US2379159A - Process for the catalytic conversion of hydrocarbons - Google Patents

Process for the catalytic conversion of hydrocarbons Download PDF

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US2379159A
US2379159A US496854A US49685443A US2379159A US 2379159 A US2379159 A US 2379159A US 496854 A US496854 A US 496854A US 49685443 A US49685443 A US 49685443A US 2379159 A US2379159 A US 2379159A
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gasoline
catalyst
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conversion
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Elmer R Kanhofer
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Universal Oil Products Co
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    • CCHEMISTRY; METALLURGY
    • C10PETROLEUM, GAS OR COKE INDUSTRIES; TECHNICAL GASES CONTAINING CARBON MONOXIDE; FUELS; LUBRICANTS; PEAT
    • C10GCRACKING HYDROCARBON OILS; PRODUCTION OF LIQUID HYDROCARBON MIXTURES, e.g. BY DESTRUCTIVE HYDROGENATION, OLIGOMERISATION, POLYMERISATION; RECOVERY OF HYDROCARBON OILS FROM OIL-SHALE, OIL-SAND, OR GASES; REFINING MIXTURES MAINLY CONSISTING OF HYDROCARBONS; REFORMING OF NAPHTHA; MINERAL WAXES
    • C10G11/00Catalytic cracking, in the absence of hydrogen, of hydrocarbon oils
    • C10G11/14Catalytic cracking, in the absence of hydrogen, of hydrocarbon oils with preheated moving solid catalysts
    • C10G11/18Catalytic cracking, in the absence of hydrogen, of hydrocarbon oils with preheated moving solid catalysts according to the "fluidised-bed" technique

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  • This invention relates particularly to a twostage process for the catalytic conversion of hydrocarbon oils into gasoline fractions of high antiknock value. More specifically, it is concerned with a combination of a series of interdependent and cooperative steps for the production of a gasoline fraction low in olens and suitable for use as'an aviation base blending fuel.
  • Hydrocarbon oils heavier than gasoline such as kerosene, gas oil, fuel oil, etc.
  • the high olefin-content gasoline has likewise been heretofore subjected to treatment with a cracking catalyst at a temperature within the range of from about 600 to about 1000 F.
  • the catalytic masses employed in these reactions comprises particularly the so-calledl silicaalumina, silica-zirconia or silica-alumina-zirconia composites, made by the separate or simultaneous precipitation of silica and alumina and/or zirconia under conditions such that alkali metal ions are eliminated.
  • Other cracking catalysts such as acid treated clays may also be used,v although not necessarily with equivalent results.
  • the catalyst requires regeneration inv order to restore its activity.
  • air or other oxygen-containingv gases are contacted with the catalyst and regeneration is effected at a temperature which may in the high temperature cracking step.
  • the present invention is concerned with the process utilizing a low temperature cracking step followed by a high temperature cracking step and finally by reactivation of the catalyst.
  • the present invention is characterized by the following cooperative steps in order to produce high yields of gasoline of low olefin content and particularly suitable for use as aviation base blending fuel: i
  • An oil heavier than gasoline is subjected to treatment in commingled state with an olefinic gasoline in a first conversion step in the presence of a cracking catalystv at a temperature of from about 600 to about 1000 F. under conditions to produce a gasoline fraction of low olefin content.
  • the products of this conversion step are separated into a low boiling gasolinefraction having an end boiling point of from about 200 to about 250 F., which in some cases may be as high as 300 or even up to 400 F., and higher boiling products.
  • the higher boiling products from the first conversion step are subjected to cracking in a second conversion step in contact with, a siliceous catalyst and particularly the spent catalyst from the first conversion step, the second conversion step being at a temperature of from about 900 to about' 1200 F. and under conditions to produce an olenic gasoline.
  • the olenic gasoline is thensup'plied tothe rst conversion step for treatment inthe manner heretofore described.
  • the present invention includes -ther'fvollowing important features:
  • the low .boiling gasoline fraction recovered lfrom the second ⁇ conversion step of the process will have an end lboiling point similar to or higher than the low boilinggasoline fraction recovered from theiflrfstlconversion step of the, process as heretofore described.
  • an intermediate naphtha fraction such as one having an initial boiling point within' the range of from about 200 to about 300 or 350 F., and an end boiling point within the range of from about 300 to about 400 F.
  • an intermediate naphtha fraction may be separated and withdrawn from the products ofthe second conversion step and vall or a portion Aof this naphtha may beblended be of the order of, or higher than, that employed with the low boiling low olefin content gasoline recovered as the final product ofthe vprocess from the iirst conversion step.
  • the naphtha fraction will below in olefin content and high in aromatic content so that it is particularly suitable for blending with the low boiling gasoline fractior for the production of aviation gasoline.
  • the present invention is particularly applicable to the treatment of oil in a process employing a moving bed of catalyst.
  • the type of process now known as the Fluidized operation is especially preferred in the present invention.
  • the catalyst powder is maintained in constant agitation by a rising stream of reactants and the net upward flow of the reactants is greater than that of the catalyst particles.
  • the present invention relates to a process for the manufacture of gasoline of low olefin content and of high antiknock value which comprises subjecting an oil heavier than gasoline in commingled state with an oleflnic gasoline to contact in a first conversion step with a siliceous catalyst under conditions to produce a low boiling gasoline fraction of 'low olefin content, separating the same from heavier hydrocarbons and subjecting the latter to cracking in a second conversion step in contact with a siliceous catalyst under conditions to produce a low boiling olenic gasoline, and supplying said low boiling olenic gasoline to treatment in the first step as heretofore described.
