GB2213477A - Process for producing carbon black - Google Patents
Process for producing carbon black Download PDFInfo
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- GB2213477A GB2213477A GB8828651A GB8828651A GB2213477A GB 2213477 A GB2213477 A GB 2213477A GB 8828651 A GB8828651 A GB 8828651A GB 8828651 A GB8828651 A GB 8828651A GB 2213477 A GB2213477 A GB 2213477A
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- feedstock
- carbon black
- gas stream
- combustion gas
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- C—CHEMISTRY; METALLURGY
- C09—DYES; PAINTS; POLISHES; NATURAL RESINS; ADHESIVES; COMPOSITIONS NOT OTHERWISE PROVIDED FOR; APPLICATIONS OF MATERIALS NOT OTHERWISE PROVIDED FOR
- C09C—TREATMENT OF INORGANIC MATERIALS, OTHER THAN FIBROUS FILLERS, TO ENHANCE THEIR PIGMENTING OR FILLING PROPERTIES ; PREPARATION OF CARBON BLACK ; PREPARATION OF INORGANIC MATERIALS WHICH ARE NO SINGLE CHEMICAL COMPOUNDS AND WHICH ARE MAINLY USED AS PIGMENTS OR FILLERS
- C09C1/00—Treatment of specific inorganic materials other than fibrous fillers; Preparation of carbon black
- C09C1/44—Carbon
- C09C1/48—Carbon black
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- C—CHEMISTRY; METALLURGY
- C09—DYES; PAINTS; POLISHES; NATURAL RESINS; ADHESIVES; COMPOSITIONS NOT OTHERWISE PROVIDED FOR; APPLICATIONS OF MATERIALS NOT OTHERWISE PROVIDED FOR
- C09C—TREATMENT OF INORGANIC MATERIALS, OTHER THAN FIBROUS FILLERS, TO ENHANCE THEIR PIGMENTING OR FILLING PROPERTIES ; PREPARATION OF CARBON BLACK ; PREPARATION OF INORGANIC MATERIALS WHICH ARE NO SINGLE CHEMICAL COMPOUNDS AND WHICH ARE MAINLY USED AS PIGMENTS OR FILLERS
- C09C1/00—Treatment of specific inorganic materials other than fibrous fillers; Preparation of carbon black
- C09C1/44—Carbon
- C09C1/48—Carbon black
- C09C1/50—Furnace black ; Preparation thereof
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- Chemical & Material Sciences (AREA)
- Organic Chemistry (AREA)
- Pigments, Carbon Blacks, Or Wood Stains (AREA)
Description
2.2' 13 4 7 7 11 Process for Producing Carbon Black Backimund of the
Invention Carbon black is produced by the incomplete combustion of a hydrocarbon such as petroleum, natural gas and other well-known materials at high temperatures. When separated from the reaction gases, the product is a fluffy, carbon black powder.
In a typical furnace process for the production of carbon black, a fuel and an oxidant such as air are reacted to provide a stream of hot combustion gases. A hydrocarbon feedstock is injected into the stream of hot combustion gases resulting in the formation of carbon black. The temperature of the carbon black containing gas stream is then lowered by quenching with any conventional means such as a water spray. The black is separated from the stream of gases in which it is suspended by known techniques, such as by cyclones and filters; and then pelletized and dried.
Carbon black is incorporated into rubber compounds in order to impart reinforcement properties to the rubber compound. Among the many properties of carbon black which are important to the rubber industry is the aggregate size distribution of the carbon black. The rubber industry has found that for certain purposes blacks having wide aggregate size distribution are highly desirable.
Accordingly, an object of the present invention is to provide a process for producing carbon blacks having a wider aggregate size distribution as measured by an increase in the A D50 values of the blacks.
Summary of the Invention
The process of the present invention involves injecting liquid feedstock in the form of non-preatomized coherent streams or preaton-dzed streams into a staged (modular) carbon black forn-ting process at two separate locations. A portion of the feedstock is injected prior to the combustion gas stream having reached maximum velocity at a point upstream of which no further 2 increase in the crushed DBP structure of the carbon black caused by injecting feedstock in the hot combustion gas stream prior to the point at which the combustion gas stream has reached maximum velocity is observed, and also where an increase in the width of the aggregate size distribution of the carbon black is achieved. The remainder of the feedstock is injected at the point where the combustion gas stream has reached maximum velocity.
