| 活塞发动机高空动力恢复方法的探索研究 |
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| 引用本文： | 徐斌.活塞发动机高空动力恢复方法的探索研究[J].航空动力学报,2009,24(8). |
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| 作者姓名： | 徐斌 |
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| 作者单位： | 北京航空航天大学 交通科学与工程学院 |
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| 摘 要： | 本文分析了新一代无人机动力的发展，针对小型无人机的活塞式动力装置的性能特点，提出了一种小型无人机二级增压系统匹配的高空实现方法。并对发动机的高空性能进行了初步分析，验证了方案的可行性，为高空无人机动力设计提供了设计依据。
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| 关 键 词： | 小型无人机 活塞动力装置 二级增压 模拟计算 |
| 收稿时间： | 7/25/2008 4:17:37 PM |
Research into the method of restoration for high-altitude piston engine |
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| Xu Bin.Research into the method of restoration for high-altitude piston engine[J].Journal of Aerospace Power,2009,24(8). |
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| Authors: | Xu Bin |
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| Institution: | Dept. of Transport Science and Engineering, Bei Hang University |
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| Abstract: | In this paper, the power development of a new generation of UAV has been analyzed, for the performance characteristics of the small UAV is powered by the piston devices, a method that small UAV is carried out for two-stage supercharging system designed to match for achieving at high altitude. A preliminary analysis on the high-altitude performance of engine, verify the feasibility of the programme, provide the design basis for high-altitude UAV. |
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| Keywords: | small UAV piston power unit two-stage supercharging simulation calculation |
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