  • olenic gasoline or gasoline of high olefin content is used in the present specification and claims to mean the type of gasoline normally produced by cracking of heavier oil in contact with a cracking catalyst under temperatures of the order of about 900 to about 1200 F. at a weight hourly space velocity which is usually above 1.
  • weight hourly space velocity is defined as the weight of oil of catalyst in the reaction zone.
  • gasoline of low olefin content is intended to mean the gasoline produced by treatment of a heavier oil in commingled state with a high olefin content gasoline in the presence of a cracking catalyst at temperatures of the order of about 600 to about 1000 F. but at a weight hourly space velocity which is usually below 1.
  • the temperature and space velocity may be correlated in order to produce either high olefin or low olefin content gasolines and also that these operating conditions will be dependent upon the activity of the particular catalyst employed. 'I'hus in the first conversion step in which a low olen content gasoline is produced, if the temperature employed is within the upper limits of the range heretofore given, the space velocity will be correspondingly increased. Likewise, if the temperature employed is withinthe lower limits of the range heretofore specified, the 4space velocity may be correspondingly reduced. A similar situation occurs in connection with the second conversion step for the production of high olefin content gasoline.
  • reaction in the nrst per hour per weight conversion step of the process serves to increase the yield of the low boiling low olefin-content gasoline produced in the process. It is believed that hydrogen from the heavier oil is transferred to the low boiling oleflnic hydrocarbons during the reaction and at the same time the heavier oil is cracked to produce additional low boiling oleflns, which are likewise saturated by the hydrogen released from the heavier oil. Whatever portions of the heavier oil which are not converted under the relatively mild conversion conditions of the first step of the process are subsequently in the second step of the process converted under the more severe conditions employed therein.
  • the present invention relates to a process for the manufacture of aviation base blending fuel which comprises subjecting a mixture of raw oil heavier than gasoline and an oleilnic gasoline formed in the process, in the manner to be hereinafter described, 4to contact in a first conversion step with an active cracking catalyst under fluidized conditions at a temperature within the range of from about 600 to about 1000 F.
  • a hydrocarbon charging oil such as kerosene, gas oil, or any other hydrocarbon oil heavier than gasoline
  • pump 3 by means of which it is directed through line 4 and valve 5 and is admixed with a low boiling high olefin content gasoline fraction formed in the process, in the manner to be hereinafter described in detail, and directed through line 5 and valve 1 to commingle with the charging oil in line I.
  • the mixture is then directed into and through heating coil 8 in furnace structure 9, wherein the mixture is heated to the desired temperature.
  • Heated products are then directed through line I0 and valve Il, whereafter they are commingled with fresh or reactivated powdered catalyst introduced through standpipe l2 and valve I3 and obtained in the manner to be hereinafter described in detail.
  • the mixture of oil and catalyst is then directed through line I4 into reactor I5 which comprises the iirst conversion step o! the process for the production of a low boiling low olefin content gasoline fraction.
  • a turbulent mass of catalyst powder is maintained in constant agitation by a rising stream of reactants introduced by means of line I4 and the conversion products formed during the reaction.
  • the top of this turbulent bed is indicated diagrammatically by line i5.
  • the temperature in this zone will ordinarily range from approximately 600 to approximately 1000 F. and preferably will be from about 850 to about 950 F.
  • Pressure in this zone will ordinarily be slightly above atmospheric and may be of the order of 5 to 25 pounds per square inch gauge, although in some cases pressures as high as 100 pounds per square inch gauge or more may be employed.
  • Weight hourly space velocities will usually not be greater than l, although, as hertofore mentioned, higher space velocities may be employed depending upon the temperature utilized.
  • Vaporous conversion products containing some suspended catalyst are withdrawn from the top of reactor
  • the conversion products are then withdrawn through line
  • the low olen low boiling gasoline fraction may have an end boiling point within ⁇ the range of from about 200 to about 400 F. and more generally will have an end boiling point of from about 200 to about 250 F.
  • This fraction is withdrawn from the upper portion of fractionator 2
  • AIn receiver 21 a separation is effected between the gaseous phase and the liquid phase, the gaseous phase being withdrawn through line 28 and valve 29 to storage or elsewhere as desired.
  • This gaseous-phase will contain a relatively high proportion of isobutane and is particularly suitable for use in subsequent alkylation or other conversion treatments.
  • the distillate collected in receiver 21 is withdrawn therefrom through line 30 and valve 3
  • is withdrawn therefrom through line 35 and valve 39 to pump 40, by means of which all or a portion thereof is supplied through line 4
  • the heavier oil Prior to its introduction into heating coil 43, the heavier oil may be commingled with a, recycle oil formed in the process, in the manner to lne/hereinafter described, and directed through line 45 ,and valve 45 into line 4
  • the heavier oil introduced into line 43 is heated therein to the desired temperature and is then directed through line 41 and valve 45, whereafter it is commingled with a partly spent powdered catalyst introduced through valve 49 rand standpipe 50 and obtained in the manner to be hereinafter described in detail.
  • the resulting mixture of catalyst and oil is then directed through line 5
  • a portion of the heavier oil may be diverted from line 41 through line 53 and valve 54, to commingle with a portion oi the freshly regenerated catalyst withdrawn through valve 55 and standpipe 55, the resulting mixture being directed through line 51 into reactor 52.
