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Advanced Ceramic Matrix Composite Gas Turbine Engine Research Combustor (20-RD-220)

Award Information
Agency: Department of Defense
Branch: Army
Contract: W911QX-21-P-0012
Agency Tracking Number: A201-027-0066
Amount: $111,500.00
Phase: Phase I
Program: SBIR
Solicitation Topic Code: A20-027
Solicitation Number: 20.1
Timeline
Solicitation Year: 2020
Award Year: 2020
Award Start Date (Proposal Award Date): 2020-06-01
Award End Date (Contract End Date): 2021-05-01
Small Business Information
4401 Dayton-Xenia Rd.
Dayton, OH 45432-1894
United States
DUNS: 074689217
HUBZone Owned: No
Woman Owned: Yes
Socially and Economically Disadvantaged: No
Principal Investigator
 Amarendra Rai
 (937) 426-6900
 arai@ues.com
Business Contact
 Louise Tincher
Phone: (937) 426-6900
Email: ltincher@ues.com
Research Institution
N/A
Abstract

Light weight silicon carbide (SiC) based ceramic matrix composites (CMCs) are currently being considered for military gas turbine engine combustor parts operating at higher temperatures (≥1310°C). However, such composites suffer from surface recession in the high temperature combustion environment of the turbine engine with high water vapor contents. Moreover, there are issues associated with the currently utilized manufacturing technologies for the SiC based CMCs. UES, Inc. in collaboration with Pennsylvania State University proposes to develop advanced processes to manufacture environmentally resistant CMC combustor parts. Relevant characteristics of the fabricated parts will be evaluated.

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

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