GB2068659A - Control of electrostatic precipitators - Google Patents
Control of electrostatic precipitators Download PDFInfo
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- GB2068659A GB2068659A GB8003569A GB8003569A GB2068659A GB 2068659 A GB2068659 A GB 2068659A GB 8003569 A GB8003569 A GB 8003569A GB 8003569 A GB8003569 A GB 8003569A GB 2068659 A GB2068659 A GB 2068659A
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- 239000012717 electrostatic precipitator Substances 0.000 title abstract 2
- 239000000428 dust Substances 0.000 claims abstract description 28
- 230000015556 catabolic process Effects 0.000 claims abstract description 9
- 230000005684 electric field Effects 0.000 claims abstract description 3
- 239000012716 precipitator Substances 0.000 claims description 72
- 238000000034 method Methods 0.000 claims description 12
- 239000002245 particle Substances 0.000 abstract description 25
- 230000005540 biological transmission Effects 0.000 abstract description 8
- 230000002411 adverse Effects 0.000 abstract 1
- 238000012360 testing method Methods 0.000 description 17
- 239000007789 gas Substances 0.000 description 11
- 150000002500 ions Chemical class 0.000 description 11
- 238000009826 distribution Methods 0.000 description 9
- 230000006872 improvement Effects 0.000 description 9
- 238000011068 loading method Methods 0.000 description 9
- 230000008901 benefit Effects 0.000 description 5
- 238000009533 lab test Methods 0.000 description 5
- 239000002956 ash Substances 0.000 description 4
- 239000003245 coal Substances 0.000 description 4
- 230000000694 effects Effects 0.000 description 4
- 238000009434 installation Methods 0.000 description 4
- 238000013508 migration Methods 0.000 description 4
- 230000005012 migration Effects 0.000 description 4
- 238000001556 precipitation Methods 0.000 description 4
- 239000003990 capacitor Substances 0.000 description 2
- 238000007796 conventional method Methods 0.000 description 2
- 230000000875 corresponding effect Effects 0.000 description 2
- 238000011065 in-situ storage Methods 0.000 description 2
- 238000005259 measurement Methods 0.000 description 2
- 230000003287 optical effect Effects 0.000 description 2
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 2
- 238000012935 Averaging Methods 0.000 description 1
- 102000016550 Complement Factor H Human genes 0.000 description 1
- 108010053085 Complement Factor H Proteins 0.000 description 1
- NINIDFKCEFEMDL-UHFFFAOYSA-N Sulfur Chemical compound [S] NINIDFKCEFEMDL-UHFFFAOYSA-N 0.000 description 1
- 239000005864 Sulphur Substances 0.000 description 1
- 238000005054 agglomeration Methods 0.000 description 1
- 230000002776 aggregation Effects 0.000 description 1
- PNEYBMLMFCGWSK-UHFFFAOYSA-N aluminium oxide Inorganic materials [O-2].[O-2].[O-2].[Al+3].[Al+3] PNEYBMLMFCGWSK-UHFFFAOYSA-N 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000010835 comparative analysis Methods 0.000 description 1
- 230000002596 correlated effect Effects 0.000 description 1
- 230000008878 coupling Effects 0.000 description 1
- 238000010168 coupling process Methods 0.000 description 1
- 238000005859 coupling reaction Methods 0.000 description 1
- 230000007423 decrease Effects 0.000 description 1
- 230000002950 deficient Effects 0.000 description 1
- 230000002542 deteriorative effect Effects 0.000 description 1
- 230000001627 detrimental effect Effects 0.000 description 1
- 239000010419 fine particle Substances 0.000 description 1
- 239000010881 fly ash Substances 0.000 description 1
- 238000002347 injection Methods 0.000 description 1
- 239000007924 injection Substances 0.000 description 1
- 238000011835 investigation Methods 0.000 description 1
- 239000011236 particulate material Substances 0.000 description 1
- 230000035515 penetration Effects 0.000 description 1
- 230000008569 process Effects 0.000 description 1
- 230000010349 pulsation Effects 0.000 description 1
- 230000009467 reduction Effects 0.000 description 1
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- 239000002912 waste gas Substances 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B03—SEPARATION OF SOLID MATERIALS USING LIQUIDS OR USING PNEUMATIC TABLES OR JIGS; MAGNETIC OR ELECTROSTATIC SEPARATION OF SOLID MATERIALS FROM SOLID MATERIALS OR FLUIDS; SEPARATION BY HIGH-VOLTAGE ELECTRIC FIELDS
- B03C—MAGNETIC OR ELECTROSTATIC SEPARATION OF SOLID MATERIALS FROM SOLID MATERIALS OR FLUIDS; SEPARATION BY HIGH-VOLTAGE ELECTRIC FIELDS
- B03C3/00—Separating dispersed particles from gases or vapour, e.g. air, by electrostatic effect
- B03C3/34—Constructional details or accessories or operation thereof
- B03C3/66—Applications of electricity supply techniques
- B03C3/68—Control systems therefor
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- Engineering & Computer Science (AREA)
- Automation & Control Theory (AREA)
- Electrostatic Separation (AREA)
Abstract
High DC voltage and superposed pulses are supplied to a multi-section electrostatic precipitator. The pulse rise time and decay time are made short enough so that adverse sparking conditions do not develop. The DC base voltage is adjusted in coordination with the superposed pulse characteristics (voltage, frequency, and shape) to maintain an average current through the collected dust layer just below or at that value which would cause electrical breakdown of the dust layer. The pulses produce instantaneously very high ion densities and electric field strengths. Alternate sections only may be pulsed, with the other sections functioning as collecting sections. In other designs, all sections may be pulsed to provide sufficient current to hold the collected particles on the collecting surfaces and to prevent reentrainment. At least one of the sections may be a pulsed transmission line. <IMAGE>
Description
SPECIFICATION
Method of operating a multiple-section precipitator for collection of high resistivity dust
This invention relates to a method of operating a multiple-section precipitator for the collection of high
resistivity dust.
