Actions for Lean premixed flames for low NO{sub x} combustors [electronic resource].
Lean premixed flames for low NO{sub x} combustors [electronic resource].
- Published
- Oak Ridge, Tenn. : Distributed by the Office of Scientific and Technical Information, U.S. Dept. of Energy, 1995.
- Physical Description
- pages 249-275 : digital, PDF file
- Additional Creators
- United States. Department of Energy. Office of Energy Efficiency and Renewable Energy and United States. Department of Energy. Office of Scientific and Technical Information
Access Online
- Restrictions on Access
- Free-to-read Unrestricted online access
- Summary
- Gas turbines are being used throughout the world to generate electricity. Due to increasing fuel costs and environmental concerns, gas turbines must meet stringent performance requirements, demonstrating high thermal efficiencies and low pollutant emissions. In order for U.S. manufactured gas turbines to stay competitive, their NOₓ levels must be below 10 ppm and their thermal efficiencies should approach 60%. Current technology is being stretched to achieve these goals. The twin goals of high efficiency and low NOₓ emissions require extending the operating range of current gas turbines. Higher efficiency requires operation at higher pressures and temperatures. Lower NOₓ emissions requires lower flame temperatures. Lower flame temperatures can be achieved through partially to fully pre-mixed combustion. However, increased performance and lower emissions result in a set of competing goals. In order to achieve a successful compromise between high efficiency and low NOₓ emissions, advanced design tools must be developed. One key design tool is a computationally efficient, high pressure, turbulent flow, combustion model capable of predicting pollutant formation in an actual gas turbine. Its development is the goal of this program. Achieving this goal requires completion of three tasks. The first task is to develop a reduced chemical kinetics model describing N{sub O}x formation in natural gas-air systems. The second task is to develop a computationally efficient model that describes turbulence-chemistry interactions. The third task is to incorporate the reduced chemical kinetics and turbulence-chemistry interaction models into a commercially available flow solver and compare its predictions with experimental data obtained under carefully controlled conditions so that the accuracy of model predictions can be evaluated.
- Report Numbers
- E 1.99:doe/metc--96/1023-vol.2
E 1.99: conf-9510109--vol.2
conf-9510109--vol.2
doe/metc--96/1023-vol.2 - Subject(s)
- Other Subject(s)
- Note
- Published through SciTech Connect.
10/01/1995.
"doe/metc--96/1023-vol.2"
" conf-9510109--vol.2"
"DE96000562"
Advanced turbine systems (ATS) annual review, Morgantown, WV (United States), 17-18 Oct 1995.
Tseng, L.; Sojka, P.; Bryjak, J.
USDOE Morgantown Energy Technology Center, WV (United States)
View MARC record | catkey: 13600201