While U.S. Patent Application Serial No. 626,704 filed July 2,1984 teaches that the crashed DBP structure of a carbon black can be increased by injecting liquid feedstock into a combustion gas stream at a point where maximum velocity of the combustion gas stream is reached and at a point prior to that where the maximum velocity of the combustion gas stream is reached, there is no suggestion that the crushed DBP structure of the blacks produced by this process would not increase infinitely as the distance between feedstock injection points increases.
Brief Description of the Drawino
Figure 1 is a schematic, diagrarnmAc, longitudinal, sectional view of a typical carbon black-producing furnace which was utilized in all of the Examples of the present application.
Figure 2 is a histogram showing a size distribution curve of carbon black aggregates and illustrating the A D5O of the aggregate size distribution of a sample of carbon black.
Detailed Description of the Invention
Referring to Figure 1, there is shown a furnace 1 which is illustrative of the furnaces used to prepare carbon black using the process of the present invention. Furnace 1 is comprised generally of four zones, namely, a mixing chamber 3, a combustion zone 10, a transition zone 13, and a reaction zone 31.
Mixing chamber 3 is defined by wall 4, the outer side of interior partition 9 and upstream wall 6. Attached to the inner side of partition 9 at the upstream end of the partition is flame holder 11. Combustion chamber 10 is defined by the inner side of partition 9, the downstream side of flame holder 11 and terminates at downstream point 12. Through wall 6 is inserted conduit 8 through which fuel is introduced into mixing chamber 3. Through sidewall 4 is inserted conduit 5 through which an oxidant is introduced into chamber 3. Through conduit 8 is inserted internal probe 19 through which feedstock may be injected into the furnace prior to the point where the hot combustion gas stream reaches maximum velocity and at the point where no increase in CDBP structure of the resultant black caused by injecting feedstock into the hot combustion gas stream prior to the point at which the hot combustion gas stream has reached maximum velocity is observed. Injection probe 19 is an axially aligned probe which may be liquid-cooled and which terminates in end cap 27. End cap 27 t c>, 3 has a plurality of orifices 29 oriented radially about the circumference thereof. Downstream from corn bustion chamber 10 is transition zone 13 which is defined by wall 17. Circurnferentially located around wall 17 are a plurality of substantially transversely oriented orifices 21 through which feedstock may be injected into zone 13.
Downstream from transition zone 13 is reaction zone 31 which is defined by wall 37. Zone 31 can be of variable length and cross-sectional area depending upon the reaction conditions desired. In tl-ds instance reaction zone 31 has an internal diameter of 36 inches. Quench probe 41 is inserted into reaction zone 31 through wall 37. Water is injected through quench probe 41 into reaction zone 31 to terminate the carbon black forn-ting reaction.
In general, the process of the present invention for producing blacks having a wider aggregate size distribution is achieved as follows. Into the n-dxing chamber of the furnace there is introduced through a fuel conduit a suitable fuel and through an oxidant conduit a suitable oxidant such as air, oxygen, n-dxtures of air and oxygen, or the like. Among the fuels suitable for use in the reaction with the oxidant stream in the combustion chamber to generate the hot combustion gases are included any readily combustible matter whether in gaseous, vaporous or liquid form such as hydrogen, carbon monoxide, methane, acetylene, alcohols, kerosene, liquid hydrocarbon fuels and the like.
