IL25632A - Separators - Google Patents

Separators

Info

Publication number
IL25632A
IL25632A IL2563266A IL2563266A IL25632A IL 25632 A IL25632 A IL 25632A IL 2563266 A IL2563266 A IL 2563266A IL 2563266 A IL2563266 A IL 2563266A IL 25632 A IL25632 A IL 25632A
Authority
IL
Israel
Prior art keywords
grid
particles
rods
fluid
stream
Prior art date
Application number
IL2563266A
Other languages
Hebrew (he)
Original Assignee
Mc Donnell Douglas Corp
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Mc Donnell Douglas Corp filed Critical Mc Donnell Douglas Corp
Publication of IL25632A publication Critical patent/IL25632A/en

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B01—PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
    • B01D—SEPARATION
    • B01D45/00—Separating dispersed particles from gases or vapours by gravity, inertia, or centrifugal forces
    • B01D45/12—Separating dispersed particles from gases or vapours by gravity, inertia, or centrifugal forces by centrifugal forces
    • B01D45/14—Separating dispersed particles from gases or vapours by gravity, inertia, or centrifugal forces by centrifugal forces generated by rotating vanes, discs, drums or brushes
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B01—PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
    • B01D—SEPARATION
    • B01D45/00—Separating dispersed particles from gases or vapours by gravity, inertia, or centrifugal forces
    • B01D45/12—Separating dispersed particles from gases or vapours by gravity, inertia, or centrifugal forces by centrifugal forces
    • B01D45/16—Separating dispersed particles from gases or vapours by gravity, inertia, or centrifugal forces by centrifugal forces generated by the winding course of the gas stream, the centrifugal forces being generated solely or partly by mechanical means, e.g. fixed swirl vanes

Landscapes

  • Chemical & Material Sciences (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Centrifugal Separators (AREA)
  • Cleaning In General (AREA)

