Tapered fuel gallery for a fuel nozzle
A fuel injector is provided for a turbine engine. This fuel injector includes a fuel nozzle, and the fuel nozzle includes a gallery, one or more feed passages and a plurality of exit passages. The gallery extends within the fuel nozzle circumferentially around an axis between a first end of the gallery and a second end of the gallery. A size of the gallery changes as the gallery extends circumferentially around the axis between the first end of the gallery and the second end of the gallery. The one or more feed passages extend within the fuel nozzle to the gallery. The one or more feed passages are configured to supply fuel to the gallery. The exit passages extend within the fuel nozzle from the gallery. The exit passages are configured to receive the fuel from the gallery.
1. A fuel injector for a turbine engine, comprising:
a fuel nozzle comprising a gallery, a plurality of feed passages and a plurality of exit passages;
the gallery extending within the fuel nozzle circumferentially around an axis between a first end of the gallery and a second end of the gallery, a size of the gallery decreasing as the gallery extends circumferentially around the axis from the first end of the gallery to the second end of the gallery;
the plurality of feed passages extending within the fuel nozzle to the gallery, the plurality of feed passages configured to supply a fuel to the gallery, and the plurality of feed passages comprising a first feed passage that is fluidly coupled with the gallery at a first feed passage orifice;
the plurality of exit passages extending within the fuel nozzle from the gallery, the plurality of exit passages configured to receive the fuel from the gallery, and the plurality of exit passages comprising a first exit passage that is fluidly coupled with the gallery at a first exit passage orifice; and
wherein the first exit passage orifice is circumferentially between the first feed passage orifice and the first end of the gallery.
2. The fuel injector of claim 1 , wherein an axial height of the gallery decreases as the gallery extends circumferentially around the axis from the first end of the gallery to the second end of the gallery.
3. The fuel injector of claim 1 , wherein a cross-sectional area of the gallery decreases as the gallery extends circumferentially around the axis from the first end of the gallery to the second end of the gallery.
4. The fuel injector of claim 1 , wherein the plurality of feed passages are fluidly coupled to the gallery at the first end of the gallery.
5. The fuel injector of claim 1 , wherein the gallery extends, more than two-hundred and seventy degrees and less than three-hundred and sixty degrees, circumferentially around the axis from the first end of the gallery to the second end of the gallery.
6. The fuel injector of claim 1 , wherein the first exit passage extends along a centerline that is non-parallel with the axis.
7. The fuel injector of claim 1 , wherein
the plurality of feed passages further comprises a second feed passage;
the second feed passage is fluidly coupled with the gallery at a second feed passage orifice;
and
the first exit passage orifice is circumferentially between the first feed passage orifice and the second feed passage orifice.
8. The fuel injector of claim 1 , wherein
a longitudinal centerline of the first exit passage is parallel with the axis.
9. The fuel injector of claim 1 , wherein
the first exit passage orifice is a first exit passage inlet orifice and the first exit passage extends within the fuel nozzle between the first exit passage inlet orifice and a first exit passage outlet orifice; and
the first exit passage inlet orifice is circumferentially offset from the first exit passage outlet orifice.