SBIR-STTR Award

Modeling of Integrally Bladed Rotor (IBR) Blends
Award last edited on: 4/14/2019

Sponsored Program
STTR
Awarding Agency
DOD : Navy
Total Award Amount
$895,409
Award Phase
2
Solicitation Topic Code
N13A-T002
Principal Investigator
Mark D Landon

Company Information

Optimal Solutions Software LLC (AKA: Optimal Solutions Inc)

3000 West Pancheri Drive Suite 3
Idaho Falls, ID 83402
   (208) 529-9696
   mlandon@optimalsolutions.us
   www.optimalsolutions.us

Research Institution

University of Michigan

Phase I

Contract Number: N68335-13-C-0373
Start Date: 8/15/2013    Completed: 3/15/2014
Phase I year
2013
Phase I Amount
$147,792
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 PIs 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.

Benefit:
Develop an automated process to easily determine the appropriate and viability of blends (repairs) made to Integrated Blade Rotors. This process will drastically reduce the analysis time and required expertise to make in the field repairs to Integrated Blade Rotors on jet engines.

Keywords:
ASD, ASD, Sculptor, parameterization, FEA analysis, Integrated Blade Rotors, MAX method, IBR, stochastic investigations

Phase II

Contract Number: N68335-15-C-0373
Start Date: 8/24/2015    Completed: 8/28/2018
Phase II year
2015
Phase II Amount
$747,617
The main goal of Phase II is to validate the Phase I prototype and develop an integrated design and analysis tool for assessing large damage and blends for compressor IBRs on gas turbine engines and other blade systems. This tool will have at its core the automated analytical modeling of as-measured or as-expected airfoil blends for the structural and aero response to the shape change due to blends using the University of Michigans MAX method and Optimal Solutions Softwares Sculptor. The resulting technology will help expand the existing library

Benefit:
The anticipated benefits and commercial applications of the research and development of this Phase II project are the expansion of the blend limits on Integrally Bladed Rotors (IBR). This expansion of the current limits increases the size, shape, and number of blends/repairs that can be executed on a given IBR thus lowering the cost of engine removal from the aircraft to make repairs and extending the current life cycle of the of the engine. The product of this project will be a tool that can used to perform computer simulations to predict the structural and aerodynamic response of the proposed blends.

Keywords:
integrally bladed rotor, Arbitrary Shape Deformation, modes, Sculptor, IBR, frequencies, blend, MAX