GB2151604A - Production of carbon black - Google Patents
Production of carbon black Download PDFInfo
- Publication number
- GB2151604A GB2151604A GB08431483A GB8431483A GB2151604A GB 2151604 A GB2151604 A GB 2151604A GB 08431483 A GB08431483 A GB 08431483A GB 8431483 A GB8431483 A GB 8431483A GB 2151604 A GB2151604 A GB 2151604A
- Authority
- GB
- United Kingdom
- Prior art keywords
- gas stream
- combustion gas
- combustion
- feedstock
- stream
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
- 239000006229 carbon black Substances 0.000 title claims abstract description 45
- 238000004519 manufacturing process Methods 0.000 title description 5
- 239000000567 combustion gas Substances 0.000 claims abstract description 86
- 235000019241 carbon black Nutrition 0.000 claims abstract description 44
- 239000007788 liquid Substances 0.000 claims abstract description 34
- 238000000034 method Methods 0.000 claims abstract description 31
- 238000002485 combustion reaction Methods 0.000 claims abstract description 28
- 230000008569 process Effects 0.000 claims abstract description 25
- 229930195733 hydrocarbon Natural products 0.000 claims abstract description 24
- 150000002430 hydrocarbons Chemical class 0.000 claims abstract description 24
- 239000004215 Carbon black (E152) Substances 0.000 claims abstract description 21
- 239000007787 solid Substances 0.000 claims abstract description 19
- LTUJKAYZIMMJEP-UHFFFAOYSA-N 9-[4-(4-carbazol-9-yl-2-methylphenyl)-3-methylphenyl]carbazole Chemical compound C12=CC=CC=C2C2=CC=CC=C2N1C1=CC=C(C=2C(=CC(=CC=2)N2C3=CC=CC=C3C3=CC=CC=C32)C)C(C)=C1 LTUJKAYZIMMJEP-UHFFFAOYSA-N 0.000 claims abstract 2
- 238000006243 chemical reaction Methods 0.000 claims description 21
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 claims description 9
- 229910052799 carbon Inorganic materials 0.000 claims description 9
- 238000010791 quenching Methods 0.000 claims description 8
- 239000000446 fuel Substances 0.000 claims description 7
- 239000007800 oxidant agent Substances 0.000 claims description 7
- 230000001590 oxidative effect Effects 0.000 claims description 7
- 230000000171 quenching effect Effects 0.000 claims description 6
- 230000001427 coherent effect Effects 0.000 claims description 5
- 238000001816 cooling Methods 0.000 claims description 5
- 238000002156 mixing Methods 0.000 claims description 5
- 230000035515 penetration Effects 0.000 claims description 4
- 238000010008 shearing Methods 0.000 claims description 4
- 238000002347 injection Methods 0.000 abstract description 12
- 239000007924 injection Substances 0.000 abstract description 12
- 238000010058 rubber compounding Methods 0.000 abstract description 7
- 230000007704 transition Effects 0.000 description 18
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 description 14
- 239000007789 gas Substances 0.000 description 7
- 239000000047 product Substances 0.000 description 7
- 239000000523 sample Substances 0.000 description 7
- 229920001971 elastomer Polymers 0.000 description 6
- 239000000203 mixture Substances 0.000 description 6
- 239000005060 rubber Substances 0.000 description 6
- 239000003345 natural gas Substances 0.000 description 5
- 230000000704 physical effect Effects 0.000 description 5
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 5
- 238000010521 absorption reaction Methods 0.000 description 4
- 239000003570 air Substances 0.000 description 4
- UHOVQNZJYSORNB-UHFFFAOYSA-N Benzene Chemical compound C1=CC=CC=C1 UHOVQNZJYSORNB-UHFFFAOYSA-N 0.000 description 3
- YXFVVABEGXRONW-UHFFFAOYSA-N Toluene Chemical compound CC1=CC=CC=C1 YXFVVABEGXRONW-UHFFFAOYSA-N 0.000 description 3
- 230000015572 biosynthetic process Effects 0.000 description 3
- 238000009472 formulation Methods 0.000 description 3
- OFBQJSOFQDEBGM-UHFFFAOYSA-N n-pentane Natural products CCCCC OFBQJSOFQDEBGM-UHFFFAOYSA-N 0.000 description 3
- 239000008188 pellet Substances 0.000 description 3
- 229920003051 synthetic elastomer Polymers 0.000 description 3
- 239000005061 synthetic rubber Substances 0.000 description 3
- KAKZBPTYRLMSJV-UHFFFAOYSA-N Butadiene Chemical compound C=CC=C KAKZBPTYRLMSJV-UHFFFAOYSA-N 0.000 description 2
- CURLTUGMZLYLDI-UHFFFAOYSA-N Carbon dioxide Chemical compound O=C=O CURLTUGMZLYLDI-UHFFFAOYSA-N 0.000 description 2
- ATUOYWHBWRKTHZ-UHFFFAOYSA-N Propane Chemical compound CCC ATUOYWHBWRKTHZ-UHFFFAOYSA-N 0.000 description 2
- PPBRXRYQALVLMV-UHFFFAOYSA-N Styrene Chemical compound C=CC1=CC=CC=C1 PPBRXRYQALVLMV-UHFFFAOYSA-N 0.000 description 2
- XLOMVQKBTHCTTD-UHFFFAOYSA-N Zinc monoxide Chemical compound [Zn]=O XLOMVQKBTHCTTD-UHFFFAOYSA-N 0.000 description 2
- HSFWRNGVRCDJHI-UHFFFAOYSA-N alpha-acetylene Natural products C#C HSFWRNGVRCDJHI-UHFFFAOYSA-N 0.000 description 2
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 2
- 239000006227 byproduct Substances 0.000 description 2
- 125000002534 ethynyl group Chemical group [H]C#C* 0.000 description 2
- 238000001125 extrusion Methods 0.000 description 2
