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 |