The invention is directed towards optimizing operation of the precipitator so as to overcome the problems
of handling difficult dusts and their inherently deficient particle charging and collecting fields.
It has been discovered that very high particle charging can be obtained by superposing very short pulses
at very high voltage levels onto the base DC voltage without causing electrical breakdown within the
precipitator. Depending on the shortness of pulsation, very high instantaneous ion densities, and possibly
high electron densities, are emitted from the discharge electrodes which expand to the collecting electrode as a result of the applied underlying base voltage. By suitable adjustment of such parameters as base
voltage, pulse voltage, pulse rise time, pulse width and pulse repetition rate, very efficient particle charging
at adequate particle collecting fields can be obtained.
By adjusting the pulse characteristics in combination with discharge electrode diameters and interelec
trode spacing, a very high degree of freedom is obtained with respect to optimizing the charging and
collecting fields.
An important advantage of the present invention is the ability to vary the charging and collecting fields
independently of each other. By superimposing pulse voltages over a base voltage of the same polarity, the
pulse characteristics may be varied along with the base voltage, independently of each other, so that each
may be adjusted to a level that results in optimum precipitator performance.
In accordance with this invention, there is provided a method of operating a multiple section precipitator
for the collection of high resistivity dust, said precipitator having at least three sections, each section having
discharge electrodes comprised of wires having diameters of from 0.109 to 0.250 inches (0.277 to 0.635 cm)
said wire electrodes being spaced from 31/2 to 51/2 inches apart (8.89 to 13.97 cm), each section having
collecting plates spaced 9 inches (22.86 cm) apart, the spacing from each electrode to a collecting plate being
4.5 inches (11.43 cm), the collecting plates of each section having a total area of at least 8200 square feet (761
square metres), said method comprising the steps of::
a. applying a DC base voltage in the 30-50 kilovolts range between the discharge electrodes and the
collection plates;
b. setting said DC base voltage to have a value near to but just below the corona starting voltage and
such that the resultant electric field is within the range 3.0 - 7.5 kilovolts per inch (1.18 - 2.95 kv/cm);
c. applying in parallel, to the discharge electrodes of at least one but one more than the first two sections,
short pulse voltages in the 50 - 80 kilovolts range, said pulses being of the same polarity as said DC base
voltage, said pulses being applied at a pulse repetition rate in the range of 80 - 200 pulses per second;
d. setting said pulse voltages plus DC base voltage to have a peak above the normal DC breakdown level;;
e. setting said pulses voltages to have a fast rise time not greater than 200 nanoseconds and a short
decay time, said pulse having a width of from 250 to 1500 nanoseconds, to avoid excessive sparking;
f. adjusting said DC base voltage in coordination with adjustment of said applied voltage pulses to vary
the charging and collecting fields independently of each other and to maintain an average current through
the collected dust layer just below or at that value which would cause electrical breakdown of the dust layer.
Reference is now made to the accompanying drawings, wherein Figure 1 is a schematic view of a multiple section precipitator used in making the laboratory tests.
Figure 2 is a schematic view of a pulser circuit used in test runs.
Figure 3 is a schematic illustration of a folded transmission line which may be employed as one of the sections of the multiple section precipitator.
In Figure 1, dust or other particulate material in a waste gas stream is fed through a perforated plate 13
prior to the inlet section of a multiple section, single duct precipitator. In Figure 1 there are only three
sections shown but preferably there are at least four sections.
In Figure 1, each section includes a pair of opposing collecting plates 20, spaced about 9" (23 cm) apart.
The following plates may be of various dimensions. Suspended between a pair of high tension bars 31, and
centred between the collecting plates 20 in each section, is a set of nine discharge wire electrodes 30, each as
long as the plates. These discharge electrodes are of uniform size and spacing in any one installation but
may vary in different installations. In one embodiment each discharge wire electrode has a diameter of 0.109
inches (0.277 cm) and the electrodes are spaced 51/4 inches (13.33 cm) apart. In another embodiment, each
discharge wire electrodes has a diameter of 0.25 inches (0.635 cm) and the electrodes space 31/2 inches (8.89
cm) apart. The spacing from each electrode to a collecting plate is 4.5 inches (11.43cm).