- 229910052740 iodine Inorganic materials 0.000 description 2
- 239000011630 iodine Substances 0.000 description 2
- 239000003350 kerosene Substances 0.000 description 2
- 238000005259 measurement Methods 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 239000003921 oil Substances 0.000 description 2
- 239000001301 oxygen Substances 0.000 description 2
- 229910052760 oxygen Inorganic materials 0.000 description 2
- 239000004033 plastic Substances 0.000 description 2
- 229920003023 plastic Polymers 0.000 description 2
- 238000002360 preparation method Methods 0.000 description 2
- 239000012744 reinforcing agent Substances 0.000 description 2
- 239000007921 spray Substances 0.000 description 2
- 239000004636 vulcanized rubber Substances 0.000 description 2
- ZCYVEMRRCGMTRW-UHFFFAOYSA-N 7553-56-2 Chemical compound [I] ZCYVEMRRCGMTRW-UHFFFAOYSA-N 0.000 description 1
- UGFAIRIUMAVXCW-UHFFFAOYSA-N Carbon monoxide Chemical compound [O+]#[C-] UGFAIRIUMAVXCW-UHFFFAOYSA-N 0.000 description 1
- QAHFOPIILNICLA-UHFFFAOYSA-N Diphenamid Chemical compound C=1C=CC=CC=1C(C(=O)N(C)C)C1=CC=CC=C1 QAHFOPIILNICLA-UHFFFAOYSA-N 0.000 description 1
- OTMSDBZUPAUEDD-UHFFFAOYSA-N Ethane Chemical compound CC OTMSDBZUPAUEDD-UHFFFAOYSA-N 0.000 description 1
- VGGSQFUCUMXWEO-UHFFFAOYSA-N Ethene Chemical compound C=C VGGSQFUCUMXWEO-UHFFFAOYSA-N 0.000 description 1
- 239000005977 Ethylene Substances 0.000 description 1
- 244000043261 Hevea brasiliensis Species 0.000 description 1
- CTQNGGLPUBDAKN-UHFFFAOYSA-N O-Xylene Chemical compound CC1=CC=CC=C1C CTQNGGLPUBDAKN-UHFFFAOYSA-N 0.000 description 1
- 235000021355 Stearic acid Nutrition 0.000 description 1
- NINIDFKCEFEMDL-UHFFFAOYSA-N Sulfur Chemical compound [S] NINIDFKCEFEMDL-UHFFFAOYSA-N 0.000 description 1
- 230000009471 action Effects 0.000 description 1
- 239000000654 additive Substances 0.000 description 1
- 150000001298 alcohols Chemical class 0.000 description 1
- 150000001336 alkenes Chemical class 0.000 description 1
- 125000003118 aryl group Chemical group 0.000 description 1
- 239000001273 butane Substances 0.000 description 1
- 229910002092 carbon dioxide Inorganic materials 0.000 description 1
- 239000001569 carbon dioxide Substances 0.000 description 1
- 229910002091 carbon monoxide Inorganic materials 0.000 description 1
- 239000007795 chemical reaction product Substances 0.000 description 1
- 239000000571 coke Substances 0.000 description 1
- 238000007796 conventional method Methods 0.000 description 1
- 238000005336 cracking Methods 0.000 description 1
- 239000006185 dispersion Substances 0.000 description 1
- -1 ethylene, propylene Chemical group 0.000 description 1
- 239000000945 filler Substances 0.000 description 1
- 239000000295 fuel oil Substances 0.000 description 1
- 239000001257 hydrogen Substances 0.000 description 1
- 229910052739 hydrogen Inorganic materials 0.000 description 1
- 125000004435 hydrogen atom Chemical class [H]* 0.000 description 1
- 230000006872 improvement Effects 0.000 description 1
- 239000004615 ingredient Substances 0.000 description 1
- 238000009413 insulation Methods 0.000 description 1
- PNDPGZBMCMUPRI-UHFFFAOYSA-N iodine Chemical compound II PNDPGZBMCMUPRI-UHFFFAOYSA-N 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 229910052751 metal Inorganic materials 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- VUZPPFZMUPKLLV-UHFFFAOYSA-N methane;hydrate Chemical compound C.O VUZPPFZMUPKLLV-UHFFFAOYSA-N 0.000 description 1
- IJDNQMDRQITEOD-UHFFFAOYSA-N n-butane Chemical compound CCCC IJDNQMDRQITEOD-UHFFFAOYSA-N 0.000 description 1
- 150000002790 naphthalenes Chemical class 0.000 description 1
- 229920003052 natural elastomer Polymers 0.000 description 1
- 229920001194 natural rubber Polymers 0.000 description 1
- QIQXTHQIDYTFRH-UHFFFAOYSA-N octadecanoic acid Chemical compound CCCCCCCCCCCCCCCCCC(O)=O QIQXTHQIDYTFRH-UHFFFAOYSA-N 0.000 description 1
- OQCDKBAXFALNLD-UHFFFAOYSA-N octadecanoic acid Natural products CCCCCCCC(C)CCCCCCCCC(O)=O OQCDKBAXFALNLD-UHFFFAOYSA-N 0.000 description 1
- 239000000049 pigment Substances 0.000 description 1
- 229920000642 polymer Polymers 0.000 description 1
- 239000012716 precipitator Substances 0.000 description 1
- 239000001294 propane Substances 0.000 description 1
- 239000000376 reactant Substances 0.000 description 1
- 230000003134 recirculating effect Effects 0.000 description 1
- 238000012552 review Methods 0.000 description 1
- 229930195734 saturated hydrocarbon Natural products 0.000 description 1
- 238000000926 separation method Methods 0.000 description 1
- 238000001179 sorption measurement Methods 0.000 description 1
- 238000005507 spraying Methods 0.000 description 1
- 239000008117 stearic acid Substances 0.000 description 1
- 229910052717 sulfur Inorganic materials 0.000 description 1
- 239000011593 sulfur Substances 0.000 description 1
- 239000011269 tar Substances 0.000 description 1
- 150000003505 terpenes Chemical class 0.000 description 1
- 235000007586 terpenes Nutrition 0.000 description 1
