Coated Ceramic Matrix Composite (CMC) Low Pressure Turbine (LPT) Blade Development

Period of Performance: 04/05/2009 - 01/05/2010


Phase 1 SBIR

Recipient Firm

Diversitech, Inc.
110 Boggs Lane, Suite 230
Cincinnati, OH 45246
Principal Investigator


The objective of this program is to develop an integrated approach for the development of methods for the prediction and manufacture of special features such as holes, cooling channels, dovetails, leading and trailing edges in ceramic composite turbine blades. BENEFIT: The development of cooled ceramic composite turbine components will extend the engine operating efficiencies to a new level. This will aid the reduction in fuel consumption and reduced engine weights for future engine applications