US2985955A - Metal clad article - Google Patents

Metal clad article Download PDF

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US2985955A
US2985955A US647973A US64797357A US2985955A US 2985955 A US2985955 A US 2985955A US 647973 A US647973 A US 647973A US 64797357 A US64797357 A US 64797357A US 2985955 A US2985955 A US 2985955A
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metal
titanium
clad
steel
metals
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US647973A
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Rostoker William
Robert F Domagala
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Armour Research Foundation
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Armour Research Foundation
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Priority to US98006A priority patent/US3060557A/en
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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23KSOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K35/00Rods, electrodes, materials, or media, for use in soldering, welding, or cutting
    • B23K35/001Interlayers, transition pieces for metallurgical bonding of workpieces
    • B23K35/005Interlayers, transition pieces for metallurgical bonding of workpieces at least one of the workpieces being of a refractory metal
    • 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
    • Y10T428/12806Refractory [Group IVB, VB, or VIB] metal-base component
    • 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
    • Y10T428/12806Refractory [Group IVB, VB, or VIB] metal-base component
    • Y10T428/12819Group VB metal-base component
    • 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
    • Y10T428/12924Fe-base has 0.01-1.7% carbon [i.e., steel]

Definitions

  • This invention relates to a method of cladding one metal with another and to the products resulting from such method and more particularly the instant invention relates to a cladding method in which an intermediate metal is, or intermediate metals are, interposed between the base metal and the cladding metal, such interposed material acting as a diffusion barrier to eliminate the formation of brittle and continuous intermetallic compounds between the base and the cladding metal.
  • An object of the instant invention to provide a method whereby hithertofore impossible permanent metal cladding may be performed, the end product of such cladding procedure being extremely stable and not subject to separation during forming operation or in service.
  • Another object of the instant invention is to provide a metal cladding process whereby the clad metal will be strongly adherent to the base metal and where the formation of continuous and brittle intermetallic compounds of the base metal and clad metal does not occur.
  • Still another object of the instant invention is to prevent the formation of continuous and brittle intermetallic compounds between the base metal and the clad metal.
  • titanium has excellent corrosion resistance in sea water and various chemical environments. Unfortunately, the high cost of the metal precludes its use in many potential applications.
  • titanium may be clad onto steel and the ratio of titanium to steel is quite small. Thus, steel is the load sustaining member, while the corrosion resistance of titanium is fully utilized.
  • This problem of separation of the clad metal from the base metal is not limited to the titanium and steel system but as we and others have found may occur in practically every case in which the two metals form continuous and brittle intermetallic compounds at their interface. As the intermetallic compounds are formed, embrittlement of the joint or weld occurs.
  • the instant invention may be utilized in all cladding systems where continuous and brittle intermetallic compounds are normally formed at the interface of two metals.
  • the basic concept underlying our invention is the fact that a third metal may be interposed between two other metals to firmly clad these two other metals if the intermediate metal does not form continuous and brittle intermetallic compounds with either the clad or the base metal.
  • a third metal may be interposed between two other metals to firmly clad these two other metals if the intermediate metal does not form continuous and brittle intermetallic compounds with either the clad or the base metal.
  • Pure metals each have their own intrinsic crystal structure and physical properties.
  • the simplest alloys are microscopically fine mixtures of the pure metals or solid solutions thereof. It frequently happens that the alloy of two pure metals at some simple ratio of atomic concentrations contains neither of the pure metals in their free form.
  • the alloy has a new crystal structure unlike either of the parent metals, has quite different physical properties and is almost invariably brittle and is called an intermetallic compound or an intermediate phase.
  • sequence of structures with increasing alloy may be:
  • clad metal and base metal used in the above chart may be interchanged, depending upon which metal is considered the clad.
  • zirconium as the base metal, iron could be clad thereon by the interposition of a layer of titanium and a layer of vanadium therebetween.
  • a difiusion barrier consisting of two or even more metals should be next considered.
  • Such a quadripartite cladding system must be used when a single known interposed metal which forms harmful intermetallics with neither the base now the clad cannot be found.
  • Aluminum-beryllium-magnesium-iron in either cladding aluminum to iron or vice versa Aluminum forms intermetallics with iron with the end result that these materials will separate when heated and bent. If beryllium alone is interposed between the aluminum and iron the clad will also fail, failure occurring at the beryllium-iron interface since these two metals form intermetallics. The aluminum-beryllium interface will remain stably united since these metals do not form intermetallics.
  • a roll clad operation is normally performed by laying a slab of one metal on top of the other. Such composite is usually first welded around the edges to prevent relative movement and to exclude air and then the unit is hot rolled using very large reductions per pass. This results in the development of a pressure weld between the two metals. The pressure weld must be of sufficient strength to tolerate bending of the clad without separation. If this simple rolling operation is performed on a composite titanium and steel unit it is possible to bond the two metals. However, the result and clad, after annealing, cannot tolerate bending operations such as are needed to fabricate the clad into some useful form. Continuous brittle intermetallic compounds form at the interface through interdiflusion to negate the sought desirable end product.
  • the relative thickness of the starting materials will be the same in the finished product.
  • Ductile vanadium sheet of practically any thickness is interposed between the titanium-steel interface. Thickness of 0.025 and 0.050 inch have been successfully utilized.
  • the steel may be of either the plain carbon or the stainless variety.
  • the initial sandwich assembly must preclude the admission of air during rolling, for both vanadium and titanium are quite reactive with various components of air at the rolling temperature. This exclusion is most conveniently accomplished by welding the vanadium to the titanium and the vanadium to the steel, being careful not to form a titanium-steel fusion bond.
  • Another air exclusion method is to form a cavity in the steel for the insertion of the vanadium and titanium covering with a steel plate and welding shut.
  • hot rolling is performed in the usual manner. Rolling is performed at a temperature range from about 750 to 1000 centigrade. The thickness reduction per rolling pass seems to be of no consequence.
  • reductions of 0.025 and 0.100 inch per pass yielded clads of similar quality. The minimum reduction for bonding seems to be about 60%, although the quality of the clad may not be very good until a reduction of near has been accomplished. Even greater reductions (80-95%) have provided better clads.
  • the process of cladding titanium onto plain carbon steel comprising the steps of: forming a four-layer composite of titanium, vanadium, copper and plain carbon steel, the vanadium layer being positioned between the titanium and the copper and the copper layer being positioned between the vanadium and the steel whereby the formation of intermetallic compounds between the titanium and steel is prevented; uniting the edges of said composite to prevent the introduction of air between the layers; and rolling said composite at a temperature from 750 C. to 1000" C. under adequate pressure to insure the interbonding of the composite.

