| 摘要 |
<p>A system for supplying fuel to a combustor 14 includes a combustion chamber 38, a liner 46 that circumferentially surrounds at least a portion of the combustion chamber 38, and a flow sleeve 48 that circumferentially surrounds at least a portion of the liner 46. A tube 60 provides fluid communication for a working fluid to flow through the flow sleeve 48 and the liner 46 and into the combustion chamber 38, and the tube 60 includes a tube wall. A plurality of fuel ports 64 through the tube wall provide fluid communication for fuel to flow through the tube wall and into the tube 60, and the fuel ports 64 are non-circular.</p> |
