SBIR/STTR Research Award

Enhancing Engine Operating Envelope by Ignition and Lean Blowout Modeling and Simulation

Award identifier 261703e55ba85e5ce2af7aa31c5acc28bc040eda36fbf6e47865dff0ebce7bc5Awarding agency Department of Defense · Air Force

Award amount

$100,000

Program and phase

SBIR · Phase I

Award year

2003

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Award details

Awarding agency
Department of Defense
Branch
Air Force
Recipient company
COMBUSTION SCIENCE & ENGINEERING, INC.
Proposal award date
Not reported
Contract end date
Not reported
UEI
FRYVEE1WQKB1
Solicitation number
Not reported
Topic code
Not reported

Research abstract

Combustion Science & Engineering, Inc. (CSE) proposes to develop an advanced modeling tool that incorporates the abilities of CFD to properly predict flow field variables with the ability to consider complicated chemical kinetics through the use ofchemical reactor modeling. This tool will be capable of predicting the ignition, relight, and lean blowout behavior of aircraft gas turbine combustor designs. Previous research has shown that the complex chemical processes involved in ignition andblowout could not be adequately represented by a single global reaction rate. Hence, analytical techniques that allow for the use of detailed chemical kinetics must be used for predicting events such as ignition, relight, or lean blowout. CSE hasdeveloped techniques that combine the use of CFD with chemical reactor modeling to predict the flameholding or blowout potential of stagnation or recirculation zones in combustors operating using lean, premixed natural gas / air mixtures. Blowout ispredicted incorporating the important fluid mechanic parameters of the potential flameholding region (determined from CFD) in PSR codes, which allow for the consideration of complex kinetics. This work serves as the basis for the proposed modeling tool.These techniques must be refined and extended for use in aircraft gas turbine engines. An important product from this project will be the development of an automated algorithm for predicting ignition and flameholding potential in combustors. Thisproduct will give the design engineer much more freedom to test new combustor designs operating at wider range of pressures, temperature and fuel / air mixtures. The market for this product will include gas turbine designers and manufacturers for bothmilitary and civilian aircraft. The use of this tool will significantly reduce development costs by eliminating some design iterations and hardware testing, which is quite expensive and time-consuming. This tool will also be useful for engineersdeveloping stationary gas turbines for power generation.

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.

Research funding history

40 SBIR/STTR records share this UEI (1999–2024). Reported award amounts total $13,904,216. Reported amounts are not federal obligations.

Phases: Phase I, Phase II

Agencies: Department of Defense, Department of Energy, Department of Health and Human Services

Agency intelligence

Department of Defense

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