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IGCC performance comparison for variations in gasifier type and gas turbine firing temperaturePerformance estimates were made for a series of integrated coal gasification combined cycle (IGCC) power systems using three generic types of coal gasification subsystems. The objectives of this study were (1) to provide a self consistent comparison of IGCC systems using different types of gasifiers and different oxidants and (2) to use this framework of cases to evaluate the effect of a gas turbine firing temperature and cooling approach an overall system efficiency. The basic IGCC systems considered included both air and oxygen blown versions of a fluidized bed gasifier, represented by the Westinghouse design, and an entrained bed gasifier, represented by the Texaco design. Also considered were systems using an oxygen blown, fixed bed gasifier, represented by the British Gas Corporation (BGC) slagging gasifier. All of these gasifiers were integrated with a combined cycle using a gas turbine firing temperature of 1700 K (2600 F) and a compressor pressure ratio of 16:1. Steam turbine throttle conditions were chosen to be 16.6 MPa/811 K (2400 psia/1000 F) with a single reheat to 810 K (1000 F). Some of these cases were modified to allow the evaluation of the effect of gas turbine firing temperature. Turbine firing temperatures from state of the art 1365 K (2000 F) to an advanced technology 1920 K (3000 F) were analyzed. A turbine cooling technology that maintains metal temperatures below acceptable limits was assumed for each level of firing temperature. System performance comparisons were made using three advanced turbine cooling technologies for the 1920 K (3000 F) firing temperature. The results indicate that the IGCC using the BGC gasifier had the highest net system efficiency (42.1 percent) of the five gasification cases considered.
Document ID
19830016766
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Stochl, R. J.
(NASA Lewis Research Center Cleveland, OH, United States)
Nainiger, J. J.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 4, 2013
Publication Date
January 1, 1983
Subject Category
Energy Production And Conversion
Report/Patent Number
NAS 1.15:83310
E-1549
NASA-TM-83310
Report Number: NAS 1.15:83310
Report Number: E-1549
Report Number: NASA-TM-83310
Accession Number
83N25037
Funding Number(s)
PROJECT: RTOP 778-14-10
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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