- 238000012360 testing method Methods 0.000 description 1
- 238000012956 testing procedure Methods 0.000 description 1
- 125000000383 tetramethylene group Chemical group [H]C([H])([*:1])C([H])([H])C([H])([H])C([H])([H])[*:2] 0.000 description 1
- 229930195735 unsaturated hydrocarbon Natural products 0.000 description 1
- 238000011144 upstream manufacturing Methods 0.000 description 1
- 239000008096 xylene Substances 0.000 description 1
- 239000011787 zinc oxide Substances 0.000 description 1
Classifications
-
- 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
-
- 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
Landscapes
- Chemical & Material Sciences (AREA)
- Organic Chemistry (AREA)
- Pigments, Carbon Blacks, Or Wood Stains (AREA)
- Production Of Liquid Hydrocarbon Mixture For Refining Petroleum (AREA)
Abstract
This disclosure relates to an improved furnace process for producing carbon blacks by the incomplete combustion of hydrocarbonaceous feedstock by varying the process described in U.S. Reissue Patent No. 28974 by carrying out the injection of a portion of the liquid hydrocarbon feedstock into the combustion gas stream as solid streams substantially radially at a location where the combustion gas stream has not attained maximum velocity whereby the resultant blacks have increased CDBP values and have properties which impart improved hysteresis to rubber formulations in which the blacks are incorporated.
Description
SPECIFICATION
Production of carbon black
This invention relates to the production of furnace blacks having many important applications.
These include use as fillers, pigments, and reinforcing agents in rubber and in plastics.
The furnace process for preparing carbon blacks involves a cracking and/or incomplete combustion of a hydrocarbon feedstock such as natural gas or cycle stock in an enclosed conversion zone at temperatures above 1256"K (1800"F) to produce carbon black. The carbon black entrained in the gases emanating from the conversion zone is then cooled and collected by any suitable means commonly used in the industry. It has, however, been desirable, although difficult, to produce furnace blacks of similar properties capable of imparting improved hysteretic properties to rubber formulations.
Accordingly, the primary object of this invention is to provide a process for preparing carbon blacks which are characterised by having properties indicative of improved hysteresis capabilities and having lower tinting strengths and higher values for crushed DBP (CDBP).
A further object of the invention is to provide a method for controlling the values of the tinting strength and CDBP of carbon blacks.
It has been found that the above objects may be achieved by modifying a modular or staged process for producing carbon black of the type disclosed and claimed in U.S. Reissue Patent
No. 28,974. The staged process consists of an initially prepared primary (first-stage) combustion zone wherein a stream of hot gaseous combustion products is formed; a second or transition zone wherein a liquid hydrocarbon feedstock in the form of solid streams (coherent jets) is injected substantially transversely from the outer or inner periphery of the combustion gas stream into the pre-formed stream of hot gases; and a third zone (the reaction zone) wherein the carbon black formation occurs prior to termination of the reaction by quenching.
In processes of the aforementioned type where feedstock is injected from the outer periphery of the combustion gas stream, there is a possibility for combustion gases to pass through the system without having been utilized. This will occur, for example, when the hydrocarbon feedstock does not completely fill the area through which the combustion gases are flowing, thereby permitting unused heat in the form of combustion gases to escape. There is a greater tendency for this to occur as the size of the reactor is increased. To prevent this uneconomic loss of combustion gases, it is disclosed in U.S. Patent No. 3,922,335 to inject additional feedstock into the interior region of the combustion gas stream where the feedstock injected from the outer periphery of the transition zone would not reach.The patent describes the use of a suitable device such as a probe through which the additional liquid hydrocarbon feedstock would be injected into the core of the combustion gas stream in a substantially transverse manner, and in a direction from the center or core of the combustion gas stream outwardly toward the wall of the reactor. By so doing, it is shown that the combustion gases will be thoroughly utilized for the intended purposes of shearing atomizing, and dispersing the oil droplets. The injection of feedstock into the interior region of the combustion gas stream occurs in the same plane as that from which the feedstock is injected from the outer periphery of the transition zone toward the interior of the combustion gas stream. The process described in U.S.
