THERAPEUTIC ANGIOGENESIS BY SF/HGF GENE TRANSFER

Award Information
Agency:
Department of Health and Human Services
Amount:
$99,975.00
Program:
SBIR
Contract:
N/A
Solitcitation Year:
N/A
Solicitation Number:
N/A
Branch:
N/A
Award Year:
1999
Phase:
Phase I
Agency Tracking Number:
1R43HL062048-01
Solicitation Topic Code:
N/A
Small Business Information
ANGION BIOMEDICA CORPORATION
14 BOND ST, STE 100, GREAT NECK, NY, 11021
Hubzone Owned:
N
Woman Owned:
N
Socially and Economically Disadvantaged:
N
Duns:
N/A
Principal Investigator
 PETER MENTO
 () -
Business Contact
Phone: (516) 869-6400
Research Institution
N/A
Abstract
Not Available High Cycle Fatigue (HCF) is affecting aircraft system readiness, operability and cost of ownership. State-of-the-art passive damping treatments, while effective, are limited to temperatures below 500 degrees F and to static structures. The needs and environment posed by gas turbine engines far exceed the limitations of the available viscoelastic damping treatments. MiTi has conceived a powder structural damping approach that is insensitive to temperature and accounts for the high centrifugal loads encountered in rotating airfoils. Initial powder damping feasibility has been demonstrated and powder material damping characteristics are being experimentally determined. Transfer of this new technology to practical applications requires evaluation in structural elements to verify the proposed design stategies. In support of this program and to ensure technology transfer to product, major engine company support has been obtained. Specific objectives of this program are to 1) develop a high temperature powder damping design methodology for both rotating and static structural elements, 2) design and build a powder damped cantilever beam test specimen using powder material damping data presently being acquired under Air Force sponsorship, 3) fabricate the cantilever beam test specimen and demonstrate the effect of powder damping in controlling blade vibratory response, and 4) prepare a preliminary design of a simulated blade for detailed static and rotating verification testing

* information listed above is at the time of submission.

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