US2307243A - Drawing be-containing alloys - Google Patents

Drawing be-containing alloys Download PDF

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US2307243A
US2307243A US370357A US37035740A US2307243A US 2307243 A US2307243 A US 2307243A US 370357 A US370357 A US 370357A US 37035740 A US37035740 A US 37035740A US 2307243 A US2307243 A US 2307243A
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film
alloys
cadmium
alloy
thickness
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US370357A
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George H Slagle
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Beryllium Corp
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Beryllium Corp
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    • CCHEMISTRY; METALLURGY
    • C10PETROLEUM, GAS OR COKE INDUSTRIES; TECHNICAL GASES CONTAINING CARBON MONOXIDE; FUELS; LUBRICANTS; PEAT
    • C10MLUBRICATING COMPOSITIONS; USE OF CHEMICAL SUBSTANCES EITHER ALONE OR AS LUBRICATING INGREDIENTS IN A LUBRICATING COMPOSITION
    • C10M7/00Solid or semi-solid compositions essentially based on lubricating components other than mineral lubricating oils or fatty oils and their use as lubricants; Use as lubricants of single solid or semi-solid substances
    • CCHEMISTRY; METALLURGY
    • C10PETROLEUM, GAS OR COKE INDUSTRIES; TECHNICAL GASES CONTAINING CARBON MONOXIDE; FUELS; LUBRICANTS; PEAT
    • C10MLUBRICATING COMPOSITIONS; USE OF CHEMICAL SUBSTANCES EITHER ALONE OR AS LUBRICATING INGREDIENTS IN A LUBRICATING COMPOSITION
    • C10M2201/00Inorganic compounds or elements as ingredients in lubricant compositions
    • C10M2201/04Elements
    • C10M2201/05Metals; Alloys
    • CCHEMISTRY; METALLURGY
    • C10PETROLEUM, GAS OR COKE INDUSTRIES; TECHNICAL GASES CONTAINING CARBON MONOXIDE; FUELS; LUBRICANTS; PEAT
    • C10NINDEXING SCHEME ASSOCIATED WITH SUBCLASS C10M RELATING TO LUBRICATING COMPOSITIONS
    • C10N2040/00Specified use or application for which the lubricating composition is intended
    • C10N2040/20Metal working
    • C10N2040/24Metal working without essential removal of material, e.g. forming, gorging, drawing, pressing, stamping, rolling or extruding; Punching metal
    • CCHEMISTRY; METALLURGY
    • C10PETROLEUM, GAS OR COKE INDUSTRIES; TECHNICAL GASES CONTAINING CARBON MONOXIDE; FUELS; LUBRICANTS; PEAT
    • C10NINDEXING SCHEME ASSOCIATED WITH SUBCLASS C10M RELATING TO LUBRICATING COMPOSITIONS
    • C10N2040/00Specified use or application for which the lubricating composition is intended
    • C10N2040/20Metal working
    • C10N2040/241Manufacturing joint-less pipes
    • CCHEMISTRY; METALLURGY
    • C10PETROLEUM, GAS OR COKE INDUSTRIES; TECHNICAL GASES CONTAINING CARBON MONOXIDE; FUELS; LUBRICANTS; PEAT
    • C10NINDEXING SCHEME ASSOCIATED WITH SUBCLASS C10M RELATING TO LUBRICATING COMPOSITIONS
    • C10N2040/00Specified use or application for which the lubricating composition is intended
    • C10N2040/20Metal working
    • C10N2040/242Hot working
    • CCHEMISTRY; METALLURGY
    • C10PETROLEUM, GAS OR COKE INDUSTRIES; TECHNICAL GASES CONTAINING CARBON MONOXIDE; FUELS; LUBRICANTS; PEAT
    • C10NINDEXING SCHEME ASSOCIATED WITH SUBCLASS C10M RELATING TO LUBRICATING COMPOSITIONS
