US3642632A - Anthranilic acid esters as lubricant additives - Google Patents

Abstract

AN ESTER OF ANTHRANILIC ACID OR AN ESER OF A DERIVATIVE SUCH ACID HAVING THE GENERAL STRUCTURAL FORMULA:

(R-OOC-),(X-NH-)BENZENE

WHERE R IS A C1 TO C10 ALKYL GROUP AND X IS HYDROGEN, ALKYL OR A PHENYL GROUP, HAS BEEN FOUND TO BE AN EFFECTIVE OXIDATION AND CORROSION INHIBITOR IN LUBRICATING OILS, ESPECIALLY SYNTHETIC ESTER OILS.

Description

United States 3,642,632 ANTHRANILIC ACID ESTERS AS LUBRICANT ADDITIVES John F. Cohurn, 7 Franklin Ave., Cranford, NJ. 07016, and Stephen J. Metro, 1822 Lamherts Mill Road, Scotch Plains, NJ. 07076 No Drawing. Filed May 24, 1968, Ser. No. 731,735 Int. Cl. C1011! 1/26, 1/32 US. Cl. 252-515 A 4 Claims ABSTRACT OF THE DISCLOSURE BACKGROUND OF THE INVENTION Field of the invention The invention relates to lubricant compositions and in a more particular sense to synthetic oil compositions having improved resistance to deterioration under high performance service conditions. The improved resistance to deterioration may be attributed to the incorporation of esters of anthranilic acid as additives to the lubricant.

Description of the prior art The problem of deterioration of lubricating oils and formation of harmful deposits under high performance service conditions has been the cause of much concern in providing satisfactory lubrication of internal combustion engines. This problem is especially acute in lubricating engines of the gas turbine type, e.g. turbojet, turboprop and turbofan engines, where lubricants encounter extremely high temperatures. These severe service conditions, which favor oxidation reactions, may break a lubricant down into harmful acidic products which attack the metal parts of the engine or which may act as further oxidation catalysts. The problem is especially serious with regard to magnesium corrosion. Magnesium, which is finding ever increasing use as a constituent of light weight metal engines, is especially susceptible to attack by the acidic products of a deteriorated lubricant. In recent years it has been the practice to incorporate into lubricating oils additive compositions to inhibit oxidation and corrosion. Anthranilic acid has been mentioned in US. Pats. 3,151,075 and 3,146,201 as additives for lubricating oils. This compound, however, is totally unacceptable for use in jet type engines. Investigation has shown that anthranilic acid at high temperatures becomes extremely corrosive to engine parts.

SUMMARY OF THE INVENTION It has now been found that an anthranilic acid derivative having the general structural formula:

coon H where R is a C to C preferably a C to C normal or branched alkyl group and X is selected from the group consisting of hydrogen, a C to C normal or branched alkyl group and an unsubstituted or alkyl substituted phenyl group, is an effective oxidation and corrosion inatent hibitor in lubricating oils. This compound is especially effective in inhibiting magnesium corrosion. This additive, which will be recognized as a specific class of amines, is an ester of anthranilic acid or an ester of a derivative of that acid. The amount of the ester incorporated into the lubricating oil is a minor corrosion and oxidation inhibiting amount, usually 0.5 to 4.0 wt. percent based on the total amount of the final lubricating composition.

Examples of anthranilic acid derivatives which may be employed in the lubricating composition of this invention include esters of anthranilic acid such as methyl anthranilate, ethyl anthranilate, propyl anthranilate, 2-ethylhexyl anthranilate, etc. and esters of derivatives of anthranilic acid (i.e. X is other than hydrogen) such as methyl-N-methyl-anthranilate, 2-ethylhexyl-N-methyl anthranilate, methyl-N-phenyl anthranilate, 2-ethylhexyl-N-phenyl anthranilate, isodecyl-N-phenyl anthranilate, methyl-N-ethylphenyl anthranilate, etc.

The esters described above may generally be prepared by reacting an anthranilic anhydride with an appropriate alcohol according to the following reaction:

where X is hydrogen or an alkyl group. The ester may also be prepared via the acid chloride route which is particularly appropriate, where X is a phenyl group.

CsH5 6H5 C5115 Isatoic anhydride (the anhydride of anthranilic acid) is available from Maumee Chemical Company. N-methyl isatoic anhydride is available from Aldrich Chemical Company. N-phenylanthranilic acid is available from Eastman Kodak Company. Methods of producing the esters generally described above have been discussed in French Pat. 1,363,127 and in the Journal of Organic Chemistry, volume 24, p. 1214 (1959).

