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厘米级微型蒸发管式燃烧室性能实验研究
引用本文:熊庆荣,雷雨冰,黄国平,梁德旺.厘米级微型蒸发管式燃烧室性能实验研究[J].航空动力学报,2007,22(5):733-738.
作者姓名:熊庆荣  雷雨冰  黄国平  梁德旺
作者单位:南京航空航天大学,能源与动力学院,南京,210016
基金项目:国家自然科学基金 , 国防科技应用基础研究基金
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.

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
文章编号:1000-8055(2007)05-0733-06
收稿时间:5/8/2006 12:00:00 AM
修稿时间:2006年5月8日

Experimental research on a centimeter-scale micro combustor with vaporizing tube
XIONG Qing-rong,LEI Yu-bing,HUANG Guo-ping and LIANG De-wang.Experimental research on a centimeter-scale micro combustor with vaporizing tube[J].Journal of Aerospace Power,2007,22(5):733-738.
Authors:XIONG Qing-rong  LEI Yu-bing  HUANG Guo-ping and LIANG De-wang
Institution:College of Energy and Power Engineering, Nanjing University ofAeronautics and Astronautics, Nanjing 210016, China;College of Energy and Power Engineering, Nanjing University ofAeronautics and Astronautics, Nanjing 210016, China;College of Energy and Power Engineering, Nanjing University ofAeronautics and Astronautics, Nanjing 210016, China;College of Energy and Power Engineering, Nanjing University ofAeronautics and Astronautics, Nanjing 210016, China
Abstract: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.
Keywords:aerospace propulsion system  micro combustor  vaporizing tube  combustion efficiency  experimental research
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