US2241815A - Method of treating copper alloy castings - Google Patents

Method of treating copper alloy castings Download PDF

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Publication number
US2241815A
US2241815A US224497A US22449738A US2241815A US 2241815 A US2241815 A US 2241815A US 224497 A US224497 A US 224497A US 22449738 A US22449738 A US 22449738A US 2241815 A US2241815 A US 2241815A
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Prior art keywords
castings
treatment
copper alloy
copper
heat treatment
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US224497A
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Franz R Hensel
Earl I Larsen
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Duracell Inc USA
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PR Mallory and Co Inc
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Priority to US224497A priority Critical patent/US2241815A/en
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    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C9/00Alloys based on copper
    • C22C9/06Alloys based on copper with nickel or cobalt as the next major constituent

Definitions

  • This invention relates to the production of copper alloy castings, containing high percentages of copper.
  • Another object of the present invention is to produce castings which can be readily brazed, soldered or welded, without destroying their physical properties.
  • the present invention comprises a combination of elements, methods of manufacture and the product thereof, brought out and exemplified in the disclosure, hereinafter set forth, the scope of the invention being indicated in the appended claims.
  • alloys have been described containing hardening elements, such as the silicides of the iron group metals.
  • harden materials of this type it has been necessary to apply a double heat treatment, the first part of which is generally classified as a solution treatment, and which consists in heating the material to a high temperature and then rapidly quenching.
  • a second treatment is employed, comprising a prolonged heating at a lower temperature. This is usually called the aging or precipitation treatment because this treatment causes the decomposition of a super-saturated solid solution, the precipitated particles being so small in most cases that they cannot be detected under a microscope.
  • composition inconsistency of physical properties could not be eliminated or correlated with composition.
  • other elements such as magnesium, aluminum, zinc, tin, phosphorus and cadmium, in percentages up to 5% without, however, resulting in improvement of the ultimate strength as long as the double heat treatment was employed.
  • the process of annealing is applied to sand castings or chill castings, irrespective of cross section. It usually consists in heating alloys for the present invention can be prepared without taking any special precautions. Usually the copper is melted first, then the alloy additions are made, preferably in the form of a suitable hardener and the melt is poured in either sand, chill or other molds. The castings should then be used without any application of hot working because such hot working operationswill partly destroy the beneficial eifect of the single heat treatment described in this application.
  • the castings prepared as indicated above are well suited for such parts as electrode wheels, current carrying members, heat carrying members, axles, shafts and corrosion resistant parts.
  • the preferred composition of the castings is as follows:
  • copper alloys containing nickel and silicon may also contain such elements as zinc, tin, silver, cadmium, magnesium, beryllium, aluminum,- titanium, zirconium, chromium, manganese, iron and cobalt.
  • the method of improving the properties of copper which comprises alloying with copper 0.5 to 5% of an element selected from the group consisting of nickel and cobalt and 0.1 to 2% silicon, casting the resulting alloy and then annealing the alloy in the as cast condition at a temperature between 400 C. and 600 C. for a period of from several minutes to several hours to improve the hardness and tensile strength.
  • the method of improving the physical properties and particularly the tensile strength of castings consisting of 0.5 to 5% nickel, 0.1 toi 2% silicon and the balance copp r which comprises applying a single heat treatment to said castings in the as cast condition, said heat treatment consisting of an anneal for a period of from several minutes to several hours at a temperature within the range 400 C. and 600 C.

