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Tools for Reliable Modeling of Crack Propagation In Turbine Engine Metallic Components

Award Information
Agency: Department of Defense
Branch: Air Force
Contract: FA8650-11-M-5137
Agency Tracking Number: F103-157-1955
Amount: $99,904.00
Phase: Phase I
Program: SBIR
Solicitation Topic Code: AF103-157
Solicitation Number: 2010.3
Solicitation Year: 2010
Award Year: 2011
Award Start Date (Proposal Award Date): 2011-01-07
Award End Date (Contract End Date): N/A
Small Business Information
10 Halfmoon Executive Park Drive
Clifton Park, NY -
United States
DUNS: 012076795
HUBZone Owned: No
Woman Owned: No
Socially and Economically Disadvantaged: No
Principal Investigator
 Ottmar Klaas
 Senior Software Engineer
 (518) 348-1639
Business Contact
 Mark Beall
Title: President
Phone: (518) 348-1639
Research Institution

This Phase I SBIR will provide a flexible and expandable system for the simulation of crack propagation in structures focusing on turbine engine metallic components. The work here will build off of years of work already invested in developing such a system. The software will be designed to be easily incorporated into existing design processes by directly utilizing CAD design geometry and existing commercial finite element analysis software. The current software will be extended to incorporate probabilistic techniques for predicting component life considering variations in both component properties and operating conditions. BENEFIT: The failure of engineered structures due to propagation of cracks has caused many highly visible and costly accidents in recent years in structures ranging from bridges to aircraft. Better understanding of this failure mode and ease of evaluating the potential for such failures is critical to improving the design of a wide range of products. The software developed in this project will be specifically designed for easy integration with existing design processes to reduce unexpected failures and allow further optimization of structures to reduce weight and cost.

* Information listed above is at the time of submission. *

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