INCREASED TURBINE ENGINE PERFORMANCE THROUGH MAGNETIC COMPRESSION

Award Information
Agency:
Department of Defense
Branch
Air Force
Amount:
$182,000.00
Award Year:
1990
Program:
SBIR
Phase:
Phase II
Contract:
n/a
Award Id:
8717
Agency Tracking Number:
8717
Solicitation Year:
n/a
Solicitation Topic Code:
n/a
Solicitation Number:
n/a
Small Business Information
2763 Culver Ave, Dayton, OH, 45429
Hubzone Owned:
N
Minority Owned:
N
Woman Owned:
N
Duns:
n/a
Principal Investigator:
John B Barber
(513) 296-1806
Business Contact:
() -
Research Institution:
n/a
Abstract
FOR INCREASED TURBINE ENGINE PERFORMANCE HIGHER ROTOR SPEED AND COMPRESSION RATIOS ARE REQUIRED. THE OBJECTIVE OF THIS PROGRAM IS TO REDUCE THE BLADE STRESSES ASSOCIATED WITH INCREASED ROTOR SPEEDS AND COMPRESSION RATIOS. A MAGNETIC SYSTEM APPROACH WILL BE INVESTIGATED. DETAILED MECHANICAL, MAGNETIC, AND THERMAL ANALYSES WILL BE PERFORMED TO DETERMINE FEASIBILITY.

* information listed above is at the time of submission.

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