3,922,335 is shown to provide exceptionally high throughput and high yields, and to have the ability to produce high quality carbon blacks.
There are instances, however, where it is desired to produce carbon blacks in a manner similar to both of the above processes but to produce blacks having different properties. In particular, it may be desirable to produce carbon blacks having reduced tinting strength and increased CDBP, which are indicators of increased rebound and better hysteretic properties.
The modification of the present modular or staged process which makes possible the preparation of the blacks having improved hysteresis involves carrying out the injection of a portion of the liquid hydrocarbon feedstock into the combustion gas stream as solid streams substantially radially at a location where the combustion gas stream has not attained maximum velocity.
Accordingly, therefore, the present invention provides a modular process for producing furnace carbon blacks wherein a fuel and an oxidant are reacted in a first zone so as to provide a stream of hot primary combustion gases possessing sufficient energy to convert a carbon blackyielding liquid hydrocarbon feedstock to carbon black, and wherein in a second zone liquid hydrocarbon feedstock is peripherally injected, in the form of a plurality of solid streams (coherent jets), into the stream of gaseous combustion products at a location 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 the degree of penetration required for proper shearing and mixing of the feedstock and wherein a third zone the feedstock is decomposed and converted into carbon black prior to termination of the carbon forming reaction by quenching, and then cooling, separating and recovering the resultant carbon black, characterised in that a sufficient portion of the total amount of liquid hydrocarbon feedstock is introduced in the form of a plurality of solid streams, substantially radially into the combustion gas stream from the periphery thereof prior to the point at which the stream of combustion gases reaches maximum velocity. to thereby produce carbon blacks having increased CDBP values.
The feedstock may be injected from the outer or inner periphery of the combustion gas stream substantially radially into the lower velocity combustion gas stream.
It is preferred, however, to inject the solid streams of feedstock into the lower velocity combustion gas stream from the inner periphery thereof radially outwardly into the combustion gas stream. In the present staged process. maximum velocity of the combustion gas stream is reached at approximately the mid-point of the transition zone. Thus, for example, when the injection is being made through a probe, the modification can be carried out by retracting the probe into the first or primary combustion zone so that the feed stock, injected radially, whether inwardly or outwardly, enters a combustion gas stream having a lower velocity. The actual point or plane where the feedstock is injected into the lower velocity combustion gas stream in a radial direction may be varied considerably depending upon the specific grade or type of carbon black desired.It is believed that the radially inward or outward injection of the solid streams of liquid feedstock into a lower velocity combustion gas stream results in the formation of coarser size oil droplets which appear to be associated with increased CDBP values.
In the preparation of the hot combustion gases employed in preparing the blacks of the present invention, there are reacted in a suitable combustion chamber a liquid or gaseous fuel and a suitable oxidant stream such as air, oxygen, mixtures of air and oxygen or the like.
Among the fuels suitable for use in reacting with the oxidant stream in the combustion chamber to generate the hot combustion gases are included any of the readily combustible gas, vapor or liquid streams such as hydrogen, carbon monoxide, methane, acetylene. alcohols, and kerosene.
It is generally preferred, however, to utilize fuels having a high content of carbon-containing components and, in particular, hydrocarbons. For example, streams rich in methane such as natural gas and modified or enriched natural gas are excellent fuels as well as other streams containing high amounts of hydrocarbons such as various hydrocarbon gases and liquids and refinery by-products including ethane, propane, butane, and pentane fractions, fuel oils and the like. As referred to herein, the primary combustion represents the amount of oxidant used in the first stage of the modular process relative to the amount of oxidant theoretically required for the complete combustion of the first stage hydrocarbon to form carbon dioxide and water. 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 chamber and the reaction chamber of at least 1.0 p.s.i. (6.9 kPa) and preferably of 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 kinetic energy to atomize a carbon blackyielding liquid hydrocarbonaceous feedstock sufficiently well to produce the desired carbon black products.The resultant combustion gas stream emanating from the primary combustion zone attains a temperature of at least about 2400"F. (1316"C), with the most preferable temperatures being at least above about 3000"F. (1649"C.). The hot combustion gases are propelled in a downstream direction at a high linear velocity which is accelerated by introducing the combustion gases into an enclosed transition stage of smaller diameter which may, if desired, be tapered or restricted such as by means of a conventional venturi throat.
In the present process a portion of the liquid feedstock is injected in the form of a plurality of solid streams from the inner or outer periphery of the combustion gas stream in a substantially radially outward or inward direction into the combustion gases at a point in the process where the combustion gas stream has not yet reached maximum velocity i.e., approximately the midpoint of the transition zone. The remainder of the liquid feedstock is injected in the form of a plurality of solid streams substantially radially at approximately the mid-point of the transition zone into the combustion gases from the outer or inner periphery of the combustion gas stream, with preference for injection from the outer periphery.By means of this technique for injecting the feedstock, the levels of tinting strength and CDBP of the carbon blacks produced are altered in a direction favoring improved hysteresis.
In the second stage of the process, the combustion gases are flowing at high velocity and there exists a gas kinetic head of at least about 1.0 p.s.i. (6.9 kPa). The portion of liquid carbon black-yielding hydrocarbon feedstock which is injected in the form of solid streams into the combustion gases in the transition or second zone, must be injected under sufficient pressure to achieve proper penetration thereby insuring a high rate of mixing and shearing of the hot combustion gases and the liquid hydrocarbon feedstock. The liquid feedstock is injected substantially transversely from the outer or inner periphery of the stream of hot combustion gases in the form of a plurality of solid streams (coherent jets) which penetrate well into the interior region, or core, of the stream of combustion gases.
