Turbine engine with combustor premix system

Power plants – Combustion products used as motive fluid

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Details

60 3923, 60736, 60737, 60745, F02C 7224

Patent

active

044295278

ABSTRACT:
A turbine engine having a combustor premix system for mixing fuel and air to provide increased efficiency by reducing temperature peaks in the combustor. The system includes a primary mixing chamber for mixing compressed air and atomized fuel and a secondary mixing chamber located between the primary mixing chamber and the combustor for mixing additional compressed air to the fuel-air mixture. The secondary mixing chamber comprises a plurality of tubes with air metering ports in the walls thereof and a control assembly to vary the air flow to the ports for off design engine operating conditions, and optimizes fuel-air mixtures for the combustor at all engine operating speeds improving fuel economy and exhaust pollution control. The primary mixing chamber is located adjacent to and between the compressor for the air and the combustor so that the fuel-air mixture flowing therethrough tends to cool the compressor and the chamber itself shields the compressor from radiant heat from the combustor.

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Nagey et al., "Low Emission Turbine Passenger Car?", Mechanical Engineering, Jan., 1974.
NASA Jet Propulsion Laboratory, "Two-Stage Combustor Reduces Pollutant Emissions", NASA Tech Briefs, Spring, 1981.

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