US3317341A - Metallic film diffusion for boundary lubrication - Google Patents

Description

United States Patent 3,317,341 METALLIC FILM DIFFUSION FOR BOUNDARY LUBRICATION Donald H. Buckley, North Olmsted, and Robert L. Johnson, Fairview Park, Ohio, assignors to the United States of America as represented by the Administratgrfiof the National Aeronautics and Space Adminisa on No Drawing. Filed Oct. 15, 1963, Ser. No. 316,477

. 1 Claim. (Cl. 117---65.2)

The invention described herein may be manufactured and used by or for the Government of the United States of America for governmental purposes without the payments of any royalties thereon or therefor.

The invention relates generally to metallic film lubricants and, more particularly, to diffusing a metallic film into a metal or other material for use as a lubricant.

In aerospace applications where high reliability is desirable, it becomes necessary for moving parts to operate over substantial temperature ranges in the vacuum of outer space. Difficulty is experienced with available oil and grease lubricants because of their high evaporation rates. Some inorganic solid and soft materials having very low evaporation rates in vacuum appear to have promise as solid film lubricants for space. Where such lubricants are used as a liquid or in dispersed powder form, problems of Zero gravity prohibit adequate lubrication as the lubricant will not maintain itself within the environment of the surfaces to be lubricated. Consequently, a lubrication system is used whereby a solid film lubricant is formed on a surface to be lubricated which would act as a boundary lubricant. However, where metallic film lubricants are required, difiiculty is experienced in applying them to material surfaces used in aerospace environments. The main ditficulty is that these metallic films will not maintain themselves on the surface to be lubricated after application. Further, the conditions of outer space dictate high operating temperatures due to solar radiation and heat generation experienced from rocket engine combustion. Therefore, it is also necessary to have lubricant films which will be resistant to temperatures to 1,000 F.

Accordingly, an object of the invention is to provide for a method to apply to metal, ceramic and cermet surfaces metallic films which can be used as boundary lubricants in an aerospace environment.

Another object of this invention is the production of articles with surfaces of a metallic film diffused therein as distinguished from a mere coating of a metallic film.

Still another object of the invention is to provide metallic film lubricants having low friction properties which can withstand temperatures to 1,000 P. and have a low evaporation rate. v

Briefly, these and other objects of the invention are attained by preparing the'surface to be lubricated, rubbing thereon liquified metals such as gallium and gallium in combination with tin, indium and lead, heating the surface with the metal thereon, allowing the surface to cool and Wiping the excess metal therefrom. Subsequently, a postheat treatment is given wherein the surface with the metallic film thereon is reheated and allowed to cool to room temperature thereby improving the frictionand wear properties of the surface with the metallic fihn.

Other objects and advantages of the present invention will be described and will be apparent from the following description and the several embodiments thereof.

The method of the present invention consists of cleaning the surface upon Which the lubricant film is to be applied. The surface is prepared by rinsing it with acetone or another solvent to remove grease and oil. Subsequently, the surface is polished with moist levigated alumina or other similar grinding compounds with a soft cloth. This polishing continues until the surface is perfectly clean.

After polishing the surface and thereby improving to a degree the surface finish, the surface is thoroughly rinsed with tap water followed by distilled water. The rinsing process can also be accomplished with alcohol or another similar type of fluid.

After cleaning the surface to which the lubricating film is to be applied, the metal which is to comprise the lubricant film is applied to the surface at a temperature above which it is in a liquid state. The liquified metal is applied to the surface by means of an applicator which, depending upon the surface and/or the temperature of the metal, can be a polishing cloth. The metal is rubbed over and diffused into the surface by applying a sufficient amount of pressure to the applicator. Where the temperature of the metal is beyond that which can be handled by a human hand, the applicator can be of a soft heat resistant material not reactive with the liquified metal nor abrasive to the surface upon which the liquid metal film is to be applied.

After the liquid metal is uniformly distributed over the surface, the sample is heated to a temperature of approximately F. above its initial liquid phase temperature to allow the liquified metal to completely coat the surface and diffuse into the material surface. The sample is then allow to cool to its lower liquid phase temperature and wiped dry with a nonabrasive cloth to remove any excess metal. It has been found that this method will form a solid metallic film boundary lubricant on a surface approximately 0.001 inch thick.

It has been further found that for most films, a postheat treatment is preferable. The post-heat treatment consists of placing the surface with the metallic film thereon into an enclosed chamber for heating to a temperature of approximately 400 F. above its initial liquidphase temperature for a period of approximately one hour. In a method for accomplishing the aforesaid, a vacuum furnace can be used to eliminate oxidation problems. The surface with the lubricant film thereon is then removed from the furnace and is allowed to cool to room temperature. The post-heat treatment temperature and the length of time in the furnace can be varied; accordingly, this variance would affect the friction and wear properties of the surfaces associated with the film.

By use of the aforesaid method of the present invention, it is possible to impregnate materials with a metal which heretofore could not be done wherein the impregnated metals would form a film on the surfaces and act as a boundary lubricant.

For space applications, it is preferable that materials selected for a boundary lubricant for use with the method of the present invention have a low shear rate to give low friction coefficients, have as low a melting or liquid phase temperature as possible, and have a low evaporation rate. Further, the film should have as low an oxidation rate as possible. A metal which can be used with themethod of the present invention is gallium. Tin, lead and indium can be added to the gallium in various amounts to provide for metallic film lubricants having reduced corrosion properties and, in some instances, a lower liquid phase temperature.

