US2196002A - Method of treating electro-deposited metal - Google Patents

Method of treating electro-deposited metal Download PDF

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US2196002A
US2196002A US213366A US21336638A US2196002A US 2196002 A US2196002 A US 2196002A US 213366 A US213366 A US 213366A US 21336638 A US21336638 A US 21336638A US 2196002 A US2196002 A US 2196002A
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copper
wire
metal
heating
steel
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Leslie C Whitney
John A Heidish
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Copperweld Steel Co
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    • CCHEMISTRY; METALLURGY
    • C25ELECTROLYTIC OR ELECTROPHORETIC PROCESSES; APPARATUS THEREFOR
    • C25DPROCESSES FOR THE ELECTROLYTIC OR ELECTROPHORETIC PRODUCTION OF COATINGS; ELECTROFORMING; APPARATUS THEREFOR
    • C25D5/00Electroplating characterised by the process; Pretreatment or after-treatment of workpieces
    • C25D5/48After-treatment of electroplated surfaces
    • C25D5/50After-treatment of electroplated surfaces by heat-treatment
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10STECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S428/00Stock material or miscellaneous articles
    • Y10S428/922Static electricity metal bleed-off metallic stock
    • Y10S428/9335Product by special process
    • Y10S428/934Electrical process
    • Y10S428/935Electroplating
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00Metal working
    • Y10T29/49Method of mechanical manufacture
    • Y10T29/4998Combined manufacture including applying or shaping of fluent material
    • Y10T29/49982Coating
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/12All metal or with adjacent metals
    • Y10T428/12493Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.]
    • Y10T428/12771Transition metal-base component
    • Y10T428/12861Group VIII or IB metal-base component
    • Y10T428/12903Cu-base component
    • Y10T428/12917Next to Fe-base component

Definitions

  • Processheat-treatthe bimetallic ingot thus formed being rolled e s are u nt y sam t ay e and drawn-into wire.
  • an outstanding advantage necessary, for mp o eal e ate al of such process is that a permanent union be- Whi n M 5 1 Order to p m f further tween the copper and the steel is formed, but it wire drawing, or it may be desirable to anneal, also has certain disadvantages, among them benormalize, or oth w se 11 t e the l P 'ing the fact that it is impossible by the use of n t i order o d e p t e i e p y ical cr pmolten copper to produce a sheath of as great erties- During such heal m n is e r purity and high electrical conductivity as is other porous Zones a likely to mil/e109, l u- 8G desired.
  • Figure 1 isv a side elevation of a bimetallic wire broken away to show the successive layers
  • Figure 2 is a side elevation of a wire which has been heated to such temperature as to develop blisters
  • Figure 3 is a transverse section of the blistered wire shown in Figure 2;
  • Figure 4 is a diagrammatic view illustrating one form of apparatus by which our process may be carried out
  • Figures 5 and 6 are diagrammatic views illustrating further steps in the manufacture
  • Figure 7 is a view similar to Figure 4 showing the preferred practice of the invention.
  • Figure 8 is a partial sectional view taken along the plane of line VIII-VIII of Figure 7;
  • Figure 9 is a photomicrograph showing the structure of the copper as deposited.
  • Figure 10 is a photomicrograph showing the electrodeposited copper after heating only.
  • Figure 11 is a photomicrograph showing the electrodeposited copper after heating and hotworking.
  • the bimetallic wire shown in Figure 1 comprises a core 2 of drawn steel. We have successfully employed simple steel wire .375" in diameter. The carbon content is immaterial and will' be determined by the physical properties desired. It will be obvious, of course, that alloy steel wires may also be employed if need be.
  • the core 2 is covered with a continuous sheath 3 of acid copper. The copper may be deposited directly on the steel, but we have found it advantageous to use an intermediate layer 4 of nickel. It will be understood, of course, that instead of nickel, alkaline copper, electrolytic tin, zinc or iron, or other metal may be used, or if desired, the wire, prior to the deposition of copper, may be subjected to a chemical dip of arsenic trioxide in hydrochloric acid and water.
  • the percentage of copper in the final product will vary according to the requirements of the user.
  • Bimetallic wire is usually rated according to the percentage relation which its conductivity bears to a solid copper wire of the same diameter.
  • a conductivity wire is one whose ratio of steel to copper is such that the wire will have a conductivity 30% of the conductivity of a solid copper wire of the same diameter.
  • it is necessary to electrodeposit sufficient copper to make the diameter of the starting body 0% conductivity wire may be made from a starting body having a steel core .375" in diameter and a diameter, with the copper sheath, of .467".
  • Figure 3 which shows the wire in cross section, illustrates a blister 5a within the boundaries of the copper and a blister 5b at the interface between the copper and the steel.
