共查询到17条相似文献,搜索用时 218 毫秒
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跨临界热泵循环在大温差加热时具有显著优势。为了寻求更高效的跨临界热泵循环,对R23跨临界热泵循环进行了理论分析,计算了压缩机排气压力对系统性能的影响。计算结果表明,R23热泵系统存在最优高压侧压力,最优高压侧压力与制冷剂气冷器出口温度、蒸发温度、过热度都有关系,其中以制冷剂气冷器出口温度对最优高压侧压力影响最大。以制冷剂气冷器出口温度为自变量,利用多项式函数对最优高压侧压力进行了拟合,拟合的最大相对误差为-3.14%,平均相对偏差为1.22%。结果可以为R23跨临界热泵系统的设计和控制提供理论参考。 相似文献
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为了研究跨临界CO2热泵空调系统在不同工况下的制热性能,应用MATLAB软件,对带回热器的跨临界CO2系统进行仿真研究。针对系统内排气压力Pcond、蒸发温度Tevp、气冷器排气温度Tout、过热度ΔT等因素,探究其对系统制热COP的影响。研究结果表明:Tevp、ΔT每升高1℃,系统COP分别上升5%~7%、0.1%~1.3%;Tout每增加1℃,系统COP降低0.17~0.04。通过仿真研究得出,跨临界CO2系统的最优排气压力Pcond_opt,并拟合得到其计算关联式。 相似文献
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建立了跨临界CO_2双级压缩增压系统的热力学模型,并对气体冷却器出口温度、膨胀罐内压力、过冷度等影响系统性能的因素进行了数值分析。结果表明:系统的最佳排气压力随着气冷器出口温度的升高而迅速升高,且在气冷器出口温度不发生改变的情况下,最佳排气压力随着蒸发温度的降低略微有所升高,而系统最佳COP随气冷器出口温度的升高而快速下降。系统的最佳干度值随着气冷器出口温度的升高而增大。在一定的蒸发温度下,系统COP随着膨胀罐内压力的增大而逐渐减小,同时随着过冷度的增大系统COP逐渐增大,但要比蒸发温度对系统性能的影响要小些。 相似文献
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为进一步研究跨临界CO_2热泵的系统性能,针对所设计CO_2热泵系统进行实验。实验结果表明:在风机频率一定时,系统热负荷、压缩机轴功率、系统出风温度均随压缩机频率的增大而增大。蒸发温度从-2℃升至4℃,COP增幅为26%,CO_2在气冷器出口温度降低10℃左右时,系统COP增幅大于30%。实验工况下跨临界CO_2热泵系统出风温度变化范围在50℃-100℃,在获得大于75℃出风温度时,热力学第二定律效率超过30%,CO_2气冷器出口温度、高压侧压力、蒸发温度的升高都会提高系统热力学第二定律效率。 相似文献
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对带和不带回热器(IHX)的跨临界二氧化碳两相引射制冷系统进行了实验研究,主要分析了回热器、实验工况、引射器尺寸参数对系统性能的影响。结果表明:对于固定的气冷器出口温度、不同的气冷器压力工况,回热器的使用可使系统制冷量提高0.85%-8.60%,COP提高0.88%-11.7%;对于固定的气冷器压力,在不同的气冷器出口温度条件下,其制冷量可提高1.14%-2.92%,COP可提高0.99%-2.75%;在气冷器压力较低及出口温度较高的工况条件下,回热器对系统性能影响较大,系统COP及制冷量的最大改善均发生在上述工况条件下;喷嘴直径与引射器混合室长度之间存在一个最优匹配,两者的最优匹配能使系统COP大大提高。 相似文献
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《低温与超导》2016,(10)
为研究R12回热循环对航天器单级蒸汽压缩式热泵系统性能的影响,搭建了热泵性能测定实验装置,从排气温度、耗功量、制冷量及制冷系数等方面分析了回热循环对热泵系统性能的影响。结果表明:在有、无回热循环两种工况下,实验测得的排气温度、耗功量、制冷量、制冷系数均随量热器温度的升高而增大;同一量热器温度下,回热循环在提高系统制冷量的同时会增加压缩机耗功,引起排气温度升高,但制冷量的增长幅度大于压缩机耗功的增长幅度。当量热器内温度为16℃、20℃、24℃、28℃时,回热循环带来的制冷系数增长率分别为50%、39.6%、32.7%、27.6%。因此R12回热循环对提高系统制冷系数是有效的。在此基础上,基于Aspen Plus软件建立了实验流程模型,采用NRTL-RK物性方法对有、无回热热泵循环进行模拟计算。模拟结果与实验结果两者间误差较小,说明软件模拟实际热泵流程的可靠性较高,今后可进一步利用Aspen Plus软件作热泵系统性能的深入研究。 相似文献
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为探究热泵供水温度对CO2空气源热泵系统性能的影响,保持室外环境温度15.5℃不变,调节热泵供水温度,测试冷却水流量、气冷器出水温度、压缩机排气温度、气冷器CO2进出口温差、压缩机排气压力、压缩机耗功量、系统制热量、气冷器热交换完善度、系统COP的变化情况。结果表明:供水温度由45℃升至85℃,气冷器出水温度、压缩机排气温度、气冷器CO2进出口温差、压缩机排气压力随之增加,冷却水流量随之减小。系统制热量增加了7.3%、气冷器热交换完善度下降了20.0%、系统COP下降了35%、压缩机功耗增加了65.1%。 相似文献
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采用CO_2天然混合制冷剂的制冷系统热力学分析 总被引:1,自引:1,他引:0
受工况条件的限制,CO2制冷系统在实际应用中往往需要采用跨临界循环,高压侧压力高达10MPa及以上。高的运行压力对系统各部件、设备的安全运行均提出更高要求,从而造成初投资增大。采用CO2混合工质,可以有效地改善纯的CO2系统存在的不足。针对三组CO2天然混合工质——R744/R290、R744/R600、R744/R600 a,在特定的工况条件下,对制冷系统进行了热力学理论分析和计算。探讨了混合工质中CO2不同质量配比、不同蒸发器出口制冷剂温度对系统制冷量、COP和冷凝压力的影响。结果表明:在相同工况下,R744/R290的冷凝压力比R744R/600高12~23%,比R744/R600 a高19~24%;R744/R290的COP值比R744/R600高33~41%,比R744/R600 a高25~32%。 相似文献