As referred to herein, the primary combustion represents the amount of oxidant in the first stage of the modular process divided by the amount of oxidant theoretically required for the complete combustion of the fuel present in the first stage of the process to form carbon dioxide and water, multiplied by 100 to give a percentage. While the primary combustion may range from 100 to 500%, the prefer-red primary or first stage combustion may vary from about 120 to about 300%. In this manner there is generated a stream of hot combustion gases flowing at a high linear velocity. It has furthermore been found that a pressure differential between the combustion cliz.mber and the reaction chan-Lber of at least 1.0 p.s.i. (6.9 kPa) and preferably about 1.5 p.s.i. (10.3 kPa) to 10 p.s.i. (69 kPa) is desirable. Under these conditions, there is produced a stream of gaseous combustion products possessing sufficient energy to convert a carbon black-yielding liquid hydrocarbonaceous feedstock into the desired carbon black products. The resultant combustion gases emanating from the combustion stage attain a temperature of at least about 24000 F, (13500 C) with the most preferred temperature being at least above about 300C)OF (16500 Q.
The hot combustion gases are propelled in a downstream direction and are discharged from the downstream end of the combustion chamber at a high linear velocity which is accelerated by passing the combustion gases into an enclosed transition zone of smaller diameter which may, if desired, be tapered or restricted, At approximately the n-dd-point of the transition zone in the furnace the combustion gas stream reaches ma)dmum velc>dty.
According to the process of the present invention, an amount of liquid feedstock ranging from 4 about 20 to about 80%, and preferably from about 25 to about 75% of the total amount of the liquid hydrocarbonaceous feedstock required is injected in the form of non-preaton-dzed coherent streams or preaton-dzed streams, preferably non-preatornized coherent streams, substantial]), transversely, in a direction outwardly or inwardly, into the combustion gas stream from the periphery thereof prior to the point where maximum velocity of the combustion gas stream is reached and at a point upstream of wl-dch no further increase in crushed DBP structure caused by injecting a portion of the feedstock into the hot combustion gas stream prior to the point at which the combustion gas stream has reached max:imurn velocity is observed and where a wider aggregate size distribution is obtained. When the liquid feedstock is injected transversely outwardly into the hot combustion gas stream prior to the stream having reached maximum velocity, the feedstock is preferably injected through a feedstock injection probe. At the point where the combustion gas stream has reached maximum velocity, the remaining amount of the liquid hydrocarbon feedstock ranging from about 20 to about 80% of the total hydrocarbon feedstock, and preferably an amount ranging from about 25 to about 75%, of the total feedstock is injected. At this point the liquid feedstock is injected in the form of a plurality of nonpreaton-tized coherent streams or preatornized streams, preferably nonprealon-tized, into the hot combustion gas stream in a direction substantially radial or transverse to the flow of the combustion gas stream either from the outer or inner periphery of the combustion gas stream. In a preferred embodiment of the process, the feedstock is injected at the point where the combustion gas stream has reached maximum velocity through a plurality of transversely oriented orifices within the wall of the transition zone of the furnace in a direction radially inwardly to the flow of the combustion gas stream. Suitable for use herein as hydrocarbon feedstocks are unsaturated hydrocarbons such as acetylene, olefins such as ethylene, propylene, butylene, aromatics such as benzene, toluene, xylene, certain saturated hydrocarbons and volatilized hydrocarbons such as kerosenes, naphthalenes, terpenes, ethylene tars, aromatic cycle stocks and the like. With respect to the above injections of feedstock at the defined locations, the feedstock may be the same or different.
The amounts of feedstock, fuel, and/or oxidant employed herein will be adjusted so as to result in an overall percent combustion ranging from about 15 to about 60 percent and preferably from about 15 to about 40 percent. The overall combustion represents the total amount of oxidant used in the carbon forn-dng process divided by the amount of oxidant required for the complete combustion of the total amount of fuel and feedstock present in the carbon forming process so as to yield carbon dioxide and water, multiplied by 100 in order to arrive at a percentage.
Sufficient residence time is provided to allow the carbon black forn-drig reactions to occur prior to termination of the reaction by quenching. An exemplary manner of quenching is accomplished by injecting water through a quench nozzle. However, there are many other methods known in the art for fl, quenching the carbon black forn-dng process. The hot effluent gases containing the carbon black products suspended therein are then subjected to the conventional steps of cooling, separation and collection of carbon black. The separation of the carbon black from the gas stream is readily accomplished by any conventional means such as a precipitator, cyclone separator, bag filter, or combination thereof.
