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The flow model proposed in this work stimulates the 'sequential combustor system' where a second combustion chamber is employed after the first stages of the turbine.
In many situations, combustion instabilities involve a coupling between the non-steady combustion process and the acoustic modes of the combustor system.
The coupling between the fluid dynamics, heat addition, and the acoustics of a combustor system determine whether it is prone toward combustion instability.
This study also shows that the fundamental frequency of the combustor system should be within the range of critical frequencies of the non-reactive burner system to sustain possible sound emissions.
In this combustor system, catalytic combustion temperature is controlled under 1000 °C, premixed gas is injected from the premixing nozzles to the catalytic combustion gas and lean premixed combustion over 1300 °C is carried out in the ceramic liner.
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The device emulated several features of practical combustor systems but with a simpler geometry, well-defined boundary conditions and using the simplest configuration found in literature (laminar flames).
In a chemical looping combustor (CLC) system, the solid circulation rate (SCR) is a key parameter that determines the design, operating conditions and the overall efficiency of the system.
By incorporating the designed micro planar combustor into the micro-TPV system, a system efficiency of 4.1% could be obtained.
In this paper, a new type of micro planar combustor for micro thermophotovoltaic system is proposed, which has multi-mode heat transfer passages in the combustion channel.
However, in the SOFC/GT hybrid system, the combustor temperature can be controlled, by manipulating the fuel cell current, to regulate the amount of fuel sent to the combustor.
This study proposes a multiple-channel micro combustor for a micro-TPV system.
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