| Gas Turbine Reheat Using In-Situ Combustion | |
| Lippert, T.E. ; Bachovchin, D.M. | |
| Siemens Westinghouse | |
| 关键词: Combustion; Vanes; Aerodynamics; Kinetics; Mathematical Models; | |
| DOI : 10.2172/993806 RP-ID : None RP-ID : FC26-00NT40913 RP-ID : 993806 |
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| 美国|英语 | |
| 来源: UNT Digital Library | |
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【 摘 要 】
Siemens Westinghouse Power Corporation (SWPC) is developing in-situ reheat (fuel injection via airfoil injection) as a means for increasing cycle efficiency and power output, with possibly reduced emissions. In addition to kinetic modeling and experimental task, CFD modeling (by Texas A&M) of airfoil injection and its effects on blade aerodynamics and turbine performance. This report discusses validation of the model against single-vane combustion test data from Siemens Westinghouse, and parametric studies of injection reheat in a modern turbine. The best location for injection is at the trailing edge of the inlet guide vane. Combustion is incomplete at trailing edges of subsequent vanes. Recommendations for further development are presented.
【 预 览 】
| Files | Size | Format | View |
|---|---|---|---|
| 993806.pdf | 3781KB |
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