Composite bearing structure of alternating hard and soft metal, and process for making the same

Claim 2

A composite metal member suitable for providing a bearing of improved wear characteristics, the member comprising: a substrate of a base metal composition, having a bearing precursor surface; a plurality of spaced areas of a hard metal composition, the spaced areas of the hard metal composition having been metallurgically bonded to the bearing precursor surface in a substantially molten state of the hard metal composition, the spaced areas protruding from the bearing precursor surface, each area of hard metal composition being substantially entirely isolated from all other areas of hard metal composition thereby forming gaps between said protruding areas, and a soft metal composition disposed on the bearing precursor surface to substantially fill the gaps between the protruding areas of the hard metal composition, the combined spaced areas of the hard metal composition and the soft metal composition adapted for being machined into a bearing surface.

Claim 3

The composite metal member of claim 1 wherein the areas of hard metal composition are substantially regularly spaced.

Claim 4

The composite metal member of claim 2 wherein the areas of hard metal composition comprise substantially continuous strips.

Claim 5

The composite metal member of claim 2 wherein the areas of hard metal composition comprise islands.

Claim 6

The composite metal member of claim 1 wherein the base metal composition is selected from a group consisting of ferrous metals, ferrous metal based alloys, nickel, nickel based alloys, cobalt, cobalt based alloys, copper and copper based alloys.

Claim 7

The composite metal member of claim 1 wherein the hard metal composition is a hardfacing alloy selected from a group consisting of metal carbide based hardfacing alloys and intermetallic alloys.

Claim 8

The composite metal member of claim 1 wherein the soft metal composition has an Rc hardness at least approximately 5 units less than the Rc hardness of the hard metal composition.

Claim 9

The composite metal member of claim 1 wherein the soft metal composition is selected from a group consisting of copper, copper based alloys, silver, silver based alloys, tin, tin based alloys, lead, and lead based alloys.

Claim 10

A composite metal bearing comprising: a substrate member of a base metal composition including a support surface underlying a bearing surface; a plurality of spaced areas of a hardfacing metal different in composition than the base metal composition, said spaced areas of the hardfacing metal having been metallurgically bonded to the support surface of the substrate in a substantially molten state of the hardfacing metal, protruding from the support surface, and being isolated from one another so as to form gaps between adjacent areas, and a soft metal composition having a hardness of at least five Rc units less than the hardness of the hardfacing metal, the soft metal being disposed on the support surface in the gaps among the spaced areas of hardfacing metal and substantially entirely filling said gaps, the areas of the hardfacing metal and the soft metal jointly comprising the bearing surface.

Claim 11

A composite metal bearing comprising: a substrate member of a base metal composition including a support surface underlying a bearing surface; a plurality of spaced areas of a hardfacing metal different in composition than the base metal composition, said spaced areas of the hardfacing metal having been metallurgically bonded to the support surface of the substrate in a substantially molten state of the hardfacing metal, protruding from the support surface, and being isolated from one another so as to form gaps between adjacent areas, and a soft metal composition having a hardness of at least five Rc units less than the hardness of the hardfacing metal, the soft metal being disposed on the support surface in the gaps among the spaced areas of hardfacing metal and substantially entirely filling said gaps, the areas of the hardfacing metal and the soft metal jointly comprising the bearing surface.

Claim 12

The composite metal bearing of claim 9 wherein the gaps between areas of the hardfacing metal are approximately of 1/32" to 1/8" magnitude.

Claim 13

The composite metal bearing of claim 9 wherein the areas of hardfacing metal comprise substantially elongated strips being approximately 1/8"-1/4" wide.

Claim 14

The composite metal bearing of claim 9 wherein the base metal composition is selected from a group consisting of ferrous metals, ferrous metal based alloys, nickel, nickel based alloys, cobalt, cobalt based alloys, copper and copper based alloys, the hardfacing metal is selected from a group consisting of carbide based hardfacing alloys and intermetallic hardfacing alloys, and the soft metal is selected from a group consisting of copper, copper based alloys, silver, silver based alloys, tin, tin based alloys, nickel, nickel based alloys, lead and lead based alloys.

Claim 15

A composite metal bearing have a bearing surface of alternating areas of a hardfacing metal composition and a soft metal composition, prepared by the process comprising the steps of: depositing a powdered hardfacing metal composition on a suitable bearing precursor surface of a metal substrate of a base metal composition; scanning with a high intensity energy source the powdered hardfacing composition in a predetermined pattern to cause rapid localized melting of the hardfacing composition in the predetermined pattern and to form in the predetermined pattern a metallurgical bond between the hardfacing composition and the substrate, the predetermined pattern being configured to provide spaced areas impacted by the energy source; permitting rapid cooling of the molten hardfacing composition whereby isolated spaced areas of solid hardfacing composition are formed which protrude from the precursor surface in the predetermined pattern; substantially filling all gaps between the protruding areas of the hardfacing composition with a melt of a soft metal composition; permitting the melt of the soft metal to solidify, and removing a layer of the hardfacing composition and of the soft metal composition to provide the bearing surface of the alternating areas of hardfacing metal and soft metal.

Claim 16

A composite metal bearing have a bearing surface of alternating areas of a hardfacing metal composition and a soft metal composition, prepared by the process comprising the steps of: depositing a powdered hardfacing metal composition on a suitable bearing precursor surface of a metal substrate of a base metal composition; scanning with a high intensity energy source the powdered hardfacing composition in a predetermined pattern to cause rapid localized melting of the hardfacing composition in the predetermined pattern and to form in the predetermined pattern a metallurgical bond between the hardfacing composition and the substrate, the predetermined pattern being configured to provide spaced areas impacted by the energy source; permitting rapid cooling of the molten hardfacing composition whereby isolated spaced areas of solid hardfacing composition are formed which protrude from the precursor surface in the predetermined pattern; substantially filling all gaps between the protruding areas of the hardfacing composition with a melt of a soft metal composition; permitting the melt of the soft metal to solidify, and removing a layer of the hardfacing composition and of the soft metal composition to provide the bearing surface of the alternating areas of hardfacing metal and soft metal.