Description

Patented May 13, 1941 UNITED STATES PATENT. OFFICE METHOD OF TREATING COPPER. ALLOY CASTINGS Franc R. Hensel and Earl I. Larsen, Indianapolis, Ind., assignors to R. R. Mallory & Co. Inc., Indianapolis, had, a corporation of Delaware No Drawing. Application August 12, 1938, Serial No. 224,497
2 Claims.
This invention relates to the production of copper alloy castings, containing high percentages of copper.
It is an object of the invention to produce castings of improved hardness, electrical and structural parts and in the mechanical held, in-
applications where. high thermal conductivity is required, together with improved strength. It is a further object of this invention to produce castings which will not anneal at elevated temperatures.
It is a further object of this invention to produce castings which have a high ratio of elastic limit to tensile strength.
Another object of the present invention is to produce castings which can be readily brazed, soldered or welded, without destroying their physical properties.
Other objects will be apparent from the following description, taken in connection with the appended claims.
The present invention comprises a combination of elements, methods of manufacture and the product thereof, brought out and exemplified in the disclosure, hereinafter set forth, the scope of the invention being indicated in the appended claims.
While a preferred embodiment of the invention is described herein, it is contemplated that considerable variation may be made in the method of procedure and a combination of elements, githout departing from the spirit of the inven- In the prior art, alloys have been described containing hardening elements, such as the silicides of the iron group metals. harden materials of this type, it has been necessary to apply a double heat treatment, the first part of which is generally classified as a solution treatment, and which consists in heating the material to a high temperature and then rapidly quenching. In addition to this first treatment, a second treatment is employed, comprising a prolonged heating at a lower temperature. This is usually called the aging or precipitation treatment because this treatment causes the decomposition of a super-saturated solid solution, the precipitated particles being so small in most cases that they cannot be detected under a microscope.
Heretofore, attempts have been made to manu- I iacture castings commercially 01' copper hard- In order to ened with nickel silicide, using the double heat treatment of the prior art just described. The result was such a large number of failures of the castings that manufacture of this alloy was discontinued.
We have found that for many uses the above double heat treatment will not produce the desired results when applied to copper alloys hardened with nickel or cobalt silicide.
While the castings show a considerable increase in hardness and conductivity, after such a double treatment, at the same time they become, very frequently, extremely brittle, and show very low tensile strength. In a large number of castings treated that way, the ultimate tensile strength was only 5,000 p. s, i., and in many instances, it was so low that the castings broke as a result of this heat treatment. Numerous tests were made, in which melting conditions and alloying conditions were variedffiowever,
the inconsistency of physical properties could not be eliminated or correlated with composition. In addition to copper and nickel silicide, other elements were added, such as magnesium, aluminum, zinc, tin, phosphorus and cadmium, in percentages up to 5% without, however, resulting in improvement of the ultimate strength as long as the double heat treatment was employed.
We then made experiments in which the heat treatment was completely changed in such a manner that the solution treatment was entirely eliminated and only a single heat treatment, corresponding to an anneal, was used. The result was that hardness values could be obtained closely approaching those and in some cases equivalent to the ones obtained with the double heat 1 treatment. The electrical conductivity, resulting from the single annealing treatment, was
additions of nickel and silicon, are approximately as follows:
Tensile strength p. s. i.-- 60,000 Brinell hardness -200 Electrical conductivity ..per cent 40-45 The ductility is a function of the chemical composition only and will vary from 5 to 35%, after our annealing treatment.
The process of annealing is applied to sand castings or chill castings, irrespective of cross section. It usually consists in heating alloys for the present invention can be prepared without taking any special precautions. Usually the copper is melted first, then the alloy additions are made, preferably in the form of a suitable hardener and the melt is poured in either sand, chill or other molds. The castings should then be used without any application of hot working because such hot working operationswill partly destroy the beneficial eifect of the single heat treatment described in this application.
The castings prepared as indicated above are well suited for such parts as electrode wheels, current carrying members, heat carrying members, axles, shafts and corrosion resistant parts.
The preferred composition of the castings is as follows:
. v Per cent Nickel 0.5 to 5 Silicon 0.1 to 2 Copper Balance It is possible likewise to improve alloys containing small percentages of aditional ingredients by the single heat treatment described above; thus copper alloys containing nickel and silicon may also contain such elements as zinc, tin, silver, cadmium, magnesium, beryllium, aluminum,- titanium, zirconium, chromium, manganese, iron and cobalt.
While the present invention, as to its objects and advantages, has been'described herein as carried out in specific embodiments thereof, it is not desired to be limited thereby, but it is intended to cover the invention broadly, within the spirit and scope of the appended claims.
What is claimed is:
l. The method of improving the properties of copper which comprises alloying with copper 0.5 to 5% of an element selected from the group consisting of nickel and cobalt and 0.1 to 2% silicon, casting the resulting alloy and then annealing the alloy in the as cast condition at a temperature between 400 C. and 600 C. for a period of from several minutes to several hours to improve the hardness and tensile strength.
2. The method of improving the physical properties and particularly the tensile strength of castings consisting of 0.5 to 5% nickel, 0.1 toi 2% silicon and the balance copp r which comprises applying a single heat treatment to said castings in the as cast condition, said heat treatment consisting of an anneal for a period of from several minutes to several hours at a temperature within the range 400 C. and 600 C.
FRANZ R. I-IENSEL.
EARL I. LARSEN.
US224497A 1938-08-12 1938-08-12 Method of treating copper alloy castings Expired - Lifetime US2241815A (en)