  • Reactor 52 may be similar in design to reactor I5 and thus line 55 indicates the top of the turrbulent bed, numeral 59 indicates the cyclone separator and line 50 is provided for the return of catalyst back to the reactor. However, as heretofore mentioned, reactorv 52 will be operated at a temperature within the range of from about 900 to about 1200 F. at a. Weight hourly space velocity which will usually be greater than l, these operating conditions being dependent upon the activity of the particular catalyst employed.
  • the vaporous conversion products containing some suspended catalyst are directed through cyclone separator 59 in which the catalyst is separated out and the hydrocarbon conversion products are then directed through line 5
  • fractionator 53 a low boiling high olefin content gasoline fraction is separated and this fraction may have an end boiling point similar to or diierent than that heretofore described in connection with the overhead products withdrawn through line 22 from fractionator 2
  • this ⁇ fraction will have an end boiling point within the range of from a'boutA 200 to about 250 F. and is directed through line 54 and valve 55 into and through condenser 55 and rundown line 51 containing valve 58 into receiver 59.
  • the gases are released from receiver 59 through line 10 and valve 1
  • the distillate collected in receiver 59 is withdrawn therefrom through line 12 and valve 13 to pump 14, by means of which it is supplied through line 15 and a portion thereof recycled by way of line 15 and valve 11 to the upper portion of fractionator 53 to serve as a cooling and reiluxing medium therein.
  • a portion of the distillate from receiver 59 may be withdrawn to storage or elsewhere as desired through line 18 and valve 19 but, in accordance with the present invention, at least a portion of the distillate is directed through line 5 and valve 1 to commingle with the hydrocarbon charging oil introduced through line in the manner heretofore described.
  • an intermediate naphtha fraction having an initial boiling point within the range of from about 200 to about 350 F. and an end boiling point within the range of from about 250 to about 400 F. preferably one having an initial boiling point within the range of from about 200 to about 300 F. and an end fboiling point within the range of from about 250 to about 350 F., may be separated from other products in fractionator 53 and withdrawn therefrom through line B0 and valve 5
  • the naphtha fraction will be low in olefin content and high in aromatic content so that it is particularly suitable for use as a blending agent in aviation gasoline.
  • the heavier oil separated in fractlonator 33 may be withdrawn therefrom through line 01 and withdrawn from the process through line I3 and valve 80 to storage or elsewhere as desired.
  • the heavier oil may be directed through line and valve 9
  • 4 and valve lli. 'I'his heavy naphtha fraction will have an initial boiling point above the intermediate naphtha fraction withdrawn through line 80 and an end lboiling point within the range of from about 400 toI about 500 F. 'I'he heavy naphtha fraction may be recycled for further treatment by way of lines 90, 45, 4
  • the spent catalyst in reactor 52 is directed into standpipe 93 wherein the catalyst is stripped of its volatile hydrocarbons absorbed therein by an upwardly moving stream of gas, such as steam, fluegas, etc., introduced through line 34 and valve 95.
  • This gas not only serves to strip volatile hydrocarbons from the catalyst but also serves to maintain the powdered catalyst in a fiuidized state so that the suspension will readily ow like a liquid.
  • 'I'he spent catalyst is supplied through valve 96 and is picked up bya stream of air or other suitable oxidizing gas introduced through line 91 and valve 90 and the mixture is supplied through line 09 to regenerator
  • 00 the hydrocarbonaceous deposit formed on the catalyst is removed from the catalyst by a combustion reaction.
  • Spent reactivated gases are withdrawn from the regenerator through cyclone separator
  • the catalyst is at too high a temperature when withdrawn from the regenerating zone and heat exchanger
  • the catalyst in reactor II after it has served to effect conversion of the charging oil and low boiling high olefin gasoline, is withdrawn through standpipe Ill into line Il.
  • Line H2 containing valve H3 is provided for the introduction of a suitable stripping medium to remove volatile hydrocarbons from the catalyst and to maintain the powdered catalyst in fluidized state. It is a particular feature of the present invention that this catalyst, after having been used in the first conversion step, will retain sufficient activity for use in the second conversion step of the process.
  • a low olefin, high antiknock gasoline fraction having an end boiling point of about 250 F. may be separated from the conversion products and the heavier hydrocarbon oil commingled with the spent catalyst from the first conversion step and subjected to cracking at a temperature of about 950 F. and at a weight hourly liquid space velocity of about 1.7.
  • isobutane 8.0% of isopentane as well as of butylenes.
  • the isopentane may be blended with the aviation gasoline, while the isobutane and butylenes may be utilized in a1- kylation reactions for the production of an alkvlate which may also be used in the aviation gasoline.
  • a process for the manufacture of a gasoline of low olen content, high antiknock value and suitable for use in aviation gasoline which comprises commingling an oil heavier than gasoline with a gasoline of higher olefin content than said first mentioned gasoline, and utilizing the commingled stream to convey freshly regenerated powdered cracking catalyst into a rst reaction zone operated at a temperature within the range of from about 600 to about 1000 F.
  • the process as defined in claim 3 further characterized in that the first conversion zone is maintained at a. temperature of from about' 600 F. to about 1000 F. and the second conversion zone at a temperature of from about 900 F. to about 1200 F.

Description

`lune 26, 1945. 2,379,159
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LON BQQN SSR Patented June 26, 1945 PROCESS FOR THE CATALYTIC COIWI'ERSIONl F HYDROCARBONS Elmer R. Kanhoter, Riverside, Ill., asslgnor 'to Universal Oil Products Company, Chicago, lll., a corporation oi' Delaware Application July 31, 1943, Serial No. 496,854
7 Claims. (Cl. 196-49) This invention relates particularly to a twostage process for the catalytic conversion of hydrocarbon oils into gasoline fractions of high antiknock value. More specifically, it is concerned with a combination of a series of interdependent and cooperative steps for the production of a gasoline fraction low in olens and suitable for use as'an aviation base blending fuel.