    • C10N2040/00Specified use or application for which the lubricating composition is intended
    • C10N2040/20Metal working
    • C10N2040/243Cold working
    • CCHEMISTRY; METALLURGY
    • C10PETROLEUM, GAS OR COKE INDUSTRIES; TECHNICAL GASES CONTAINING CARBON MONOXIDE; FUELS; LUBRICANTS; PEAT
    • C10NINDEXING SCHEME ASSOCIATED WITH SUBCLASS C10M RELATING TO LUBRICATING COMPOSITIONS
    • C10N2040/00Specified use or application for which the lubricating composition is intended
    • C10N2040/20Metal working
    • C10N2040/244Metal working of specific metals
    • CCHEMISTRY; METALLURGY
    • C10PETROLEUM, GAS OR COKE INDUSTRIES; TECHNICAL GASES CONTAINING CARBON MONOXIDE; FUELS; LUBRICANTS; PEAT
    • C10NINDEXING SCHEME ASSOCIATED WITH SUBCLASS C10M RELATING TO LUBRICATING COMPOSITIONS
    • C10N2040/00Specified use or application for which the lubricating composition is intended
    • C10N2040/20Metal working
    • C10N2040/244Metal working of specific metals
    • C10N2040/245Soft metals, e.g. aluminum
    • CCHEMISTRY; METALLURGY
    • C10PETROLEUM, GAS OR COKE INDUSTRIES; TECHNICAL GASES CONTAINING CARBON MONOXIDE; FUELS; LUBRICANTS; PEAT
    • C10NINDEXING SCHEME ASSOCIATED WITH SUBCLASS C10M RELATING TO LUBRICATING COMPOSITIONS
    • C10N2040/00Specified use or application for which the lubricating composition is intended
    • C10N2040/20Metal working
    • C10N2040/244Metal working of specific metals
    • C10N2040/246Iron or steel
    • CCHEMISTRY; METALLURGY
    • C10PETROLEUM, GAS OR COKE INDUSTRIES; TECHNICAL GASES CONTAINING CARBON MONOXIDE; FUELS; LUBRICANTS; PEAT
    • C10NINDEXING SCHEME ASSOCIATED WITH SUBCLASS C10M RELATING TO LUBRICATING COMPOSITIONS
    • C10N2040/00Specified use or application for which the lubricating composition is intended
    • C10N2040/20Metal working
    • C10N2040/244Metal working of specific metals
    • C10N2040/247Stainless steel
    • CCHEMISTRY; METALLURGY
    • C10PETROLEUM, GAS OR COKE INDUSTRIES; TECHNICAL GASES CONTAINING CARBON MONOXIDE; FUELS; LUBRICANTS; PEAT
    • C10NINDEXING SCHEME ASSOCIATED WITH SUBCLASS C10M RELATING TO LUBRICATING COMPOSITIONS
    • C10N2050/00Form in which the lubricant is applied to the material being lubricated
    • C10N2050/08Solids
    • CCHEMISTRY; METALLURGY
    • C10PETROLEUM, GAS OR COKE INDUSTRIES; TECHNICAL GASES CONTAINING CARBON MONOXIDE; FUELS; LUBRICANTS; PEAT
    • C10NINDEXING SCHEME ASSOCIATED WITH SUBCLASS C10M RELATING TO LUBRICATING COMPOSITIONS
    • C10N2050/00Form in which the lubricant is applied to the material being lubricated
    • C10N2050/10Semi-solids; greasy
    • CCHEMISTRY; METALLURGY
    • C10PETROLEUM, GAS OR COKE INDUSTRIES; TECHNICAL GASES CONTAINING CARBON MONOXIDE; FUELS; LUBRICANTS; PEAT
    • C10NINDEXING SCHEME ASSOCIATED WITH SUBCLASS C10M RELATING TO LUBRICATING COMPOSITIONS
    • C10N2080/00Special pretreatment of the material to be lubricated, e.g. phosphatising or chromatising of a metal

Definitions

  • Thealloys commonly contain from .10-4.0% beryllium with or without small percentages of other associated alloying elements enhancing the precipitation hardening properties of the Be or the electrical and physical properties of the beryllium-containing alloy.