  • the blisters when developed are likely to lead to veryserious difiiculties either in subsequent manufacturing 1 trolled laboratory conditions to obtain a deposit wherein a minimum of blisters and porous zones will develop upon heat treatment, we are of the belief that it is difllcult it not impossible to avoid them entirely and have ioundthat they are of frequent occurrence in commercially deposited copper.
  • Figure 9 is a photomicrograph of a commercial deposit magnified to 90 diameters, showing an etched section of a test specimen with the steel core below a layer of cyanide copper and a main deposit of acid copper above.
  • asv viewed acid copper shows distinct lines of interruption, as indicated at 6 in the drawings.
  • This particular sample was formed by'a succession of deposits, the article passing through a series of electrolytic baths.
  • the columnar structure, indicated at 7, is very marked in the drawings and is characteristic of heavy deposits.
  • the grain boundary lines extend in a direction generally perpendicular to the axis of the wire and form lines of weakness which may cause cracking of the copper on flexing or bending of the wire, or an attempted reduction thereof as by drawing.
  • the deposited copper may be recrystallized by heat treatment.
  • Figure 10 shows an etched section of avspecimen'cut from the same piece and adjacent the same point in the piece as that illustrated in Figure it, after being heated in a reducing atmosphere to 1400 F. for 30 minutes and allowed to cool man. It will be noted that the copper has recrystallized into very large grains. Such grains may be objectionablein certain cases and the heating time is commercially excessive. The radial crack has been enlarged.
  • FIG 4 illustrates diagrammatically one form of apparatus which we have successfully employed for this purpose.
  • wire W havinga wrought steel core and an electrodeposited sheath and of the dimensions given above is fed from a coil a through a water seal Q to a hollow heating tube iii.
  • the tube is contained largely within a furnace ii heated in any desired manner, as by burners it.
  • the tube iii is kept filled with hydrogen supplied from a source H through a reducing valve l3 and a tube 16 communicating with the pipe in.
  • a source H through a reducing valve l3 and a tube 16 communicating with the pipe in.
  • the delivery end of the pipe ill projects beyond the end of the furnace H and is tapered as indicated at E6.
  • the delivery end of the pipe I0 is very close to the die l5 and within the die holder l7.
  • the drawing lubricant as indicated at Ii.
  • the lubricant employed is graphite mixed with grease, which is a reducing compoundand it is placed around the end of the tube so as to seal. it of! from the atmosphere as well as to provide lubri cation for drawing.
  • the wire is drawn through the apparatus by a drawing block IQ of usual construction.
  • Figure ll is l a photomicrograph of an etched section oi a specimen cut from the same piece and from the same location therein as that illustrated in Figures 9 and 10. After heating, as before described, this specimen was given a 9% reduction by hot drawing through die it and cooled under a water spray.
  • the copper has been homogenized by heat and pressure so as to give a grain structure of the character of annealed wrought metal. At'the same time, ithas the purity 01' electrolytic metal and is free of porosity.
  • the heating to which the wire was subjected wassufiiclent to cause blisters and porous zones, but tests of the metal show it to be free of these defects.
  • the radial crack 1a which originally ex.- tended through the several specimens, has been fully closed.
  • FIG. 11 is not of the columnar form which characterizes the deposited copper shown in Figure 9.
  • the grains are smaller than in Figure 10, more uniform in size, and definitely equiraxed.
  • Another important advantage is that a very flrm union between the steel and thecopper is eflected. This union is so perfect that it successfully resists the severe tests hereinafter described.
  • the product shown in Figure ii may be subsequently worked either hot or cold and heat treated without danger of developing blisters or porous zones.
  • Figures 5 and 6 we have diagrammatically illustrated such further treatment.
  • FIGs 7 and 8 illustrate a modified form of apparatus which we. now prefer for practicing the method of our invention.
  • a wire W similar to that indicated in Figure 4 is unwound from a reel tt onto a guide sheave 3i.
  • the wire passes over a coating sheave 82, partially immersed in a bath of die lubricant 33, composed of engine oil and graphite.
  • the sheave $2 has a large peripheral groove 3% divided into segments by notched, radial vanes 36.
  • the lat- Sid ter insure the picking up of adequate die lubricant to thoroughly coat the wire.
  • the wire passes through a muille 38, a die 31', mountedon a support 38, and a cooling tank 39 provided with water sprays 40, after which it is wound up on the usual drawing block ii.
  • the water sprays quickly cool the material to room temperature and 'make it possible to operate at drawing speeds higher than'would otherwise be possible.
  • Electrical connections 42 and 43 extend i'roma suitable source of heating current to the sheave 3
  • electric current is passed through that portion of the wire betweenthe sheave II and support 38 to heat it to the desired temperature, say 1400 F.
  • the desired temperature say 1400 F.