Suitable for use herein as hydrocarbon feedstocks which are readily volatilizable under the conditions of the reaction are unsaturated hydrocarbons such as acetylene; olefins such as ethylene, propylene and butylene; aromatics such as benzene, toluene and xylene; certain saturated hydrocarbons; and volatilized hydrocarbons such as kerosene, naphthalenes, terpenes, ethylene tars, aromatic cycle stocks and the like.
The third stage of the modular process is a reaction zone which will permit sufficient residence time for the carbon black forming reaction to occur prior to termination of the reaction by quenching. The residence time in each instance depends upon the particular conditions of the process and the particular black desired.
Subsequent to the carbon black forming reaction having proceeded for the desired period of time, the reaction is terminated by spraying thereon a quench liquid, such as water, using at least one set of spray nozzles. The hot effluent gases containing the carbon black products suspended therein are then passed downstream where the steps of cooling, separating and collecting the carbon black are carried out in conventional manner. For example, the separation of the carbon black from the gas stream is readily accomplished by conventional means such as a precipitator, cyclone separator, bag filter, or combinations thereof.
When practicing the present invention, the amounts of feedstock injected into the primary combustion zone and at the point where the combustion gases have reached maximum velocity are any amounts of proportions which result in the process yielding carbon blacks having increased CDBP values. Furthermore, the blacks will impart improved hysteretic properties to rubber composition containing the blacks. It is preferred to inject an amount of from about 20 to about 80% of the liquid feedstock as solid streams in the primary combustion zone, with the remaining amount of the feedstock being injected as solid streams at approximately the point in the transition zone where the combustion gas stream has reached maximum velocity.In a particularly preferred embodiment, an amount of from about 40 to about 60% of the feedstock is injected in the primary combustion zone, with the remaining amount of the feedstock being injected at approximately the point in the transition zone where the combustion gas stream has reached maximum velocity.
The following testing procedures are used in evaluating the analytical and physical properties of the blacks produced by the present invention.
IODINE ADSORPTION NUMBER
This is determined in accordance with ASTM D-1510-70.
TINT STRENGTH
The tint strength of a carbon black sample is determined relative to an industry tint reference black in accordance with ASTM D3265-76a.
DIBUTYL PHTHA LA TE (DBP) ABSORPTION NUMBER
The DBP absorption number of a carbon black is determined in accordance with ASTM D 2414-76. The results reported indicate whether or not the carbon black is in fluffy or pellet form.
CRUSHED DBP ABSORPTION NUMBER (CDBP)
A carbon black pellet is subjected to a crushing type action and the structure is then measured in accordance with ASTM D-3493-79.
MODULUS AND TENSILE
These physical properties are determined in accordance with the procedures described in
ASTM D-412. In brief, the modulus measurement relates to the pounds per square inch pull observed when a sample of vulcanized rubber is stretched to 300% of its original length. The tensile measurement is a determination of the number of pounds per square inch pull required to rupture or break a sample of vulcanized rubber in a tension test.
EXTRUSION SHRINKAGE
This is determined in accordance with ASTM D-2230-37 (Method B).
REBOUND
This is determined in accordance with the procedure set forth in ASTM D-1054.
The invention will be more readily understood by reference to the following examples. There are, of course, many other forms 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 these 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.
EXAMPLE 1 In this example there is employed a suitable reaction apparatus provided with means for supplying combustion gas-producing reactants, i.e., a fuel and an oxidant, either as separate streams or as precombusted gaseous reaction products to the primary combustion zone, and also means for supplying the carbon black-yielding hydrocarbonaceous feedstock which are
movable so as to permit the adjustment of the location of the radially inward or outward
injection of feedstock into the combustion gas stream prior to the point where maximum velocity is attained. The apparatus may be constructed of any suitable material such as metal and either provided with refractory insulation or surrounded by cooling means such as a recirculating liquid which is preferably water.Additionally, the reaction apparatus is equipped with temperature and pressure recording means, means for quenching the carbon black-forming reaction such as spray nozzles, means for cooling the carbon black product and means for separating and recovering the carbon black from other undesired by-products. In carrying out the present example, any suitable burner may be utilized in the primary or first stage combustion in which a primary combustion of 150% may be obtained.The first stage combustion gases having a 150% primary combustion, are formed by charging into the combustion zone of the apparatus air preheated to a temperature of 1200"F. (922'K.) at a rate of 475 k.s.c.f.h. (3.736 m3/sec), and natural gas at a rate of 32.6 k.s.c.f.h. (0.256 m3/sec) thereby generating a stream of hot combustion gases flowing in a downstream direction at a high linear velocity. The rapidly flowing stream of combustion gases passes into a second or transition zone which is of smaller cross-sectional diameter in order to increase the linear velocity of the stream of combustion gases. A suitable liquid hydrocarbonaceous feedstock is then introduced substantially transversely into the resultant stream of hot combustion gases.The feedstock is injected in the form of solid streams both from the outer periphery radially inwardly toward the core of the combustion gases through 1 2 unobstructed orifices each of which has a size of 0.059 inch (1.50 mm), and from the inner periphery radially outwardly into the combustion gas stream through 6 unobstructed orifices each of which has a size of 0.059 inch (1.50 mm). Accordingly, in this run one-third (1 /3) of the feedstock is injected from the inner periphery outwardly, with the remaining two-thirds (2/3) being injected inwardly from the outer periphery of the combustion gas stream.The total feedstock injection occurs in the same plane, namely at approximately the mid-point of the transition zone, at a combined rate of 968 g.p.h. (1.02
1 /sec), and under conditions sufficient to assure a proper degree of penetration into the combustion gas stream so that coke formation in the reactor will not occur. The transition zone of the apparatus has a diameter of 1 2.4 inches (315 mm) and a length of 11 inches (279 mm).
