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专利名称：Turbine combustor system having
aerodynamic feed cap
发明人：Khan, Abdul Rafey,Bobba, Mohan
Krishna,Crawley, Bradley Donald,Rohrssen,Robert Joseph
申请号：EP13163005.5申请日：20130409公开号：EP2653783B1公开日：20190612
摘要：Embodiment be related to reduce low discharge or without mobility status theturbine of head end (52) burner (14). Embodiment includes a kind of system, with turbinecombustors (14). Turbine combustor fuel nozzle (20) includes having inner casing (130)and shell (92), and be disposed around fuel nozzle (20) and (90) with outer wall andbackboard (88) in feed cap (50). Backboard (88) engages the shell (20) of respectiveupstream end (92) and the outer wall feed cap (50) of fuel nozzle (90). Turbine burner(14) configures the outer wall (50) so that the feed cap (90) that the first forced airextends via air path (72), the feed cap (50) of backboard (88) and entrance fuel nozzle(20).
申请人：GEN ELECTRIC
地址：US
国籍：US
代理机构：Fischer, Michael Maria
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