摘要
为研究撞击式喷嘴凝胶自燃推进剂着火及火焰特性,在单喷嘴矩形燃烧室内进行了凝胶一甲基肼/四氧化二氮(MMH/NTO)喷雾燃烧过程试验研究。试验采用撞击角为75°、90°、105°的两股互击式喷嘴和撞击角为90°的两股燃料撞击一股氧化剂(F-O-F)、两股氧化剂撞击一股燃料(O-F-O)三股互击式喷嘴,首先结合高速摄影与纹影技术拍摄了燃烧过程纹影图像,随后采用高速摄影直接拍摄了燃烧过程火焰自然辐射发光图像。通过图像处理,提取了火焰着火距离、火焰轴向传播速度、火焰夹角以及反应距离,并分析了喷嘴类型、燃料射流速度的影响。试验结果表明,凝胶MMH/NTO燃烧主要发生在液膜破碎成液丝之后,射流速度越快,燃气扩散速度越快;凝胶MMH/NTO推进剂采用撞击角为105°的两股互击式喷嘴时着火距离最短;凝胶MMH/NTO着火时火焰轴向传播速度随燃料射流速度增加而增加,撞击角为90°时火焰沿喷注面下游传播速度较快;凝胶MMH/NTO稳态燃烧时火焰夹角随燃料射流速度增加而增加,反应距离随燃料射流速度增加而减小,其中撞击角为90°的两股互击式喷嘴火焰夹角最大,撞击角为105°的两股互击式喷嘴反应距离最短。
Aiming at elucidating the detailed ignition and flame characteristics of gelled hypergolic bipropellants utilizing an impinging injector,an experiment is conducted to investigate the combustion processes of gelled Monomethylhydrazine/Nitrogen Tetroxide(MMH/NTO)in a square combustion chamber with a single impinging injector.Unlike-impinging injector,including 75°,90°,and 105°impinging angles,and 90°impinging angle triplet impinging injector,including Fuel-Oxidizer-Fuel(F-O-F)and Oxidizer-Fuel-Oxidizer(O-F-O),are used in the experiment.Schlieren technology and a high-speed camera are combined to investigate the spray and combustion processes firstly,then natural flame images are obtained by a high-speed camera directly.The ignition distance,axial flame speed,flame angle,and induction distance are obtained by image processing technology,and then the effect of injector type and jet velocity of fuel are discussed.The results show that the combustion of gelled MMH/NTO occurrs after liquid sheets breakup into ligaments,and the gas diffusion rate increases with the increasing of fuel jet velocity.The ignition distance of gelled MMH/NTO is the shortest when using the 105°unlike-impinging injector.The axial flame speed increases with the increasing of fuel jet velocity,and it’s quicker when the impinging angle is90°.During the steady combustion,the flame angle increases when the jet velocity of fuel increases,but the induction distance decreases conversely.The flame angle is the maximum when using the 90°unlike-impinging injector,and induction distance is the shortest if using the 105°unlike-impinging injector.
作者
夏益志
王勇
洪流
杨伟东
陈宏玉
XIA Yizhi;WANG Yong;HONG Liu;YANG Weidong;CHEN Hongyu(Science and Technology on Liquid Rocket Engine Laboratory,Xi'an Aerospace Propulsion Institute,Xi'an 71010O,China)
出处
《航空学报》
EI
CAS
CSCD
北大核心
2020年第1期129-138,共10页
Acta Aeronautica et Astronautica Sinica
基金
液体火箭发动机技术重点实验室基金(6142704020203)
关键词
一甲基肼
四氧化二氮
凝胶
互击式喷嘴
着火
火焰
monomethylhydrazine
nitrogen tetroxide
gel
impinging injector
ignition
flame
