| 活塞发动机高空动力恢复方法的探索 |
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| 引用本文： | 徐斌,梁郑岳.活塞发动机高空动力恢复方法的探索[J].航空动力学报,2009,24(8):1736-1740. |
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| 作者姓名： | 徐斌 梁郑岳 |
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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： | 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,为高空无人机动力装置提供了设计依据.
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| 关 键 词： | small unmanned aerial vehicle（UAV） piston power unit two-stage supercharging simulation calculation |
| 收稿时间： | 2008/7/25 0:00:00 |
| 修稿时间： | 2008/12/8 0:00:00 |
Research into the restoration method for high-altitude piston engine |
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| XU Bin and LIANG Zheng-yue.Research into the restoration method for high-altitude piston engine[J].Journal of Aerospace Power,2009,24(8):1736-1740. |
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| Authors: | XU Bin and LIANG Zheng-yue |
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| Institution: | School of Transportation Science and Engineering;Beijing University of Aeronautics and Astronautics;Beijing 100191;China |
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| Abstract: | The power development of a new generation of unmanned aerial vehicle(UAV) was analyzed.According to the performance characteristic of small UAV powered by the piston devices,a method matching small UAV's two-stage supercharging system was designed for realization at high altitude.A preliminary analysis on the high-altitude performance of engine was conducted to verify the feasibility of the programme,providing a design basis for high-altitude UAV. |
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| Keywords: | small unmanned aerial vehicle (UAV) piston power unit two-stage supercharging simulation calculation |
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