  • Another object is to facilitate the production of wire, rod and tubular articles from said alloys. Still another object is toimprove the drawing properties of said alloys. Other objects and advantages will be apparent as the invention is more fully hereinafter disclosed.
  • the thickness of the metallic lubricating film provided on the Be-contaim'ng alloys in accordance with the present invention may vary widely without essential departure therefrom, as one skilled in the art will perceive, depending upon the specific metallic lubricant employed and upon the specific alloy being drawn. In general the thickness of the film should be no more than is required to provide the desired lubrication initially, and an extension of the film over the entire elongated length of the alloy subsequently to drawing. Film thicknesses sufficient to provide a drawing sheath for the alloy however are not within the scope of the present invention.
  • a metallic lubricating film comprised of cadmium in the drawing of copperberyllium alloys containing from .104.0% beryllium will be described.
  • a cadmium film ranging from a minimum thickness of about .00001 inch to a maximum of about .0002 inch is a satisfactory metallic lubricating film in the drawing of copper-beryllium alloys.
  • the thickness of the cadmium film provided may vary within this thickness range with respect to the extent of elongation to be applied to the alloy in one or more drawing passes.
  • a thickness of about .00001 inch is sufllcient to provide lubrication of most Cu.Be alloys during a reduction in area of up to as high as 70%, al-
  • the cadmium film thickness should be no more than is necessary to provide surface lubrication over the entire extended length of the alloy being drawn. Accordingly with any given degree of elongation per pass there is a minimum initial film thickness to accomplish this result. Any film thickness over this minimum film thickness is undesired for the purpose of the present invention, although cadmium film thicknesses up to .0002 inch may generally be employed without deleterious results particularly in the larger sized rods and wires.
  • the alloy is subjected to a plurality of separate drawing passes each pass reducing the crosssectional area a determined percent, the total number of said separate passes being calculated to accomplish a determined total percent reduction in area before the work hardening characteristics of the alloy are increased to' an extent inhibiting further cold mechanical deformation.
  • the cadmium film thickness must be at least sufilcient to provide for an extension of the metallic lubricating film cover the total extended length obtained in the plurality of drawing passes.
  • a cadmium film thickness not in excess of about .0002 is about the maximum permissible lubricating thickness on the surface of any copper-beryllium alloy capable of being subjected to cold mechanical deformation by drawing thesame through a die. Thicknesses in excess of'this thickness tend to strip off and to clog up the die opening.
  • a cadmium film thickness of about .0001 inch is about the most satisfactory thickness to apply generally to all copper-beryllium alloys containing beryllium within the range specified to provide sufilcient metallic lubricant for 'a total reduction in area in a plurality of drawing operations of between 40 to
  • the copper-beryllium alloy at the conclusion of the hot working operation and when at a rod diameter of about .750 inch is first subjected to a high temperature heating followed by a rapid cooling operation heretofore customarily applied thereto to condition the alloy for cold mechanical treatment.
  • the surface of the alloy then is thoroughly cleaned of surface scale and oxides and the cleaned metal surface then is coated with an adherent film'of cadmium to a thickness not in excess of about .0002 inch.
  • This cadmium film coating may be applied in a plurality of ways without essential departure from the present invention.
  • Film coatings obtained by immersion or deposition plating are preferred.
  • Film coatings obtained by electro-deposition are generally satisfactory for the purposes of the present invention where the current densities employed are sufllcient to produce the desired film adherence.
  • Film thicknesses obtained by dipping in a molten metal bath when accompanied by partial surface alloying of the cadmium with the copper appear equally as effective as those obtained by immersion or deposition plating.
  • the subsequent cold drawing of the alloy is accomplished in a manner heretofore well known in the art, with the advantage that by the use of the metallic lubricant the copper-beryllium alloys may be drawn at greater speed rates through the die and in considerably greater quantities than heretoi'ore possible and moreover can be given considerably larger percent reductions in area before the work hardening effects require annealing before further cold reductions can be applied.