Description

PATENT ATTORNEYS · D ' B J D S ' D Ί 11) File C/ 24483 PATENTS AND DESIGNS ORDINANCE SPECIFICATION Separators snnsst »jpr»3 I (we) DOUGLAS AIHCHA T COS AMY, ISO., a corporation of the State of Delaware, U.S.A., of 3000 Goean Fark Boulevard Santa Monica* California, U.S.A. do hereby declare the nature of this invention and in what manner the same is to be performed, to be particularly described and ascertained in and by the following statement: - This invention relates to separator apparatus for removing particles from fluid streams or separating one fluid from another and more particularly to such apparatus incorporating a series of bars or rods forming a grid through which the fluid is passed.
In general, successful operation of such apparatus is dependent upon the establishment of local fields of centrifugal force to which the fluid is subjected as it passes through the apparatus. At present the primary application of such apparatus is the removal of particles from a particle laden stream. Particles above a predetermined size are moved by the centrifugal force out of one portion of the stream into another portion of the stream. The two portions of the stream are then separated and delivered separately from the apparatus.
In all known prior grid type cleaners the separating forces are developed by passing the fluid stream to be treated over the surface of the grid, the individual elements of the grid being so shaped and spaced as to create the centrifugal field and to divide the streams into the particle free and particle carrying portions. The effectiveness of cleaners of this type is dependent upon the strength of the centrifugal field established which is in turn a function of the relative speed of the grid rods and the stream to be treated. The relative speed of the stream and the grid to effect separation of very small particles is so large as to impose a practical limitation on the minimum size of particles which can be removed from the air stream.
Effective control of boundary layer phenomenon has also proved to be troublesome in prior grid type separators. Particles entrained in a boundary layer will move with the boundary layer, often with the result that particles are moved into the portion of the fluid stream which is intended to be particle free.
With the foregoing considerations in mind it is the principal purpose and object of the present invention to provide improved grid type cleaners which overcome these and other problems by the provision of unique grid members, preferably cylindrical rods, which are rotated at high speed to create the necessary local centrifugal field and to establish controlled boundary layers which are utilized positively to effect the cleaning and separating action.
It is a further object of the present invention to provide improved grid cleaners having an efficiency much higher than that obtainable in prior cleaners.
It is also an object of the present invention to provide improved grid type cleaners which are com-pletely self cleaning and which, because of unique boundary layer phenomena established in the grid members, are not subject to abrasive action of the particles in the fluid being treated and which are thus subjected to substantially no wear in operation.
Additional objects and advantages of the present invention will become apparent as the description proceeds in connection with the accompanying drawings in which: Figure 1 is a side elevation of an air cleaner-incorporating the present invention; Figure 2 is an enlarged fragmentary vertical section illustrating the cleaner of the present invention; Figure 3 is an enlarged fragmentary section showing details of construction of the individual grid rods and their mounting; Figures 4, 5 and 6 are transverse sections taken respectively on lines 4-4, 5-5 and 6-6 of Figure 3; and Figure 7 is an enlarged fragmentary section illustrating diagrammatically the separating action affected by the apparatus of the present invention.
Referring now more particularly to the drawings the cleaner apparatus of the present invention, indicated generally at 20 in Figure 1, is of generally vertically elongated cylindrical construction and comprises an upper housing member 22 having an inlet air opening 24, an intermediate housing member 26 having an air outlet opening 28, and a lower removable receptacle 30 in which the impurities removed from the air stream are collected.
Conveniently, the entire apparatus is mounted on a stand assembly 32.
The upper housing member 22 has a pair of downwardly projecting flanges 3 and 36 which telescope over the inner and outer surfaces, respectively, of the grid rod mounting section 38 of the intermediate housing member 26, The parts are held in assembled relation with the bottom edge of the flange 36 in contact with an annular supporting surface on the intermediate housing 26 by a plurality of screws 40, the parts being sealed by 0-rings 42, 44 and 46, to form an annular manifold 48 having an air inlet opening 50 adapted for connection to a source of air under pressure.
At its lower end intermediate housing member 26 terminates in an inwardly projecting mounting flange 52 to which an intermediate ring 5 and a bottom cover 56 are secured by inner and outer sets of screws 58 and 60. These parts are sealed by 0-rings 62, 63, 64 and 65 to form a lower annular manifold 66. The upper and lower manifolds 48 and 66 are connected by one or more air transfer pipes 68.
The particle receptacle 30 is detachably secured in place by a clamp ring 70 secured to the outer periphery of the ring 54.
From the structure thus far described it will be apparent that the air cleaner is of essentially hollow construction to permit free passage of the air from the inlet 24 to outlet 28. Interposed in the path of the air is the cleaner structure per se which comprises a series of parallel rod assemblies 7 which are preferably arranged in the form of a circular grid so that all of the air flowing from the inlet 24 to the outlet 28 must pass through the relatively narrow spaces between the individual grid rods.
As best shown in Figure 3 the individual grid rod assemblies 72 comprise rotatable tubular cylindrical rod members 74 and fixed internal support members 76.
The support members 76 each include a top mounting head 78 received with a close clearance fit in a bore 80 in the mounting section 38 of the intermediate housing member. The head 78 carries an 0-ring 82 to seal the . parts when they are assembled .
Each member 76 also includes mounting areas 84 and 86 ad jacent its upper end and similar mounting areas 88 and 90 adjacent its lower end connected by an elongated cylindrical section 92. The reduced cylindrical lower end portion 96 of the mounting member 76 extends with a close clearance fit into a collar 98 frictionally held in a bore 100 of the ring 52 by an 0-ring 102. An 0-ring 104 similarly seals the interior of collar 98. A Bellville spring 106 yieldably holds the upper surface of the collar 98 against a shoulder 108 on the mounting member 76.
Preferably, compressed air is used to both drive the rods 7 and to support the rods for high speed rotation. For this purpose the upper ends of the support members 76 are open to the upper manifold 48 and are each provided with an interior passage 108 extending from the top of the support member to the region adjacent the lower support area 90. The enlarged upper end of the passage 108 communicates with a pair of small vertical drilled passages 110 and 112 which lead to tangential nozzles 114 and 116, respectively,, (Figure 4) which in turn lead to an annular air chamber 118 formed by a reduced section of the support member 76. The air exits from the chamber 118 through a pair of opposed nozzles 120 and 122 formed integrally with or secured to the upper end of the rod member 74 producing ro tation of the rod member at the desired speed . After passing through the nozzles 120 and 122 the air flows through a plurality of radial passages 124 (not shown) and Joins the main internal air flow.