It has been found that by injecting feedstock at the two locations in accordance with the process of the present invention, blacks having wider aggregate size distribution are produced.
The following test procedures are used in detem-dning the analy6cal properties of the blacks produced by the present invention.
IODNE ADSO=\1 NUMBER The iodine adsorption number of a carbon black sample is determined in accordance with ASTM D-1510-81.
1INT STRENGTH The tint strength of a carbon black sample is detern-dned relative to an industry tint reference black in accordance with ASTM D-3265-76a.
DIBUTYL PHTHALATE MBM ABSORIMON The DBP absorption number of a carbon black is determined in accordance with ASTM D 2414-84. The results reported indicate whether the carbon black is in fluffy or pellet form.
CRUliED DBP ABSORMON NUMBER (CDBP) The CDBP absorption number of a carbon black pellet is deterrnined in accordance with ASTM D-3493-84.
6 AGGREGATE SIZE DISTRIBUTION (A D 50) The aggregate size distribution (A D 50) of a sample of carbon black is determined in the following manner. A histogram is made of the Stokes diameter of the aggregates of the carbon black sample versus the relative frequency of their c>ccurence in a given sample. As shown in Figure 2, a line (B) is drawn from the peak (A) of the histogram in a direction parallel to the Y axis to and ending at the X-axis at point (C) of the histogrant The midpoint (F) of the resultant line (B) is determined and a line (G) is drawn through the n-ddpoint (F) thereof parallel to the X-aAs. Line (G) intersects the distribution curve of the histogram at two points D and E. The absolute value of the difference of the two Stokes diameters of the carbon black particles at points D and E is the A D 50 value. The data used to generate the histogram are determined by the use of a disk centrifuge such as one manufactured by Joyce L4>ebl Co. Ltd. of Tyne and Wear, United Kingdom. The following procedure is a modification of the procedure described in the instruction manual of the Joyce Loebl disk centrifuge file reference DCF 4.008 published on February 1, 1985, the teachings of which are hereby incorporated by reference, and was used in determining the data.
PROCEDURE mg of a carbon black sample are weighed in a weighing vessel. 3 drops of a surfactant produced and sold by the Shell Chen-dcal Co. under the registered trademark NONTIDET P-40 are added to the carbon black and the resultant mixture is stirred to produce a uniform paste. 50 cc of a solution of 20% absolute ethanol and 80% distilled water are added to the paste and dispersed by means of ultrasonic energy for 15 minutes using a sonifier having the Model No. W385 manufactured by Heat Systems Ultrasonics Inc. Farmingdale New York.
Prior to the the run, the following data are entered into the computer which records the data from the disk centrifuge:
1. The specific gravity of carbon black, taken as 1.86g/cc, 2. The volume of the solution of the carbon black dispersed in the above solution of water and ethanol, which in this instance is 0.5 cc, 3. The volume of spin fluid wl-dch, in this instance, is 14 cc of water, 4. The viscosity of the spin fluid which in Eds instance is taken as 0. 933 centipoise at 230 C, 7 c 5. The density of the spin fluid which, in this instance, is 0.9975 g/cc at 230 6. The disk speed which, in this instance, is 8,000 rpm, 7. The data sampling interval which,.in this instance, is 1 second.
C, The disk centrifuge is operated at 8000 rpm while the stroboscope Is operating. 14 cc of distilled water are injected into the spinning disk as the spin fluid. The turbidity level is set to 0; and Icc of the solution of 20% absolute ethanol and 80% distilled water is injected as a buffer liquid. The cut and boost buttons of the disk centrifuge are then operated to produce a smooth concentration gradient between the spin fluid and the buffer liquid and the gradient is monitored visually. When the gradient becomes smooth such that there is no distinguishable boundary between the two fluids, 0.5 cc of the dispersed carbon black in aqueous ethanol solution is injected into the spinning disk and data collection is started immediately. If streaming occurs the run is aborted. The disk is spun for 20 nlinutes following the injection of the dispersed carbon black in aqueous ethanol solution. Following the 20 minutes of spinning, tile disk is stopped, the temperature of the spin fluid is measured, and the average of the temperature of the spin fluid measured at the beginning of the run and the temperature of the spin fluid measured at the end of the run is entered into the computer which records the data from the disk centrifuge. The data is analyzed according to the standard Stokes equation and presented as a histogram as shown in Figure 2.
