COMBUSTOR SYSTEMS AND METHODS
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United States of America Patent
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Issued Date -
Feb 22, 2024
app pub date -
Nov 3, 2021
filing date -
Nov 12, 2020
priority date (Note) -
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Abstract
System comprising a gas turbine engine fuel injection apparatus (11) arranged to deliver to a combustion chamber (9) of a gas turbine engine a first injection fluid comprising a first fuel and a second injection fluid comprising a second fuel. The apparatus is arranged to deliver the first and second injection fluids in a manner such that the first injection fluid is delivered in a first stream and the second injection fluid is delivered in a second stream. Further, such that there is a delivery zone (47) corresponding to a first location at which both the first and second streams have been delivered in which the first stream is substantially radially surrounded by the second stream.
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