Premixer array
A premixer array for a gas turbine engine includes a plurality of swirled premixer tubes and a plurality of non-swirled premixer tubes. The premixer array further includes a pilot tube for providing a pilot product. The plurality of swirled premixer tubes may guide and spread out the pilot product in a radial direction, in a circumferential direction, or both in a radial direction and a circumferential direction. The plurality of swirled premixer tubes may include clockwise swirled and counterclockwise swirled premixers. Also, included is a method of controlling the flow of pilot products.
1 . An annular mixer for a gas turbine engine, the annular mixer being located directly upstream, in a flow direction, of a combustion section of the gas turbine engine, such that, during operation of the gas turbine engine, the annular mixer provides a pilot fuel and a fuel-air mixture to the combustion section, the annular mixer comprising:
a plurality of premixer arrays arranged in a circumferential direction of the annular mixer, the plurality of premixer arrays defining an A-Zone, a B-Zone, and a C-Zone of the annular mixer that each extend in the circumferential direction with the A-Zone being adjacent to an outer liner of the combustion section, the B-Zone being disposed radially inward of the A-Zone along a radial direction, and the C-Zone being disposed radially inward of the B-Zone along the radial direction and adjacent to an inner liner of the combustion section, each premixer array of the plurality of premixer arrays comprising:
a premixer array mounting plate coupled to a bulkhead wall of the combustion section that extends between the inner liner and the outer liner, the premixer array mounting plate defining a plurality of tube ports extending therethrough, the plurality of tube ports being disposed in each of the A-Zone, the B-Zone, and the C-Zone;
one or more pilot fuel tubes coupled to the premixer array mounting plate via one or more pilot tube ports of the plurality of tube ports and configured to provide the pilot fuel to the annular mixer;
one or more non-swirled premixer tubes coupled to the premixer array mounting plate via one or more non-swirled premixer tube ports of the plurality of tube ports and configured to provide the fuel-air mixture to the annular mixer that mixes with the pilot fuel, a first non-swirled premixer tube of the one or more non-swirled premixer tubes being located in the B-Zone, and a second non-swirled premixer tube of the one or more non-swirled premixer tubes being located in the C-Zone adjacent to the first non-swirled premixer tube; and
a plurality of swirled premixer tubes coupled to a plurality of swirled premixer tube ports of the plurality of tube ports and configured to provide the fuel-air mixture to the annular mixer that mixes with the pilot fuel, the plurality of swirled premixer tubes including:
a first subset of swirled premixer tubes located in the A-Zone and configured to guide the pilot fuel radially outward along the radial direction toward the outer liner of the combustion section, a first pilot fuel tube of the one or more pilot fuel tubes being located in a center of the first subset of swirled premixer tubes;
a second subset of swirled premixer tubes located in the B-Zone and configured to guide the pilot fuel radially inward along the radial direction toward the first non-swirled premixer tube and the C-Zone; and
a single swirled premixer tube located in the C-Zone and configured to guide the pilot fuel radially inward along the radial direction toward the inner liner of the combustion section.
2 . The annular mixer of claim 1 ,
wherein, in each premixer array of the plurality of premixer arrays, the single swirled premixer tube located in the C-Zone guides the pilot fuel along the radial direction away from the second non-swirled premixer tube.
3 . The annular mixer of claim 1 , wherein, in each premixer array of the plurality of premixer arrays, at least one of the plurality of swirled premixer tubes is configured to guide the pilot fuel to the inner liner or the outer liner of the combustion section.
4 . The annular mixer of claim 1 , wherein, in each premixer array of the plurality of premixer arrays, the first subset of swirled premixer tubes, the second subset of swirled premixer tubes, or both, comprises at least one clockwise swirled premixer tube that includes first tangential openings angled in a clockwise direction such that a first flow of the fuel-air mixture through the first tangential openings exits the at least one clockwise swirled premixer tube in a clockwise manner and at least one counterclockwise swirled premixer tube that includes second tangential openings angled in a counterclockwise direction such that a second flow of the fuel-air mixture through the second tangential openings exits the at least one counterclockwise swirled premixer tube in a counterclockwise manner.