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An experimental study of condensation heat transfer characteristics of flow inside horizontal micro-fin tubes is carried out using R410A, R22, and R32 as the test fluids. This study especially focuses on the influence of heat transfer area upon the condensation heat transfer coefficients. The test sections were made of double tubes using the counter-flow type; the refrigerants condensation inside the test tube enabled heat to exchange with cooling water that flows from the annular side. The saturation temperature and pressure of the refrigerants were measured at the inlet and outlet of the test sections to defined state of refrigerants, and the surface temperatures of the tube were measured. A differential pressure transducer directly measured the pressure drops in the test section. The heat transfer coefficients and pressure drops were calculated using the experimental data. The condensation heat transfer coefficient was measured at the saturation temperature of 48°C with mass fluxes of 50–380 kg/(m2s) and heat fluxes of 3–12 kW/m2. The values of experimental heat transfer coefficient results are compared with the predicted values from the existing correlations in the literature, and a new condensation heat transfer coefficient correlation is proposed. 相似文献
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In this study, condensation of pure refrigerant R134a vapor inside a smooth vertical tube was experimentally investigated. The test section was made of a copper tube with inside diameter of 7.52 mm and length of 1 m. Experimental tests were conducted for mass fluxes in the range of 20–175 kg/m2s with saturation pressure ranging between 5.8 and 7 bar. The effects of mass flux, saturation pressure, and temperature difference between the refrigerant and tube inner wall (ΔT) on the heat transfer performance were analyzed through experimental data. Obtained results showed that average condensation heat transfer coefficient decreases with increasing saturation pressure or temperature difference (ΔT). In addition, for the same temperature difference (ΔT), heat can be removed from the refrigerant at a higher rate at relatively low pressure values. Under the same operating conditions, it was shown that average condensation heat transfer coefficient increases as mass flux increases. Finally, the most widely used heat transfer coefficient correlations for condensation inside smooth tubes were analyzed through the experimental data. The best fit was obtained with Akers et al.'s (1959) correlation with an absolute mean deviation of 22.6%. 相似文献