1 The process of die present invention for producing carbon black having wider aggregate size distribution will be more readily understood by reference to the following examples. There are, of course, many other embodiments of this invention which will become obvious to one skilled in the art once the invention has been fully disclosed and it will accordingly be recognized that the following examples are given for the purpose of illustration only, and are not to be construed as limiting the scope of this invention in any way.
The furnace depicted in Figure 1 is illustrative of the furnaces used in each of the following examples. In examples 1-3 the same liquid hydrocarbon was utilized as a fuel. Furthermore, in examples 1-3 a liquid hydrocarbon different from that used as the fuel was utilized throughout as the feedstock.
1 8 Example 1
Utilizing the furnace shown in Figure 1, there was introduced into mixing chamber 3 air preheated to a temperature of 1238"F (670rC) at a rate of 500 rnscfh (3.933 NM3/sec) and liquid hydrocarbon fuel at a rate of 238 gal/hr (900 L/h). A stream of hot combustion gases were generated therefrom having a 154% primary combustion flowing in a downstream direction at a high linear velocity. Potassium was added to the combustion gases in the form of an aqueous solution such that 84 ppm of potassium was added relative to the total amount of feedstock which was used.
Subsequently, 25% of the total feedstock was introduced in the form of non-preatomized coherent liquid streams radially outwardly into the hot combustion gas stream through probe 19 prior to the point where the combustion gas stream reached maximum velocity. Probe 19 had an outside diameter of 2 inches (5.1 cm) and was equipped with a 1/4 inch NPT end cap 27 having six 0.070 inch (1.78 mm) diameter orifices perpendicularly oriented and located equiangularly about the circumference th6reof. In this example, probe 19 was positioned such that end cap 27 was 11.8 inches (30 cm) upstream of orifices 21.
The remaining 75% of the feedstock was injected radially inwardly in the form of non-preatomized coherent streams into the hot combustion gas stream through 12 orifices 21 at the point where the combustion gases had reached maximum velocity i.e., at the rr-dd-point of transition zone 13. Transition zone 13 has a length of 11 inches (27.9 cm) and an internal diameter of 12.4 inches (31.5 cm). Orifices 21 were transversely oriented, each 0.078 inches (1.99 mm) in diameter and spaced equiangularly in a single plane about the circumference of wall 17 of transition zone 13. The total amount of feedstock was injected at a combined rate of 1437 gal/hr (5439 L/h).
Me process was carried out such that the overall combustion was 20.5%. Reaction chamber 31 was 36 inches, (91 cm) in diameter. Quench nozzle 41 was located at a point about 10 feet (2.45 m) downstream from orifices 21. The analytical properties of the black are reported in the Table.
Example 2
Carbon black was produced using the apparatus, feedstock and process o f Example 1 -Arith the following exceptions. In this example, probe 19 was positioned such that end cap 27 was 19.7 inches (50 cm) upstream of orifices 21 within transition zone 13 and 123 ppm of potassium relative to the total amount of feedstock utilized was added in the form of an aqueous solution to the hot combustion gas strearn. The analytical properties of the black are reported in the Table.
9 9 1-1 Carbon black was produced using the apparatus, feedstock and process of Example 1 with the following exceptions. Internal probe 19 was positioned such that end cap 27 was 23.6 inches (60 cm) upstream of orifices 21 and 123 pprn of potassium relative to the total amount of feedstock utilized was added in the form of an aqueous solution to the hot combustion gas stream.The analytical properties of the black are reported in the Table.
Table
ANALY1ICALPROPER= EMMple 1 g2m le 2 Emn2ple3 Potassium Addition Relative to Amount of Feedstock 84 123 123 Separation Distance of Feedstock Injection Points.
11.8 inches 19.7 inches 23.6 inches (30 cm) (50 cm) (60 cm) AD 50mu 68 77 83 Tinting Strength% 98 98 96 Iodine No.
