Patent Application
20060019843
The present invention relates to grease compositions. More particularly the invention relates to grease compositions employing olefin oligomers as the base oil in the grease.
Lubricating greases contain three primary components: base oil, thickener and additives. The base oil provides lubricity, the thickener gives body and structure to the grease, and the additives increase resistance of the grease to oxidation, rust, corrosion and the like.
Conventionally base oils used in greases include mineral and synthetic oils and mixtures of each. Examples of mineral oils used are paraffinic and naphthenic oils. Examples of synthetic oils used are: esters including but not limited to polyol and dibasic acid esters, poly-glycols, synthetic hydrocarbons such as PAO (poly alpha olefins) and silicone oils.
A wide variety of materials are used as thickeners in lubricating greases, the selection of which often depends upon the application for the grease. Among the thickeners used in lubricating greases are intended soaps and complex soaps of these metals: aluminum, barium, calcium, iron, lead, lithium, magnesium, potassium, sodium, strontium, tin, titanium, zinc, or the following non-soap thickeners: calcium sulfonate, clay, pigments, polyurea, and polytetrafluoroethylene.
Additives that are used in greases include antioxidants, anticorrodants, metal deactivators, colorants and the like.
Greases are formulated with the view of meeting performance criteria based upon the intended use. For example, lubricating greases used in aviation applications are often required to have specific performance properties at both low and high temperatures. Among these properties are low temperature torque and high temperature evaporation. Low temperature torque is a measurement used to determine whether a grease is too firm such as to inhibit bearings from rotating freely at low temperatures. Good low temperature performance can be achieved by using an oil in the grease that is low in viscosity. The low temperature properties of a grease are typically measured using the ASTM method D 1478, Low Temperature Torque Of Ball Bearing Greases, which measures the freedom with which a ball bearing packed with grease operates when cooled to a specified temperature. The freedom of bearing rotation is reported by the D 1478 method, as the torque required to start and maintain rotation of the bearing. Torque is typically reported in units of Newton-meters.
One of the high temperature properties of a lubricating grease important to aviation applications is low evaporation. If the oil evaporates it is not available to lubricate and the performance of the grease lubricated component will be jeopardized. This is the case when aircraft lubricants are exposed to high temperatures as well as reduced atmospheric pressure when operating during flight. Both conditions can promote the evaporation of the oil used in the grease. An approach for avoiding excessive evaporation is to use greases with high base oil viscosity. Tests typically used to measure the evaporation loss of lubricating grease are the ASTM test methods D 972, and D 2595, Evaporation Loss Of Lubricating Greases. In each of these tests heated air passes over the surface of the grease for a specified time with the air heated to a specified temperature as called for by the aviation grease specification.
One particular specification, Boeing Material Specification, BMS 3-33A, Grease, Aircraft, General Purpose, calls for a grease in which the low temperature starting torque in the ASTM D 1478 test shall not exceed 0.10 Newton-meter and in which the evaporation weight loss of the grease, when evaluated in the ASTM D 2595 test for 500 hours at 121° C. shall not exceed 10.0 wt %.
When the type of oil selected for a grease to meet the Boeing Material Specification, BMS 3-33A is 100% poly alpha olefin (PAO), experience has shown that difficulty is encountered because the low viscosity PAO needed to meet the low temperature torque requirements results in excessive high temperature evaporation. One approach to overcome this difficulty is to use PAO blends with synthetic esters as the grease base oil; however, esters may hydrolyze in hot and wet environments and produce species that may be corrosive to various metals. Therefore it would be desirable to provide a grease having a PAO base oil that is free of polyesters and that can meet the Boeing specification.
Broadly stated, the present invention relates to a grease composition comprising a major portion of an oil of lubricating viscosity and a minor portion of a grease thickener sufficient to thicken the oil to grease consistency wherein the oil of lubricating viscosity consists essentially of a mixture of dimer, trimer and higher oligomers of poly alpha olefins, poly internal olefins and mixtures thereof in which the oligomer mixture contains less than 10 wt % of dimer.
The base oil used in the present invention is a mixture of dimers, trimers and higher oligomers of poly alpha olefins, poly internal olefin and mixtures thereof. Preferably the base oil is a mixture of PAO oils derived from linear alpha olefins that have been polymerized and additionally hydrogenated to remove unsaturated double bonds and that have been fractionated to obtain a particular product slate. PAO's have numbers assigned to them to indicate the approximate viscosity in centistokes at 100° C. In Table 1 there is shown the segment distribution for a number of PAO oils derived from 1-decene. Segments containing 20 carbons are dimers, 30 carbons are trimers and 40 carbons are tetramers, for example. In the present invention the PAO oligomers preferably are derived from alpha olefins having from about 5 to about 14 carbon atoms. Indeed 1-decene is especially preferred alpha olefin used in forming the oligomers. Additionally it is preferred that the base oil have a viscosity not greater than 25 cSt at 40° C. For example, a mixture of base PAO oils having a viscosity in the range of about 13 cSt to about 20 cSt at 40° C. would be suitable for use in the present invention.
In order to meet the low temperature torque and high temperature evaporation requirements of Boeing specification BMS 3-33A the base poly-olefin oligomer oil used in formulating the grease will contain less than 10 wt % dimer, for example, from 5 wt % to 10 wt %. Typically the oil also will contain greater than about 75 wt % trimer, for example, from 75 wt % to about 95 wt %.
The base oil will comprise a major amount of the grease composition, for example, from about 65 wt % to about 80 wt % based on the total weight of the grease.
The grease also comprises a minor amount of a thickener sufficient to thicken the oil to grease consistency. Typically the thickener will comprise about 5 wt % to about 20 wt % of the grease.
Suitable thickeners include soap thickeners and non-soap thickeners. Examples of soap thickeners include soaps of lithium, sodium, calcium, barium, aluminum, zinc and the like. Examples of non-soap thickeners include calcium sulfonate, clay, silica gel, urea compounds and the like.
The composition of the invention may also include minor but effective amounts of other grease additives including antioxidants, anticorrodants, metal deactivators, rust inhibitors, extreme pressure agents, colorants, and the like.
The compositions are prepared in conventional grease blending equipment by manufacturing the thickener at temperatures up to about 150° C. to 200° C. and thoroughly mixing in the additives at temperatures generally from 35° C. to about 100° C.
The invention will be further illustrated by the following examples.
Three PAO blends were made from various combinations of the PAO oils listed in Table 1. The composition of the three blends is given in Table 2.
Each of the three PAO oil blends were then formed into a grease using approximately 9 wt % (based on 12-hydroxy stearic acid) of lithium complex thickener and approximately 17% additives consisting of typical corrosion inhibitors, antiwear agents, extended pressure agents and antioxidants. The resulting greases were then subjected to ASTM tests D1478 and D2595. The results of the test also are shown in Table 2.
(1) BMS 3-33 A Requires: 0.75 starting maximum and 0.10 running maximum
(2) BMS 3-33 A Requires 10% maximum
As can be seen oil blend 1 meets the low temperature torque requirements of BMS 3-33A but not the evaporation requirement. The data also shows that as the dimer amount is reduced the high temperature evaporation property is improved.
This application claims the benefit of U.S. Ser. No. 60/519,926 filed Nov. 14, 2003.
| Number | Date | Country | |
|---|---|---|---|
| 60519926 | Nov 2003 | US |
