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为提高传统先进绝热压缩空气储能(AA-CAES)系统性能,在原系统上耦合了太阳能辅热子系统,并对耦合太阳能辅热的AA-CAES系统性能进行了研究。结果表明:在相同压缩机级数下,冷罐和热罐温度均随膨胀机级数的增加缓慢升高;在相同膨胀机级数下,冷罐和热罐温度随压缩机级数的增加逐渐降低;当压缩机与膨胀机级数相等时,系统储能效率、储能密度和耦合储能效率均比二者级数不等时更高;随着换热器效能的提高,系统冷罐和热罐温度升高、膨胀功和压缩功增大,而系统储能效率和耦合储能效率先提高后降低。 相似文献
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为解决液化空气储能系统(LAES)压缩热利用不完全的问题,构建了耦合有机朗肯循环的液化空气储能系统(ORC-LAES)。对ORC-LAES系统建立热力学性能计算模型,在设计参数下分析压缩机出口压力、膨胀机入口压力、加压水初温、加压水流量比及膨胀机级数对ORC-LAES系统性能的影响。结果表明,当压缩机出口压力由6 MPa上升到16 MPa、加压水初温从293 K上升到323 K时,系统的循环效率、火用效率和液化率均下降;当膨胀机入口压力由8 MPa上升到18 MPa时,系统循环效率和火用效率均增加;当加压水流量比由0.51上升到0.96时,系统循环效率和火用效率先增加再减少,流量比为0.71时,系统的循环效率和火用效率达到最大;在压缩热利用上耦合有机朗肯循环要优于增加膨胀机级数;ORC-LAES系统与LAES系统相比,循环效率提高4.8%,火用效率提升5.1%。 相似文献
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《中外能源》2020,(9)
压缩空气储能系统压缩机受系统自身特性影响,长期处于变工况运行状态。对某多级压缩空气储能系统大型空气压缩机变工况条件下级间性能开展试验研究,即利用压缩机管网特性试验平台,开展排气压力6.5~9.5MPa范围试验测试,对压缩机各级吸气和排气压力、吸气和排气温度、压缩机排气量、电机电流、电压等参数进行实时采集。通过对压缩机实时变工况下各项参数分析,具体研究压缩机的容积效率、循环指示功率、等温效率、各级压比分配和各级压损随出口负荷变化而变化的规律。研究结果表明:压缩机的容积效率基本不随工况的变化而变化,平均为0.96;循环指示功率随出口负荷的增加而增加;压缩机的多变效率从74.02%上升到78.14%,多变效率随着排气压力的增加而增加;低压级压比增大速度较快,易达到额定状态,高压级压比达到额定状态较缓;一~四级的相对压力损失基本保持不变,五级出口排气到集气汇管的相对压力损失随着出口负荷的增大而减小。 相似文献
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提出一种非等比压缩结构的储能系统,在此基础上提出4种具体的系统结构方案,并与以往文献提到的等比压缩结构的储能系统进行对比分析。结果发现:在总压缩比相同的情况下,等比压缩结构的先进绝热压缩空气储能(AA-CAES)系统的储能密度随压缩级数的增大而减小,储能效率随压缩级数的增大而升高;对于非等比压缩结构的储能系统,储热介质能达到的温度越高,则系统的储能密度越大;用2种储热介质分阶段存储压缩热,可减小换热器的换热温差,降低系统的不可逆损失,从而提高系统的储能效率。 相似文献
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为解决压缩空气储能系统储能密度和效率低的问题,建立了基于地下储气室的多级回热式跨临界压缩二氧化碳储能系统(Compress Carbon Dioxide Energy storage,TC-CCES)热力学模型及■分析模型,采用二氧化碳代替空气作为存储介质,对系统进行热力学性能分析和敏感性分析。结果表明:TC-CCES的储能密度达到57.29 kW·h/m~3,是先进绝热压缩空气储能系统(Advanced adiabatic CAES,AA-CAES)的2~25倍,储能效率和■效率分别为58.41%和67.89%,均高于AA-CAES;在TC-CCES中,储能过程的压缩机级间冷却器、释能过程的膨胀再热器以及回热系统中热泵■损失较大,通过提高系统储能压力、释能压力以及降低系统低压储气室入口压力,可以提高系统的储能效率和■效率。 相似文献
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《动力工程学报》2016,(4):313-319
根据压缩空气储能系统的结构特性,采用正交设计和数值模拟方法对压缩空气储能系统的压缩机绝热效率、级间冷却温度、储气室最低工作压力、回热度、膨胀透平绝热效率和燃烧室效率等6个参数进行实验设计和数值模拟,并对模拟结果进行效率分析.通过对实验结果的方差进行分析,得到设计参数对系统效率的影响程度.结果表明:在压缩空气储能系统中,压缩机绝热效率、级间冷却温度、回热度、压缩机绝热效率与级间冷却温度的交互作用、级间冷却温度与回热度的交互作用以及压缩机绝热效率与膨胀透平绝热效率之间的交互作用为影响压缩空气储能系统总过程效率的显著因素;在现有技术水平下,降低压缩机级间冷却温度和提高回热度是提高压缩空气储能系统效率的最佳选择. 相似文献
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为深入分析耦合太阳能辅热的先进绝热压缩空气储能(AA-CAES+CSP)系统的运行特性,在先进绝热压缩空气储能(AA-CAES)系统基础上建立相关模型,对比分析这2个系统性能,并探究关键参数对AA-CAES+CSP系统性能影响。结果表明:相比于AA-CAES系统,AA-CAES+CSP系统循环效率提高7.90%,储能密度提高4.46%;当压缩机级数N1=膨胀机级数N2=级数N时,循环效率和储能密度最高,N1与N2相差越小,系统性能越优;随着储气室对流换热系数hc的增大,循环效率先大幅度降低,后缓慢增大,储能密度则持续增大,且在hc较小时,N越大,循环效率越低,而当hc较大时则相反,储能密度则随N的增大而持续增大,但N越大,同一hc对系统性能的影响越小;循环效率随储气室最大压比的增大而减小,储能密度则相反,且在最大压比较小时,N越大,循环效率越小,储能密度越大,但当N较大时,N越大,循环效率和储能密度均越大。 相似文献
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《International Journal of Hydrogen Energy》2022,47(63):26789-26797
The issues related to the reliability of hydrogen engines of unmanned vehicles and increasing the efficiency of using hydrogen as fuel when using the method of its production during the decomposition of hydrogen-containing molecules of liquid-phase organic compounds in a plasma discharge under the action of intense ultrasonic exposure are considered. Experiments have shown that as a result of decomposition in the acoustoplasma discharge of liquid hydrocarbons, solid-phase carbon-containing products are formed, chemical transformations occur in the liquid phase and hydrogen-containing combustible gas is formed. Hydrogen-containing gas can be used as fuel immediately after synthesis, i.e. it does not require separation, since in addition to hydrogen it contains only impurities of CO2 and water vapor. The purpose of the study is to formalize the basic conditions for tightening the control of mutual compliance with the efficiency of hydrogen engines of the same series in the conditions