The role of stator vanes is to straighten the air flow on each stage of axial compressors. They are so subject to dynamically fluctuating high pressure loads. Furthermore, monobloc clustered designs have been developed to facilitate manufacturing process and reduce costs, but they result in loss of cyclic symmetry properties and very low structural damping. This makes it more difficult to predict vibratory behavior, when taking high modal density and extreme sensitivity to mistuning into account, and even more essential to ensure structural strength in the context of fatigue. In most cases, mistuning due to geometrical and material tolerances is unknown. Here, a non-intrusive spectral stochastic method has been developed to predict the vibratory behavior of a clustered stator vane in which the Young modulus of some blades is associated with a random variable representing the mistuning effect. This method is based on a stochastic modal analysis which consists in projecting eigenfrequencies and modes shapes on a polynomial chaos basis. Computation of spectral coefficients is performed through non intrusive ways — making the method applicable to any problem — as Smolyak projection or regression by least square method. These two methods are compared based on criteria of computations costs, accuracy, robustness and convergence. These methods have been tested on a simplified stator vane model - based on a 2D Euler-Bernoulli beams assembly. Regression method provides rather accurate results unlike Smolyak projection whatever the initial configurations of the problem. Computation costs are reasonable but could increase really fast according to polynomial degree and stochastic dimension. Thus, regression method is an accurate, robust and fast enough method to predict the vibratory behavior of a mistuned clustered stator vane.
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ASME Turbo Expo 2015: Turbine Technical Conference and Exposition
June 15–19, 2015
Montreal, Quebec, Canada
Conference Sponsors:
- International Gas Turbine Institute
ISBN:
978-0-7918-5677-2
PROCEEDINGS PAPER
Vibratory Behavior Prediction of a Mistuned Clustered Stator Vane: Non-Intrusive Stochastic Methods
Jonathan Philippe,
Jonathan Philippe
École Centrale de Lyon, Ecully Cedex, France
SAFRAN Snecma, Moissy-Cramayel, France
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Fabrice Thouverez,
Fabrice Thouverez
École Centrale de Lyon, Ecully Cedex, France
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Laurent Blanc,
Laurent Blanc
École Centrale de Lyon, Ecully Cedex, France
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Marion Gruin
Marion Gruin
SAFRAN Snecma, Moissy-Cramayel, France
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Jonathan Philippe
École Centrale de Lyon, Ecully Cedex, France
SAFRAN Snecma, Moissy-Cramayel, France
Fabrice Thouverez
École Centrale de Lyon, Ecully Cedex, France
Laurent Blanc
École Centrale de Lyon, Ecully Cedex, France
Marion Gruin
SAFRAN Snecma, Moissy-Cramayel, France
Paper No:
GT2015-42358, V07BT32A006; 8 pages
Published Online:
August 12, 2015
Citation
Philippe, J, Thouverez, F, Blanc, L, & Gruin, M. "Vibratory Behavior Prediction of a Mistuned Clustered Stator Vane: Non-Intrusive Stochastic Methods." Proceedings of the ASME Turbo Expo 2015: Turbine Technical Conference and Exposition. Volume 7B: Structures and Dynamics. Montreal, Quebec, Canada. June 15–19, 2015. V07BT32A006. ASME. https://doi.org/10.1115/GT2015-42358
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