This paper proposes an original approach to the reduced-order modelling of integrally bladed disks. It is proposed to build a reduction basis which is independent from the rotational speed, from only one modal, cyclic-symmetry calculation performed at rest, and a few static computations. Based on previous works, a polynomial expansion is used which leads to a parametric approximation of the stiffness matrix for the entire operating range. Furthermore, the Kirsch Combined Approximation (KCA) method is used for building the final reduction basis. This method is based on successive approximations of the negative binomial expansion applied to the reanalysis eigenproblem. After giving a general overview of the main theoretical aspects, the paper focuses on the reanalysis problem based on the combined approximations method. Finally, the application of the extended reduction method to the case of a real bladed disk is presented. It is shown that the use of combined approximations provides a very accurate estimation of a Campbell diagram, and allows substantial computational time savings.
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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
A Contribution to the Reduced-Order Analysis of Bladed Disks Using Combined Approximations for Quick Campbell Diagrams Assessment
Jean de Cazenove,
Jean de Cazenove
Turbomeca, Bordes, France
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Moustapha Mbaye,
Moustapha Mbaye
Turbomeca, Bordes, France
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Jean-Philippe Ousty,
Jean-Philippe Ousty
Turbomeca, Bordes, France
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Scott Cogan
Scott Cogan
University of Franche-Comté, Besancon, France
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Jean de Cazenove
Turbomeca, Bordes, France
Moustapha Mbaye
Turbomeca, Bordes, France
Jean-Philippe Ousty
Turbomeca, Bordes, France
Scott Cogan
University of Franche-Comté, Besancon, France
Paper No:
GT2015-43701, V07BT32A030; 10 pages
Published Online:
August 12, 2015
Citation
de Cazenove, J, Mbaye, M, Ousty, J, & Cogan, S. "A Contribution to the Reduced-Order Analysis of Bladed Disks Using Combined Approximations for Quick Campbell Diagrams Assessment." Proceedings of the ASME Turbo Expo 2015: Turbine Technical Conference and Exposition. Volume 7B: Structures and Dynamics. Montreal, Quebec, Canada. June 15–19, 2015. V07BT32A030. ASME. https://doi.org/10.1115/GT2015-43701
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