Control Sensor for Turbine Engine Augmentor Rumble and Screech

Award Information
Agency:
Department of Defense
Branch
Air Force
Amount:
$449,949.00
Award Year:
2001
Program:
SBIR
Phase:
Phase II
Contract:
F40600-01-C-0014
Award Id:
55335
Agency Tracking Number:
001XP-0660
Solicitation Year:
n/a
Solicitation Topic Code:
n/a
Solicitation Number:
n/a
Small Business Information
87 Church Street, East Hartford, CT, 06108
Hubzone Owned:
N
Minority Owned:
N
Woman Owned:
N
Duns:
021804661
Principal Investigator:
JamesMarkham
Chief Executive Officer
(860) 528-9806
jim@AFRInc.com
Business Contact:
MichaelSerio
President
(860) 528-9806
mserio@AFRInc.com
Research Institute:
n/a
Abstract
During aircraft turbine engine operation, augmentor (afterburner) operation is often associated with combustion instabilities (oscillations) that can be potentially detrimental to the turbine engine if the resonant amplitude levels are excessive.Oscillation in the frequency range of 50-100 Hz is commonly called

* information listed above is at the time of submission.

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