  • Test specimens of material produced according to the procedure just described may be conveniently made up as follows:
  • Tubular specimens 1" long may readily be test-- ed for ductility and local defects; such. as the radial crack Ia shown in Figures 9 and 10, by driving a conical plug into one end, forcing the ends to "hell ou
  • the specimens which have been subjected to heating only, without hot drawing, and those heated only to 1000 F. or below, regardless of the amount of hot reduction (up to a maximum of 29%) show definite local failure as by cracking or splitting axially.
  • the reduction effected by the die l5 should be sufficient to insure that its influence is felt throughout the copper. This is best insured by providing a sufficient reduction by the die to reduce the cross sectional area of the base as well as to work the copper. . Generally speaking, the thicker the copper, the more mechanical work should be done in order to insure satisfactory results.
  • the invention is of general applicability and may be used in the manufacture of bimetallic bodies of other forms, such as rods, sheets, strips, and shapes. It may also be used for the manufacture of bimetallic or multimetallic bodies other than copper on steel, as for example, nickel on copper, nickel on iron, chromium on copper, copper on nickel, etc.
  • the invention is also useful in the manufacture of bodies of a single metal, as for example, copper may be deposited on a copper core, or the invention in certain aspects may be used for rendering workable commercial cathode copper which heretofore has been considered mechanically unworkable. It will be understood, therefore, that while we have illustrated and described a present preferred embodiment of the invention, in addition to an alternate practice, it is not so limited, but may be otherwise embodied or practiced within the scope of the following claims.
  • the steps consisting in electrodepositing a thick layer of copper over a steel base, heating the body and hot drawing it under non-oxidizing conditions which inhibit the formation of undesirable compounds of the electrodeposited metal to reduce the bimetallic body by a single pass through a die to a thickness approximating the original thickness of the base, thereby to compact and homogenize the copper.
  • the steps consisting in electrodepositing a thick layer of copper over a steel base and hot drawing the bimetallic body under non-oxidizing conditions which inhibit the formation of undesirable compounds of the electrodeposited metal to reduce it by a single pass through a die to a thickness substantially equivalent to that of a bimetallic body formed from a base of the same original thickness as the base of the body in question, and

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  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Chemical Kinetics & Catalysis (AREA)
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Description

April 1940- c. WHITNEY ET AL 2,196,002
umnon or TREATING ELECTRODEPOSITED mm Filgd June 1:, 1938 v 2 Shets-Sheet 1 INVENTOR S Leslie hl fney8 John A. dI-Sh April 2, @940. c. WHITNEY E1 AL METHOD OF TREATING ELECTRODEPOSITED METAL Filed June 15, 1938 2 Sheets-Sheet 2 TigJO.
Figll.
mvsmons Leslie C.Whifpey 3 1 John A.Heidlsh Patented Apr. 2, 1940 p a omrco STATES PATENT OFFICE mi lion or man-mo summosrosrrso METAL Leslie 0. Whitney, Forest Hills, and John A.
Heidish, Glassport, Pa asalsnors to Copperweld Steel Company, Glassport, Pa a corporation of Pennsylvania Application June 13, 1938, Serial No. 213,386
" '2 Claims. (Cl. all-lac) This invention relates to the treatment or electial in many of the products) the grain structro deposited metal and is herein particularly ture of the copper is unsatisfactory. The copper described as applied to the manufacture of a biwhich is first deposited is flue-g a ned, but as t e metallic wire or rod. Specifically, it is lllusthickness of the coating increases, the grains betrated and described as applied to the manufaccome much larger and are'columnar in character. 5 5 ture of a bimetallic rod or wire having a steel Because of this columnar structure, the opp core and a copper coating, although the inventends to crack if the wire is flexed in any material tion has numerous other applications. mount, t us d c destroying the This is a continuation-in-part of our copendus o es st a d other P ysical p ope t sing application Ser. No. 649,529, filed December For t e fo e fl g M it is commercially 30, 1e32, for Manufacture of electrodeposited desirable to form a bimetallic article of considerlmetal. 4 ably larger crosssectional' dimensions than the A bimetallic wire ha a steel cor and a cop-- final product and, to work this article clown to per sheath combines high strength with proteche final iz Uufort m t ll'. this pr c r tlon against corrosion and is used in many places e ely e ph sizes a u ber of h d t a ove where this combination or properties is desirae de ab u e t c s 0f the 0 p- I ble. Suchv/ire also has the property of high elecper p si ed must e consider b y crea or n trical conductivity compared with ferrous wires. Such a starting y than is t thickness of the It has been proposed to make wire of this cllarcopper in, the al pr d in Order t0 3 the actor by a wide variety of processes the most d s ed t ckn ss of copper there nrand the de-- conspicuously successful of which has been the facts a s o umnar truc re a e emmolterl process wherein molten copper has been vEmil/sited!