SBIR/STTR Research Award

High-Temperature, High-Bandwidth Fiber Optic Pressure and Temperature Sensor for Gas Turbine Applications""

Award identifier fa7a2ae0c7c7e1b33e2fcd2e48689b99ff6714b8cfdfdb60b43d3e13fbc8779dAwarding agency Department of Defense · Air Force

Award amount

$493,041

Program and phase

STTR · Phase II

Award year

2003

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Award details

Awarding agency
Department of Defense
Branch
Air Force
Recipient company
LUNA INNOVATIONS INCORPORATED
Proposal award date
Not reported
Contract end date
Not reported
UEI
SJHFCDGKJJC5
Solicitation number
Not reported
Topic code
Not reported

Research abstract

The accurate measurement of gas flow conditions in the compressor, combustors, and turbines of gas turbine engines is important in order to assess performance, predict failure, and facilitate data-driven maintenance. Surface measurements of pressure andtemperature in high temperature regions help engineers optimize performance, and to redesign compressor and turbine stages. As higher turbine efficiencies continue to demand higher temperatures, sensor technology must keep pace to meet these demands.Clearly, there is a need for sensor systems capable of acquiring pressure and temperature measurements in high-temperature, combustion environments.During the Phase II effort, Luna will build on the Phase I research to develop a fiber optic pressure and temperature sensor capable of simultaneously measuring temperature and pressure at extreme temperatures, and high frequencies. Transducers will haveexceptional accuracy and temperature stability. All exposed material will be metal-oxide ceramics, or alloys compatible with the turbine housing. Development will continue on a newly-invented, low-cost, compact fiber optic readout system to meetfull-authority digital engine control (FADEC) applications. This Phase II effort is distinguished from related work in high-temperature sensors by the development of intrinsic temperature compensation, and of the low-cost, high-speed fiber optic readoutsystem, and of sensors compatible with that system. Research in the high temperature instrumentation area will provide transducers with commercial uses that will include 1) aerospace turbines, 2) high temperature monitoring in gas turbine power generation facilities, 3) high temperature industrial processmonitoring, and 4) automotive sensing for engine health monitoring and control. The aerospace and power gas turbine markets are each multi-billion dollar industries. Luna Innovations reasonably expects to capture at least a fraction of this market withthe proposed extreme temperature sensors, resulting in a conservative estimate of annual revenues at $10 million. As target operating temperatures increase, the market size decreases, as does the number of competitors. Our target market is the extremetemperature conditions found in gas turbines for the aerospace and power generation industries. In these applications, the ceramic-based sensors produced by Luna will dominate the high temperature sensor market.

Technology keywords

Not reported

Research funding history

994 SBIR/STTR records share this UEI (1991–2026). Reported award amounts total $336,438,763. Reported amounts are not federal obligations.

Phases: Phase I, Phase II, Phase II – Direct to Phase II

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

Agency intelligence

Department of Defense

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