  • copperberyllium alloys containing about 2% Be ordinarily require about eight (8) anneals during reduction of the same from a size approximating .750 inch to a size approximating .032 inch.
  • anneals On surfacing the alloy with cadmium 'to a film thickness not in excess of about .0002 inch but preferabhr to a film thickness approximating .0001 inch, I have found that only about anneals are necessary and that I can cold reduce the alloy between 40% and 65% reduction in area in a plurality of separate drawing operations between each anneal.
  • a metallic lubricant and at drawing speeds as high as about 156 feet per minute up to 300 pounds of the wire may be drawn through the die without deleterious eflect upon the die size.
  • the advantage of the present invention is more marked in multiple die drawing of Cu.Be alloys. For example, considerable difilculty heretofore has been experienced in the multiple die drawing of Cu.Be alloys of the smaller sizes where higher drawing speeds are desired of around 500 feet per minute. Ordinarily without the metallic lubricant of the present invention only about 1 to 2 pounds of a Cu.Be alloy containing about 2% Be can be drawn before one or more of the dies is deleteriously affected.
  • the film thickness employed in the drawing of these alloys is the same as that found most suitable for the higher Be content copper alloys.
  • Nickel-beryllium alloys for example, are exceedingly difilcult to draw commercially due to excessive strain on the draw head and very serious die wear.
  • the drawing of these alloys is materially simplified and rendered commercially practical.
  • the method of eliminating excessive die wear and drawhead strain in the cold drawing of wire comprised of an alloy of copper containing from .10-4.0% Be which comprises surfacing the wire prior to drawing with a relatively thin film of a metallic lubricant consisting of cadmium, the thickness of said film being not in excess of about .0002 inch.

Description

Patented Jan. 5, 1943 UNITED STATES PATENT OFFICE naawmc BE-OONTAINING armors George H. Slagle, Temple, Pa., assignorto The Beryllium Corporation, Temple, Pm, a corporation of Delaware No Drawing. Application December 16, 1940,
Serial No. 370,351
2 Claims. (Cl- 20521) tubes from Be-containing alloys of one of the metals of the group containing Cu, Ni, Fe and Co. Thealloys commonly contain from .10-4.0% beryllium with or without small percentages of other associated alloying elements enhancing the precipitation hardening properties of the Be or the electrical and physical properties of the beryllium-containing alloy.
Another object is to facilitate the production of wire, rod and tubular articles from said alloys. Still another object is toimprove the drawing properties of said alloys. Other objects and advantages will be apparent as the invention is more fully hereinafter disclosed.
In accordance with these objects, I have discovered that the excessive die wear ordinarily encountered in the drawing of the said alloys and occasioned either by the presence of metal oxide or of berryllide compounds on the surface of said alloys is efiectively eliminated by coating the alloy surface with a relatively thin film of a relatively soft metallic lubricant consisting of one of the group of metals Cd, Ag, Sn, Zn and Pb.
The thickness of the metallic lubricating film provided on the Be-contaim'ng alloys in accordance with the present invention may vary widely without essential departure therefrom, as one skilled in the art will perceive, depending upon the specific metallic lubricant employed and upon the specific alloy being drawn. In general the thickness of the film should be no more than is required to provide the desired lubrication initially, and an extension of the film over the entire elongated length of the alloy subsequently to drawing. Film thicknesses sufficient to provide a drawing sheath for the alloy however are not within the scope of the present invention.
As one specific embodiment of the present invention, but not as a limitation theerof, the adaptation of the same to a metallic lubricating film comprised of cadmium in the drawing of copperberyllium alloys containing from .104.0% beryllium will be described. I have found that for the purposes of the present invention a cadmium film ranging from a minimum thickness of about .00001 inch to a maximum of about .0002 inch is a satisfactory metallic lubricating film in the drawing of copper-beryllium alloys. In general the thickness of the cadmium film provided may vary within this thickness range with respect to the extent of elongation to be applied to the alloy in one or more drawing passes. In general, a thickness of about .00001 inch is sufllcient to provide lubrication of most Cu.Be alloys during a reduction in area of up to as high as 70%, al-
though preferably the total reduction in area would not exceed about 50%.
