A high-temperature frameless starter-generator integrated into an aircraft engine
- Authors: Ismagilov F.R.1, Khairullin I.K.1, Vavilov V.E.1, Farrakhov D.R.1, Yakubov A.M.1, Bekuzin V.I.1
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Affiliations:
- Ufa State Aviation Technical University
- Issue: Vol 59, No 1 (2016)
- Pages: 107-111
- Section: 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
Cite item
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.
About the authors
F. R. Ismagilov
Ufa State Aviation Technical University
Email: aynurpov@mail.ru
Russian Federation, ul. Karla Marksa 12, Ufa, 450000
I. Kh. Khairullin
Ufa State Aviation Technical University
Email: aynurpov@mail.ru
Russian Federation, ul. Karla Marksa 12, Ufa, 450000
V. E. Vavilov
Ufa State Aviation Technical University
Email: aynurpov@mail.ru
Russian Federation, ul. Karla Marksa 12, Ufa, 450000
D. R. Farrakhov
Ufa State Aviation Technical University
Email: aynurpov@mail.ru
Russian Federation, ul. Karla Marksa 12, Ufa, 450000
A. M. Yakubov
Ufa State Aviation Technical University
Author for correspondence.
Email: aynurpov@mail.ru
Russian Federation, ul. Karla Marksa 12, Ufa, 450000
V. I. Bekuzin
Ufa State Aviation Technical University
Email: aynurpov@mail.ru
Russian Federation, ul. Karla Marksa 12, Ufa, 450000