全部 标题 作者
关键词 摘要

OALib Journal期刊
ISSN: 2333-9721
费用:99美元

查看量下载量

相关文章

更多...
热力发电  2015 

离散隔板式迷宫叶顶冷却效率试验分析

, PP. 38-42

Keywords: 燃气轮机,动叶叶顶,迷宫结构,间隙高度,气膜冷却

Full-Text   Cite this paper   Add to My Lib

Abstract:

为减小涡轮机动叶顶部间隙泄漏造成的气动损失、提高叶顶冷却效率,提出在凹槽叶顶离散排布小隔板迷宫。根据某涡轮机动叶结构,设计了迷宫叶顶气膜冷却效率试验台,通过稳态液晶技术测量了间隙叶高比分别为1.0%,2.0%,3.0%和吹风比分别为1.0,1.5,2.0时隔板迷宫叶顶和凹槽叶顶的气膜冷却效率。结果表明:2种叶顶结构的平均冷却效率均随着叶顶间隙高度的增加而减小;在某间隙高叶比和吹风比范围内,隔板迷宫叶顶冷却效率最多比凹槽叶顶冷却效率高出63%;隔板迷宫显著扩大了叶顶的冷却范围,提高了冷却效率,使冷却效率的分布更加均匀。

References

[1]  黄力森,陈红英.m701f型燃气轮机冷却空气系统[j].热力发电,2006,35(10):54-59.huanglisen,chenhongying.thecoolingairsystemofm701ftypegasturbines[j].thermalpowergeneration,2006,35(10):54-59.
[2]  chyumk,moonhk,metzgerde.heattransferinthetipregionofgroovedturbineblades[j].journalofturbomachinery,1989,111:131-138.
[3]  wheelerps,maryq.tipleakagelossesinsubsonicandtransonicblade-rows[c].asme2011turboexpo:turbinetechnicalconferenceandexposition.vancouver,britishcolumbia,canada,gt-2011-45798,2011.
[4]  palafoxp,oldfieldmlg,irelandpt.bladetipheattransferandaerodynamicsinalargescaleturbinecascadewithmovingendwall[j].journalofturbomachinery,2012,134:021020.
[5]  wheelerps,atkinsnr,hel.turbinebladetipheattransferinlowspeedandhighspeedflows[j].journalofturbomachinery,2011,133:041025.
[6]  shyamv,ameria.comparisonofvarioussupersonicturbinetipdesignstominimizeaerodynamiclossandtipheating[c].asme2011turboexpo:turbinetechnicalconferenceandexposition.vancouver,britishcolumbia,canada,gt2011-46390,2011.
[7]  林汝谋.工业燃气轮机发展的关键技术[j].热力发电,1999,28(1):26-28.linrumou.keydevelopmentsofindustrialgasturbine[j].thermalpowergeneration,1999,28(1):26-28.
[8]  bunkerrs.axialturbinebladetip:function,design,anddurability[j].journalofpropulsionandpower,2006,22(2):271-285.
[9]  张永军,王会社,王文三,等.无导叶对转涡轮高压动叶叶尖开槽的研究[j].工程热物理学报,2009,30(3):402-406.zhangyoungjun,wanghuishe,wangwensan,etal.aninvestigationonaerodynamicperformanceofavanelesscounter-rotatingturbinewithrecessedhigh-pressurerotortips[j].journalofengineeringthermophysics,2009,30(3):402-406.
[10]  zhangq,hel.overtipshockwavestructureanditsimpactonturbinebladetipheattransfer[j].journalofturbomachinery,2011,133:041001.
[11]  zhangq,dowddo,hel.transonicturbinebladetipaerothermalperformancewithdifferenttipgaps_parti:tipheattransfer[j].journalofturbomachinery,2011,133:041027.
[12]  rahmanmh,kimsi,hassani.effectofinlettemperatureuniformityandnonuniformityonthetipleakageflowandrotorbladetipandcasingheattransfercharacteristics[j].journalofturbomachinery,2012,134:021001.
[13]  krishnababusk,hodsonhp,boothgd.aerothermalinvestigationoftipleakageflowinafilmcooledindustrialturbinerotor[j].journalofturbomachinery,2010,132:021016.
[14]  gaozh,narzaryd,mhetrass.effectofinletflowangleongasturbinebladetipfilmcooling[j].journalofturbomachinery,2009,131:031005.

Full-Text

comments powered by Disqus

Contact Us

service@oalib.com

QQ:3279437679

WhatsApp +8615387084133