期刊文献+

超低热值燃料微型燃气轮机中压气机的流场分析与性能预测

The Analysis of Flow-field and the Predication of Performance of a Compressor in a Gas Turbine System Utilizing Ultra-low Heat Value Fuel
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摘要 介绍了超低热值燃料微型燃气轮机系统中压气机的特点,模拟了其流场,预测了其工作性能,并与前人研究的具有相似流量的压气机作了流场与性能的对比。最终得到:小流量大轮径是此类压气机的结构特点;与小轮径压气机相比,流动较难控制;高效率区向高转速方向延伸并且远离喘振线。 This paper introduced the characteristics of the compressor in a gas turbine system utilizing ultra-low heat value fuel, simulated the flow-field and the performance, and compared with the previous compressor with similar mass flow. The results indicate that small mass flow and large impeller diameter are the structural characteristics ; it is difficult to control the flow compared to the small impeller diameter compressor; zones of more efficiency extend to high-speed condition and they are far from the surge line.
出处 《汽轮机技术》 北大核心 2009年第3期161-164,186,共5页 Turbine Technology
基金 国家自然科学基金项目(编号:90610019) 上海市国际合作基金项目(编号:06DZ07006)资助
关键词 超低热值燃料 压气机 小流量大轮径 流场分析 性能预测 ultra-low heat value fuel compressor small flow rate and large impeller diameter flow-field analysis performance prediction
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参考文献8

  • 1John D.Northall.The Influence of Variable Gas Properties on Turbemachinery Computational Fluid Dynamics[J].ASME Journal of Turbomachienry,2006,128:632-637.
  • 2M.Zangeneh,M.Schleer,F.Ploger.S.S.Hong.Investigation of an Inversely Designed Centrifugal Compressor Stage--Part Ⅰ:Design and Numerical Verification[J].ASME Journal of Turbomachienry,2004,126:73-81.
  • 3M.Schleer,S.S.Hong,M.Zangeneh,C.Roduner.Investigation of an Inversely Designed Centrifugal Compressor Stage-Part Ⅱ:Experimental Investigations[J].ASME Journal of Turbomachienry,2004,126:82-90.
  • 4Ali Merchant.Aerodynamic Design and Performance of Aspirated Airfoils[J].ASME Journal of Turbomachienry,2003,125:141 -147.
  • 5L.Porreca,T.Behr,J.Schlienger,A.I.Kalfas,R.S.Abhari.Fluid Dynamics and Performance of Partially and Fully Shrouded Axial Turbines[J].ASME Journal of Turbomachienry,2005,127:668-677.
  • 6楚武利,吴艳辉,卢新根.小型高速离心压气机级内部的三维流场分析[J].应用力学学报,2006,23(4):511-515. 被引量:6
  • 7陈云永,刘波,靳军,王掩刚.高转速径向进气离心压气机流场特性分析[J].汽轮机技术,2006,48(1):46-48. 被引量:3
  • 8Reinhard Monig.Frank Miidner.Raft Raper.Viscous-Flow Two -Dimensional Analysis Including Secondary Flow Effects[J].ASME Journal of Turbomachienry,2001,123:558 -566.

二级参考文献13

  • 1Burce G J,Masme M.Computer aided Turbomachinery Design System[C].I Mech E,C554/026/98,1998.
  • 2Siddharth Thakur.CFD Predictions of Turbomachinery Flows Using quasi-steady and unsteady models[R].AIAA~2003-4133,2003.
  • 3M.Oana,O.Kawamoto,H.Ohtani and Y.Yamamoto.Approach to High Performance Transonic Centrifugal Compressor[R].AIAA 2002-3536,2002.
  • 4Nikos Markopoulos,Yedidia Neumeier,J.V.R.Prasad and Ben T.Zinn.Unsteady Disturbance Theory And Modeling for Centrifugal Compressors[R].AIAA~2000-3208,2000.
  • 5Alex Stein,Saeid N&i and L.N.Sankar.Numerical Analysis of Stall and Surge in a High-Speed Centrifugal Compressor[RR].AIAA 2000-0226,2000.
  • 6NUMECA IGG/ AutoGrid Manual.NUMECA International[R].Brus2sels,2000.
  • 7Krain H,Hoffmann B,Park H.Aerodynamics of a centrifugal compressor impeller with transonic inlet conditions[R].ASME Paper GT,1995:79.
  • 8Bonaiut D,Arnone A,Ermini M,et al.Analysis and optimization of transonic centrifugal compressor impellers using the design of experiments technique[R].ASME Paper GT,2002:30619.
  • 9Benini E,Toffolo A,Lazzaretto A.Centrifugal compressor of a 100 KW microturbine:part1-experimental and numerical investigations on overall performance[R].ASME Paper GT,2003:38152.
  • 10Hayami H,Hojo M,Hirata N et al.Flow with shock waves in a transonic centrifugal compressor with a low-solidity cascade diffuser using PIV[R].ASME paper GT,2004:53268.

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