加热器提供。加热器在热声发动机的能量传递和转化过程中起着举足轻重的作用。针对热声发动机的工作特点,介绍了一种采用时均流对流换热公式进行热声发动机用加热器设计的方法。基于该方法,设计了一种新型热声发动机用电加热器,并应用于自行研制的太型多功能行波热声发动机试验台。设计计算和实验结果表明,该加热器能够充分满足热声发动机的加热要求。本文对以振荡流体为特征的换热器设计具有一定参考价值。 相似文献
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In an open cycle traveling wave thermoacoustic engine, the hot heat exchanger is replaced by a steady flow of hot gas into the regenerator to provide the thermal energy input to the engine. The steady-state operation of such a device requires that a potentially large mean temperature difference exist between the incoming gas and the solid material at the regenerator's hot side, due in part to isentropic gas oscillations in the open space adjacent to the regenerator. The magnitude of this temperature difference will have a significant effect on the efficiencies of these open cycle devices. To help assess the feasibility of such thermoacoustic engines, a numerical model is developed that predicts the dependence of the mean temperature difference upon the important design and operating parameters of the open cycle thermoacoustic engine, including the acoustic pressure, mean mass flow rate, acoustic phase angles, and conductive heat loss. Using this model, it is also shown that the temperature difference at the regenerator interface is approximately proportional to the sum of the acoustic power output and the conductive heat loss at this location. 相似文献
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热力学循环的实质是一种非等熵的循环 ,热声热机和斯特林热机振荡现象在满足热力学循环一般规律的同时 ,而各有其特殊性 ,故其各自的振荡本质是有差异的 ,用于描述两者的网络模型也必然有差异。 相似文献
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Thermoacoustic prime movers can generate pressure oscillation without any moving parts on self-excited thermoacoustic effect. The details of the numerical simulation methodology for thermoacoustic engines are presented in the paper. First, a four-port network method is used to build the transcendental equation of complex frequency as a criterion to judge if temperature distribution of the whole thermoacoustic system is correct for the case with given heating power. Then, the numerical simulation of a thermoacoustic-Stirling heat engine is carried out. It is proved that the numerical simulation code can run robustly and output what one is interested in. Finally, the calculated results are compared with the experiments of the thermoacoustic-Stirling heat engine (TASHE). It shows that the numerical simulation can agrees with the experimental results with acceptable accuracy. 相似文献