As hereinabove indicated, the cadmium film thickness should be no more than is necessary to provide surface lubrication over the entire extended length of the alloy being drawn. Accordingly with any given degree of elongation per pass there is a minimum initial film thickness to accomplish this result. Any film thickness over this minimum film thickness is undesired for the purpose of the present invention, although cadmium film thicknesses up to .0002 inch may generally be employed without deleterious results particularly in the larger sized rods and wires. In the drawing of copper-beryllium alloys, however, the alloy is subjected to a plurality of separate drawing passes each pass reducing the crosssectional area a determined percent, the total number of said separate passes being calculated to accomplish a determined total percent reduction in area before the work hardening characteristics of the alloy are increased to' an extent inhibiting further cold mechanical deformation. Under these conditions, therefore, the cadmium film thickness must be at least sufilcient to provide for an extension of the metallic lubricating film cover the total extended length obtained in the plurality of drawing passes.
I have found that a cadmium film thickness not in excess of about .0002 is about the maximum permissible lubricating thickness on the surface of any copper-beryllium alloy capable of being subjected to cold mechanical deformation by drawing thesame through a die. Thicknesses in excess of'this thickness tend to strip off and to clog up the die opening.
I have found that a cadmium film thickness of about .0001 inch is about the most satisfactory thickness to apply generally to all copper-beryllium alloys containing beryllium within the range specified to provide sufilcient metallic lubricant for 'a total reduction in area in a plurality of drawing operations of between 40 to In the practice of the present invention, the copper-beryllium alloy at the conclusion of the hot working operation and when at a rod diameter of about .750 inch is first subjected to a high temperature heating followed by a rapid cooling operation heretofore customarily applied thereto to condition the alloy for cold mechanical treatment. The surface of the alloy then is thoroughly cleaned of surface scale and oxides and the cleaned metal surface then is coated with an adherent film'of cadmium to a thickness not in excess of about .0002 inch.
This cadmium film coating may be applied in a plurality of ways without essential departure from the present invention. The more firmly adherent the film to the surface of the alloy the better the film is for the purposes of the present invention. Film coatings obtained by immersion or deposition plating are preferred. Film coatings obtained by electro-deposition, however, are generally satisfactory for the purposes of the present invention where the current densities employed are sufllcient to produce the desired film adherence. Film thicknesses obtained by dipping in a molten metal bath when accompanied by partial surface alloying of the cadmium with the copper appear equally as effective as those obtained by immersion or deposition plating.
Following the surfacing of the alloy with the cadmium film to the desired thickness the subsequent cold drawing of the alloy is accomplished in a manner heretofore well known in the art, with the advantage that by the use of the metallic lubricant the copper-beryllium alloys may be drawn at greater speed rates through the die and in considerably greater quantities than heretoi'ore possible and moreover can be given considerably larger percent reductions in area before the work hardening effects require annealing before further cold reductions can be applied.
As an example of this improvement, copperberyllium alloys containing about 2% Be ordinarily require about eight (8) anneals during reduction of the same from a size approximating .750 inch to a size approximating .032 inch. On surfacing the alloy with cadmium 'to a film thickness not in excess of about .0002 inch but preferabhr to a film thickness approximating .0001 inch, I have found that only about anneals are necessary and that I can cold reduce the alloy between 40% and 65% reduction in area in a plurality of separate drawing operations between each anneal.
As an example of the efflciency of the cadmium lubricant in the drawing of copper-beryllium alloys, wire comprised of copper-beryllium and containing Be about 2% when reduced in diameter from .155 inch to .125 inch, a reduction in area of about 35%, without such a metallic lubricant will destroy the die size of a tungsten carbide die before more than 10 pounds of the wire has been drawn therethrough. With a metallic lubricant and at drawing speeds as high as about 156 feet per minute up to 300 pounds of the wire may be drawn through the die without deleterious eflect upon the die size.