After passing through the three or more sections of the precipitator illustrated in Figure 1, the gas exits
through the outlet duct 50. Hoppers 40 are provided in each section below the collecting plates 20 for
collection of the particles collected on the plates 20.
In some modes of operation, the discharge electrodes 30 in each of the sections are pulsed. In other modes
of operation, only the discharge electrodes of the inlet section are pulsed. Where only the inlet section is
pulsed, the discharge electrodes of the other sections have DC base voltage applied and these sections
function as collecting sections.
In most installations, the configuration of the discharge electrodes will be such that DC and pulse voltages are applied in parallel to the individual electrodes of each section. In some cases however, it may be advantageous to elm ply a folded tranmission line as the discharge electrode. Such a folded transmission line is illustrated in Figure 3 of the drawings and will be described later.
The essential feature of the pulser circuit shown in Figure 2 is the pulsing switch 61 which is a physical gap between the high voltage electrode 62 and the ground electrode 63. For a pulse to be generated, the gap has to break down temporarily, dumping the energy from capacitor 64 into a water load resistance 70, resulting in a pulse voltage. The rate of rise of pulse and its- decay are determined by R-C component 66-69. The charging resistor 66 as shown in the circuit determines the frequency of pulses. Separation of the gap determines the voltage at which the gap breaks down and, hence, the pulse voltage. Pulse width is determined by the water load resistance 70, storage capacitance 64, and the capacitance of precipitator load.
The coupling capacitor 71 couples the base voltage from DC power supply with the pulse voltage produced by the above means.
To establish optimum operating conditions for the precipitator of Figure 1, the following variable parameters were studied:
Variables Range (1) Pulse width : 250-1500 nanoseconds (2) Pulse voltage : 30-80 KVp (3) Pulse frequency : 80-1000pps (4) Discharge electrode diameters a. 0.109"at5.25"
with interelectrode spacing (0.277cm at 13.33cm)
b. 0.156" at 5.25"
(0.396cm at 13.33cm)
c. 0.25" at 3.50"
(0.635cm at 8.89cm)
d. 0.50" at 1.75"
(1.270cm at 4.45cm) (5) Gas temperature 160-320"F.
(6) Particle size and 5Fm mass median
concentration diameter, 3-4
grains/scfd (7) Gas Velocity : 4-6 ft/sec (122-183 cm/sec) (8) Basevoltage 10KV-50KV (9) Particle Resistivity 1011 - 1013 ohm-cm
The observations made included the following:
(1) Pulse Width - Increasing the pulse width from 300 to 1000 nanoseconds was beneficial to precipitator performance. (Only the decay time was subject to variation. The rise time remained substantially steady at about 100 nanoseconds).
(2) Pulse Voltage - Optimum performance was obtained with the pulser operating at the highest voltage possible for both the 0.25" and 0.109" discharge electrodes. Pulse voltages up to 80 KVp were used. The pulse voltage and width were monitored, as shown in Figure 2.
(3) Pulse frequency - Increasing the pulse frequency from 100 pps to 200 pps did not have an appreciable effect on precipitator performance when both the pulse voltage and pulse width were kept constant.
increasing the pulse frequency to 1000 pps had a detrimental effect. The base voltage had to be reduced to low levels (about 10 kv) and current densities were difficu It to control.
(4) Discharge Electrode Diameters and Inter-electrode Spacing - The discharge electrodes were 0.109" (0.277 cm) diameter at 51/4". (13.33 cm) spacing and 0.25" (0.635 cm) diameter at 31/2" (8.89 cm) spacing.
Plate-to-plate spacing was 9" (23 cm).
(5) Gas Temperature - The dust was kept hot prior to injection into the air stream so as to prevent any agglomeration due to moisture. The high resistivity dust tests were at gas temperatures between 280 and 320 F.
(6) Base Voltage - The base voltage during pulse energization does not have to be at its highest presparking level. There is an optimum base voltage depending on resistivity of flyash after which further increase results in deteriorating precipitator performance. for effective pulser operation, the base voltages should be below normal DC breakdown. In cases of very high resistivity, the base voltage may preferably be below the DC corona starting voltage.
(7) Current Densities - For optimum operating conditions, precipitator current densities varied between 5 and 10 milliamperes per thousand square feet of collecting surface. By using high pulse voltages and adjusting the pulse frequency and the base voltage, precipitator currents can be adjusted to operate below back-corona situations.
The Laboratory Tests
Figure 1 shows the arrangement of the precipitator used in the laboratory test programme. Dust was fed to the system by a weigh feeder in order to accurately control dust loading. The dust was well dispersed in the inlet air stream by means of an ejector-distributor arrangement in the duct. Electric heaters were used to heat the inlet air to its desired operating temperature prior to entraining the dust. Duststream of the dust feed, a low-efficiency mechanical collector was used to remove larger particles and, therefore, present precipitator with a relatively fine particle size.
