Centrifugal separator having frame secured within a vessel

Abstract

A centrifugal separator for separation of particles from a gas stream is disclosed. The centrifugal separator includes a self-supporting frame for mounting inside an existing vessel for guiding the gas stream. The frame comprises a holder configured to hold the frame at a position inside the vessel, and a first partition for dividing the vessel into a first section and a second section. The first section is upstream of the second section. The separator includes a gas inlet communicating with the first section, and a gas outlet communicating with the second section. A centrifugal rotor is arranged to be rotatably supported in the frame around a rotational axis, the rotor having a first and a second end portion and including a plurality of separation plates defining separation passages between the plates. The centrifugal separator is configured such that the first and second sections communicate via the separation passages of the rotor.

Claims

1. A centrifugal separator for separation of particles from a gas stream, comprising: a self-supporting frame for mounting inside an existing vessel for guiding the gas stream, the frame comprising a holder configured to hold the frame at a position inside the vessel, the holder being secured to the vessel and connected to the frame to maintain the frame stationary with respect to the vessel and a first partition extending across an entire width of the frame to divide the vessel into a first section and a second section, wherein the first section is upstream of the second section; a gas inlet communicating with the first section; a gas outlet communicating with the second section; and a centrifugal rotor arranged to be rotatably supported in the frame around a rotational axis, the rotor having a first and a second end portion and comprising a plurality of separation plates defining separation passages between the plates, wherein the centrifugal separator is configured such that the first and second sections communicate via the separation passages of the rotor.

2. The centrifugal separator according to claim 1, wherein the frame comprises a first frame portion, rotatably supporting the first end portion of the rotor in a first bearing, and a second frame portion, rotatably supporting the second end portion of the rotor in a second bearing.

3. The centrifugal separator according to claim 2, wherein the first frame portion comprises the first partition.

4. The centrifugal separator according to claim 1, wherein the frame comprises a cylindrical tubular element connecting the first and the second frame portions, and wherein the centrifugal rotor is arranged inside the tubular element.

5. The centrifugal separator according to claim 1, wherein the frame is configured to be releasably mountable in the vessel.

6. The centrifugal separator according to claim 5, wherein the frame is configured to be releasably connectable to a cylindrical inner surface of the vessel by means of the holder.

7. The centrifugal separator according to claim 1, further comprising a portion of the vessel for guiding the gas stream, wherein the portion of the vessel has an inner surface and wherein the frame is configured to be releasably connectable to the inner surface of the vessel by means of the holder.

8. The centrifugal separator according to claim 6, wherein the holder is configured to engage with the cylindrical inner surface of the vessel by expanding in the radial direction when compressed in the axial direction.

9. The centrifugal separator according to claim 5, wherein the holder comprises one or more radially slotted frustoconical discs.

10. The centrifugal separator according to claim 1, wherein the vessel comprises a flange, and wherein the frame is configured to cooperate with the flange of the vessel, such that it is releasably connected to the flange of the vessel.

11. The centrifugal separator according to claim 1, wherein the holder is arranged in the region of the first partition.

12. A method comprising the step of mounting the centrifugal separator according to claim 1 in the existing vessel for guiding a gas stream.

13. The method according to claim 12, wherein the existing vessel is a pressure vessel for guiding a pipeline stream.

14. The centrifugal separator according to claim 2, wherein the frame comprises a cylindrical tubular element connecting the first and the second frame portions, and wherein the centrifugal rotor is arranged inside the tubular element.

15. The centrifugal separator according to claim 3, wherein the frame comprises a cylindrical tubular element connecting the first and the second frame portions, and wherein the centrifugal rotor is arranged inside the tubular element.

16. The centrifugal separator according to claim 4 wherein the frame is configured to be releasably mountable in the vessel.

17. The centrifugal separator according to claim 2 further comprising a portion of the vessel for guiding the gas stream, wherein the portion of the vessel has a cylindrical inner surface and wherein the frame is configured to be releasably connectable to a cylindrical inner surface of the vessel by means of the holder.

