发明名称 Variable volume combustor
摘要 The present application provides a variable volume combustor for use with a gas turbine engine. The variable volume combustor may include a liner, a number of micro-mixer fuel nozzles positioned within the liner, and a linear actuator so as to maneuver the micro-mixer fuel nozzles axially along the liner.
申请公布号 US9546598(B2) 申请公布日期 2017.01.17
申请号 US201313760090 申请日期 2013.02.06
申请人 GENERAL ELECTRIC COMPANY 发明人 Ostebee Heath Michael;Ziminsky Willy Steve;Johnson Thomas Edward;Keener Christopher Paul
分类号 F23R3/28;F02C7/22;F23R3/10;F23C5/06 主分类号 F23R3/28
代理机构 Sutherland Asbill & Brennan LLP 代理人 Sutherland Asbill & Brennan LLP
主权项 1. A variable volume combustor for use with a gas turbine engine, comprising: a liner; a plurality of micro-mixer fuel nozzles positioned within the liner, wherein the plurality of micro-mixer fuel nozzles is positioned within a cap assembly, wherein the plurality of micro-mixer fuel nozzles is in communication with a common fuel tube; a linear actuator attached to the common fuel tube so as to maneuver the cap assembly and the plurality of micro-mixer fuel nozzles axially along the liner; and a seal positioned between the cap assembly and the liner to create a seal between the liner and the cap assembly as the cap assembly moves axially along the liner.
地址 Schenectady NY US