# US 11,028,463 B2 · Copper alloy containing tin, method for producing same, and use of same > Agents: this data is available as JSON from the patentgrep API and MCP server — see https://patentgrep.com/llms.txt - Number: US 11,028,463 B2 - Document ID: US11028463B2 - Status: Granted - Kind: B2 - Application number: 16/078,950 - Filed: 2017-02-10 - Published: 2019-02-28 - Granted: 2021-06-08 - Earliest claimed: 2016-03-03 - Assignees: Wieland-Werke AG - Applicants: Wieland-Werke AG - Inventors: Kai Weber - Web page: https://patentgrep.com/patent/US11028463B2 ## CPC - C22C 9/02: with tin as the next major constituent - B22D 21/025: {Casting heavy metals with high melting point, i.e. 1000 - 1600 degrees C, e.g. Co 1490 degrees C, Ni 1450 degrees C, Mn 1240 degrees C, Cu 1083 degrees C} - C22F 1/08: of copper or alloys based thereon - C22C: ALLOYS (treatment of alloys C21D, C22F) - B22D: CASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES (shaping of plastics or substances in a plastic state B29C; metallurgical processing, selection of substances to be added to metal C21, C22) - C22F: CHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS (surface treatment of metallic material involving at least one process provided for in class C23 and at least one process covered by this subclass, C23F17/00) ## Abstract The invention relates to a high-strength as-cast copper alloy containing tin, with excellent hot-workability and cold-workability properties, high resistance to abrasive wear, adhesive wear and fretting wear, and improved corrosion resistance and stress relaxation resistance, consisting (in wt. %) of: 4.0 to 23.0% Sn, 0.05 to 2.0% Si, 0.005 to 0.6 B, 0.001 to 0.08% P, optionally up to a maximum of 2.0% Zn, optionally up to a maximum of 0.6% Fe, optionally up to a maximum of 0.5% Mg, optionally up to a maximum of 0.25% Pb, with the remainder being copper and inevitable impurities, characterised in that the ratio of Si/B of the element content of the elements silicon and boron lies between 0.3 and 10. The invention also relates to a casting variant and a further-processed variant of the tin-containing copper alloy, a production method, and the use of the alloy. ## Claims ### Claim 1 A tin-containing copper alloy consisting of (in % by weight): 4.0% to 23.0% Sn, 0.05% to 2.0% Si, 0.005% to 0.6% B, 0.001% to 0.08% P, optionally up to a maximum of 2.0% Zn, optionally up to a maximum of 0.6% Fe, optionally up to a maximum of 0.5% Mg, optionally up to a maximum of 0.25% Pb, the balance being copper and unavoidable impurities, wherein the Si/B ratio of the element contents of the elements silicon and boron is between 0.3 and 10. ### Claim 2 A tin-containing copper alloy consisting of (in % by weight): 4.0% to 23.0% Sn, 0.05% to 2.0% Si, 0.005% to 0.6% B, 0.001% to 0.08% P, optionally up to a maximum of 2.0% Zn, optionally up to a maximum of 0.6% Fe, optionally up to a maximum of 0.5% Mg, optionally up to a maximum of 0.25% Pb, the balance being copper and unavoidable impurities, wherein the Si/B ratio of the element contents of the elements silicon and boron is between 0.3 and 10; after casting, the following microstructure constituents are present in the alloy: a) 1% to 98% by volume of Sn-rich δ phase (1), b) 1% to 20% by volume of Si-containing and B-containing phases (2), c) the balance being a solid solution of copper, consisting of low-tin α phase (3), wherein the Si-containing and B-containing phases (2) are ensheathed by tin and/or the Sn-rich δ phase (1); in the casting, the Si-containing and B-containing phases (2) which are in the form of silicon borides constitute seeds for homogeneous crystallization during the solidification/cooling of the melt, such that the Sn-rich δ phase (1) is distributed homogeneously in the microstructure in the form of islands and/or a network; the Si-containing and B-containing phases (2) which are in the form of boron silicates and/or boron phosphorus silicates, together with phosphorus silicates, assume the role of a wear-protective and/or corrosion-protective coating on semifinished products and components of the alloy. ### Claim 3 A tin-containing copper alloy consisting of (in % by weight): 4.0% to 23.0% Sn, 0.05% to 2.0% Si, 0.005% to 0.6% B, 0.001% to 0.08% P, optionally up to a maximum of 2.0% Zn, optionally up to a maximum of 0.6% Fe, optionally up to a maximum of 0.5% Mg, optionally up to a maximum of 0.25% Pb, the balance being copper and unavoidable impurities, wherein the Si/B ratio of the element contents of the elements silicon and boron is between 0.3 and 10; after a further processing of the alloy by at least one annealing operation or by at least one hot forming operation and/or cold forming operation