US2156331A - Method of coating steel strips - Google Patents

Method of coating steel strips Download PDF

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US2156331A
US2156331A US140999A US14099937A US2156331A US 2156331 A US2156331 A US 2156331A US 140999 A US140999 A US 140999A US 14099937 A US14099937 A US 14099937A US 2156331 A US2156331 A US 2156331A
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metal
strip
copper
bath
molten
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US140999A
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Thomas B Chace
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Clad Metals Industries Inc
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    • CCHEMISTRY; METALLURGY
    • C23COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23CCOATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C2/00Hot-dipping or immersion processes for applying the coating material in the molten state without affecting the shape; Apparatus therefor
    • C23C2/34Hot-dipping or immersion processes for applying the coating material in the molten state without affecting the shape; Apparatus therefor characterised by the shape of the material to be treated
    • C23C2/36Elongated material
    • C23C2/38Wires; Tubes
    • CCHEMISTRY; METALLURGY
    • C23COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23CCOATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C2/00Hot-dipping or immersion processes for applying the coating material in the molten state without affecting the shape; Apparatus therefor
    • C23C2/04Hot-dipping or immersion processes for applying the coating material in the molten state without affecting the shape; Apparatus therefor characterised by the coating material

Definitions

  • My invention relates', generally, to the art of cladding metals and it has particular relation to the cladding of strips or sheets of base metal as a continuous process to make a composite strip f 5 or sheet product having a corrosion resisting surface.
  • the object of my invention is to provide a process for making a composite strip having a corrosion resisting 5 surface formed by cuprous metal that may bev simply and eiiiciently performed and which will provide a relatively inexpensive product.
  • Another object of my invention is to apply a cuprous metal layer around the entire surface 10 of a base metal strip or sheet that will be integrally bonded thereto and have a relatively smooth finished surface.
  • a further object of my invention is to apply cuprous cladding metal to steel strips or sheets by l5 passing them through molten uprous cladding metal at suchspeed that very ittle of the iron in the strips or sheets dissolves out into the molten cladding metal or is present in the cladding metal bonded to the strips orV sheets.
  • a still further object of my invention is to prevent oxidation of a 'metal' strip while it is being passed into and out of baths of molten cladding metal.
  • Another object of my invention is to preheat a 26 base 'metal strip'to welding temperature before passing it into a bathof molten cuprous metal.
  • Still another object of my invention is to successively pass a base metal strip through a plurality of molten cuprous metal baths maintained 80 at succeedingly lower temperatures while excluding the atmosphere from contact with the strip .as it is being passed into andout of the molten metal baths.
  • a further object of my invention is to pass the 35 composite strip between finishing rolls to provide a smooth nished surface and increase the density of the metal forming the coating.
  • Figure 1 illustrates, diagrammatically, how the composite strip may be formed by passing it through a plurality of cuprous metal baths maintained atcertain predetermined temperatures
  • Figure 2 illustrates how the composite strip may be passed between iinishing rolls after the cladding process has been completed
  • Figure 3 is a fragmentary sectional view of the composite strip showing. at an exaggerated scale, the diil'erent layers of clad metal on the base metal backing strip.
  • the reference character I designates a steel strip or base metal strip that is first passed into a bath I I of molten flux, such as glass or borax or the like, and then it passes as shown at I2 into a bath I3 of molten cuprous metal such as a copper-nickel alloy, a portion of which is integrally bonded to the base metal strip. As shown at Il, the strip then next is passed through a second bath I of 'molten cuprous metal that is preferably formed of a silicon-copper alloy.
  • the composite strip, as shown at I6, then may be wound on a suitable reel or worked as will be presently set forth.V It will be observed that the base metal strip or the composite metal strip is not exposed to the atmos-.
  • Suitable rollers I9 are provided, as illustrated, for guiding the strip through the various flux and metal baths. .
  • , 22 and 23, formed of suitable refractory material such as fire brick, carborundum and the like, may be employed for holding thev several baths and separating them.V These walls may have metal reenforcing or backing as is well known in furnace and foundry practice.
