Modeling and Simulation for Robust Ceramic Matrix Composite (CMC) Manufacturing Processes

Award Information
Agency:
Department of Defense
Amount:
$99,650.00
Program:
SBIR
Contract:
FA8650-08-M-5225
Solitcitation Year:
2008
Solicitation Number:
2008.1
Branch:
Air Force
Award Year:
2008
Phase:
Phase I
Agency Tracking Number:
F081-038-0655
Solicitation Topic Code:
AF081-038
Small Business Information
ADVANCED COMPUTATIONAL & ENGINEERING SER
750 Cross Pointe Rd., Suite E, Gahanna, OH, 43230
Hubzone Owned:
N
Woman Owned:
N
Socially and Economically Disadvantaged:
N
Duns:
125624986
Principal Investigator
 Kyle Koppenhofer
 Principal
 (614) 861-7015
 kyle@acescolumbus.com
Business Contact
 Jeffrey Crompton
Title: Principal
Phone: (614) 861-7015
Email: jeff@acescolumbus.com
Research Institution
N/A
Abstract
Increasing the power density of current jet aircraft engines requires the replacement of conventional high temperature materials by new materials capable of operating at higher temperatures. Ceramics and ceramic matrix composites (CMCs) represent excellent candidates for increased use in hot engine parts due to their ability to withstand temperatures in excess of 2000 C. Due to the complexity of the manufacturing CMCs, limited guidelines exist that can readily transfer between different components. Consequently experimental approaches are needed to develop detailed manufacturing procedures. The extensive development time and budget needed for this approach can be significantly reduced if predictive design tools for the RMI process were available. This work will develop analytical tools to analyze the multiple interdependent physical phenomena of relevance for the manufacture of CMCs. The analyses will be integrated into a design tool capable of providing engineers with an environment to analyze the CMC manufacturing process thus reducing the need for iterative experimental approaches. Consequently, the costs associated with manufacturing critical CMC components will be dramatically reduced and provide engines with improved thrust and fuel efficiency while reducing emissions.

* information listed above is at the time of submission.

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