Systems and methods for sustainable economic development through integrated full spectrum production of renewable energy
US-9231267-B2 · Jan 5, 2016 · US
US11193671B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-11193671-B2 |
| Application number | US-201816179040-A |
| Country | US |
| Kind code | B2 |
| Filing date | Nov 2, 2018 |
| Priority date | Nov 2, 2018 |
| Publication date | Dec 7, 2021 |
| Grant date | Dec 7, 2021 |
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A fuel oxygen conversion unit includes a contactor defining a liquid fuel inlet, a stripping gas inlet and a fuel/gas mixture outlet; and a fuel gas separator defining a fuel/gas mixture inlet in flow communication with the fuel/gas mixture outlet of the contactor and an axis. The fuel gas separator further includes a stationary casing; and a separator assembly including a core and a plurality of paddles extending from the core, the separator assembly rotatable about the axis within the stationary casing to separate a fuel/gas mixture received through the fuel/gas mixture inlet into a liquid fuel flow and stripping gas flow.
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What is claimed is: 1. A fuel oxygen conversion unit comprising: a contactor defining a liquid fuel inlet, a stripping gas inlet and a fuel/gas mixture outlet; and a fuel gas separator that extends between a first end and a second end thereof, and along an axis defined by the fuel gas separator, the fuel gas separator defining a radial direction, a first circumferential direction extending about the axis, and a fuel/gas mixture inlet in flow communication with the fuel/gas mixture outlet of the contactor, the fuel gas separator comprising: a stationary casing defining an inner surface that diverges away from the axis towards the second end; and a separator assembly including a core and a plurality of paddles extending from the core, each of the plurality of paddles defining a length that extends from a first location that is adjacent to the first end of the fuel gas separator and to a second location that is adjacent to the second end of the fuel gas separator, the separator assembly rotatable in the first circumferential direction about the axis within the stationary casing to separate a fuel/gas mixture received through the fuel/gas mixture inlet into a liquid fuel flow and a stripping gas flow, wherein each of the plurality of paddles define a sweep angle relative to the radial direction that is greater than or equal to 0 such that each of the plurality of paddles extend in the radial direction or slope away from the core and in a direction opposite the first circumferential direction, wherein the core of the separator assembly includes a gas permeable boundary, the gas permeable boundary defining a filter outer radius and a filter length along the axis, wherein the plurality of paddles extend from the filter outer radius. 2. The fuel oxygen conversion unit of claim 1 , wherein the core of the separator assembly is a gas permeable core extending along the axis of the fuel gas separator. 3. The fuel oxygen conversion unit of claim 1 , wherein the filter outer radius of the gas permeable boundary is substantially constant substantially along the filter length. 4. The fuel oxygen conversion unit of claim 1 , wherein the fuel/gas mixture inlet is positioned proximate the first end, wherein a liquid fuel outlet is positioned proximate the second end. 5. The fuel oxygen conversion unit of claim 1 , wherein the fuel gas separator further defines a liquid fuel outlet, wherein the fuel/gas mixture inlet of the fuel gas separator defines an inlet radius along the radial direction relative to the axis, wherein the liquid fuel outlet of the fuel gas separator defines an outlet radius along the radial direction relative to the axis, and wherein the outlet radius is greater than the inlet radius. 6. The fuel oxygen conversion unit of claim 1 , wherein the plurality of paddles of the separator assembly extend outwardly from the core and are spaced along the first circumferential direction. 7. The fuel oxygen conversion unit of claim 1 , wherein the plurality of paddles each define a length along the axis and a clearance with the stationary casing, and wherein the clearance of each of the plurality of paddles is substantially constant along their entire respective lengths. 8. The fuel oxygen conversion unit of claim 1 , wherein the sweep angle is greater than 0. 9. The fuel oxygen conversion unit of claim 8 , wherein the sweep angle is greater than 10 degrees and less than 45 degrees. 10. The fuel oxygen conversion unit of claim 8 , wherein the sweep angle is greater than 15 degrees and less than 30 degrees. 11. The fuel oxygen conversion unit of claim 1 , wherein the fuel gas separator defines a stripping gas outlet, wherein the fuel/gas mixture inlet is positioned proximate the first end, and wherein the stripping gas outlet is also positioned proximate the first end such that the stripping gas flow enters and exits the fuel gas separator at the first end. 12. The fuel oxygen conversion unit of claim 1 , wherein the inner surface of the stationary casing is a first section of the inner surface of the stationary casing positioned proximate the first end of the fuel gas separator, wherein the stationary casing further defines a second section of the inner surface of the stationary casing positioned proximate the second end of the fuel gas separator, and wherein the second section of the inner surface of the stationary casing diverges away from the axis towards the second end. 13. The fuel oxygen conversion unit of claim 12 , wherein each of the plurality of paddles are configured as continuous, single piece paddles extending from a location within the first section of the inner surface of the stationary casing along an axial direction to a location within the second section of the inner surface of the stationary casing. 14. The fuel oxygen conversion unit of claim 1 , further comprising: a gas oxygen reduction unit, wherein the fuel oxygen conversion unit defines a circulation gas path extending from a stripping gas outlet of the fuel gas separator to the stripping gas inlet of the contactor, and wherein the gas oxygen reduction unit is positioned in flow communication with the circulation gas path. 15. The fuel oxygen conversion unit of claim 14 , further comprising: a gas boost pump positioned in flow communication with the circulation gas path. 16. A gas turbine engine comprising: a combustion section; and a fuel delivery system for providing a flow of fuel to the combustion section, the fuel delivery system comprising a fuel oxygen conversion unit, the fuel oxygen conversion unit comprising: a contactor defining a liquid fuel inlet, a stripping gas inlet and a fuel/gas mixture outlet; and a fuel gas separator that extends between a first end and a second end thereof, and along an axis defined by the fuel gas separator, the fuel gas separator defining a radial direction, a first circumferential direction extending about the axis, and a fuel/gas mixture inlet in flow communication with the fuel/gas mixture outlet of the contactor, the fuel gas separator comprising: a stationary casing; and a separator assembly including a core and a plurality of paddles extending from the core, each of the plurality of paddles defining a length that extends from a first location that is adjacent to the first end of the fuel gas separator and to a second location that is adjacent to the second end of the fuel gas separator, the separator assembly rotatable in the first circumferential direction about the axis within the stationary casing to separate a fuel/gas mixture received through the fuel/gas mixture inlet into a liquid fuel flow and a stripping gas flow, wherein each of the plurality of paddles define a sweep angle relative to the radial direction that is greater than or equal to 0 such that each of the plurality of paddles extend in the radial direction or slope away from the core and in a direction opposite the first circumferential direction, wherein the core of the separator assembly includes a gas permeable boundary, the gas permeable boundary defining a filter outer radius and a filter length along the axis, wherein the plurality of paddles extend from the filter outer radius. 17. The gas turbine engine of claim 16 , wherein the fuel/gas mixture inlet is positioned proximate the first end, wherein a liquid fuel outlet is positioned proximate the second end. 18. The fuel oxygen conversion unit of claim 1 , wherein the inner surface of the stationary casing that diverges away from the axis towards the second end defines a radius and has a substantially frustoc
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