A Process to In-Situ Form Cooling Channels in SiC/SiC Composite Turbine Blades and Nozzles

Award Information
Agency: Department of Defense
Branch: Army
Contract: W911W6-08-C-0009
Agency Tracking Number: A072-012-0838
Amount: $120,000.00
Phase: Phase I
Program: SBIR
Awards Year: 2007
Solicitation Year: 2007
Solicitation Topic Code: A07-012
Solicitation Number: 2007.2
Small Business Information
7960 S. Kolb Rd., Tucson, AZ, 85706
DUNS: 147518286
HUBZone Owned: N
Woman Owned: N
Socially and Economically Disadvantaged: N
Principal Investigator
 James Withers
 (520) 574-1980
Business Contact
 Raouf Loutfy
Title: President
Phone: (520) 574-1980
Email: mercorp@mercorp.com
Research Institution
Ceramic matrix composites (CMCs) such as silicon carbide/silicon carbide (SiC/SiC) extends the temperature capabilities of turboshaft engines thru higher temperature capabilities and reduced weight which provides improved horsepower-to-weight ratios. However, even uncooled ceramics can extend the capabilities of the engine to a certain plateau. If effective cooling channels could be incorporated into CMC (SiC/SiC) blades and nozzles even further increases in temperature capabilities at reduced weight and subsequent improved horsepower-to-weight ratios are achievable. A unique in-situ fabrication processing approach can produce cooling channels in controlled architectures within a SiC/SiC composite cross section. The processing will be developed and validated with establishing the mechanical properties and cooling effectiveness of SiC/SiC specimens containing multiple cooling channels which will be coordinated with engine OEMs.

* information listed above is at the time of submission.

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