专利名称：COMBUSTOR ASSEMBLY FOR A TURBINE
ENGINE
发明人：Gregory Allen Boardman,Pradeep Naik,Allen
Michael Danis
申请号：US15189061申请日：20160622
公开号：US20170370588A1公开日：20171228
专利附图：
摘要：A rich-quench-lean combustor assembly for a gas turbine engine includes a linerextending between a forward end and an aft end. The liner includes a plurality of quench
air jets positioned between the forward end and the aft end. The combustor assemblyadditionally includes a dome attached to or formed integrally with the liner, the domeand the liner together defining at least in part a combustion chamber. A fuel nozzle isattached to the dome, the fuel nozzle configured as a premix fuel nozzle for providing asubstantially homogenous mixture of fuel and air to the combustion chamber, themixture of fuel and air having an equivalence ratio of at least 1.5.
申请人：General Electric Company
地址：Schenectady NY US
国籍：US
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