GAS TURBINE COMBUSTION CHAMBER
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United States of America Patent
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Issued Date -
May 29, 2014
app pub date -
Feb 22, 2012
filing date -
Feb 25, 2011
priority date (Note) -
Abandoned
status (Latency Note)
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Abstract
The present invention relates to a gas-turbine combustion chamber with an outer combustion chamber wall concentric to a gas-turbine center axis and with an inner combustion chamber wall, with several burners arranged spread over the circumference of the combustion chamber, and with air inlet recesses which in at least one radial plane are provided spread over the circumference on an outer combustion chamber wall and on an inner combustion chamber wall, where the burner is designed to form a flow provided with a swirl and where air inlet recesses assigned to a burner are dimensioned in differing size in order to generate airflows of differing size, characterized in that at least one of the respective air inlet recesses is designed for supplying air in the flow direction of the swirl of the combustion chamber flow and is provided with flow guidance walls.
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