SBIR/STTR Research Award

Passive Combustion Control Device for Noise Reduction and Improved Life in Turbine Engines

Award identifier 7f2cbe90db145c98617441d877fe467dc981df5b91b5b66e407e647349a0d833Awarding agency Department of Defense · Navy

Award amount

$100,000

Program and phase

SBIR · Phase I

Award year

2007

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Award details

Awarding agency
Department of Defense
Branch
Navy
Recipient company
ULTRAMET
Proposal award date
2006-11-29
Contract end date
2007-12-15
UEI
N8ZRMWX85NZ6
Solicitation number
2006.2
Topic code
N06-146

Research abstract

To reduce combustion instability and noise in turbine engines, Ultramet will team with the University of Alabama to design, model, fabricate, and test refractory hafnium carbide/silicon carbide open-cell ceramic foam to be used in the combustion chamber as a passive control device. Previous work at the University of Alabama utilized Ultramet’s open-cell silicon carbide foam as a porous insert medium burner for lean premixed combustion to reduce pollutant emissions. When combustion took place inside the foam, nitrogen oxide and carbon monoxide emissions were greatly reduced; temperature across the test burner was homogenized; and the noise level inside the combustor was drastically reduced. However, the lifetime of the silicon carbide foam burner was limited because of the relatively low melting point of the silicon dioxide protective layer that forms at the surface. The proposed ceramic alloy foam is protected from oxidation by a much more refractory surface oxide, hafnium silicate, which offers a nominally 1000°F higher use temperature. The ceramic alloy also has improved survivability in combustion environments containing a significant quantity of water vapor. Two approaches using open-cell foam as a passive control device will be explored. In the first, the foam will be located downstream of the reaction zone to dissipate the combustion noise and/or instability generated upstream. In the second, the vortex shedding mechanism of combustion instability will be curtailed by placing foam within the recirculation region of the reaction zone.

Technology keywords

Not reported

Other awards by this recipient

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Awards with the same topic code

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Research funding history

380 SBIR/STTR records share this UEI (1983–2025). Reported award amounts total $105,154,309. 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, National Science Foundation, Department of Transportation, Department of Health and Human Services

Agency intelligence

Department of Defense

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