Claims
- 1. A rotating gas diffuser for shearing fine gas bubbles from the surface thereof when the diffuser is immersed in a body of liquid and rotated therein, which comprises:
- a hollow rotatable shaft, said shaft defining a main feed line for the gas to be introduced into said body of liquid,
- a disk like member mounted on said shaft perpendicular to the axis of rotation thereof, said member defining at least one gas plenum in operative connection with said main feed line, at least one wall of said plenum being porous to permit the passage of gas through said wall to the outer surface of said disk like member so that the introduction of gas into said main feed line when the gas diffuser is rotating about its axis of rotation while immersed in said body of liquid will cause gas to flow into said gas plenum and out through said porous wall thereof to produce nascent gas bubbles on the surface of said disk like member, which nascent bubbles are sheared off to form fine gas bubbles by the viscous shear forces exerted by said liquid as the disk member rotates in said body of liquid, and
- means for minimizing the coalescence of said fine sheared bubbles, resulting from turbulence in the wake and jet surrounding the rotary disk like member that is caused by vortices shed from the edge of the disk like member and spiraling outward from said edge, said means including said disk like member, wherein the ratio of the overall diameter of said disk like member to the maximum thickness thereof in the gas diffusing area occupied by said gas plenums is at least about 32:1.
- 2. The rotating gas diffuser of claim 1 in which the ratio of the overall diameter of said disk like member to the maximum thickness thereof in the gas diffusing area occupied by said gas plenums is at least about 48:1.
- 3. The rotating gas diffuser of claim 1 in which the ratio of the overall diameter of said disk like member to the maximum thickness thereto in the gas diffusing area occupied by said gas plenums is at least about 64:1.
- 4. The rotating gas diffuser of claim 1 in which the ratio of the overall diameter of said disk like member to the maximum thickness thereof in the gas diffusing area occupied by said gas plenums is at least about 128:1.
- 5. The rotating gas diffuser of claim 1 in which the ratio of the overall diameter of said disk like member to the maximum thickness thereof in the gas diffusing area occupied by said gas plenums is at least about 256:1.
- 6. The rotating gas diffuser of claim 1 in which both the top wall and the bottom wall of said gas plenum are porous and permit the passage of gas therethrough.
- 7. The rotating gas diffuser of claim 1 in which the top surface and bottom surface of said disk like member are substantially parallel to each other throughout their area.
- 8. The rotating gas diffuser of claim 1 in which the top surface and bottom surface of said disk like member are substantially parallel to each other except in the outer edge portion of said disk, where the disk tapers in cross section to a smaller thickness at the perimeter of said member.
- 9. The rotating member of a rotating gas diffuser for submersion into a body of liquid, which comprises:
- a rotatable disk like member having a gas inlet and defining at least one gas plenum in operative connection with said inlet and at least one wall of said plenum being porous to permit the passage of gas through said wall to the outer surface of said disk like member so that the introduction of gas into said gas inlet when the gas diffuser is rotating about its axis of rotation while immersed in said body of liquid will cause gas to flow into said gas plenum and out through said porous wall thereof to produce nascent gas bubbles on the surface of said disk like member, which nascent bubbles are sheared off to form fine gas bubbles by the viscous shear forces exerted by said liquid as the disk member rotates in said body of liquid, and
- means for minimizing the coalescence of said fine sheared bubbles, resulting from turbulence in the wake and jet surrounding the rotary disk like member that is caused by vortices shed from the edge of the disk like member and spiraling outward from said edge, said means including said disk like member, wherein the ratio of the overall diameter of said disk like member to the maximum thickness thereof in the gas diffusing area occupied by said gas plenums is at least about 32:1.
- 10. The rotatable disk like member of claim 9 in which the ratio of the overall diameter of said disk like member to the maximum thickness thereof in the gas diffusing area occupied by said gas plenums is at least about 48:1.
- 11. The rotatable disk like member of claim 9 in which the ratio of the overall diameter of said disk like member to the maximum thickness thereof in the gas diffusing area occupied by said gas plenums is at least about 64:1.
- 12. The rotatable disk like member of claim 9 in which the ratio of the overall diameter of said disk like member to the maximum thickness thereof in the gas diffusing area occupied by said gas plenums is at least about 128:1.
- 13. The rotatable disk like member of claim 9 in which the ratio of the overall diameter of said disk like member to the maximum thickness thereof in the gas diffusing area occupied by said gas plenums is at least about 256:1.
- 14. The rotatable disk like member of claim 9 in which both the top wall and the bottom wall of said gas plenum are porous and permit the passage of gas therethrough.
- 15. The rotatable disk like member of claim 9 in which the top surface and bottom surface of said disk like member are substantially parallel to each other throughout their area.
- 16. The rotatable disk like member of claim 9 in which the top surface and bottom surface of said disk like member are substantially parallel to each other except in the outer edge portion of said disk, where the disk tapers in cross section to substantially zero thickness at the perimeter thereof.
Parent Case Info
This is a continuation of application Ser. No. 801,569, filed May 31, 1977, which was a continuation of application Ser. No. 618,257, filed Sept. 30, 1975, both of which are now abandoned.
US Referenced Citations (4)
Non-Patent Literature Citations (2)
Entry |
AIAP Journal, vol. 9, No. 2, Feb. 1971, "Turbulent Boundary Layer on a Rotating Disk", by Paul Cooper, pp. 255-261. |
Elements of Physics, by Smith, 1948, McGraw-Hill, pp. 149-150. |
Continuations (2)
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Number |
Date |
Country |
Parent |
801569 |
May 1977 |
|
Parent |
618257 |
Sep 1975 |
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