US2361962A - Method of metal-clading - Google Patents
Method of metal-clading Download PDFInfo
- Publication number
- US2361962A US2361962A US446617A US44661742A US2361962A US 2361962 A US2361962 A US 2361962A US 446617 A US446617 A US 446617A US 44661742 A US44661742 A US 44661742A US 2361962 A US2361962 A US 2361962A
- Authority
- US
- United States
- Prior art keywords
- metal
- coating
- clading
- sprayed
- layer
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
Links
- 238000000034 method Methods 0.000 title description 14
- 239000002184 metal Substances 0.000 description 45
- 229910052751 metal Inorganic materials 0.000 description 45
- 239000011248 coating agent Substances 0.000 description 13
- 238000000576 coating method Methods 0.000 description 13
- 239000010953 base metal Substances 0.000 description 11
- 238000005507 spraying Methods 0.000 description 8
- 229910052782 aluminium Inorganic materials 0.000 description 6
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 6
- 230000004927 fusion Effects 0.000 description 5
- 239000000956 alloy Substances 0.000 description 4
- 229910045601 alloy Inorganic materials 0.000 description 4
- 239000000463 material Substances 0.000 description 4
- 150000002739 metals Chemical class 0.000 description 3
- 238000002844 melting Methods 0.000 description 2
- 230000008018 melting Effects 0.000 description 2
- 239000002245 particle Substances 0.000 description 2
- 230000000704 physical effect Effects 0.000 description 2
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 1
- HCBIBCJNVBAKAB-UHFFFAOYSA-N Procaine hydrochloride Chemical compound Cl.CCN(CC)CCOC(=O)C1=CC=C(N)C=C1 HCBIBCJNVBAKAB-UHFFFAOYSA-N 0.000 description 1
- 229910052799 carbon Inorganic materials 0.000 description 1
- 230000007797 corrosion Effects 0.000 description 1
- 238000005260 corrosion Methods 0.000 description 1
- QFXZANXYUCUTQH-UHFFFAOYSA-N ethynol Chemical group OC#C QFXZANXYUCUTQH-UHFFFAOYSA-N 0.000 description 1
- 239000007789 gas Substances 0.000 description 1
- 230000006698 induction Effects 0.000 description 1
- 239000007788 liquid Substances 0.000 description 1
- 239000002923 metal particle Substances 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000010422 painting Methods 0.000 description 1
- 239000002516 radical scavenger Substances 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
Images
Classifications
-
- C—CHEMISTRY; METALLURGY
- C23—COATING 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
- C23C—COATING 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
- C23C4/00—Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge
- C23C4/18—After-treatment
-
- C—CHEMISTRY; METALLURGY
- C23—COATING 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
- C23C—COATING 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
- C23C26/00—Coating not provided for in groups C23C2/00 - C23C24/00
- C23C26/02—Coating not provided for in groups C23C2/00 - C23C24/00 applying molten material to the substrate
-
- C—CHEMISTRY; METALLURGY
- C23—COATING 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
- C23C—COATING 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
- C23C4/00—Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge
- C23C4/04—Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge characterised by the coating material
- C23C4/06—Metallic material
- C23C4/08—Metallic material containing only metal elements
Definitions
- metal-clad is understood by industry to apply to coating one metal with another in such a manner that the material which forms the clad or coating is in the rolled, wrought or cast form, and it is bonded to the base metal in a metallurgical unin, which is known as a welded fusion.
- Figs. 1 to 4 are reproduced photomicrographs, showing the coarse conglomerate of'of metal A applied to the base metal B, held together by mechanical cohesion, at C in Figs. 1 and 2, whereas in Figs. 3 and 4, the coating is fused together and to the surface of the base metal.
- the method of metal-clading described herein consists of two phases. 'I'he object to be metal clad is rst covered by the metal selected for the purpose by means of metal spraying.
- the preferred method is to apply first the cladmetal by spraying it on to the desired thickness and then coat that with aluminum deposited to form a layer only a few thousandths oi an inch in thickness. Any other suitable deoxidizer can be applied in place of the aluminum if desired.
- the object is preheated and then the sprayed coating is remelted progressively by applicable -means such as the carbon arc, the single or multiple iet oxyacetylene llame, or, whenever the geometry of the object makes it permissible, high frequency induction.
- applicable -means such as the carbon arc, the single or multiple iet oxyacetylene llame, or, whenever the geometry of the object makes it permissible, high frequency induction.
