| Title: | Метод охлаждения лопаток турбин газотурбинных установок и газотурбинных двигателей на новом физическом принципе – явлении термоэлектронной эмиссии |
| Other Titles: | Method of cooling of turbine blades of gas-turbine plants and gas-turbine engines on a new physical approach – the phenomenon of thermionic issue |
| Authors: | Колычев, А.В. Керножицкий, В.А. |
| Issue Date: | 2016 |
| Publisher: | Самарский университет |
| Citation: | Материалы докладов междунар. науч.-техн. конф. 22-24 июня 2016 г. Ч. 1, с. 197-198 |
| Abstract: | Article is devoted a new method and the device of cooling of turbine blades of Gas-turbine plants (GTP), Gasturbine engines (GTE), Pumping gas assembly (PGA) and Gas Turbine Converters (GTC) of Space vehicles (SV), based on a physical principle new in given subject domain - the phenomenon of thermionic issue - electron emission by heated metal. Implementation of a method and the device of thermoissue cooling of turbine blades allows to increase simultaneously reliability, durability GTP, GTE, PGA and GTС of SV and thus is essential to raise their EFFICIENCY. |
| Description: | УДК 621.45 |
| URI: | http://repo.ssau.ru/jspui/handle/123456789/14308 |
| ISBN: | 978-5-7883-1084-8 |
| Appears in Collections: | Проблемы и перспективы развития двигателестроения |
Files in This Item:
| File | Description | Size | Format | |
|---|---|---|---|---|
| 197-198.pdf | Основная статья | 144.59 kB | Adobe PDF | View/Open |
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