The ester additive will generally be used in lubricants which encounter high performance service conditions such as encountered in the operation of modern jet type aircraft. Generally, the basestocks of such lubricants are synthetic ester oils. It is in this type of lubricant which the ester dramatically demonstrates its effectiveness. It is contemplated, however, that the ester additive can be used in mineral oils.

The mineral or synthetic oils in which these esters are employed generally should have a viscosity within the range of about 35 to 200 SUS at 210 F. and flash points of about 350 to 600 F. Lubricating oils having a vis cosity index of or higher may be employed.

The synthetic oils include synthetic lubricating oils having a viscosity of at least 30 SUS at 100 R, such as esters of monobasic acids (e.g. ester of C Ox-o alcohol with C Oxo acid, ester of C Oxo alcohol with octanoic acid, etc.), esters of dibasic acids (e.g. di-Z-ethyl hexyl sebacate, dinonyl adipate, etc.), esters of glycols (e.g. C Oxo acid diester of tetraethylene glycol, etc.), complex esters (e.g. the complex ester formed by reacting one mole of sebacic acid with two moles of tetraethylene glycol and two moles of 2-ethyl-hexanoic acid, complex ester formed by reacting one mole of tetraethylene glycol with two moles of sebacic acid and two moles of 2-ethyl hexanol, complex ester for-med by reacting together one mole of azelaic acid, one mole of tetraethylene glycol, one mole 4 the tests, an average of several runs, are recorded in the table below.

TABLE 425 F., 48 hour O.C.S. test Amotal weight, mg./cm. AkvJ 100 F. Lubricant additive Cu Mg Steel Al Ag cs. Atau Methyl anthranilate +0. 01 0. 03 0. 01 0. 01 0. 04 15. 30 3. 26 2-Ethylhexyl anthranilate --0. 05 +0. 01 +0. 01 0. 05 -0. 04 14. 00 1. 41 Methyl-N-phenyl anthranilate 0. 02 0. 07 +0. 01 +0. 04 +0. 04 16. 59 7. 21 Z-ethylhexyl-N-phenyl anthranilate..- +0. 21 0. 91 +0.09 +0. 04 +0. 07 15. 56 9. 84 Isodecyl-N-phenyl Anthranilate. --10.43 +0. +0. 09 +0. 14 16. 43 11. Methyl-N-methyl anthranilate. 15. 31 3. 11 2ethylhexyl-N-methyl anthranila 15.33 3. 67 Di-(octylphenyDamine 22. 07 4. 90

of C Oxo alcohol, and one mole of C Oxo acid), or mixtures of any of the above in any proportions.

The preparation of the lubricating compositions involves no special techniques. Generally, the lubricants are formed by adding an appropriate amount of the ester to the basestock and heating and stirring the composition until the additive is dissolved.

Other lubricating additives can also be added to the compositions of the invention in amounts of about 0.001 to 10.0 weight percent each, based on the total weight of the composition. Examples of such additives include: rust preventives, such as calcium petroleum sulfonate or sorbitan monooleate; V.I. improvers, such as the polymethacrylates; load carrying agents, such as tricresyl phosphate and free sebacic acid; pour point depressants; dyes; grease thickeners; and the like.

DESCRIPTION OF THE PREFERRED EMBODIMENTS The following example is demonstrative of the preparation of the lubricating composition of this invention.

EXAMPLE To 100 grams of a synthetic lubricating base oil was added 1.3 grams of methyl anthranilate and 3.14 grams of a combination of conventional antioxidants, corrosion inhibitors and load carrying agents. This combination was heated and stirred at a temperature of 210 F. until a solution was efiected. The conventional additives were employed so the finished lubricant would have the qualities more nearly exhibited by a working lubricant. The synthetic lubricating base oil was composed of a mixture of a bout 25 wt. percent of an ester of neopentylglycol and fatty acids having an average chain length of C and about 75 Wt. percent of an ester of trimethylolpropane and the same fatty acid. The methyl anthranilate was prepared by reacting isatoic anhydride (a commercial product of Maumee Chemical Company) with methyl alcohol at a temperature of about 65 C. in the presence of sodium hydroxide.