In all of the runs, hydrated alumina was used as the high-resistivity dust. Its particle size distribution at the precipitator inlet was characterized by a mean diameter of 4.5 microns and a geometric standard deviation of 2.76. Particulate loading at the precipitator inlet was 3 grains/scfd. Resistivity of the dust was controlled by varying the operating temperature. For the tests reported in this paper the temperature levels were chosen to provide operation at very high resistivity with back-corona limitation, and moderately high resistivity with sparking limitation: at 300 F the resistivity of the dust was 5 x 1012 ohm-cm and at 200"F the resistivity was 2.5 x 1011 ohm-cm.
The precipitator itself was a single-duct precipitator consisting of three energized sections with total collecting plate area of 54 square feet (50,168cm2). Each section was 4.5 feet (137 cm) long with an effective flow height of 2 feet (61 cm). Collecting plate spacing was 9 inches (23 cm) and discharge electrodes were .109 inch (0.277 cm) shrouded wires spaced 51/4 inches (13.33 cm) apart. The air velocity in the precipitator was 5 feet (152 cm)/sec for all runs. Thus the specific collection area (SCA) was 120 square feet (111484cm2) 1000 acfm.
The precipitator was operated as a two stage precipitator, the inlet section being energized separately from the downstream two sections. During the pulse-energized runs, only the inlet sections was pulsed, the downstream sections conventionally energized, serving as the collecting section. Base electrical energization of both sections was provided by 70 kVp full-wave rectified power supplies. Pulses were superimposed on the base voltage in the inlet section from the pulser system.
Prior to the test programme outlet particulate concentrations from the precipitator were measured over a range of precipitation efficiencies under the operating conditions described above. These loadings were correlated with optical density as measured at the precipitator outlet using a Lear-Siegler RM4 optical transmissometer. During the test programme transmissometer readings were taken and the correlation curve was used to determine the outlet loading during each run for precipitation efficiency calculation.
Table I presents the individual tests achieved during the test programme. Results are grouped according to resistivity level and mode of operation (pulsed or conventional), not chronologically. Each of the runs was made at its uptimum condition of energization; i.e. for the conventional runs, voltage was set at a value yielding maximum efficiency, and for the pulsed runs, the combination of base voltage, pulse voltage, pulse width, and frequency was set to yield best performance. Thus, the numbers reported in Table I are optimums so that comparison among modes can be made on the basis of best performance. All of the runs are shown to provide an indication of the reproducibility of results.
TABLE I
Laboratory data for pulsed vs. conventional energization
Mode of Temp. Resistivity Precipitation W
Operation (Degrees K) (ohm-cm) Efficiency (%) (m/sec/ (m/sec)
Conventional 367 2.5 x 1011 96.3 .140 .286
98.0 .166 .375
96.3 .140 .286
96.3 .140 .286
95.7 .133 .265
95.3 .129 .253
97.5 .156 .342
97.0 .148 .315
Pulsed 367 2.5 x 1011 98.0 .166 .375
98.0 .166 .375
98.3 .172 .401
97.3 .153 .330
99.7 .246 .707
98.3 .172 .401
98.0 .166 .375
98.0 .166 .375
Conventional 422 5 x 1012 82.7 .0743 .104
82.7 .0743 .104
80.3 .0688 .0920
82.3 .0733 .102
80.0 .0681 .0906
82.7 .0743 .104
Pulsed 422 5 X 1012 95.3 .129 .253
96.0 .136 .275
95.3 .129 .253
94.3 .121 .228
All runs were conducted with inlet loading - 3 grain/scf and gas velocity = 5 feet (152 cm) sec.
Precipitator electrode geometries were conventional as described.
Each test was run at optimum electrical energization.
For each of the cases, Table I shows collection efficiency, Deutsch migration velocity, w, and the modified migration velocity, wk. The modified migration velocity is preferred for use in comparative evaluations of pulsed vs. unpulsed performance because its value in a given case is independent of the efficiency level. The modified efficiency equation is:
I-n = exp [- (wkA/V)m] where
n - collection efficiency, fractional
A = collecting area, m2
V - volumetric flow rate, m3/sec
wk = modified migration velocity, m/sec
m = exponent depending on inlet particle size distributioni
For the laboratory dust m - 635
Examination of Table I shows the expected trends in the data. Precipitator efficiencies for 5 x 1 us2 ohm-cm resistivity level are lower than for the 2.5 x 1011 level for both pulsed and conventional operation. However, at each resistivity level the pulsed operation is more efficienct than conventional. In order to quantify the improvement in performance attributable to pulsed energization, a single value of wk was calculated for each mode of operation based on the average penetration (I-n) for that mode. A very good quantitative measure of improvement due to pulsing is then the ratio of these wk values at each resistivity level. This is because wk
is a direct indicator of the level of precipitator energization. 3 Since the wk ratio represents an enhancement
of precipitator energization it is termed the 'enhancement factor', H.
Table II shows the effective wk for each operating mode and the enhancement factors at each resistivity
level.
