| 变循环发动机组合变几何调节方案 |
| |
| 引用本文： | 骆广琦,李游,刘琨,吴涛,胡砷纛. 变循环发动机组合变几何调节方案[J]. 航空动力学报, 2014, 29(10): 2273-2278 |
| |
| 作者姓名： | 骆广琦 李游 刘琨 吴涛 胡砷纛 |
| |
| 作者单位： | 空军工程大学 航空航天工程学院, 西安 710038;空军工程大学 航空航天工程学院, 西安 710038;空军工程大学 航空航天工程学院, 西安 710038;空军工程大学 航空航天工程学院, 西安 710038;空军工程大学 航空航天工程学院, 西安 710038 |
| |
| 基金项目： | 中航工业发动机支持项目（1402-05） |
| |
| 摘 要： | 基于面向对象的设计思想,设计出了一个双涵道变循环发动机(VCE)的性能计算模型,并选取了双涵道VCE具有代表性的典型工作点,进行了双涵道VCE的组合变几何调节的相关研究.结果表明:在双涵道VCE的亚声速巡航和超声速巡航工作点,合理调节风扇导流叶片角度可以更大程度发挥双涵道VCE性能优势;在亚声速巡航工作点时选取的方案4和超声速巡航工作点时选取的方案4均比双涵道VCE设计点的变几何调节方案性能更优.
|
| 关 键 词： | 变循环发动机 变几何 组合调节 超声速巡航 亚声速巡航 |
| 收稿时间： | 2013-07-22 |
Combined variable geometry regulation schemes for variable cycle engine |
| |
| LUO Guang-qi,LI You,LIU Kun,WU Tao and HU Shen-dao. Combined variable geometry regulation schemes for variable cycle engine[J]. Journal of Aerospace Power, 2014, 29(10): 2273-2278 |
| |
| Authors: | LUO Guang-qi LI You LIU Kun WU Tao HU Shen-dao |
| |
| Affiliation: | Aeronautics and Astronautics Engineering College, Airforce Force Engineering University, Xi'an 710038, China;Aeronautics and Astronautics Engineering College, Airforce Force Engineering University, Xi'an 710038, China;Aeronautics and Astronautics Engineering College, Airforce Force Engineering University, Xi'an 710038, China;Aeronautics and Astronautics Engineering College, Airforce Force Engineering University, Xi'an 710038, China;Aeronautics and Astronautics Engineering College, Airforce Force Engineering University, Xi'an 710038, China |
| |
| Abstract: | Based on object-oriented design thought, a caculation model of double bypass variable cycle engine (VCE) was built, and the typical engine work points were selected to study optimized method of combined variable geometry regulation. The results show that suitable adjustment of fan guide vane angle can adequately develop double bypass VCE performance advantage at subsonic cruise and supersonic cruise points of double bypass VCE. The scheme 4 at the subsonic and supersonic cruise points are all better than adjustment schemes at the design point. |
| |
| Keywords: | variable cycle engine variable geometry combined regulation supersonic cruise subsonic cruise |
| 本文献已被 CNKI 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》下载全文 |
|