An Oxidation-Corrosion-Stability Test was carried out on several lubricating compositions containing the anthranilic esters described above. Such test determines the oxidation and corrosion inhibiting elfect of the ester additive. The same test was conducted on a lubricant containing di-(octylphenyl) amine, a standard oxidation and corrosion inhibiting additive. The base oil in which the additives were incorporated was the synthetic lubricant as described in the example. Also included in the lubricant compositions which were tested was the combination of conventional additives described in the above example. The lubricant com-position contained 100 parts by weight of synthetic oil. The ester additive and the di-(octylphenyl) amine were present in amounts of 13 parts by weight. The conventional auxiliary additives were present in a total amount of 3.14 parts by weight. The results of The 425 F. Oxidation-Corrosion-Stability Test was carried out by blowing air at the rate of volumes per hour through 1 volume of the lubricating composition maintained at a temperature of 425 F. for 48 hours. At the end of the test, the increase in viscosity and the increase in total acid number (T.A.N.) were determined. The corrosive characteristic of the lubricant was determined by immersing various weighed metal strips in the oil and measuring weight change at the end of the test. The change in weight signifies either corrosion due to oxidation of the metal or weight gain due to deposits. The test is a close simulation of the conditions under which high performance jet type engines operate and is an appropriate test of the serviceability of a lubricant.

As seen from the test above, the oxidative stability of a lubricant containing the anthranilate esters was generally greatly superior to the lubricant containing the standard antioxidant. This is indicated by a smaller change in total acid number, which was observed in most cases when the ester was used, and in a smaller change in viscosity, which was observed in all cases where the anthranilate ester was used. The corrosivity of a lubricant containing the anthranilate ester to the various metals described in the above table was minimal in all cases and the ester was distinctly superior to di-(octylphenyl) amine in inhibiting the corrosion of magnesium. This was most dramatically illustrated in the cases of 2-ethylhexyl anthranilate and 2-ethylhexyl-N-methyl anthranilate, which were 1300 times more effective in inhibiting corrosion than the di-(octylphenyl) amine.

What is claimed is:

1. A lubricating composition suitable for high performance service at high temperature in internal combustion engines consisting essentially of:

(a) a major amount of a synthetic ester lubricating oil;

and

(b) a minor corrosion and oxidation inhibiting amount of 05-40% by weight of a compound having the formula 0 II 3 OR wherein R is C to C alkyl group, and X is selected from the group consisting of hydrogen, C to C alkyl groups and phenyl groups.

2. A lubricating composition as in claim 1 wherein X is hydrogen.

3. A lubricating composition as claimed in claim 1 wherein the compound is selected from the group consisting of methyl anthranilate, Z-ethylhexyl anthranilate, methyl-N-phenyl anthranilate, methyl-N-methyl anthranilate, Z-ethylhexyl-N-methyl anthranilate.

4. A method of lubricating which comprises coating rubbing magnesium surfaces with a lubricating composition comprising a major amount of a synthetic ester 1 lubricating oil containing a minor corrosion and oxidation inhibiting amount of 0.5-5.0% by weight of a compound 5 having the formula:

where R is a C to C alkyl group, and X is selected from the group consisting of hydrogen, C to C alkyl groups and phenyl groups.

References Cited UNITED STATES PATENTS Clarke 208-329 X Trautman 252-5l.5 A Kavanagh et al. 25251.5 A Provine et a1 252-403 X Eickemeyer et a1. 252-51.5 Cupper et al. 252-565 Furey 252-56'5 Stern 252-49.5 X Foster et a1 252-50 Cyba 252-32.7

US. Cl. X.R.

UNITED S'LUVHCS PAIIEINT OFIFICE GER FEE/Q}- in (N3 COiilUuC i. i QN iatent N0. 3.5 3 3 v Dated February 5, 9 N

Q Inven John F. Coburn' et a1 It is certified Umt error appears in the abo\ e--1'.dcutified patent and that: said Letters Patent are hereby corrected as shown below:

In column 1, line '6, after "07076" insert assignors' to Esso Research and Engineering Company,

a. corporation of Delawarew-i In column 1, line 13, after "derivative" insert v In column L, line 66, before "C insert -a--.

Signed and sealed this 28th day of November 1972.

(SEAL) Attest:

EDWARD M.FLETCHER,JR. ROBERT GOTTSCHALK Attesting Qiificer- Commissioner of Patents