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Multi-Disciplinary Design of High-RPM Electric Generator with External Rotor for Unmanned Aerial Vehicle

Vyacheslav Vavilov(1), Flur Ismagilov(2), Irek Khayrullin(3), Ruslan Karimov(4*)

(1) Department of Electromechanics, Ufa State Aviation Technical University, Russian Federation
(2) Department of Electromechanics, Ufa State Aviation Technical University, Russian Federation
(3) Department of Electromechanics, Ufa State Aviation Technical University, Russian Federation
(4) Department of Electromechanics, Ufa State Aviation Technical University, Russian Federation
(*) Corresponding author


DOI: https://doi.org/10.15866/irease.v9i4.10340

Abstract


The article describes the main approaches for the design of high-speed electric generators in unmanned aerial vehicles. Two generators for unmanned aerial vehicles with power of 2.3 and 3.3 kW were calculated at rotor speeds of 48,000 and 60,000 rpm respectively. Losses in these electric generators were estimated, and their heat calculations were made, as well as the calculations of rotor dynamics. The results can be used in practice for the creation of new prospective UAVs.
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Keywords


High-rpm Electric Generator with External Rotor; Unmanned Aerial Vehicle; UAV Power Supply System

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References


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