The reactor section has a diameter of 18 inches (457 mm) and a length of 9 feet (2.74 m), prior to quenching the reaction.
The reaction is carried out such that the overall combustion of the process is 26.1 %, or 3.83 equivalence ratio, and the water quench for terminating the reaction is located at a point 9 feet downstream of the location of feedstock injection. The analytical and performance characteristics of this black are reported in Table I. Moreover, this black is utilized herein as a control for
Example No. 2 since the feedstock was totally introduced at the mid-point of the transition zone where maximum velocity of the combustion gas stream was reached.
EXAMPLE 2
The procedure of Example 1 is followed using the same apparatus. The main difference in this example from that of Example 1 involves altering the location at which the injection of liquid hydrocarbon feedstock in the form of solid streams from the inner periphery radially outwardly into the combustion gas stream is carried out. In this run the partial injection of liquid feedstock from the inner periphery occurs at a location where the combustion gas stream has not yet attained maximum velocity, i.e., prior to approximately the mid-point of the transition zone.
More specifically, combustion air, preheated to 1200"F. (922'K.) is introduced into the primary combustion zone at a rate of 475 k.s.c.f.h. (3.736 m3/sec) and natural gas is introduced at a rate of 19.8 k.s.c.f.h. (0.156 m3/sec) in order to provide a primary or first stage combustion fire having a 247% primary combustion. In this run, the total rate at which liquid hydrocarbon feedstock is injected into the combustion gas stream is 978 g.p.h. (1.03 1 /sec). Here, as in
Example 1, the liquid feedstock is injected in the form of solid streams (coherent jets) from the outer periphery and from the inner periphery of the combustion gas stream. More precisely, 50% of the feestock is injected at approximately the mid-point of the transition zone through 3 unobstructed orifices each of which has a size of 0.110 inch (2.74 mm) from the outer periphery radially inwardly into the combustion gas stream. The remaining 50% of the liquid feedstock is injected as solid streams from the inner periphery of the combustion gas stream in a radially outward direction into the combustion gas stream through 3 unobstructed orifices each of which has a size of 0.11 3 inch (2.87 mm). However, the liquid feedstock injection from the inner periphery in this run is carried out at a location which is 1 8 inches (457 mm) upstream from the plane where maximum velocity of the combustion gas stream is reached, namely at approximately the mid-point of the transition zone.The resultant combustion gas stream passes into the reaction zone where the carbon black forming reaction is quenched with water at a point located 9 feet (2.74 m) downstream of the plane where maximum velocity of the combustion gas stream is reached, i.e., approximately the mid-point of the transition zone. The overall percent combustion of the run is 27.8%. The analytical and physical properties of this black are reported in Table I.
Example No. 1 2
Iodine No., mgI2/g black 89 82
Tinting Strength, % 112 99
DBP Absorption, pellets, cc/lOOg 134 129
CDBP (24M4), cc/lOOg 103 105
The suitability of the blacks of the present invention as low-hysteretic reinforcing agents for rubber compositions is clearly shown in the following Table II. In evaluating the blacks, the rubber formulations are readily prepared by conventional methods. For example, the rubber and the carbon black are intimately admixed together on a conventional mixing machine of the type normally used for mixing rubber or plastics such as a Banbury mixer and/or roll mill in order to insure satisfactory dispersion. The rubber formulations are compounded according to standard industry formulations for a natural rubber or synthetic rubber-containing formulation.The resulting vulcanizates are cured for the time specified in determining the particular physical property. In evaluating the performance of the carbon blacks of the present invention, the following formulation is utilized wherein the quantities are specified in parts by weight. The rubber formulation specifically used herein is the Synthetic Rubber Recipe of ASTM-D-3191-79 and is characterized as follows::
Ingredient Amount Polymer (SBR 1500/23.5% styrene, 76.5% butadiene) ing Zinc Oxide 3 1
Sulfur 175 Stearic Acid
N-tert-butyl-2 benzotbiazole aul fenam ide 1
Carbon Black so In the following Table II there are demonstrated the advantageous and unexpected results achieved by the use of the carbon black products described hereinabove as additives in rubber formulations. It will, of course, be apparent that the examples, while being illustrative of the present invention, should not be construed as limiting or restrictive in any way.
TABLE II
Physical Properties of Synthetic
Rubber Vulcanizates
Carbon Black Sample Ex. l* Ex. 2* 300% Modulus, 35 min., psi + 590 + 305 I a' I N (MPa) (+4.068) (+2.103)
300% Modulus, 50 min., psi + 670 + 335 N N N N (MPa) (+4.621) (+2.310)
Tensile, 50 min., psi + 295 + 55 N N N U (MPa) (+2.034) (+0.379)
Extrusion Shrinkage, % 89 89
Rebound, 60 min, % -3.9 -1.4
*The data are given relative to IRB No. 5.
