Research into the restoration method for high-altitude piston engine

XU Bin; LIANG Zheng-yue

Volume 24 Issue 8

Aug. 2009

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Article Navigation > Journal of Aerospace Power > 2009 > 24(8): 1736-1740

XU Bin, LIANG Zheng-yue. Research into the restoration method for high-altitude piston engine[J]. Journal of Aerospace Power, 2009, 24(8): 1736-1740.

Citation:

XU Bin, LIANG Zheng-yue. Research into the restoration method for high-altitude piston engine[J]. Journal of Aerospace Power, 2009, 24(8): 1736-1740.

XU Bin, LIANG Zheng-yue. Research into the restoration method for high-altitude piston engine[J]. Journal of Aerospace Power, 2009, 24(8): 1736-1740.

Citation:

XU Bin, 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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Research into the restoration method for high-altitude piston engine

School of Transportation Science and Engineering, Beijing University of Aeronautics and Astronautics, Beijing 100191, China

Received Date: 2008-07-25
Rev Recd Date: 2008-12-08
Publish Date: 2009-08-28

Abstract

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.
- small unmanned aerial vehicle(UAV),
- piston power unit,
- two-stage supercharging,
- simulation calculation