[1] 林宇震,许全宏,刘高恩.燃气轮机燃烧室[M].北京:国防工业出版社,2008.
[2] BahrDW.TechnologyfortheDesignofHighTemperatureRiseCombustors[R].AIAA85-1292.
[3] MongiaHC.EngineeringAspectsofComplexGasTurbineCombustionMixers,PartⅠ:HighΔT[R].AIAA(a)1.5C-1C-0.8C(b)1.5CC-1C-0.8C(c)1.5C-1CC-0.8C(d)1.5C-1C-0.8CCFig.18Effectsoffuel-airratioonpatternfactorfordifferenttripleswirlers2106推进技术2016年2011-107.
[4] BrundishKD,MillerMN,MorganLC,etal.VariableFuelPlacementInjectorDevelopment[R].ASME2003-GT-38417.
[5] MorganLC,WheatleyAJ,BrundishKD.DevelopmentofaVariableFuelPlacementAirblastAtomizer[R].ASME2001-GT-0377.
[6] FoustMJ,ThomsenD,SticklesR.DevelopmentoftheGEAviationLowEmissionsTAPSCombustorforNextGenerationAircraftEngines[R].AIAA2012-0936.
[7] LazikW,DoerrT,BakeS,etal.DevelopmentofLean-BurnLow-NOxCombustionTechnologyatRolls-RoyceDeutschland[R].ASME2008-GT-51115.
[8] LiGQ,AngierS,LambolezO,etal.ExperimentalStudyofVelocityFlowFieldforaMultipleSwirlSprayCombustor[R].AIAA2002-0618.
[9] LiGQ,GutmarkEJ.CombustionCharacteristicsofaMultipleSwirlSprayCombustor[R].AIAA2003-0489.
[10] 刘百磷,林宇震,袁怡祥,等.高温升燃烧室贫油熄火稳定性研究[J].推进技术,2003,24(5):456-459.(LIUBai-lin,LINYu-zhen,YUANYi-xiang,etal.ResearchontheLeanBlow-OutStabilitiesoftheHighTemperatureRiseCombustor[J].JournalofPropulsionTechnology,2003,24(5):456-459.)
[11] 袁怡祥,林宇震,刘高恩.三旋流器头部燃烧室拓宽燃烧稳定工作范围的研究[J].航空动力学报,2004,19(1):142-147.
[12] PengYH,XuQH,LinYZ.ExperimentalStudiesofthePrimaryZoneFlowFieldandCombustionPerformanceofaTripleSwirlerCombustor[R].ASME-GT2005-68218.
[13] 吴治永,林宇震,刘高恩,等.基于CFD分析改进三旋流燃烧室头部设计[J].推进技术,2009,30(5):533-537.(WUZhi-yong,LINYu-zhen,LIUGaoen,etal.DomeStructureModificationofaHighTemperatureRiseCombustorBasedonCFDSimulation[J].JournalofPropulsionTechnology,2009,30(5):533-537.)
[14] 常峰,索建秦,梁红侠,等.同心圆式主副模分区燃烧组织燃烧室数值研究[J].推进技术,2012,33(5):760-764.(CHANGFeng,SUOJian-qin,LIANGHong-xia,etal.NumericalStudyofCo-AxialPilotandMainModuleCombustor[J].JournalofPropulsionTechnology,2012,33(5):760-764.)
[15] 王铮钧,索建秦,黎明,等.基于LPP的多点喷射低污染燃烧室头部方案优化研究[J].推进技术,2015,36(7):1036-1045.(WANGZheng-jun,SUOJian-qin,LIMing,etal.OptimizedStudyofaDomeforLowEmissionCombustorwithMultipointInjectionBasedonLPP[J].JournalofPropulsionTechnology,2015,36(7):1036-1045.)
[16] LiuFQ,MuY,LiuCX,etal.EffectofFuelStagedProportiononNOxEmissionPerformanceofCentrallyStagedCombustor[R].ASME2013-GT-94299.
[17] 万斌,程明,张成凯,等.三旋流单头部燃烧室点火特性的试验研究[C].沈阳:中国航空学会第八届动力年会,2014.
[18] DingGY,HeXM,ZhaoZQ,etal.EffectofDifferentTripleSwirlersonthePerformanceofaTripleSwirlerCombustor[J].ProceedingsoftheInstitutionofMechanicalEngineers,PartG:JournalofAerospaceEngineering,2015,229(1):26-37.
[19] DingGY,HeXM,ZhaoZQ,etal.EffectofDilutionHolesonthePerformanceofaTripleSwirlerCombustor[J].ChineseJournalofAeronautics,2014,27(6):1421-1429.
[20] 丁国玉,安伯堃,何小民,等.三级轴向旋流器燃烧室的贫油熄火特性试验[J].航空动力学报,2015,30(2):356-361.
[21] 丁国玉,何小民,赵自强,等.三级轴向旋流器影响燃烧室性能的试验[J].航空动力学报,2015,30(3):686-693.
[22] 丁国玉,何小民,赵自强,等.油气及进口参数对三级旋流器燃烧室性能的影响[J].航空动力学报,2015,30(1):53-58.
[23] 丁国玉,何小民,薛冲,等.头部及掺混孔对三级旋流器燃烧室出口温度分布影响的试验[J].航空动力学报,2015,30(4):807-813.
[24] 丁国玉,何小民,赵自强,等.无掺混孔三级旋流器燃烧室燃烧性能试验[J].航空动力学报,2014,29(12):2868-2873.(编辑:张荣莉)
|
