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Parametric performance analysis of steam-injected gas turbine with a thermionic-energy-converter-lined combustorThe performance of steam-injected gas turbines having combustors lined with thermionic energy converters (STIG/TEC systems) was analyzed and compared with that of two baseline systems; a steam-injected gas turbine (without a TEC-lined combustor) and a conventional combined gas turbine/steam turbine cycle. Common gas turbine parameters were assumed for all of the systems. Two configurations of the STIG/TEC system were investigated. In both cases, steam produced in an exhaust-heat-recovery boiler cools the TEC collectors. It is then injected into the gas combustion stream and expanded through the gas turbine. The STIG/TEC system combines the advantage of gas turbine steam injection with the conversion of high-temperature combustion heat by TEC's. The addition of TEC's to the baseline steam-injected gas turbine improves both its efficiency and specific power. Depending on system configuration and design parameters, the STIG/TEC system can also achieve higher efficiency and specific power than the baseline combined cycle.
Document ID
19820015802
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Choo, Y. K.
(NASA Lewis Research Center Cleveland, OH, United States)
Burns, R. K.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 4, 2013
Publication Date
February 1, 1982
Subject Category
Energy Production And Conversion
Report/Patent Number
E-1048
NASA-TM-82736
NAS 1.15:82736
Report Number: E-1048
Report Number: NASA-TM-82736
Report Number: NAS 1.15:82736
Accession Number
82N23678
Funding Number(s)
PROJECT: RTOP 778-46-12
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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