Abstract
An optimal design of the starter-generator integrated into aircraft engines is studied. The authors give a review for modern designs and technical solutions of the problem.
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Original Russian Text © F.R. Ismagilov, I.Kh. Khairullin, V.E. Vavilov, A.M. Yakupov, 2017, published in Izvestiya VUZ, Aviatsionnaya Tekhnika, 2017, No. 3, pp. 133–137.
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Ismagilov, F.R., Khairullin, I.K., Vavilov, V.E. et al. Comparison of two configurations of a starter-generator integrated into the aircraft engine. Russ. Aeronaut. 60, 463–468 (2017). https://doi.org/10.3103/S1068799817030217
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DOI: https://doi.org/10.3103/S1068799817030217