Optical Flame Emissions Sensor for High-Speed Reacting Flows

Award Information
Agency: Department of Defense
Branch: Air Force
Contract: F33615-01-C-2126
Agency Tracking Number: 001PR-1940
Amount: $749,758.00
Phase: Phase II
Program: SBIR
Awards Year: 2001
Solicitation Year: N/A
Solicitation Topic Code: N/A
Solicitation Number: N/A
Small Business Information
INNOVATIVE SCIENTIFIC SOLUTIONS, INC.
2766 Indian Ripple Rd, Dayton, OH, 45440
DUNS: 884812025
HUBZone Owned: N
Woman Owned: N
Socially and Economically Disadvantaged: N
Principal Investigator
 Cambell Carter
 Senior Engineer
 (937) 255-8704
 cartercd@innssi.com
Business Contact
 Larry Goss
Title: President
Phone: (937) 429-4980
Email: gosslp@innssi.com
Research Institution
N/A
Abstract
Optical emissions sensors have the potential to be used in gauging combustion activity and quantifying heat release, fuel-air mixture, and combustor efficiency within a wide variety of combustor devices (both stationary and mobile). We propose to developboth chemiluminescence sensors-to derive equivalence ratio within the cavity pilot flame from the measured quantities, OH*, CH* and/or C2*-and infrared emissions sensors-to derive combustor efficiency from measured quantities, H2O, CO2, CO andtemperature-for supersonic combusting ramjet (scramjet) engines. The principal advantage of this approach over other optical-sensors-based approaches (e.g., absorption) is greater simplicity, since only a suitable photodetector is needed. In addition,solid-state optical emissions sensors are rugged, possess a wide field of view, require minimal optical access, and can be configured for species selectivity. During the Phase II program, we will develop combustor optical emission sensor hardware andsoftware for implementation in a scramjet combustor. Additional tasks involve designing rugged coupling optics/electronics and testing these designs in a direct-connect scramjet test facility.

* information listed above is at the time of submission.

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