U.S. patent number 3,747,299 [Application Number 05/223,512] was granted by the patent office on 1973-07-24 for electrostatic precipitator.
Invention is credited to Ta-Kuan Chiang.
United States Patent |
3,747,299 |
Chiang |
July 24, 1973 |
ELECTROSTATIC PRECIPITATOR
Abstract
An electrostatic precipitator in which particles entrained in
the gas stream are first electrically pre-charged by induction and
conduction from a closed and non-emitting electrode configuration
then further charged toward their saturation charge in an optimized
particle charging section by corona field charging mechanism and
finally collected in an optimized precipitation field. To retain
the collected particles a controlled and confined electric wind
turbulence is provided at the collection plates together with ion
showers of the same polarity as of the charged particles. Particle
reentrainment even during mechanical dislodgement is eliminated by
the effective use of turbulence mixing and diffusion of the
confined electric wind near at the collection wall, and is further
assured by the recharging and recollection of particles
accomplished by the ion showers in an optimized precipitation
field.
Inventors: |
Chiang; Ta-Kuan (Berkeley
Heights, NJ) |
Family
ID: |
22836825 |
Appl.
No.: |
05/223,512 |
Filed: |
February 4, 1972 |
Current U.S.
Class: |
95/79; 96/62;
96/77 |
Current CPC
Class: |
B03C
3/12 (20130101); B03C 2201/14 (20130101) |
Current International
Class: |
B03C
3/12 (20060101); B03C 3/04 (20060101); B03c
003/12 () |
Field of
Search: |
;55/2,112,136,137,138,139,134,135,128,129,150,151,154 |
References Cited
[Referenced By]
U.S. Patent Documents
Primary Examiner: Talbert, Jr.; Dennis E.
Claims
I claim:
1. A method of electrostatically precipitating particles entrained
in a gas stream comprising
passing the gas stream through a particle pre-charging zone to
impart at least a minimal charge to substantially all of the
particles,
passing all of the particles so pre-charged through a corona field
zone to impart a saturation charge to all of the said pre-charged
particles,
passing the particles so saturation-charged through a non-emitting
precipitation field to collect the particles on a collection
surface, and
providing local ion showers to the particles on the collection
surface to maintain charges on the collected particles.
2. The method according to claim 1 wherein a controlled electric
wind turbulence limited to the aerodynamic surface boundary region
of said collection surface is provided.
3. The method according to claim 1 wherein said collection surface
comprises first and second plates biased to opposite polarities and
wherein first and second ion showers each having a polarity
matching the polarity of the corresponding one of said plates are
provided.
4. In a particle precipitator wherein particles entrained in a gas
stream are subjected to a corona saturation charging field and
thereafter to a passive precipitation field in a particle
collection zone, the improvement characterized in that
a particle pre-charging zone is established prior to the corona
field to impart at least some minimal charge to substantially all
particles entering the corona field, and in that
local ion showers are provided over the aerodynamic surface
boundary region of the collection surface of the particle
collection zone.
5. Apparatus including a gas stream duct for electrostatically
precipitating particles entrained in a gas stream comprising
non-emitting particle pre-charging means position in said gas
duct,
corona field particle charge means positioned in said duct
downstream of said pre-charging means,
non-emitting collection field producing means positioned in said
duct downstream of said corona field particle charging means and
defining a particle collection region of said gas duct, and
a plurality of emitting means positioned adjacent the surface
boundary region of said particle collection region.
6. Apparatus according to claim 5 wherein said plurality of
emitting means is biased to provide a confined electric wind
turbulence in said surface boundary region of said particle
collection region of said duct walls.
7. Apparatus according to claim 6 wherein said plurality of
emitting means provides ion showers to said surface boundary region
of said duct.
8. Apparatus according to claim 5 wherein said particle
pre-charging means includes a plurality of closed configuration
electrodes porous to particle and gas flow.
9. Apparatus according to claim 5 further comprising gas stream
channeling means inserted in said gas duct in the area thereof
defined by said particle pre-charging and particle charging means
for dividing said gas stream duct into a number of subducts each
including one of said particle pre-charging means and one of said
particle charging means, and
means for individually biasing the particle pre-charging and
particle charging means located within a continuous one of said
subducts.