- the remelting must be carried out with a sufiiciently high power imput to permit liquefying the sprayed on metal and causing it to fuse to the base metal without allowing the heat to dwell long enough to cause a metallurgical change in the base metal.
- Remelting the overlay progressively permits retaining the original contour and thickness thereof.
- Metal deposited by means of/metal spraying is only a conglomerate of small particles held together by partial fusion and by mechanical cohesion or the interlocked particles as seen in the reproduced photomicrograph Figs. 1 and 2.
- adhesion of the sprayed on metal to the base metal is likewise purely mechanical.
- the structure of the metal in the Coating A shows the more homogeneous characteristics resulting from the fusion of the conglomerate mass.
- At C' may be seen the result of the fusion of the coating to the surface of the' metal body B', while the characteristics of the metal in the body are not materially changed.
- the building up of the sprayed on overlay another thin coat of aluminum is applied.
- the role l of this secondary overlay is to act as a scavenger or deoxidizer in remelting the partly oxidized conglomerate.
- the aluminum may be applied in several thin layers: the first direct on the base metal, one at about the middle of the desired sprayed on thickness, and nally one over the nal thickness of the sprayed on metal. While aluminum is the preferred substance for deoxidizing, any other metal oi suitable characteristics may be applied.
- a quantity of the metal or alloy which is required to obtain the desired alloy in the converted clad material is procured in finely divided form and is applied by means of a suitable vehicle and it is painted on the completed sprayedon overlay and then it is covered with the final layer of aluminum. In remelting. the ilnely divided metal particles of the added metal or alloy dissolve in the body oi.' the overlay forming the desired composition.
- a method of metal-clading a metal body the steps of applying a clad-metal by spraying it on to the desired thickness, preheating the body below the melting temperature o! any of the metals, and then progressively remelting the clad-metal with a sufllciently high power heat concentration to permit liquefying the sprayed on metal and causing it to fuse to the body without allowing the heat to dwell long enough to cause a metallurgical change in the metal of the body.
- a method of .metal-clading a metal body the steps of applying a clad-metal by spraying it on to the desired thickness, coating it with a thinV layer of deoxidizer, preheating the body below the melting tem-perature of any of the metals, and then progressively remelting the clad-metal with a sufficiently high power heat concentration to permit liquefying the sprayed on metal and causing it to fuse to the body without allowing the heat to dwell long enough to cause a metallurgical change in the metal of the body.
- a method of coating a metal surface with a layer of another metal, said layer having any desired thickness and shape or contour comprising applying said layer in conglomerate form to the desired thickness and shape, then applying concentrated heat progressively in a manner to melt a comparatively small expanse of the layer at a time, with only suiiicient heat to simultaneously melt only a micronlm of the metal surface in contact with said expanse and without causing 9, metallurgical change in the metal below the surface.
- a method of coating a metal surface with a layer of another metal, said layer having any desired thickness and shape or contour comprising applying said layer in conglomerate form to the desired thickness and shape, preheating the combination to a moderate temperature to reduce the heat gradient in the performance of the following step, and then applying concentrated heat progressively in a manner to melt a comparatively small expanse of the layer at a time, with only suiilcient heat to simultaneously melt only a microfilm of the metal surface in contact with said expanse and without causing a metallurgical change in the metal below the surface.
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Physics & Mathematics (AREA)
- Plasma & Fusion (AREA)
- Coating By Spraying Or Casting (AREA)
Description
Nov. 7, 1944. B. RoNAY METHOD OF METAL-CLADING Filed June ll, 1942 `Flel Fm Y4 Lm/MM BELA RONAY nieuwe Nw... 7, 1944 UNITED STATES PATENT OFFICE METBGD F METAL-CIADING Bela Bonay, Annapolis, Md.
Application June 11, 194%, Serial No. 448,617 Claims. (Ci. 117-22) (Granted under the act of March 3, 1883, as amended April 30, 1928; 37d 0. G. 757) This application pertains to a method of metalclading. The purpose of metal-clading is to provide a metal object fabricated of a material having certain physical properties with a fused on coating of another metal whose physical properties may be different from those of the base metal but which, in addition, possesses another property, usually resistance to corrosion to cetain liquids or gases, to a degree which far exceeds that of the base metal in regard to the useful life of the fabricated product.
The term metal-clad is understood by industry to apply to coating one metal with another in such a manner that the material which forms the clad or coating is in the rolled, wrought or cast form, and it is bonded to the base metal in a metallurgical unin, which is known as a welded fusion.