18. A centrifugal separator for separation of particles from a gas stream, comprising: a vessel; a self-supporting frame for mounting inside the vessel for guiding the gas stream, the frame comprising a first partition for dividing the vessel into a first section and a second section, the first section being upstream of the second section; a gas inlet communicating with the first section; a gas outlet communicating with the second section; a centrifugal rotor arranged to be rotatably supported in the frame around a rotational axis, the rotor having a first and a second end portion and comprising a plurality of separation plates defining separation passages between the plates; and a holder for securing the frame within the vessel, the holder comprising a ring spaced axially from the first partition, a frustoconical element extending between the ring and the first partition and a plurality of fasteners extending between the ring and the first partition, wherein a compression force between the ring and first partition created by the plurality of fasteners causes the frustoconical element to expand in a radial direction.

19. The centrifugal separator according to claim 18, wherein the frustoconical element is a radially slotted disc.

20. The centrifugal separator according to claim 18, wherein the frustoconical element contacts an inner surface of the ring and an outer surface of the first partition.

Description

BRIEF DESCRIPTION OF DRAWINGS

(1) The invention is now described, by way of example, with reference to the accompanying drawings, in which:

(2) FIG. 1 shows a cross-section along the rotational axis of a centrifugal separator according to the invention, arranged in a cylindrical vessel for conveying a gas stream.

(3) FIG. 2 shows a partially cut-out perspective view of a rotor of such a centrifugal separator.

(4) FIG. 3 shows an axial cross-section of a holding means with frustoconical slotted disc.

(5) FIG. 4 shows a perspective view of a vortex generator configured to bring the gas stream in rotation.

(6) FIG. 5 shows a cross-section perpendicular to the rotational axis of a vortex generator configured to bring the gas stream in rotation according to another embodiment.

DESCRIPTION OF EMBODIMENTS

(7) In FIG. 1 a centrifugal separator 1 for separation of particles from a gas stream is shown arranged in a cylindrical vessel 19 in the form of a cylindrical pipe for guiding the gas stream. The separator comprises a self-supporting frame 2 for mounting inside the vessel 19. Self-supporting is understood as an ability of the frame to support itself without relying on support from the vessel such as during mounting and dismounting. The frame is provided with a first partition 15 for dividing the vessel into a first section and a second section, wherein the first section is upstream of the second section. The first partition 15 extends across an entire width of the frame 2 as seen in FIG. 1 to divide the vessel into the first and second sections. The separator further comprises a gas inlet 3 communicating with the first section and a gas outlet 4 communicating with the second section.

(8) The centrifugal separator further comprises a centrifugal rotor 5 arranged to be rotatable in the frame around a rotational axis x. The rotational axis extends in the direction of the extension of the vessel. The rotor comprises a shaft 26 having a first and a second end portion. The first end portion is supported in a first frame portion 15a by means of a first bearing 13. The first frame portion 15a comprises the first partition 15. The second end portion is supported in the frame by means of a second bearing 14 held in a second frame portion 21. With reference to FIG. 2, the rotor is described in more detail. The rotor comprises a disc support structure 27 connected to the rotor axis and extending between the first and second end portions of the rotor axis. The disc support structure has three plate like wings extending along the rotor axis and radially outwards from the rotor axis. In an alternative embodiment the disc support structure comprises two or more wings, such as six wings. Towards the second end portion of the rotor axis, a bottom disc 28 is attached to the wings of the disc support structure. On the bottom disc, and guided by the radially outer portions of the plate like wings, a plurality of frustoconical separation discs 6 are stacked. The separation discs may be made of a lightweight material such as plastic, or of metal such as stainless steel. The separation discs are each provided with distance members in order to provide separation passages 7 between the discs in the stack. The distance members are in the form of elongated protrusions extending from a radially inner portion to a radially outer portion of each separation disc, having an extension along a line or a curve. The elongated distance members, or caulks, may be straight or curved and may be integrated in the discs or attached to the discs. The distance members may alternatively or additionally comprise distance members in the form of dot-shaped caulks or microcaulks, distributed over the surface of the separation discs. On top of the stack of separation discs a top disc 29 is provided. The top disc is attached to the wings of the disc support structure. The stack of separation discs are compressed by the top disc and the bottom disc. Radially inside the separation discs a central gas space 8 is formed, divided into three parts by the wings of the disc support structure 27. The top disc is provided with a central opening 30 such that the central gas space of the rotor is open for passage of gas through the top disc. The top disc is provided with a flange 31 circumventing the central opening providing a cylindrical outer sealing surface, 18a.

