US2728646A - Gasoline containing corrosion inhibitor - Google Patents

Gasoline containing corrosion inhibitor Download PDF

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US2728646A
US2728646A US279925A US27992552A US2728646A US 2728646 A US2728646 A US 2728646A US 279925 A US279925 A US 279925A US 27992552 A US27992552 A US 27992552A US 2728646 A US2728646 A US 2728646A
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gasoline
aniline
phosphate
corrosion
acid phosphate
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Vaughn Samuel Clyde
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TIDE WATER ASSOCIATED OIL Co
TIDE WATER ASSOCIATED OIL COMP
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TIDE WATER ASSOCIATED OIL COMP
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    • CCHEMISTRY; METALLURGY
    • C10PETROLEUM, GAS OR COKE INDUSTRIES; TECHNICAL GASES CONTAINING CARBON MONOXIDE; FUELS; LUBRICANTS; PEAT
    • C10LFUELS NOT OTHERWISE PROVIDED FOR; NATURAL GAS; SYNTHETIC NATURAL GAS OBTAINED BY PROCESSES NOT COVERED BY SUBCLASSES C10G, C10K; LIQUEFIED PETROLEUM GAS; ADDING MATERIALS TO FUELS OR FIRES TO REDUCE SMOKE OR UNDESIRABLE DEPOSITS OR TO FACILITATE SOOT REMOVAL; FIRELIGHTERS
    • C10L1/00Liquid carbonaceous fuels
    • C10L1/10Liquid carbonaceous fuels containing additives
    • C10L1/14Organic compounds
    • CCHEMISTRY; METALLURGY
    • C10PETROLEUM, GAS OR COKE INDUSTRIES; TECHNICAL GASES CONTAINING CARBON MONOXIDE; FUELS; LUBRICANTS; PEAT
    • C10LFUELS NOT OTHERWISE PROVIDED FOR; NATURAL GAS; SYNTHETIC NATURAL GAS OBTAINED BY PROCESSES NOT COVERED BY SUBCLASSES C10G, C10K; LIQUEFIED PETROLEUM GAS; ADDING MATERIALS TO FUELS OR FIRES TO REDUCE SMOKE OR UNDESIRABLE DEPOSITS OR TO FACILITATE SOOT REMOVAL; FIRELIGHTERS
    • C10L1/00Liquid carbonaceous fuels
    • C10L1/10Liquid carbonaceous fuels containing additives
    • C10L1/14Organic compounds
    • C10L1/22Organic compounds containing nitrogen
    • C10L1/222Organic compounds containing nitrogen containing at least one carbon-to-nitrogen single bond
    • C10L1/223Organic compounds containing nitrogen containing at least one carbon-to-nitrogen single bond having at least one amino group bound to an aromatic carbon atom
    • CCHEMISTRY; METALLURGY
    • C10PETROLEUM, GAS OR COKE INDUSTRIES; TECHNICAL GASES CONTAINING CARBON MONOXIDE; FUELS; LUBRICANTS; PEAT
    • C10LFUELS NOT OTHERWISE PROVIDED FOR; NATURAL GAS; SYNTHETIC NATURAL GAS OBTAINED BY PROCESSES NOT COVERED BY SUBCLASSES C10G, C10K; LIQUEFIED PETROLEUM GAS; ADDING MATERIALS TO FUELS OR FIRES TO REDUCE SMOKE OR UNDESIRABLE DEPOSITS OR TO FACILITATE SOOT REMOVAL; FIRELIGHTERS
    • C10L1/00Liquid carbonaceous fuels
    • C10L1/10Liquid carbonaceous fuels containing additives
    • C10L1/14Organic compounds
    • C10L1/26Organic compounds containing phosphorus
    • C10L1/2633Organic compounds containing phosphorus phosphorus bond to oxygen (no P. C. bond)
    • C10L1/2658Organic compounds containing phosphorus phosphorus bond to oxygen (no P. C. bond) amine salts

Definitions

  • the present invention relates to corrosion inhibitors for gasolines having high octane ratings, and especially those gasolines designed for use in aircraft type internal combustion engine. More particularly, it relates to corrosion inhibitors formed as reaction products from alkyl acid phosphates and certain amines, and, which are compatible with other desirable additives. It further relates to anti-corrosive gasoline and means for producing the same. It also relates to the means for manufacturing corrosion inhibitors.
