Rotary degassers and components therefor
US-2017176106-A1 · Jun 22, 2017 · US
US10465987B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-10465987-B2 |
| Application number | US-201415024894-A |
| Country | US |
| Kind code | B2 |
| Filing date | Sep 26, 2014 |
| Priority date | Sep 27, 2013 |
| Publication date | Nov 5, 2019 |
| Grant date | Nov 5, 2019 |
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The dual-function impeller can be rotated in molten metal in a direction of rotation, as part of a rotary injector. The impeller can have a body having an axis, a plurality of blades circumferentially interspaced around an axis, and an aperture coinciding with the axis. The blades having both a radially extending portion facing the direction of rotation and collectively generating a radial flow component upon said rotation, and a slanted portion also facing the direction of rotation, inclined relative to a radial plane, and collectively generating an axial flow component directed away from the rotary injector upon said rotation.
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What is claimed is: 1. A dual-function impeller for rotation in molten metal in a direction of rotation, as part of a rotary injector, the impeller comprising: a body having an axis and a central injection path along the axis, a set of radial blade portions circumferentially interspaced from one another around the axis, located adjacent to the injection path, each having a radial blade leading face facing the direction of rotation, the radial blade leading faces collectively configured for generating a radial flow component upon said rotation, a plurality of channels, each channel extending between a corresponding pair of adjacent radial blade portions; a set of radial surfaces circumferentially interspaced from one another around the axis, each one of the radial surfaces forming an axial limit to a corresponding one of the channels; and a set of axial blade portions circumferentially interspaced from one another around the axis, radially-outwardly from the set of radial blade portions, each having a leading face facing the direction of rotation, the axial blade leading faces being inclined relative to a radial plane and collectively configured for generating an axial flow component directed axially away from the rotary injector upon said rotation, the axial blade leading faces extending continuously from corresponding ones of the radial blade leading faces. 2. The dual function impeller of claim 1 wherein each of the radial blade portions is adjacent a corresponding one of the axial blade portions and is configured for leading the molten metal directly to the corresponding axial blade portion upon said rotation. 3. The dual function impeller of claim 1 wherein the radial blade portions have a radial length which corresponds to between 30 and 70% of a combined radial length of the radial blade portion and axial blade portion. 4. The dual function impeller of claim 1 wherein an angle of inclination of the axial blade leading faces relative to the corresponding radial planes is between 30 and 60°. 5. The dual function impeller of claim 1 wherein the set of radial surfaces forms part of a disc-shaped portion. 6. The dual function impeller of claim 5 wherein the disc-shaped portion has a proximal surface located opposite the radial blade portions and facing a shaft of the rotary injector, the proximal surface being free of blade portions and surrounding a connector hub of the body. 7. The dual function impeller of claim 5 wherein the disc-shaped portion has a distal annular surface extending radially between the central injection path and a radially-inner end of the radial blade portions, the distal annular surface bearing the set of radial surfaces. 8. The dual function impeller of claim 5 wherein at least a portion of the axial blade portions protrudes radially from the disc-shaped portion. 9. The dual function impeller of claim 8 wherein the at least a portion of the axial blade portions which protrudes radially from the disc-shaped portion protrude therefrom in a direction opposite from a shaft of the rotary injector which leads to the impeller and coinciding with an outlet direction of the central injection path. 10. A dual-function impeller for rotation in molten metal in a direction of rotation, as part of a rotary injector, the impeller comprising: a body having an axis and a central injection path along the axis, a set of radial blade portions circumferentially interspaced from one another around the axis, located adjacent to the injection path, each having a radial blade leading face facing the direction of rotation, the radial blade leading faces collectively configured for generating a radial flow component upon said rotation, a plurality of channels, each channel extending between a corresponding pair of adjacent radial blade portions; a set of radial surfaces circumferentially interspaced from one another around the axis, each one of the radial surfaces forming an axial limit to a corresponding one of the channels; and a set of axial blade portions circumferentially interspaced from one another around the axis, radially-outwardly from the set of radial blade portions, each having a leading face facing the direction of rotation, the axial blade leading faces being inclined relative to a radial plane and collectively configured for generating an axial flow component directed axially away from the rotary injector upon said rotation; wherein the set of radial surfaces forms part of a disc-shaped portion; and wherein the disc-shaped portion has a proximal surface located opposite the radial blade portions and facing a shaft of the rotary injector, the proximal surface being free of blade portions and surrounding a connector hub of the body. 11. The dual function impeller of claim 10 wherein each of the radial blade portions is adjacent a corresponding one of the axial blade portions and is configured for leading the molten metal directly to the corresponding axial blade portion upon said rotation. 12. The dual function impeller of claim 10 wherein the radial blade portions have a radial length which corresponds to between 30 and 70% of a combined radial length of the radial blade portion and axial blade portion. 13. The dual function impeller of claim 10 wherein an angle of inclination of the axial blade leading faces relative to the corresponding radial planes is between 30 and 60°. 14. A dual-function impeller for rotation in molten metal in a direction of rotation, as part of a rotary injector, the impeller comprising: a body having an axis and a central injection path along the axis, a set of radial blade portions circumferentially interspaced from one another around the axis, located adjacent to the injection path, each having a radial blade leading face facing the direction of rotation, the radial blade leading faces collectively configured for generating a radial flow component upon said rotation, a plurality of channels, each channel extending between a corresponding pair of adjacent radial blade portions; a set of radial surfaces circumferentially interspaced from one another around the axis, each one of the radial surfaces forming an axial limit to a corresponding one of the channels; and a set of axial blade portions circumferentially interspaced from one another around the axis, radially-outwardly from the set of radial blade portions, each having a leading face facing the direction of rotation, the axial blade leading faces being inclined relative to a radial plane and collectively configured for generating an axial flow component directed axially away from the rotary injector upon said rotation; wherein the set of radial surfaces forms part of a disc-shaped portion; and wherein at least a portion of the axial blade portions protrudes radially from the disc-shaped portion. 15. The dual function impeller of claim 14 wherein each of the radial blade portions is adjacent a corresponding one of the axial blade portions and is configured for leading the molten metal directly to the corresponding axial blade portion upon said rotation. 16. The dual function impeller of claim 14 wherein the radial blade portions have a radial length which corresponds to between 30 and 70% of a combined radial length of the radial blade portion and axial blade portion. 17. The dual function impeller of claim 14 wherein an angle of inclination of the axial blade leading faces relative to the corresponding radial planes is between 30 and 60°.
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