Bearing of an internal combustion engine and process for producing the same

Claim 2

A process for producing a bearing to be used in an internal combustion engine, said bearing comprising a base, a bearing material layer, and an at least quaternary alloy-overlay consisting of (i) from about 5% to about 20% of tin, (ii) from about 0.05% to about 10% of at least one element selected from the group consisting of indium and thallium, (iii) from about 0.05% to about 5% of at least one wear resistance-enhancing element selected from the group consisting of antimony, manganese, bismuth, nickel, copper, calcium, and barium, and (iv) lead and impurities in balance, all percentages being by weight, said process for forming said at least quaternary alloy-overlay comprising the steps of: separately forming on said bearing material layer in any order, at least one first layer and at least one second layer structure, contiguous with each other, said at least one first layer comprising at least one element selected from the group consisting of indium and thallium; and said at least one second layer structure comprising at least one second layer consisting of one element, a binary alloy or a ternary alloy, said second layer structure comprising lead, about 5 to about 20% tin and from about 0.05 to about 5% of at least one wear resistance-enhancing element selected from the group consisting of antimony, manganese, bismuth, nickel, copper, calcium, and barium; and heating said first layer and said second layer structure to such a temperature that interdiffusion between said layer and layer structure takes place, thereby forming a single overlay layer comprising said at least quaternary alloy-overlay.

Claim 3

A process for producing a bearing to be used in an internal combustion engine, said bearing comprising a base, and an at least quaternary alloy-overlay consisting of (i) from about 5% to about 20% of tin, (ii) from about 0.05% to about 10% of at least one element selected from the group consisting of indium and thallium, (iii) from about 0.05% to about 5% of at least one wear resistance-enhancing element selected from the group consisting of antimony, manganese, bismuth, nickel, copper, calcium, and barium, and (iv) lead and impurities in balance, all percentages being by weight, said process for forming said at least quaternary alloy-overlay comprising the steps of: separately forming on said base in any order, at least one first layer and at least one second layer structure, contiguous with each other, said at least one first layer comprising at least one element selected from the group consisting of indium and thallium; and said at least one second layer structure comprising at least one second layer consisting of one element, a binary alloy, or a ternary alloy, said second layer structure comprising lead, about 5 to about 20% tin, and from about 0.05 to about 5% of at least one wear resistance-enhancing element selected from the group consisting of antimony, manganese, bismuth, nickel, copper, calcium, and barium; and heating said first layer and second layer structure to such a temperature that interdiffusion between said layer and layer structure takes place, thereby forming a single overlay layer comprising said at least quaternary alloy-overlay.

Claim 4

A process for producing a bearing to be used in an internal combustion engine, said bearing comprising a base, and an at least quaternary alloy-overlay consisting of (i) from about 5% to about 20% of tin, (ii) from about 0.05% to about 10% of at least one element selected from the group consisting of indium and thallium, (iii) from about 0.05% to about 5% of at least one wear resistance-enhancing element selected from the group consisting of antimony, manganese, bismuth, nickel, copper, calcium, and barium, and (iv) lead and impurities in balance, all percentages being by weight, said process for forming said at least quaternary alloy-overlay comprising the steps of: separately forming on said base in any order, at least one first layer and at least one second layer structure, contiguous with each other, said at least one first layer comprising at least one element selected from the group consisting of indium and thallium; and said at least one second layer structure comprising at least one second layer consisting of one element, a binary alloy, or a ternary alloy, said second layer structure comprising lead, about 5 to about 20% tin, and from about 0.05 to about 5% of at least one wear resistance-enhancing element selected from the group consisting of antimony, manganese, bismuth, nickel, copper, calcium, and barium; and heating said first layer and second layer structure to such a temperature that interdiffusion between said layer and layer structure takes place, thereby forming a single overlay layer comprising said at least quaternary alloy-overlay.

Claim 5

A process according to claim 1 or 2, wherein said forming steps comprise: forming on said bearing material layer a second layer portion comprising at least tin; and forming on said second layer portion a first layer comprising at least one element selected from the group consisting of indium and thallium.