  • the appearance of water as a separate phase in aviation gasoline may be caused either by entrained water from the fueling pumps used in fueling aircraft, since these use water displacement to pump the gasoline; or, by moisture in the air above the gasoline in the fuel tank, since, at temperatures prevalent in high altitude flying, the moisture condenses and precipitates.
  • Another class of important additives often used in aviation gasoline is composedof certain anti-knock agents designed particularly for rich mixture operation.
  • these additives are aniline and its homologs, such as for example, ethyl aniline, methyl aniline, amyl aniline, diamyl aniline, cumidine, and xylidine.
  • aromatic amines are very effective for this particular purpose when used in proportions of about one to three percent of the gasoline, and function as cumene substitutes in aviation gasoline blends.
  • the amine and alkyl acid phosphate may be reacted, or neutralized, by mixing the theoretical neutralizing quantities of the two components, heating above room temperature, care being taken not to exceed temperature at which decomposition takes place, and then thoroughly mixing until reaction is complete.
  • the reaction product is tested to determine the degree of neutralization, and after neutralization is confirmed as complete, said reaction product is then blended into gasoline as desired, or may be blended into a small amount of gasoline to be used as a gasoline concentrate.
  • the aniline or homolog thereof may be added in whatever order desired.
  • the aminealkyl acid phosphate neutralization product is insoluble in aniline and its homologs and as a consequence thereof a one package additive is not practical.
  • Another procedure for manufacturing the novel reaction products which inhibit corrosion comprises dissolving the amine or gasoline concentrate of amine in the gasoline to be treated, and then adding a predetermined amount of alkyl acid phosphate.
  • the alkyl acid phosphate may be added to the gasoline and then the required amount of amine. added.
  • the blend is then mixed thoroughly for about a half-hour to insure complete reaction.
  • a similar procedure may be followed for the preparation of a gasoline concentrate, should this be desired.
  • the blend or concentrate is then tested for degree of neutralization, and when found to be satisfactory as evidenced by its non-precipitation or non-haze formation, the aniline or its homolog, or a gasoline concentrate thereof, may then be added and the gasoline thoroughly mixed for ultimate use.
  • the alkyl acid phosphates which may be used in the neutralization step of the present process are those having from 8 to 16 carbon atoms per alkyl group.
  • the preferred alkyl acid phosphate is Lorol acid phosphate, which is a mixture of the phosphoric esters of Lorol alcohol.
  • Lorol alcohol is used in the trade to denote a mixture of primary normal aliphatic alcohols of 8 to 12 carbon atoms which are obtained by fractionation of the alcohols resulting from the reduction of cocoanut and/or palm kernel oils. Lorol acid phosphate mixtures are readily obtainable on the market and for this reason are preferred to the more purified esters of greater scarcity and higher price.
  • the proper proportions of amino bicyclo hexyl and alkyl acid phosphate may readily be determined by an electrome'tric titration of a sample of the alkyl acid phosphate with aqueous KOH solution to a pHof' about 9. From the amount of KOH used the quantity of amine required to neutralize the acid radicals of the phosphate may easily becalculated. It is always desirable to' have a slight excess of amine present, and good results have beenobtained with as much as 50% excess of amino bicyclo hexyl.
  • the lower concentration limit of the reaction. product with respect to the finished gasoline should be about 0.002% by Weight. This was determined by means of'ASTM' D665-47T corrosion test modified to a-hath temperature of 80'82 F.
  • the upper concentration limit is determinedbythat amount of neutralization product which would cause engine deterioration clue to the excessive quantity of phosphates then present. The upper limit is about 0.05% by weight.
  • Example 1 Into a suitable vessel equipped with means for heating, agitating, and'cooling the charge, there are introduced 154' parts by weight of ortho amino bicyclo hexyl, followed gradually by 150 parts of a mixture of mono. and di.
  • Lorol acid phosphates (Ortholeum 162).
  • the mixture is agitated vigorously and cooled as required to keep the temperature below 200 F.
  • the reaction is vigorous'and exothermic, consequently the rate of addition of the phosphate is controlled to avoid exceeding the above temperature limit.
  • the resulting mixture is stirred for about 1 hour at 140 F.
  • the reaction product is a viscous, oily liquid, yellow in color.
