RU2006135401A - MECHANICAL PROCESSING ALLOY ON THE BASIS OF COPPER AND METHOD OF ITS PRODUCTION - Google Patents

MECHANICAL PROCESSING ALLOY ON THE BASIS OF COPPER AND METHOD OF ITS PRODUCTION Download PDF

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Publication number
RU2006135401A
RU2006135401A RU2006135401/02A RU2006135401A RU2006135401A RU 2006135401 A RU2006135401 A RU 2006135401A RU 2006135401/02 A RU2006135401/02 A RU 2006135401/02A RU 2006135401 A RU2006135401 A RU 2006135401A RU 2006135401 A RU2006135401 A RU 2006135401A
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Russia
Prior art keywords
stage
heat treatment
tin
nickel
lead
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RU2006135401/02A
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Russian (ru)
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RU2348720C2 (en
Inventor
Эмманюэль ВЕНСАН (CH)
Эмманюэль ВЕНСАН
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Свиссметал-Юмс Юзин Металлюржик Сюисс Са (Ch)
Свиссметал-Юмс Юзин Металлюржик Сюисс Са
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Priority to RU2006135401/02A priority Critical patent/RU2348720C2/en
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  • Metal Extraction Processes (AREA)
  • Continuous Casting (AREA)

Claims (14)

1. Способ производства металлического продукта, состоящего из сплава, содержащего от 1 до 20 мас.% никеля, от 1 до 20 мас.% олова, от 0,2 до 2 мас.% свинца, остальным по существу является медь,1. A method of manufacturing a metal product consisting of an alloy containing from 1 to 20 wt.% Nickel, from 1 to 20 wt.% Tin, from 0.2 to 2 wt.% Lead, the rest essentially copper, при этом способ включает термическую обработку, включающую стадию нагрева и гомогенизации сплава,wherein the method includes a heat treatment comprising a step of heating and homogenizing the alloy, определение достаточно медленной скорости охлаждения для предотвращения растрескивания и достаточно высокой для ограничения образования двухфазной структуры, иdetermining a sufficiently slow cooling rate to prevent cracking and high enough to limit the formation of a two-phase structure, and последующую стадию охлаждения с заданной скоростью.the subsequent stage of cooling at a given speed. 2. Способ по п.1, в котором после термической обработки следует стадия холодной деформации, осуществляемая прокаткой, волочением в проволоку, формованием с вытяжкой или ковкой.2. The method according to claim 1, in which after the heat treatment is followed by a stage of cold deformation, carried out by rolling, drawing into wire, molding with a hood or forging. 3. Способ по п.1, в котором термическую обработку проводят в проходной печи.3. The method according to claim 1, in which the heat treatment is carried out in a continuous furnace. 4. Способ по п.1, включающий первоначальную стадию непрерывного литья с последующей стадией ковки или первоначальную стадию «статической» отливки заготовки или стадию распылительного формовании заготовки или стадию полунепрерывного литья заготовки с последующей стадией экструзии.4. The method according to claim 1, comprising the initial stage of continuous casting followed by a stage of forging or the initial stage of "static" casting of the workpiece or the stage of spray molding of the workpiece or the stage of semi-continuous casting of the workpiece with the subsequent stage of extrusion. 5. Способ по п.1, в котором термическая обработка происходит при температуре от 690 до 920°С.5. The method according to claim 1, in which the heat treatment occurs at a temperature of from 690 to 920 ° C. 6. Способ по п.1, в котором поперечный размер металлического продукта во время термической обработки составляет от 1 до 100 мм.6. The method according to claim 1, in which the transverse size of the metal product during heat treatment is from 1 to 100 mm 7. Способ по п.1, в котором скорость охлаждения на стадии охлаждения термической обработки составляет от 10 до 24000°С/мин или от 10 до 4000°С/мин, или от 100 до 1500°С/мин.7. The method according to claim 1, in which the cooling rate in the cooling stage of the heat treatment is from 10 to 24000 ° C / min or from 10 to 4000 ° C / min, or from 100 to 1500 ° C / min. 8. Способ по п.1, в котором скорость охлаждения на стадии охлаждения термической обработки составляет от 100 до 1000°С/мин.8. The method according to claim 1, in which the cooling rate in the cooling stage of the heat treatment is from 100 to 1000 ° C / min. 9. Способ по п.1, включающий стадию вытягивания в проволоку или формования с вытяжкой, или ковки, или прокатки.9. The method according to claim 1, comprising the step of drawing into a wire or molding with a hood, or forging, or rolling. 10. Способ по п.1, включающий обработку со спинодальным твердением.10. The method according to claim 1, including processing with spinodal hardening. 11. Способ по п.1, где сплав содержит от 6 до 8 мас.% никеля, от 4 до 6 мас.% олова и от 0,5 до 2 мас.% свинца.11. The method according to claim 1, where the alloy contains from 6 to 8 wt.% Nickel, from 4 to 6 wt.% Tin and from 0.5 to 2 wt.% Lead. 12. Способ по п.1, где сплав содержит от 8 до 10 мас.% никеля, от 5 до 7 мас.% олова и от 0,5 до 2 мас.% свинца.12. The method according to claim 1, where the alloy contains from 8 to 10 wt.% Nickel, from 5 to 7 wt.% Tin and from 0.5 to 2 wt.% Lead. 13. Способ по п.1, в котором сплав содержит от 14 до 16 мас.% никеля, от 7 до 9 мас.% олова и от 0,5 до 2 мас.% свинца.13. The method according to claim 1, in which the alloy contains from 14 to 16 wt.% Nickel, from 7 to 9 wt.% Tin and from 0.5 to 2 wt.% Lead. 14. Продукт, полученный способом по п.1.14. The product obtained by the method according to claim 1.
RU2006135401/02A 2004-04-05 2004-04-05 Machinable alloy on basis of copper and method of its manufacturing RU2348720C2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU2006135401/02A RU2348720C2 (en) 2004-04-05 2004-04-05 Machinable alloy on basis of copper and method of its manufacturing

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RU2006135401A true RU2006135401A (en) 2008-04-20
RU2348720C2 RU2348720C2 (en) 2009-03-10

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Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105229192B (en) * 2013-03-14 2018-09-11 美题隆公司 Improve the formability of forging copper-nickel-tin alloy
US9487850B2 (en) * 2013-03-14 2016-11-08 Materion Corporation Ultra high strength copper-nickel-tin alloys
CN107354414B (en) * 2013-03-15 2019-11-29 美题隆公司 Metastable alloy and product with uniform grain size
JP7084137B2 (en) * 2014-03-17 2022-06-14 マテリオン コーポレイション High-strength and uniform copper-nickel-tin alloy and manufacturing process
US10844671B2 (en) 2014-03-24 2020-11-24 Materion Corporation Low friction and high wear resistant sucker rod string
CN114753779A (en) 2014-06-05 2022-07-15 美题隆公司 Coupling for rod
US10844670B2 (en) 2014-06-05 2020-11-24 Materion Corporation Couplings for well pumping components
TWI728969B (en) 2015-03-18 2021-06-01 美商麥提利恩公司 Magnetic copper alloys
RU2760688C1 (en) * 2021-06-10 2021-11-29 Публичное акционерное общество «Авиационная корпорация «Рубин» Method for manufacturing billets from antifriction bronze by casting with following extrusion

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