of their mass production. Methods of mathematical statistics and hardware-software modeling were used in the study. The term “unerroric of quality mutual compliance control” is introduced to describe a set of hardware and software tools for such control. The principle of in-depth testing of the technical condition of such engines of one series is described in a multidimensional formulation of the quality control problem for three of their operating parameters at once. The conditions for increasing the mutual correspondence of the measured values of such parameters in the conditions of serial production of hydrogen engines are formalized. 相似文献
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基于《水工混凝土掺用氧化镁技术规范》中的Ⅰ型氧化镁(MgO),研究了该型MgO膨胀剂(MEA)细度对掺粉煤灰水泥浆体膨胀性能的影响。即采用X射线衍射分析(XRD)及同步热分析(TG DSC)分析了掺MEA水泥浆体中MgO的水化性。结果表明,养护温度相同时,MEA的细度对水泥浆体内MEA中MgO的水化和水泥浆体的膨胀无显著影响,产生的膨胀均能补偿水泥浆体的收缩;MEA的细度可从试验设计采用的45 μm筛筛余15%左右增加到30%左右,这将有利于MEA生产企业的节能降耗。 相似文献
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General expressions for the heat of vaporization of mixtures at constant pressure; at constant temperature; and at constant pressure, temperature, and composition are proposed. The last one is related to the liquid-vapor interface where steady vaporization or condensation is taking place. Numerical examples by the proposed expressions are shown for binary mixtures of HCFC22(R22) and (HCFC123(R123) © 1997 Scripta Technica, Inc. Heat Trans Jpn Res, 25(1): 12–24, 1996 相似文献
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应用瞬态谱分析方法对燃烧流化床声波信号进行了频谱分析,发现气泡能量分布呈Gamma分布形式,在Argyrious和Yoshida等人提出的模型的基础上,发展了燃烧流化床气泡能量分布模型,并通过优化迭代对模型参数进行求解,在实验和理论的基础上得出了更加切合实际的燃烧流化床气泡能量分布模型 相似文献
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城镇生活污水处理装置是由农村户用沼气地发展演变而来,是一种小型、分散化处理污水的装置 ,是环境建设的需要。文章着重从我国环保政策及目标、生活污水造成的污染状况、急需整治的公共设施、生活污水净化装置的演变以及社会经济效益和环境效益等方面,阐述了其产业化的重要性。 相似文献
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Linear and nonlinear analyses of the instabilities and distortion of liquid streams injected into a gaseous media are discussed. The various fundamental mechanisms and the predictive capabilities for the distortions are emphasized. Round jets, planar sheets, annular sheets, and conical sheets are discussed in detail. The balance between capillary and inertial forces is primarily examined. The method for simplifying the analyses in the case of thin liquid sheets is discussed. The capabilities for representing the droplet size distribution that follows the stream disintegration are outlined. 相似文献
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The paper deals with second law thermodynamic analysis of a basic gas turbine based gas-steam combined cycle. The article investigates the effect of variation of cycle parameters on rational efficiency and component-wise non-dimensionalised exergy destruction of the plant. Component-wise inefficiencies of the combined cycle have been quantified with the objective to pin-point the major sources of exergy destruction. The parameter that affects cycle performance most is the TIT (turbine inlet temperature). TIT should be kept on the higher side, because at lower values, the exergy destruction is higher. The summation of total exergy destruction of all components in percentage terms is lower (44.88%) at TIT of 1800 K & rp,c = 23, as compared to that at TIT = 1700 K. The sum total of rational efficiency of gas turbine and steam turbine is found to be higher (54.91%) at TIT = 1800 K & rp,c = 23, as compared to that at TIT = 1700 K. Compressor pressure ratio also affects the exergy performance. The sum total of exergy destruction of all components of the combined cycle plant is lower (44.17%) at higher value of compressor pressure ratio (23)& TIT = 1700 K, as compared to that at compressor pressure ratio (16). Also exergy destruction is minimized with the adoption of multi-pressure-reheat steam generator configuration. 相似文献