MgI.)/gbIack 60 60 59 DBP Absorption Pellets cc/100 g 109 106 107 CDBP (24M4) 5r,1100 a 90 88 90 The data in the Table shows that the process of the present invention results in the production of carbon blacks having increased A D5O values while maintaining substantially J 4 7 11 identical values for structure and surface areas. Furthermore, from the data and the examples one would conclude that the A D50 value of a carbon black could be further increased as the distance between the two points of feedstock injection of this invention is increased.
In examples 1-3, different amounts of potassium were added in order to achieve a given level of structure of the carbon black. In so doing the effect of the present invention is shown indirectly by noting that equal amounts of potassium were required in examples 2 and 3, both of which exceeded the amount required in example 1 in order to reach the given structure level of the carbon black. 77he increase in the amount of potassium used in examples 2 and 3 compared to that used in example 1 shoivs that at the separation distance of example I the stnicture was still increasing with respect to the increasing distance between feedstock injection points, ai further increasing the separation distance between feedstock injection points, the constant amounts of potassium utilized in examples 2 and 3 show that there has been no further Increase In CDBP caused by injection of the portion of feedstock into the hot combustion gases prior to reaching maximum velocity at the ncreasing distances between feedstock Injection in eamples 2 and 3.
12 Qain-ts 1. In a modular process for producing furnace carbon blacks wherein a fuel and an oxidant are reacted so as to provide a stream of hot primary combustion gases possessing sufficient energy to convert a carbon black yielding liquid hydrocarbon feedstock to carbon black, and wherein liquid hydrocarbon feedstock is peripherally injected, in the form of a plurality of non-preatomized coherent streams or preatomized streams, into the stream of gaseous combustion products at a point where the combustion gas stream has reached maximum velocity in a direction substantially transverse to the direction of flow of the stream of combustion gases and under sufficient pressure to achieve a degree of penetration required fQr proper shearing and mixing of the feedstock, and wherein the feedstock is decomposed and converted into carbon black prior to termination of the carbon forn-drig reaction by quenching, and then cooling, separating and recovering the resultant carbon black, the improvement wMch comprises introducing a sufficient portion of the total amount of liquid hydrocarbon feedstock into the combustion gas stream prior to the point at which the stream of combustion gases reaches n- Laximum velocity and at a point upstream of wWch no further increase of the CDBP of the resultant carbon black caused by injecting feedstock into the hot combustion gas stream prior to the point at which the combustion gas stream has reached maximum velocity is observed to thereby produce carbon blacks having wider aggregate size distribution.
2. A process as defined in claim 1 wherein an amount of from about 20 to about 800/c of the total amount of liquid feedstock is injected into the combustion gas stream prior to the point where maximum velocity of the combustion gas stream is reached and upstream of which no further increase of the CDBP of the resultant carbon black caused by injecting feedstock into the hot combustion gas stream prior to the point at which the combustion gas stream has reached maximum velocity is observed, with the remainder of the feedstock being added at the point where the combustion gas stream has reached maximum velocity.
3. A process as defined in claim 1 wherein an amount of from about 25 to about 75% of the total amount of liquid feedstock is injected into the combustion gas stream prior to the point where maximum velocity of the combustion gas stream is reached and upstream of which no further increase in 0 13 the CDBP of the resultant carbon black caused by injecting feedstock into the hot combustion gas stream prior to the point at which the combustion gas stream has reached maximum velocity is observed, with the remainder of the feedstock being added at the point where the combustion gas stream has reached maximum velocity.
4. A process as defined in claim 1 wherein the feedstock which is injected into the hot combustion gas stream at the point where the hot combustion gas stream has reached maximum velocity is in the form of nonpreatornized, coherent streams.
5. A process as defined in claim 1 wherein the liquid hydr0carbon feedstock which is injected into the stream of hot combustion gases prior to the point at which the stream of combustion gases has reached maximum velocity and upstream of which no further increase in the CDBP of the resultant carbon black caused by injecting feedstock into the hot combustion gas stream prior to the point at which the combustion gas stream has reached maximurn velocity is observed, is injected in a substantially transverse direction to the flow of the hot combustion gas stream and the feedstock is in the form of non-preatornized coherent streams.
