Thermal physics of hydrogen-oxygen combuster chambers for high-temperature turbines combined-cycle power plant
- Authors: Guryanov A.I.1, Piralishvili G.S.1, Vereschagin I.M.1
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Affiliations:
- Rybinsk state academy of aviation technology named after P.A. Solovyev
- Issue: Vol 10, No 3-2 (2011): Special Issue
- Pages: 137-144
- Section: AIRCRAFT AND SPACE ROCKET ENGINEERING
- URL: https://journals.ssau.ru/vestnik/article/view/6797
- DOI: https://doi.org/10.18287/2541-7533-2011-0-3-2(27)-137-144
- ID: 6797
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Abstract
There are presented the results of the numerical modeling hydrogen combustion in oxidizing environment of the premixed steam-oxygen mixture in operating conditions of the promising combustion chambers that can be used as high-temperature steam’s generators for combined cycle power plants. It is defined a geometry of the mixing module, flame stabilizer and primary combustion zone that provides high mixing quality and absence of local zones of overheating construction’s elements of the combustion chamber.
About the authors
A. I. Guryanov
Rybinsk state academy of aviation technology named after P.A. Solovyev
Author for correspondence.
Email: marialex2004@mail.ru
Candidate of Technical Sciences, Associate Professor
Russian FederationG. Sh. Piralishvili
Rybinsk state academy of aviation technology named after P.A. Solovyev
Email: marialex2004@mail.ru
post-graduate student
Russian FederationI. M. Vereschagin
Rybinsk state academy of aviation technology named after P.A. Solovyev
Email: ivan_ver89@mail.ru
student
Russian Federation