Investigation of modification design of the fan stage in axial compressor

(整期优先)网络出版时间:2010-02-12
/ 1
TheS2flowpathdesignmethodofthetransoniccompressorisusedtodesigntheonestagefaninordertoreplacetheoriginaldesignedbladecascadewhichhastwo-stagetransonicfanrotors.Inthemodificationdesign,thecamberlineisparameterizedbyaquarticpolynomialcurveandthethicknessdistributionofthebladeprofileiscontrolledbythedouble-thricepolynomial.Therefore,theinletflowhasbeenpre-compressedandthelocationandintensityoftheshockwaveatsupersonicareahavebeencontrolledinordertoletthenewbladeprofileshavebetteraerodynamicperformance.Thecomputationalresultsshowthatthenewsinglestagefanrotorincreasestheefficiencybytwopercentatthedesignconditionandthetotalpressureratioisslightlyhigherthanthatoftheoriginaldesign.Atthesametime,italsomeetsthemassflowrateandthegeometricalsizerequirementsforthemodificationdesign.