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High-Temperature Amorphous Coating for CMCs for Protection against Hot Corrosion

Award Information
Agency: Department of Defense
Branch: Navy
Contract: N68335-06-C-0173
Agency Tracking Number: N043-250-0828
Amount: $749,954.00
Phase: Phase II
Program: SBIR
Solicitation Topic Code: N04-250
Solicitation Number: 2004.3
Timeline
Solicitation Year: 2004
Award Year: 2006
Award Start Date (Proposal Award Date): 2006-05-31
Award End Date (Contract End Date): 2008-05-31
Small Business Information
1801 Maple Ave. Suite 5316
Evanston, IL 60201
United States
DUNS: 020126814
HUBZone Owned: No
Woman Owned: No
Socially and Economically Disadvantaged: Yes
Principal Investigator
 Sankar Sambasivan
 President & CEO
 (847) 467-5282
 sankar@atfinet.com
Business Contact
 John Rechner
Title: Manager, Contracts and En
Phone: (847) 467-5235
Email: jrechner@atfinet.com
Research Institution
N/A
Abstract

Ceramic matrix composites (CMCs) are being targeted for many military and commercial applications due to their lightweight and high temperature stability. CMCs possess high strength, and are being investigated for use in next-generation aircraft engines. CMCs show great promise for this application, but are subject to degradation from hot corrosion, a process in which atmospheric salts combine with engine exhaust, and can react with CMC materials at high temperatures. Hot corrosion may be a limiting factor in implementing CMCs in aircraft engines, and protection schemes are required. A thermally stable amorphous aluminum phosphate material was investigated in Phase I as a coating on non-oxide CMCs to promote resistance to hot corrosion. The coating material is a low cost, solution derived material which has a unique glass structure that is resistant to crystallization even at elevated temperatures, and has demonstrated resistance to sodium sulfate at elevated temperatures. In this Phase II project, ATFI will work with our industrial partners to build on Phase I results with the objective to develop a prototype part and explore preliminary considerations for technology transition. Effectiveness at reducing damage from hot corrosion as well as impact on mechanical properties of the CMC will be studied.

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

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