Control Sensor for Turbine Engine Augmentor Rumble and Screech

Award Information
Agency:
Department of Defense
Branch:
Air Force
Amount:
$0.00
Award Year:
2001
Program:
SBIR
Phase:
Phase I
Contract:
F40600-01-C-0014
Agency Tracking Number:
001XP-0660
Solicitation Year:
N/A
Solicitation Topic Code:
N/A
Solicitation Number:
N/A
Small Business Information
ADVANCED FUEL RESEARCH, INC.
87 Church Street, East Hartford, CT, 06108
Hubzone Owned:
N
Socially and Economically Disadvantaged:
N
Woman Owned:
N
Duns:
021804661
Principal Investigator
 James Markham
 Chief Executive Officer
 (860) 528-9806
 jim@AFRInc.com
Business Contact
 Michael Serio
Title: President
Phone: (860) 528-9806
Email: mserio@AFRInc.com
Research Institution
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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