TABLE II
Averaged laboratory data for each operating mode
Mode of Temp Resist. Precip. wk Enhance
Operation "K (ohm-cm) Eff (%) m/sec ment Factor
Conventional 96.55 .295
367 2.5 x 1011 1.33
Pulsed 98.20 .392
Conventional 81.80 .0993
422 5. 1012 2.53
95.22 .251
Pulsed
Because of the large number of individual runs involved in Table land their good reproducibility in each
mode of operation, it is felt that the values of the enhancement factor and their difference at the two
resistivity levels have very significant meaning. The fact that the level of enhancement of wk increases as
resistivity increases supports the previously described concept of the effect of pujised energization.The
poorer the conventional energization, the greater degree of improvement possible by pulsing. it should be
noted, however, that although the enhancement factor increases with resistivity, the value of wk for both
conventional and pulsed energization decreases. This shows that pulse-energized precipitation as well as
conventional is subject to resistivity- caused limitations although the limitation to the pulsed performance is
much less severe. This is reasonable based on theory, because, no matter how precipitator energization is
achieved, dielectric break-down of the dust layer will preclude further useful energization. With pulsed
energization, however, greater and more uniform ion densities and higher effective field strengths exist
when this limit is reached.
It was mentioned previously that only the inlet section of the laboratory precipitator was pulsed. This is consistent with the expectation that pulsed energization acts primarily to enhance particle charge. Thus, the
laboratory setup represents a two-stage precipitator in which enhanced charging is accomplished in the inlet
section and the downstream sections act primarily as collecting sections. Indeed it was found in a series of
laboratory tests that pulsing more than the inlet section results in no significant performance improvement
over pulsing only the inlet section. This, however, was not borne out in the full scale tests. See below.
Full Scale Results
Full-scale investigation of pulsed energization was conducted on a Research-Cottrell precipitator following
a mechanical collector serving a pulverized coal fired boiler. Each of its two fields was equipped with
separate pulsers. Each pulsed field contained a collecting plate area of 8200 ft2 (762m2). Plate spacing was 9
inches (23cm) and discharge electrodes were .109 inch diameter wires spaced 51/2 inch (13.97 cm) apart. The
downstream unpulsed precipitator consisted of two fields each with collecting area of 10800 ft2 (1003 m2).
The total collecting area of the precipitators was therefore 38,000 ft2 (3530 m2).
In order to characterize pulsed and conventional operation of the precipitator, a full test programme was
run at the site. During the test programme lowsulphur coal was burned and the boiler was operated steadily
at full load. The coal burned during the test programme averaged about 1.1% sulphur with 18% ash content.
Gas volume flow through the precipitator varied about 110,000 acfm. Data taken during the test programme
included in-situ resistivity measurements, particle size distributions, velocity traverses, stack opacity
readings using a Lear Siegler transmissometer, precipitator outlet loadings, mechanical collector inlet
loadings, and all electrical and boiler operating data. Coal and ash samples were collected during each run.
Due to unacceptable flow patterns between the mechanical collector outlet and precipitator inlet it was not
possible to measure directly the precipitator inlet loading and size distribution. However, by applying the
mechanical collector performance curves to the measured mechanical collector inlet data, it was possible to calculate the loading and particle size distribution to the precipitator for purposes of isolating precipitator
performance. The size distribution of the ash to the inlet of the precipitator was found to be characterized by a mean diameter of 2.2 microns with a geometric standard deviation of 2.2.
Operation of the precipitator during the test programme was typical of the moderately-high resistivity
limitation characterized by heaving sparking at very low current levels resulting in poor energization. The in-situ resistivity measurements were compatible with this type of operation. They arrange from 1 x 1011 to 9 x 1011 ohm-cm, averaging about 5 x 1011 ohm-cm.
All of the runs made during the test program were at optimum levels of operation for the mode being tested, i.e. both pulsed and unpulsed operations were set to yield maximum collection efficiency. Pulser variables in all runs were set at levels previous determined to be optimum.
Because it was possible to pulse each of the two inlet fields independently, four modes of operation were tested;
1) All fields energized conventionally.
2) Inlet field (A) pulsed, others conventional.
3) Second field (B) pulsed, others conventional.
4) Both inlet fields (A+B) pulsed, others conventional.
Table III presents data for runs made during the test program. The data are grouped by the mode of operation as described above, not chronologically. As with the laboratory data, precipitator efficiency, w, and wk are reported for each run. In addition, the average stack opacity and specific collection area for each run are reported; variations in SCA were due to fluctuations in gas volume. Finally the enhancement factor
H, is reported for each pulsed run. It is based on the average value of wk of .0805 for the unpulsed runs.
