Centrifugal separator having a vortex generator

US10710101B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-10710101-B2
Application numberUS-201314439513-A
CountryUS
Kind codeB2
Filing dateNov 19, 2013
Priority dateNov 23, 2012
Publication dateJul 14, 2020
Grant dateJul 14, 2020

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  1. Title

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  2. Abstract

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  3. Assignees and inventors

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  4. Key dates

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  5. First independent claim

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  6. CPC / IPC classifications

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  7. Citations and related patents

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Abstract

Official abstract text for this publication.

A centrifugal separator and a method for separation of particles from a gas stream is disclosed. The separator includes a frame, a gas inlet and a gas outlet. A centrifugal rotor is arranged to be rotatable in the frame around a rotational axis and includes a plurality of separation plates defining separation passages between the plates. A central gas chamber in the rotor communicates with a radially inner portion of the separation passages and the gas outlet. A space surrounding the rotor communicates with a radially outer portion of the separation passages and the gas inlet. A device is configured to bring the gas stream in rotation upstream of the rotor. The centrifugal rotor is configured such that the rotational flow of the gas mixture drives the rotation of the centrifugal rotor for separating particles from the same gas stream being conducted from the space surrounding the rotor, through the separation passages between the plates and towards the central gas chamber.

First claim

Opening claim text (preview).

The invention claimed is: 1. A centrifugal separator for separation of particles from a gas stream, comprising: a frame, a gas inlet and a gas outlet; a centrifugal rotor arranged to be rotatable in the frame around a rotational axis and comprising a plurality of separation plates stacked along an axial length of the rotor and defining separation passages between the plates; a central gas chamber in the rotor communicating with a radially inner portion of the separation passages and the gas outlet; a first space surrounding the rotor and communicating with a radially outer portion of the separation passages and the gas inlet; and a vortex generator axially spaced from the centrifugal rotor to create a second space in an axial space between the vortex generator and the separation plates to bring the gas stream in rotation upstream of the plurality of separation plates and downstream of the gas inlet, the first space and second space defining a flow path between the vortex generator and separation plates such that the gas stream flows from the vortex generator and then radially inward toward the separation plates, and the vortex generator comprising a passage having an entrance and an exit, the exit being downstream of the entrance, wherein a vortex created by the vortex generator enters the first space and drives the rotation of the centrifugal rotor for separating particles from the same gas stream by being conducted from the first space surrounding the rotor, through the separation passages between the plates and towards the central gas chamber, and wherein the vortex generator configured to bring the gas stream in rotation is non-rotating during operation of the apparatus. 2. The centrifugal separator according to claim 1 , wherein the vortex generator is configured to bring the gas stream in rotation by deflecting the gas stream towards a tangential direction of the centrifugal rotor. 3. The centrifugal separator according to claim 2 , wherein the vortex generator comprises a gas deflecting ring having at least one vane inclined with respect to the axial direction of the centrifugal rotor. 4. The centrifugal separator according to claim 3 , wherein the at least one vane extends radially outside the separation plates of the rotor. 5. The centrifugal separator according to claim 4 , wherein there are a plurality of vanes and the inclination of the vanes with respect to the axial direction of the centrifugal rotor increases gradually along the extent of the vanes in the direction of the flow of the gas stream from the gas inlet to the gas outlet. 6. The centrifugal separator according to claim 3 , wherein there are a plurality of vanes distributed around the rotational axis and the inclination of the vanes with respect to the axial direction of the centrifugal rotor increases gradually along the extent of the vanes in the direction of the flow of the gas stream from the gas inlet to the gas outlet. 7. The centrifugal separator according to claim 1 , wherein the gas inlet is arranged at an angle to the rotational axis of the centrifugal rotor, wherein the angle is within the range of 70-110 degrees, and wherein the vortex generator configured to bring the gas stream in rotation upstream of the rotor comprises an inlet gas deflecting member arranged to deflect the gas stream from the gas inlet towards a tangential direction of the centrifugal rotor. 8. The centrifugal separator according to claim 1 , wherein the rotor has a first and a second axial end portion, and wherein the rotor is rotatably supported in the frame by means of a first bearing at the first axial end portion and a second bearing at the second axial end portion. 9. The centrifugal separator according to claim 1 , wherein the gas inlet is arranged at an angle to the rotational axis of the centrifugal rotor, wherein the angle is within the range of 80-100 degrees, and wherein the vortex generator configured to bring the gas stream in rotation upstream of the rotor comprises an inlet gas deflecting member arranged to deflect the gas stream from the gas inlet towards a tangential direction of the centrifugal rotor. 10. The centrifugal separator according to claim 1 , wherein the gas inlet is arranged at an angle of 90 degrees to the rotational axis of the centrifugal rotor, and wherein the vortex generator configured to bring the gas stream in rotation upstream of the rotor comprises an inlet gas deflecting member arranged to deflect the gas stream from the gas inlet towards a tangential direction of the centrifugal rotor. 11. The centrifugal separator according to claim 1 , wherein the vortex generator extends across an entire width of the frame. 12. The centrifugal separator according to claim 1 , wherein the vortex generator comprises a ring shaped gas deflecting member and a plurality of inclined vanes extending outwardly from the ring shaped gas deflecting member a first end of each vane spaced from a second end of each vane in the axial and circumferential direction. 13. The centrifugal separator according to claim 1 , wherein the outlet extends along a longitudinal axis of the central gas chamber. 14. A centrifugal separator for separation of particles from a gas stream, comprising: a frame, a gas inlet and a gas outlet; a centrifugal rotor arranged to be rotatable in the frame around a rotational axis and comprising a plurality of separation plates defining separation passages between the plates; a central gas chamber in the rotor communicating with a radially inner portion of the separation passages and the gas outlet; a first space surrounding the rotor and communicating with a radially outer portion of the separation passages and the gas inlet; and a vortex generator axially spaced from the centrifugal rotor to create a second space in an axial space between the vortex generator and the separation plates, the vortex generator configured to bring the gas stream in rotation upstream of the rotor and downstream of the gas inlet, the first space and second space defining a flow path between the vortex generator and separation plates such that the gas stream flows from the vortex generator and then radially inward toward the separation plates, and the vortex generator comprising a passage having an entrance and an exit, the exit being downstream of the entrance, wherein a vortex created by the vortex generator enters the first space and drives the rotation of the centrifugal rotor for separating particles from the same gas stream by being conducted from the first space surrounding the rotor, through the separation passages between the plates and towards the central gas chamber, wherein the vortex generator configured to bring the gas stream in rotation is non-rotating during operation of the apparatus, wherein the frame is configured to be mountable inside a vessel for guiding the gas stream, and comprises a first partition for dividing the vessel into a first section upstream of the first partition and a second section downstream of the first partition, wherein the gas inlet is in communication with the first section, the gas outlet is in communication with the second section, and wherein the centrifugal separator is configured such that the first and second sections communicate via the separation passages of the rotor. 15. The centrifugal separator according to claim 14 , wherein a seal is provided between the first partition and the centrifugal rotor. 16. The centrifugal separator according to claim 14 , wherein the frame is a self-supporting frame for mounting inside an existing vessel for guiding the gas stream, and

