In-line swirl vortex separator
11097214 · 2021-08-24
Inventors
Cpc classification
B01D45/16
PERFORMING OPERATIONS; TRANSPORTING
B04C2003/006
PERFORMING OPERATIONS; TRANSPORTING
B04C5/103
PERFORMING OPERATIONS; TRANSPORTING
B04C3/06
PERFORMING OPERATIONS; TRANSPORTING
B04C3/00
PERFORMING OPERATIONS; TRANSPORTING
International classification
Abstract
An in-line swirl vortex separator to separate solids, liquids, particulate from a vapor stream. The swirl vortex separator includes a swirl element and a vortex element. The vortex element creates pairs of vortices that are substantially equal and opposite in direction.
Claims
1. An in-line swirl vortex separator for separation of solid particulates and/or fine liquid droplets from a vapor stream comprising: a housing, the housing including a swirl element and at least one vortex element, the at least one vortex element proximate and downstream from the swirl element, each vortex element comprising at least one pair of converging or diverging vortex tabs positioned against an inner surface of the housing, wherein each pair of vortex tabs has a vortex tab axis aligned with a direction of vapor flow, and wherein each pair of converging or diverging vortex tabs creates a pair of vortices that are substantially equal and opposite in direction adjacent the inner surface of the housing; and a liquid injector and liquid injection system connected to the housing to deliver a film of liquid over the inner surface of the housing.
2. The in-line swirl vortex separator as in claim 1 where each pair of vortex tabs are angled relative to the vortex tab axis between each pair of vortex tabs.
3. The in-line swirl vortex separator as in claim 2 where the angle between each vortex tab and the vortex tab axis is 12-28°.
4. The in-line swirl vortex separator as in claim 1 where each vortex tab has a leading edge and a trailing edge and wherein each leading edge and trailing edge is any one of straight, swept forward, swept backwards, convex or concave relative to a direction of flow.
5. The in-line swirl vortex separator as in claim 1 wherein the housing has an inside diameter (ID) and each vortex tab has a height and wherein a ratio of ID to height is between 5:1 and 50:1.
6. The in-line swirl vortex separator as in claim 1 wherein each vortex tab has a length and a height and a ratio of length to height is between 2:1 and 6:1.
7. The in-line swirl vortex separator as in claim 1 wherein the housing further comprises an outer housing radial to the housing, the outer housing configured to create an annular space between the housing and outer housing and wherein the housing includes a circumferential drain adjacent a downstream end of the housing enabling solid/liquid flowing along the housing to drain to the annular space.
8. The in-line swirl vortex separator of claim 7, where the annular space enables gas within the annular space to be recycled to an upstream location within the housing.
9. The in-line swirl vortex separator as in claim 7 where the annular space includes a sump for draining fluids/solids from within the annular space.
10. The in-line swirl vortex separator as in claim 1 wherein the swirl element includes a plurality of stator vanes angled between 40-70° relative to a longitudinal axis of the housing, the stator vanes for inducing swirling flow of gas/liquid/solids flowing through the housing.
11. The in-line swirl vortex separator as in claim 10 where the vortex tab axis between each pair of vortex tabs is substantially aligned with the angle of the stator vanes.
12. The in-line swirl vortex separator as in claim 10 where each pair of vortex tabs are adjustable in at least one of height relative to an inner surface of the housing and the angle of the vortex tab axis relative to the longitudinal axis of the housing.
13. The in-line swirl vortex separator as in claim 1 where the housing further comprises a liquid injection system, the liquid injection system to deliver a liquid: a. proximate and upstream of the swirl element; b. between the swirl element and the at least one vortex element; or c. proximate the at least one vortex element.
14. The in-line swirl vortex separator as in claim 13 further comprising a liquid/solid reservoir for receiving liquid/solid from the housing and a pump for returning recovered/liquid solid to the housing at an upstream position of the housing.
15. A method of separating solid particulates and/or fine liquid droplets from a vapor stream within a housing comprising the steps of: a. swirling the vapor stream to form a swirling vapor stream; b. introducing a liquid film by a liquid injector over an inner surface of the housing to deliver a film of liquid over the inner surface of the housing; c. generating pairs of vortices by at least one pair of converging or diverging vortex tabs on an inner wall of the housing, where in the swirling vapor stream, the vortices are substantially equal and opposite in direction adjacent the inner wall of the housing, and where each of the pairs of vortex tabs has a vortex tab axis aligned with a direction of vapor flow; and d. removing the contaminant from the vapor stream.
16. The method of claim 15, wherein the combined effects of swirling and the vortices generate centrifugal force in the same direction.
17. The method of claim 16, further comprising the step of injecting liquid: proximate and upstream of the swirling; between the swirling and the vortices; or proximate the vortices.
18. The method of claim 17 further comprising the step of recovering liquid from a downstream location of the housing and recycling at least a portion of the recovered liquid to an upstream location of the housing.