10. Apparatus according to claim 9 wherein said particle
pre-charging means and said particle charging means contained
within the same one of said subducts are each biased to the same
electric polarity.
11. Apparatus for electrically precipitating particles entrained in
a gas stream comprising
a gas stream duct having an inlet and an outlet and conductive wall
surfaces connected to a source of reference potential,
particle pre-charging means disposed at the inlet of said duct and
connected to a potential source for establishing a non-emitting
electric field in the vicinity of said duct inlet,
emitting electrode means disposed in said duct downstream of said
particle pre-charging means for establishing an emitting electric
field extending over a short axial length of said duct, said
emitting electrode means defining a particle saturation charging
region in said duct,
central electrode means having a substantial particle collection
surface area positioned in said duct downstream of said emitting
electrode means, said central electrode being connected to a source
of potential to establish a passive, non-emitting particle
collection field extending over a substantial axial length of said
duct, said particle collection field being directed from said
central electrode to the adjacent conductive wall surfaces of said
duct, and
a plurality of emitting electrode means disposed throughout the
length of said central electrode for providing ion showers over the
aerodynamic boundary surface of said central electrode.
12. Apparatus according to claim 11 wherein said central electrode
is connected to a source of potential of polarity opposite to that
of the nearest of said emitting electrodes in said particle
saturation charging region.
13. Apparatus according to claim 11 wherein the combination further
comprises a second plurality of emitting electrode means disposed
in said duct adjacent to said conductive wall surfaces thereof over
an axial length thereof substantially equal to the axial length in
said duct of said central electrode, said second plurality of
emitting electrodes being connected to a source of potential for
establishing ion showers over the aerodynamic boundary layer
portion of the adjacent conductive wall surfaces of said duct.
14. Apparatus according to claim 13 further comprising channeling
means inserted in said duct in the areas thereof defined by said
particle pre-charging electrode and said particle saturation
charging region for dividing said gas stream into a plurality of
subducts, each of said subducts including a particle pre-charging
electrode and at least one particle saturation charging electrode,
wherein at least one of said subducts includes a particle
pre-charging electrode connected to a source of potential of
opposite polarity to that to which the particle pre-charging
electrode of another of said subducts is connected.
15. Apparatus according to claim 14 wherein the particle
pre-charging and particle saturation charging electrodes within the
same subduct are connected to respective sources of potential
having the same polarity.
16. Apparatus according to claim 13 wherein said first plurality of
emitting electrodes is biased to provide ion showers of opposite
polarity to that provided by said second plurality of ion showers.
Description
BACKGROUND OF THE INVENTION
The present invention relates to the electrostatic precipitation of
particles entrained in a gas stream and, more particularly, to a
method of and apparatus for, more efficient precipitation by
reducing the reentrainment of particulate matter.
Electrostatic precipitation of particles entrained in a gas stream
is widely known and used in many industrial applications and for
air cleaning. There are two types of electrostatic precipitators in
use, namely, the Cottrell type and the two-stage type.
Structurally, the Cottrell type has a plurality of fixed collectors
with emitters equally spaced and centrally located with respect to
the collectors; the two-stage type has a short section that
contains a number of fixed emitters followed immediately by a
relatively long section containing a plurality of fixed collectors
and passive electrodes centrally located with respect to the
collectors. Functionally, entrained particles are charged and
collected through the entire length of collectors in the Cottrell
type; whereas particle charging and collection are separately
accomplished in the two separate sections in the two-stage type.
The first section is called the particle charging stage; the second
section is called the particle collection stage. In practice, the
Cottrell type is used in general for high particle loading, low gas
velocity and continuous applications; whereas the two-stage type is
used exclusively for low particle loading, high gas velocity and
intermittent applications. The prior art systems thus do not
provide a universal type precipitator for high particle loading,
high gas velocity and continuous applications of gas
separation.
The major shortcomings in the Cottrell type are due to particle
reentrainment and low precipitation rate. Particle reentrainment
may be caused by aerodynamic or electric wind turbulence or by
improper mechanical dislodgement for particle removal. Low
precipitation rate is characterized by low particle drift velocity
due to an unoptimized precipitation field intrinsically limited by
corona sparkover voltages. Another shortcoming in the Cottrell type
under heavy particle loading is that particle depositions occur on
emitters. In the past, it has been attempted to compensate for
these shortcomings by a lengthening of the collection zone to
compensate for ineffective particle charging and collection and
reentrainment.
