WAN Zhongmin, QUAN Wenxiang, YAN Hanzhang, CHEN Xi, HUANG Taiming, ZHANG Yan, ZHANG Jing, KONG Xiangzhong. Performance analysis of fuel cell system for unmanned aerial vehicle[J]. CIESC Journal, 2019, 70(S2): 329-335
WAN Zhongmin, QUAN Wenxiang, YAN Hanzhang, CHEN Xi, HUANG Taiming, ZHANG Yan, ZHANG Jing, KONG Xiangzhong. Performance analysis of fuel cell system for unmanned aerial vehicle[J]. CIESC Journal, 2019, 70(S2): 329-335DOI: 10.11949/0438-1157.20190597.
Performance analysis of fuel cell system for unmanned aerial vehicle
The biggest technical difficulty in developing small drones is to solve the problems of their power systems. In order to maintain the flight of aircraft
the power system of small drone also provides energy for the airborne equipment. Therefore
the unmanned aerial vehicle (UAV) power unit requires a small volume with high energy density
and can be easily and efficiently converted into thrust force. In this paper
proton exchange membrane fuel cell (PEMFC) is used as the power source candidate of the UAV. Based on the PEMFC stack model and the environmental model
numerical simulations were conducted by Matlab to investigate the effect of altitude on operation status and thermodynamic performance of PEMFC system. The results indicated that as the height increases
the variations of system output voltage
output electric power and system electrical efficiency exhibit a downward trend. When the height is constant
the output power of the system has the highest value with the rise of current density
but the output voltage of the stack and the output efficiency of the system decrease. Moreover
it has been found that the increase of the hydrogen inlet pressure intensifies the output voltage
electric power and electrical efficiency of the system. For the purpose of performance improvement of PEMFC system at a certain height
it is necessary to select a suitable current density and a high hydrogen inlet pressure.
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