SBIR/STTR Research Award

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

Award identifier 6e2f7e5071fa89f2b71a8d9177326045d24da96436f6c477ddf73dd87ae0094dAwarding agency Department of Defense · Navy

Award amount

$719,874

Program and phase

SBIR · Phase II

Award year

2008

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Award details

Awarding agency
Department of Defense
Branch
Navy
Recipient company
ULTRAMET
Proposal award date
2008-09-30
Contract end date
2011-02-10
UEI
N8ZRMWX85NZ6
Solicitation number
2006.2
Topic code
N06-146

Research abstract

Reduction of combustion-generated noise is one of the most significant challenges in the development of advanced gas turbine engines. Several processes contribute to the noise, but combustion instabilities pose the most serious threat to engine operation and safety. In Phase I, highly porous open-cell foam structures were employed to modify the combustor flow field and passively suppress unsteady flow fluctuations, thereby reducing noise. Use of structural foam inserts in gas turbine engines offers an effective, simple, and reliable approach for combustion control and noise reduction. Material development and component fabrication were conducted by Ultramet, and design, analysis, and component testing were performed by the University of Alabama. Two approaches were explored. In the first, the foam insert was located downstream of the reaction zone to dissipate the combustion noise and instability generated upstream. In the second, the vortex shedding mechanism of combustion instability was curtailed by placing the foam insert within the recirculation region of the reaction zone. The porous insert media were experimentally demonstrated to reduce combustion noise by up to 15 dB, depending on the operating conditions and test configuration. In Phase II, Ultramet will team with the University of Alabama and Solar Turbines (a subsidiary of Caterpillar Inc.), the world’s largest manufacturer of small- and medium-sized (1 to 5 MW) industrial gas turbines, to perform comprehensive component design and material optimization, ultimately leading to performance demonstration of open-cell foam noise reduction components through hot-fire testing under realistic turbine operating conditions using gaseous methane propellant.

Technology keywords

Not reported

Other awards by this recipient

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Awards with the same topic code

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

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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