The advantage of the present invention is more marked in multiple die drawing of Cu.Be alloys. For example, considerable difilculty heretofore has been experienced in the multiple die drawing of Cu.Be alloys of the smaller sizes where higher drawing speeds are desired of around 500 feet per minute. Ordinarily without the metallic lubricant of the present invention only about 1 to 2 pounds of a Cu.Be alloy containing about 2% Be can be drawn before one or more of the dies is deleteriously affected. By the practice of the present invention and with an initial cadmium thickness of about .0001 inch, for example, between 300 to 500 pounds ofwire may be drawn, for example, from a wire size of about .032 inch to a wire size of about .016 inch through a plurality of dies each giving the wire about a 25% reduction in area, at drawing speeds as high as 500 feet per minute without deleteriously affecting the plurality of die sizes.
The two examples above given indicate the marked economic advantage gained by the practice of the present invention. When diamond dies are employed the advantage of the present inventionis still more marked, for example, under the same circumstances given in the paragraph above over 1000 pounds of the wire may be drawn as contrasted to less than 200 pounds without the metallic lubricant.
The above noted drawing results are characteristic of those obtainable with all copper-beryllium alloys containing beryllium .10-4.0% by the practice of the present invention. The lower beryllium content alloys appear to draw more easily than the higher beryllium content alloys,
eating film described.
In general, the film thickness employed in the drawing of these alloys is the same as that found most suitable for the higher Be content copper alloys. Nickel-beryllium alloys, for example, are exceedingly difilcult to draw commercially due to excessive strain on the draw head and very serious die wear. By the practice of the present invention the drawing of these alloys is materially simplified and rendered commercially practical.
Whereas, hereinabove I have described the present invention giving the metal cadmium as a specific example of the metallic lubricant employed, it is believed apparent that other metals may be employed for such purpose without essential departure therefrom such as, for example, tin, lead, zinc, silver and copper, which for the purpose of the present invention are to be considered substantial equivalents for cadmium.
The precise film thicknesses of these metals eifective as lubricating film will vary from that thickness hereinabove indicated as being proper for cadmium as one skilled in the art will perceive. The lubricating properties of tin appear to be closely approximate that of cadmium and film thicknesses of tin approximating that hereinabove given for cadmium are equally as good for the purposes of the present invention.
Having hereinabove broadly and specifically described the present invention and given one specific embodiment of the same, it is believed apparent that many modifications may be made therein without essential departure therefrom and all such are contemplated as may fall within the scope of the following claims.
What I claim is:
1. In the cold drawing of copper-beryllium alloys containing from .10-4.0% Be from rod to wire size, the improvement which comprises surfacing the rod with an adherent relatively thin coating of cadmium not exceeding about .0002 inch in thickness.
2. The method of eliminating excessive die wear and drawhead strain in the cold drawing of wire comprised of an alloy of copper containing from .10-4.0% Be which comprises surfacing the wire prior to drawing with a relatively thin film of a metallic lubricant consisting of cadmium, the thickness of said film being not in excess of about .0002 inch.
GEORGE E. SLAGLE.
US370357A 1940-12-16 1940-12-16 Drawing be-containing alloys Expired - Lifetime US2307243A (en)

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Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2653494A (en) * 1946-12-24 1953-09-29 Edward C Creutz Method of forging metals
US2872343A (en) * 1946-03-14 1959-02-03 Lowell D Eubank Method of protectively coating uranium
US2978799A (en) * 1954-05-19 1961-04-11 Benteler Werke Ag Internally and externally coppercoated steel tubes and their manufacture

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2872343A (en) * 1946-03-14 1959-02-03 Lowell D Eubank Method of protectively coating uranium
US2653494A (en) * 1946-12-24 1953-09-29 Edward C Creutz Method of forging metals
US2978799A (en) * 1954-05-19 1961-04-11 Benteler Werke Ag Internally and externally coppercoated steel tubes and their manufacture

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