TABLE III
Full-scale precipitator data for pulsed vs.
conventional energization
Fields SCA Precipitator Stack w wk H
Pulsed (ft2/1000 acfm Efficiency (%) Opacity (%) (m/sec) (m/sec)
& m2/1000 acfm)
None 341 (31.7) 93.84 25.9 .0415 .0768 -
None 369 (34.3) 95.70 25.6 .0433 .0861 -
None 351 (32.6) 94.58 26.7 .0422 .0802 -
A 340 (31.6) 95.29 23.7 .0457 .0893 1.11
A 329 (30.6) 98.28 15.6 .0627 .145 1.80
A 339 (31.5) 96.05 21.5 .0484 .0978 1.21
B 349 (32.4) 95.35 22.8 .0447 .0876 1.09
B 371 (34.5) 95.56 20.8 .0426 .0842 1.05
A+B 337 (31.3) 97.84 16.3 .0578 .129 1.60
A+B 355 (33.0) 97.99 17.0 .0559 .127 1.58
A+B 371 (34.5) 98.24 16.3 .0553 .128 1.59
A+B 371 (34.5) 97.17 16.7 .0488 .105 1.30
For the particle size distribution determined at the inlet to the precipitator, the exponent, m, in the modified
Deutsch efficiency equation is substantially the same as found for the laboratory dust, i.e. 0.625. The actual levels of w and wk are lower for the full-scale tests than for the corresponding laboratory tests. This is a normally expected difference.
Examination of the data in Table Ill shows consistent improvement in performance creditable to pulsed energization. The best improvement occurred in those runs in which both fields A and B were pulsed; the average enhancement factor for these four runs was 1.5. Pulsing either field A alone or B alone also improved performance in every run but not to the same extent as A and B together.
While the test programme was being conducted, it was very obvious, just by observing the stack, that the pulsed modes of operation were improving the precipitator performance. Plotting stack opacity vs. number of sections pulsed shows the benefits in going from zero to one to two pulsed fields in the precipitator. In fact, the plot appears to indicate that further significant benefits can be realized by pulsing additional fields.
The improvement is going from one to two pulsed fields is shown both in the enhancement factors in
Table Ill and in the opacity reduction. This appears to contradict the laboratory results which showed essentially no additional improvement in pulsing more than one section. The explanation for this probably lies in the fact that the full scale operation is limited at a lower level of energization than the laboratory, for both pulsed and unpulsed operation.
It is, therefore, reasonable to expect that a greater pulsed precipitator length is necessary in the full-scale application to accomodate the benefits of enhanced energization. In fact, it may further be expected that enhancement factors greater than those measured in the laboratory are possible in this situation because of
the very low energization basis of conventional operation. This is indicated by the data in Table Ill.
Laboratory and full-scale tests have confirmed that the pulsed energization system significantly enhances
precipitator performance for the collection of high resistivity dust. Laboratory data showed enhancement
factors in the range of 1.33 to 2.53 for moderately high to very high resistivity; field data for a moderately
high resistivity ash showed the ratio to be 1.5.
The improvement noted above may possibly be explained by the following hypothesis: The pulse voltage
is substantially responsible for corona generation. ions and electrons are generated during the rising portion
of pulse voltage. The greater the peak volage, greater will be the ions generated. Also, peak currents
produced during the pulse will be orders of magnitude higher than the average current on the collecting
plates. It is believed that extremely high ion densities are realized due to the pulse. These ions mutually repel
each other during the pulseless period and expand towards the collecting plates under the field due to base
voltage. It is felt that particle charging takes place during the time between pulses, in the presence of very 'high ion concentration and the field due to base voltage.
It is also hypothized that the ionic space charge field further enhances the charging process. Also, the nature
of corona during pulse energization is significantly different from that under conventional methods. Pulsed corona is very uniform and well distributed along discharge wires while the corona under conventional
methods is spotty and randomly changes locations along the wire. Further, the radius of corona glow during
pulsed energization is much larger than the conventional corona glow radius.Thus, pulsed corona is more
likely to result in improved corona current distribution in the precipitators. - In summary, the extremely high instantaneous ion densities, high ionic space charge and the uniformity of
corona current distribution will act together during pulse energization to result in particle charge magnitude
superior to those found in conventional energization methods.
CONCLUSIONS (a) EffectofPulse Voltage
It is concluded that increased pulse voltages result in higher field strengths and lead to better particle
charging during each pulse. It is likely that the ion density per pulse is also higher. Thus, pulse voltages
should be increased as much as possible for a precipitator configuration so as to maximize particle charging.
Increasing the pulse voltage does not increase the average current significantly.
(b) Effect of Pulse Frequency
For a given pulse voltage, the ion density per second can be increased in almost linear proportion by
increasing the frequency of the pulses. This leads to higher average current. Since average current on the
plates is crucial for the onset of back-corona for high resistivity dusts, pulse frequency should be carefully
controiled to keep the average current always under the critical current density required to trigger
back-corona.
(c) EffectofPulse Width
The pulse width is composed of pulse rise time and pulse decay time. It is believed that pulse rise time is
responsible for ion and electron generation, while pulse decay time can provide high field strength
conditions for particle charging. The shorter the pulse rise time, the higher can be the precipitator sparking
voltage and hence higher particle charging. Increase in pulse decay time can also increase particle charging,
in that particles car; get charged under a longer period of high field strength. However, there is a limit for
increasing the pulse decay time. Longer decay time approximates DC operation and hence lower sparking
voltages will result. Increasing the rise time, will also lead to the same result and wil not be effective for
charging.
(d) Effect of Base Voltage
The base voltage should be operated below normal breakdown voltage (possibly below corona starting voltage) for high resistivity dust collection. it is known that DC corona is a non-uniform corona discharge,
and, hence, for high resistivity application back-corona could be triggered by the combination of DC corona
and pulses. It is believed that the base voltage will perform the particle collection function and help in rapid
expansion of the pulse generated ion-cloud to the collecting plate, leading to a uniform current distribution.