6. A process as defined in claim 5 wherein the liquid hydrocarbon feedstock which is injected into the stream of hot combustion gases prior to the point at which the stream of combustion gases has reached nuiximum velocity and upstream of which no further increase in the CD13P of the resultant carbon black caused by injecting feedstock into the hot combustion gas stream prior to the point at which the combustion gas stream has reached maximum velocity is observed, is injected outwardly from the inner periphery of the hot combustion gas stream.
7. A process as defined in claim I wherein the liquid hydrocarbon feedstock is injected in the form of non-preaton-dzed coherent streams in a substantially transverse direction outwardly from the inner periphery of the combustion gas stream into the stream of combustion gases prior to the point at which the stream of combustion gases has reached maximum velocity and upstream of which no further increase in the CDBP of the resultant carbon black caused by injecting feedstock into the hot combustion gas stream prior to the point at which the combustion gas stream has reached maximum velocity is observed, and the liquid hydrocarbon feedstock is injected in the form of non-preatornized coherent streams in a substantially transverse direction inwardly from the outer periphery of the hot combustion gas stream into the combustion gas stream at the point where maximum velocity of the combustion gas stream is reached.
cl Published 1989 at The Patent Office, State House. 6671 High Holborn, London WC1R 4TP. Further copies maybe obtained from The PateatOfftce Sales Branch, St Mary Cray, Orpington- Kent BR5 3RD Printed by Multiplex techniques ltd, St Mary Cray, Kent, Cori. 1/87
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
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US13086187A | 1987-12-10 | 1987-12-10 |
Publications (3)
Publication Number | Publication Date |
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GB8828651D0 GB8828651D0 (en) | 1989-01-11 |
GB2213477A true GB2213477A (en) | 1989-08-16 |
GB2213477B GB2213477B (en) | 1991-11-13 |
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GB8828651A Expired - Fee Related GB2213477B (en) | 1987-12-10 | 1988-12-08 | Process for producing carbonblack |
Country Status (18)
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JP (1) | JP2582879B2 (en) |
KR (1) | KR920002625B1 (en) |
CN (1) | CN1035671A (en) |
AR (1) | AR245762A1 (en) |
AU (1) | AU591618B2 (en) |
BR (1) | BR8806415A (en) |
CA (1) | CA1336475C (en) |
DE (1) | DE3841285A1 (en) |
ES (1) | ES2010042A6 (en) |
FR (1) | FR2624517B1 (en) |
GB (1) | GB2213477B (en) |
IN (1) | IN171963B (en) |
IT (1) | IT1227512B (en) |
MX (1) | MX169842B (en) |
MY (1) | MY107373A (en) |
NL (1) | NL8803035A (en) |
PT (1) | PT89184B (en) |
TR (1) | TR23831A (en) |
Cited By (1)
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US20220018537A1 (en) * | 2016-10-10 | 2022-01-20 | King Abdullah University Of Science And Technology | Burners for conversion of methane to olefins, aromatics, and nanoparticles |
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JP2889326B2 (en) * | 1989-09-14 | 1999-05-10 | 昭和キャボット株式会社 | Carbon black and rubber composition |
US5236992A (en) * | 1991-11-18 | 1993-08-17 | Cabot Corporation | Carbon blacks and their use in rubber applications |
DE10336575A1 (en) * | 2003-08-08 | 2005-03-10 | Degussa | soot |
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US3952087A (en) * | 1974-09-13 | 1976-04-20 | Cabot Corporation | Production of high structure carbon blacks |
