Concepts of Gas Turbine Engine Improvement Through the Use of Choked-Flow Turbines
- 作者: Bogdanov V.I.1
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隶属关系:
- Solov’ev Rybinsk State Aviation Technical University
- 期: 卷 61, 编号 2 (2018)
- 页面: 244-251
- 栏目: Aircraft and Rocket Engine Theory
- URL: https://journals.rcsi.science/1068-7998/article/view/230508
- DOI: https://doi.org/10.3103/S1068799818020137
- ID: 230508
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详细
The new conceptual design of simple gas turbine engines for different purposes is presented. A choked-flow low-pressure turbine is used that allows reducing the number of stages and gas temperature in the relative motion ahead of blades. Application of such turbines with uncooled blades to reduce the cost of power-limited engines is considered.
作者简介
V. Bogdanov
Solov’ev Rybinsk State Aviation Technical University
编辑信件的主要联系方式.
Email: bogdanov-vasiliy@yandex.ru
俄罗斯联邦, ul. Pushkina 53, Rybinsk, 152934
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