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| 无人机和巡航导弹用涡扇/涡喷发动机的设计特点 | |
| 引用本文： | 郭琦,李兆庆. 无人机和巡航导弹用涡扇/涡喷发动机的设计特点[J]. 燃气涡轮试验与研究, 2007, 20(2): 58-62 |
| 作者姓名： | 郭琦 李兆庆 |
| 作者单位： | 中国燃气涡轮研究院,四川,成都,610500;中国燃气涡轮研究院,四川,成都,610500 |
| 摘 要： | 无人机和巡航导弹发动机有许多共性,人们有时候会把它们混淆。本文详细分析了无人机和巡航导弹的区别,对比研究了它们对发动机的要求和关键属性,随后分析了无人机和巡航导弹对涡扇/涡喷发动机的特殊要求与设计特性,以及目前正在开发的先进技术。 |
| 关 键 词： | 涡扇发动机 设计特点 无人飞行器 巡航导弹 |
| 文章编号： | 24488806 |
| 修稿时间： | 2006-07-07 |
Design Characteristics of Turbofan/Turbojet engines for UAV/Cruise Missile Application |
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| GUO Qi,LI Zhao-qing. Design Characteristics of Turbofan/Turbojet engines for UAV/Cruise Missile Application[J]. Gas Turbine Experiment and Research, 2007, 20(2): 58-62 | |
| Authors: | GUO Qi LI Zhao-qing |
| Affiliation: | China Gas Turbine Establishment, Chengdu 610500,China |
| Abstract: | Cruise missiles are occasionally confused with UAVs because they are both unmanned.Their distinctions are clearly made in this paper.The requirements and key attributes of engines for UAV/cruise missile applications are introduced.The special requirements and design characteristics are subsequently analyzed,and the advenced technologies under development currently are also described. |
| Keywords: | turbofan engines design characteristics UAVs cruise missiles |
| 本文献已被 CNKI 维普 万方数据 等数据库收录！ | |