Self repairing Composites for Airplane Components

Award Information
Agency:
Department of Defense
Branch:
Air Force
Amount:
$499,999.00
Award Year:
2005
Program:
SBIR
Phase:
Phase II
Contract:
FA8650-05-C-3510
Agency Tracking Number:
F031-1888
Solicitation Year:
2003
Solicitation Topic Code:
AF03-238
Solicitation Number:
2003.1
Small Business Information
NATURAL PROCESS DESIGN
1250 East Eighth Street, Winona, MN, 55987
Hubzone Owned:
N
Socially and Economically Disadvantaged:
N
Woman Owned:
Y
Duns:
023802098
Principal Investigator
 Carolyn Dry
 President
 (507) 452-9113
 drycementmixer@aol.com
Business Contact
 Carolyn Dry
Title: President
Phone: (217) 452-9113
Email: drycementmixer@aol.com
Research Institution
N/A
Abstract
In self-repairing composites, usually liquid chemicals are contained inside a fiber or bead vessel that is embedded inside the polymer composite matrix or laminate. Damage such as an impact or fatigue microcracking causes the breaking of the vessel, release of internal chemicals into the damage site where they wet the sides of the damage site, react together or with the matrix resin and close or fill the damage thus repairing the composite. This very accurate repair, which occurs whenever and wherever needed, would enable the self-repair of thermoset composite laminates such as airplanes components. Even though the system from Phase I is shown to be feasible, there are areas to refine in system design in order to make a prototype in SBIR Phase II. The drive to a more commercializable product will include more complex and slightly larger specimens made by autoclave and/or vartm which are subjected to simulated conditions of the end use.

* information listed above is at the time of submission.

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