- poured around a specially prepared steel billet, Other d mculties also arise. Processheat-treatthe bimetallic ingot thus formed being rolled e s are u nt y sam t ay e and drawn-into wire. an outstanding advantage necessary, for mp o eal e ate al of such process is that a permanent union be- Whi n M 5 1 Order to p m f further tween the copper and the steel is formed, but it wire drawing, or it may be desirable to anneal, also has certain disadvantages, among them benormalize, or oth w se 11 t e the l P 'ing the fact that it is impossible by the use of n t i order o d e p t e i e p y ical cr pmolten copper to produce a sheath of as great erties- During such heal m n is e r purity and high electrical conductivity as is other porous Zones a likely to mil/e109, l u- 8G desired. It is also dlmcult, particularly where la ly w th a thick oa- These l st s a e the percentage of copper in the wire is high, to probably due to the presence of foreign matter obtain concentriclty of the core and the sheath. which expands or forms a s up n h at n o H These cllmcultles. which are inherent in the they may e due to interruption in e c ystal older processes, argue for the manufacture of gr wth nd consequent lines of weakness in the bimetallic wire by a process of. electrodeposltl'ng metal. Howeve We do not limit ourselves to the copper over a steel core, but while many ateither 0! these theories. The fact remains that tempts have been made most of them have reblisters and p r s Zones are manifested l on sulted in failure because of a number of dif-- heating of athick Goemlally Produced l ctrorficulties which arise out oz? the step of electrodeposited body of metal, especially where the w depositing a relatively thicls coating of the .copsame has been put on in successive layers, as, for per or other sheath metal. example, by passing it through a series of cost- It hasbeeln propwed to draw the steel wire to lug baths. Once the blisters or porous zones have i its final slze ;and deposit the copper thereov'er. developed subsequent drawing of the wire in the 45 This, however} is not satisfactory for a number ordinary fashion does not heal them and a de-' of reasons. Itis desirable to subject the blmetal tective product results. lic body to cold work in order to develop the Considerable culty also arises due to lacll: proper physical properties. The copper in the of proper adherence of the copper to the base "as deposited" condition is porous. it is dlflicult metal. Even when the greatest care is elmaloyed, 50
if not impossible to obtain merely by electro difflculties arise on this score. Attempts to draw deposition a continuously extending and por wire made in this fashion, particularly where manent bond between the copper and the base blisters or porous zones have developed, result in metal. It the copper deposit is of any substan flaking or peeling of the copper and consequent M tlal thickness (and such thicknesses are essendamagecr spoilage oi the wire. 5@
Attempts have been made to overcome these defects by heat treatment, but these have not proved satisfactory. A thin coating of copper may by heat treatment be made to adhere fairly well to the base metal, but the difficulties of porosity are still present.
The difliculty of blistering upon heating has been recognized and it has been attempted to overcome the same by careful control of the heating conditions. However, such proposals have not worked out satisfactorily in practice. If it is attempted to limit the heating of the metal to such low temperature that the blisters do not develop, it is frequently impossible to obtain the desired results, and such operation requires so much time as to render it commercially impractical. Furthermore, such prolonged heating is conducive to the growth of very large grains, which grain structure is frequently undesirable.
We have found that these difficulties may be overcome and a superior product obtained by going contrary to established practice and deliberately heating the metal, and in some cases in an amount sufficient to develop porosity, and then working it under such conditions as to compact and homogenize the porous metal. We prefer to carry out these steps on the electrodeposited metal preliminary to any further reduction thereof and have discovered that by so doing the metal is put in such condition that it can be readily worked and can be subsequently heat treated without any danger of blisters or other porous zones developing. We have found that there are certain limitations as to the temperature to which the electrodeposited metal is heated and the extent of the hot drawing to which it is subjected. Specifically, the deposited metal must be heated to a temperature of about 1000 F. or higher and subjected to a reduction in sectional area by hot drawing of at least 5%.
We prefer to carry out the steps of our process in a continuous manner, preferably passing the metal continuously through a heating zone and hot working it as it is delivered from such zone.
We have found that it is important to maintain the metal during the heating and hot working steps in an atmosphere which inhibits the formation of undesirable compounds of the electrodeposited metal. It is definitely undesirable, for example, to allow the formation of oxides of the metal. If the metal is blistered or cracked, the formation of oxides opposes the healing of the surfaces during the hot work which follows the development of such porous zone. We have successfully employed an atmosphere of hydrogen.
The use of our process gives as a new and improved product a metal body characterized by the purity of electrolytic metal and a grain structure of the character of annealed wrought metal. Stated in another way, the metal has the purity of electrolytic metal and it' has been homogenized by heat and pressure. Such metal is particularly desirable as a sheath for a bimetallic article.
