公开(公告)号：EP3254032A2

公开(公告)日：2017-12-13

申请号：EP16706097.9

申请日：2016-02-04

申请人： ExxonMobil Upstream Research Company

发明人： BORCHERT, Bradford David ,  TROUT, Jesse Edwin ,  SIMMONS, Scott Robert ,  VALEEV, Almaz ,  SLOBODYANSKIY, Ilya Aleksandrovich ,  SIDKO, Igor Petrovich ,  GINESIN, Leonid Yul'evich

IPC分类号： F23R3/10 ,  F23C9/00 ,  F23R3/28

CPC分类号： F23R3/28 ,  F02C3/04 ,  F02C3/34 ,  F23C9/00 ,  F23C2202/50 ,  F23R3/002 ,  F23R3/10 ,  F23R3/286 ,  F23R3/30 ,  F23R3/32 ,  F23R3/343 ,  F23R3/346 ,  F23R3/36 ,  F23R2900/00001 ,  F23R2900/00005 ,  Y02E20/16 ,  Y02T50/675

摘要： A system having a gas turbine engine is provided. The gas turbine engine includes a turbine and a combustor coupled to the turbine. The combustor includes a combustion chamber, one or more fuel nozzles upstream from the combustion chamber, and a head end having an end cover assembly. The end cover assembly includes an oxidant inlet configured to receive an oxidant flow, a central oxidant passage, and at least one fuel supply passage. The central oxidant passage is in fluid communication with the oxidant inlet, and the central oxidant passage is configured to route the oxidant flow to the one or more fuel nozzles. The at least one fuel supply passage is configured to receive a fuel flow and route the fuel flow into the one or more fuel nozzles.