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

Award Information
Agency:
Department of Defense
Branch
Army
Amount:
$70,000.00
Award Year:
2007
Program:
SBIR
Phase:
Phase I
Contract:
W911W6-08-C-0009
Award Id:
81362
Agency Tracking Number:
A072-012-0838
Solicitation Year:
n/a
Solicitation Topic Code:
n/a
Solicitation Number:
n/a
Small Business Information
7960 S. Kolb Rd., Tucson, AZ, 85706
Hubzone Owned:
N
Minority Owned:
N
Woman Owned:
N
Duns:
147518286
Principal Investigator:
JamesWithers
C.E.O.
(520) 574-1980
jcwithers@mercorp.com
Business Contact:
RaoufLoutfy
President
(520) 574-1980
mercorp@mercorp.com
Research Institute:
n/a
Abstract
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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