In the accompanying drawings, illustrating our invention as applied to the manufacture of bimetallic wire with a steel core and a copper sheath:
Figure 1 isv a side elevation of a bimetallic wire broken away to show the successive layers;
Figure 2 is a side elevation of a wire which has been heated to such temperature as to develop blisters;
Figure 3 is a transverse section of the blistered wire shown in Figure 2;
Figure 4 is a diagrammatic view illustrating one form of apparatus by which our process may be carried out;
Figures 5 and 6 are diagrammatic views illustrating further steps in the manufacture;
Figure 7 is a view similar to Figure 4 showing the preferred practice of the invention and,
diagrammatically, the apparatus used therein;
Figure 8 is a partial sectional view taken along the plane of line VIII-VIII of Figure 7;
Figure 9 is a photomicrograph showing the structure of the copper as deposited;
Figure 10 is a photomicrograph showing the electrodeposited copper after heating only; and
Figure 11 is a photomicrograph showing the electrodeposited copper after heating and hotworking. a
The bimetallic wire shown in Figure 1 comprises a core 2 of drawn steel. We have successfully employed simple steel wire .375" in diameter. The carbon content is immaterial and will' be determined by the physical properties desired. It will be obvious, of course, that alloy steel wires may also be employed if need be. The core 2 is covered with a continuous sheath 3 of acid copper. The copper may be deposited directly on the steel, but we have found it advantageous to use an intermediate layer 4 of nickel. It will be understood, of course, that instead of nickel, alkaline copper, electrolytic tin, zinc or iron, or other metal may be used, or if desired, the wire, prior to the deposition of copper, may be subiected to a chemical dip of arsenic trioxide in hydrochloric acid and water.
The percentage of copper in the final product will vary according to the requirements of the user. Bimetallic wire is usually rated according to the percentage relation which its conductivity bears to a solid copper wire of the same diameter. Thus a conductivity wire" is one whose ratio of steel to copper is such that the wire will have a conductivity 30% of the conductivity of a solid copper wire of the same diameter. In order to make 30% conductivity wire from a bimetallic starting body having a steel core .375" in diameter, it is necessary to electrodeposit sufficient copper to make the diameter of the starting body 0% conductivity wire may be made from a starting body having a steel core .375" in diameter and a diameter, with the copper sheath, of .467". The above examples require copper deposits of .028" and .046", respectively. These deposits are very much heavier than those employed in commercial electroplating and introduce the difficulties above referred .to. The ordinary commercial electrodeposit for purposes of surface protection is measurable only in ten-thousandths of an inch, whereas we are concerned with electrodeposits very much thicker. For example, even a wire having a copper sheath whose cross section is of the total cross section of the wire willhave a thickness of .005" on a core .375". These heavy deposits, when heated to the temperatures required for heat treating the metal, are very likely to develop blisters. We have shown blisters at 5 in Figure 2.
Figure 3, which shows the wire in cross section, illustrates a blister 5a within the boundaries of the copper and a blister 5b at the interface between the copper and the steel. The blisters when developed are likely to lead to veryserious difiiculties either in subsequent manufacturing 1 trolled laboratory conditions to obtain a deposit wherein a minimum of blisters and porous zones will develop upon heat treatment, we are of the belief that it is difllcult it not impossible to avoid them entirely and have ioundthat they are of frequent occurrence in commercially deposited copper. Figure 9 is a photomicrograph of a commercial deposit magnified to 90 diameters, showing an etched section of a test specimen with the steel core below a layer of cyanide copper and a main deposit of acid copper above. It will be noted that, asv viewed acid copper shows distinct lines of interruption, as indicated at 6 in the drawings. This particular sample was formed by'a succession of deposits, the article passing through a series of electrolytic baths. The columnar structure, indicated at 7, is very marked in the drawings and is characteristic of heavy deposits. The grain boundary lines extend in a direction generally perpendicular to the axis of the wire and form lines of weakness which may cause cracking of the copper on flexing or bending of the wire, or an attempted reduction thereof as by drawing. A radial crack appears at la, and is found to extend a consider-= able distance along the length of the'test specimen.
The deposited copper may be recrystallized by heat treatment. For example, Figure 10 shows an etched section of avspecimen'cut from the same piece and adjacent the same point in the piece as that illustrated in Figure it, after being heated in a reducing atmosphere to 1400 F. for 30 minutes and allowed to cool man. It will be noted that the copper has recrystallized into very large grains. Such grains may be objectionablein certain cases and the heating time is commercially excessive. The radial crack has been enlarged.
It is desired to obtain a structure which is free or excessively large grains and radial cracks and yet reduces the heating time to a minimum. We effect this result and homogenize the copper by combined heating and working. I
Figure 4 illustrates diagrammatically one form of apparatus which we have successfully employed for this purpose. wire W havinga wrought steel core and an electrodeposited sheath and of the dimensions given above is fed from a coil a through a water seal Q to a hollow heating tube iii. The tube is contained largely within a furnace ii heated in any desired manner, as by burners it. The tube iii is kept filled with hydrogen supplied from a source H through a reducing valve l3 and a tube 16 communicating with the pipe in. In the passage of the wire W through the pipe iii, it is raised to the desired temperature and is then in condition to be subjected to hot work. This is accomplished in the example shown by a wire die IS. The delivery end of the pipe ill projects beyond the end of the furnace H and is tapered as indicated at E6. The delivery end of the pipe I0 is very close to the die l5 and within the die holder l7.
under the microscope, the.
