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contributor authorKalathakis, C.
contributor authorAretakis, N.
contributor authorRoumeliotis, I.
contributor authorAlexiou, A.
contributor authorMathioudakis, K.
date accessioned2017-11-25T07:15:51Z
date available2017-11-25T07:15:51Z
date copyright2017/1/2
date issued2017
identifier issn0742-4795
identifier othergtp_139_06_061701.pdf
identifier urihttp://138.201.223.254:8080/yetl1/handle/yetl/4233707
description abstractA simulation environment allowing steady state and transient modeling is used for assessing several gas turbine based cycles proposed for solar hybridization. First, representative open cycle gas turbine configurations, namely, (a) single shaft (SS), (b) recuperated single-shaft, (c) twin shaft (TS), and (d) two-spool three-shaft, intercooled, recuperated, are evaluated. The importance of design point selection in terms of solar share value is highlighted. Solar steam injection gas turbine cycle (STIG) alternatives, namely, solar steam only and solar/fuel gas steam, are then assessed. Finally, the concept of a dual fluid receiver (DFR) for exploiting the rejected solar power by producing steam during sunny hours with high irradiation is demonstrated. The effects of hybridization on performance and operability are established and evaluated. Solarization effect on performance is estimated in terms of annual produced power and fossil fuel savings. The results indicate that the spool arrangement affects the suitability of a gas turbine for hybridization. Recuperated configurations performed better for the design constrains imposed by current technology solar parts. Solar steam injection is a promising solution for retrofitted fuel-only and conventional STIG engines.
publisherThe American Society of Mechanical Engineers (ASME)
titleAssessment of Solar Gas Turbine Hybridization Schemes
typeJournal Paper
journal volume139
journal issue6
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.4035289
journal fristpage61701
journal lastpage061701-9
treeJournal of Engineering for Gas Turbines and Power:;2017:;volume( 139 ):;issue: 006
contenttypeFulltext


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