The major shortcoming in the two-stage type of precipitator is due
to the inability to hold precipitated particles onto the collection
plates in the collection stage even though the precipitation field
has been optimized. Prior attempts to hold the collected particles
for this type of precipitator have included the use of some kind of
chemical adhesives coated on the collector plates which must be
cleaned and recoated with adhesives after each use. This approach
prevents continuous operation and the handling of high dust
loading.
Precipitators have also been proposed in which the particle
collection surfaces are in the form of endless belts, conductive,
semi-conductive of dielectric, charged or non-charged, that
continuously or periodically move through the collection zone.
Although, particle reentrainment due to mechanical dislodgement is
reduced, the complexity of a moving system after all is impractical
for many reasons. It is the object of this invention to provide a
simple yet efficient precipitator system by combining the
advantages of the prior art systems and by eliminating their
shortcomings such that the present invention is capable of for all
applications of gas separation, i.e., any particle loading, high
gas velocity and continuous applications.
SUMMARY OF THE INVENTION
The present invention deviates from the prior art systems by having
three separate functional stages, namely, a particle pre-charging
section, a particle charging section and a particle collection
section. Each section can then be independently optimized for its
respective design function. The function of the particle
pre-charging section is to assure that all particles passing this
section will carry a small amount of charge of the same polarity as
obtained later in the particle charging section. Advantageously,
pre-charging of a particle may be done by induction and conduction
charging so that any particle deposition on the pre-charging
electrodes will not offset its pre-charging function. It is however
understood that induction and conduction charging is most effective
with respect to non-dielectric particles.
Further charging of the particles to saturation is accomplished in
the particle charging section which employs corona discharges from
emitting electrodes. By the use of the particle pre-charging
section no particle deposition will occur on the emitting
electrodes in the particle charging section because there are no
uncharged or oppositely-charged particles in the zone.
Structurally, the particle pre-charging section is accomplished by
placing a row or rows of rod electrodes of a closed configuration
porous to inlet particles and gas flow at the inlet of the
precipitator system of my invention. These electrodes, passive,
i.e., non-emitting, are raised to high potentials of the same
polarity as that of the emitters in the particle charging section.
All particles passing these electrodes are then inductively charged
to a small degree but are charged to the same polarity obtained in
the following particle charging section. Pre-charging electrodes
can be of other closed configurations, such as rings, honeycombs,
screens or meshes porous to particle and gas flow. The main point
is that they be non-emitting and of the same polarity as the
emitters in the particle charging section. Non-emitting electrodes
are essential here for the reentrainment of any particles on these
electrodes results in these particles being charged to the correct
polarity by conduction.
All particles leaving the pre-charging section are then further
charged up to saturation by field charging in the particle charging
section. The important attribute of the operation of the particle
charging section of my invention is that all particles entering the
particle charging section carry a small amount of charge of the
same polarity as that of the emitters, and therefore particles are
kept away from the emitters resulting clean emitters with
consistent charging properties. Advantageously, the particle
charging section may have any configuration suitable for particle
charging by corona discharge and the geometry thereof may be
optimized for particle charging to saturation and yet minimized for
particle collection.
In further accordance with my invention, electric wind turbulence
and ion showers are utilized to enhance particle collection and to
prevent particle reentrainment in the particle collection section.
In an exemplary embodiment, a duct-type collection section
comprises a centrally located passive electrode and a plurality of
emitters located at a small distance away from the collector plate
surfaces of the duct but a large distance away relative to the
centrally located passive electrode. A high voltage of the same
polarity of the emitters in the particle charging section is
applied to the central electrode. Another high voltage, of suitable
magnitude less than that of the central electrode, and of the same
polarity as of the central electrode, is applied to the emitters in
the particle collection section. The emitters in the collection
section are small in diameter and are located closely to the
collector plate surfaces but far away from the central electrode.