In Figure 4, a bimetallic The small space between the die l6 and the open end of the pipe I6 is packed by.
the drawing lubricant, as indicated at Ii. The lubricant employed is graphite mixed with grease, which is a reducing compoundand it is placed around the end of the tube so as to seal. it of! from the atmosphere as well as to provide lubri cation for drawing. The wire is drawn through the apparatus by a drawing block IQ of usual construction. The highly desirable final structure obtainable by our process is shown in Figure ll, which is l a photomicrograph of an etched section oi a specimen cut from the same piece and from the same location therein as that illustrated in Figures 9 and 10. After heating, as before described, this specimen was given a 9% reduction by hot drawing through die it and cooled under a water spray. It will'be noted that the copper has been homogenized by heat and pressure so as to give a grain structure of the character of annealed wrought metal. At'the same time, ithas the purity 01' electrolytic metal and is free of porosity. The heating to which the wire was subjected wassufiiclent to cause blisters and porous zones, but tests of the metal show it to be free of these defects. The radial crack 1a which originally ex.- tended through the several specimens, has been fully closed.
It will be further noted that the structure illustrated-in Figure 11 is not of the columnar form which characterizes the deposited copper shown in Figure 9. The grains are smaller than in Figure 10, more uniform in size, and definitely equiraxed. Another important advantage is that a very flrm union between the steel and thecopper is eflected. This union is so perfect that it successfully resists the severe tests hereinafter described.
The product shown in Figure ii may be subsequently worked either hot or cold and heat treated without danger of developing blisters or porous zones. In Figures 5 and 6, we have diagrammatically illustrated such further treatment. The wire W1 is shown in Figure 5 as being cold worked by drawing through a die it! and thereafter passed through a heat treating furnace 2i,as shown in Figure 6. This subse=- quent cold working and heating further im= proves the product.
Figures 7 and 8 illustrate a modified form of apparatus which we. now prefer for practicing the method of our invention. As therein shown, a wire W similar to that indicated in Figure 4 is unwound from a reel tt onto a guide sheave 3i. From the sheave 36, the wire passes over a coating sheave 82, partially immersed in a bath of die lubricant 33, composed of engine oil and graphite. As shown in Figure 8, the sheave $2 has a large peripheral groove 3% divided into segments by notched, radial vanes 36. The lat- Sid ter insure the picking up of suficient die lubricant to thoroughly coat the wire.
From the coating bath 3%, the wire passes through a muille 38, a die 31', mountedon a support 38, and a cooling tank 39 provided with water sprays 40, after which it is wound up on the usual drawing block ii. The water sprays quickly cool the material to room temperature and 'make it possible to operate at drawing speeds higher than'would otherwise be possible.
Electrical connections 42 and 43 extend i'roma suitable source of heating current to the sheave 3| and support 38, respectively. By means of these connections, electric current is passed through that portion of the wire betweenthe sheave II and support 38 to heat it to the desired temperature, say 1400 F. By making conaffects the change in grain structure already referred to, but also causes the die lubricant to be baked onto the wire. This heating also creates a reducing atmosphere within the muflie.
Test specimens of material produced according to the procedure just described may be conveniently made up as follows:
To provide specimens having different conductivity precentages (viz., 40%, and 20%), short lengths of steel rods having diameters of .500", .535, and .585" are subjected to electrodeposition suilicient to build them up to a common diameter of .650". For greater accuracy, these specimens are then turned down to a slightly smaller diameter such as .632", and then etched in nitric acid to a final diameter of .630". The test rods are then subjected to heating, for example, to 1000 F., for a period of 30 minutes in a reducing atmosphere. After heating, the rods are hot drawn through. dies which would normally produce various percentages of reduction in sectional area, e. g., 5%, 15%, 25%, and The pull required to draw the material through these dies, however, results in drafts of approximately 10%, 19%, 28%, and 38%.
After heating and hot drawing, a short length is cut out of the mid portion of the rods and the steel'core drilled through from end to end. The drilled sections are then placed in a hot 10% sulphuric acid bath to dissolve out the remainder of the steel core, leaving the copper in the form of a tube.