Hydrocarbon oils heavier than gasoline, such as kerosene, gas oil, fuel oil, etc., have heretofore been subjected to cracking in the presence of siliceous-type catalysts at temperatures in the range of from about 900 to about 1200 F. to produce gasoline which has a high antiknock value, but which is generally unsuitable as an aviation base blending fuel'because of its relatively high olefin content. The high olefin-content gasoline has likewise been heretofore subjected to treatment with a cracking catalyst at a temperature within the range of from about 600 to about 1000 F. under conditions to produce a gasoline fraction which not only retains the high antiknock characteristics of the olefin charge, but also has a relatively low olefln content and a resulting high lead susceptibility. It has also been heretofore proposed to subject a heavier oil in admixture with an olenic gasoline to conversion in the presence of a cracking catalyst at a temperature within the range of from about 600 to about 1000 F. under conditions to effect cracking of the heavier oil into a gasoline fraction which is low in olen content and at the same time converting the oleiinic gasoline into a gasoline which is low in olefin content, butr which retains its high antiknock characteristics. Such a combination process is of the greatest importance in the production of aviation base blending fuel and it is with an improvement in a combination process of this type that the present invention is directed to.
The catalytic masses employed in these reactions comprises particularly the so-calledl silicaalumina, silica-zirconia or silica-alumina-zirconia composites, made by the separate or simultaneous precipitation of silica and alumina and/or zirconia under conditions such that alkali metal ions are eliminated. Other cracking catalysts, such as acid treated clays may also be used,v although not necessarily with equivalent results. Eventually the catalyst requires regeneration inv order to restore its activity. In reactivating the catalytic masses, air or other oxygen-containingv gases are contacted with the catalyst and regeneration is effected at a temperature which may in the high temperature cracking step. The present invention is concerned with the process utilizing a low temperature cracking step followed by a high temperature cracking step and finally by reactivation of the catalyst.
The present invention is characterized by the following cooperative steps in order to produce high yields of gasoline of low olefin content and particularly suitable for use as aviation base blending fuel: i
(l) An oil heavier than gasoline is subjected to treatment in commingled state with an olefinic gasoline in a first conversion step in the presence of a cracking catalystv at a temperature of from about 600 to about 1000 F. under conditions to produce a gasoline fraction of low olefin content. The products of this conversion step are separated into a low boiling gasolinefraction having an end boiling point of from about 200 to about 250 F., which in some cases may be as high as 300 or even up to 400 F., and higher boiling products.
(2) The higher boiling products from the first conversion step are subjected to cracking in a second conversion step in contact with, a siliceous catalyst and particularly the spent catalyst from the first conversion step, the second conversion step being at a temperature of from about 900 to about' 1200 F. and under conditions to produce an olenic gasoline. The olenic gasoline is thensup'plied tothe rst conversion step for treatment inthe manner heretofore described.
L In, additionito the above, the present invention includes -ther'fvollowing important features:
` 4(1) -The low .boiling gasoline fraction recovered lfrom the second `conversion step of the process will have an end lboiling point similar to or higher than the low boilinggasoline fraction recovered from theiflrfstlconversion step of the, process as heretofore described. Hydrocarbon. oil-boiling above this lowjeboiliflg gasoline fractionma-ybe recycledA to the second conversion stepin order to obtain increased yields or otherimprovements in the desired gasoline fraction. l
(2) When desired, an intermediate naphtha fraction, such as one having an initial boiling point within' the range of from about 200 to about 300 or 350 F., and an end boiling point within the range of from about 300 to about 400 F., may be separated and withdrawn from the products ofthe second conversion step and vall or a portion Aof this naphtha may beblended be of the order of, or higher than, that employed with the low boiling low olefin content gasoline recovered as the final product ofthe vprocess from the iirst conversion step. The naphtha fraction will below in olefin content and high in aromatic content so that it is particularly suitable for blending with the low boiling gasoline fractior for the production of aviation gasoline.
(3) Depending on the balance between the transfer of the catalyst in the various-stages of the process, provision is also made for supplying a portion of the freshly regenerated catalyst to a second conversion step.
The present invention is particularly applicable to the treatment of oil in a process employing a moving bed of catalyst. The type of process now known as the Fluidized operation is especially preferred in the present invention. In this type of operation the catalyst powder is maintained in constant agitation by a rising stream of reactants and the net upward flow of the reactants is greater than that of the catalyst particles. In both the moving bed type of process and the fluidized operation there is usually a transfer of catalyst from one zone to another zone, the transfer being accomplished by any suitable means including, for example, suspension or mixture of the catalyst in the reactants or in any other suitable transfer medium, me-
chanical conveyors, etc.
In a broad aspect the present invention relates to a process for the manufacture of gasoline of low olefin content and of high antiknock value which comprises subjecting an oil heavier than gasoline in commingled state with an oleflnic gasoline to contact in a first conversion step with a siliceous catalyst under conditions to produce a low boiling gasoline fraction of 'low olefin content, separating the same from heavier hydrocarbons and subjecting the latter to cracking in a second conversion step in contact with a siliceous catalyst under conditions to produce a low boiling olenic gasoline, and supplying said low boiling olenic gasoline to treatment in the first step as heretofore described.
