A high-temperature frameless starter-generator integrated into an aircraft engine
- Autores: Ismagilov F.1, Khairullin I.1, Vavilov V.1, Farrakhov D.1, Yakubov A.1, Bekuzin V.1
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Afiliações:
- Ufa State Aviation Technical University
- Edição: Volume 59, Nº 1 (2016)
- Páginas: 107-111
- Seção: 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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Resumo
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.
Sobre autores
F. Ismagilov
Ufa State Aviation Technical University
Email: aynurpov@mail.ru
Rússia, ul. Karla Marksa 12, Ufa, 450000
I. Khairullin
Ufa State Aviation Technical University
Email: aynurpov@mail.ru
Rússia, ul. Karla Marksa 12, Ufa, 450000
V. Vavilov
Ufa State Aviation Technical University
Email: aynurpov@mail.ru
Rússia, ul. Karla Marksa 12, Ufa, 450000
D. Farrakhov
Ufa State Aviation Technical University
Email: aynurpov@mail.ru
Rússia, ul. Karla Marksa 12, Ufa, 450000
A. Yakubov
Ufa State Aviation Technical University
Autor responsável pela correspondência
Email: aynurpov@mail.ru
Rússia, ul. Karla Marksa 12, Ufa, 450000
V. Bekuzin
Ufa State Aviation Technical University
Email: aynurpov@mail.ru
Rússia, ul. Karla Marksa 12, Ufa, 450000