A review of the data presented above reveals that blacks produced by the present process exhibit the desired properties. When incorporated into the rubber formulations, there is a significant improvement in the rebound property which is an indicator or a rubber vulcanisate having improved hysteresis.
Claims (6)
1. A modular process for producing furnace carbon blacks wherein a fuel and an oxidant are reacted in a first zone 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 in a second zone liquid hydrocarbon feedstock is peripherally injected, in the form of a plurality of solid streams (coherent jets), into the stream of gaseous combustion products at a location 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 the degree of penetration required for proper shearing and mixing of the feedstock, and wherein in a third zone the feedstock is decomposed and converted into carbon black prior to termination of the carbon forming reaction by quenching, and then cooling, separating and recovering the resultant carbon black, characterised in that a sufficient portion of the total amount of liquid hydrocarbon feedstock is introduced in the form of a plurality of solid streams substantially radially into the combustion gas stream from the periphery thereof prior to the point at which the stream of combustion gases reaches maximum velocity, to thereby produce carbon blacks having increased CDBP values.
2. A process as defined in claim 1 wherein an amount of from 20 to 80% of the total amount of liquid feedstock is injected into the combustion gas stream prior to the location where maximum velocity of the combustion gas stream is reached, with the remainder being added at approximately the point where the combustion gas stream has reached maximum velocity.
3. A process as defined in claim 1 or 2 wherein an amount of from 40 to 60% of the total amount of liquid feedstock is injected into the combustion gas stream prior to the location where maximum velocity of the combustion gas stream is reached, with the remainder being added at approximately the point where the combustion gas stream has reached velocity.
4. A process as defined in claim 1, 2 or 3 wherein the liquid hydrocarbon feedstock which is injected into the stream of combustion gases prior to the point at which the stream of combustion gases has reached maximum velocity is injected in a substantially transverse direction outwardly from the inner periphery of the combustion gas stream.
5. A process as defined in claim 1, 2, 3, or 4 wherein the liquid hydrocarbon feedstock which is injected into the combustion gas stream at approximately the point where maximum velocity is reached is injected in a substantially transverse direction inwardly from the outer periphery of the combustion gas stream.
6. A process for producing furnace carbon blacks substantially as described herein with reference to Example 2.
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US56468583A | 1983-12-23 | 1983-12-23 | |
| US62670484A | 1984-07-02 | 1984-07-02 |
Publications (3)
| Publication Number | Publication Date |
|---|---|
| GB8431483D0 GB8431483D0 (en) | 1985-01-23 |
| GB2151604A true GB2151604A (en) | 1985-07-24 |
| GB2151604B GB2151604B (en) | 1987-09-16 |
Family
ID=27073625
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB08431483A Expired GB2151604B (en) | 1983-12-23 | 1984-12-13 | Production of carbon black |
Country Status (26)
| Country | Link |
|---|---|
| KR (1) | KR930002758B1 (en) |
| AR (1) | AR242423A1 (en) |
| AU (1) | AU566537B2 (en) |
| BE (1) | BE901375A (en) |
| BR (1) | BR8406309A (en) |
| CA (1) | CA1229468A (en) |
| CS (1) | CS252478B2 (en) |
| DD (1) | DD228554B3 (en) |
| DE (1) | DE3443872A1 (en) |
| DK (1) | DK614884A (en) |
| ES (1) | ES538528A0 (en) |
| FR (1) | FR2557125B1 (en) |
| GB (1) | GB2151604B (en) |
| HU (1) | HUT36491A (en) |
| IL (1) | IL73894A (en) |
| IN (1) | IN163602B (en) |
| IT (1) | IT1177495B (en) |
| LU (1) | LU85695A1 (en) |
| MX (1) | MX162201A (en) |
| NL (1) | NL190378C (en) |
| PH (1) | PH20652A (en) |
| PL (1) | PL145192B1 (en) |
| PT (1) | PT79728A (en) |
| RO (1) | RO89530A (en) |
| SE (1) | SE461530B (en) |
| YU (1) | YU218184A (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4765964A (en) * | 1983-09-20 | 1988-08-23 | Phillips Petroleum Company | Carbon black reactor having a reactor throat |
| US4976945A (en) * | 1988-05-24 | 1990-12-11 | Mitsubishi Kasei Corporation | Process for producing carbon black |
| US5093407A (en) * | 1989-09-14 | 1992-03-03 | Cabot Corporation | Carbon blacks and rubber compositions containing the carbon blacks |
| EP0513189A4 (en) * | 1990-02-06 | 1993-05-12 | Cabot Corporation | Carbon black exhibitng superior treadwear/hysteresis performance |
Families Citing this family (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| IN171963B (en) * | 1987-12-10 | 1993-02-20 | Cabot Corp | |
| DE102023002671A1 (en) | 2023-06-26 | 2025-01-02 | Günter Etzrodt | Process for the production of pigment black from sustainable raw materials without carbon dioxide emissions and its use |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US28974A (en) * | 1860-07-03 | Celestino domtngxjez | ||
