|
|||||
|
|
| 冲压发动机燃烧室点火性能试验 | |
| 引用本文： | 李春光,吉洪湖,王健,张振家. 冲压发动机燃烧室点火性能试验[J]. 推进技术, 2011, 32(4): 530-533 |
| 作者姓名： | 李春光 吉洪湖 王健 张振家 |
| 作者单位： | 1. 南京航空航天大学能源与动力学院,江苏南京210016／中国航天科工集团三十一研究所高超声速冲压发动机技术重点实验室,北京100074 2. 南京航空航天大学能源与动力学院,江苏南京,210016 3. 中国航天科工集团三十一研究所高超声速冲压发动机技术重点实验室,北京,100074 |
| 摘 要： | 对具有四个旁侧进气道带机械火焰稳定装置的整体式冲压喷气发动机的起动点火性能进行了试验研究,分析了点火能量、稳定器槽宽、来流温度、点火余气系数等因素对冲压燃烧室的点火延迟时间的影响。研究表明,点火能量是影响冲压燃烧室点火起动的重要因素,通过提高点火能量可以实现冲压发动机的快速点火起动;另外,稳定系数越高,点火余气系数对应的燃烧效率越高,发动机点火越容易。 |
| 关 键 词： | 冲压喷气发动机 燃烧室 火焰稳定器 点火试验 点火延迟 |
| 收稿时间： | 2011-01-12 |
| 修稿时间： | 2011-06-15 |
Experiments on ignition performance of ramjet combustor |
|
| LI Chun-guang,JI Hong-hu,WANG Jian and ZHANG Zhen-jia. Experiments on ignition performance of ramjet combustor[J]. Journal of Propulsion Technology, 2011, 32(4): 530-533 | |
| Authors: | LI Chun-guang JI Hong-hu WANG Jian ZHANG Zhen-jia |
| Affiliation: | LI Chun-guang 1,2,JI Hong-hu1,WANG Jian2,ZHANG Zhen-jia2(1.Coll.of Energy and Power,Nanjing Univ.of Aeronautics and Astronautics,Nanjing 210016,China,2.Science and Technology on Scramjet Lab.,The 31st Research Inst.of CASIC,Beijing 100074,China) |
| Abstract: | The experimental investigations on the ignition performance of an integrated ramjet engine with 4-side inlets were performed as well as a flame stabilization device.The influence of the ignition energy supplied,the gut width of the stabilizer,the coming flow temperature and the equivalence ratio on the ignition response time for the ramjet were studied.The results indicated that the ignition energy is an important factor for the ignition and starting of the ramjet combustor.The increase of the ignition ener... |
| Keywords: | Ramjet engine Combustion chamber Flame holder Ignition test Ignition delay |
| 本文献已被 CNKI 万方数据 等数据库收录！ | |
| 点击此处可从《推进技术》浏览原始摘要信息 | |
| 点击此处可从《推进技术》下载全文 | |