SBIR/STTR Research Award

Turbine Inlet Gas Temperature Measurement System

Award identifier 9ba1594514b4c3420799c34badbbd447b7696e3da260f1f7359f850dd71c8616Awarding agency Department of Defense · Air Force

Award amount

$749,995

Program and phase

SBIR · Phase II

Award year

2010

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Award details

Awarding agency
Department of Defense
Branch
Air Force
Recipient company
ADVANCED FUEL RESEARCH, INC.
Proposal award date
2010-09-30
Contract end date
2012-09-30
UEI
E7PVK58C6UJ5
Solicitation number
2008.3
Topic code
AF083-260

Research abstract

The Air Force is seeking new technology that will provide the means to accurately measure and monitor turbine inlet gas temperature in gas turbine engines, particularly in advanced engines operating at very high temperatures (>3,100 degree F). In Phase I of this program, Advanced Fuel Research, Inc. demonstrated that turbine inlet gas temperature can be determined from non-intrusive measurements of the thermal radiation emitted by gases in the turbine inlet region. A pattern recognition algorithm utilizing a neural network was developed to determine the temperature by monitoring the emission signatures of combustion products in the gas stream, despite the presence of thermal radiation from surrounding hot surfaces. The technique is entirely passive, and provides a line-of-sight temperature measurement in the turbine inlet region without intrusion into the gas path. In Phase II, the techniques demonstrated in Phase I will be extended and advanced to yield a deliverable prototype that provides accurate temperature measurements over the full range of temperatures and pressures encountered in advanced gas turbine engines. During this development project, the Phase II prototype will be field tested on advanced combustion rigs at a private-sector research center and a federal research center. The deliverable system will provide significant benefits to the Air Force during the development testing of advanced engines, yielding engines with higher specific power, lower emissions, and increased efficiency. BENEFIT: The project will result in a product that will benefit the military and military aircraft engine industry and also find dual use by benefiting the commercial aircraft engine industry and power generation industry that utilize gas turbine engines. In addition to commercial applications in the gas turbine engine industries, commercial applications include other combustion-dependent markets including U.S. manufacturing industries of steel, aluminum, metal casting, glass, chemicals, forest products, and petroleum.

Technology keywords

Not reported

Other awards by this recipient

Verified by the same UEI. These are other public SBIR/STTR award pages, not a merged company record.

Awards with the same topic code

Verified by an exact topic code match. This is not a text-similarity match.

Research funding history

248 SBIR/STTR records share this UEI (1983–2021). Reported award amounts total $48,007,871. Reported amounts are not federal obligations.

Phases: Phase I, Phase II

Agencies: Department of Defense, Department of Energy, National Science Foundation, National Aeronautics and Space Administration, Environmental Protection Agency, Department of Commerce

Agency intelligence

Department of Defense

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