实验流体力学
實驗流體力學
실험류체역학
JOURNAL OF EXPERIMENTS IN FLUID MECHANICS
2014年
1期
44-48
,共5页
脉冲爆轰发动机%文氏管%雾化混合%两相爆轰%爆燃转爆轰
脈遲爆轟髮動機%文氏管%霧化混閤%兩相爆轟%爆燃轉爆轟
맥충폭굉발동궤%문씨관%무화혼합%량상폭굉%폭연전폭굉
pulse detonation engine%venturi%atomization and mixing%two-phase detonation%deflagration to detonation transition
为了研究喷嘴位置对脉冲爆轰发动机性能的影响,设计加工了直径为80mm的汽油/空气两相脉冲爆轰发动机(PDE),在PDE文氏管内不同位置安装喷嘴,进行了冷态雾化和热态燃烧转爆轰试验,分析了马尔文激光粒度仪测得的液滴尺寸分布和动态压力传感器测得的信号。试验结果表明:喷嘴的安装位置对脉冲爆轰发动机的性能具有显著影响;喷嘴安装在文氏管喉部时爆轰管内雾化混合效果最好,爆轰波峰值压力最大为3.5 MPa,工作频率最高为30Hz;喷嘴安装在文氏管入口时爆轰管内雾化混合效果最差,爆轰波峰值压力最小为0.9MPa,工作频率最低为15 Hz;在试验范围内,改善雾化混合效果有利于提高脉冲爆轰发动机的工作频率。研究结果对脉冲爆轰发动机的设计具有参考价值。
為瞭研究噴嘴位置對脈遲爆轟髮動機性能的影響,設計加工瞭直徑為80mm的汽油/空氣兩相脈遲爆轟髮動機(PDE),在PDE文氏管內不同位置安裝噴嘴,進行瞭冷態霧化和熱態燃燒轉爆轟試驗,分析瞭馬爾文激光粒度儀測得的液滴呎吋分佈和動態壓力傳感器測得的信號。試驗結果錶明:噴嘴的安裝位置對脈遲爆轟髮動機的性能具有顯著影響;噴嘴安裝在文氏管喉部時爆轟管內霧化混閤效果最好,爆轟波峰值壓力最大為3.5 MPa,工作頻率最高為30Hz;噴嘴安裝在文氏管入口時爆轟管內霧化混閤效果最差,爆轟波峰值壓力最小為0.9MPa,工作頻率最低為15 Hz;在試驗範圍內,改善霧化混閤效果有利于提高脈遲爆轟髮動機的工作頻率。研究結果對脈遲爆轟髮動機的設計具有參攷價值。
위료연구분취위치대맥충폭굉발동궤성능적영향,설계가공료직경위80mm적기유/공기량상맥충폭굉발동궤(PDE),재PDE문씨관내불동위치안장분취,진행료랭태무화화열태연소전폭굉시험,분석료마이문격광립도의측득적액적척촌분포화동태압력전감기측득적신호。시험결과표명:분취적안장위치대맥충폭굉발동궤적성능구유현저영향;분취안장재문씨관후부시폭굉관내무화혼합효과최호,폭굉파봉치압력최대위3.5 MPa,공작빈솔최고위30Hz;분취안장재문씨관입구시폭굉관내무화혼합효과최차,폭굉파봉치압력최소위0.9MPa,공작빈솔최저위15 Hz;재시험범위내,개선무화혼합효과유리우제고맥충폭굉발동궤적공작빈솔。연구결과대맥충폭굉발동궤적설계구유삼고개치。
Pulse detonation engines (PDE)have received the widespread attention in recent years .However,there are many unresolved issues related to PDE.In order to achieve higher lev-els of thrust,PDEs require relatively small times to complete the liquid fuel atomization and mix-ture with air for increasing the operating frequency.But the nozzle location can have influence on the performances of atomization and mixing in PDE.To study the nozzle location on the perform-ances of PDEs,a gasoline/air two phases pulse detonation engine with a diameter of 80mm and a length of 1 .2 m was designed.PDEs consist of a mixing chamber,ignition and detonation cham-ber.And the venturi is installed in the mixing chamber.The experiments of atomization of the liquid fuel and deflagration to detonation transition(DDT)were carried out by installing a nozzle in three different locations of the venturi.The droplet size distribution in front of the ignition chamber measured by Malven laser mastersizer and signals measured by dynamic pressure sensor were analyzed.The experimental results show that the nozzle location has a significant influence on performances of the PDE.When the nozzle is installed in the throat of venturi,PDE has the best gasoline-air distribution(the sauter mean radius is less than 76.9μm),the highest peak pres-sure of detonation wave(3.5MPa at 30Hz,5MPa at 10Hz)and the highest operating frequency (30Hz).When the nozzle is installed in the expanding of venturi,the sauter mean radius is 85. 4μm,the peak pressure of detonation wave is 4.0MPa and the operating frequency is 20Hz. When the nozzle is installed in the entrance of venturi,PDE has the worst gasoline-air distribu-tion(the sauter mean radius is more than 93.4μm),the lowest peak pressure of detonation wave (0.9MPa at 15Hz,1.1MPa at 10Hz)and the lowest operating frequency(15Hz).In the experimental range,the operating frequency can be increased by improving the effect of atomization and mix-ing .The results offer reference for further research of deflagration to detonation transition mech-anism and atomization of the liquid fuel,design and operation of the pulse detonation engine.