SBIR/STTR Research Award

Innovative Subgrid-Scale Combustion Modeling for Gas Turbines

Award identifier 2c2937922070633cb3427f0362a23d7310b6bd18f721804143d8fcd6d577af0dAwarding agency Department of Energy

Award amount

$99,499

Program and phase

SBIR · Phase I

Award year

2010

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Award details

Awarding agency
Department of Energy
Branch
Not reported
Recipient company
COMBUSTION RESEARCH & FLOW TECHNOLOGY INC
Proposal award date
Not reported
Contract end date
2011-03-18
UEI
XGYZK5MHNJZ8
Solicitation number
DE-FOA-0000161
Topic code
39 a

Research abstract

New high-efficiency, low-emission, fuel-flexible gas turbine designs will operate at fuel lean conditions near the flame blow-out limit. To maintain high efficiency and flame stability under these conditions, a detailed knowledge of the flame dynamics will be required from both experimental and computational studies. From a computational perspective, accurate turbulent combustion models are required to evaluate advanced turbine designs. However, current combustion models applied for design analysis lack the necessary physical modeling to accurately predict flows near the lean blow-out limit. Under this proposed effort a new and innovative modeling strategy will be developed to accurately predict flows near the lean blow-out limit. This new model will also be computationally inexpensive so that it may be applied routinely within design analysis. The objective of this program is to develop a fast running, turbulent combustion model for large eddy simulation (LES) that will be accurate for all flame regimes of gas turbine operation, including near the lean blow-out limit. This new formulation will be based on a parameterization of the linear-eddy model (LEM). The LEM is a comprehensive mixing model that accurately captures the interaction of flow turbulence with flame structure in all flame regimes. Statistics from this model will be parameterized in terms of a reduced set of variables and stored within a database that is used to produce the required closure statistics for an LES prediction. This model will be fast because the closure statistics are retrieved from a database and not computed during the simulation. The model will also be general and applicable to all flame regimes because the closure statistics will be produced from the LEM formulation. Commercial Application and Other Benefits: A software tool kit developed under this effort will produce the model statistics and database required for an LES prediction. The database for a particular problem may be used within any CFD flow solver, and for RANS flow solvers as well. Combustion models generated by the tool kit will be applicable to a wide range of military and commercial combustion applications including gas turbines, power generation systems, furnaces, incinerators, internal combustion engines, aircraft engines, etc. CRAFT Tech will market this tool kit for license to commercial customers as well as to other CFD flow solver development companies.

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

303 SBIR/STTR records share this UEI (1995–2025). Reported award amounts total $121,181,328. 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

Agency intelligence

Department of Energy

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