Swirler mount interface for gas turbine engine combustor
US-10598381-B2 · Mar 24, 2020 · US
US12092324B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-12092324-B2 |
| Application number | US-202217655196-A |
| Country | US |
| Kind code | B2 |
| Filing date | Mar 17, 2022 |
| Priority date | Mar 17, 2022 |
| Publication date | Sep 17, 2024 |
| Grant date | Sep 17, 2024 |
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A flare cone for a mixer assembly includes an annular conical wall extending circumferentially about a mixer assembly centerline, the annular conical wall including a conical inner surface defining a conical opening of the annular conical wall, and an annular axial wall extending in a longitudinal direction with respect to the mixer assembly centerline, the annular axial wall disposed at a radially outward portion of the annular conical wall and connected to the annular conical wall. The annular conical wall and the annular axial wall define an annular step circumferentially about the mixer assembly centerline and extending upstream in the longitudinal direction between a downstream end of the annular conical wall and an aft surface of the annular axial wall.
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We claim: 1. A mixer assembly of a combustor, the mixer assembly defining a centerline axis therethrough, the mixer assembly comprising: a swirler assembly including a primary swirler and a secondary swirler disposed downstream of the primary swirler; and a flare cone disposed at a downstream end of the secondary swirler, the flare cone comprising: (a) an annular conical wall extending circumferentially about the centerline axis, the annular conical wall including a conical inner surface defining a conical opening of the annular conical wall, and (b) an annular axial wall extending in a longitudinal direction with respect to the centerline axis, the annular axial wall disposed at a radially outward portion of the annular conical wall and connected to the annular conical wall, wherein the annular conical wall and the annular axial wall define an annular step circumferentially about the centerline axis and extending upstream in the longitudinal direction between a downstream end of the annular conical wall and an aft surface of the annular axial wall, wherein the flare cone further comprises an annular inner axial wall extending upstream in the longitudinal direction from an upstream end of the annular conical wall, wherein an annular cavity is defined between the annular axial wall and the annular inner axial wall, and wherein the flare cone includes a plurality of slotted cooling passages each having an inlet at the annular cavity and an outlet at a surface of the annular step. 2. The mixer assembly according to claim 1 , wherein the downstream end of the annular conical wall comprises an annular conical wall aft surface extending radially outward from a downstream end of the conical inner surface of the annular conical wall to the annular step. 3. The mixer assembly according to claim 1 , wherein the conical inner surface of the annular conical wall comprises a continuously curved conical inner surface extending from an upstream end of the continuously curved conical inner surface to a downstream end of the continuously curved conical inner surface. 4. The mixer assembly according to claim 3 , wherein (a) a beginning portion of the continuously curved conical inner surface at the upstream end of the continuously curved conical inner surface is arranged at a first conical wall angle with respect to the centerline axis, (b) an ending portion of the continuously curved conical inner surface at the downstream end of the continuously curved conical inner surface is arranged at a second conical wall angle with respect to the centerline axis, and (c) a middle portion of the continuously curved conical inner surface between the beginning portion and the ending portion transitions from the first conical wall angle to the second conical wall angle. 5. The mixer assembly according to claim 4 , wherein the first conical wall angle is forty-five degrees and the second conical wall angle is sixty degrees. 6. The mixer assembly according to claim 1 , wherein the surface of the annular step and the conical inner surface of the annular conical wall intersect at the downstream end of the annular conical wall and form an acute angle therebetween. 7. The mixer assembly according to claim 6 , wherein the conical inner surface of the annular conical wall comprises a continuously curved conical inner surface extending from an upstream end of the continuously curved conical inner surface to a downstream end of the continuously curved conical inner surface. 8. The mixer assembly according to claim 7 , wherein (a) a beginning portion of the continuously curved conical inner surface at the upstream end of the continuously curved conical inner surface is arranged at a first conical wall angle with respect to the centerline axis, (b) an ending portion of the continuously curved conical inner surface at the downstream end of the continuously curved conical inner surface is arranged at a second conical wall angle with respect to the centerline axis, and (c) a middle portion of the continuously curved conical inner surface between the beginning portion and the ending portion transitions from the first conical wall angle to the second conical wall angle. 9. The mixer assembly according to claim 8 , wherein the first conical wall angle is forty-five degrees and the second conical wall angle is sixty degrees. 10. The mixer assembly according to claim 1 , further comprising a deflector wall connected to the annular axial wall at a downstream end of the annular axial wall, and extending radially outward from an outer surface of the annular axial wall, wherein the deflector wall is formed integral with the flare cone. 11. The mixer assembly according to claim 10 , wherein the deflector wall includes a plurality of cooling passages therethrough. 12. A mixer assembly of a combustor, the mixer assembly defining a centerline axis therethrough, the mixer assembly comprising: a swirler assembly including a primary swirler and a secondary swirler disposed downstream of the primary swirler; and a flare cone disposed at a downstream end of the secondary swirler, the flare cone comprising: (a) an annular conical wall extending circumferentially about the centerline axis, the annular conical wall including a conical inner surface defining a conical opening of the annular conical wall, and (b) an annular axial wall extending in a longitudinal direction with respect to the centerline axis, the annular axial wall disposed at a radially outward portion of the annular conical wall and connected to the annular conical wall, wherein the annular conical wall and the annular axial wall define an annular step circumferentially about the centerline axis and extending upstream in the longitudinal direction between a downstream end of the annular conical wall and an aft surface of the annular axial wall, wherein the annular conical wall further comprises a backside cooling passage, wherein a flare cone flange is defined between the backside cooling passage and the conical inner surface of the annular conical wall, wherein the conical inner surface of the annular conical wall comprises a continuously curved conical inner surface extending from an upstream end of the continuously curved conical inner surface to a downstream end of the continuously curved conical inner surface, and wherein (a) a beginning portion of the continuously curved conical inner surface at the upstream end of the continuously curved conical inner surface is arranged at a first conical wall angle with respect to the centerline axis, (b) an ending portion of the continuously curved conical inner surface at the downstream end of the continuously curved conical inner surface is arranged at a second conical wall angle with respect to the centerline axis, and (c) a middle portion of the continuously curved conical inner surface between the beginning portion and the ending portion transitions from the first conical wall angle to the second conical wall angle. 13. The mixer assembly according to claim 12 , wherein the first conical wall angle is forty-five degrees and the second conical wall angle is sixty degrees. 14. The mixer assembly according to claim 12 , wherein the backside cooling passage includes a backside cooling passage aft surface that is a continuously curved surface that is congruent with the continuously curved conical inner surface. 15. A flare cone for a mixer assembly, the flare cone defining a centerline axis therethrough, the flare cone comprising: an annular conical wall extending circumferentially about the centerline axis, the annular conical wall including a conical inner surface definin
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