Figs. 1 to 4 are reproduced photomicrographs, showing the coarse conglomerate of'of metal A applied to the base metal B, held together by mechanical cohesion, at C in Figs. 1 and 2, whereas in Figs. 3 and 4, the coating is fused together and to the surface of the base metal.
The method of metal-clading described herein consists of two phases. 'I'he object to be metal clad is rst covered by the metal selected for the purpose by means of metal spraying.
The preferred method is to apply first the cladmetal by spraying it on to the desired thickness and then coat that with aluminum deposited to form a layer only a few thousandths oi an inch in thickness. Any other suitable deoxidizer can be applied in place of the aluminum if desired.
Following the above given operation the object is preheated and then the sprayed coating is remelted progressively by applicable -means such as the carbon arc, the single or multiple iet oxyacetylene llame, or, whenever the geometry of the object makes it permissible, high frequency induction.
The remelting must be carried out with a sufiiciently high power imput to permit liquefying the sprayed on metal and causing it to fuse to the base metal without allowing the heat to dwell long enough to cause a metallurgical change in the base metal. Remelting the overlay progressively permits retaining the original contour and thickness thereof. v
Metal deposited by means of/metal spraying is only a conglomerate of small particles held together by partial fusion and by mechanical cohesion or the interlocked particles as seen in the reproduced photomicrograph Figs. 1 and 2. The
adhesion of the sprayed on metal to the base metal is likewise purely mechanical..
The reproduced photomicrographs in Figs. 3 and 4 show that on remelting the sprayed on conglomerate a homogeneous, cast structure is produced which adheres to the base metal with a true brazed or welded-on fusion.
The structure of the metal in the Coating A shows the more homogeneous characteristics resulting from the fusion of the conglomerate mass. At C' may be seen the result of the fusion of the coating to the surface of the' metal body B', while the characteristics of the metal in the body are not materially changed.
In describing the first phase of the subject method it was mentioned that on completion o1 the building up of the sprayed on overlay another thin coat of aluminum is applied. The role l of this secondary overlay is to act as a scavenger or deoxidizer in remelting the partly oxidized conglomerate. If desired. the aluminum may be applied in several thin layers: the first direct on the base metal, one at about the middle of the desired sprayed on thickness, and nally one over the nal thickness of the sprayed on metal. While aluminum is the preferred substance for deoxidizing, any other metal oi suitable characteristics may be applied.
The above described method is applicable to al1 shapes which may be successfully coated by metal spraying and with all metals which can be sprayed. J
When it is desired to increase or alter the alloy content o! any of the materials available in wire form :for spraying, the following procedure is applicable.
A quantity of the metal or alloy which is required to obtain the desired alloy in the converted clad material is procured in finely divided form and is applied by means of a suitable vehicle and it is painted on the completed sprayedon overlay and then it is covered with the final layer of aluminum. In remelting. the ilnely divided metal particles of the added metal or alloy dissolve in the body oi.' the overlay forming the desired composition.
From the foregoing description it is evident that various modifications in the method may be resorted to without departing from the spirit of the basic invention or 'the scope of the appended claims.
"I'he invention described herein, i! patented, may be manufactured and used by or for the Government for governmental purposes without the payment to me of any royalty thereon.
WhatI claim is:
1. In a method of metal-clading a metal body, the steps of applying a clad-metal by spraying it on to the desired thickness, preheating the body below the melting temperature o! any of the metals, and then progressively remelting the clad-metal with a sufllciently high power heat concentration to permit liquefying the sprayed on metal and causing it to fuse to the body without allowing the heat to dwell long enough to cause a metallurgical change in the metal of the body.
2. In a method of .metal-clading a metal body, the steps of applying a clad-metal by spraying it on to the desired thickness, coating it with a thinV layer of deoxidizer, preheating the body below the melting tem-perature of any of the metals, and then progressively remelting the clad-metal with a sufficiently high power heat concentration to permit liquefying the sprayed on metal and causing it to fuse to the body without allowing the heat to dwell long enough to cause a metallurgical change in the metal of the body.
3. A method of coating a metal surface with a layer of another metal, said layer having any desired thickness and shape or contour, comprising applying said layer in conglomerate form to the desired thickness and shape, then applying concentrated heat progressively in a manner to melt a comparatively small expanse of the layer at a time, with only suiiicient heat to simultaneously melt only a micronlm of the metal surface in contact with said expanse and without causing 9, metallurgical change in the metal below the surface.