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Cited By (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3020326A (en) * 1958-08-21 1962-02-06 Minnesota Mining & Mfg Thermoelectric alloys and elements
DE1278110B (en) * 1960-03-09 1968-09-19 Ver Deutsche Metallwerke Ag Use of a hardenable copper alloy for the production of semi-finished products with increased shape change capacity
DE2718495A1 (en) * 1977-04-26 1978-11-02 Diehl Fa Copper alloys - for friction plate and frusto=conical elements in synchromesh gears
DE2942345A1 (en) * 1979-02-12 1980-08-21 Ampco Pitsburgh Corp COPPER ALLOY WITH IMPROVED ELECTRICAL CONDUCTIVITY
EP0203389A1 (en) * 1985-04-26 1986-12-03 Olin Corporation Multipurpose copper alloys with moderate conductivity and high strength, and process for manufacturing them
US4728372A (en) * 1985-04-26 1988-03-01 Olin Corporation Multipurpose copper alloys and processing therefor with moderate conductivity and high strength
DE3814439A1 (en) * 1987-04-28 1988-11-10 Mitsubishi Metal Corp MATERIAL FOR ELECTRICAL CONTACT SPRINGS MADE OF A COPPER ALLOY AND THE USE THEREOF
DE4415629C1 (en) * 1994-05-04 1995-08-17 Wieland Werke Ag Use of copper@-nickel@-silicon@ alloy in mfr. of cast pistons for pressure casting machines
DE102004013181B3 (en) * 2004-03-17 2005-09-22 Federal-Mogul Nürnberg GmbH Piston for an internal combustion engine, method of manufacturing a piston, and use of a copper alloy to make a piston
DE102005023308A1 (en) * 2005-05-13 2006-11-16 Federal-Mogul Wiesbaden Gmbh & Co. Kg Plain bearing composite material for plain bearing shells comprises a support layer made from steel, a bearing metal layer made from a copper alloy and a sliding layer applied to the bearing metal layer
WO2006120018A1 (en) 2005-05-13 2006-11-16 Federal-Mogul Wiesbaden Gmbh & Co. Kg Plain bearing composite material, use thereof and production methods therefor
DE102005023306B4 (en) * 2005-05-13 2007-04-05 Federal-Mogul Wiesbaden Gmbh & Co. Kg Slide bearing composite, use and manufacturing process
DE102005063324B4 (en) * 2005-05-13 2008-02-28 Federal-Mogul Wiesbaden Gmbh & Co. Kg Slide bearing composite, use and manufacturing process
US20090035174A1 (en) * 2005-03-24 2009-02-05 Nippon Mining & Metals Co., Ltd. Copper Alloy for Electronic Materials
US20090081471A1 (en) * 2005-05-13 2009-03-26 Maik Wilhelm Slide Bearing Composite Material, Use and Method of Production
US20100323218A1 (en) * 2005-05-13 2010-12-23 Maik Wilhelm Plain bearing composite material, use thereof and production methods therefor

