New geometric mistuning modeling approaches for integrally bladed rotors (IBRs) are developed for incorporating geometric perturbations to a fundamental disk–blade sector, particularly the disk–blade boundary or connection. Reduced-order models (ROMs) are developed from a Craig–Bampton component mode synthesis (C–B CMS) framework that is further reduced by a truncated set of interface modes that are obtained from an Eigen-analysis of the C–B CMS constraint degrees of freedom (DOFs). An investigation into using a set of tuned interface modes and tuned constraint modes for model reduction is then performed, which offers significant computational savings for subsequent analyses. Two configurations of disk–blade connection mistuning are investigated: as-measured principal component (PC) deviations and random perturbations to the interblade spacing. Furthermore, the perturbation sizes are amplified to investigate the significance of incorporating mistuned disk–blade connections during solid model generation from optically scanned geometries. Free and forced response results are obtained for each ROM and each disk–blade connection type and compared to full finite element model (FEM) solutions. It is shown that the developed methods provide accurate results with a reduction in solution time compared to the full FEM. In addition, results indicate that the inclusion of a mistuned disk–blade connection deviations are small or conditions where large perturbations are localized to a small areas of the disk–blade connection.
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July 2015
Research-Article
Geometric Mistuning Reduced-Order Models for Integrally Bladed Rotors With Mistuned Disk–Blade Boundaries
Joseph A. Beck,
Joseph A. Beck
1
Manufacturing and Industrial
Technologies Division,
e-mail: Joseph.Beck.8@us.af.mil
Technologies Division,
Air Force Research Laboratory
,Wright-Patterson AFB, OH 45433
e-mail: Joseph.Beck.8@us.af.mil
1Corresponding author.
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Jeffrey M. Brown,
Jeffrey M. Brown
Turbine Engine Division,
Air Force Research Laboratory
,Wright-Patterson AFB, OH 45433
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Alex A. Kaszynski,
Alex A. Kaszynski
Turbine Engine Division,
Air Force Research Laboratory
,Wright-Patterson AFB, OH 45433
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Charles J. Cross,
Charles J. Cross
Turbine Engine Division,
Air Force Research Laboratory
,Wright-Patterson AFB, OH 45433
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Joseph C. Slater
Joseph C. Slater
Associate Dean
Defense Aerospace Studies,
Defense Aerospace Studies,
Wright State University
,Dayton, OH 45435
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Joseph A. Beck
Manufacturing and Industrial
Technologies Division,
e-mail: Joseph.Beck.8@us.af.mil
Technologies Division,
Air Force Research Laboratory
,Wright-Patterson AFB, OH 45433
e-mail: Joseph.Beck.8@us.af.mil
Jeffrey M. Brown
Turbine Engine Division,
Air Force Research Laboratory
,Wright-Patterson AFB, OH 45433
Alex A. Kaszynski
Turbine Engine Division,
Air Force Research Laboratory
,Wright-Patterson AFB, OH 45433
Charles J. Cross
Turbine Engine Division,
Air Force Research Laboratory
,Wright-Patterson AFB, OH 45433
Joseph C. Slater
Associate Dean
Defense Aerospace Studies,
Defense Aerospace Studies,
Wright State University
,Dayton, OH 45435
1Corresponding author.
Contributed by the International Gas Turbine Institute (IGTI) of ASME for publication in the JOURNAL OF TURBOMACHINERY. Manuscript received April 4, 2013; final manuscript received June 11, 2014; published online December 23, 2014. Assoc. Editor: Rakesh Srivastava.
This material is declared a work of the U.S. Government and is not subject to copyright protection in the United States. Approved for public release; distribution is unlimited.
J. Turbomach. Jul 2015, 137(7): 071001 (11 pages)
Published Online: July 1, 2015
Article history
Received:
April 4, 2013
Revision Received:
June 11, 2014
Online:
December 23, 2014
Citation
Beck, J. A., Brown, J. M., Kaszynski, A. A., Cross, C. J., and Slater, J. C. (July 1, 2015). "Geometric Mistuning Reduced-Order Models for Integrally Bladed Rotors With Mistuned Disk–Blade Boundaries." ASME. J. Turbomach. July 2015; 137(7): 071001. https://doi.org/10.1115/1.4029122
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