Accordingly, the optimized precipitation field resulting from the
maximum voltage appliable to the central electrode without
sparkover is practically undisturbed. Furthermore, the emitters in
the collection section function to provide ion showers to hold
particles onto the collector surfaces until deliberate dislodgement
is allowed to take place. It is an aspect of the operation of the
emitters when located closely to the collectors that the electric
wind turbulence is confined to small eddies in the region of the
emitters and the collector surfaces. This region is also the
aerodynamic boundary layer region. Accordingly the small eddies
along the collector wall help to bring in particles aerodynamically
from the center region toward the collection plates in addition to
the particles being driven by the optimized precipitation field.
Whenever the collected particles become thick enough to fall by
gravity, a proper mechanical dislodging force may be applied to the
collector for particle removal. Any particles that are broken loose
and therefore which would otherwise be susceptible of becoming
reentrained during mechanical dislodgement will, however, be
charged up immediately by the near-by emitters. Further, because
the emitters in the particle collection zone of my invention
produce ionization of the gas stream only in the immediate vicinity
of the collection plates, the electric wind accompanying this
ionization is confined to little eddies adjacent the collection
plates. These eddies sweep up the re-charged particles and carry
them to the collection plates.
BRIEF DESCRIPTION OF THE DRAWINGS
A better understanding of the invention may be obtained by
referring now to the following detailed description in conjunction
with the figures of the accompanying drawing, in which:
FIG. 1 is a top horizontal sectional view of one embodiment of the
electrostatic precipitator of the present invention;
FIG. 2 is a vertical end sectional view of the embodiment of FIG.
1;
FIG. 3 is an expanded horizontal sectional view of the pre-charging
section of the apparatus of FIG. 1;
FIG. 4 is a horizontal sectional view of an alternate embodiment of
the electrostatic precipitator of the present invention; and
FIG. 5 is an expanded detail of the particle collection section of
FIG. 4.
DETAILED DESCRIPTION
in FIG. 1, a representative embodiment of the invention includes a
gas stream duct 60 divided into three functional sections: the
particle pre-charging section 20, the particle charging section 30,
and the particle collection section 40. A number of non-emitting
rod electrodes 22 are arranged in a closed configuration and
positioned within gas stream duct 60 in the pre-charging section 20
by the use of a suitable number of insulating supports (not shown).
The interior walls of duct 60 define the collector plate surfaces
50. Electrodes 22 and the adjacent areas of plates 50 define the
particle pre-charging section 20.
The particle charging section 30 is located downstream from the
pre-charging section 30 and includes two wire emitters 32 located
at the center of the duct 60. Wire emitters 32 are mounted within
duct 60 via suitable insulating means (not shown) to insulate them
electrically from collector plates 50.
The particle collection section 40 comprises a central electrode
sheet 42 which is insulated from plates 50 and which partitions the
main duct 60 into two subordinate gas ducts 70. A number of wire
emitting electrodes 44 also insulated from collector plate walls 50
are positioned at equal distance from each other and closely spaced
with respect to collection plates 50. It is understood that the
number and configuration of the electrodes in each of sections 20,
30, and 40 shown in the drawing are for illustration purpose only.
For instance, electrode 20 need not be limited to only one row, but
can include a number of rows; nor need the closed configuration be
of rod-shaped elements, but rings, honeycombs, screens, or meshes
may be employed so long as electrode 20 is porous to particle and
gas flow and yet of closed configuration and non-emitting.
All electrodes 22, 42, and emitters 32, 44 are connected to high
voltage power supplies that have the same polarity with respect to
the collection plates 50; as illustrated in FIG. 1, they are all at
negative potentials with respect to the collection plates 50 which
are, as illustrated, at ground potential. The potential of
pre-charging electrode 22 is maintained at a level which will not
result in corona discharge. The emitters 32 are however placed at
the optimum voltage for particle charging by corona discharge. The
center electrode 42 is maintained at an optimum voltage just below
sparkover threshold for achieving the maximum precipitation field
for particle collection. The voltage applied on wire emitters 44 is
kept at a minimum magnitude just sufficient to maintain adequate
corona discharges and ion showers to provide particle holding force
when collected.