Cited By (27)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3020326A (en) * 1958-08-21 1962-02-06 Minnesota Mining & Mfg Thermoelectric alloys and elements
DE1278110B (en) * 1960-03-09 1968-09-19 Ver Deutsche Metallwerke Ag Use of a hardenable copper alloy for the production of semi-finished products with increased shape change capacity
DE1278110C2 (en) * 1960-03-09 1973-09-20 Ver Deutsche Metallwerke Ag USE OF A CURABLE COPPER ALLOY FOR THE MANUFACTURE OF SEMI-FINISHED PRODUCTS WITH INCREASED MOLDING CAPACITY
DE2718495A1 (en) * 1977-04-26 1978-11-02 Diehl Fa Copper alloys - for friction plate and frusto=conical elements in synchromesh gears
DE2942345A1 (en) * 1979-02-12 1980-08-21 Ampco Pitsburgh Corp COPPER ALLOY WITH IMPROVED ELECTRICAL CONDUCTIVITY
EP0203389A1 (en) * 1985-04-26 1986-12-03 Olin Corporation Multipurpose copper alloys with moderate conductivity and high strength, and process for manufacturing them
US4728372A (en) * 1985-04-26 1988-03-01 Olin Corporation Multipurpose copper alloys and processing therefor with moderate conductivity and high strength
AU586674B2 (en) * 1985-04-26 1989-07-20 Olin Corporation Multipurpose copper alloys and processing therefor with moderate conductivity and high strength
DE3814439A1 (en) * 1987-04-28 1988-11-10 Mitsubishi Metal Corp MATERIAL FOR ELECTRICAL CONTACT SPRINGS MADE OF A COPPER ALLOY AND THE USE THEREOF
DE4415629C1 (en) * 1994-05-04 1995-08-17 Wieland Werke Ag Use of copper@-nickel@-silicon@ alloy in mfr. of cast pistons for pressure casting machines
DE102004013181B3 (en) * 2004-03-17 2005-09-22 Federal-Mogul Nürnberg GmbH Piston for an internal combustion engine, method of manufacturing a piston, and use of a copper alloy to make a piston
WO2005093244A1 (en) 2004-03-17 2005-10-06 Federal-Mogul Nürnberg GmbH Piston for an internal combustion engine, method for producing said piston and use of a copper alloy in the production of a piston
US20090035174A1 (en) * 2005-03-24 2009-02-05 Nippon Mining & Metals Co., Ltd. Copper Alloy for Electronic Materials
US8317948B2 (en) * 2005-03-24 2012-11-27 Jx Nippon Mining & Metals Corporation Copper alloy for electronic materials
US20090081471A1 (en) * 2005-05-13 2009-03-26 Maik Wilhelm Slide Bearing Composite Material, Use and Method of Production
DE102005023306B4 (en) * 2005-05-13 2007-04-05 Federal-Mogul Wiesbaden Gmbh & Co. Kg Slide bearing composite, use and manufacturing process
DE102005063325B4 (en) * 2005-05-13 2008-01-10 Federal-Mogul Wiesbaden Gmbh & Co. Kg Slide bearing composite, use and manufacturing process
DE102005063324B4 (en) * 2005-05-13 2008-02-28 Federal-Mogul Wiesbaden Gmbh & Co. Kg Slide bearing composite, use and manufacturing process
DE102005023308A1 (en) * 2005-05-13 2006-11-16 Federal-Mogul Wiesbaden Gmbh & Co. Kg Plain bearing composite material for plain bearing shells comprises a support layer made from steel, a bearing metal layer made from a copper alloy and a sliding layer applied to the bearing metal layer
WO2006120018A1 (en) 2005-05-13 2006-11-16 Federal-Mogul Wiesbaden Gmbh & Co. Kg Plain bearing composite material, use thereof and production methods therefor
US20090263053A1 (en) * 2005-05-13 2009-10-22 Gerd Andler Plain Bearing Composite Material, Use Thereof and Production Methods Therefor
US20100068557A1 (en) * 2005-05-13 2010-03-18 Gerd Andler Plain Bearing Composite Material, Use Thereof and Production Methods Therefor
US20100323218A1 (en) * 2005-05-13 2010-12-23 Maik Wilhelm Plain bearing composite material, use thereof and production methods therefor
US7993758B2 (en) 2005-05-13 2011-08-09 Federal-Mogul Wiesbaden Gmbh & Co. Kg Slide bearing composite material
US8241758B2 (en) 2005-05-13 2012-08-14 Federal-Mogul Weisbaden Gmbh & Co. Kg Plain bearing composite material, use thereof and production methods therefor
DE102005023308B4 (en) * 2005-05-13 2007-02-08 Federal-Mogul Wiesbaden Gmbh & Co. Kg Slide bearing composite, use and manufacturing process
US8360647B2 (en) 2005-05-13 2013-01-29 Federal-Mogul Wiesbaden Gmbh Plain bearing composite material, use thereof and production methods therefor

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