While we prefer to heat the material to 1000 F. or higher, to insure removal of all defects, it is possible to obtain an improvement of the physical properties of the deposited metal by heating to a somewhat lower temperature. Tensile tests on tubular specimens indicate that the maximum increase in ductility may be obtained .by heating to the temperatures indicated belowfif the electrodeposition has been carried out under optimum or ideal conditions:
Percent conductivity Percent hot of specimen Tempemmm' o reduction 20 600to800orthe practice l8 10001101200 10 to is 30 800 to 1000 or the practice. 10 to 38 1N0 10 to 28 40 800m 1000 l0t0 18 If the electrodeposition has been carried out under somewhat less favorable conditions, such as prevail in ordinary commercial practice, it has been found that a higher temperature say from 1400 F. to 1600 F. will produce the maximum improvement in physical properties of 30% conductivity material with a hot reduction of 10%.
Tubular specimens 1" long may readily be test-- ed for ductility and local defects; such. as the radial crack Ia shown in Figures 9 and 10, by driving a conical plug into one end, forcing the ends to "hell ou The specimens which have been subjected to heating only, without hot drawing, and those heated only to 1000 F. or below, regardless of the amount of hot reduction (up to a maximum of 29%) show definite local failure as by cracking or splitting axially. Specimens which have been heated to temperatures above 1000 F. (up to a maximum of 1800 F.) and hot drawn to reduce them by from 9% to 29%, all show uniform belling out" with corresponding thinning of the edges, but without any localized failures such as cracks or longitudinal splitting. This confirms the conclusions drawn from Figures 9, l0, and 11 as to the healing of defects such as radial cracks in the copper sheath by the combined heating and hot drawing.
Our investigations show that the temperature to which the copper-steel body above described should be heated in carrying out our process is between 600 F. and 1900 F. As the maximum temperature is approached, care must be exercized to make sure that the copper does not flow and become eccentric to the steel. If it is attempted to operate below the minimum temperature above given, it will be found difficult or impossible to carry out the processsuccessfully. It is preferred to use a temperature at least as high as that of any subsequent treatment to which the copper-steel body may be subjected and to follow this with the hot working at any temperature within the limits described above.
The reduction effected by the die l5 should be sufficient to insure that its influence is felt throughout the copper. This is best insured by providing a sufficient reduction by the die to reduce the cross sectional area of the base as well as to work the copper. .Generally speaking, the thicker the copper, the more mechanical work should be done in order to insure satisfactory results.
We have herein described our invention with particular reference to a bimetallic wire having a steel core and a copper sheath. However, the invention is of general applicability and may be used in the manufacture of bimetallic bodies of other forms, such as rods, sheets, strips, and shapes. It may also be used for the manufacture of bimetallic or multimetallic bodies other than copper on steel, as for example, nickel on copper, nickel on iron, chromium on copper, copper on nickel, etc. The invention is also useful in the manufacture of bodies of a single metal, as for example, copper may be deposited on a copper core, or the invention in certain aspects may be used for rendering workable commercial cathode copper which heretofore has been considered mechanically unworkable. It will be understood, therefore, that while we have illustrated and described a present preferred embodiment of the invention, in addition to an alternate practice, it is not so limited, but may be otherwise embodied or practiced within the scope of the following claims.
We claim:
1. In the method of making a bimetallic body, the steps consisting in electrodepositing a thick layer of copper over a steel base, heating the body and hot drawing it under non-oxidizing conditions which inhibit the formation of undesirable compounds of the electrodeposited metal to reduce the bimetallic body by a single pass through a die to a thickness approximating the original thickness of the base, thereby to compact and homogenize the copper.
2. In the method of making a bimetallic body, the steps consisting in electrodepositing a thick layer of copper over a steel base and hot drawing the bimetallic body under non-oxidizing conditions which inhibit the formation of undesirable compounds of the electrodeposited metal to reduce it by a single pass through a die to a thickness substantially equivalent to that of a bimetallic body formed from a base of the same original thickness as the base of the body in question, and
having a coating of copper of such thickness that including electrolytically depositing the sheath 2. firm bond between the steel and the copper can on the core to a thickness such'that the sectional be secured by heating alone; area of the sheath is a substantial fraction (e. g.
3. In the method of making electrodeposited about one-tenth or greater) of the sectional area copper, the steps consisting in electrodepositing a of the core and altering the grain structure of the 6 layer of copper, heating the metal, drawing the sheath as deposited to render the article capable metal while hot through a die, and lubricating of being drastically cold worked, by heating the the metal during drawing by a reducing subarticle to a temperature suitable for hot working stance. and reducing the sectional area of the article at 4. In the method of making a bimetallic wire, least 5% by drawing while at substantially such 10 the steps consisting in electrodepositing copper temperature. on an elongated steel core such as a rod or wire, 7. In a method of making bimetallic wire comheating the bimetallic body and drawing the bip sing a ferrous core and a opp r shea h. the metallic body while hot through a die, and lubristeps including electrolytically depositing copper eating the body during drawing by a reducing on a ferrous core to a thickness such that the secsubstance. tional area of the copper is a substantial fraction 5. In the method of making a bimetallic wire, or that of the core, and altering the grain structhe steps consisting in electrodepositing a suiture of the copper as deposited to render the wire ficiently thick layer of copper on an elongate steel capable of being drastically cold drawn by heatcore such as a large wire or rod as to produce ing the wire to a temperature suitable for hot 29 a conductor of about 30% conductivity, heating working and reducing its sectional area at least the bimetallic body and reducing it while hot by 5% by drawing while substantially at said temfrom 5% to about by a single pass under perature. non-oxidizing conditions through a die. LESLIE C.
