Paper
13 May 2024 An approach of hybrid power and propulsion system design and performance comparison on a long-range compound-wing unmanned aerial vehicle
Bojian Chen, Xiaojie Wu, Zezhao Wang, Pengpeng Xu
Author Affiliations +
Proceedings Volume 13159, Eighth International Conference on Energy System, Electricity, and Power (ESEP 2023); 1315994 (2024) https://doi.org/10.1117/12.3024438
Event: Eighth International Conference on Energy System, Electricity and Power (ESEP 2023), 2023, Wuhan, China
Abstract
Research has found that using a series hybrid power system instead of a pure electric propulsion system is one of the most effective waysto improve the endurance capabilities of vertical take-off and landing (VTOL) fixed-wing unmanned aircraft systems (UAS), without changing the external power layout. A design scheme for a hybrid power system for UAVs is proposed in this paper, and the relationship between key data such as airspeed, cruise range, and fuel consumption is established based on ground experiments. A simulation model is built to verify the system under specific working conditions, which strengthens the practical application ability of fixed-wing unmanned aerial systems.
(2024) Published by SPIE. Downloading of the abstract is permitted for personal use only.
Bojian Chen, Xiaojie Wu, Zezhao Wang, and Pengpeng Xu "An approach of hybrid power and propulsion system design and performance comparison on a long-range compound-wing unmanned aerial vehicle", Proc. SPIE 13159, Eighth International Conference on Energy System, Electricity, and Power (ESEP 2023), 1315994 (13 May 2024); https://doi.org/10.1117/12.3024438
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KEYWORDS
Batteries

Unmanned aerial vehicles

Design

Power consumption

Ice

Combustion

Power grids

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