Gas turbine combustor fuel injector flow device including vanes
US-11280495-B2 · Mar 22, 2022 · US
US11885496B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-11885496-B2 |
| Application number | US-202117243246-A |
| Country | US |
| Kind code | B2 |
| Filing date | Apr 28, 2021 |
| Priority date | Apr 28, 2020 |
| Publication date | Jan 30, 2024 |
| Grant date | Jan 30, 2024 |
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A fluid nozzle includes a first fluid circuit, a second fluid circuit spaced apart from the first fluid circuit and a fuel circuit. The fuel circuit is defined between the first and second fluid circuits and between a first fuel circuit wall and a second fuel circuit wall. A ring-shaped permeable barrier is positioned between the first and second fuel circuit walls configured and adapted to provide a controlled resistance to fuel flow. A fuel distributor includes a first fuel circuit wall and a second fuel circuit wall spaced apart from the first fuel circuit wall. A fuel circuit is defined between the first and second fuel circuit walls. A ring-shaped permeable barrier is positioned between first and second fuel circuit walls. A combustion assembly includes a combustor housing, a combustor dome positioned at an upstream end of the combustor housing, and a fluid nozzle positioned adjacent the combustor dome.
Opening claim text (preview).
What is claimed is: 1. A fluid nozzle comprising: a first fluid circuit; a second fluid circuit spaced apart from the first fluid circuit; a fuel circuit defined between the first and second fluid circuits and between a first fuel circuit wall and a second fuel circuit wall; and a ring-shaped permeable barrier that forms a complete annulus between the first and second fuel circuit walls, wherein the ring-shaped permeable barrier is configured and adapted to provide a controlled resistance to fuel flow, and wherein the first and second fuel circuit walls each define at least a portion of the boundary of the fuel circuit upstream from the ring-shaped permeable barrier. 2. The fluid nozzle as recited in claim 1 , wherein the ring-shaped permeable barrier includes a sintered metal distributor body. 3. The fluid nozzle as recited in claim 1 , wherein the ring-shaped permeable barrier has an outer diameter inlet and an inner diameter outlet, wherein the inner diameter outlet includes a beveled surface. 4. The fluid nozzle as recited in claim 1 , wherein the ring-shaped permeable barrier is produced by additive manufacturing. 5. The fluid nozzle as recited in claim 1 , wherein at least one of the first or second fluid circuits is a swirling air circuit. 6. The fluid nozzle as recited in claim 1 , wherein at least one of the first or second fluid circuits is a non-swirling air circuit. 7. The fluid nozzle as recited in claim 1 , wherein the first fluid circuit is defined between a first annular swirler shell and second annular swirler shell. 8. The fluid nozzle as recited in claim 1 , further comprising a fuel inlet in fluid communication with the fuel circuit. 9. A fuel distributor comprising: a first fuel circuit wall; a second fuel circuit wall spaced apart from the first fuel circuit wall, wherein a fuel circuit is defined between the first and second fuel circuit walls; and a ring-shaped permeable barrier that forms a complete annulus between the first and second fuel circuit walls, wherein the ring-shaped permeable barrier is configured and adapted to provide a controlled resistance to fuel flow in the fuel circuit, and wherein the first and second fuel circuit walls each define at least a portion of the boundary of the fuel circuit upstream from the ring-shaped permeable barrier. 10. The fuel distributor as recited in claim 9 , wherein the ring-shaped permeable barrier includes a sintered metal distributor body. 11. The fuel distributor as recited in claim 9 , wherein the ring-shaped permeable barrier has an outer diameter inlet and an inner diameter outlet, wherein the inner diameter outlet includes a beveled surface. 12. The fuel distributor as recited in claim 9 , wherein the ring-shaped permeable barrier is produced by additive manufacturing. 13. The fuel distributor as recited in claim 9 , further comprising a fuel inlet in fluid communication with the fuel circuit. 14. A combustion assembly comprising: a combustor housing; a combustor dome positioned at an upstream end of the combustor housing; and a fluid nozzle positioned adjacent to the combustor dome, the fluid nozzle including: a first fluid circuit; a second fluid circuit spaced apart from the first fluid circuit; a fuel circuit defined between the first and second fluid circuits and between a first fuel circuit wall and a second fuel circuit wall; and a ring-shaped permeable barrier, that forms a complete annulus between the first and second fluid circuit walls, wherein the ring-shaped permeable barrier is configured and adapted to provide a controlled resistance to fluid flow, and wherein the first and second fuel circuit walls each define at least a portion of the boundary of the fuel circuit upstream from the ring-shaped permeable barrier. 15. The combustion assembly as recited in claim 14 , wherein the ring-shaped permeable barrier includes a sintered metal flow distributor body. 16. The combustion assembly as recited in claim 14 , wherein the ring-shaped permeable barrier has an outer diameter inlet and an inner diameter outlet, wherein the inner diameter outlet includes a beveled surface. 17. The combustion assembly as recited in claim 14 , wherein the ring-shaped permeable barrier is produced by additive manufacturing. 18. The combustion assembly as recited in claim 14 , wherein the first fluid circuit is a swirling air circuit. 19. The combustion assembly as recited in claim 14 , wherein the second fluid circuit is a non-swirling air circuit. 20. The combustion assembly as recited in claim 14 , wherein the first fluid circuit is defined between a first annular swirler shell and second annular swirler shell.
characterised by the fuel supply (burners F23D) · CPC title
Fuel supply systems · CPC title
the capillary action taking place in one or more rigid porous bodies · CPC title
Fuel vaporizer · CPC title
with swirl means · CPC title
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