期刊文献+

通流式气波转子性能试验研究 被引量:1

Performance Test of a Through-flow Wave Rotor
下载PDF
导出
摘要 气波转子是利用气波来传递能量的一种压力交换装置,已成功应用于内燃机及燃气轮机上.为研究通流式(through-flow,TF)气波转子特性,重新设计了定子,搭建了试验台架,并完成了TF气波转子的性能台架试验.进行了不同转速、不同温度、不同压力工况下的性能试验.结果表明,提高气波转子能量入口处的压力和温度有利于提高其性能,TF气波转子的最佳转速为13 000 r/min左右.试验结果表明该TF气波转子结构基本合理,能提高进气压力,最大压比可达2.0. A wave rotor is a pressure exchanger, which utilizes direct pressure transfer between fluids by pressure waves. It has been applied on a gas turbine or internal combustion engine. This paper investigates the performance of a through-flow (TF) wave rotor based on a test rig. The test rig includes a Comprex CX93 rotor together with redesigned casings. The experiment is completed based on different operating conditions such as varied speed, temperature, and pressure. Results show that the higher pressure and temperature of the inlet of the wave rotor causes better performance, the optimization rotational speed of the TF wave rotor is about 13 000 r/min. The designed TF wave rotor structure is reasonable and it produces high-pressure compressed air. The maximum compression pressure ratio is up to 2.0.
出处 《北京工业大学学报》 EI CAS CSCD 北大核心 2012年第4期607-613,共7页 Journal of Beijing University of Technology
基金 国家自然科学基金资助项目(51006012)
关键词 气波转子 气波 最佳转速 wave rotor pressure wave optimization speed
  • 相关文献

参考文献22

  • 1HIRCEAGA M,IANCU F,MUELLER N.Wave rotorstechnology and applications[C]∥The 11th InternationalConference on Vibration Engineering,Timisoara,Romania,September 27-30,2005. 被引量:1
  • 2WEBER H E.Shock wave engine design[M].New York:John Wiley and Sons,1995. 被引量:1
  • 3FRACKOWIAK M,IANCU F,POTRZEBOWSKI A.Numerical simulation of unsteady-flow processes in waverotors[C]∥2004ASME International MechanicalEngineering Congress,California,November 13-19,2004,IMECE2004-60973. 被引量:1
  • 4AKBARI P,NALIM R,MUELLER N.A review of waverotor technology and its applications[J].Journal ofEngineering for Gas Turbines and Power,2006,128:717-735. 被引量:1
  • 5AKBARI P,MUELLER N.Performance improvement ofsmall gas turbines through use of wave rotor topping cycles[C]∥Proceedings of ASME Turbo Expo 2003,Atlanta,Georgia,June 16-19,2003,GT2003-38772. 被引量:1
  • 6WELCH G E,PAXSON D E,WILSON J,et al.Wave-rotor-enhanced gas turbine engine demonstrator[C]∥GasTurbine Operation and Technology for Land,Sea and AirPropulsion and Power Systems Symposium,Ottawa,October 18-21,1999,NASA/TM-1999-209459. 被引量:1
  • 7DEMPSEY E,MUELLER N,AKBARI P,et al.Performance optimization of gas turbines utilizing four-portwave rotors[C]∥4th International Energy ConversionEngineering Conference and Exhibit,San Diego,California,Jun 26-29 2006,AIAA 2006-4152. 被引量:1
  • 8NALIMI R,PEKKAN K.Internal combustion wave rotorsfor gas turbine engine enhancement[C]∥Proceedings ofthe International Gas Turbine Congress 2003,Tokyo,November 2-7,2003,IGTC2003Tokyo FR-303. 被引量:1
  • 9WEBER F,GUZZELLA L.Control oriented modeling of apressure-wave supercharger(PWS)to gasoline engine[J].SAE 2000 Transactions,Journal of Engines,section3,SAE2000-01-0567,109:665-674. 被引量:1
  • 10SPRING P,ONDER C H,GUZZELLA L.EGR controlof pressure-wave supercharged IC engines[J].ControlEngineering Practice,2007,15:1520-1532. 被引量:1

二级参考文献6

同被引文献15

  • 1廖达雄,任泽斌,余永生,杨永.等压混合引射器设计与实验研究[J].强激光与粒子束,2006,18(5):728-732. 被引量:47
  • 2WeberHE.Shockwaveenginedesign[M].NewYork:JohnWileyandSonsInc,1995. 被引量:1
  • 3ScottT.Re-examinationofthecrypto-steadypressure-exchanger(Virtualturbomachine)[R].AIAAPaper,2001-2927. 被引量:1
  • 4GarrisCA.Anewconceptforahublessrotaryjet[R].AIAAPaper,1991-1903. 被引量:1
  • 5AminSM,GarrisCA.Anexperimentalinvestigationofanon-steadyflowthrustaugmenter[R].AIAAPaper,1995-2802. 被引量:1
  • 6HongWJ,GarrisCA.Non-steadyflowejectortechnologyappliedtorefrigerationwithenvironmentalbenefits[R].AIAAPaper,2000-0726. 被引量:1
  • 7HongWJ,AlhussanK.Thesupersonicrotor-vanepressure-exchangeejector[R].AIAAPaper,2001-0858. 被引量:1
  • 8ZhangHF,GarrisCA.Acomparativestudyofflowinductionbypressureexchange[R].AIAAPaper,2004-2343. 被引量:1
  • 9HongWJ,AlhussanK,ZhangHF.Anovelthermallydrivenrotor-vanepressure-exchangeejectorrefrigerationsystemwithenvironmentalbenefitsandenergyefficiency[J].Energy,2004,29:2331-2345. 被引量:1
  • 10AlhussanK.Studytheeffectofchanginginletarearatioofasupersonicpressure-exchangeejector[R].AIAAPaper,2005-0519. 被引量:1

引证文献1

二级引证文献1

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部