Design methods of the ABB ALSTOM POWER gas turbine dry low emission combustion system

Proceedings of the Institution of Mechanical Engineers, Part A: Journal of Power and Energy

Volumn 214, Issue 4, 2000, Pages 293-315

  Alkabie, H ^a  

^a Alstom UK   (United Kingdom)

Author keywords

Aerothermodynamics; Combustion; Design; DLE; Emission; Gas turbine; NO(x); Premixing

Indexed keywords

AERODYNAMICS; CARBON MONOXIDE; COMBUSTION; COMPUTATIONAL FLUID DYNAMICS; GAS EMISSIONS; GAS TURBINES; MACHINE DESIGN; PARAMETER ESTIMATION;

AEROTHERMODYNAMICS; AIR MASS MAPPING; DRY LOW EMISSION (DLE) COMBUSTION SYSTEMS; FULL-LOAD OPERATING CONDITIONS; RADIAL SWIRLER INJECTORS; THERMAL BARRIER COATINGS (TBC);

COMBUSTORS;

COMBUSTION; EMISSION CONTROL; GAS TURBINE; NITROGEN OXIDE;

EID: 0033839661     PISSN: 09576509     EISSN: None     Source Type: Journal    
DOI: 10.1243/0957650001537895     Document Type: Article

References (30)

1. Low NO(x) technologies for stationary gas turbines
2. Fuel-air nonuniformity effect on nitric oxide emissions
3. Effect of initial fuel distribution and subsequent mixing on emissions from lean premixed flames
4. Ultra low NO(x) emissions for gas and liquid fuels using radial swirlers
5. The influence of fuel placement on NO(x) emissions from flames stabilised by radial swirlers
6. Radial swirler for low emissions gas turbine combustion
7. Experimental evolution of fuel injection configurations for a lean premixed NO(x) gas turbine combustor
8. Velocity temperature and species characteristics of the flow in a gas turbine combustor
9. Influence of fuel placement on NO(x) emissions from flames stabilised by radial swirlers
10. Radial swirlers with peripheral fuel injection for ultra-low NO(x) emissions
11. Ultra low NO(x) turbine combustion using radial swirlers
12. The influence of fuel placement on NO(x) emissions from flames stabilised by radial swirlers at gas turbine primary zone
13. The aerodynamics of radial swirlers in lean gas turbine primary zones
14. Numerical modeling of the turbulent reaction flow around premixed baffle stabiliser
15. Low NO(x) combustor design without premixing for aero-engine application
16. The effect of imperfect fuel-air mixing in a burner on NO formation from nitrogen in air and the fuel
17. Effect of large scale structures on turbulent flame propagation
18. Flame stabilization in high velocity flow
19. Preliminary studies of autoignition and flashback in a premixing pre-vaporising flame tube using jet-A fuel at lean equivalence ratios
20. Effect of combustion upon precessing vortex cores generated by swirl combustors
21. Noise source in swirl burners
22. Effect of heat release and swirl on the recirculation within swirlstabilized flames
23. Full coverage impingement heat transfer: Cooling effectiveness
24. Flame radiation in gas turbine combustion chamber
25. Mixing of a row of jets with a confined crossflow