N. Tarasov, V. Chirkov, Ilfat A. Kunsbaev, N. Nalivayko
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Synchronous motor with direct launch for fuel transfer pumps
This article presents the prospects for using synchronous motors with permanent magnets and with a short-circuited winding on the rotor as part of a fuel pump for aerospace equipment. The article also presents the results of computer modeling and experimental verification of engine data.