19. The method of claim 15 wherein the angle, position, height and length of the vortex tabs are matched to a gas flow rate within the housing to effect separation of solid particles smaller than 1 micron from the flowing gas.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
(1) The invention is described with reference to the drawings wherein:
(2)
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DETAILED DESCRIPTION OF THE INVENTION
(8) Generally, the present disclosure describes systems and methods for separation of solid particulates and/or fine liquid droplets from a vapor stream. The system is particularly effective in separating smaller medium sized particles (about 1-10 microns) and smaller particles (<1 micron) and fine liquid droplets from a flowing gas stream.
OVERVIEW
(9) With reference to the figures, an in-line swirl vortex separator is described. As shown in
(10) In a preferred embodiment, and as described below, the separation and recovery of fine solid particles can be improved by introducing a film of liquid over the interior housing wall. Liquid may be introduced upstream of the swirl element 50a, upstream of the vortex elements 50b or at another location 50c and can be effective in enhancing entrainment of the solid particles within the liquid.
(11) Further details and embodiments of the invention as well as the operation of the invention are described.
(12) Housing
(13) Generally, the housing 12 is a cylindrical tube that can be oriented horizontally (
(14) The housing may comprise an inner housing wall 12c where the primary separation as described takes place as well as an outer housing 12d wall that defines an annular space 12e. The annular space can both enable fluids/solids to drain towards a sump 22 for removal from the system as well as a flow path to recycle gas towards the upstream end of the housing as will be described in greater detail below. Gas/liquids/solids entering the annular space may also exit the system through optional port 20c.
(15) In one embodiment, the diameter D of the inner housing is generally about 2-8 inches and preferably about 4-6 inches.
(16) In one embodiment, the tube may be tapered narrowing towards the downstream end (not shown).
(17) Housing Drain and Sump
(18) A housing drain 20 is positioned downstream of the vortex tabs 16. The housing drain is typically a raised lip 20a extending around the circumference of the housing and having dimensions allowing solid/liquids to flow under the lip and enter the annular space. The sump 22 will preferably be located at a lower region of the housing such that any liquids and entrained solids can flow by gravity from the system.
(19)
(20) Gas may exit the system through exit E.
(21)
(22) Swirl Element
(23) The swirl element 14 is located adjacent the upstream end 12a the housing. The swirl element generally functions to induce a rotational flow into the flowing gas/liquid/solid mixture 18 as it enters the housing. The swirl element will generally include a fixed series of stator vanes 14a angled to deflect the mixture in a radial direction and towards the inner housing 12c. An actively driven fan (not shown) may be positioned upstream or downstream of the stator vanes to provide flow to the mixture. The stator vanes will typically be angled between 40 and 70 degrees with respect to the housing axis 24 as shown in
(24) Vortex Elements
(25) The vortex elements are positioned within the housing in pairs downstream of the swirl element. As shown in
(26) The vortex elements generally comprise a pair of converging vanes or diverging vanes. That is the narrow end of the vortex tab “cone” can face upstream or downstream. Cones shown in
(27) Each pair of vortex elements is generally evenly distributed about the housing and are positioned so as to generally not overlap with one another in the direction of flow. That is, it is generally desirable that one pair of vanes does not directly block a downstream pair of vanes so as to enable smooth swirling motion through the housing.
(28) Vanes may have a variety of shapes and be positioned in a number of ways within the housing while enabling the creation of counter-rotating vortices.
(29) As shown in
(30) The vane axis F will generally be parallel to the trailing edges swirl element vanes, that is angle approximately 40-70 degrees with respect to the HA.
(31) The spacing 2S between vortex vanes and their height H are important to ensure that the vortices form and that they reach the sidewall 12c. Generally, H should be between 5-20% of diameter of housing.
(32) The length L to height H ratio of each vane should be between 2:1 and 6:1.
(33) Vanes may be adjustable, namely pivotal and/or extendable 60 with respect to the housing as shown in
(34) As shown in
(35) The spacing S between vortex tabs 16a, 16b depends on the height H of the vortex tabs. Generally, if the vortex tabs 16 are too high and the spacing between too close, the vortices will not properly form and hence small particles will not get to the sidewall 12a. If the spacing is too wide, then the small particles are not affected by the vortices and also not get to the sidewall.
(36) Pressure Reduction and Smooth Flow
(37) Preferably, the system will include systems to prevent pressure build-up and otherwise maintain even flow through the system. In one embodiment, the system includes flow surfaces 30 downstream of the swirl element to prevent the creation of disruptive turbulent flow that may affect the flow over the vortex tabs. Similarly, as shown in
(38) Liquid Injection
(39) As noted, the system preferably includes a liquid injection system 50a, 50b, 50c that is used to enhance the capture of solid/liquids. In various embodiments, liquid is injected under pressure in a manner and location so as to create a film 26 over the housing wall 12a as shown schematically in
(40) The liquid may be water or other liquids (eg. methanol) that may help entrain a particular solid. That is, the liquid may be selected on the basis of its ability to react with the solid and/or the interfacial interaction between a particular solid and liquid combination. In another embodiment, the introduced liquid may effectively neutralize the acidity or basicity of an input stream. For example, a caustic solution may be used with a stream containing acidic particles and gas as a means of neutralizing the acidic stream for downstream handling and/or to minimize damaging effects of the stream on other equipment.
