Annular dome assembly for a combustor
An annular dome assembly for a combustor. The annular dome assembly includes an annular dome including one or more dome panels defining the annular dome. A first dome panel includes a dome upstream surface and a dome downstream surface opposite the dome upstream surface. One or more dome arms extend from the dome upstream surface. One or more apertures extend from the dome upstream surface to the dome downstream surface. The annular dome assembly also includes a deflector assembly including one or more deflector panels defining the deflector assembly. A first deflector panel includes a deflector upstream surface and a deflector downstream surface opposite the deflector upstream surface. One or more deflector arms extend from the deflector upstream surface. Each of the one or more deflector arms are mounted within a respective aperture of the annular dome.
1. An annular dome assembly for a combustor, the annular dome assembly comprising:
an annular dome including one or more dome panels defining the annular dome, a first dome panel of the one or more dome panels including:
a dome upstream surface and a dome downstream surface opposite the dome upstream surface;
an opening for receiving a mixer assembly;
a plurality of dome arms extending from the dome upstream surface; and
a plurality of apertures extending through the first dome panel from the dome upstream surface to the dome downstream surface, wherein the plurality of dome arms define the plurality of apertures; and
a deflector assembly including one or more deflector panels defining the deflector assembly, a first deflector panel of the one or more deflector panels including:
a deflector upstream surface and a deflector downstream surface opposite the deflector upstream surface; and
a plurality of deflector arms extending from the deflector upstream surface, each of the plurality of deflector arms mounted within a respective aperture of the first dome panel and extending upstream of the dome upstream surface, wherein the plurality of deflector arms is spaced around a first circumference that is defined about the opening of the first dome panel, has a first diameter, and is radially between the opening and an outer circumference of the first deflector panel, each of the plurality of deflector arms being positioned at the first diameter.
2. The annular dome assembly of claim 1 , wherein the plurality of deflector arms is a first plurality of deflector arms, the first deflector panel further including a second plurality of deflector arms spaced around a second circumference that is defined about the opening of the first dome panel, has a second diameter, and is radially between the opening and the outer circumference of the first deflector panel, each of the plurality of deflector arms being positioned at the second diameter.
3. The annular dome assembly of claim 2 , wherein the second diameter is greater than the first diameter.
4. The annular dome assembly of claim 1 , wherein the plurality of dome arms and the plurality of deflector arms are secured together by one or more fastening mechanisms disposed entirely upstream of dome upstream surface.
5. The annular dome assembly of claim 4 , wherein the one or more fastening mechanisms include at least one of brazing or welding.
6. The annular dome assembly of claim 4 , wherein the one or more fastening mechanisms include at least one of studs, bolts, screws, or rivets.
7. The annular dome assembly of claim 6 , wherein the at least one of the studs, the bolts, the screws, or the rivets are inserted radially through the plurality of dome arms and the plurality of deflector arms.
8. The annular dome assembly of claim 1 , wherein the first deflector panel includes a plurality of segments.
9. The annular dome assembly of claim 8 , wherein each of the plurality of segments includes one or more of the plurality of deflector arms.
10. The annular dome assembly of claim 8 , wherein the plurality of segments are separated by one or more gaps formed between each of the plurality of segments, wherein the one or more gaps are shaped to provide a flow of cooling air to the deflector downstream surface of the first deflector panel.
11. A turbine engine comprising:
a combustion section including an annular dome assembly and a plurality of mixer assemblies, the annular dome assembly comprising:
an annular dome including one or more dome panels defining the annular dome, a first dome panel of the one or more dome panels including:
a dome upstream surface and a dome downstream surface opposite the dome upstream surface;
an opening for receiving a mixer assembly;
a plurality of dome arms extending from the dome upstream surface; and
a plurality of apertures extending through the first dome panel from the dome upstream surface to the dome downstream surface, wherein the plurality of dome arms define the plurality of apertures; and
a deflector assembly including one or more deflector panels defining the deflector assembly, a first deflector panel of the one or more deflector panels including:
a deflector upstream surface and a deflector downstream surface opposite the deflector upstream surface; and
a plurality of deflector arms extending from the deflector upstream surface, each of the plurality of deflector arms mounted within a respective aperture of the first dome panel and extending upstream of the dome upstream surface, wherein the plurality of deflector arms is spaced around a first circumference that is defined about the opening of the first dome panel, has a first diameter, and is radially between the opening and an outer circumference of the first deflector panel, each of the plurality of deflector arms being positioned at the first diameter.
12. The turbine engine of claim 11 , wherein the plurality of deflector arms is a first plurality of deflector arms, the first deflector panel further including a second plurality of deflector arms spaced around a second circumference that is defined about the opening of the first dome panel, has a second diameter, and is radially between the opening and the outer circumference of the first deflector panel, each of the plurality of deflector arms being positioned at the second diameter.
13. The turbine engine of claim 12 , wherein the second diameter is greater than the first diameter.
14. The turbine engine of claim 11 , wherein the plurality of dome arms and the plurality of deflector arms are secured together by one or more fastening mechanisms disposed entirely upstream of dome upstream surface.
15. The turbine engine of claim 14 , wherein the one or more fastening mechanisms include at least one of brazing or welding.
16. The turbine engine of claim 14 , wherein the one or more fastening mechanisms include at least one of studs, bolts, screws, or rivets.
17. The turbine engine of claim 16 , wherein the at least one of the studs, the bolts, the screws, or the rivets are inserted radially through the plurality of dome arms and the plurality of deflector arms.
18. The turbine engine of claim 11 , wherein the first deflector panel includes a plurality of segments.
19. The turbine engine of claim 18 , wherein each of the plurality of segments includes one or more of the plurality of deflector arms.
20. The turbine engine of claim 18 , wherein the plurality of segments are separated by one or more gaps formed between each of the plurality of segments, wherein the one or more gaps are shaped to provide a flow of cooling air to the deflector downstream surface of the first deflector panel.