Process for treating a bearing surface to modify microasperities

Claim 2

A process for treating a bearing surface for elastohydrodynamic lubrication, the bearing surface having microasperities for retaining lubricant, which comprises: generating a high density energy beam; and producing relative motion between the beam and the bearing surface to define a succession of points at each of which the beam impinges upon the bearing surface for an interaction time during which localized heating occurs and then rapid cooling begins to cause partial melting followed by rapid solidification that, in the direction normal to the bearing surface extends to a depth less than the microasperity height and that, owing to said relative mmotion, extends throughout an area of the bearing surface to define a microdimpled surface having rounded microasperities with residual compressive stress for retaining lubricant and enhancing resistance to wear and fatigue.

Claim 3

A process according to claim 1, wherein the high density energy beam is a laser beam.

Claim 4

A process according to claim 2, wherein the laser beam is produced by a laser having a power level of at least 500 watts.

Claim 5

A process according to claim 1, wherein the laser beam has a power density of at least 100 watts/cm 2 at the point of impingement on the bearing surface.

Claim 6

A process according to claim 1, wherein the bearing surface is defined by a layer of hard metal deposit covering a steel substrate.

Claim 7

A process for treating a bearing surface defined by a layer of hard metal deposit comprising an alloy containing chromium, tungsten, iron, nickel, and carbon having microasperities, which comprises: generating a high density energy beam; and producing relative motion between the beam and the bearing surface to define a succession of points at each of which the beam impinges upon the bearing surface for an interaction time during which localized heating occurs and then rapid cooling begins to cause partial melting followed by rapid solidification that, in the direction normal to the bearing surface extends to a depth less than the microasperity height and that, owing to said relative motion, extends throughout an area of the bearing surface to define a microdimpled surface.

Claim 8

A process for treating a bearing surface defined by a layer of hard metal deposit comprising an alloy containing chromium, tungsten, iron, nickel, and carbon having microasperities, which comprises: generating a high density energy beam; and producing relative motion between the beam and the bearing surface to define a succession of points at each of which the beam impinges upon the bearing surface for an interaction time during which localized heating occurs and then rapid cooling begins to cause partial melting followed by rapid solidification that, in the direction normal to the bearing surface extends to a depth less than the microasperity height and that, owing to said relative motion, extends throughout an area of the bearing surface to define a microdimpled surface.

Claim 9

A process according to claim 6, wherein the beam is produced by a laser beam that during said interaction time has an incident energy of between about 90 joules/cm 2 to about 3750 joules/cm 2 .

Claim 10

A process for treating a hard facing alloy bearing surface having microasperities having an average height of less than about 100 micrometers and which are generally regularly oriented in a pattern of machining lines, the process comprising: generating a laser beam by a laser having an output power in excess of at least about 100 watts; passing the generated beam through an optical system to produce an effective beam diameter in the range of about 200 microinches to about 2029 microinches; and producing relative motion between the beam and the bearing surfaces to define a succession of points at each of which the beam having said effective beam diameter impinges upon the bearing surface for an interaction time in the range of about 0.4 milliseconds to about 1.5 seconds, during which interaction time localized heating occurs and then rapid cooling begins to cause partial melting followed by rapid solidification that, in the direction normal to the bearing surface extends to a depth less than the microasperity height and that, owing to said relative motion, extends throughout an area of the bearing surface to define a microdimpled surface.

Claim 11

A process for treating a hard facing alloy bearing surface having microasperities having an average height of less than about 100 micrometers and which are generally regularly oriented in a pattern of machining lines, the process comprising: generating a laser beam by a laser having an output power in excess of at least about 100 watts; passing the generated beam through an optical system to produce an effective beam diameter in the range of about 200 microinches to about 2029 microinches; and producing relative motion between the beam and the bearing surfaces to define a succession of points at each of which the beam having said effective beam diameter impinges upon the bearing surface for an interaction time in the range of about 0.4 milliseconds to about 1.5 seconds, during which interaction time localized heating occurs and then rapid cooling begins to cause partial melting followed by rapid solidification that, in the direction normal to the bearing surface extends to a depth less than the microasperity height and that, owing to said relative motion, extends throughout an area of the bearing surface to define a microdimpled surface.

Claim 12

A process according to claim 8, wherein the hard facing alloy covers a steel substrate.

Claim 13

A process according to claim 9, wherein the hard facing alloy includes chromium, tungsten, iron, nickel, and carbon.

Claim 14

A process according to claim 10, wherein the composition of the hard facing alloy by approximate weight is 30% chromium, 12.5% tungsten, 3% iron, 3% nickel, 2.5% carbon, and smaller percentages of manganese, silicon, and molybdenum.

Claim 15

A process according to claim 9, wherein the hard facing alloy absorbs about 20% of the energy impinging on it so that the absorbed energy per unit area is in the range of about 90 joules/cm 2 to about 3750 joules/cm 2 .

Claim 16

A process according to claim 8, wherein the localized heating raises the temperature of peak portions of the microasperities sufficiently to vaporize some of the material forming the peak portions.