| DDK-1自动点火起动装置在涡喷发动机模拟空中点火起动试验中的应用 |
| |
| 引用本文： | 朱青,范晓宏. DDK-1自动点火起动装置在涡喷发动机模拟空中点火起动试验中的应用[J]. 推进技术, 1990, 11(6): 56-63,77 |
| |
| 作者姓名： | 朱青 范晓宏 |
| |
| 作者单位： | 航空航天部31所(朱青)，重庆航天设计院(范晓宏) |
| |
| 摘 要： | 本文介绍DDK-1自动点火起动装置在某高空台模拟高空情况下,起动与S进气道匹配的某涡喷发动机的试验情况.DDK-1自动点火起动装置使该发动机在空中模拟状态下从点火起动到加速完全实现自动化.这是在国内涡喷发动机高空模拟试验中首次应用.该系统具有实际应用价值.
|
| 关 键 词： | 涡轮喷气发动机 高空模拟 试车台 自动点火 |
AN APPLICATION OF AUTOMATIC IGNITOR DDK-1 TO TURBOJET ENGINE TEST UNDER SIMULATED ALTITUDE CONDITION |
| |
| Zhu Qin The and Fan Xiaohong. AN APPLICATION OF AUTOMATIC IGNITOR DDK-1 TO TURBOJET ENGINE TEST UNDER SIMULATED ALTITUDE CONDITION[J]. Journal of Propulsion Technology, 1990, 11(6): 56-63,77 |
| |
| Authors: | Zhu Qin The and Fan Xiaohong |
| |
| Affiliation: | Zhu Qin (The 31st Research Institute)Fan Xiaohong (The Design Institute of Aerospace of Chong Qing) |
| |
| Abstract: | In this paper, an application of automatic ignitor DDK-1 in tests of turbojet with a s-shape air inlet under simulated altitude condition are intro-ducted. Automatic ignitor DDK-1 is useful for turbojet test in simulated altitude condition. Due to the use of automatic ignitor DDK-1, the process of engine test under high altitude simulation condition from igniting and starting to speeding up is completely automazited. It is the first application of this ignitor to turbojet test under simulated altitude condition in China,and available in pratical applications. |
| |
| Keywords: | Turbojet engine Altitude simulated test cell Autoignition In-flight ignition test Firing unit |
| 本文献已被 CNKI 维普 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》下载免费的PDF全文 |