'The term olenic gasoline or gasoline of high olefin content is used in the present specification and claims to mean the type of gasoline normally produced by cracking of heavier oil in contact with a cracking catalyst under temperatures of the order of about 900 to about 1200 F. at a weight hourly space velocity which is usually above 1. The term weight hourly space velocity is defined as the weight of oil of catalyst in the reaction zone. On the other hand, the gasoline of low olefin content is intended to mean the gasoline produced by treatment of a heavier oil in commingled state with a high olefin content gasoline in the presence of a cracking catalyst at temperatures of the order of about 600 to about 1000 F. but at a weight hourly space velocity which is usually below 1. However, it is understood that the temperature and space velocity may be correlated in order to produce either high olefin or low olefin content gasolines and also that these operating conditions will be dependent upon the activity of the particular catalyst employed. 'I'hus in the first conversion step in which a low olen content gasoline is produced, if the temperature employed is within the upper limits of the range heretofore given, the space velocity will be correspondingly increased. Likewise, if the temperature employed is withinthe lower limits of the range heretofore specified, the 4space velocity may be correspondingly reduced. A similar situation occurs in connection with the second conversion step for the production of high olefin content gasoline.
It is emphasized that the reaction in the nrst per hour per weight conversion step of the process. in which the heavier oil and the oleflnic gasoline are treated in commingled state, serves to increase the yield of the low boiling low olefin-content gasoline produced in the process. It is believed that hydrogen from the heavier oil is transferred to the low boiling oleflnic hydrocarbons during the reaction and at the same time the heavier oil is cracked to produce additional low boiling oleflns, which are likewise saturated by the hydrogen released from the heavier oil. Whatever portions of the heavier oil which are not converted under the relatively mild conversion conditions of the first step of the process are subsequently in the second step of the process converted under the more severe conditions employed therein.
In one specific embodiment the present invention relates to a process for the manufacture of aviation base blending fuel which comprises subjecting a mixture of raw oil heavier than gasoline and an oleilnic gasoline formed in the process, in the manner to be hereinafter described, 4to contact in a first conversion step with an active cracking catalyst under fluidized conditions at a temperature within the range of from about 600 to about 1000 F. at a weight hourly space velocity of not greater than l to produce a low boiling gasoline fraction of low olefin content, separating the low boiling low olefin content gasoline from heavier hydrocarbons, subjecting said heavier hydrocarbons to cracking in a second conversion step in contact under fluidized conditions with at least a portion of the catalyst which has previously been employed in the first conversion step, the second conversion step being effected at a temperature of from about 900 to about 1200 F. at a weight hourly space velocity of greater than 1, separating the products of the second conversion step into a low boiling high olefin-content gasoline fraction and heavier hydrocarbons, supplying at least a portion of said low boiling high olefin content gasoline to treatment in the first conversion step as heretofore described, and recycling at least a portion of saidheavier hydrocarbons to said second conversion step for further treatment therein.
The invention will be more fully explained in connection with the attached diagrammatic flow drawing which illustrates several specific embodiments of the invention. The embodiments in the invention illustrated describe a process using fluidized operation which, as heretofore stated, is preferred. However, the invention may be practiced in a process using other types of operation.
Referring to the drawing, a hydrocarbon charging oil such as kerosene, gas oil, or any other hydrocarbon oil heavier than gasoline, is supplied through line I and valve 2 to pump 3, by means of which it is directed through line 4 and valve 5 and is admixed with a low boiling high olefin content gasoline fraction formed in the process, in the manner to be hereinafter described in detail, and directed through line 5 and valve 1 to commingle with the charging oil in line I. The mixture is then directed into and through heating coil 8 in furnace structure 9, wherein the mixture is heated to the desired temperature. Heated products are then directed through line I0 and valve Il, whereafter they are commingled with fresh or reactivated powdered catalyst introduced through standpipe l2 and valve I3 and obtained in the manner to be hereinafter described in detail. The mixture of oil and catalyst is then directed through line I4 into reactor I5 which comprises the iirst conversion step o! the process for the production of a low boiling low olefin content gasoline fraction.
In reactor I a turbulent mass of catalyst powder is maintained in constant agitation by a rising stream of reactants introduced by means of line I4 and the conversion products formed during the reaction. The top of this turbulent bed is indicated diagrammatically by line i5. As previously mentioned, the temperature in this zone will ordinarily range from approximately 600 to approximately 1000 F. and preferably will be from about 850 to about 950 F. Pressure in this zone will ordinarily be slightly above atmospheric and may be of the order of 5 to 25 pounds per square inch gauge, although in some cases pressures as high as 100 pounds per square inch gauge or more may be employed. Weight hourly space velocities will usually not be greater than l, although, as hertofore mentioned, higher space velocities may be employed depending upon the temperature utilized.
Vaporous conversion products containing some suspended catalyst are withdrawn from the top of reactor |5 through cyclone separator I1 wherein entrained catalyst is separated from the vaporous conversion products and returned through line |5 to the reactor. The conversion products are then withdrawn through line |9 and valve 20 and are supplied to fractionator 2| wherein a low olen content gasoline fraction is separated from heavier hydrocarbons.