Description

United States Patent Ofice Patented May 30, 1961 METAL CLAD ARTICLE William Rostoker, Oak Lawn, and Robert F. Domagala,
Chicago, Ill., assignors to Armour Research Foundation of Illinois Institute of Technology, Chicago, 111., a corporation of Illinois No Drawing. Filed Mar. 25, 1957, Ser. No. 647,973
1 Claim. (Cl. 29-4711) This invention relates to a method of cladding one metal with another and to the products resulting from such method and more particularly the instant invention relates to a cladding method in which an intermediate metal is, or intermediate metals are, interposed between the base metal and the cladding metal, such interposed material acting as a diffusion barrier to eliminate the formation of brittle and continuous intermetallic compounds between the base and the cladding metal.
An object of the instant invention to provide a method whereby hithertofore impossible permanent metal cladding may be performed, the end product of such cladding procedure being extremely stable and not subject to separation during forming operation or in service.
Another object of the instant invention is to provide a metal cladding process whereby the clad metal will be strongly adherent to the base metal and where the formation of continuous and brittle intermetallic compounds of the base metal and clad metal does not occur.
Still another object of the instant invention is to prevent the formation of continuous and brittle intermetallic compounds between the base metal and the clad metal.
Other objects, features and advantages of the instant invention will become apparent to those skilled in this art from the following disclosures thereof.
Many attempts have been made to clad one metal with another with varying degrees of success. Such processes and end products have assumed a greater importance in present day technology with the existence of extremely severe operating conditions. It has become desirable to combine the cheapness of base metals such as steel with highly corrosion resistant but expensive metals, for example, titanium, in order to be able to utilize the, advantages of each. In some cases cost is not the important factor, for two expensive metals may be united to have the beneficial attributes of each in the finished product. It is well-known in the artand we have found in our experiments that in many cases it is impossible to form durable clads, particularly when the metals are used or treated under high temperature conditions and when continuous and brittle intermetallic compounds of the, two metals are formed.
It is known that titanium has excellent corrosion resistance in sea water and various chemical environments. Unfortunately, the high cost of the metal precludes its use in many potential applications. By the use of the instant invention titanium may be clad onto steel and the ratio of titanium to steel is quite small. Thus, steel is the load sustaining member, while the corrosion resistance of titanium is fully utilized.
When the attempt is made to clad for example titanium onto steel, although the titanium will adhere at low temperatures this is not the case after annealing and subsequent circumstances where the clad is subjected to stress, as for example by bending or other fabrication procedures. At high temperatures, or under physical stress, the titanium will separate from the steel and result in the destruction of the usefulness of the clad. Once the titanium and iron have separated not only may the structural element of which they are a part be vitally impaired but also the steel is no longer afforded the protection of the titanium and becomes subject to corrosive influences and the like.
This problem of separation of the clad metal from the base metal is not limited to the titanium and steel system but as we and others have found may occur in practically every case in which the two metals form continuous and brittle intermetallic compounds at their interface. As the intermetallic compounds are formed, embrittlement of the joint or weld occurs.
The instant invention may be utilized in all cladding systems where continuous and brittle intermetallic compounds are normally formed at the interface of two metals. The basic concept underlying our invention is the fact that a third metal may be interposed between two other metals to firmly clad these two other metals if the intermediate metal does not form continuous and brittle intermetallic compounds with either the clad or the base metal. Using the titanium-steel example once more we see the following: at room temperatures unstressed titanium clad steel is stable and will not separate, form intermetallic compounds, or become brittle.
However as the temperature of the bimetal is increased the intermetallics form by diffusion a continuous intervening layer with subsequent embrittlement. If a thin sheet of vanadium is inserted between the titanium and steel and then the tri-layered mass heated and compressed to form the finished product the material will be extremely stable at elevated temperatures and there is no harmful formation of intermetallic compounds with the consequence involved therein. This phenomenon is explained by the fact that vanadium does not form continuous brittle intermetallic layers with either titanium or iron and therefore acts as a diffusion barrier between the two metals. The utilization of a diffusion barrier metal is novel and the teachings of the instant invention make it readily used in a broad variety of cladding materials.
