Throttle body with a plurality of channels extending three-dimensional spiral-shaped
US-2018283580-A1 · Oct 4, 2018 · US
US10711937B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-10711937-B2 |
| Application number | US-201815887659-A |
| Country | US |
| Kind code | B2 |
| Filing date | Feb 2, 2018 |
| Priority date | May 25, 2017 |
| Publication date | Jul 14, 2020 |
| Grant date | Jul 14, 2020 |
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A method of custom manufacturing a fluid pressure reduction device for use in a process control valve. The method includes creating the fluid pressure reduction device using an additive manufacturing technique, which generally includes forming a body and forming a plurality of flow paths in the body. The body has an inner wall and an outer wall spaced radially outward of the inner wall. The flow paths are formed in the body between the inner wall and the outer wall of the body. Each of the flow paths includes an inlet section formed in one of the inner and outer walls, a curved intermediate section, and an outlet section formed in the other of the inner and outer walls.
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The invention claimed is: 1. A fluid pressure reduction device for use in a fluid flow control device, the fluid pressure reduction device comprising: a unitary body having an inner wall and an outer wall spaced radially outward of the inner wall; a plurality of first flow paths defined between the inner wall and the outer wall of the body, each of the first flow paths comprising an inlet section, an outlet section, and a curved intermediate section between the inlet and outlet sections, wherein the inlet section of each of the first flow paths is oriented along a respective first inlet axis, and wherein the first inlet axes are arranged along a first plane; and a plurality of second flow paths defined between the inner wall and the outer wall of the body, each of the second flow paths comprising an inlet section, an outlet section, and a curved intermediate section between the inlet and outlet sections, wherein the inlet section of each of the second flow paths is oriented along a respective second inlet axis, and wherein the second inlet axes are arranged along a second plane that is parallel to but spaced from the first plane, wherein the curved intermediate section of each of the first and second flow paths comprises a pair of loops, and wherein each of the loops has a first portion that extends outward and upward from the respective inlet section, and a second portion that is connected to the first portion and extends inward and upward into the respective outlet section. 2. The fluid pressure reduction device of claim 1 , wherein the inlet sections of the first flow paths and the inlet sections of the second flow paths are formed in the inner wall, and wherein the outlet sections of the first flow paths and the outlet sections of the second flow paths are formed in the outer wall. 3. The fluid pressure reduction device of claim 1 , wherein the unitary body comprises a central opening and a perimeter surrounding the central opening, the central opening defining a central longitudinal axis of the unitary body, and wherein the first and second planes are perpendicular to the central longitudinal axis. 4. The fluid pressure reduction device of claim 3 , wherein the plurality of second flow paths are rotated about the central longitudinal axis relative to the plurality of first flow paths, such that the plurality of second flow paths are offset from the plurality of first flow paths. 5. The fluid pressure reduction device of claim 1 , wherein for each of the first and second flow paths, the inlet section has a cross-sectional area that is smaller than a cross-sectional area of a respective outlet section associated with the inlet section. 6. The fluid pressure reduction device of claim 1 , wherein the outlet section of each of the first flow paths is oriented along a respective first outlet axis that is parallel to but spaced from the respective first inlet axis of a respective inlet section. 7. The fluid pressure reduction device of claim 1 , wherein the curved intermediate section of each of the first and second flow paths consists of the pair of loops. 8. A fluid pressure reduction device for use in a fluid flow control device, the fluid pressure reduction device comprising: a unitary body comprising a central opening and a perimeter surrounding the central opening, the central opening defining a central longitudinal axis, and the perimeter having an inner wall and an outer wall spaced radially outward of the inner wall; a plurality of first flow paths defined between the inner wall and the outer wall of the body, each of the first flow paths comprising an inlet section, an outlet section, and a curved intermediate section between the inlet and outlet sections, wherein the inlet section of each of the first flow paths is oriented along a respective first inlet axis, and wherein the first inlet axes are arranged along a first plane that is perpendicular to the central longitudinal axis; and a plurality of second flow paths defined between the inner wall and the outer wall of the body, each of the second flow paths comprising an inlet section, an outlet section, and a curved intermediate section between the inlet and outlet sections, wherein the inlet section of each of the second flow paths is oriented along a respective second inlet axis, and wherein the second inlet axes are arranged along a second plane that is parallel to but spaced from the first plane, wherein the curved intermediate section of each of the first and second flow paths comprises a pair of loops, and wherein each of the loops has a first portion that extends outward and upward from the respective inlet section, and a second portion that is connected to the first portion and extends inward and upward into the respective outlet section. 9. The fluid pressure reduction device of claim 8 , wherein the plurality of second flow paths are rotated about the central longitudinal axis relative to the plurality of first flow paths, such that the plurality of second flow paths are offset from the plurality of first flow paths. 10. The fluid pressure reduction device of claim 8 , wherein for each of the first and second flow paths, the inlet section has a cross-sectional area that is smaller than a cross-sectional area of a respective outlet section associated with the inlet section. 11. The fluid pressure reduction device of claim 8 , wherein the outlet section of each of the first flow paths is oriented along a respective first outlet axis that is parallel to but spaced from the respective first inlet axis of a respective inlet section. 12. The fluid pressure reduction device of claim 8 , wherein the curved intermediate section of each of the first and second flow paths consists of the pair of loops. 13. A method of manufacturing, comprising: creating a fluid pressure reduction device using an additive manufacturing technique, the creating comprising: forming a body having an inner wall and an outer wall spaced radially outward of the inner wall; and forming a plurality of flow paths in the body between the inner wall and the outer wall of the body, each of the flow paths comprising an inlet section formed in the inner wall, an outlet section formed in the outer wall, and a curved intermediate section between the inlet and outlet sections, wherein the curved intermediate section of each of the flow paths comprises a pair of loops, and wherein each of the loops has a first portion that extends outward and upward from the respective inlet section, and a second portion that is connected to the first portion and extends inward and upward into the respective outlet section. 14. The method of claim 13 , wherein the additive manufacturing technique comprises 3D printing. 15. The method of claim 13 , wherein the plurality of flow paths comprise a plurality of first flow paths and a plurality of second flow paths, wherein the inlet section of each of the first flow paths is oriented along a respective first inlet axis, and wherein the inlet section of each of the second flow paths is oriented along a respective second inlet axis. 16. The method of claim 15 , wherein the first inlet axes are arranged along a first plane, and wherein the second inlet axes are arranged along a second plane that is parallel to but spaced from the first plane. 17. The method of claim 16 , wherein the body comprises a unitary body, wherein the unitary body comprises a central opening and a perimeter surrounding the central opening, the central opening defining a central longitudinal axis of the unitary body, and where in the first and second planes a
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