5 . The annular mixer of claim 1 , wherein, in each premixer array of the plurality of premixer arrays, at least one of the first subset of swirled premixer tubes or the second subset of swirled premixer tubes comprises a first clockwise swirled premixer tube, a second clockwise swirled premixer tube, a first counterclockwise swirled premixer tube, and a second counterclockwise swirled premixer tube.
6 . The annular mixer of claim 5 , wherein, in each premixer array of the plurality of premixer arrays, the first clockwise swirled premixer tube is located adjacent to the first counterclockwise swirled premixer tube such that a first flow of the fuel-air mixture exiting the first clockwise swirled premixer tube is opposed to a second flow of the fuel-air mixture exiting the first counterclockwise swirled premixer tube to form an opposed fuel-air mixture flow comprised of the first flow of the fuel-air mixture and the second flow of the fuel-air mixture, and wherein the opposed fuel-air mixture flow guides the pilot fuel in the radial direction.
7 . The annular mixer of claim 5 , wherein, in each premixer array of the plurality of premixer arrays, the first subset of swirled premixer tubes is configured to guide the pilot fuel from the first pilot fuel tube of the one or more pilot fuel tubes toward the outer liner of the combustion section.
8 . The annular mixer of claim 1 , wherein, in each premixer array of the plurality of premixer arrays, the second subset of swirled premixer tubes is configured to guide the pilot fuel from a second pilot fuel tube of the one or more pilot fuel tubes radially outward toward the first subset of swirled premixer tubes and radially inward toward the first non-swirled premixer tube and the single swirled premixer tube.
9 . The annular mixer of claim 1 , wherein, in each premixer array of the plurality of premixer arrays, the first subset of swirled premixer tubes is arranged in a square in plan view, the center of the first subset of swirled premixer tubes being a center of the square.
10 . The annular mixer of claim 1 , wherein, in each premixer array of the plurality of premixer arrays, the second subset of swirled premixer tubes is configured to guide the pilot fuel from a second pilot fuel tube of the one or more pilot fuel tubes radially outward along the radial direction toward the first subset of swirled premixer tubes.
11 . The annular mixer of claim 1 , wherein, in each premixer array of the plurality of premixer arrays, each of the first subset of swirled premixer tubes and the second subset of swirled premixer tubes comprises a first clockwise swirled premixer tube, a second clockwise swirled premixer tube, a first counterclockwise swirled premixer tube, and a second counterclockwise swirled premixer tube, and
wherein, in each premixer array of the plurality of premixer arrays, the first clockwise swirled premixer tube of the first subset of swirled premixer tubes is adjacent the first counterclockwise swirled premixer tube of the second subset of swirled premixer tubes and the first counterclockwise swirled premixer tube of the first subset of swirled premixer tubes is adjacent the first clockwise swirled premixer tube of the second subset of swirled premixer tubes.
12 . The annular mixer of claim 1 , wherein each premixer array of the plurality of premixer arrays further comprises a second pilot fuel tube of the one or more pilot fuel tubes that is located in the B-Zone, and
wherein, in each premixer array of the plurality of premixer arrays, the second subset of swirled premixer tubes is configured to guide the pilot fuel from the second pilot fuel tube of the one or more pilot fuel tubes radially outward toward the first subset of swirled premixer tubes and radially inward toward the first non-swirled premixer tube and the single swirled premixer tube.
13 . The annular mixer of claim 12 , wherein, in each premixer array of the plurality of premixer arrays, the first pilot fuel tube is a gas pilot fuel tube and the second pilot fuel tube is a liquid pilot fuel tube.
14 . The annular mixer of claim 13 , wherein, in each premixer array of the plurality of premixer arrays, the second pilot fuel tube of the one or more pilot fuel tubes is located in a center of the second subset of swirled premixer tubes.