(e) Optimizing Precipitator Performance On the basis of the foregoing, a precipitator may be optimized by using suitable discharge and collecting
electrode configurations that will increase the DC corona starting voltage so as to operate at higher
collecting fields. The precipitator should be operated with the base voltage near or below the corona starting
voltage. The pulse voltage should be increased to the highest practically feasible value. Pulse width and
frequency should then be adjusted for a given precipitator to operate at its optimum performance.
For particles of moderate resistivity, it will be possible to make use of the pulsed energization concept by
increasing the base voltage to values higher than its corona-starting voltage since back-corona will not be a
problem. The pulse voltage could then be adjusted, along with the pulse frequency and pulse width, to
optimize the precipitator performance.
It was previously mentioned that in most installations where precipitator has multiple ducts, the discharge electrodes will be connected in parallel, but that in some cases a folded transmission line may be used as the discharge electrodes. Such a folded transmission line is illustrated in Figure 3.
In Figure 3, four collecting plates 21-24 are seen forming a lane for gas flow between each pair of collecting plates. The four plates 21-24 seen in Figure 3 are merely illustrative of a larger number of plates and a larger number of lanes which might be employed. Suspended in each lane between the collecting plates 21-24 are discharge wire electrodes 32-35. The gas flow is in the direction indicated by the arrow in Figure 3.
Thus, the gas flow is parallel to the sidewalls of the collecting plates and transverse to the discharge electrodes 32-35. Each of the corresponding discharge wire electrodes in each lane are tied together, either at the bottom or at the top, to form a continuous folded transmission line, as illustrated in Figure 3. A pulse input applied at 36 will be transmitted to all the discharge electrodes as in a folded transmission line. The advantage of the use of a transmission line for the transfer of pulse voltage is that the pulse voltages may be less affected by precipitator capacitance and hense less affected by the size of the precipitator. Thus, it may be easier to control the wave shape of the pulse.
Claims (5)
1. A method of operating a multiple section precipitator for the collection of high resistivity dust, said precipitator having at least three sections, each section having discharge electrodes comprised of wires having diameters of from 0.109 to 0.250 inches (0.277 to 0.635 cm) said wire electrodes being spaced from 31/2 to 51/2 inches (8.89 to 13.97 cm) apart, each section having collecting plates spaced 9 inches (22.86 cm) apart, the spacing from each electrode to a collecting plate being 4.5 inches (11 .43 cm), the collecting plates of each section having a total area of at least 8200 square feet (761 square metres) said method comprising the steps of::
a. applying a DC base voltage in the 30-50 kilovolts range between the discharge electrodes and the
collection plates;
b. setting said DC base voltage to have a value near to but just below the corona starting voltage and
such that the resultant electric field is within the range 3.0-7-5 kilovolts per inch (1.18-2.95 kv/cm);
c. applying in parallel, to the discharge electrodes of at least one but not more than the first two sections;
short pulse voltages in the 50-80 kilovolts range, said pulses being of the same polarity as said DC base
voltage, said pulses being applied at a pulse repetition rate in the range of 80-200 pulses per second;
d. setting said pulse voltages plus DC base voltage to have a peak above the normal DC breakdown level;;
e. setting said pulse voltages to have a fast rise time not greater than 200 nanoseconds and a short decay
time, said pulse having a width of from 250 to 1500 nanoseconds, to avoid excessive sparking;
f. adjusting said DC base voltage in coordination with adjustment of said applied voltage pulses to vary
the charging and collecting fields independently of each other and to maintain an average current
through the collected dust layer just below or at that value which would cause electrical breakdown of
the dust layer.
2. The method according to Claim 1 wherein the first two sections of the multiple section precipitator are pulsed by separate pulsers.
3. The method according to Claim 1 or 2 wherein the pulse voltage rise time is of the order of 100 nanoseconds.
4. The method according to Claim 1, 2 or 3, wherein the average precipitator current through the collected dust layer is between 5 and 10 millamperes per thousand square feet (5.3 to 10.8 ma/100m2)of collecting surface.