in addition to at least one annealing operation, the following microstructure constituents are present in the alloy: a) up to 75% by volume of Sn-rich δ phase (1), b) 1% to 20% by volume of Si-containing and B-containing phases (2), c) the balance being a solid solution of copper, consisting of low-tin α phase (3), wherein the Si-containing and B-containing phases (2) are ensheathed by tin and/or the Sn-rich δ phase (1); the Si-containing and B-containing phases (2) present, which are in the form of silicon borides, constitute seeds for static and dynamic recrystallization of the microstructure during the further processing of the alloy, which enables the establishment of a homogeneous and fine-grain microstructure; the Si-containing and B-containing phases (2) which are in the form of boron silicates and/or boron phosphorus silicates, together with phosphorus silicates, assume the role of a wear-protective and/or corrosion-protective coating on the semifinished products and components of the alloy. ### Claim 4 (depends on 1) The tin-containing copper alloy as claimed in claim 1, wherein the element silicon is present at from 0.05% to 1.5%. ### Claim 5 (depends on 1) The tin-containing copper alloy as claimed in claim 1, wherein the element silicon is present at from 0.5% to 1.5%. ### Claim 6 (depends on 1) The tin-containing copper alloy as claimed in claim 1, wherein the element boron is present at from 0.01% to 0.6%. ### Claim 7 (depends on 1) The tin-containing copper alloy as claimed in claim 1, wherein the element phosphorus is present at from 0.001% to 0.05%. ### Claim 8 (depends on 1) The tin-containing copper alloy as claimed in claim 1, wherein the alloy is free of lead aside from any unavoidable impurities. ### Claim 9 (depends on 1) A process for producing end products and components having near-end-product form from a tin-containing copper alloy as claimed in claim 1 with the aid of a sandcasting process, a shell mold casting process, a precision casting process, a full mold casting process, a pressure diecasting process, or a lost foam process. ### Claim 10 (depends on 1) A process for producing strips, sheets, plates, bolts, round wires, profile wires, round bars, profile bars, hollow bars, pipes and profiles from a tin-containing copper alloy as claimed in claim 1 with the aid of a permanent mold casting process or a continuous or semicontinuous strand casting process. ### Claim 11 (depends on 10) The process as claimed in claim 10, wherein a further processing of a cast state comprises the performance of at least one hot forming operation within the temperature range from 600 to 880° C. ### Claim 12 (depends on 9) The process as claimed in claim 9, wherein at least one annealing treatment is conducted within the temperature range from 200 to 880° C. for a duration of 10 minutes to 6 hours. ### Claim 13 (depends on 10) The process as claimed in claim 10, wherein a further processing of a cast state or of a hot-formed state or of an annealed cast state or of an annealed hot-formed state comprises the performance of at least one cold forming operation. ### Claim 14 (depends on 13) The process as claimed in claim 13, wherein at least one annealing treatment is conducted within the temperature range from 200 to 880° C. for a duration of 10 minutes to 6 hours. ### Claim 15 (depends on 13) The process as claimed in claim 13, wherein a stress relief annealing/age annealing operation is conducted within the temperature range from 200 to 650° C. for a duration of 0.5 to 6 hours. ### Claim 16 (depends on 1) Adjustment gibs and sliding gibs, friction rings and friction disks, slide bearing faces in composite components, sliding elements and guide elements in internal combustion engines, valves, turbochargers, gears, exhaust gas aftertreatment systems, lever systems, braking systems and joint systems, hydraulic aggregates, and machines and installations in mechanical engineering, comprising the tin-containing copper alloy as claimed in claim 1. ### Claim 17 (depends on 1) Components, wire elements, guiding elements, and connection elements in electronics/electrical engineering, comprising the tin-containing copper alloy as claimed in claim 1. ### Claim 18 (depends on 1) Metallic articles in the breeding of seawater-dwelling organisms, percussion instruments, propellers, wings, marine propellers and hubs for shipbuilding, housings of water pumps, oil pumps and fuel pumps, guide wheels, runner wheels and paddle wheels for pumps and water turbines, gears, worm gears, helical gears, forcing nuts and spindle nuts, and pipes, seals and connection bolts in the maritime and chemical industry, comprising the tin-containing copper alloy as claimed in claim 1.