Design of an Inflight Power Generation and Storage System for Use in UAVs

被引:0
作者
Dobbs, Steven [1 ]
Yu, Zhen [2 ]
Anderson, Kevin R. [3 ]
Franco, Jonathan A. [1 ]
Deravanessian, Alexander E. [3 ]
Lin, Albert [3 ]
Ahn, Andrew [3 ]
机构
[1] Calif State Polytech Univ Pomona, Dept Aerosp Engn, Pomona, CA 91768 USA
[2] Calif State Polytech Univ Pomona, Dept Elect & Comp Engn, Pomona, CA 91768 USA
[3] Calif State Polytech Univ Pomona, Dept Mech Engn, Pomona, CA 91768 USA
来源
2018 IEEE CONFERENCE ON TECHNOLOGIES FOR SUSTAINABILITY (SUSTECH) | 2018年
关键词
UAV; power generation; piezo; super-capacitor; Li-Ion battery;
D O I
暂无
中图分类号
X [环境科学、安全科学];
学科分类号
08 ; 0830 ;
摘要
This paper describes the design of an inflight power generation, management and storage system applicable to Unmanned Air Vehicles (UAV). Emerging UAV, drones and other aircraft can use electrical propulsion systems. To extend battery charge and aircraft range, power can be generated from multiple sources during flight including aero-elastic vibrations from gusts and flutter, and bending movements and sunlight These sources of "free" energy can be summed and used during flight operation. This research will employ the aero-elastic vibrations of the wing that will be captured using motor generator created devices that uses vibrations to generate electricity. Stress flexing piezoelectric devices will be attached at the root of the wing, where the most bending strain occurs. Flexible solar panels are collocated to the top of UAV wing to enhance energy harvesting. These three sources will be summed together to power the propeller of an aircraft. A Maximum Power Point Tracker (MPPT) hoard is utilized to adjust the input voltage to harvest power from the wing vibration phenomenon and transform this power to supply the voltage requirements of the battery or graphene super-capacitors under load.
引用
收藏
页码:272 / 279
页数:8
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