  • the reaction product is then tested for neutrality by means of the aforementioned neutralization test, and, if found to be acid, additional amino bicyclo hexyl'is added. Finally, five pounds of the finished additive are added to 17,000 gallons of aviation gasoline in a blender and agitated for about 15 minutes.
  • Example II A 10% by weight solution in gasoline of the finished additive from Example I is prepared by dissolving 100 pounds of the reaction product in 900 pounds of gasoline in a mixer. The gasoline-additive concentrate is thoroughly mixed for about one hour, and 50 pounds of this concentrate then blended into 17,000 gallons of aviation gasoline. The resulting mixture is agitated for about minutes. Finall, 1020 pounds of mixed xylidines are added and mixing continued for an additional 30 minutes. This finished product is comparable to that obtained in Example i.
  • Example III To 17,000 gallons of aviation gasoline in a blender are added 2.94 lbs. of ortho amino bicyclo hexyl. The resulting mixture is thoroughly agitated for about 10 minutes, and then 2.68 pounds of a mixture of mono and di Lorol. acid phosphate (Ortholeurn 162) are added with continued mixing for about one-half hour. After the neutralization testsindicate theproduction of a satisfac- 4 tory reaction product, 1020 pounds of mono methyl aniline are added and" a'g'i't'atit'an continued for another halfhour. As in the former examples, tests indicate the production of excellent quality finished gasoline.
  • Example IV The same procedure is used as in Example I except that 77 parts by'weight of 'meta' amino bicyclo'hexyl are used in lieu of 154' parts by weight of ortho amino bicyclo hexyl; and, parts by weight of Ortholeum 162 is used in lieu of parts by weight.
  • Example V factory reaction product 340 pounds of mono methyl aniline are added and agitation continued for another half-hour. As in the former examples, tests indicate theproduction of excellent quality finished gasoline.
  • aviation gasolines are used inthe above examples forpurposes of illustration, and such gasolines may comprise the following:
  • the. invention in its broadest scope comprehends the treatment of any motor fuel.
  • the reaction product of the present invention may be blended in proper proportions in any desired: gasolinewith the-advantage that the purchaseror user may add any suitable amount of aniline or homologs thereof, for the purpose of obtaining. rich mixture anti-knock properties, without difiiculties arising from precipitation or haze formation which is generally encountered when less satisfactory corrosion inhibitors are used.
  • a completely homogeneous, corrosion-resistantaviation' fuel having a high rich mixture anti-knock rating comprising gasoline containing. sufficient aromatic amine from the group consisting of aniline. and homologs of aniline to substantially increase the rich mixture antiknoclc' properties of the gasoline and between 0.002% and 0.05% by weight of the' finished gasoline of the addition product resulting from contacting an alkyl acid phosphate having from 8 to 16 carbon atoms per alkyl group with between 1.00% and 150% of the quantity theoretically required to neutralize said phosphate of amino bicyclo hexyl.
  • alkyl acid phosphate is a phosphoric acid ester derived from a mixture of primary normal aliphaticalcohols of 8 to" 12 carbon atoms obtainable by the fractionation of alcohols resulting from the reduction of cocoanut oil.
  • An anti-corrosive gasoline as in claim 1 which contains in addition sufiicient tetraethyl lead to increase the anti-knock properties.
  • the method of simultaneously improving the anticorrosive and the rich mixture anti-knock properties of a gasoline which comprises forming in said gasoline a corrosion inhibiting amount of the addition product of an alkyl acid phosphate having 8 to 16 carbon atoms per alkyl group and amino bicyclo hexyl and in which all the acid hydrogen of said phosphate is neutralized by said amino bicyclo hexyl, then adding suflicient aromatic amine from the group consisting of aniline and homologs of aniline to substantially increase the rich mixture anti-knock properties.
  • the method of inhibiting the formation of an insoluble precipitate when an amine-phosphate corrosion inhibitor is added to a gasoline containing an aniline octane booster which comprises adding to a gasoline an alkyl acid phosphate having 8 to 16 carbon atoms per alkyl group, adding between 100% and about 150% of the quantity theoretically required to neutralize all the acid hydrogen of said phosphate of amino bicyclo hexyl thereby forming in said gasoline an addition product of said amine with said phosphate, then adding sufficient aromatic amine from the group consisting of aniline and homologs of aniline to substantially increase the rich mixture anti-knock properties of the gasoline, the amounts of the amino bicyclo hexyl and the alkyl acid phosphate being sufficient to produce an addition product of between 0.002% and 0.05% by weight of the finished gasoline.