(9) Again turning to FIG. 1, a narrow gap is formed between a sealing surface 18a formed on the flange 31 of the top disc and a corresponding cylindrical sealing surface 18b on the first partition. The gap forms a gap sealing 18 between the first 16 and second 17 sections in the vessel. The central gas chamber 8 in the rotor communicates with a radially inner portion of the separation passages 7 and the gas outlet 4 via the central opening of the top disc and openings 32 formed in the first partition, surrounding the first bearing 13. Further, a space 9 is formed radially outside and surrounding the rotor. The space 9 surrounding the rotor communicates with the radially outer portion of the separation passages 7 and the gas inlet 3. The centrifugal separator is configured such that the first and second sections of the vessel communicate via the separation passages 7 of the rotor.

(10) The frame comprises a bottom sealing ring 33 forming the gas inlet 3 in the frame. The bottom sealing ring is sealingly connected, 38, to the inner vessel wall 25. A cylindrical frame tube 24 extends along the inner wall of the vessel as a part of the frame, from the bottom sealing ring to the first partition 15 and connects with the other parts of the frame to provide a self-supporting frame structure. The second frame portion 21 supporting the second bearing 14 is connected to and supported by the inner wall of the cylindrical frame tube. The space between the gas inlet 3 and device 10, discussed below, creates a chamber 22.

(11) The frame 2 further comprises a holding means 20 to hold the frame at a position inside the vessel. The holding means comprises in a ring shaped part 34 sealingly connected, by means of a sealing member 37, to the inner vessel wall 25. The holding means is configured to engage with the cylindrical inner surface of the vessel by providing an expandable outer diameter. With reference to FIG. 3, the holding means is described in more detail. The ring shaped part 34 is connected to the first partition 15 by a plurality of bolts 35 distributed around the circumference of the ring shaped part 34. The holding means comprises one or more radially slotted frustoconical discs 36 mounted such that compression of the disc by tightening the bolts of the ring shaped part causes slotted radially outer portions 36a of the disc to expand and engage with the cylindrical inner surface of the vessel. Thus the expandable outer diameter is realized by a by tightening the compressive bolts 35.

(12) Again with reference to FIG. 1, the centrifugal separator comprises a stationary vortex generator 10 configured to bring the gas stream in rotation. The vortex generator 10 configured to bring the gas stream in rotation is positioned upstream of the rotor and formed in the second frame portion 21. The vortex generator 10 comprises a gas deflecting member 11 comprising a plurality of vanes 12 which are inclined with respect to the axial direction x of the centrifugal rotor and distributed around the rotational axis. The vanes are arranged in a passage 11a formed in the second frame portion upstream of the rotor. The passage 11a extends radially outside the separation plates of the centrifugal rotor. With reference to FIG. 4, the vortex generator 10 configured to bring the gas stream in rotation is shown in further detail. The vortex generator 10 comprises a gas deflecting ring 11 comprising a plurality of vanes 12 extending outwardly from the gas deflecting ring and distributed around the rotational axis of the rotor. The vanes are inclined with respect to the axial direction of the rotor, which inclination is gradually increased along the length of the vanes in the direction of the flowing gas.

(13) According to one embodiment, the vanes may be movable/or and the inclination of the vanes may be adjusted during operation in order to control the speed of rotation of the gas stream.