6. In a method of making a composite metallic JOHN A. HEIDISH. 25
article including a core and asheath, the steps
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Cited By (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2420291A (en) * 1940-07-22 1947-05-13 Nat Standard Co Electrodepositing copper upon steel wire
US2490700A (en) * 1943-08-24 1949-12-06 John S Nachtman Production of alloy coating on base metal material
US2546447A (en) * 1945-05-15 1951-03-27 American Steel & Wire Co Art of drawing fine steel wire
US2689399A (en) * 1950-12-05 1954-09-21 Western Electric Co Plated article and method of making it
US3031068A (en) * 1954-07-21 1962-04-24 Ajax Mfg Co Wire lubricating device
US3187413A (en) * 1961-03-02 1965-06-08 G M Lab Inc Process of manufacturing servo motor rotors
US3197861A (en) * 1960-06-01 1965-08-03 Continental Can Co Production of non-porous vacuum metallized coatings on strip material
US3210843A (en) * 1959-10-06 1965-10-12 Seul Vincens Method of influencing the surface profile of solid elements, more especially of surface-improved or plated metal strips or sheets
US3475813A (en) * 1966-12-28 1969-11-04 Combustion Eng Welding process involving post weld formation of molten pool
FR2389691A1 (en) * 1977-05-06 1978-12-01 Kabmatik Ab
US4436560A (en) 1982-01-25 1984-03-13 Kabushiki Kaisha Toyota Chuo Kenkyusho Process for manufacturing boride dispersion copper alloys
EP0179517A1 (en) * 1984-10-23 1986-04-30 N.V. Bekaert S.A. Ferrous substrate with rubber adherent metal coating and method of making the same
US5087300A (en) * 1989-09-01 1992-02-11 Fujikura Ltd. Method for manufacturing high-conductivity copper-clad steel trolley wire
US20090155620A1 (en) * 2006-03-08 2009-06-18 Kabushiki Kaisha Bridgestone Brass-plated steel wire for reinforcing rubber articles and method for manufacturing the same

Cited By (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2420291A (en) * 1940-07-22 1947-05-13 Nat Standard Co Electrodepositing copper upon steel wire
US2490700A (en) * 1943-08-24 1949-12-06 John S Nachtman Production of alloy coating on base metal material
US2546447A (en) * 1945-05-15 1951-03-27 American Steel & Wire Co Art of drawing fine steel wire
US2689399A (en) * 1950-12-05 1954-09-21 Western Electric Co Plated article and method of making it
US3031068A (en) * 1954-07-21 1962-04-24 Ajax Mfg Co Wire lubricating device
US3210843A (en) * 1959-10-06 1965-10-12 Seul Vincens Method of influencing the surface profile of solid elements, more especially of surface-improved or plated metal strips or sheets
US3197861A (en) * 1960-06-01 1965-08-03 Continental Can Co Production of non-porous vacuum metallized coatings on strip material
US3187413A (en) * 1961-03-02 1965-06-08 G M Lab Inc Process of manufacturing servo motor rotors
US3475813A (en) * 1966-12-28 1969-11-04 Combustion Eng Welding process involving post weld formation of molten pool
FR2389691A1 (en) * 1977-05-06 1978-12-01 Kabmatik Ab
US4178784A (en) * 1977-05-06 1979-12-18 Kabmatik Ab Method for removing plating residues from a plated wire
US4436560A (en) 1982-01-25 1984-03-13 Kabushiki Kaisha Toyota Chuo Kenkyusho Process for manufacturing boride dispersion copper alloys
EP0179517A1 (en) * 1984-10-23 1986-04-30 N.V. Bekaert S.A. Ferrous substrate with rubber adherent metal coating and method of making the same
AU580100B2 (en) * 1984-10-23 1988-12-22 N.V. Bekaert S.A. Ferrous substrate with rubber adherent metal coating and method of making the same
US5087300A (en) * 1989-09-01 1992-02-11 Fujikura Ltd. Method for manufacturing high-conductivity copper-clad steel trolley wire
US20090155620A1 (en) * 2006-03-08 2009-06-18 Kabushiki Kaisha Bridgestone Brass-plated steel wire for reinforcing rubber articles and method for manufacturing the same
US8202626B2 (en) * 2006-03-08 2012-06-19 Kabushiki Kaisha Bridgestone Brass-plated steel wire for reinforcing rubber articles and method for manufacturing the same

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