Modeling of Integrally Bladed Rotor (IBR) Blends

Award Information
Agency:
Department of Defense
Amount:
$79,634.00
Program:
STTR
Contract:
N68335-13-C-0373
Solitcitation Year:
2013
Solicitation Number:
2013.A
Branch:
Navy
Award Year:
2013
Phase:
Phase I
Agency Tracking Number:
N13A-002-0207
Solicitation Topic Code:
N13A-T002
Small Business Information
Optimal Solutions Software LLC
PO Box 2427, Idaho Falls, ID, -
Hubzone Owned:
N
Woman Owned:
N
Socially and Economically Disadvantaged:
N
Duns:
012832130
Principal Investigator
 Mark Landon
 Chief Technical Officer
 (208) 521-4660
 mlandon@gosculptor.com
Business Contact
 Phil Belnap
Title: President
Phone: (208) 569-4942
Email: pbelnap@gosculptor.com
Research Institution
 University of Michigan
 Patrick J Woods
 Wolverine Tower
3003 South State Street
Ann Arbor, MI, 48109-1274
 (734) 764-8566
 Nonprofit college or university
Abstract
The overall goal of this Phase I project is to show the feasibility of using state-of-the-art parameterization tools for shape changes (i.e., volumetric deformation/morphing provided by Sculptor) coupled with a fast FEA tool (i.e., the MAX method) to quickly calculate the dynamic response of the many different shapes necessary for sample-based stochastic vibration analysis of IBRs with blends. The PI's MAX method is the basis for a robust and computationally effective technology for dynamic analysis. The MAX method allows for quick FEA analysis of different blend shapes for statistical investigations. Current state-of-the-art FEA analysis of industrial models, with several thousands of separate calculations (samples) for stochastic investigations, requires prohibitively long computation time for any realistic results. For example, it is not unusual for a single dynamic analysis of a single IBR to require over 10 days of CPU time. In contrast, the MAX method is expected to require only a few seconds of CPU time. The combination of the MAX method and the mesh morphing technology provided by Sculptor will enable the analysis of blends with arbitrary shape.

* information listed above is at the time of submission.

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