Email this article Comparison of two configurations of a starter-generator integrated into the aircraft engine
- Authors: Ismagilov F.R.1, Khairullin I.K.1, Vavilov V.E.1, Yakupov A.M.1
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Affiliations:
- Ufa State Aviation Technical University
- Issue: Vol 60, No 3 (2017)
- Pages: 463-468
- Section: Aircraft and Rocket Engine Design and Development
- URL: https://journal-vniispk.ru/1068-7998/article/view/230235
- DOI: https://doi.org/10.3103/S1068799817030217
- ID: 230235
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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.
About the authors
F. R. Ismagilov
Ufa State Aviation Technical University
Email: aynurpov@mail.ru
Russian Federation, ul. Karla Marksa 12, Ufa, Bashkorstan, 450000
I. Kh. Khairullin
Ufa State Aviation Technical University
Email: aynurpov@mail.ru
Russian Federation, ul. Karla Marksa 12, Ufa, Bashkorstan, 450000
V. E. Vavilov
Ufa State Aviation Technical University
Email: aynurpov@mail.ru
Russian Federation, ul. Karla Marksa 12, Ufa, Bashkorstan, 450000
A. M. Yakupov
Ufa State Aviation Technical University
Author for correspondence.
Email: aynurpov@mail.ru
Russian Federation, ul. Karla Marksa 12, Ufa, Bashkorstan, 450000
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