Passive air-fuel mixing prechamber
A pre-combustion chamber and fuel technology, applied in the direction of combustion chamber, continuous combustion chamber, turbine/propellant fuel delivery system, etc.
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[0060]The embodiments described herein serve to address the challenge of fuel flexible premixing in gas turbine combustion systems by enabling the fuel injection and premixing process to be more consistent over a wide range of fuel LHV and thus fuel volumetric flow rates . In virtually all gas turbine combustion system premixer designs, pressure drop occurs in the gas flow path, usually across one or more swirlers, vanes or orifices. In one design approach, the pressure drop across the fuel injection orifice is designed to approximately match the pressure drop on the air side. In this way, any sound disturbance in the combustion system affects both the air flow and the fuel flow equally; therefore, the fuel / air ratio remains somewhat constant regardless of sound pressure fluctuations. However, if a new fuel with a strongly different LHV is introduced, the change in fuel injection pressure drop will cause the system to become unbalanced, among other effects.
[0061] figure...
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