Particles and gas flow are indicated by arrows in FIG. 1. At the
inlet of gas flow to duct 60 it is to be expected that most of the
particles in the gas stream will pass through the pre-charging
electrode 22. Nevertheless, some particles will collide with
electrode 22 and therefore deposit right on it. As illustrated in
FIG. 3, particles that pass the pre-charging electrode 22 without
colliding will carry a small amount of negative charge by
induction. Particles that are deposited on electrode 22 will pick
up negative charges by conduction. If the particles that have been
deposited on electrode 22 should somehow become reentrained in the
gas stream, they will nevertheless carry a small amount of negative
charge with them. Accordingly, all particles leaving the
pre-charging section 20 will be negatively charged.
Further charging of particles toward saturation is accomplished by
the corona field emanating from emitters 32 in the particle
charging section 30. Since the only function of the corona field in
the particle charging section is for charging particles (and not
for causing particles to be precipitated therein), it then can be
optimized for this purpose and the ducts can be designed taking
into account the fact that my emitters 32 are clean emitters.
Further, the corona field in section 30 emanating from emitters 32
need only extend over a relatively short axial length of the duct
in the direction of gas flow since the particle charging time
constant is only of the order of fractional milliseconds and
particle collection is not the goal in this section. Additionally,
the shorter the particle charging section, the less likelihood
there will be of any particle collection within this section. Since
there will be no particle collection, mechanical alignment of
emitters 32 with respect to walls 50 will be easier than in prior
art Cottrell type systems in which the emitting field is the
principal mechanism for particle collection.
In the particle collection section 40, a uniform electric field
optimized for precipitation of already charged particles is
provided by the potential applied to central electrode plate 42. A
plurality of emitters 44 are arranged in close proximity to the
collector plates 50 on each side of central electrode 42. Emitters
44 are equally spaced along both walls 50 to provide an electric
wind turbulence that is confined to small eddies in the region of
the aerodynamic boundary layer adjacent to each of walls 50 in the
collection section 40. In effect, the controlled electric wind
created by emitters 44 acts like a plane of electric air pumps
altering the gas flow in the immediate vicinity of the collection
plates 50. Although this pumping effect may be negligible in an
aerodynamic sense, it plays a role in enhancing the particle
precipitation rate as compared to that produced by an electrostatic
precipitation field alone.
As the particles carrying their saturation charges enter particle
collection section 40, they are electrically driven toward the
collection plates due to the optimized electric field from center
electrode 42. Furthermore, as the particles drift close to the
vicinity of the emitters 44, they are immediately subjected to the
electric wind turbulence occurring due to the ionization of the air
between the emitters 42 and the adjacent one of the collecting
walls 50. Furthermore, emitters 44 also provide ion showers to
replenish charges to the particles collected on plates 50 such that
a strong electrostatic force continuously acts on the collected
particles militating against particle reentrainment in the gas
stream. In this respect, the present invention is entirely
different than prior art systems of the two-stage type where
particles after collection lose their charge in a matter of time
depending on thier conductivity and to the point that electrostatic
force is no longer sufficient to prevent particle
reentrainment.
As the collected layer of particles on the collection plates 50
becomes thick enough to fall by its own weight due to gravity
forces, a conventional mechanical dislodging force may be applied
to the collection plates 50 for particle removal. Such rapping
mechanisms are well known. Should any particles become broken loose
during the rapping procedure they will however be charged up
immediately by the near-by emitters 42 and be brought back for
immediate collection by turbulence mixing and diffusion in the
small aerodynamic eddies existing in the region. It should be noted
that the optimized precipitation field provided by central
electrode 42 is not appreciably altered by the ionization field
emanating from emitter 44 because these emitters are closely
positioned to the collecting plate walls 50. Thus, particle
reentrainment due to mechanical dislodgement presents no problem in
the present invention.
It is thus seen that in my invention the collection zone 40 has a
passive central electrode, i.e., one which does not cause
ionization of the main gas stream. Accordingly, there is no
electric wind due to the central electrode and the field from the
central electrode may be optimized for particle deposition. This
differs from the particle collection mechanism in the Cottrell type
of precipitator in which an electric wind blows against the full
cross section of the gas stream duct causing large eddies and
whirlpools that militate for continual particle reentrainment. In
the aerodynamic boundary layer vicinity of the collection plate
walls 50, however, I provide a number of emitting electrodes that
perform a dual function, that of creating a confined electric wind
turbulence in the boundary layer region and also that of providing
ion showers to the already collected particles. These ions showers
maintain charge on the collected particles and prevent them from
being reentrained.