Description

GASOLINE CONTAINING CORROSION INHIBITOR No Drawing. Application April 1, 1952, Serial No. 279,925
7 Claims. (Cl. 44-60 The present invention relates to corrosion inhibitors for gasolines having high octane ratings, and especially those gasolines designed for use in aircraft type internal combustion engine. More particularly, it relates to corrosion inhibitors formed as reaction products from alkyl acid phosphates and certain amines, and, which are compatible with other desirable additives. It further relates to anti-corrosive gasoline and means for producing the same. It also relates to the means for manufacturing corrosion inhibitors.
Recently, corrosion inhibitors for gasoline have attained importance as a result of research designed to inhibit corrosion in fuel systems and storage tanks, particularly where moist gasoline may come in contact with such metals as iron, copper, brass or the like. This type of corrosion is caused usually by the presence of water, and occurs generally at the water-gasoline interface. Furthermore, various components used in leaded gasolines are thought to be active promoters of corrosion. g
The appearance of water as a separate phase in aviation gasoline may be caused either by entrained water from the fueling pumps used in fueling aircraft, since these use water displacement to pump the gasoline; or, by moisture in the air above the gasoline in the fuel tank, since, at temperatures prevalent in high altitude flying, the moisture condenses and precipitates.
Another class of important additives often used in aviation gasoline is composedof certain anti-knock agents designed particularly for rich mixture operation. Foremost among these additives are aniline and its homologs, such as for example, ethyl aniline, methyl aniline, amyl aniline, diamyl aniline, cumidine, and xylidine. These aromatic amines are very effective for this particular purpose when used in proportions of about one to three percent of the gasoline, and function as cumene substitutes in aviation gasoline blends.
Although corrosion inhibitors and the above mentioned anti knock agents function excellently when each isz'used in the absence of the other, many of the common corrosion inhibitors are not compatible therewitha Consequent- -ly, when many of the alkyl acid'phosphate-amine neutralization products conventionally used for anti-corrosion purposes are added to a gasoline containing aniline or a homolog of aniline, an undesirable precipitate or-haze forms. The deleterious effects of precipitates in liquid fuels are well recognized, and in this instance they may Amino bicyclo hexyl, also know as amino dicyclo hexyl States Patent 2,728,646 Patented Dec. 27, 1955 or carbon substituted cyclohexyl cyclohexyl amine, may be produced as either the ortho, para, or meta isomers, each of which is satisfactory for use in the present invention.
While certain variations and deviations from the teachings of the present invention are encompassed within its scope and spirit, it is nevertheless recommended that the process of manufacturing the finished gasolines containing desired additives be carried out in specified steps. For example, the order of addition of materials as well as the method of mixing the components must follow definite patterns.
The amine and alkyl acid phosphate may be reacted, or neutralized, by mixing the theoretical neutralizing quantities of the two components, heating above room temperature, care being taken not to exceed temperature at which decomposition takes place, and then thoroughly mixing until reaction is complete. The reaction product is tested to determine the degree of neutralization, and after neutralization is confirmed as complete, said reaction product is then blended into gasoline as desired, or may be blended into a small amount of gasoline to be used as a gasoline concentrate. The aniline or homolog thereof may be added in whatever order desired. However, the aminealkyl acid phosphate neutralization product is insoluble in aniline and its homologs and as a consequence thereof a one package additive is not practical.
Another procedure for manufacturing the novel reaction products which inhibit corrosion comprises dissolving the amine or gasoline concentrate of amine in the gasoline to be treated, and then adding a predetermined amount of alkyl acid phosphate. Alternately, the alkyl acid phosphate may be added to the gasoline and then the required amount of amine. added. The blend is then mixed thoroughly for about a half-hour to insure complete reaction. A similar procedure may be followed for the preparation of a gasoline concentrate, should this be desired. The blend or concentrate is then tested for degree of neutralization, and when found to be satisfactory as evidenced by its non-precipitation or non-haze formation, the aniline or its homolog, or a gasoline concentrate thereof, may then be added and the gasoline thoroughly mixed for ultimate use.
