Abstract
This category of components includes recuperators, preheaters, regenerators, intercoolers, and aftercoolers, Figure 14.1 Within these components the process of heat exchange occurs between the high and low temperature sides. The working principle of these components is the same ([1, 2, 2]). However, different working media are involved in the heat transfer process. More recently recuperators are applied to small and medium size gas turbine engines to improve their thermal efficiency. The exhaust thermal energy is used to warm up the compressor exit air before it enters the combustion chamber. A typical recuperator consists of a low pressure hot side flow path, a high pressure cold side flow path, and the wall that separates the two flow paths. A variety of design concepts are used to maximize the heat exchange between the hot and the cold side by improving the heat transfer coefficients. A cold side flow path may consist of a number of tubes with turbulators, fin pins, and other features that enhance the heat transfer coefficient. Based on the individual recuperator design concept, hot gas impinges on the tube surface in cross flow or counter flow directions. The working media entering and exiting the recuperator is generally combustion gas that exits the diffuser (hot side) and air that exits the compressor (cold side)
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Bibliography
Schobeiri T., 1986: “A General Computational Method for Simulation and Prediction of Transient Behavior of Gas Turbines,” ASME-86-GT-180.
Schobeiri, M. T., Abouelkheir, M., Lippke, C., 1994, “GETRAN: A Generic, Modularly Structured Computer Code for Simulation of Dynamic Behavior of Aero-and Power Generation Gas Turbine Engines,” an honor paper, ASME Transactions, Journal of Gas Turbine and Power, Vol. 1, pp. 483–494.
Schobeiri, M. T., Attia, M, Lippke, C., 1994, “Nonlinear Dynamic Simulation of Single and Multi-spool Core Engines, Part I, II: Theoretical Method, Simulation Cases” AIAA, Journal of Propulsion and Power, Volume 10, Number 6, pp. 855–867, 1994.
Kays, W. M, London, A. L., 1984, “Compact Heat Exchangers,” McGraw-Hill Book Company, third Edition.
Hansen, H., 1976, “Wärmeübertragung im Gegenstrom, Gleichstrom und Kreuzstrom, 2.” Auflage, ISBN 3ß540ß07552ß6 Springer-Verlag, Berlin Heidelberg New York.
Lefebvre, AS.H ., 1983, “Gas Turbine Combustion,” Hemisphere Publishing Corporation.
Marek, C. J., and Huhasz, A. J., 1974, “Simulataneous Film and Convection Cooling of a Plate inserted in the Exhaust Stream of a Gas Turbine Combustor,” NASA TND-7689.
Planck, M., 1959, “Theory of Heat Radiation,” Dover Publication, Inc, New York.
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Schobeiri, M.T. (2019). Modeling of Recuperators, Combustion Chambers, Afterburners. In: Gas Turbine Design, Components and System Design Integration. Springer, Cham. https://doi.org/10.1007/978-3-030-23973-2_14
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DOI: https://doi.org/10.1007/978-3-030-23973-2_14
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