西安交通大学能源与动力工程学院,西安,710049
网络首发:2009-07-10,
纸质出版:2009
移动端阅览
付雷, 邓清华, 丰镇平. 微型向心透平级速比与DN值的最优选择[J]. 西安交通大学学报, 2009,43(7):16-20.
Analysis and Optimal Selection of Stage Velocity Ratio and DN-Value for Micro Radial Turbine[J]. 2009, 43(7): 16-20.
基于向心透平轮周效率的表达式
利用解析法分析了微型向心透平级速比和反动度的匹配关系
研究了关键参数变化对匹配结果的影响
对从级速比派生出的叶轮进口直径与转速的乘积值(DN值)这一参数进行了选取分析.结果表明:在向心透平设计时
级速比必须与反动度进行匹配选择
单纯选择级速比不能使向心透平具有较高的轮周效率; 对于不同的微型向心透平叶轮结构
级速比选取范围不同
径向-轴流式为0.64~0.72
纯径向式为0.72~0.80
级速比为0.72可作为这两种叶轮结构形式选择时的分界点; 叶轮DN值能直接反映出叶轮材料、结构形式、设计工况、叶轮尺寸以及轴承轴系等因素
这些因素直接关系向心透平能否实现微型化
因此叶轮DN值是一个高度集中的参数
在微型向心透平设计中可替代级速比.
Based on the expression of the wheel efficiency for radial turbines
the matching relationship between the stage velocity ratio and the reaction degree was analyzed by the analytic method. The influences of the key parameters on the matching results were discussed. Then
the DN-value derived from the stage velocity ratio was analyzed and selected. The results indicate that the stage velocity ratio should match the reaction degree in the design of micro radial turbines
otherwise the higher wheel efficiency can not be obtained. With the different structure of the micro turbine
the optimum range of the stage velocity ratio is 0.64-0.72 for a radial-axial turbine and 0.72-0.80 for a pure radial turbine
respectively. Moreover
the DN-value is relative to structural style
size
design working condition
efficiency
bearing and shafting of the micro radial turbine more directly than the stage velocity ratio. These results imply that the DN-value is a highly concentrated parameter and can be applied in the design of micro radial turbines instead of the stage velocity ratio.
EPSTEIN H A. Millimeter-scale, MEMS gas turbine engines [J]. ASME Journal of Engineering for Gas Turbines and Power, 2004, 126(2):205-226.
FRECHETTE L G, JACOBSON S A, BREUER K S, et al. Demonstration of microfabricated high-speed turbine supported on gas bearings[C]∥Solid-state Sensor. Hilton Head Island, South Carolina, USA: Transducers Research Foundation, 2000:43-47.
PEIRS J, REYNAERTS D, VERPLAETESN F, et al. A microturbine for electric power generation[J]. Sensors and Actuators: Physical, 2004, 113(1):86-93.
MATSUNUMA T, YOSHIDA H, IKI N, et al.Micro gas turbine with ceramic nozzle and rotor[C]∥Proceedings of the ASME Turbo Expo 2005. New York, USA:American Society of Mechanical Engineers, 2005:973-979.
ISOMURA K, MURAYAMA M, YAMAGUCHI H, et al. Development of micro-turbo charger and micro-combustor as feasibility studies of three-dimensional gas turbine at micro-scale[C]∥Proceedings of the ASME Turbo Expo 2003. New York, USA: American Society of Mechanical Engineers, 2003:685-690.
ISOMURA K, MURAYAMA M, YAMAGUCHI H, et al. Component development of micromachined gas turbine generators[C]∥Technical Digest Power MEMS 2002. Piscataway, New Jersey, USA: IEEE, 2002:32-35.
MATSUO E, YOSHIKI H, NAGASHIMA T, et al. The development of ultra gas turbines [J]. Journal of the Japan Institute of Energy, 2005, 84(3):192-199.
MATSUURA K, KATO C, YOSHIKI H, et al. Prototyping of small-sized two-dimensional radial turbines[C]∥Proceedings of the International Gas Turbine Congress 2003. Tokyo, Japan: IGTC, 2003:1-7.
付雷,石龑,邓清华,等. 毫米级微型透平的气动优化设计研究 [J]. 西安交通大学学报,2009,43(1):15-19.
FU Lei, SHI Yan, DEND Qinghua, et al. Aerodynamic design and optimization of a radial inflow millimeter-scale turbine [J]. Journal of Xi'an Jiaotong University, 2009,43(1):15-19.
付雷, 邓清华, 丰镇平. 厘米级微型燃机向心透平初步设计与数值分析 [C]∥中国工程热物理学会第十三届学术会议论文集. 北京:中国工程热物理学会, 2007:350-355.
李燕生, 陆桂林. 向心透平与离心压气机[M]. 北京:机械工业出版社,1987:55-56.
毫米级微型透平的气动优化设计研究.西安交通大学学报,2009,43(1):15-19.
叶轮机械气动优化设计中的近似模型方法及其应用.西安交通大学学报,2007,41(2):125-135.
离心叶轮的速度系数对级性能的影响.西安交通大学学报,2008,42(7):807-810.
串列叶片式离心叶轮内流场的数值研究.西安交通大学学报,2007,41(11):1275-1278.
基于多孔介质模型的刷式密封泄漏流动特性研究.西安交通大学学报,2007,41(7):768-711.
附着空化流动下离心泵水力性能数值预测.西安交通大学学报,2006,40(3):257-260.
附着空化流动的模型和算法.西安交通大学学报,2006,40(3):253-256.
0
浏览量
4
下载量
1
CSCD
关联资源
相关文章
相关作者
相关机构
京公网安备11010802024621