CAJ | 학술논문

为了研究单凹腔驻涡燃烧室的点火和贫油熄火特性，设计了一个带扩压器和内外机匣的单凹腔驻涡燃烧室矩形试验件，采用试验研究和半经验分析相结合的方法对其点火和贫油熄火进行了研究。试验在常压状态下进行，采用RP3航空煤油作为燃料，所用供油喷嘴为空心锥离心喷嘴，试验中的进口空气温度在287～487K变化，进口空气流量在0.2109～0.4219kg/s变化，对应进口马赫数从0.15变化到0.31。结果表明：单凹腔驻涡燃烧室的点火和贫油熄火油气比均随着燃烧室进口温度和进口流量的增加而减小，单凹腔驻涡燃烧室的点火油气比比贫油熄火油气比约大50%。经过半经验分析，得到了影响单凹腔点火和熄火的综合参数A，该参数能够较好地解释和评价各种因素对贫油熄火的影响。
위료연구단요강주와연소실적점화화빈유식화특성，설계료일개대확압기화내외궤갑적단요강주와연소실구형시험건，채용시험연구화반경험분석상결합적방법대기점화화빈유식화진행료연구。시험재상압상태하진행，채용RP3항공매유작위연료，소용공유분취위공심추리심분취，시험중적진구공기온도재287～487K변화，진구공기류량재0.2109～0.4219kg/s변화，대응진구마혁수종0.15변화도0.31。결과표명：단요강주와연소실적점화화빈유식화유기비균수착연소실진구온도화진구류량적증가이감소，단요강주와연소실적점화유기비비빈유식화유기비약대50%。경과반경험분석，득도료영향단요강점화화식화적종합삼수A，해삼수능구교호지해석화평개각충인소대빈유식화적영향。
A rectangular single-cavity trapped vortex combustor(STVC)comprising casing and diffuser was designed,and ignition and lean blowout characteristic experiments were accomplished at atmospheric pressure, and semi-analytical results were obtained. Aviation kerosene RP3 was employed as fuel,and cone-shaped pres?sure swirl atomizer was used for fuel supply. In all the operating conditions,inlet temperature of the combustor varies from 287K up to 487K,and inlet air mass flow rate ranges from 0.2109kg/s up to 0.4219kg/s,the corre?sponding Mach number ranges from 0.15 to 0.31. It is revealed that the fuel air ratios of ignition and lean blowout decrease while inlet temperature and air mass flow rate increase,and the former is approximately 50%more than the latter. A synthesized parameter,that affects ignition and lean blowout characteristics of the single-cavity trapped vortex combustor,is derived in a semi-empirical method. This parameter can well interpret and estimate the effects of various factors on lean blowout.