The following examples describe in greater detail the metallic'film lubricants and the procedure for applying to a surface the aforesaid metals for use as a metallic film for boundary lubrication:

As a first example, gallium is used as the metallic film lubricant. Gallium is in liquid form over a temperature range of more than 3500 F. At atmospheric pressures, the liquid range is from approximately 86 F. to 3600 F. Gallium also has a low evaporation rate, that being 1 l0 grams/cmF/sec. While the gallium in actual application is applied to the surfaces of face seals which are made out of metals and ceramics, such as tool steels and alumina, or to bearing cages made out of graphite, lead and titanium, for the purposes of this example the gallium as well as the other metals were applied to a fiat disc surface made out of 440 C. stainless steel which can be used in conjunction with a rider of friction and wear measurements.

As previously described in the method of the present invention, the disc specimen is prepared by rinsing with acetone to remove greases, oils and other contaminants contained thereon. Subsequently, the disc is polished with levitated alumina on a soft cloth and thoroughly rinsed with tap water followed by distilled water. Subsequently, liquid gallium is applied under pressure to the surface by means of a soft polishing cloth applicator in order to uniformly distribute the gallium over and into the surface of the disc. The aforesaid was accomplished at the lower liquid phase temperature of the gallium which is approximately 86 F. The disc with the gallium contained thereon and diffused therein is heated to a temperature of approximately 200 F. to allow the gallium to more completely coat and diifuse into the surface of the disc. The sample is subsequently wiped with a dry cloth to remove excess gallium immediately after heating. Subsequently, the sample is allowed to cool forming a film of approximately 0.001 inch thick on a the surface of the disc.

The disc with the gallium film is given'an' additional treatment consisting of placing the disc specimen with:

the metallic film into a vacuum furnace and heating the disc to 500 F. for a period of approximately one hour. The disc is then removed from the furnace and allowed to cool to room temperature.

It has been found that for gallium where the time of the post-heat treatment was substantially less than one hour and at temperatures substantially lower than 500 F., the friction and wear for the disc-film combination was higher. Whereas, when the post-heat treatment temperature was 1,000 F., the friction and wear properties were the same as for 500 F. Consequently, in the present embodiment of the invention, optimal friction and Wear results were obtained with a post-heat temperature between 450 F. and 550 F. for an approximate period of one hour.

The following table is an example of friction and wear properties of the gallium as a metallic surface film using the method of the present invention using two material combinations under atmospheric conditions and in a vacuum.

Gallium Tin (Percent Weight) (Percent Weight) The tin-gallium eutectic alloys give approximately the same friction and wear properties as the pure gallium film in Table 1.

As a third example, approximately 24.5 percent by weight indium is added to the gallium which produces an initial liquid phase temperature of approximately 60 F. giving the additional advantage of applying this eutectic alloy at a lower temperature than that of pure gallium. The indium-gallium eutectic alloy is applied as in Example Z-for the tin-gallium eutectic alloy.

' The following additional eutectic alloys of indiumgallium are found to provide adequate boundary lubrication to temperatures beyond 1,000 F. and have an initial liquid phase temperature below that of pure gallium.

Gallium Indium (Percent Weight) (Percent Weight) In use of any type of metallic film applied to a surface as herein described, it is preferable that for the purposes of the method of the present invention that the metal used for the film have as low an initial liquid phase temperature as possible. For gallium at normal atmospheric conditions, the following can be achieved by the addition of tin or indium to the gallium.

As a second example of the present invention, approximately 8 percent tin is added to gallium which lowers the initial liquid phase temperature of the pure gallium 7 weight contained therein,

steel. Tin, indium and lead added to the gallium in varivarious materials.

As a fourth example, lead is added to the gallium in various amounts from 5 percent to 50 percent. The addition of lead to gallium will not reduce its liquid phase temperature. The corrosivity of the alloy can, however, be reduced. Friction and wear tests for the gallium-lead alloy with amounts of lead by percent up to 50 percent, indicated that the friction and wear properties of this alloy did not vary significantly from that of pure gallium alone.

In an embodiment using the method of the present invention, a metallic lubricant film can be formed on the contacting surfaces of rotating machinery such as gears, elements of rolling-contact bearings and rotating face seals. A further embodiment using the method of the present invention can be the formation of an intermediate metallic film between two heat transfer surfaces in contact whereby the contact of the surfaces is not on the asperities of the surfaces but rather, the contact is over the entire area as defined by the metallic film.

The present invention and specific embodiments thereto provide not only for metallic film boundary lubricants to and beyond 1,000 F., but also lubricants having low friction coefficients and low evaporation rates in aerospace applications.

It is apparent from the above description that various modifications in the specific materials and procedures described may be made within the scope of the invention. Therefore, the invention is not intended to be limited to the particular materials and procedures described in detail herein except as may be required by the appended claim.

We claim:

A method of forming a metallic film of gallium and alloys thereof having low friction and wear properties on alumina and stainless steel surface which comprises removing foreign material from the surface upon which said metallic film is to be applied, polishing said surface a to improve said surface finish, applying a gallium coating References Cited by the Examiner UNITED STATES PATENTS 2,567,762 9/1951 Burkholcler 117131 X 2,700,623 1/1955 Hall 117-71 3,141,238 7/1964 Harman 29498 3,184,330 5/1965 Carter 117-131 X ALFRED L. LEAVITT, Primary Examiner.

J. R. BATTEN, JR., Assistant Examiner. 5