Another embodiment of the precipitator of the present invention is
illustrated in FIGS. 4 and 5. This embodiment also includes a
particle pre-charging section 220, a particle charging section 230
and a particle collection section 240. However, the particle
pre-charging section 220 and the particle charging section 230 are
now divided into four narrower subducts formed by collection plates
250 and auxiliary ground plates 250'. The outermost of these
subducts include negatively poled pre-charging electrodes 222 in
pre-charging section 220 and negatively poled emitting electrodes
232 in the particle charging section 230. The innermost of the
subducts includes positively poled pre-charging electrodes 222' in
pre-charging section 230 and positively poled emitting electrodes
232' in particle charging section 230.
The central electrode 242 in the particle collection section 240 is
connected to an externally applied voltage of the polarity opposite
to that of the nearest preceding emitters 232' in the particle
charging section. Two rows of new emitters 244' are included near
the central electrode 242, in addition to the emitters 244 near the
collection plates 250. The voltage applied on emitters 244' has the
same polarity as but is lower in magnitude than that of the central
electrode 242. As illustrated in FIG. 5, emitters 244' energized
with voltage of lesser magnitude than that of the central electrode
242 are electrically at a positive potential with respect to the
central electrode 242. Emitters 244' therefore provide positive ion
showers to the central electrode 242. Small aerodynamic eddies are
also generated and confined to the surface boundary region near the
central electrode 242. In analogous fashion, negative ion showers
and eddies in the surface boundary region near the collection
plates 250 are provided by emitters 244.
As particles leave the particle pre-charging section 220 they are
charged by induction and conduction to a small degree with the
polarity according to the polarity of electrodes 222 and 222',
respectively. The particles are then further charged to their
saturation by the corresponding emitters 232 and 232' in the
particle charging section. In the particle collection section 240
the particles with positive charges will now be collected on the
central electrode 242, and particles with negative charges will be
collected on the collection plates 250. With this embodiment, the
collection surfaces for particles has effectively been doubled over
that of the embodiment of FIG. 1 of the same duct volume.
Accordingly, I have shown an electrostatic precipitator having
three stages, a first pre-charging stage employing passive, closed
configuration electrodes, a second saturation charging stage
employing corona discharge electrodes but in a region confined to a
short axial length of gas flow to minimize particle deposition on
the emitters and, finally, a particle collection stage which
employs a passive electrode for providing an electric field
optimized for precipitation of the already charged particles and in
addition, in the aerodynamic boundary layer region of the
collection plate surfaces, a plurality of small emitting electrodes
biased to provide a confined electric wind turbulence in the
boundary layer region and to shower the immediate adjacent
collection plate surfaces with ions to maintain electric charges on
the collected particles.
It will be apparent to those skilled in the art that modifications
may be made in the above-described illustrative embodiment.
Moreover, to assist in the construction of an illustrative
embodiment of my invention, I suggest the following dimensions and
voltages: In the particle pre-charging section 20 the voltage
V.sub.pc applied to the passive electrode 22 may be approximately
10 kilovolts for rod-shaped electrodes 22 that are between 0.125
and 0.250 inches in diameter. In the particle charging section 30,
the voltage V.sub.pe applied to emitting electrodes 32 may be
approximately 35 kilovolts for wire-shaped emitting electrodes that
are from 0.020 to 0.040 inches in diameter. It will be apparent
that emitting electrodes 32 may be of other geometries such as that
of a saw-tooth, a string of needlepoints, barbs, etc. With the
voltage V.sub.pe of 35 kilovolts, the desired electric field
intensity E.sub.32 in the particle charging section will be
approximately 30 to 32 kilovolts per centimeter. In the particle
collection section 40, the voltage V.sub.p applied to the central
passive electrode 42 may be approximately 38.1 kilovolts per inch
of distance d between the central electrode and the collection
plate wire 50 wherein an electric field intensity E of 15 kilovolts
per centimeter is desired. The voltage V.sub.dis applied to
emitting electrodes 44 may be of approximately 10 kilovolts for
emitting electrodes 44 which are of 0.020 to 0.040 inch diameter
wire rods. The wire rod electrodes 44 may be positioned
approximately a quarter inch away from the adjacent collection
plate wall 50.
* * * * *