(41) General Theory of Operation
(42) Without being bound to any particular theory, it is generally understood that the swirl element induces a centrifugal force on the denser particles (ie. solids and liquids) which moves these particles radially towards the housing. As the swirling mixture engages with the vortex tabs, the solid/liquid particles flow over the vortex tabs forming a spiraling stream of solid/liquid particles flowing off each vortex tab (see
(43) In the preferred embodiment, where the housing has a liquid film flowing over the housing, the vortices a) disrupt what may otherwise be laminar flow of liquid over the housing and b) bring the stream of particles against the liquid film at a sharper angle where they may impact against and become trapped within the liquid film. In other words, the vortex tabs interrupt what may be the laminar flow of liquid over the housing which creates a more turbulent surface which both increases the surface area of the liquid film which enhances the ability of the liquid film to entrain solid particles.
(44) In comparison, centrifugal systems that do not have vortex tabs, while bringing solid/liquid particles close to the housing by centrifugal forces, these systems can create laminar boundary layers that are difficult for very fine and low mass particles to enter.
(45) In operation, the flow of the input mixture is maintained at a level to induce counter rotating vortices of the vortex tabs.
(46) Applications
(47) Example applications include applications where it is desirable to remove small particles from a gas stream. Examples of gas sources include flue gases containing dust/smoke/ash particles from a furnace, incinerator, boiler, etc. and gas transmission lines.
(48) The system may be used as a filter upstream of HVAC systems on the air intake to an air heater such as a furnace or an air cooler such as a chiller or HVAC system, or it could be used without heating/cooling as an air filter/purifier in an air intake system. Example air intake systems could be air intakes for vacuum systems, engine intakes or any standalone air filtration system.
Example 1
(49) A system comprising a horizontal clear tube having a 6 inch internal diameter and 4.5 foot length was tested with a 700 ACFM (actual cubic feet per minute) air flow. The system included swirl element vanes oriented at 50 degrees to the flow path together with 4 pairs of vortex tabs spaced evenly about the inner housing. Each pair of vortex vanes had straight leading and trailing edges and had a height of 0.4 inches and a length of 2.3 inches. For testing purposes, fine threads were attached to the inner trailing edge corner to visually observe the creation and direction of flow of vortices off the trailing edges. The vortex vanes of a pair were separated by 0.5 inches and angled at approximately 50 degrees to the longitudinal axis of the housing.
(50) For a given vortex tab orientation, air flow was established and the movement of tell tales observed. As airflow was steadily increased from 0 to 700 ACFM, the telltales would initially show no discernable pattern of movement. As air flow was increased, counter rotating vortices would be observed.
(51) Upon establishing air flow, water was introduced upstream of the swirl element via high pressure atomizing nozzles so as to create a fine distributed mist upstream of the swirl element. The water was observed as 4 discernable spiraling streams downstream of each of the 4 pairs of vortex tabs which demonstrated that the water mist particles collided with each other and moved to the housing wall in an observable stream. Separate spiraling water streams were not observed upstream of the vortex tabs.
(52) Similarly, when the same system was tested without vortex tabs, no discernable water patterns were seen along the length of the housing.
(53) In one test, a recycle tube was used to allow the recycling of air to a position upstream of the swirl element. In this test, no internal and central tube was included. This test showed that recycled air reduced the pressure drop across the swirl element and improved the formation of the spiraling streams of water.
Example 2
(54) A vertical clear tube housing with a 4 inch outside diameter and an inside diameter of 3.75 inches was set with a swirl element that induced a swirl at 58 degrees to the longitudinal axis. An inside tube having an OD of 1.32 inches ran the length of the tube in the centre.
(55) Water was injected above the swirl element through 6 holes having 0.08 inch diameter and evenly spaced about the tube housing. The flow rate of the water was maintained at approximately 6 gallons per hour.
(56) Air flow through the housing was maintained at 100 ACFM (actual cubic feet per minute). Talcum powder having a mean particle size diameter less of 0.5 microns was introduced to the air flow via a 100 psi air injection system upstream of the swirl element at right angles to the direction of air flow through the housing. With the rate of injection and angles of intersection, the powder was observed as being fully dispersed within the air flow almost instantaneously.
(57) A bank of Filterite™ sub micron filters was set downstream at the gas exit to catch any particulate carry over. The filters were weighed before and after each run.
(58) A total of 3 lbs of talcum powder was introduced to the system over a 10 minute run. The filters were weighed using a gram scale to determine a mass carry over of the particulate. No measurable difference in the weight of the filters was seen after running the entire 3 pounds of powder. The water recovered from the housing was milky white.
(59) The pressure drop across the swirl element was 1.8 inches of water column.
(60) Importantly, the pressure drop was substantially less than a typical cyclone separator which would typically operate at 28 inches of water column and would only be able to separate particles greater than 10 microns.
(61) While the present invention has been described in the context of specific embodiments thereof, other alternatives, modifications, and variations will become apparent to those skilled in the art having read the foregoing description. Accordingly, it is intended to embrace alternatives, modifications, and variations as fall within the broad scope of the appended claims.