Claim 17

The composite metal bearing of claim 13 prepared by the process wherein the powdered hardfacing composition is deposited on the precursor surface in a substantially uniform layer, and wherein after the step of rapid cooling of the molten hardfacing composition the process further comprises the step of removing remaining powdered hardfacing composition from the bearing precursor surface.

Claim 18

The composite metal bearing of claim 14 wherein the powdered hardfacing composition is intermixed with a suitable binder for the step of depositing on the precursor surface.

Claim 19

The composite metal bearing of claim 15 wherein the binder is a volatile solvent.

Claim 20

The composite metal bearing of claim 15 wherein the binder is cellulose acetate.

Claim 21

The composite metal bearing of claim 13 prepared by the process wherein the step of depositing the powdered hardfacing composition and the step of scanning with a high intensity energy source are conducted substantially simultaneously.

Claim 22

The composite metal bearing of claim 13 wherein bearing surface is substantially parallel with the underlying bearing precursor surface of the metal substrate.

Claim 23

The composite metal bearing of claim 13 wherein the high intensity energy source used in the step of scanning is a laser beam.

Claim 24

The composite metal bearing of claim 13 wherein the base metal composition is selected from a group consisting of ferrous metals, ferrous metal based alloys, nickel, nickel based alloys, cobalt, cobalt based alloys, copper and copper based alloys, the hardfacing metal is selected from a group consisting of carbide based hardfacing alloys and intermetallic hardfacing alloys, and the soft metal is selected from a group consisting of nickel, nickel based alloys, copper, copper based alloys, silver, silver based alloys, tin, tin based alloys, lead and lead based alloys.

Claim 25

A process for preparing a composite metal bearing, comprising the steps of: depositing a hardfacing metal composition on a suitable bearing precursor surface of a substrate member of a base metal composition; scanning with a high intensity energy source the hardfacing composition in a predetermined pattern to cause rapid localized melting of the hardfacing composition in the predetermined pattern and to form in the predetermined pattern a metallurgical bond between the hardfacing composition and the substrate, the predetermined pattern being configured to provide spaced areas impacted by the energy source; permitting rapid cooling of the molten hardfacing composition whereby isolated, spaced areas of solid hardfacing composition are formed which protrude from the precursor surface in the predetermined pattern; substantially filling all gaps between the protruding areas of the hardfacing composition with a melt of a soft metal composition; permitting the melt of the soft metal to solidify, and removing a layer of the hardfacing composition and of the soft metal composition to provide a bearing surface of alternating areas of hardfacing metal and soft metal.

Claim 26

A process for preparing a composite metal bearing, comprising the steps of: depositing a hardfacing metal composition on a suitable bearing precursor surface of a substrate member of a base metal composition; scanning with a high intensity energy source the hardfacing composition in a predetermined pattern to cause rapid localized melting of the hardfacing composition in the predetermined pattern and to form in the predetermined pattern a metallurgical bond between the hardfacing composition and the substrate, the predetermined pattern being configured to provide spaced areas impacted by the energy source; permitting rapid cooling of the molten hardfacing composition whereby isolated, spaced areas of solid hardfacing composition are formed which protrude from the precursor surface in the predetermined pattern; substantially filling all gaps between the protruding areas of the hardfacing composition with a melt of a soft metal composition; permitting the melt of the soft metal to solidify, and removing a layer of the hardfacing composition and of the soft metal composition to provide a bearing surface of alternating areas of hardfacing metal and soft metal.

Claim 27

The process of claim 22 wherein the high intensity energy source used in the step of scanning, is a laser beam.

Claim 28

The process of claim 22 wherein the step of depositing the hardfacing metal composition and the step of scanning are conducted substantially simultaneously.

Claim 29

The process of claim 22 where in the step of depositing, the hardfacing metal composition is mixed with a suitable binder, and the step of scanning is conducted after the step of depositing.

Claim 30

The process of claim 22 where in the step of depositing, the hardfacing metal composition is deposited on the bearing precursor surface as a substantially uniform layer covering said precursor surface; the step of scanning is conducted after the step of depositing, and wherein after the step of rapid cooling the process further comprises a step of removing loose hardfacing composition remaining on the bearing precursor surface.

Claim 31

The process of claim 22 wherein the step of scanning is conducted in a predetermined pattern configured for providing substantially parallel disposed, substantially regularly spaced strips on the precursor surface in which the hardfacing metal composition is to be impacted by the high intensity energy source and to be melted thereby.

Claim 32

The process of claim 22 wherein the step of scanning is conducted in a predetermined pattern configured for providing isolated, substantially regularly spaced islands on the precursor surface in which the hardfacing composition is to be impacted by the high intensity energy source and is to be melted thereby.

Claim 33

The process of claim 22 wherein the step of removing is conducted to provide a bearing surface disposed substantially parallel with the underlying precursor surface.

Claim 34

The process of claim 22 wherein the base metal composition is selected from a group consisting of ferrous metals, ferrous metal based alloys, nickel, nickel based alloys, cobalt, cobalt based alloys, copper, and copper based alloys, the hardfacing metal composition is selected from a group consisting of carbide based hardfacing alloys, and intermetallic hardfacing alloys, and the soft metal is selected from a group consisting of nickel, nickel based alloys, copper, copper based alloys, silver, silver based alloys, tin, tin based alloys, lead, and lead based alloys.