  • nickel greatly increases the weldability of copper to steel and at the same time it raises the melting point of copper.
  • These two properties are of great importance in the production of the composite strip as disclosed herein. For example, a 5% nickelcopper alloy will weld to properly cleaned and fluxed steel surfaces almost instantaneously at a temperature slightly above the melting point of the nickel-copper alloy.
  • the strip I0 may be rapidly pulled through the molten cuprous metal bath I3 at a high rate of speed and, consequently, the amount of iron that is dissolved into the bath I3 is minimized, as is likewise the amount of iron held in the coating metal on solidication.
  • the base metal strip I0 may be preheated before entering the slag bath or it may be preheated by contact with the bath.
  • the bath Il of flux is heated to approximately 2200" F., so that the base metal strip will be preheated to the desired temperature.
  • This preheating temperature is employed if the cuprous metal bath I3 is composed of 80% copper and 20% nickel. Such an alloy melts at about 21'70o F., so that the iiux bath I I is maintained. at approximately this temperature to properly preheat the base metal strip. 4
  • the copper-nickel alloy readily welds to the steel backing strip, it is very sensitive to oxidizing atmospheres and it must be prevented from coming in contact with them. Furthermore, the surface that is obtained on solidication of the copper-nickel alloy is not as smooth as is desired. In order to prevent oxidation ofw amounts of manganese, tin or zinc to make it more workable and to hold the melting temperature down below that of the copper-nickel alloy. By passing the strip from the bath I3 into the bath I5 underneath the layer of ilux I'I-Il, oxidation of the copper-nickel layer is prevented and the surface thereof is well adapted for receiving the silicon-copper layer.
  • the silicon-copper alloy is difficult to weld directly to steel but it bonds readily to a copper-nickel alloy.
  • the time required to bond the layer of silicon-copper to the layer of copper-nickel alloy is reduced to a minimum. Since nickel increases the melting temperature of a copper alloy while silicon decreases it, the proper temperature diiferential may be provided for the baths I3 and I5 to effect the desired coating of the base metal strip with a composite layer of cuprous metal.
  • the metal baths and their slag coverings may be kept hot by electric heat such as an arc furnace.
  • the composite strip I6 may be passed between one or more pairs of inishing rolls 24 in order to further smooth out the surfaces and to improve the density of the cladding'metal.
  • the resulting composite strip I6 is shownat an enlarged scale. It will be noted that it comprises the steel backing portion 21 having integrally bonded thereto layers 28 of the copper-nickel alloy and then integrally bonded to these layers are the outer layers Z9 of the silicon-copper alloy.
  • This composite strip or sheet material has excellent corrosion resisting qualities and at the same time the surface is suciently hard so that it cannot be readily scratched through and damaged to expose the inner portion 21 of steel backing material.
  • slag may consist of a mixture of borax and boric acid with or without the addition of molten glass. It may consist of melted limestone and silica, as in the case of smelting of iron, or any other glass-like slag suitable for the purpose.
  • the purpose of such slag is, first, to exclude the oxygen of the air and, second, to take up or dis-v solve metallic oxides or salts or like metallic impurities.
  • rollers shown may be refractory bodies. Some of these rollers may be free bodies or they may have fixed axes.
  • the strip is preferably passed entirely under the slag blanket, this is not always necessary, since the slag is made sticky and viscous enough to protect the surface oi' the hot strip if it be runv above the surface of the bath or blanket.
  • Method of making a composite metal strip which comprises: preheating a base metal strip to approximately the same temperature as the first bath through which it is passed, passing the metal strip through a copper-nickel bath maintainedslightly above its melting temperature to cause a layer of cuprous metal to 'be integrally bonded thereto, passing the strip through a silicon-copper bath maintained slightly above its melting temperature to cause a second layer of cuprous metal to be integrally bonded to the first layer Without substantially melting the same, and excluding the atmosphere from the strip While it is being passed into and out of the molten metal baths.
