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High-temperature CMC Processing for Ceramic-to-Ceramic Joining and for Interlaminar Strength Evaluation

Award Information
Agency: Department of Defense
Branch: Navy
Contract: N68335-08-C-0489
Agency Tracking Number: N082-154-0034
Amount: $80,000.00
Phase: Phase I
Program: SBIR
Solicitation Topic Code: N08-154
Solicitation Number: 2008.2
Timeline
Solicitation Year: 2008
Award Year: 2009
Award Start Date (Proposal Award Date): 2008-08-28
Award End Date (Contract End Date): 2009-02-28
Small Business Information
31304 Via Colinas, Suite 102
Westlake Village, CA 91362
United States
DUNS: 869308346
HUBZone Owned: No
Woman Owned: No
Socially and Economically Disadvantaged: No
Principal Investigator
 HeeMann Yun
 CMC Engineering/Development
 (818) 991-8500
 heemann@matechgsm.com
Business Contact
 Ed Pope
Title: President
Phone: (818) 991-8500
Email: ed@matechgsm.com
Research Institution
N/A
Abstract

There is a strong need to develop and demonstrate inter-laminar tension test methods for CMC at high temperatures in NAVY JSF Program for aero-engine components. MATECH GSM (MG) proposes to address this need by employing a variety of innovative low-cost pre-ceramic polymer-derived high temperature CMC adhesives between CMC test coupons and push rods. MG’s high-temperature CMC adhesives are designed to facilitate ceramic-to-ceramic joining for the purpose of evaluating high temperature interlaminar strengths. Traditionally, joining adhesives are mainly developed for bonding two dissimilar materials; hence its structural performances, particularly off-axis behaviors accompanied by a necessity of non-brittle failure are mostly neglected. The CMC adhesives proposed here is a ceramic matrix composite that demonstrates graceful failure but is stronger than that of the test-coupons. Due to the two already existing given materials of the test-coupon and fixture, the newly added third material must be as physically close as possible to the other two materials from the beginning. The PIP CMC processing is only one densification method among several ceramic matrix formation routes that meet this first requirement. It is low-cost, a variety of active/non-active fillers can easily be added, and it is capable of forming shapes at low temperatures.

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

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