Numerical study of the parameters of a gas turbine combustion chamber with steam injection operating on distillate fuel-Reference-Cited by-同舟云学术

Numerical study of the parameters of a gas turbine combustion chamber with steam injection operating on distillate fuel

Published:2020-09-17 Issue:0 Volume:0 Page:
ISSN:2191-0332
Container-title:International Journal of Turbo & Jet-Engines
language:en
Short-container-title:

Author:

Serbin Serhiy¹,Burunsuz Kateryna¹

Affiliation:

1. Department of Turbines , Mechanical Engineering Institute of the admiral Makarov National University of Shipbuilding , Mikolayiv , 54025 , Ukraine

Abstract

Abstract Investigations of the working process in a gas turbine combustion chamber with ecological and energy steam injection operating on liquid fuel are conducted. The mathematical model of the aerodynamic processes and liquid fuel combustion in similar burning devices based on the numerical solution of the system of conservation and transport equations for a multi-component chemically reactive turbulent system is developed. The influence of the relative steam mass flow rate (the ratio of the sum of the mass flow rates of ecological and energy steam to the fuel consumption) on the combustion chamber’s emission characteristics is determined. The obtained results can be used for parameter selection and optimization of promising high-temperature gas turbine combustion chambers with steam injection operating on liquid fuels.

Publisher

Walter de Gruyter GmbH

Subject

Aerospace Engineering

Link

https://www.degruyter.com/document/doi/10.1515/tjj-2020-0029/pdf

Reference38 articles.

1. Cheng, DY, Nelson, ALC. The chronological development of the Cheng cycle steam injected gas turbine during the past 25 years. In: Proceedings of ASME turbo expo 2002. Amsterdam, the Netherlands 2002. p. 1–8. GT-2002-30119.

2. Sahai, V, Cheng, DY. Reduction of NOx and CO to below 2 ppm in a diffusion flame. In: Proceedings of ASME turbo expo 2003 power for land, sea, and air. Atlanta, Georgia, US; 2003; GT2003-38208. p. 1–9.

3. Rao, A. Evaporative gas turbine (EvGT)/Humid air turbine (HAT) cycles. In: Handbook of clean energy systems John Wiley & Sons, Ltd; 2015. p. 1–18.

4. Guillet, R. The humid combustion to protect environment and to save the fuel: the water vapor pump and Maisotsenko cycle examples. Int J Energy a Clean Environ (IJECE) 2011;12:259–71. https://doi.org/10.1615/interjenercleanenv.2012006092.

5. Bouam, A, Aïssani, S, Kadi, R. Gas turbine performances improvement using steam injection in the combustion chamber under sahara conditions. Oil Gas Sci Technol 2008;63:251–61. https://doi.org/10.2516/ogst:2007076.

Cited by 7 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Investigation of the Characteristics of a Gas Turbine Combustion Chamber with Steam Injection Operating on Hydrogen-Containing Mixtures and Hydrogen;International Journal of Chemical Engineering;2022-12-17

2. Mathematical Modelling of Marine Power Plants with Thermochemical Fuel Treatment;Polish Maritime Research;2022-09-01

3. Improving the Efficiency of Fuel Combustion in a 2.5-MW Contact-Type Gas Turbine Engine Using the Cross-Flow Plasma-Fuel Nozzle;IEEE Transactions on Plasma Science;2022-06

4. Investigation of ecological parameters of a gas turbine combustion chamber with steam injection for the floating production, storage, and offloading vessel;International Journal of Energy and Environmental Engineering;2021-09-29

5. Computational assessment of performance parameters of an aero gas turbine combustor for full flight envelope operation;International Journal of Turbo & Jet-Engines;2021-09-01