厘米级微型蒸发管式燃烧室性能实验研究  

Experimental research on a centimeter-scale micro combustor with vaporizing tube

作　　者：熊庆荣[1] 雷雨冰[1] 黄国平[1] 梁德旺[1] 

机构地区：[1]南京航空航天大学能源与动力学院,南京210016

出　　处：《航空动力学报》2007年第5期733-738,共6页Journal of Aerospace Power

基　　金：国家自然科学基金(编号:1077011);国防基础研究重点项目(编号:K1601060711)的资助

摘　　要：为了了解和掌握厘米级蒸发管式微型燃烧室性能,并为以后的设计提供技术数据,设计了微型燃烧室实验和测试系统,在常温常压下开展了微型燃烧室性能实验,获得了微型燃烧室的阻力特性、贫油熄火特性、燃烧效率、比容热强度和出口温度分布等数据.A micro combustor experimental and testing system was designed to learn the performance of centimeter-scale micro combustor with vaporizing tube,and also provide some technical data for subsequent design. Under room temperature and pressure, the performance of micro combustion combustor was tested, during which some data were made available, such as ： resistance characteristic, weak extinction characteristic, combustion efficiency, specific volume calorific intensity and exit temperature distribution.

关 键 词：航空 航天推进系统 微型燃烧室 蒸发管 燃烧效率 实验研究 

分 类 号：V231.2[航空宇航科学与技术—航空宇航推进理论与工程]