One and a half stages of a low pressure turbine were investigated using a three-dimensional, time-accurate, viscous solver. Unsteady analyses were carried out by varying the circumferential relative position of consecutive vanes to study the effects of clocking on performance. Assuming that efficiency improvements by clocking are linked to the wake tangential position with respect to the successive blade, a certain circumferential shift in this position can be observed along the blade height due to blade twist and non-radial stacking, giving different contributions. In order to assess this phenomenon, results from three-dimensional computations were compared with a quasi three-dimensional analysis at mid-span. The effects of clocking on wake interaction mechanisms and unsteady blade loadings are presented and discussed.
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ASME Turbo Expo 2003, collocated with the 2003 International Joint Power Generation Conference
June 16–19, 2003
Atlanta, Georgia, USA
Conference Sponsors:
- International Gas Turbine Institute
ISBN:
0-7918-3689-4
PROCEEDINGS PAPER
Numerical Investigation of Three-Dimensional Clocking Effects in a Low Pressure Turbine
Andrea Arnone,
Andrea Arnone
University of Florence, Florence, Italy
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Michele Marconcini,
Michele Marconcini
University of Florence, Florence, Italy
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Alberto Scotti Del Greco,
Alberto Scotti Del Greco
University of Florence, Florence, Italy
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Ennio Spano
Ennio Spano
Fiat Avio S.p.A., Torino, Italy
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Andrea Arnone
University of Florence, Florence, Italy
Michele Marconcini
University of Florence, Florence, Italy
Alberto Scotti Del Greco
University of Florence, Florence, Italy
Ennio Spano
Fiat Avio S.p.A., Torino, Italy
Paper No:
GT2003-38414, pp. 245-254; 10 pages
Published Online:
February 4, 2009
Citation
Arnone, A, Marconcini, M, Del Greco, AS, & Spano, E. "Numerical Investigation of Three-Dimensional Clocking Effects in a Low Pressure Turbine." Proceedings of the ASME Turbo Expo 2003, collocated with the 2003 International Joint Power Generation Conference. Volume 6: Turbo Expo 2003, Parts A and B. Atlanta, Georgia, USA. June 16–19, 2003. pp. 245-254. ASME. https://doi.org/10.1115/GT2003-38414
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