It is an important qualification of the present process that the aniline or homolog thereof never be mixed with a blend containing the alkyl acid phosphate until all of the acidity of the alkyl acid phosphate has been neutralized by the amine. To test the degree of neutralization, the following procedure has been found to be effective. A drop of the reaction mixture is added to a 1% solution of aniline in aviation gasoline. If precipitation occurs on mixing then a small additional quantity of the amine is added to the reaction mixture with continued heating and agitation. This procedure is followed until a non-precipitating reaction product is finally formed from the alkyl acid phosphate and amino bicycle hexyl.
The alkyl acid phosphates which may be used in the neutralization step of the present process are those having from 8 to 16 carbon atoms per alkyl group. Mainly for commercial reasons, the preferred alkyl acid phosphate is Lorol acid phosphate, which is a mixture of the phosphoric esters of Lorol alcohol. The term Lorol alcohol is used in the trade to denote a mixture of primary normal aliphatic alcohols of 8 to 12 carbon atoms which are obtained by fractionation of the alcohols resulting from the reduction of cocoanut and/or palm kernel oils. Lorol acid phosphate mixtures are readily obtainable on the market and for this reason are preferred to the more purified esters of greater scarcity and higher price. One Lorol acid phosphate is sold under the trade name Ortholeurn 162 and is understood to be mainly a mixture of mono and di acid phosphates of Lorol alcohol. Though for the reasons stated above Lorol acid" phosphates are preferred, other alkyl acid phosphates containing from 8 to 16 carbon atoms per alkyl group are satisfactory. For example, a commercial grade of n=octyl acid phosphate was found to produce an excellent reaction product.
To form the'de'sir'ed neutralization product, the proper proportions of amino bicyclo hexyl and alkyl acid phosphate may readily be determined by an electrome'tric titration of a sample of the alkyl acid phosphate with aqueous KOH solution to a pHof' about 9. From the amount of KOH used the quantity of amine required to neutralize the acid radicals of the phosphate may easily becalculated. It is always desirable to' have a slight excess of amine present, and good results have beenobtained with as much as 50% excess of amino bicyclo hexyl.
In order to prevent corrosion effectively, the lower concentration limit of the reaction. product with respect to the finished gasoline should be about 0.002% by Weight. This was determined by means of'ASTM' D665-47T corrosion test modified to a-hath temperature of 80'82 F. The upper concentration limit is determinedbythat amount of neutralization product which would cause engine deterioration clue to the excessive quantity of phosphates then present. The upper limit is about 0.05% by weight.
Certainembodiments of the present invention are more fully illustrated by thefollowing examples:
Example 1 Into a suitable vessel equipped with means for heating, agitating, and'cooling the charge, there are introduced 154' parts by weight of ortho amino bicyclo hexyl, followed gradually by 150 parts of a mixture of mono. and di.
Lorol acid phosphates (Ortholeum 162). The mixture is agitated vigorously and cooled as required to keep the temperature below 200 F. The reaction is vigorous'and exothermic, consequently the rate of addition of the phosphate is controlled to avoid exceeding the above temperature limit. The resulting mixture is stirred for about 1 hour at 140 F. The reaction product is a viscous, oily liquid, yellow in color. v The reaction product is then tested for neutrality by means of the aforementioned neutralization test, and, if found to be acid, additional amino bicyclo hexyl'is added. Finally, five pounds of the finished additive are added to 17,000 gallons of aviation gasoline in a blender and agitated for about 15 minutes. Then 1020 pounds of mixed xylidines are added and the mixture resulting therefrom. is agitated for about a half-hour. The final gasoline is completely homogeneous, free from haze, corrosion resistant, and has a rich mixture anti-knock rating commensurate with the amount of xylidines used.
Example II A 10% by weight solution in gasoline of the finished additive from Example I is prepared by dissolving 100 pounds of the reaction product in 900 pounds of gasoline in a mixer. The gasoline-additive concentrate is thoroughly mixed for about one hour, and 50 pounds of this concentrate then blended into 17,000 gallons of aviation gasoline. The resulting mixture is agitated for about minutes. Finall, 1020 pounds of mixed xylidines are added and mixing continued for an additional 30 minutes. This finished product is comparable to that obtained in Example i.