| GB1387730A (en) * | 1972-07-28 | 1975-03-19 | Continental Carbon Co | Process and apparatus for the production of carbon black |
| US3922335A (en) * | 1974-02-25 | 1975-11-25 | Cabot Corp | Process for producing carbon black |
| GB1466341A (en) * | 1973-02-16 | 1977-03-09 | Cabot Corp | Carbon black pigments and rubber conposition |
Family Cites Families (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3046096A (en) * | 1958-12-02 | 1962-07-24 | Columbian Carbon | Carbon black manufacture |
| US4165364A (en) * | 1976-08-04 | 1979-08-21 | Sid Richardson Carbon & Gasoline Co. | Carbon black reactor with axial flow burner |
| US4289743A (en) * | 1977-07-01 | 1981-09-15 | Sid Richardson Carbon & Gasoline Co. | Double venturi carbon black reactor system |
| US4391789A (en) * | 1982-04-15 | 1983-07-05 | Columbian Chemicals Company | Carbon black process |
| CA1259164A (en) * | 1982-08-30 | 1989-09-12 | E. Webb Henderson | Carbon blacks and method and apparatus for their production |
| CA1258157A (en) * | 1983-09-20 | 1989-08-08 | Mark L. Gravley | Carbon blacks and method and apparatus for their production |
-
1984
- 1984-12-01 DE DE19843443872 patent/DE3443872A1/en active Granted
- 1984-12-04 IN IN950/MAS/84A patent/IN163602B/en unknown
- 1984-12-05 AR AR84298857A patent/AR242423A1/en active
- 1984-12-10 BR BR8406309A patent/BR8406309A/en not_active IP Right Cessation
- 1984-12-12 ES ES538528A patent/ES538528A0/en active Granted
- 1984-12-13 GB GB08431483A patent/GB2151604B/en not_active Expired
- 1984-12-19 LU LU85695A patent/LU85695A1/en unknown
- 1984-12-19 PH PH31612A patent/PH20652A/en unknown
- 1984-12-19 MX MX203827A patent/MX162201A/en unknown
- 1984-12-20 CA CA000470709A patent/CA1229468A/en not_active Expired
- 1984-12-20 DK DK614884A patent/DK614884A/en not_active Application Discontinuation
- 1984-12-20 DD DD84271299A patent/DD228554B3/en not_active IP Right Cessation
- 1984-12-21 NL NLAANVRAGE8403907,A patent/NL190378C/en not_active IP Right Cessation
- 1984-12-21 FR FR8419734A patent/FR2557125B1/en not_active Expired
- 1984-12-21 PL PL1984251136A patent/PL145192B1/en unknown
- 1984-12-21 AU AU37094/84A patent/AU566537B2/en not_active Expired
- 1984-12-21 IT IT24170/84A patent/IT1177495B/en active
- 1984-12-21 IL IL73894A patent/IL73894A/en unknown
- 1984-12-21 SE SE8406568A patent/SE461530B/en not_active IP Right Cessation
- 1984-12-21 PT PT79728A patent/PT79728A/en unknown
- 1984-12-21 BE BE0/214235A patent/BE901375A/en not_active IP Right Cessation
- 1984-12-21 CS CS8410207A patent/CS252478B2/en unknown
- 1984-12-21 YU YU02181/84A patent/YU218184A/en unknown
- 1984-12-21 HU HU844803A patent/HUT36491A/en unknown
- 1984-12-22 KR KR1019840008274A patent/KR930002758B1/en not_active Expired - Fee Related
- 1984-12-22 RO RO84116824A patent/RO89530A/en unknown
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US28974A (en) * | 1860-07-03 | Celestino domtngxjez | ||
| GB1387730A (en) * | 1972-07-28 | 1975-03-19 | Continental Carbon Co | Process and apparatus for the production of carbon black |
| GB1466341A (en) * | 1973-02-16 | 1977-03-09 | Cabot Corp | Carbon black pigments and rubber conposition |
| US3922335A (en) * | 1974-02-25 | 1975-11-25 | Cabot Corp | Process for producing carbon black |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4765964A (en) * | 1983-09-20 | 1988-08-23 | Phillips Petroleum Company | Carbon black reactor having a reactor throat |
| US4976945A (en) * | 1988-05-24 | 1990-12-11 | Mitsubishi Kasei Corporation | Process for producing carbon black |
| US5093407A (en) * | 1989-09-14 | 1992-03-03 | Cabot Corporation | Carbon blacks and rubber compositions containing the carbon blacks |
| EP0513189A4 (en) * | 1990-02-06 | 1993-05-12 | Cabot Corporation | Carbon black exhibitng superior treadwear/hysteresis performance |
Also Published As
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US4370308A (en) | Production of carbon black | |
| US5236992A (en) | Carbon blacks and their use in rubber applications | |
| US5288788A (en) | Carbon blacks imparting superior treadwear/hysteresis performance and process for producing carbon blacks | |
| US3490869A (en) | Vortex reactor for carbon black manufacture | |
| US3725103A (en) | Carbon black pigments | |
| US3952087A (en) | Production of high structure carbon blacks | |
| US6348181B1 (en) | Process for producing carbon blacks | |
| US4879104A (en) | Process for producing carbon black | |
| US4105750A (en) | Production of carbon blacks | |
| GB2151604A (en) | Production of carbon black | |
| US4645657A (en) | Production of carbon black | |
| JPH0126620B2 (en) | ||
| NZ210438A (en) | Carbon black preparation | |
| CA1081433A (en) | Production of carbon blacks | |
| KR800001355B1 (en) | Production of carbon blacks |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PE20 | Patent expired after termination of 20 years |
Effective date: 20041212 |