Control Sensor for Turbine Engine Augmentor Rumble and Screech

Award Information
Agency: Department of Defense
Branch: Air Force
Contract: F40600-01-C-0014
Agency Tracking Number: 001XP-0660
Amount: $449,949.00
Phase: Phase II
Program: SBIR
Awards Year: 2001
Solicitation Year: N/A
Solicitation Topic Code: N/A
Solicitation Number: N/A
Small Business Information
87 Church Street, East Hartford, CT, 06108
DUNS: 021804661
HUBZone Owned: N
Woman Owned: N
Socially and Economically Disadvantaged: N
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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