Example III To 17,000 gallons of aviation gasoline in a blender are added 2.94 lbs. of ortho amino bicyclo hexyl. The resulting mixture is thoroughly agitated for about 10 minutes, and then 2.68 pounds of a mixture of mono and di Lorol. acid phosphate (Ortholeurn 162) are added with continued mixing for about one-half hour. After the neutralization testsindicate theproduction of a satisfac- 4 tory reaction product, 1020 pounds of mono methyl aniline are added and" a'g'i't'atit'an continued for another halfhour. As in the former examples, tests indicate the production of excellent quality finished gasoline.
Example IV The same procedure is used as in Example I except that 77 parts by'weight of 'meta' amino bicyclo'hexyl are used in lieu of 154' parts by weight of ortho amino bicyclo hexyl; and, parts by weight of Ortholeum 162 is used in lieu of parts by weight.
Example V factory reaction product, 340 pounds of mono methyl aniline are added and agitation continued for another half-hour. As in the former examples, tests indicate theproduction of excellent quality finished gasoline.
Although aviation gasolines are used inthe above examples forpurposes of illustration, and such gasolines may comprise the following:
Alkylate 70-88% Aromatics 516%. Isop'entane 5-14%. Tetra ethyl lead. 4 cc. per gallon.
nevertheless, the. invention in its broadest scope comprehends the treatment of any motor fuel. Similarly, it will be appreciated'that' the reaction product of the present invention may be blended in proper proportions in any desired: gasolinewith the-advantage that the purchaseror user may add any suitable amount of aniline or homologs thereof, for the purpose of obtaining. rich mixture anti-knock properties, without difiiculties arising from precipitation or haze formation which is generally encountered when less satisfactory corrosion inhibitors are used.
It will now be apparent that I' have devised a novel and useful process and composition of matter which embodies-the features of advantage enumerated as desirable in: the statement of the invention and the above description and while in the present instance there are described the preferred embodiments th'ereofiwhi'ch have been found in practice to give satisfactory and reliable results, it is to be' understood that the same is susceptible of modification in=v various: particulars without departing from the spirit or scope of the invention or sacrificing any of its advantages.
I claim:
1. A completely homogeneous, corrosion-resistantaviation' fuel having a high rich mixture anti-knock rating, comprising gasoline containing. sufficient aromatic amine from the group consisting of aniline. and homologs of aniline to substantially increase the rich mixture antiknoclc' properties of the gasoline and between 0.002% and 0.05% by weight of the' finished gasoline of the addition product resulting from contacting an alkyl acid phosphate having from 8 to 16 carbon atoms per alkyl group with between 1.00% and 150% of the quantity theoretically required to neutralize said phosphate of amino bicyclo hexyl.
2. An anti-corrosive gasoline as in claim 1 wherein the amino bicyclo hexyl is ortho amino bicyclo hexyl.
3'. An anti-corrosive gasoline as in claim 1 wherein the amino bicyclo. hexyl'is meta aminobicyclo hexyl.
4'. An anti-corrosive gasoline as in claim 1 wherein the alkyl acid phosphate is a phosphoric acid ester derived from a mixture of primary normal aliphaticalcohols of 8 to" 12 carbon atoms obtainable by the fractionation of alcohols resulting from the reduction of cocoanut oil.
5. An anti-corrosive gasoline as in claim 1 which contains in addition sufiicient tetraethyl lead to increase the anti-knock properties.
6. The method of simultaneously improving the anticorrosive and the rich mixture anti-knock properties of a gasoline, which comprises forming in said gasoline a corrosion inhibiting amount of the addition product of an alkyl acid phosphate having 8 to 16 carbon atoms per alkyl group and amino bicyclo hexyl and in which all the acid hydrogen of said phosphate is neutralized by said amino bicyclo hexyl, then adding suflicient aromatic amine from the group consisting of aniline and homologs of aniline to substantially increase the rich mixture anti-knock properties.
7. The method of inhibiting the formation of an insoluble precipitate when an amine-phosphate corrosion inhibitor is added to a gasoline containing an aniline octane booster, which comprises adding to a gasoline an alkyl acid phosphate having 8 to 16 carbon atoms per alkyl group, adding between 100% and about 150% of the quantity theoretically required to neutralize all the acid hydrogen of said phosphate of amino bicyclo hexyl thereby forming in said gasoline an addition product of said amine with said phosphate, then adding sufficient aromatic amine from the group consisting of aniline and homologs of aniline to substantially increase the rich mixture anti-knock properties of the gasoline, the amounts of the amino bicyclo hexyl and the alkyl acid phosphate being sufficient to produce an addition product of between 0.002% and 0.05% by weight of the finished gasoline.
