MARC

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245 0 0 |a Advanced Turbine System (ATS)  |h [electronic resource] :  |b Task 1, System scoping and feasibility study. 
260 |a Washington, D.C. :  |b United States. Dept. of Defense ;  |a Oak Ridge, Tenn. :  |b distributed by the Office of Scientific and Technical Information, U.S. Dept. of Energy,  |c 1993. 
300 |a Pages: (52 p) :  |b digital, PDF file. 
336 |a text  |b txt  |2 rdacontent. 
337 |a computer  |b c  |2 rdamedia. 
338 |a online resource  |b cr  |2 rdacarrier. 
500 |a Published through the Information Bridge: DOE Scientific and Technical Information. 
500 |a 02/01/1993. 
500 |a "doe/mc/29234-3364" 
500 |a "DE93000280" 
500 |a van der Linden, S. 
500 |a ABB Power Generation, Inc., North Brunswick, NJ (United States). Turbine Power Div. 
520 3 |a Present GT(Gas Turbine) Systems are available to achieve 52% (LHV) thermal efficiencies, plants in construction will be capable of 54%, and the goal of this study is to identify incentives, technical issues, and resource requirements to develop natural gas-and coal-compatible ATS which would have a goal of 60% or greater based on LHV. The prime objective of this project task is to select a natural gas-fired ATS (Advanced Turbine System) that could be manufactured and marketed should development costs not be at issue with the goals of: (1) Coal of electricity 10% below 1991 vintage power plants in same market class and size. (2) Expected performance 60% efficiency and higher, (3) Emission levels, NO[sub x] < 10 ppM (0.15 lb/MW-h), CO < 20 ppM (0.30 lb/MW-h), and UHC < 20 ppM (0.30 lb/MW-h). ABB screening studies have identified the gas-fueled combined cycle as the most promising full scale solution to achieve the set goals for 1988--2002. This conclusion is based on ABB's experience level, as well as the multi-step potential of the combined cycle process to improve in many component without introducing radical changes that might increase costs and lower RAM. The technical approach to achieve 60% or better thermal efficiency will include increased turbine inlet temperatures, compressor intercooling, as well a improvements in material, turbine cooling technology and the steam turbine. Use of improved component efficiencies will achieve gas-fired cycle performance of 61.78%. Conversion to coal-firing will result in system performance of 52.17% 
536 |b AC21-92MC29234. 
650 7 |a Design.  |2 local. 
650 7 |a Steam Turbines.  |2 local. 
650 7 |a Natural Gas.  |2 local. 
650 7 |a Turbomachinery.  |2 local. 
650 7 |a Document Types.  |2 local. 
650 7 |a Gas Fuels.  |2 local. 
650 7 |a Equipment.  |2 local. 
650 7 |a Thermal Power Plants.  |2 local. 
650 7 |a Turbines.  |2 local. 
650 7 |a Power.  |2 local. 
650 7 |a Fuel Gas.  |2 local. 
650 7 |a Thermal Efficiency.  |2 local. 
650 7 |a Fuels.  |2 local. 
650 7 |a Fluids.  |2 local. 
650 7 |a Cost.  |2 local. 
650 7 |a Power Plants.  |2 local. 
650 7 |a Cooling.  |2 local. 
650 7 |a Combined-cycle Power Plants.  |2 local. 
650 7 |a Emission.  |2 local. 
650 7 |a Temperature Effects.  |2 local. 
650 7 |a Energy Sources.  |2 local. 
650 7 |a Gases.  |2 local. 
650 7 |a Materials.  |2 local. 
650 7 |a Progress Report.  |2 local. 
650 7 |a Efficiency.  |2 local. 
650 7 |a Fossil Fuels.  |2 local. 
650 7 |a Gas Turbines.  |2 local. 
650 7 |a Electric Power.  |2 local. 
650 7 |a Machinery.  |2 local. 
650 7 |a Fossil-fueled Power Plants.  |2 edbsc. 
710 1 |a United States.  |b Department of Defense.  |4 spn. 
710 1 |a United States.  |b Department of Energy.  |4 spn. 
710 2 |a National Energy Technology Laboratory (U.S.).  |4 res. 
710 1 |a United States.  |b Department of Energy.  |b Office of Scientific and Technical Information.  |4 dst. 
856 4 0 |u http://www.osti.gov/servlets/purl/6632220-WHVGOU/  |z Online Access 
907 |a .b59558647  |b 03-06-23  |c 05-25-10 
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952 f f |p Can circulate  |a University of Colorado Boulder  |b Online  |c Online  |d Online  |e E 1.99:doe/mc/29234-3364  |h Superintendent of Documents classification  |i web  |n 1