Gas turbine engine fuel injector with multiple fuel circuits
An assembly is provided for a gas turbine engine. This assembly includes a fuel injector. The fuel injector includes a nozzle and a plurality of discrete fuel circuits. The discrete fuel circuits include a first fuel circuit, a second fuel circuit and a third fuel circuit. The nozzle extends axially along an axis to a nozzle tip. The first fuel circuit includes a first fuel outlet disposed at the nozzle tip. The second fuel circuit includes a plurality of second fuel outlets arranged circumferentially about the axis at the nozzle tip in a second fuel outlet array. The third fuel circuit includes a plurality of third fuel outlets arranged circumferentially about the axis at the nozzle tip in a third fuel outlet array.
1 . An assembly for a gas turbine engine, comprising:
a fuel system including a fuel source and a fuel injector;
the fuel injector including a nozzle and a plurality of discrete fuel circuits including a first fuel circuit, a second fuel circuit and a third fuel circuit;
the nozzle extending axially along an axis to a nozzle tip;
the first fuel circuit comprising a first fuel outlet disposed at the nozzle tip, the first fuel circuit configured to direct fuel out of the nozzle through the first fuel outlet along a first trajectory;
the second fuel circuit comprising a plurality of second fuel outlets arranged circumferentially about the axis at the nozzle tip in a second fuel outlet array, the second fuel circuit further comprising a passage that extends to a first of the plurality of second fuel outlets, and the passage converges as the passage extends towards the first of the plurality of second fuel outlets, and the second fuel circuit configured to direct the fuel out of the nozzle through the first of the plurality of second fuel outlets along a second trajectory that is angularly offset from the first trajectory;
the third fuel circuit comprising a plurality of third fuel outlets arranged circumferentially about the axis at the nozzle tip in a third fuel outlet array, the third fuel circuit is configured to direct the fuel out of the nozzle through a first of the plurality of third fuel outlets along a third trajectory that is angularly offset from the first trajectory; and
the fuel system configured to deliver the fuel, during a first mode and a second mode, from the fuel source through the fuel injector where the first fuel circuit provides a first percentage of the fuel, the second fuel circuit provides a second percentage of the fuel and the third fuel circuit provides a third percentage of the fuel;
wherein, during the first mode, the first percentage and the second percentage are greater than the third percentage; and
wherein, during the second mode, the third percentage is greater than the first percentage and the second percentage.
2 . The assembly of claim 1 , wherein the fuel system is configured to deliver the fuel during a third mode, and during the third mode, the second percentage is within ten percent of the third percentage.
3 . The assembly of claim 1 , wherein, during at least one of the first mode or the second mode, the second percentage is greater than the first percentage.
4 . The assembly of claim 1 , wherein
the second trajectory is angularly offset from the first trajectory by a first angle; and
the third trajectory is angularly offset from the first trajectory by a second angle that is equal to the first angle.
5 . The assembly of claim 1 , wherein the first trajectory is coaxial with the axis.
6 . The assembly of claim 1 , wherein the first fuel outlet is coaxial with the axis.
7 . The assembly of claim 1 , wherein the first of the plurality of third fuel outlets is circumferentially offset from each of the plurality of second fuel outlets.
8 . The assembly of claim 1 , wherein the second fuel outlet array is radially aligned with the third fuel outlet array.
9 . The assembly of claim 1 , wherein the first of the plurality of second fuel outlets has a circular cross-sectional geometry.
10 . The assembly of claim 1 , wherein the first of the plurality of second fuel outlets has an elongated cross-sectional geometry.
11 . The assembly of claim 1 , wherein
the fuel injector further includes a stem;
the nozzle projects axially out from the stem along the axis to the nozzle tip;
the first fuel circuit further comprises a first fuel conduit within the stem and fluidly coupled to the first fuel outlet;
the second fuel circuit further comprises a second fuel conduit within the stem and fluidly coupled to the plurality of second fuel outlets; and
the third fuel circuit further comprises a third fuel conduit within the stem and fluidly coupled to the plurality of third fuel outlets.
12 . The assembly of claim 1 , wherein
the fuel injector further includes a stem;
the nozzle projects axially out from the stem along the axis to the nozzle tip;
the first fuel circuit further comprises a first fuel conduit within the stem and fluidly coupled to the first fuel outlet;
the second fuel circuit further comprises a second fuel conduit within the stem and fluidly coupled to the plurality of second fuel outlets; and
the third fuel circuit further comprises a third fuel conduit within the stem and fluidly coupled to the plurality of third fuel outlets;
wherein a radially extending portion of the second fuel conduit circumscribes a radially extending portion of the first fuel conduit; and
wherein a radially extending portion of the third fuel conduit circumscribes the radially extending portion of the second fuel conduit.