  • Method of making a composite metal strip which comprises: preheating a base metal strip to approximately the same temperature as the first bath through which it is passed, passing the metal strip through a copper-nickel bath maintained slightly above its melting temperature to cause a layer of cuprous metal to be integrally bonded thereto, passing the strip through a silicon-copper bath maintained slightly above its melting temperature to cause a second layer of cuprous metalto be integrally bonded to the ilrst layer Without substantially melting the same, excluding lthe atmosphere from the'strip while it is being passed into and out of the molten metal strip between finishing rolls.
  • Method of making a composite ⁇ metal strip which comprises: .passing a base metal strip through a molten flux bath maintained at approximately 2200 F., passing the metal strip from the flux bath into a molten metal bath composed of about 80% copper and 20% nickel maintained at a temperature of about 2200 F. to integrally bond a layer of the copper-nickel alloy thereto, and passing the metal strip back into the iiux bath and then into a molten metal bath composed of about 1V2% silicon and 981/2% copper maintained at a temperature of about 1900 F. to cause a layer of the silicon-copper alloy to be inlgrally bonded to the layer of copper-nickel 4.
  • Method ot making a composite metal strip which comprises: passing a base metal strip through a molten'iiux bath maintained at approximately 2200 F., passing the metal strip from the flux bath into a molten metal bath composed of about 80% copper and 20% nickel maintained at a temperature of about 2200 F. to integrally bond a layer of the copper-nickel alloy thereto, passing. the metal strip back into the iiux bath and then into a molten metal bath composed of about 11/2% silicon and 981/2% copper maintained at a temperature of about 1900 F. to cause a layer of the silicon-copper alloy to be integrally bonded to the layer of copper-nickel alloy, and passing the resulting composite metal strip between nnishing rolls.

Description

May 2, 1939. T. B. cHAcE METHOD OF COATING STEEL STRIPS Filed May 5., 1957 nNnNmql SQ@ Patented May 2, 1939 UMTED STATES METHOD or coA'rlNG srasns'rarrs 'rhmu B. cme, wmnetka, 111., assimito clad.
Metals Industries Inc.,
tion of Illinois'` Chicago, Ill.; V'a corpora- Application May s, 1931, serial No. 140,999
4 Claims.
My invention relates', generally, to the art of cladding metals and it has particular relation to the cladding of strips or sheets of base metal as a continuous process to make a composite strip f 5 or sheet product having a corrosion resisting surface.
It is well known to employ tin, lead, and zinc, or alloys of the same, for galvanizing steel sheets and strips. The products obtained from this process are not all that is desired, particularly for -the more severe corroding conditions to which metals are often subjected. One reason for failure of these products is the fact that there is no real weld between the coating metal and the base metal. The coating metal cracks or peels ofi in places, particularly if there is any bending or forming after coating. Furthermore, this type of coating metal is comparatively soft and can be eadly bruised or scratched through to the base metal, thereby leaving exposed spots that readily corrode. There are many applications for corrosion resisting sheets or strips. These include metal culverts, roofing sheets, and the like, which require that the metal be coated on both surfaces and edges. It is desirable that the coating metal be more resistant to corrosion than those now available, while still remaining in a similar price range.
By my process, as disclosed herein, it is possible to coat steel sheets and strips with copper or high copper alloys and to secure an inseparable bond between the base and coating metals which will not crack or peel during any subsequent bending, forming, or rolling. The' resulting composite strip having its surface formed by copper or copper base alloys, which are much harder than the tin, zinc and lead alloys, will be corrosion-resisting and it is not possible to scratch through the clad surface as readily as is the case when the softer tin, lead and zinc alloys are used.