Claim 6

A process according to claim 3, wherein said second layer is formed by electrolytic plating.

Claim 7

A process according to claim 2, wherein said second layer additionally comprises at least one of said wear resistance-enhancing elements.

Claim 8

A process according to claim 4, wherein said at least one wear resistance-enhancing element is selected from the group consisting of calcium and barium and is added into a plating bath in the form of fine powder.

Claim 9

A process according to claim 6, wherein said fine powder has a particle size from about 0.1 to about 1 micron and the additional amount of said fine powder in said plating bath is from about 10 to about 50 grams per liter.

Claim 10

A process according to claim 5, wherein said at least one wear resistance-enhancing element is copper or antimony and the same is dissolved in said plating solution.

Claim 11

A process according to claim 1 or 2 comprising the steps of: forming by plating on said bearing material a base layer which consists of lead and tin; forming on said base layer a first layer comprising at least one element selected from the group consisting of indium and thallium; and forming on said first layer a top layer of said second layer structure comprising said wear resistance-enhancing element.

Claim 12

A process according to claim 9, wherein said wear resistance-enhancing element of said top layer is selected from the group consisting of manganese, bismuth, and nickel and said top layer is formed by plating.

Claim 13

A process according to claim 2, wherein the content of tin in said second layer structure after the formation thereof is less than about 10%.

Claim 14

A process according to claim 1 or 2, said process comprising the steps of: forming on said bearing material layer a layer of said second layer structure comprising at least lead and tin; forming on said layer of said second layer structure a first layer comprising at least one element selected from the group consisting of indium and thallium; forming on said first layer an additional layer of said second layer structure of tin; and heating said layer, first layer, and additional layer to such a temperature that interdiffusion between these layers takes place, thereby forming a single overlay layer comprising said at least one quaternary alloy-overlay.

Claim 15

A process according to claim 12, wherein the tin content of said overlay layer is not less than 10%.

Claim 16

A process according to claim 12, wherein said interdiffusion is a solid-solid diffusion.

Claim 17

A process for producing a bearing to be used in an internal combustion engine, said bearing comprising a base, a bearing material, an at least quaternary overlay, and an additional top plating layer of tin, said overlay consisting of (i) from about 5% to about 20% of tin, (ii) from about 0.05% to about 10% of at least one element selected from the group consisting of indium and thallium, (iii) from about 0.05% to about 5% of at least one wear-resistance-enhancing element selected from the group consisting of antimony, manganese, bismuth, nickel, copper, calcium, and barium, and (iv) lead and impurities in balance, all percentages being by weight, said process for forming said at least quaternary alloy-overlay comprising the steps of: separately forming on said bearing material base, in any order, at least one first layer and an at least one second layer structure, contiguous with each other, said at least one first layer comprising at least one element selected from the group consisting of indium and thallium; and an at least one second layer structure comprising one element, a binary alloy, or a ternary alloy, wherein at least one layer of said second layer structure comprising lead, tin, and at least one wear resistance-enhancing element selected from the group consisting of antimony, manganese, bismuth, nickel, copper, calcium, and barium; forming on said second layer structure an additional top layer of tin; and heating all of said layers to such a temperature that interdiffusion between the layers takes place, thereby forming a single overlay layer and said additional top layer of tin which is formed by the non-diffused remaining tin, said second layer structure and tin diffused from said additional layer of tin comprising said at least quaternary alloy-overlay.

