Slinger combustor having main combustion chamber and sub-combustion chamber, and gas turbine engine system having the same
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United States of America Patent
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Feb 2, 2021
Grant Date -
Jan 4, 2018
app pub date -
May 31, 2017
filing date -
Jul 1, 2016
priority date (Note) -
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Abstract
A slinger combustor includes; a first compressed air line connected to a compressor and configured to supply compressed air; a first fuel line connected to a fuel storage and configured to supply fuel; a rotation shaft configured to rotate and inject the fuel supplied from the first fuel line; a main combustion chamber configured to receive the fuel injected from the rotation shaft and receive the compressed air from the first compressed air line; and a sub-combustion chamber configured to selectively discharge a flame generated in an inner space of the sub-combustion chamber to the main combustion chamber.
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