In order to weld properly a coating of copper to steel sheet or strip material, a temperature of about 2200 F. for both metals is required and this should be maintained Afor several minutes to sumciently diffuse the two. A t this temperature, and during this length of time, considerable iron dissolves from the strip or sheet metal and it contaminates the molten metal bath and also the copper coating which, on solidiflcation, is 50 found to contain appreciable amounts of free iron that not only embrittles the copper but also decreases its resistance to corrosion. Pure copper does not make as good a coating metal as some of the high copper alloys, such as silicon 55 copper. However, this alloy requires a long period (Cl. ill-70.2)
of soaking to weld to steel, thereby exaggerating the iron pickup in the bath.
Accordingly, the object of my invention, generally stated, is to provide a process for making a composite strip having a corrosion resisting 5 surface formed by cuprous metal that may bev simply and eiiiciently performed and which will provide a relatively inexpensive product.
Another object of my invention is to apply a cuprous metal layer around the entire surface 10 of a base metal strip or sheet that will be integrally bonded thereto and have a relatively smooth finished surface.
A further object of my invention is to apply cuprous cladding metal to steel strips or sheets by l5 passing them through molten uprous cladding metal at suchspeed that very ittle of the iron in the strips or sheets dissolves out into the molten cladding metal or is present in the cladding metal bonded to the strips orV sheets.
A still further object of my invention is to prevent oxidation of a 'metal' strip while it is being passed into and out of baths of molten cladding metal.
Another object of my invention is to preheat a 26 base 'metal strip'to welding temperature before passing it into a bathof molten cuprous metal.
Still another object of my invention is to successively pass a base metal strip through a plurality of molten cuprous metal baths maintained 80 at succeedingly lower temperatures while excluding the atmosphere from contact with the strip .as it is being passed into andout of the molten metal baths. i A further object of my invention is to pass the 35 composite strip between finishing rolls to provide a smooth nished surface and increase the density of the metal forming the coating.
Other objects of my inventionl will, in part, be obvious and in part appear hereinafter.
My invention is disclosed inthe embodiment hereof shown in the accompanying drawing and it comprises the process steps which will be exemplified hereinafter and the scope of the application of which will be indicated in the ap- 45 pended claims. y x
For a. more complete understanding of the nature and scope of my invention, reference may be had to the following detailed description, taken with the accompanying drawing, in 50 in connectionwhich:
Figure 1 illustrates, diagrammatically, how the composite strip may be formed by passing it through a plurality of cuprous metal baths maintained atcertain predetermined temperatures;
Figure 2 illustrates how the composite strip may be passed between iinishing rolls after the cladding process has been completed; and
Figure 3 is a fragmentary sectional view of the composite strip showing. at an exaggerated scale, the diil'erent layers of clad metal on the base metal backing strip.
Referring now particularly to Figure 1 of-the drawing, it will be observed that the reference character I designates a steel strip or base metal strip that is first passed into a bath I I of molten flux, such as glass or borax or the like, and then it passes as shown at I2 into a bath I3 of molten cuprous metal such as a copper-nickel alloy, a portion of which is integrally bonded to the base metal strip. As shown at Il, the strip then next is passed through a second bath I of 'molten cuprous metal that is preferably formed of a silicon-copper alloy. The composite strip, as shown at I6, then may be wound on a suitable reel or worked as will be presently set forth.V It will be observed that the base metal strip or the composite metal strip is not exposed to the atmos-.
phere after it has passed into the bath II oi' molten flux. As shown at I1 and I8, the flux extends over the molten cuprous metal baths I3 and I5, so that the strip is always underneath the flux and contact with atmosphere is prevented. Suitable rollers I9 are provided, as illustrated, for guiding the strip through the various flux and metal baths. . Suitable walls 20, 2|, 22 and 23, formed of suitable refractory material such as fire brick, carborundum and the like, may be employed for holding thev several baths and separating them.V These walls may have metal reenforcing or backing as is well known in furnace and foundry practice.