As heretofore mentioned, the low olen low boiling gasoline fraction may have an end boiling point within `the range of from about 200 to about 400 F. and more generally will have an end boiling point of from about 200 to about 250 F. This fraction is withdrawn from the upper portion of fractionator 2| through line 22 and valve 23 into and through condenser 24, through line rundown 25 and valve 25 into receiver 21. AIn receiver 21, a separation is effected between the gaseous phase and the liquid phase, the gaseous phase being withdrawn through line 28 and valve 29 to storage or elsewhere as desired. This gaseous-phase will contain a relatively high proportion of isobutane and is particularly suitable for use in subsequent alkylation or other conversion treatments. The distillate collected in receiver 21 is withdrawn therefrom through line 30 and valve 3| to pump 32, by means of which it is directed through line 33 and a portion thereof recycled by way of line 34 and valve 35 to the upper portion of fractionator 2| to serve as a reuxing and cooling medium therein while the remaining portion of the distillate is directed through line 35 and valve 31 and is recovered as the iinal low boiling gasoline product of the process.
The heavier oil separated in fractionator 2| is withdrawn therefrom through line 35 and valve 39 to pump 40, by means of which all or a portion thereof is supplied through line 4| and valve 42 to heating coil 43 which is positioned in furnace structure 44. Prior to its introduction into heating coil 43, the heavier oil may be commingled with a, recycle oil formed in the process, in the manner to lne/hereinafter described, and directed through line 45 ,and valve 45 into line 4|. The heavier oil introduced into line 43 is heated therein to the desired temperature and is then directed through line 41 and valve 45, whereafter it is commingled with a partly spent powdered catalyst introduced through valve 49 rand standpipe 50 and obtained in the manner to be hereinafter described in detail. The resulting mixture of catalyst and oil is then directed through line 5| into reactor 52. When desired, a portion of the heavier oil may be diverted from line 41 through line 53 and valve 54, to commingle with a portion oi the freshly regenerated catalyst withdrawn through valve 55 and standpipe 55, the resulting mixture being directed through line 51 into reactor 52.
Reactor 52 may be similar in design to reactor I5 and thus line 55 indicates the top of the turrbulent bed, numeral 59 indicates the cyclone separator and line 50 is provided for the return of catalyst back to the reactor. However, as heretofore mentioned, reactorv 52 will be operated at a temperature within the range of from about 900 to about 1200 F. at a. Weight hourly space velocity which will usually be greater than l, these operating conditions being dependent upon the activity of the particular catalyst employed.
The vaporous conversion products containing some suspended catalyst are directed through cyclone separator 59 in which the catalyst is separated out and the hydrocarbon conversion products are then directed through line 5| and valve 52 into fractionator 53. In fractionator 53 a low boiling high olefin content gasoline fraction is separated and this fraction may have an end boiling point similar to or diierent than that heretofore described in connection with the overhead products withdrawn through line 22 from fractionator 2|. Usually this `fraction will have an end boiling point within the range of from a'boutA 200 to about 250 F. and is directed through line 54 and valve 55 into and through condenser 55 and rundown line 51 containing valve 58 into receiver 59. The gases are released from receiver 59 through line 10 and valve 1|. These gases will be relatively rich in oleilns and therefore are particularly suitable for use in either alkylation, polymerization, or other suitable conversion processes. \.The distillate collected in receiver 59 is withdrawn therefrom through line 12 and valve 13 to pump 14, by means of which it is supplied through line 15 and a portion thereof recycled by way of line 15 and valve 11 to the upper portion of fractionator 53 to serve as a cooling and reiluxing medium therein. A portion of the distillate from receiver 59 may be withdrawn to storage or elsewhere as desired through line 18 and valve 19 but, in accordance with the present invention, at least a portion of the distillate is directed through line 5 and valve 1 to commingle with the hydrocarbon charging oil introduced through line in the manner heretofore described.
In one embodiment of the invention an intermediate naphtha fraction having an initial boiling point within the range of from about 200 to about 350 F. and an end boiling point within the range of from about 250 to about 400 F., preferably one having an initial boiling point within the range of from about 200 to about 300 F. and an end fboiling point within the range of from about 250 to about 350 F., may be separated from other products in fractionator 53 and withdrawn therefrom through line B0 and valve 5| to storage or elsewhere as desired. In the production of aviation gasoline, it is a particular feature of the present invention that a naphtha fraction having an initial boiling point from about 200 to 250 F. and an end boiling point from about 275 to about 325 F. is withdrawn through line 50 and is directed through line 82 containing valve 83 to pump 84, by means of which it is supplied through line 85 and valve 30 into line 30 or otherwise commingled with the low boiling low oleiin gasoline fraction. The naphtha fraction will be low in olefin content and high in aromatic content so that it is particularly suitable for use as a blending agent in aviation gasoline.
The heavier oil separated in fractlonator 33 may be withdrawn therefrom through line 01 and withdrawn from the process through line I3 and valve 80 to storage or elsewhere as desired. When desired, the heavier oil may be directed through line and valve 9| to pump 92 by means of which it is recycled by way of line 45, valve 40 and line 4| to heating coil 43 for subsequent further treatment in reactor 52. It is also within the scope of the invention to separate a heavy naphtha fraction in fractionator 33 and withdraw the same through line ||4 and valve lli. 'I'his heavy naphtha fraction will have an initial boiling point above the intermediate naphtha fraction withdrawn through line 80 and an end lboiling point within the range of from about 400 toI about 500 F. 'I'he heavy naphtha fraction may be recycled for further treatment by way of lines 90, 45, 4|, 41 and 5I into reactor 52.
