Variable volume combustor
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.
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.
2. The variable volume combustor of claim 1 , wherein the plurality of micro-mixer fuel nozzles comprises a plurality of micro-mixer fuel tubes and a fuel plate.
3. The variable volume combustor of claim 1 , wherein the common fuel tube comprises a plurality of fuel circuits therein.
4. The variable volume combustor of claim 1 , wherein the linear actuator comprises a drive rod in communication with the common fuel tube for movement therewith.
5. The variable volume combustor of claim 1 , wherein the linear actuator is positioned adjacent an end cover.
6. The variable volume combustor of claim 1 , wherein maneuvering the plurality of micro-mixer fuel nozzles along the liner varies a liner volume.
7. The variable volume combustor of claim 1 , wherein maneuvering the plurality of micro-mixer fuel nozzles along the liner varies a head end volume.
8. The variable volume combustor of claim 1 , further comprising a plurality of linear actuators.
9. A method of operating a combustor in a gas turbine, comprising:
positioning a plurality of micro-mixer fuel nozzles within a 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 that comprises a flow of fuel therein, wherein a flow of air enters an aft end of the plurality of micro-mixer fuel nozzles and mixes therein with the flow of fuel from the common fuel tube;
maneuvering the cap assembly and the plurality of micro-mixer fuel nozzles along the liner in a first direction by a linear actuator attached to the common fuel tube to provide a first liner volume, wherein the common fuel tube is maneuverable by the linear actuator;
maneuvering the cap assembly and the plurality of micro-mixer fuel nozzles along the liner in a second direction to provide a second liner volume; and
positioning a seal 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.
10. The method of claim 9 , wherein the first liner volume comprises a first reaction residence time and wherein the second liner volume comprises a second reaction residence time.
11. 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 for movement therewith, wherein the common fuel tube comprises a flow of fuel therein, wherein a flow of air enters an aft end of the plurality of micro-mixer fuel nozzles and mixes therein with the flow of fuel from the 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 so as to change a volume of 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.
12. The variable volume combustor of claim 11 , wherein the plurality of micro-mixer fuel nozzles comprises a plurality of micro-mixer fuel tubes and a fuel plate.
13. The variable volume combustor of claim 11 , wherein the linear actuator comprises a drive rod in communication with the common fuel tube for movement therewith.