Assignees

Inventors

Classifications

  • Inserts, e.g. armouring plates · CPC title

  • Centrifuges for separating predominantly gaseous mixtures · CPC title

  • B04B5/12Primary

    Centrifuges in which rotors other than bowls generate centrifugal effects in stationary containers · CPC title

  • B01D45/14Primary

    generated by rotating vanes, discs, drums or brushes · CPC title

  • with internal rotors, e.g. impeller, ventilator, fan, blower, pump · CPC title

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What does patent US10710101B2 cover?
A centrifugal separator and a method for separation of particles from a gas stream is disclosed. The separator includes a frame, a gas inlet and a gas outlet. A centrifugal rotor is arranged to be rotatable in the frame around a rotational axis and includes a plurality of separation plates defining separation passages between the plates. A central gas chamber in the rotor communicates with a ra…
Who is the assignee on this patent?
Alfa Laval Corp Ab
What technology area does this patent fall under?
Primary CPC classification B04B5/12. Mapped technology areas include Operations & Transport.
When was this patent published?
Publication date Tue Jul 14 2020 00:00:00 GMT+0000 (Coordinated Universal Time) (B2). Legal status and post-grant events are not shown on this page.
What related patents are in patentsdb?
We list 5 related publications on this page (citations in our corpus or others sharing the same primary CPC).