The spent catalyst in reactor 52 is directed into standpipe 93 wherein the catalyst is stripped of its volatile hydrocarbons absorbed therein by an upwardly moving stream of gas, such as steam, fluegas, etc., introduced through line 34 and valve 95. This gas not only serves to strip volatile hydrocarbons from the catalyst but also serves to maintain the powdered catalyst in a fiuidized state so that the suspension will readily ow like a liquid. 'I'he spent catalyst is supplied through valve 96 and is picked up bya stream of air or other suitable oxidizing gas introduced through line 91 and valve 90 and the mixture is supplied through line 09 to regenerator |00 wherein the hydrocarbonaceous deposit formed on the catalyst is removed from the catalyst by a combustion reaction. In the regenerator, as
in the reactors, a turbulent bed of'powdered catalyst is maintained by means of an upwardly flowing stream of oxygen-containing gas. The upper limit of this bed is illustrated diagrammatically by line lli. Above this point, the concentration of the catalyst steadily diminishes, while below this point, a very high concentration of catalyst is maintained.
Spent reactivated gases are withdrawn from the regenerator through cyclone separator |02 wherein entrained catalyst is thrown out by centrifugal action and returned to the catalyst bed through line |03. Vent regenerating gases are removed through line |04 containing valve |05. It is usually necessary to remove heat from the regenerator in order that the regeneration temperature will not exceed a certain maximum, and any suitable means, not illustrated, may be employed for this purpose such-as, for example, cooling and recycling a portion of the regenerated catalyst or the positioning of a closed cooling coil within the regeneration zone.
Theregenerated catalyst is withdrawn from the regenerator through standpipe I 06 wherein the catalyst is contacted with an upwardly moving stream of inert gases, preferably steam or flue gases, introduced through line |01 containing control valve 00, to desorb any oxygen which may be present with the catalyst. The catalyst withdrawn through standpipe |06 may be supplied in part through line 56 as heretofore mentioned, but at least a portion of the regenerated catalyst is directed through line |09 to be picked up bythe heated charging oil being supplied through line I0 as heretofore described. Heat exchanger ||0 is provided in case it is desired to either cool or heat the catalyst prior to introduction to reactor l5. Usually the catalyst is at too high a temperature when withdrawn from the regenerating zone and heat exchanger ||I suitably comprises a cooling zone. In some cases it may be satisfactory to heat the charging oil in coil 3 to a lower temperature and then obtain additional heat from the hot regenerated catalyst, thus eliminating heat exchanger lli.
The catalyst in reactor II, after it has served to effect conversion of the charging oil and low boiling high olefin gasoline, is withdrawn through standpipe Ill into line Il. Line H2 containing valve H3 is provided for the introduction of a suitable stripping medium to remove volatile hydrocarbons from the catalyst and to maintain the powdered catalyst in fluidized state. It is a particular feature of the present invention that this catalyst, after having been used in the first conversion step, will retain sufficient activity for use in the second conversion step of the process.
The following example is introduced for the purpose of further illustrating the novelty and utility of the present invention but not with the intention of unduly limiting the same.
A 32 A. P. I. gravityv Mid-Continent gas oil may be commingled with an oleiinic gasoline fraction having an end boiling point of about 250 F. and the mixture subjected to conversion in the presence of a silica-alumina catalyst at Table First step Second step Total C; and lighter 8. 9 6. 7 15.0 Butylenes...... 3.3 1.7 5.0 Isobutane 7. 3 3. 7 ll. 0
Normal butan l.l 0.6 |.7 Amylenes... 2.8 l.l 3.9 Isopentane 5. 8 2. 2 8.0 N orma] pentann 0. 8 0.3 l. l (.g t0 250 F 12.3 7. 2 19.5 250 to 340 F.. 5.0 5.0 340to400F... 7.6 7.6. Recycle stock ll. 4 ll. 4
Coke 6.4 3.a 10.2
a temperature of about 850 F, 'and an hourly weight space velocity of .5. A low olefin, high antiknock gasoline fraction having an end boiling point of about 250 F. may be separated from the conversion products and the heavier hydrocarbon oil commingled with the spent catalyst from the first conversion step and subjected to cracking at a temperature of about 950 F. and at a weight hourly liquid space velocity of about 1.7.
On the basis of an operation such as described above, the following products are obtainable, these productsbeing reported on the basis of weight per cent of the gas oil charging stock:
It is to be noted from the above table that 19.5% of low boiling low olefin content gasoline. based upon the gas oil charge, is, produced. This gasoline is of high antiknock value and is particularly suitable for use as aviation base blending fuel. In addition therelis produced 5% of naphtha boiling between 250 and 340 F. and 7.6% of naphtha having an end point of 400 F. All or a portion of the 340 F. end .boiling point naphtha may be blended with the low boiling gasoline fraction to increase the yield of aviation base gasoline stock.
It is to be further noted that there also is produced 11.0% of isobutane, 8.0% of isopentane as well as of butylenes. The isopentane may be blended with the aviation gasoline, while the isobutane and butylenes may be utilized in a1- kylation reactions for the production of an alkvlate which may also be used in the aviation gasoline.
The above results are compared to a two-step process in which the charging stock is cracked at a temperature of about 950 F. in the first step and the gasoline product therefrom is subjected to treatment in `a second stage at a temperature of about 900 F. In this operation there is produced 16% of a low olen high antiknock gasoline containing hydrocarbons having 6 carbon atoms to the molecule up to 340 F. end boiling point. It is to be noted that the 16% of desired gasoline for aviation base blending fuel from the last mentioned treatment is lower than the 24.5% of similar low boiling high antiknock gasoline (19.5% Cc to 250 F. 5% 250 to 340 F.) produced in accordance with the present invention. Likewise, the percent of isobutane produced in the other type of operation is 8.5% which is lower than ,11.0% produced in accordance with the present invention. Both of these operations are based upon a similar coke production of 10.2% by weight of the charging stock.
