气氢/气氧喷注器流量特性实验  

Experimental investigation on flowrate characteristics of gaseous hydrogen/gaseous oxygen injector

作　　者：高玉闪[1] 杜正刚[1] 李茂[1] 蔡国飙[1] 

机构地区：[1]北京航空航天大学宇航学院,北京100191

出　　处：《航空动力学报》2010年第4期841-846,共6页Journal of Aerospace Power

基　　金：国家863基金

摘　　要：针对热试实验所用的两种典型结构气氢/气氧喷注器,开展了不同反压下的流量特性实验.重点考察了燃料喷嘴对氧化剂喷嘴流量特性的影响和压降变化对喷嘴流量特性的影响.研究结果表明：反压从0.2~4 MPa的范围内变化时,双路同时工作时氧化剂喷嘴的流量系数要大于其自身单路工作时的流量系数;氧化剂喷嘴和燃料喷嘴的流量系数均随压降的增大而增大,并且增长趋势逐渐平缓.所得结论对气-气喷注器的设计和改进具有重要意义.Experimental investigation on flowrate characteristics of two different types of GH2/GO2 injectors at different back pressure conditions were used for hot fire test.The effect of the fuel injector on oxidizer injector and the effect of pressure drop on the flowrate characteristics were investigated.The results show that the discharge coefficient of oxidizer injector is bigger than the oxidizer working alone when the oxidizer injector and the fuel injector are simultaneously working,as the back pressure changed from 0.2 MPa to 4 MPa.The discharge coefficient of the oxidizer injector and the fuel injector becomes bigger with the increase of pressure drop,but the trend becomes slower.The results presented in this paper may provide valuable reference for the design and improvement of the gas-gas injector.

关 键 词：气氢/气氧喷注器 流量系数 推进剂 反压 压降 

分 类 号：V431[航空宇航科学与技术—航空宇航推进理论与工程]