航空工程进展
航空工程進展
항공공정진전
ADVANCES IN AERONAUTICAL SCIENCE AND ENGINEERING
2012年
1期
110-115
,共6页
李平%王治武%南向谊%何国强
李平%王治武%南嚮誼%何國彊
리평%왕치무%남향의%하국강
混合器%掺混%加力燃烧室%组合动力
混閤器%摻混%加力燃燒室%組閤動力
혼합기%참혼%가력연소실%조합동력
mixer%mixing%after burner%combined power
合理的混合器结构对组合动力系统的高效燃烧和推进性能具有重要意义。为了获得最佳掺混效果,缩短燃烧室长度,利用CFD程序分别对环形、旋流器型和波瓣混合器中内、外涵燃气/空气的流动和掺混特性进行了全三维数值模拟。燃气为甲烷液氧富燃燃气。结果表明:无论采用何种混合器,随着掺混距离的增加,总温和组分均趋均匀;其中,波瓣混合器的掺混效果最好,内外双旋流型混合器的掺混效果次之,环形混合器的掺混效果较差;环形混合器内涵燃气喷射角度对燃气/空气掺混效果具有一定的影响,燃气与轴向成15°喷射时,掺混效果优于无角度喷射。
閤理的混閤器結構對組閤動力繫統的高效燃燒和推進性能具有重要意義。為瞭穫得最佳摻混效果,縮短燃燒室長度,利用CFD程序分彆對環形、鏇流器型和波瓣混閤器中內、外涵燃氣/空氣的流動和摻混特性進行瞭全三維數值模擬。燃氣為甲烷液氧富燃燃氣。結果錶明:無論採用何種混閤器,隨著摻混距離的增加,總溫和組分均趨均勻;其中,波瓣混閤器的摻混效果最好,內外雙鏇流型混閤器的摻混效果次之,環形混閤器的摻混效果較差;環形混閤器內涵燃氣噴射角度對燃氣/空氣摻混效果具有一定的影響,燃氣與軸嚮成15°噴射時,摻混效果優于無角度噴射。
합리적혼합기결구대조합동력계통적고효연소화추진성능구유중요의의。위료획득최가참혼효과,축단연소실장도,이용CFD정서분별대배형、선류기형화파판혼합기중내、외함연기/공기적류동화참혼특성진행료전삼유수치모의。연기위갑완액양부연연기。결과표명:무론채용하충혼합기,수착참혼거리적증가,총온화조분균추균균;기중,파판혼합기적참혼효과최호,내외쌍선류형혼합기적참혼효과차지,배형혼합기적참혼효과교차;배형혼합기내함연기분사각도대연기/공기참혼효과구유일정적영향,연기여축향성15°분사시,참혼효과우우무각도분사。
The mixer configuration has an important effect on the combustion and propulsive performance of the combined power system.In order to obtain the best mixing performance and reduce the combustor length,the mixer optimization based on numerical simulation is addressed.The flow of gas/air and mixing characteristic inside three different mixers are obtained from three-dimensional CFD simulation.The annular mixer,swirl mixer and lob mixer are designed and used here.The burnt gas from inner flow passage is rich methane/O2(l)burnt gas,while air flows by the by-bass.The simulation results indicate that no matter which mixer is used,the total temperature and species distribution turn to be uniform with the mixing length increasing.The best mixing performance occurrs in the lob mixer,and secondary mixing performance occurrs in the swirl mixer,while the annular mixer is of the worst mixing performance.The injection angle of burnt gas is of considerable effect on the mixing performance.The mixing performance with injection angle of 15 degree is better than that with injection angle of zero.