US4018878A (en) * | 1975-12-29 | 1977-04-19 | Ashland Oil, Inc. | Process for producing carbon black |
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US4315902A (en) * | 1980-02-07 | 1982-02-16 | Phillips Petroleum Company | Method for producing carbon black |
JPS5717422A (en) * | 1980-07-04 | 1982-01-29 | Dow Chemical Co | Removal of chlorate in caustic solution by electrodeposition iron |
DE3443872A1 (en) * | 1983-12-23 | 1985-07-04 | Cabot Corp., Boston, Mass. | METHOD FOR THE PRODUCTION OF FURNACE RUSS |
IN163294B (en) * | 1983-12-23 | 1988-09-03 | Cabot Corp | |
CA1300342C (en) * | 1985-06-24 | 1992-05-12 | E. Webb Henderson | Process and apparatus for producing carbon black |
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1988
- 1988-08-18 IN IN589/MAS/88A patent/IN171963B/en unknown
- 1988-09-29 MX MX013218A patent/MX169842B/en unknown
- 1988-12-06 CA CA000585090A patent/CA1336475C/en not_active Expired - Fee Related
- 1988-12-06 IT IT8822880A patent/IT1227512B/en active
- 1988-12-06 BR BR888806415A patent/BR8806415A/en not_active Application Discontinuation
- 1988-12-07 PT PT89184A patent/PT89184B/en not_active IP Right Cessation
- 1988-12-08 GB GB8828651A patent/GB2213477B/en not_active Expired - Fee Related
- 1988-12-08 TR TR88/0885A patent/TR23831A/en unknown
- 1988-12-08 AU AU26666/88A patent/AU591618B2/en not_active Ceased
- 1988-12-08 DE DE3841285A patent/DE3841285A1/en not_active Withdrawn
- 1988-12-09 AR AR88312676A patent/AR245762A1/en active
- 1988-12-09 MY MYPI88001428A patent/MY107373A/en unknown
- 1988-12-09 JP JP63310261A patent/JP2582879B2/en not_active Expired - Fee Related
- 1988-12-09 NL NL8803035A patent/NL8803035A/en not_active Application Discontinuation
- 1988-12-09 ES ES8803752A patent/ES2010042A6/en not_active Expired
- 1988-12-09 FR FR888816241A patent/FR2624517B1/en not_active Expired - Fee Related
- 1988-12-10 CN CN88108477A patent/CN1035671A/en active Pending
- 1988-12-10 KR KR1019880016491A patent/KR920002625B1/en not_active IP Right Cessation
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US3952087A (en) * | 1974-09-13 | 1976-04-20 | Cabot Corporation | Production of high structure carbon blacks |
US4018878A (en) * | 1975-12-29 | 1977-04-19 | Ashland Oil, Inc. | Process for producing carbon black |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20220018537A1 (en) * | 2016-10-10 | 2022-01-20 | King Abdullah University Of Science And Technology | Burners for conversion of methane to olefins, aromatics, and nanoparticles |
Also Published As
Publication number | Publication date |
---|---|
NL8803035A (en) | 1989-07-03 |
BR8806415A (en) | 1989-08-22 |
PT89184A (en) | 1989-12-29 |
AU591618B2 (en) | 1989-12-07 |
FR2624517A1 (en) | 1989-06-16 |
KR890010129A (en) | 1989-08-07 |
PT89184B (en) | 1994-11-30 |
CN1035671A (en) | 1989-09-20 |
DE3841285A1 (en) | 1989-06-22 |
IN171963B (en) | 1993-02-20 |
IT8822880A0 (en) | 1988-12-06 |
JPH01190760A (en) | 1989-07-31 |
AU2666688A (en) | 1989-06-15 |
CA1336475C (en) | 1995-08-01 |
AR245762A1 (en) | 1994-02-28 |
FR2624517B1 (en) | 1990-08-24 |
GB8828651D0 (en) | 1989-01-11 |
GB2213477B (en) | 1991-11-13 |
IT1227512B (en) | 1991-04-12 |
TR23831A (en) | 1990-09-25 |
ES2010042A6 (en) | 1989-10-16 |
MX169842B (en) | 1993-07-28 |
KR920002625B1 (en) | 1992-03-30 |
JP2582879B2 (en) | 1997-02-19 |
MY107373A (en) | 1995-11-30 |
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Legal Events
Date | Code | Title | Description |
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PCNP | Patent ceased through non-payment of renewal fee |
Effective date: 19961208 |