A high-temperature frameless starter-generator integrated into an aircraft engine

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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


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