Aero Propulsion and Power Technology

Award Information
Agency: Department of Defense
Branch: Air Force
Contract: F33615-01-M-2147
Agency Tracking Number: 011PR-2124
Amount: $100,000.00
Phase: Phase I
Program: SBIR
Awards Year: 2001
Solicitation Year: N/A
Solicitation Topic Code: N/A
Solicitation Number: N/A
Small Business Information
56 Rogers Street, Cambridge, MA, 02142
DUNS: 786127522
HUBZone Owned: N
Woman Owned: N
Socially and Economically Disadvantaged: N
Principal Investigator
 B.P. Masters
 VP of Engineering
 (617) 252-0660
 brett@mide.com
Business Contact
 M.C. van Schoor
Title: President
Phone: (617) 252-0660
Email: tienie@mide.com
Research Institution
N/A
Abstract
The proposed innovation is a High-bandwidth, Efficient, fuel Flow Actuator (HEFA). The design stems from a systems perspective, including power electronics, mass & volumetrically efficient driving mechanism, preferential failure modes, and thermallytolerant operation. Our solution leverages innovations in flow, mechanical packaging, electromechanical and power transfer efficiency to yield a robust performance device for combustion control. The actuator targets the problem of pressure fluctuations inaircraft engines. Specifically, it focuses on eliminating pressure fluctuations through high bandwidth modulation of the fuel. The results of controlling unwanted fluctuations are reduced high cycle fatigue (improved lifetime and reliability), improvedcombustion efficiency, and potentially reduced pollutant emissionsThe proposed solution will directly benefit DoD programs to control pressure oscillations in high performance engines such as those slated for future fighter aircraft. Furthermore, as amajor manufacturer of aircraft engines and ground based gas turbines, General Electric views the development of systems and techniques for suppressing and/or eliminating the pressure oscillations, which are inherent to all gas turbine combustion systems,as important to the reduction of engine development and operation costs.

* Information listed above is at the time of submission. *

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