电邮这篇文章 Comparison of two configurations of a starter-generator integrated into the aircraft engine
- 作者: Ismagilov F.R.1, Khairullin I.K.1, Vavilov V.E.1, Yakupov A.M.1
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隶属关系:
- Ufa State Aviation Technical University
- 期: 卷 60, 编号 3 (2017)
- 页面: 463-468
- 栏目: Aircraft and Rocket Engine Design and Development
- URL: https://journals.rcsi.science/1068-7998/article/view/230235
- DOI: https://doi.org/10.3103/S1068799817030217
- ID: 230235
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详细
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.
作者简介
F. Ismagilov
Ufa State Aviation Technical University
Email: aynurpov@mail.ru
俄罗斯联邦, ul. Karla Marksa 12, Ufa, Bashkorstan, 450000
I. Khairullin
Ufa State Aviation Technical University
Email: aynurpov@mail.ru
俄罗斯联邦, ul. Karla Marksa 12, Ufa, Bashkorstan, 450000
V. Vavilov
Ufa State Aviation Technical University
Email: aynurpov@mail.ru
俄罗斯联邦, ul. Karla Marksa 12, Ufa, Bashkorstan, 450000
A. Yakupov
Ufa State Aviation Technical University
编辑信件的主要联系方式.
Email: aynurpov@mail.ru
俄罗斯联邦, ul. Karla Marksa 12, Ufa, Bashkorstan, 450000
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