A high-temperature frameless starter-generator integrated into an aircraft engine
- Авторы: Ismagilov F.1, Khairullin I.1, Vavilov V.1, Farrakhov D.1, Yakubov A.1, Bekuzin V.1
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Учреждения:
- Ufa State Aviation Technical University
- Выпуск: Том 59, № 1 (2016)
- Страницы: 107-111
- Раздел: Aircraft Instruments and Instrumentation Computer Complexes
- URL: https://journals.rcsi.science/1068-7998/article/view/229602
- DOI: https://doi.org/10.3103/S1068799816010177
- ID: 229602
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Аннотация
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.
Об авторах
F. Ismagilov
Ufa State Aviation Technical University
Email: aynurpov@mail.ru
Россия, ul. Karla Marksa 12, Ufa, 450000
I. Khairullin
Ufa State Aviation Technical University
Email: aynurpov@mail.ru
Россия, ul. Karla Marksa 12, Ufa, 450000
V. Vavilov
Ufa State Aviation Technical University
Email: aynurpov@mail.ru
Россия, ul. Karla Marksa 12, Ufa, 450000
D. Farrakhov
Ufa State Aviation Technical University
Email: aynurpov@mail.ru
Россия, ul. Karla Marksa 12, Ufa, 450000
A. Yakubov
Ufa State Aviation Technical University
Автор, ответственный за переписку.
Email: aynurpov@mail.ru
Россия, ul. Karla Marksa 12, Ufa, 450000
V. Bekuzin
Ufa State Aviation Technical University
Email: aynurpov@mail.ru
Россия, ul. Karla Marksa 12, Ufa, 450000