An analysis has been developed to simulate the time-transient vibratory motion of a general configuration engine turbomachinery free-standing blade when subjected to in-service blade-on-casing tip-rub events. The analysis imports the at-speed stress-stiffened blade stiffness matrix and lumped mass matrix from a finite element model of the actual blade. Formulation and computational approaches are presented. Correct characterization of the blade tip-surface rub mechanics tribology models necessitates using empirical information that is currently being acquired from single-blade spin-pit tests now in progress in a parallel companion phase of this research. Output results for validation cases are presented. The analysis efficiently simulates complete transients involving multiple successive incursions (blade on casing hits), tracking the blade tip contact force distribution and blade motion throughout the simulated time frame including blade motion during, between and after successive casing hits.
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ASME Turbo Expo 2005: Power for Land, Sea, and Air
June 6–9, 2005
Reno, Nevada, USA
Conference Sponsors:
- International Gas Turbine Institute
ISBN:
0-7918-4727-6
PROCEEDINGS PAPER
Simulation of Engine Blade Tip-Rub Induced Vibration
Kevin Turner,
Kevin Turner
GE Transportation, Evendale, OH
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Maurice Adams,
Maurice Adams
Case Western Reserve University, Cleveland, OH
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Michael Dunn
Michael Dunn
Ohio State University, Columbus, OH
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Kevin Turner
GE Transportation, Evendale, OH
Maurice Adams
Case Western Reserve University, Cleveland, OH
Michael Dunn
Ohio State University, Columbus, OH
Paper No:
GT2005-68217, pp. 391-396; 6 pages
Published Online:
November 11, 2008
Citation
Turner, K, Adams, M, & Dunn, M. "Simulation of Engine Blade Tip-Rub Induced Vibration." Proceedings of the ASME Turbo Expo 2005: Power for Land, Sea, and Air. Volume 4: Turbo Expo 2005. Reno, Nevada, USA. June 6–9, 2005. pp. 391-396. ASME. https://doi.org/10.1115/GT2005-68217
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