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High-Temperature Environmental Barrier Coating for Silicon Carbide Composites

Award Information
Agency: Department of Defense
Branch: Air Force
Contract: FA9550-11-C-0010
Agency Tracking Number: F08B-T21-0191
Amount: $749,957.00
Phase: Phase II
Program: STTR
Solicitation Topic Code: AF08-BT21
Solicitation Number: 2008.B
Timeline
Solicitation Year: 2008
Award Year: 2011
Award Start Date (Proposal Award Date): 2010-10-28
Award End Date (Contract End Date): N/A
Small Business Information
2 Boars Head Lane
Charlottesville, VA -
United States
DUNS: 036500804
HUBZone Owned: No
Woman Owned: No
Socially and Economically Disadvantaged: No
Principal Investigator
 Derek Hass
 Dir. of Research and Development
 (434) 977-1405
 derekh@directedvapor.com
Business Contact
 Harry Burns
Title: Pres.&CEO
Phone: (434) 977-1405
Email: harryburns@directedvapor.com
Research Institution
 Univ. of California Santa Barbara
 Carlos Levi
 
1361D Engineering II
Santa Barbara, CA 93106-
United States

 (805) 893-2381
 Nonprofit College or University
Abstract

ABSTRACT: Lightweight silicon-based ceramics are leading candidates to replace heavier nickel-based superalloys for use on hot section components in next generation gas turbine engines having increased specific power. However, exposures of these materials to the high temperatures, pressures and velocities of water vapor containing combustion environments alter the effectiveness of thermally grown silica scales in protecting the ceramic components from oxidation and component recession during service. Environmental barrier coatings(EBCs) are therefore required that protect the underlying ceramic substrate from environmental attack. Such coatings require good stability in the presence of water vapor, a mechanism for limiting the transport of oxygen and water vapor, good chemical compatibility at the interface of unlike materials, high temperature phase stability to limit volume changes resulting from phase transformations in the coating materials and the ability to provide thermal and erosion protection. The ongoing drive to promote higher temperature protection and prime reliant performance of these systems has led to interest in advanced thermal/environmental barrier coating(T/EBC) systems having enhanced performance over current state-of-the-art T/EBC systems. In this work, novel coating synthesis techniques that enable the deposition of multilayered T/EBC"s anticipated to have higher temperature capability and improved durability over of current systems are investigated. BENEFIT: This research is anticipated to result in a thermal/environmental barrier coating system that provides higher temperature capability, improved durability and better erosion resistance than current coatings. These advancements will enable the use of Si-based ceramics in a range of high temperature applications such a gas turbine engines and heat exchangers. These advances will not only benefit military engines, but also commercial and industrial engines requiring greater performance.

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

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