发明名称 FUEL NOZZLE CAP
摘要 Certain embodiments include a first individual sector having a first outer perimeter configured to fit together with outer perimeters of a plurality of individual sectors to form a combustor cap assembly of a turbine combustor, wherein the first individual sector comprises a first inner perimeter configured to fit about a nozzle outer perimeter of a first fuel nozzle, and the first individual sector is configured to fixedly attach to the first fuel nozzle.
申请公布号 US2013305725(A1) 申请公布日期 2013.11.21
申请号 US201213475882 申请日期 2012.05.18
申请人 BERRY JONATHAN DWIGHT;GENERAL ELECTRIC COMPANY 发明人 BERRY JONATHAN DWIGHT
分类号 F23R3/28 主分类号 F23R3/28
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