I claim as my invention:
1. A process for the manufacture of a gasoline of low olen content, high antiknock value and suitable for use in aviation gasoline which comprises commingling an oil heavier than gasoline with a gasoline of higher olefin content than said first mentioned gasoline, and utilizing the commingled stream to convey freshly regenerated powdered cracking catalyst into a rst reaction zone operated at a temperature within the range of from about 600 to about 1000 F. and under conditions whereby the net upward flow of hydrocarbons is greater than that of the catalyst and to produce a low olefin content gasoline, withdrawing the vaporous conversion products from said reaction zone and separating the same into a low olefin content gasoline having an end boiling point within the range of from about 200 to about 300 F., and heavier hydrocarbons, recovering said low olefin content gasoline as the product of the process, withdrawing the partly spent cracking catalyst from said reactor and utilizing said heavier hydrocarbons to convey said partly spent catalyst into a second reaction zone operated at a temperature within the range of from about 900 to about 1200 F. and under conditions whereby the net upward iiow of hydrocarbons is greater than that of the catalyst and to produce a high olen content gasoline, withdrawing the vaporous conversion products from the second reaction zone and separating the same into a high olefin content gasoline having an end boiling point within the range of from about 200 to about 300 F. and heavier hydrocarbons, commingling said high olen content gasoline with said oil heavier than gasoline as aforesaid, withdrawing the spent catalyst from said second reaction zone and conveying the same by means of an oxygen-containing gas to a regenerating zone in which the catalyst undergoes regeneration, withdrawing the regenerated catalyst from the regenerating zone and supplying the same to said rst reaction zone in the manner heretofore described,
2. The process of claim 1 further characterized in that a portion of said regenerated catalyst is supplied to the second reaction zone by means of a portion of the heavier oil separated from products of the rst reaction zone.
3. In the catalytic cracking of hydrocarbons wherein used cracking catalyst from the hydrocarbon conversion is regenerated in a regenerating zone, the process which comprises removing regenerated catalyst from said zone and introducing the same to a rst conversion zone, simultaneously introducing to said conversion zone hydrocarbon oil heavier than gasoline and olenic hydrocarbons boiling in the gasoline range, contacting-the hydrocarbons with the catalyst in said conversion zone under conditions to produce gasoline of low olefin content therefrom, separately removing vapors and partially spent catalyst from the conversion zone, fractionating the vapors to separate fractions thereof heavier than gasoline, introducing at least a portion of said fractions and said partially spent catalyst to a second conversion zone maintained at higher temperature than said first conversion zone and therein cracking the heavier than gasoline fractions in the presence of the partially spent catalyst to produce oleiinic gasoline therefrom, separately removing vapors and used catalyst from said second zone and introducing the latter to said regenerating zone, fractionating the last-mentioned vapors to separate cleflnic gasoline therefrom, and supplying at least a portion of said oleiinic gasoline to the first conversion zone.
4. The process as defined in claim 3 further characterized in that the first conversion zone is maintained at a. temperature of from about' 600 F. to about 1000 F. and the second conversion zone at a temperature of from about 900 F. to about 1200 F.
5. The process as defined in claim 3 further l characterized in that the irst conversion zone is maintained at a, temperature ofrfrom about 600 to about 1000 F. and the second conversion zone at a temperature of from about 900 F. to about 1200 F., the hydrocarbons in said first zone being contacted with the catalyst therein at a weight hourly space velocity not greater than 1 and the hydrocarbon in said second zone being contacted with the catalyst therein at a weight hourly space velocity greater than 1.
6. 'I'he process as defined in claim 3 further characterized ln that reflux condensate from the second-mentioned fractionating step is recycled to said second conversion zone.
7. The process as dened in claim 3 further characterized in that freshly regenerated catalyst is supplied from the regenerating zone to said second conversion zone.
ELMER R. KANHOFER.
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Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2432277A (en) * 1945-01-02 1947-12-09 Shell Dev Catalytic cracking of hydrocarbon oils
US2444131A (en) * 1946-03-01 1948-06-29 Universal Oil Prod Co Conversion of hydrocarbon oils
US2461958A (en) * 1944-12-14 1949-02-15 Standard Oil Dev Co Treating hydrocarbon fluids
US2462891A (en) * 1949-03-01 Contact conversion of
US2550290A (en) * 1951-04-24 Catalytic cracking of hydrocarbons
US2919241A (en) * 1955-06-17 1959-12-29 Kellogg M W Co Conversion process and apparatus with plural adjacent stages and central stripping zone
FR2155962A1 (en) * 1971-10-05 1973-05-25 Mobil Oil Corp
US4090948A (en) * 1977-01-17 1978-05-23 Schwarzenbek Eugene F Catalytic cracking process

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2462891A (en) * 1949-03-01 Contact conversion of
US2550290A (en) * 1951-04-24 Catalytic cracking of hydrocarbons
US2461958A (en) * 1944-12-14 1949-02-15 Standard Oil Dev Co Treating hydrocarbon fluids
US2432277A (en) * 1945-01-02 1947-12-09 Shell Dev Catalytic cracking of hydrocarbon oils
US2444131A (en) * 1946-03-01 1948-06-29 Universal Oil Prod Co Conversion of hydrocarbon oils
US2919241A (en) * 1955-06-17 1959-12-29 Kellogg M W Co Conversion process and apparatus with plural adjacent stages and central stripping zone
FR2155962A1 (en) * 1971-10-05 1973-05-25 Mobil Oil Corp
US4090948A (en) * 1977-01-17 1978-05-23 Schwarzenbek Eugene F Catalytic cracking process

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