Abstract
Possible ways of adopting aircraft-engine derivative gas turbines for their implementation in power units of high capacity are considered.
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Engines of 1944–2000: Aviation, Rocket, Marine, Land-Based, Ed. by I. G. Shustov (OOO AKS Konversalt, Moscow, 2000)
O. N. Favorskii, V. M. Batenin, Yu. A. Zeigarnik, et al., “The PGU MES-60 Combined-Cycle (Steam-Gas) Installation with Steam Injection and a Heat Pump for the Mosenergo Power System,” Teploenergetika, No. 9, 50–58 (2001) [Therm. Eng. 48 (9), 751–759 (2001)].
S. O. Sereda and F. Sh. Gel’medov, “Calculated Assessments of Changing Characteristics of a Multistaged Axial Compressor Due to the Effect of Water Evaporation in Its Flow Path,” Teploenergetika, No. 11, 60–65 (2004) [Therm. Eng. 51(11), 924–929 (2004)].
N. A. Dikii, “Energy Saving Environmentally Friendly Technology of Heat Transformation into Work,” Prom. Teplotekhn. 19(4–5), 106–110 (1997).
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Original Russian Text © A.S. Kosoi, 2006, published in Teploenergetika.
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Kosoi, A.S. Adoption of aviation-derivative engines for use as part of a power unit of high capacity. Therm. Eng. 53, 464–472 (2006). https://doi.org/10.1134/S0040601506060139
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DOI: https://doi.org/10.1134/S0040601506060139