The bearing sections 84, 86, 88 and 90 are of identical configuration but different orientation. As best shown in Figure 5» each of these sections is generally cylindrical and is interrupted by three equally spaced flats 126. Three drilled radial passages 128 connect the central air passage 108 with the respective centers of the cylindrical sections of the bearing areas between the flats 126. In operation, the air flowing through the passages 128 provides a thin film of air between the fixed support member 76 and the rod 7 to provide an air bearing to facilitate the high speed rotation of the rod with negligible frictional loss. To achieve the proper air bearing action, the clearance space between the cylindrical portions of the support rod 76 and the interior of the rod 7 is very small. For example, in a typical case, the interior diameter of the rod is .8750 and the diameter of the cylindrical bearing portions of the support rod 76 is .8749. After the air leaves the bearing surfaces it passes axially downwardly and exits from the bottom of the rod 74 principally through a series of radial channels 130 (Figure 6) formed in the upper surface of collar 98.
Compressed air is also supplied from the lower manifold 66 through a passage 132 into a bore 134 formed in the portion 96 of the support member 76. The air passes from the bore 134 through a plurality of drilled passages 136 into a manifold 138 formed in the collar 98 thence to a plurality of inclined passages 140 (one shown) to the small clearance space provided between the lower end of the rod 74 and the upper flat surface of the collar 98 to provide an air thrust bearing at this point.
In a typical case the individual rods will rotate at a high speed, i.e., 50,000 rpm - 100,000 rpm although somewhat higher or lower speeds may be used in some installations. This rotation may be obtained by the air turbine drive illustrated or by mechanical drives including belts, gears and the like. Also, the rods are preferably driven at essentially the same speed. In the specific example illustrated the diameter of the rods 74 is about 7/8 " .
Accordingly, if the rods are rotated at 75,000 rpm the surface speed of the rods is over 17*000 feet/minute. In apparatus having these dimensions and speed, the spacing between adjacent portions of the rods (which has been exaggerated in Figure 7 will be in the naghborhood of ,040 inches.
When the cleaner is in operation, a stream of particle laden air is established, either by the rotation of the grid rods or by an external source of air under pressure, which flows circumferentially of the grid structure and radially outwardly through the spaces between the adjacent grid rods 74. In a typical case the air stream flows at a rate of 1200 cfm and carries particles of one to four microns in size. The particles entrained in the air stream will approach the inner surface of the grid and will be subjected to the unique action of the grid rods which will now be described in detail with reference to Figure 7.
As the rods rotate, a boundary layer of varying thickness is established over the surface of their cylindrical body portions, the boundary layer varying in thickness as a function of the difference in the surface speed of the rods and the speed to the surrounding air.
The term "boundary layer" as used herein refers to the body of fluid set in motion by the rotation of the rods. As is well known the velocity of this body of fluid varies as an inverse function of the distance from the surface of the rods, reaching a maximum which is essentially the same as the surface speed of the rods. In the embodiment shown, the boundary layer will assume a configuration illustrated by the shaded area b in Figure 7, i.e. the boundary layer will be relatively thin or non-existent in the region in which the air stream is moving in the same direction as the surface of the rods and will be relatively thick in the region where the rods and the air stream are moving in opposite directions. The exact thickness and distribution of the boundary layer is susceptible of close calculation in a specific case.
Preferably the apparatus is operated by connecting the inlet 24 to a source of particle laden fluid under pressure. A pressurized fluid source, however, is not necessary since the grid rods, when rotated at high speed, have sufficient pumping action to move fluid through the apparatus. In either event the fluid within the unit will be caused to flow in a rotary path either by the operation of the rods alone or by the combined action of the rods and the supply of fl id under pressure tangentially through the inlet opening 24.
All of the particles will follow a downwardly spl railing path with the larger particles moving downwardly more rapidly than the smaller particles. Large particles fall rapidly into the collector 30. The smaller particles will be caused by the centrifugal force and the outward flow of fluid through the apparatus to approach the inner surface of the grid formed by the rods. When the particles reach the Individual rods they are accelerated by the boundary layer surrounding each rod to a speed which is essentially the same as the surface speed of the rods and are thus subjected to the action of the strong local centrifugal field established by each of the rapidly rotating rods. Accordingly, the particles are moved toward the throats formed between the adjacent rods. However, to pass through these spaces the particles must travel a radial distance less than the distance between the surface of one rod and the boundary layer at the surface of the next adjacent rod while the particle moves through the Angle A (Figure 7) . Any particles which traverse a greater distance will be caught by the inwardly moving boundary layer of the next adjacent rod and returned to the air stream circulating within the grid structure.
The actual path followed by a given particle will be determined principally by the centrifugal force Fc exerted on the particle P which is primarily a function of the mass of the particle and its angular velocity which, in turn, is determined by the rotary speed of the rods. As the particle moves radially along the path shown diagram-matically in Figure 7 i s movement will be opposed by a radially acting air drag force Fd. However, this force is small as compared to the opposing centrifugal force and it may be ignored except for exceedingly small particles. Accordingly, by rotating the rods to obtain a high surface speed and by spacing them relatively closely together, particles of even very small size are given sufficient radial velocity to cause them to pass into the boundary layer of the next associated rod for return to the main air stream at the inside of the grid where they continue their downward spiralling movement and pass ultimately into the container 30. Thus, the cleaner of the present invention is many times more effective than prior cleaners embodying stationary grid elements.
Because of the high centrifugal field created in the region of the surface of the individual grid rods they are self-cleaning and since all particles are urged away from these surfaces, the surfaces are subjected only to negligible wear in operation.
While, as stated above, the grid members are preferably cylindrical, other configurations may be utilized with good results. For example, the surfaces of the members may be grooved, fluted, or roughened.
Any type of grid member may be utilized so long as it effectively produces a high strength local centrifugal field and maintains the spacing between the peripheral surfaces of the adjacent members substantially uniform. Rods having an oval or a square cross section would not be satisfactory since they fail to maintain this uniform spacing between the rods.
The rods may be arranged to provide grids of other forms. For example, the rods may be arranged in a straight line or in the form of an arc which may be circular or non-circular. In casee where the grid is of non-circular form, seals or scrapers must be provided at opposite ends of the grid to prevent leakage in these regions. Regardless of the configuration of the grid, the rods may be rotated in either direction. Also, the direction of the air stream with respect to the grid is immaterial.

