首页 | 本学科首页   官方微博 | 高级检索  
     检索      

两种空气/煤油燃气发生器富油燃烧组织方案对比
引用本文:康忠涛,李清廉,张新桥,成鹏.两种空气/煤油燃气发生器富油燃烧组织方案对比[J].航空动力学报,2015,30(8):1997-2003.
作者姓名:康忠涛  李清廉  张新桥  成鹏
作者单位:1. 国防科学技术大学 高超声速冲压发动机技术重点实验室, 长沙 410073;
基金项目:新世纪优秀人才支持计划(NCET-13-0156)
摘    要:根据空气/煤油富油燃烧的特点,提出了两种空气/煤油燃气发生器富油燃烧组织方案,设计了采用钝体稳定火焰和旋流空气、二次喷注空气稳定火焰的两种燃气发生器.为了对比两种方案的点火和燃烧特性,对两种燃气发生器进行了一系列热试,结果表明余氧系数是燃气发生器最重要的工况参数.随着余氧系数的增加,燃气发生器的状态逐渐从启动失败变为中途熄火,最终呈正常启动状态.采用钝体稳定火焰的燃气发生器稳定工作的余氧系数边界为0.518,采用旋流空气和二次喷注空气稳定火焰可将该边界延伸到0.237,极大地扩大了燃气发生器的工作范围.与钝体稳定火焰的燃气发生器相比,旋流空气和二次喷注空气稳定火焰的燃气发生器的富油燃烧的燃烧效率提高了20%.两种方案结构复杂性相当,旋流空气和二次喷注空气稳定火焰的燃气发生器不需要冷却火焰稳定器,可提高燃气发生器的工作时间. 

关 键 词:空气/煤油燃气发生器    富油燃烧    火焰稳定    方案对比    燃烧效率
收稿时间:2014/1/24 0:00:00

Comparison of two fuel-rich combustion schemes in air/kerosene gas generator
KANG Zhong-tao,LI Qing-lian,ZHANG Xin-qiao and CHENG Peng.Comparison of two fuel-rich combustion schemes in air/kerosene gas generator[J].Journal of Aerospace Power,2015,30(8):1997-2003.
Authors:KANG Zhong-tao  LI Qing-lian  ZHANG Xin-qiao and CHENG Peng
Institution:1. Science and Technology on Scramjet Laboratory, National University of Defense Technology, Changsha 410073, China;2. College of Aerospace Science and Engineering, National University of Defense Technology, Changsha 410073, China
Abstract:Two fuel-rich combustion schemes in air/kerosene gas generator were provided, and two gas generators with flame stabilized by bluff-body, swirling air and second air injection respectively were designed based on the fuel-rich combustion characteristics of air/kerosene. A series of hot fire experiments were conducted with two gas generators to compare the ignition and combustion characteristics of the two schemes. The results show that excess oxidizer coefficient is the most important working parameter in gas generator. With the increase of excess oxidizer coefficient, the states of gas generators vary from start failure to abnormal shut up, and finally to normal start. The range of stable working excess oxidizer coefficient in bluff-body stabilized gas generator is 0.518, and can be expanded to 0.237 by stabilizing flame through swirling air and second air injection, which greatly increases the working range of gas generator. The fuel-rich combustion efficiency of swirling air and second air injection stabilized gas generator is 20% higher than that of bluff-body stabilized gas generator. As the complexity of the two schemes is comparable, swirling air and second air injection stabilized gas generator could have a longer working time without cooling the flame holder.
Keywords:air/kerosene gas generator  fuel-rich combustion  flame stabilization  scheme comparison  combustion efficiency
本文献已被 CNKI 万方数据 等数据库收录!
点击此处可从《航空动力学报》浏览原始摘要信息
点击此处可从《航空动力学报》下载免费的PDF全文
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号