5. A method of operating a multiple section precipitator for the collection of high resistivity dust, substantially as herein described with reference to the accompanying drawings.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB8003569A GB2068659B (en) | 1980-02-02 | 1980-02-02 | Control of electrostatic precipitators |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB8003569A GB2068659B (en) | 1980-02-02 | 1980-02-02 | Control of electrostatic precipitators |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| GB2068659A true GB2068659A (en) | 1981-08-12 |
| GB2068659B GB2068659B (en) | 1984-09-19 |
Family
ID=10511084
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB8003569A Expired GB2068659B (en) | 1980-02-02 | 1980-02-02 | Control of electrostatic precipitators |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB2068659B (en) |
Cited By (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2142845A (en) * | 1983-07-06 | 1985-01-30 | Smidth & Co As F L | Electrostatic screen for electrostatic precipitators |
| GB2343387A (en) * | 1998-10-20 | 2000-05-10 | Jeffrey Carl Alexander | Electrostatically enhanced gas solid contact apparatus. |
| RU2266161C1 (en) * | 2004-08-09 | 2005-12-20 | Сикорский Владимир Иванович | Electric filter voltage automatic control method |
| EP1652586A1 (en) * | 2004-10-26 | 2006-05-03 | F.L. Smidth Airtech A/S | Pulse generating system for electrostatic precipitator |
| WO2006050546A1 (en) * | 2004-11-09 | 2006-05-18 | Fleck Carl M | Method and filter arrangement for removing soot particles |
| US7527675B2 (en) | 2006-09-13 | 2009-05-05 | United Technologies Corporation | Electrostatic particulate separation system and device |
| WO2009103704A3 (en) * | 2008-02-19 | 2009-11-12 | Commissariat A L'energie Atomique | Device for electrostatic filtering using optimised emissive sites |
| RU2384370C1 (en) * | 2008-11-12 | 2010-03-20 | Владимир Иванович Сикорский | Method for automatic control of filter supply mode |
| GB2450212B (en) * | 2007-06-14 | 2012-04-04 | Babcock & Wilcox Power Generat | Method and systems to facilitate improving electrostatic precipitator performance |
| US9339822B2 (en) | 2013-03-15 | 2016-05-17 | Bruce Edward Scherer | Electrostatic precipitator with adaptive discharge electrode |
| CN119771616A (en) * | 2025-01-06 | 2025-04-08 | 福建龙净环保股份有限公司 | Multi-mode compound pulse generation method, electrostatic precipitator system, equipment and storage medium |
-
1980
- 1980-02-02 GB GB8003569A patent/GB2068659B/en not_active Expired
Cited By (18)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2142845A (en) * | 1983-07-06 | 1985-01-30 | Smidth & Co As F L | Electrostatic screen for electrostatic precipitators |
| GB2343387A (en) * | 1998-10-20 | 2000-05-10 | Jeffrey Carl Alexander | Electrostatically enhanced gas solid contact apparatus. |
| GB2343387B (en) * | 1998-10-20 | 2001-02-28 | Jeffrey Carl Alexander | Electrostatically controlled process for contacting of gases and solid particles |
| RU2266161C1 (en) * | 2004-08-09 | 2005-12-20 | Сикорский Владимир Иванович | Electric filter voltage automatic control method |
| US7547353B2 (en) | 2004-10-26 | 2009-06-16 | F.L. Smidth Airtech A/S | Pulse generating system for electrostatic precipitator |
| WO2006045311A1 (en) * | 2004-10-26 | 2006-05-04 | F.L. Smidth Airtech A/S | Pulse generating system for electrostatic precipitator |
| EP1652586A1 (en) * | 2004-10-26 | 2006-05-03 | F.L. Smidth Airtech A/S | Pulse generating system for electrostatic precipitator |
| WO2006050546A1 (en) * | 2004-11-09 | 2006-05-18 | Fleck Carl M | Method and filter arrangement for removing soot particles |
| US7527675B2 (en) | 2006-09-13 | 2009-05-05 | United Technologies Corporation | Electrostatic particulate separation system and device |
| GB2450212B (en) * | 2007-06-14 | 2012-04-04 | Babcock & Wilcox Power Generat | Method and systems to facilitate improving electrostatic precipitator performance |
| CN101952041A (en) * | 2008-02-19 | 2011-01-19 | 法国原子能及替代能源委员会 | Device for electrostatic filtering using optimised emissive sites |
| JP2011512248A (en) * | 2008-02-19 | 2011-04-21 | コミッサリア ア レネルジー アトミーク エ オ ゼネルジ ザルタナテイヴ | Electrostatic filtering device with optimal emission area |
| WO2009103704A3 (en) * | 2008-02-19 | 2009-11-12 | Commissariat A L'energie Atomique | Device for electrostatic filtering using optimised emissive sites |
| US8518163B2 (en) | 2008-02-19 | 2013-08-27 | Commissariat A L'energie Atomique Et Aux Energies Alternatives | Electrostatic filtering device using optimized emissive sites |
| CN101952041B (en) * | 2008-02-19 | 2014-08-13 | 法国原子能及替代能源委员会 | Device for electrostatic filtering using optimised emissive sites |
| RU2384370C1 (en) * | 2008-11-12 | 2010-03-20 | Владимир Иванович Сикорский | Method for automatic control of filter supply mode |
| US9339822B2 (en) | 2013-03-15 | 2016-05-17 | Bruce Edward Scherer | Electrostatic precipitator with adaptive discharge electrode |
| CN119771616A (en) * | 2025-01-06 | 2025-04-08 | 福建龙净环保股份有限公司 | Multi-mode compound pulse generation method, electrostatic precipitator system, equipment and storage medium |
Also Published As
| Publication number | Publication date |
|---|---|
| GB2068659B (en) | 1984-09-19 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PCNP | Patent ceased through non-payment of renewal fee | ||
| PE20 | Patent expired after termination of 20 years |
Effective date: 20000324 |