Engineering Journal: Science and InnovationELECTRONIC SCIENCE AND ENGINEERING PUBLICATION
Certificate of Registration Media number Эл #ФС77-53688 of 17 April 2013. ISSN 2308-6033. DOI 10.18698/2308-6033
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Article

Thermionic method of cooling turbine blades of spacecraft gas turbine converters

Published: 01.06.2016

Authors: Kolychev A.V., Kernozhitskiy V.A.

Published in issue: #5(53)/2016

DOI: 10.18698/2308-6033-2016-5-1495

Category: Power, Metallurgic and Chemical Engineering | Chapter: Turbomachines and Combination Turbine Plants

We describe a device for cooling turbine blades of spacecraft gas turbine converters, based on a new physical principle called thermionic emission, i.e. electrons being emitted by heated metal. This device will allow the reliability and durability of turbine blades of gas turbine converters to be enhanced, and their efficiency factor to be significantly increased, leading to the possibility of creating spacecraft with higher power consumption and longer active functioning perio.


References
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