Claim 18

A process for producing a bearing to be used in an internal combustion engine, said bearing comprising a base, a bearing material, an at least quaternary overlay, and an additional top plating layer of tin, said overlay consisting of (i) from about 5% to about 20% of tin, (ii) from about 0.05% to about 10% of at least one element selected from the group consisting of indium and thallium, (iii) from about 0.05% to about 5% of at least one wear-resistance-enhancing element selected from the group consisting of antimony, manganese, bismuth, nickel, copper, calcium, and barium, and (iv) lead and impurities in balance, all percentages being by weight, said process for forming said at least quaternary alloy-overlay comprising the steps of: separately forming on said bearing material base, in any order, at least one first layer and an at least one second layer structure, contiguous with each other, said at least one first layer comprising at least one element selected from the group consisting of indium and thallium; and an at least one second layer structure comprising one element, a binary alloy, or a ternary alloy, wherein at least one layer of said second layer structure comprising lead, tin, and at least one wear resistance-enhancing element selected from the group consisting of antimony, manganese, bismuth, nickel, copper, calcium, and barium; forming on said second layer structure an additional top layer of tin; and heating all of said layers to such a temperature that interdiffusion between the layers takes place, thereby forming a single overlay layer and said additional top layer of tin which is formed by the non-diffused remaining tin, said second layer structure and tin diffused from said additional layer of tin comprising said at least quaternary alloy-overlay.

Claim 19

A process for producing a bearing to be used in an internal combustion engine, said bearing comprising a base, an at least quaternary alloy-overlay, and an additional top plating layer of tin, said overlay consisting of (i) from about 5% to about 20% of tin, (ii) from about 0.05% to about 10% of at least one element selected from the group consisting of indium and thallium, (iii) from about 0.05% to about 5% of at least one wear-resistance-enhancing element selected from the group consisting of antimony, manganese, bismuth, nickel, copper, calcium, and barium, and (iv) lead and impurities in balance, all percentages being by weight, said process for forming said at least quaternary alloy-overlay comprising the steps of: separately forming on said base at least one first layer and at least one second layer structure, contiguous with each other, said at least one first layer comprising at least one element selected from the group consisting of indium and thallium wherein said first layer is formed over said second layer structure; and said at least one second layer structure consisting of one element, a binary alloy, or a ternary alloy, one said layer or a plurality of said layers comprising lead, about 5% to about 20% tin, and from about 0.05 to about 5% of at least one wear resistance-enhancing element selected from the group consisting of antimony, manganese, bismuth, nickel, copper, calcium, and barium; forming on top of said second layer structure an additional layer of tin; and heating all said layers to such a temperature that interdiffusion between the layers takes place, thereby forming a single overlay layer and said additional tin top layer which is formed by the non-diffused remaining tin, the total content of tin in said at least quaternary alloy-overlay comprising the amount of tin in said second layer structure and said first layer structure and said tin diffused from said additional layer of tin creating the composition of said at least quaternary alloy-overlay.

Claim 20

A process for producing a bearing to be used in an internal combustion engine, said bearing comprising a base, an at least quaternary alloy-overlay, and an additional top plating layer of tin, said overlay consisting of (i) from about 5% to about 20% of tin, (ii) from about 0.05% to about 10% of at least one element selected from the group consisting of indium and thallium, (iii) from about 0.05% to about 5% of at least one wear-resistance-enhancing element selected from the group consisting of antimony, manganese, bismuth, nickel, copper, calcium, and barium, and (iv) lead and impurities in balance, all percentages being by weight, said process for forming said at least quaternary alloy-overlay comprising the steps of: separately forming on said base at least one first layer and at least one second layer structure, contiguous with each other, said at least one first layer comprising at least one element selected from the group consisting of indium and thallium wherein said first layer is formed over said second layer structure; and said at least one second layer structure consisting of one element, a binary alloy, or a ternary alloy, one said layer or a plurality of said layers comprising lead, about 5% to about 20% tin, and from about 0.05 to about 5% of at least one wear resistance-enhancing element selected from the group consisting of antimony, manganese, bismuth, nickel, copper, calcium, and barium; forming on top of said second layer structure an additional layer of tin; and heating all said layers to such a temperature that interdiffusion between the layers takes place, thereby forming a single overlay layer and said additional tin top layer which is formed by the non-diffused remaining tin, the total content of tin in said at least quaternary alloy-overlay comprising the amount of tin in said second layer structure and said first layer structure and said tin diffused from said additional layer of tin creating the composition of said at least quaternary alloy-overlay.

Claim 21

A process according to claim 1, 2, 15 or 16 comprising the additional step of forming at least one barrier layer consisting of at least one metal selected from the group consisting of silver and nickel between said bearing material base and said overlay.