Implication of as Manufactured Delaminations on CMC the Life of Ceramic Matrix Composites

Award Information
Agency:
Department of Defense
Branch
n/a
Amount:
$99,914.00
Award Year:
2011
Program:
SBIR
Phase:
Phase I
Contract:
FA8650-11-M-5129
Award Id:
n/a
Agency Tracking Number:
F103-141-1850
Solicitation Year:
2010
Solicitation Topic Code:
AF103-141
Solicitation Number:
2010.3
Small Business Information
300 E. Swedesford Rd, Wayne, PA, -
Hubzone Owned:
N
Minority Owned:
N
Woman Owned:
N
Duns:
966563884
Principal Investigator:
Guido Teti
Program Manager
(610) 964-9000
guido.teti@m-r-d.com
Business Contact:
Kent Buesking
President
(610) 964-9000
buesking@m-r-d.com
Research Institution:
Stub




Abstract
The goal of the testing is to develop and life prediction theories which describe the structural re-sponse in CMCs with delaminations emanating from manufacturing imperfections. Much work have been done studying the effects of defects in CMCs particularly in the area of porosity, but no one has clearly explained the failure mechanisms ovserved in advanced CMC jet engine after burner flaps and seals. Analysis and physical evidence indicates that the combined thermo-structural and acoustic loadings combined with CMC thermal ageing/oxidation cause It is believed that the combined thermo-structural and acoustic loadings combined with thermal ageing cause the delaminations to spread across the CMC resulting in surface ply loss. The objective of the proposed effort will be to execute a research program to develop the appropriate representative S200 CMC material samples with delaminations of various sizes in test specimens and test types, and to demonstrate through tests, mathematical composite materials analysis, fracture based delamination growth modeling and finite element modeling the ability to predict test specimen structural delamination growth rate as a function of time, temperature and stress with and with-out production reportable delaminations through pre and post-test analysis predictions. BENEFIT: Several Air Force programs for ceramics matrix composites (CMCs) are targeted for use in ad-vanced jet engines. Examples are the Integrated High Performance Turbine Engine Technology (IHPTET) initiative, the versatile affordable advanced turbine engines (VAATE) initiative, Joint Strike Fighter (JSF) etc. This research will help prime engine contractor like Pratt & Whitney, Rolls Royce and General Electric.

* information listed above is at the time of submission.

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