(14) In addition to, or as an alternative to what is shown in FIG. 4, the gas inlet 3 upstream of the centrifugal rotor may be arranged at a right angle to the rotational axis of the centrifugal rotor, as shown in FIG. 5. This figure shows a cross-section of the vessel, perpendicular to the rotational axis of the rotor, at the inlet side of the centrifugal separator. It is preferred to connect external pipe connections at right angles in order to withstand high pressure in the vessel. In this embodiment, the vortex generator 10 configured to bring the gas stream in rotation upstream of the rotor comprises an inlet gas deflecting member 11 which is arranged to deflect the gas stream from the gas inlet towards a tangential direction of the centrifugal rotor. The inlet gas deflecting member 11 may be stationary or pivotally connected to the vessel 19 and may be slanted or bent such that gas flowing through the inlet 3 is deflected towards a tangential direction of the centrifugal rotor, thus achieving a rotational flow of the gas stream in the vessel. The position or inclination of the gas deflecting ring may be adjusted during operation of the separator such that to control the rotational speed of the gas stream. As shown, this may be achieved by the inlet gas deflecting member 11 being pivotally connected to the vessel at a point 39, and biased towards an initial position by means of a spring 40. The spring may be integrated with the inlet gas deflecting member at the pivot point or connecting the inlet gas deflecting member to another point of the vessel. At an increasing flow of gas the inlet gas deflecting member is deflected by the gas flow, which may result in a limitation of the speed of rotation of the gas in the vessel.

(15) With reference to FIG. 1, the separator is mounted in the vessel 19 by placing the separator with its self-supporting frame 2 inside the vessel, at a desired position inside the vessel, and expanding the diameter of the holding means 20 so that the holding means engage with the inner surface 25 of the vessel, to hold the separator at the desired position inside the vessel.

(16) During operation of the centrifugal separator a stream of gas enters into the inlet 3 of the centrifugal separator 1. The stream of gas is forced into the passage 11a where the inclined vanes 12 deflect the gas towards a tangential direction of the rotor of the separator. Thus the gas stream is brought into rotation by the vanes 12, and enters into the space 9 surrounding the rotor 5. In this space a pre-separation occurs whereas larger particles in the form of solid particles and/or liquid droplets having a density larger than the gas in the gas stream are separated from the gas stream by means of centrifugal forces in the rotating gas stream and deposited on the inner surface of the cylinder 24.

(17) From the space 9 surrounding the rotor, the rotating gas stream enters into the separation passages 7 formed between the separation discs 6 in the rotor. The rotor 5 is brought into rotation by the rotating gas stream by means of viscous forces acting on the separation discs in the separation passages. The rotation of the rotor is also facilitated by the elongated distance members of the disc stack working as vanes or turbine blades to improve the transfer of momentum from the gas stream to the rotor. Since the rotating gas stream is led from the radially outer portions of the separation passages and towards the radially inner portions of the separation passages, the gas stream is spun up thanks to the conservation of angular momentum. Thus the transfer of the rotation from the gas to the rotor is particularly efficient in this configuration.

(18) In the separation passages, particles in the form of solid particles and/or liquid droplets having a density larger than the gas in the gas stream are separated from the gas stream by centrifugal forces. Due to the smaller separation distances in the separation passages of the stack of frustoconical discs this even allows for separation of smaller and/or less dense particles from the gas stream. Particles separated from the gas stream are deposited on the inner surface of the frustoconical separation discs and transported radially outwardly by means of centrifugal forces. From the radially outer edge of the separation discs, particles separated from the gas stream in the separation passages are thrown towards and deposited at the inner surface of the cylinder 24.

(19) Thus the rotational flow of the gas mixture alone drives the rotation of the centrifugal rotor, without a drive motor driving the rotor. The resulting rotation causes separation of particles from the same gas stream. Cleaned gas conducted towards the central gas chamber 8 of the rotor is provided to the outlet 4 through the passages 30 and 32 formed in the rotor and the first partition, and transported from the separator through the vessel.