Abstract
In this paper, a starter-generator (SG) integrated into an aircraft gas turbine engine (GTE) is presented. Operating modes of the SG under different temperature conditions are described.
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Original Russian Text © F.R. Ismagilov, I.Kh. Khairullin, V.E. Vavilov, D.R. Farrakhov, A.M. Yakupov, V.I. Bekuzin, 2016, published in Izvestiya VUZ, Aviatsionnaya Tekhnika, 2016, No. 1, pp. 98–102.
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Ismagilov, F.R., Khairullin, I.K., Vavilov, V.E. et al. A high-temperature frameless starter-generator integrated into an aircraft engine. Russ. Aeronaut. 59, 107–111 (2016). https://doi.org/10.3103/S1068799816010177
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DOI: https://doi.org/10.3103/S1068799816010177