Claims (6)

LJ What we claim is:-
1. Apparatus for separating entrained particles from a stream of fluid comprising means forming a flow path for said stream, a grid assembly interposed in said flow path, said grid assembly having an upstream side and a downstream side, and grid assembly comprising a series of grid members have body portions, means mounting said members "for rotation about their axes and in spaced paralled relation to form narrow passages therebetween, means for rotating all of said grid members in the same direction at essentially the same high speed to establish boundary layers around the peripheries thereof, the boundary layer around one member angularly accelerating the particles therein thereby causing all particles above a predetermined size which approach the upstream side of said grid to traverse the narrow passage between said one member and the boundary layer surrounding the next adjacent member to be returned thereby to said upstream side of said grid.
2. Apparatus as claimed in claim 1 wherein the grid members are rods.
3. Apparatus as claimed in claim 1 or claim 2 including a housing having inlet and outlet openings for the fluid, the grid assembly being arranged in annular form and situated in the housing between the said openings.
4. . Apparatus as claimed in claim 3 including a collector attached to the housing for the particles carried out of the path of fluid flowing from the inlet opening to the outlet opening.
5. · Apparatus as claimed in claim 3 wherein the particles gradually move towards one end of the grid for removal from the housing.
6. Apparatus for separating entrained particles from a stream of fluid substantially as hereinbefore described with reference to and as shown in the accompanying drawings. For the Applicant* DR. K!NHOLO COMMAND PARTNERS
IL2563266A 1965-05-28 1966-04-26 Separators IL25632A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US45970465A 1965-05-28 1965-05-28

Publications (1)

Publication Number Publication Date
IL25632A true IL25632A (en) 1970-01-29

Family

ID=23825838

Family Applications (1)

Application Number Title Priority Date Filing Date
IL2563266A IL25632A (en) 1965-05-28 1966-04-26 Separators

Country Status (8)

Country Link
BE (1) BE681462A (en)
CH (1) CH453048A (en)
DE (1) DE1507791B2 (en)
FI (1) FI46685C (en)
GB (1) GB1070610A (en)
IL (1) IL25632A (en)
NL (1) NL6607276A (en)
SE (1) SE310649B (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108595759A (en) * 2018-03-22 2018-09-28 南京航空航天大学 A kind of Moving Boundary Problem computational methods based on OpenFOAM redevelopment

Also Published As

Publication number Publication date
CH453048A (en) 1968-05-31
SE310649B (en) 1969-05-12
NL6607276A (en) 1966-11-29
GB1070610A (en) 1967-06-01
BE681462A (en) 1966-10-31
DE1507791A1 (en) 1970-07-23
FI46685B (en) 1973-02-28
FI46685C (en) 1973-06-11
DE1507791B2 (en) 1972-03-16

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