As pointed out. in my copending applications, Serial No. 6,497, led February 14, 1935, and Serial No. 64,2'80, filed February 17, 1936, nickel greatly increases the weldability of copper to steel and at the same time it raises the melting point of copper. These two properties are of great importance in the production of the composite strip as disclosed herein. For example, a 5% nickelcopper alloy will weld to properly cleaned and fluxed steel surfaces almost instantaneously at a temperature slightly above the melting point of the nickel-copper alloy. Because of this rapid welding action the strip I0 may be rapidly pulled through the molten cuprous metal bath I3 at a high rate of speed and, consequently, the amount of iron that is dissolved into the bath I3 is minimized, as is likewise the amount of iron held in the coating metal on solidication.
It is desirable to have the base metal strip I0 heated to the welding temperature before it is passed through the bath I3. The strip I0 may be preheated before entering the slag bath or it may be preheated by contact with the bath. The bath Il of flux is heated to approximately 2200" F., so that the base metal strip will be preheated to the desired temperature. This preheating temperature is employed if the cuprous metal bath I3 is composed of 80% copper and 20% nickel. Such an alloy melts at about 21'70o F., so that the iiux bath I I is maintained. at approximately this temperature to properly preheat the base metal strip. 4
While the copper-nickel alloy readily welds to the steel backing strip, it is very sensitive to oxidizing atmospheres and it must be prevented from coming in contact with them. Furthermore, the surface that is obtained on solidication of the copper-nickel alloy is not as smooth as is desired. In order to prevent oxidation ofw amounts of manganese, tin or zinc to make it more workable and to hold the melting temperature down below that of the copper-nickel alloy. By passing the strip from the bath I3 into the bath I5 underneath the layer of ilux I'I-Il, oxidation of the copper-nickel layer is prevented and the surface thereof is well adapted for receiving the silicon-copper layer.
As fully described in my copending applications referred to hereinbefore, the silicon-copper alloy is difficult to weld directly to steel but it bonds readily to a copper-nickel alloy. Thus the time required to bond the layer of silicon-copper to the layer of copper-nickel alloy is reduced to a minimum. Since nickel increases the melting temperature of a copper alloy while silicon decreases it, the proper temperature diiferential may be provided for the baths I3 and I5 to effect the desired coating of the base metal strip with a composite layer of cuprous metal. The metal baths and their slag coverings may be kept hot by electric heat such as an arc furnace.
As shown in Figure 2 of the drawing, the composite strip I6 may be passed between one or more pairs of inishing rolls 24 in order to further smooth out the surfaces and to improve the density of the cladding'metal.
In Figure 3 of the drawing the resulting composite strip I6 is shownat an enlarged scale. It will be noted that it comprises the steel backing portion 21 having integrally bonded thereto layers 28 of the copper-nickel alloy and then integrally bonded to these layers are the outer layers Z9 of the silicon-copper alloy. This composite strip or sheet material has excellent corrosion resisting qualities and at the same time the surface is suciently hard so that it cannot be readily scratched through and damaged to expose the inner portion 21 of steel backing material.
While I speak herein of the air excluding blanket II as iiux it is to be noted that this material might more properly be designated as a slag. It may consist of a mixture of borax and boric acid with or without the addition of molten glass. It may consist of melted limestone and silica, as in the case of smelting of iron, or any other glass-like slag suitable for the purpose. The purpose of such slag is, first, to exclude the oxygen of the air and, second, to take up or dis-v solve metallic oxides or salts or like metallic impurities.
Any suitable means for keeping the metal baths hot, such as electric arc heating or resistance heating, may be employed. A gas furnace may also be utilized. The rollers shown may be refractory bodies. Some of these rollers may be free bodies or they may have fixed axes.
While the strip is preferably passed entirely under the slag blanket, this is not always necessary, since the slag is made sticky and viscous enough to protect the surface oi' the hot strip if it be runv above the surface of the bath or blanket.
Since certain changes may be made in the baths, and passing the resulting composite metal foregoing process without departing from the scope of the present invention, it is intended that all matter shown in the accompanying drawing or disclosed hereinbefore shall be interpreted as illustrative and not in a limiting sense.