References Cited in the file of this patent UNITED STATES PATENTS 2,297,114 Thompson Sept. 29, 1942 2,413,262 Stirton Dec. 24, 1946 2,550,982 Eberz May 1, 1951 2,656,375 Vaughn Oct. 20, 1953 FOREIGN PATENTS 222,547 Germany Nov. 2, 1942

Claims (1)

1. A COMPLETELY HOMOGENEOUS, CORROSION-RESISTANT AVIATION FUEL HAVING A HIGH RICH MIXTURE ANTI-KNOCK RATING, COMPRISING GASOLINE CONTAINING SUFFICIENT AROMATIC AMINE FROM THE GROUP CONSISTING OF ANILINE AND HOMOLOGS OF ANILINE TO SUBSTANTIALLY INCREASE THE RICH MIXTURE ANTIKNOCK PROPERTIES OF THE GASOLINE AND BETWEEN 0.002% AND 0.05% BY WEIGHT OF THE FINISHED GASOLINE OF THE ADDITION PRODUCT RESULTING FROM CONTACTIN AN ALKYL ACID PHOSPHATE HAVING FROM 8 TO 16 CARBON ATOMS PER ALKYL GROUP WITH BETWEEN 100% AND 150% OF THE QUANTITY THEORETICALLY REQUIRED TO NEUTRALIZE SAID PHOSPHATE OF AMINO BICYCLO HEXYL.
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Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3102071A (en) * 1960-02-08 1963-08-27 Commercial Solvents Corp Nematocidal compositions
US5650097A (en) * 1994-06-13 1997-07-22 E. I. Du Pont De Nemours And Company Corrosion inhibitor composition for steel
US6230683B1 (en) 1997-08-22 2001-05-15 Cummins Engine Company, Inc. Premixed charge compression ignition engine with optimal combustion control
US6276334B1 (en) 1998-02-23 2001-08-21 Cummins Engine Company, Inc. Premixed charge compression ignition engine with optimal combustion control
US6286482B1 (en) 1996-08-23 2001-09-11 Cummins Engine Company, Inc. Premixed charge compression ignition engine with optimal combustion control

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE222547C (en) * 1900-01-01
US2297114A (en) * 1940-06-24 1942-09-29 Universal Oil Prod Co Treatment of gasolines
US2413262A (en) * 1943-05-10 1946-12-24 Union Oil Co High-compression motor fuel
US2550982A (en) * 1947-07-12 1951-05-01 Petrolite Corp Fog inhibited hydrocarbon product and method
US2656375A (en) * 1951-09-06 1953-10-20 Tide Water Associated Oil Comp Amino bicyclohexyl-alkyl acid phosphate reaction product

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE222547C (en) * 1900-01-01
US2297114A (en) * 1940-06-24 1942-09-29 Universal Oil Prod Co Treatment of gasolines
US2413262A (en) * 1943-05-10 1946-12-24 Union Oil Co High-compression motor fuel
US2550982A (en) * 1947-07-12 1951-05-01 Petrolite Corp Fog inhibited hydrocarbon product and method
US2656375A (en) * 1951-09-06 1953-10-20 Tide Water Associated Oil Comp Amino bicyclohexyl-alkyl acid phosphate reaction product

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3102071A (en) * 1960-02-08 1963-08-27 Commercial Solvents Corp Nematocidal compositions
US5650097A (en) * 1994-06-13 1997-07-22 E. I. Du Pont De Nemours And Company Corrosion inhibitor composition for steel
US6286482B1 (en) 1996-08-23 2001-09-11 Cummins Engine Company, Inc. Premixed charge compression ignition engine with optimal combustion control
US6915776B2 (en) 1996-08-23 2005-07-12 Cummins Inc. Premixed charge compression ignition engine with optimal combustion control
US6230683B1 (en) 1997-08-22 2001-05-15 Cummins Engine Company, Inc. Premixed charge compression ignition engine with optimal combustion control
US6276334B1 (en) 1998-02-23 2001-08-21 Cummins Engine Company, Inc. Premixed charge compression ignition engine with optimal combustion control

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