发明名称 Air-fuel premixer for gas turbine combustor with variable swirler
摘要 <p>A swirler assembly (2) in a gas turbine combustor includes a hub (201), a shroud, (202) and a plurality of vanes (23) connected between the hub (201) and the shroud (202). a vane angle of the plurality of vanes (23) is adjustable.</p>
申请公布号 EP2613086(A2) 申请公布日期 2013.07.10
申请号 EP20120198037 申请日期 2012.12.19
申请人 GENERAL ELECTRIC COMPANY 发明人 BATHINA, MAHESH;PANDA, AMULYA
分类号 F23R3/14;F23C7/00;F23R3/28 主分类号 F23R3/14
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