I claim as my invention: l
1. Method of making a composite metal strip, which comprises: preheating a base metal strip to approximately the same temperature as the first bath through which it is passed, passing the metal strip through a copper-nickel bath maintainedslightly above its melting temperature to cause a layer of cuprous metal to 'be integrally bonded thereto, passing the strip through a silicon-copper bath maintained slightly above its melting temperature to cause a second layer of cuprous metal to be integrally bonded to the first layer Without substantially melting the same, and excluding the atmosphere from the strip While it is being passed into and out of the molten metal baths.
2. Method of making a composite metal strip, which comprises: preheating a base metal strip to approximately the same temperature as the first bath through which it is passed, passing the metal strip through a copper-nickel bath maintained slightly above its melting temperature to cause a layer of cuprous metal to be integrally bonded thereto, passing the strip through a silicon-copper bath maintained slightly above its melting temperature to cause a second layer of cuprous metalto be integrally bonded to the ilrst layer Without substantially melting the same, excluding lthe atmosphere from the'strip while it is being passed into and out of the molten metal strip between finishing rolls.
3. Method of making a composite`metal strip, which comprises: .passing a base metal strip through a molten flux bath maintained at approximately 2200 F., passing the metal strip from the flux bath into a molten metal bath composed of about 80% copper and 20% nickel maintained at a temperature of about 2200 F. to integrally bond a layer of the copper-nickel alloy thereto, and passing the metal strip back into the iiux bath and then into a molten metal bath composed of about 1V2% silicon and 981/2% copper maintained at a temperature of about 1900 F. to cause a layer of the silicon-copper alloy to be inlgrally bonded to the layer of copper-nickel 4. Method ot making a composite metal strip, which comprises: passing a base metal strip through a molten'iiux bath maintained at approximately 2200 F., passing the metal strip from the flux bath into a molten metal bath composed of about 80% copper and 20% nickel maintained at a temperature of about 2200 F. to integrally bond a layer of the copper-nickel alloy thereto, passing. the metal strip back into the iiux bath and then into a molten metal bath composed of about 11/2% silicon and 981/2% copper maintained at a temperature of about 1900 F. to cause a layer of the silicon-copper alloy to be integrally bonded to the layer of copper-nickel alloy, and passing the resulting composite metal strip between nnishing rolls.
THOMAS B'. CHACE.
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Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2428523A (en) * 1942-04-21 1947-10-07 American Rolling Mill Co Apparatus for and method of coating metal strip at high speeds
US2689399A (en) * 1950-12-05 1954-09-21 Western Electric Co Plated article and method of making it
FR2321550A1 (en) * 1975-08-19 1977-03-18 Politechnika Slaska Im Wincent PROCESS FOR OBTAINING COPPER ALLOY COATINGS ON FERROUS ALLOY PARTS
FR2374093A1 (en) * 1976-12-17 1978-07-13 Univ College Cardiff Cuic PROCESS FOR APPLYING AT LEAST ONE COATING LAYER ON A SUBSTRATE
US20020066769A1 (en) * 2000-10-16 2002-06-06 Haynes Gardner S. Self-brazing materials for elevated temperature applications

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2428523A (en) * 1942-04-21 1947-10-07 American Rolling Mill Co Apparatus for and method of coating metal strip at high speeds
US2689399A (en) * 1950-12-05 1954-09-21 Western Electric Co Plated article and method of making it
FR2321550A1 (en) * 1975-08-19 1977-03-18 Politechnika Slaska Im Wincent PROCESS FOR OBTAINING COPPER ALLOY COATINGS ON FERROUS ALLOY PARTS
FR2374093A1 (en) * 1976-12-17 1978-07-13 Univ College Cardiff Cuic PROCESS FOR APPLYING AT LEAST ONE COATING LAYER ON A SUBSTRATE
US20020066769A1 (en) * 2000-10-16 2002-06-06 Haynes Gardner S. Self-brazing materials for elevated temperature applications
US6783870B2 (en) * 2000-10-16 2004-08-31 Engineered Materials Solutions, Inc. Self-brazing materials for elevated temperature applications

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