Control of Fuel Atomization and Mixing for Emission Reduction in High Performance Gas Turbines

Award Information
Agency: Department of Defense
Branch: Air Force
Contract: FA8650-04-M-2445
Agency Tracking Number: F041-182-2695
Amount: $99,808.00
Phase: Phase I
Program: SBIR
Awards Year: 2004
Solicitation Year: 2004
Solicitation Topic Code: AF04-182
Solicitation Number: 2004.1
Small Business Information
DUNS: 966649048
HUBZone Owned: N
Woman Owned: N
Socially and Economically Disadvantaged: Y
Principal Investigator
 Mohammed Mawid
 Technical Director
 (937) 255-2007
Business Contact
 Mohammed Mawid
Title: Technical Director
Phone: (937) 255-2007
Research Institution
An innovative ariblast-based single-lip fuel injector with piloted fuel for advanced military gas turbine combustors is proposed for development in this SBIR. The proposed innovative fuel injector design concept will significantly improve the mixing performance of fuel and air in the vicinity of the fuel injector, thus resulting in substantially improved fuel/air mixture distribution, homogenities, uniformity and significantly lower NOx production. The proposed design concept will also reduce the mixing length required to achieve well-mixed fuel and air prior to burning and consequently shortening the mixture residence time, which will decrease combustor length and consequently engine's weight.

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

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