4. A method of coating a metal surface with a layer of another metal, said layer having any desired thickness and shape or contour, comprising applying said layer in conglomerate form to the desired thickness and shape, preheating the combination to a moderate temperature to reduce the heat gradient in the performance of the following step, and then applying concentrated heat progressively in a manner to melt a comparatively small expanse of the layer at a time, with only suiilcient heat to simultaneously melt only a microfilm of the metal surface in contact with said expanse and without causing a metallurgical change in the metal below the surface.
'5. In a method of metal-clading a metal surface, spraying a clad-metal in the desired thickness on the metal surface, applying a suitable deoxidizer by painting, then preheating the entire combination and then progressively remelting the metal coating by means of applied heat suiliciently concentrated to fuse the coating to the surface of the metal without dwelling long enough in one place to cause a metallurgical change in the base metal or to disturb the original contour and thickness of the coating,
BELA RONAY.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US446617A US2361962A (en) | 1942-06-11 | 1942-06-11 | Method of metal-clading |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US446617A US2361962A (en) | 1942-06-11 | 1942-06-11 | Method of metal-clading |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US2361962A true US2361962A (en) | 1944-11-07 |
Family
ID=23773251
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US446617A Expired - Lifetime US2361962A (en) | 1942-06-11 | 1942-06-11 | Method of metal-clading |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US2361962A (en) |
Cited By (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2694168A (en) * | 1950-03-31 | 1954-11-09 | Hughes Aircraft Co | Glass-sealed semiconductor crystal device |
| US2763920A (en) * | 1951-03-06 | 1956-09-25 | Thompson Prod Inc | Corrosion and impact-resistant article |
| US2813048A (en) * | 1954-06-24 | 1957-11-12 | Bell Telephone Labor Inc | Temperature gradient zone-melting |
| US2820375A (en) * | 1954-12-22 | 1958-01-21 | Owens Illinois Glass Co | Forming glass molding tools |
| DE968986C (en) * | 1951-09-19 | 1958-04-17 | Deutsche Edelstahlwerke Ag | Welding rod |
| US2864696A (en) * | 1956-01-31 | 1958-12-16 | Duriron Co | Nickel base alloys |
| US2885304A (en) * | 1954-09-29 | 1959-05-05 | Gen Motors Corp | Method of aluminum coating |
| US3033705A (en) * | 1956-08-13 | 1962-05-08 | Gen Motors Corp | Method of applying an aluminum coating on ferrous metal article |
| US3079275A (en) * | 1959-10-12 | 1963-02-26 | Inland Steel Co | Spray-coating process |
| US9816619B2 (en) | 2011-01-17 | 2017-11-14 | Hamilton Sundstrand Corporation | Thrust plate for butterfly valve |
| US9976664B2 (en) | 2010-11-05 | 2018-05-22 | Hamilton Sundtrand Corporation | Furnace braze deposition of hardface coating on wear surface |
-
1942
- 1942-06-11 US US446617A patent/US2361962A/en not_active Expired - Lifetime
Cited By (12)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2694168A (en) * | 1950-03-31 | 1954-11-09 | Hughes Aircraft Co | Glass-sealed semiconductor crystal device |
| US2763920A (en) * | 1951-03-06 | 1956-09-25 | Thompson Prod Inc | Corrosion and impact-resistant article |
| DE968986C (en) * | 1951-09-19 | 1958-04-17 | Deutsche Edelstahlwerke Ag | Welding rod |
| US2813048A (en) * | 1954-06-24 | 1957-11-12 | Bell Telephone Labor Inc | Temperature gradient zone-melting |
| US2885304A (en) * | 1954-09-29 | 1959-05-05 | Gen Motors Corp | Method of aluminum coating |
| US2820375A (en) * | 1954-12-22 | 1958-01-21 | Owens Illinois Glass Co | Forming glass molding tools |
| US2864696A (en) * | 1956-01-31 | 1958-12-16 | Duriron Co | Nickel base alloys |
| US3033705A (en) * | 1956-08-13 | 1962-05-08 | Gen Motors Corp | Method of applying an aluminum coating on ferrous metal article |
| US3079275A (en) * | 1959-10-12 | 1963-02-26 | Inland Steel Co | Spray-coating process |
| US9976664B2 (en) | 2010-11-05 | 2018-05-22 | Hamilton Sundtrand Corporation | Furnace braze deposition of hardface coating on wear surface |
| US10495231B2 (en) | 2010-11-05 | 2019-12-03 | Hamilton Sundstrand Corporation | Furnace braze deposition of hardface coating on wear surface |
| US9816619B2 (en) | 2011-01-17 | 2017-11-14 | Hamilton Sundstrand Corporation | Thrust plate for butterfly valve |
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