Since the use of a diffusion barrier metal as a preventative of harmful intermetallic compound formation is besically the heart of the instant invention we feel it necessary to elaborate upon the principle which determines the correct material to use. The most important limitation, of' course, is that. the interposed material be unable to form continuous and brittle intermetallic compounds with either the base or the cladding metal. If this formation is. not possible the, result will be no embrittlement and no separation of the metals during subsequent forming or in service.
To illustrate, let us assume that we wish to clad metal A with metal C and that the harmful intermetallic compound A C may be produced. Let us now interpose metal B between A and C, and heat and press or roll the' cally useless at an elevated temperature or after annealing. We found continuous intermetallic compound formation and embrittlement at the interface of what was.
once, at least to all outward appearances, a durable joint. We then interposed a thin sheet of vanadium between the two, formed it in the exact same way that the titaniumsteel combination per se was formed and then found that an extremely stable material resulted. This material did not separate on bending or become brittle at elevated temperatures.
Pure metals each have their own intrinsic crystal structure and physical properties. The simplest alloys are microscopically fine mixtures of the pure metals or solid solutions thereof. It frequently happens that the alloy of two pure metals at some simple ratio of atomic concentrations contains neither of the pure metals in their free form. The alloy has a new crystal structure unlike either of the parent metals, has quite different physical properties and is almost invariably brittle and is called an intermetallic compound or an intermediate phase.
If one examines all of the possible alloys in a simple alloy system, the sequence of structures with increasing alloy may be:
We have found that many other systems are well adapted to this method of cladding. Some of these systems are as follows:
Clad Difiusion Base Metal Barrier Metal Metal Zr Ti-i-V Fe Mo Cu Fe Mg Ti Th V Mg Be Ti V+Cu Ni Ta V Fe Be 2 V A1 Be-i-Mg Fe Ta g Cu It should be understood that the terms clad metal and base metal used in the above chart may be interchanged, depending upon which metal is considered the clad. Thus, for example, if it were necessary to use zirconium as the base metal, iron could be clad thereon by the interposition of a layer of titanium and a layer of vanadium therebetween.
A difiusion barrier consisting of two or even more metals should be next considered. Such a quadripartite cladding system must be used when a single known interposed metal which forms harmful intermetallics with neither the base now the clad cannot be found. Consider the example of aluminum-beryllium-magnesium-iron in either cladding aluminum to iron or vice versa. Aluminum forms intermetallics with iron with the end result that these materials will separate when heated and bent. If beryllium alone is interposed between the aluminum and iron the clad will also fail, failure occurring at the beryllium-iron interface since these two metals form intermetallics. The aluminum-beryllium interface will remain stably united since these metals do not form intermetallics. The problem thus is one of using the correct metal between the beryllium and iron layers, by correct of course is meant one not forming harmful intermetallics with either. Magnesium admirably fulfills these requirements. It is seen that not only must the proper metal be selected, but its correct positioning in the system must be maintained. In the example given above if the position of the magnesium and beryllium were reversed the end product, say of aluminum-cladiron would not have the desirable properties afiorded by the instant invention.
As above stated, it is quite feasible to clad steel with titanium by interposing a thin sheet of vanadium between the two metals. We have also found that the system comprising: titanium-vanadium-copper-steel is also conveniently used for this desirable end product. The various interfaces of titanium-vanadium, vanadium-copper, and
4 copper-iron do not give rise to any intermetallic compounds.
A roll clad operation is normally performed by laying a slab of one metal on top of the other. Such composite is usually first welded around the edges to prevent relative movement and to exclude air and then the unit is hot rolled using very large reductions per pass. This results in the development of a pressure weld between the two metals. The pressure weld must be of sufficient strength to tolerate bending of the clad without separation. If this simple rolling operation is performed on a composite titanium and steel unit it is possible to bond the two metals. However, the result and clad, after annealing, cannot tolerate bending operations such as are needed to fabricate the clad into some useful form. Continuous brittle intermetallic compounds form at the interface through interdiflusion to negate the sought desirable end product.
In order that our process may be fully understood the following detailed example is presented:
Example I Titanium sheet and steel sheet, 0.125 inch and /1 inch thick respectively were selected as the cladding and clad materials. The relative thickness of the starting materials will be the same in the finished product. Ductile vanadium sheet of practically any thickness is interposed between the titanium-steel interface. Thickness of 0.025 and 0.050 inch have been successfully utilized. The steel may be of either the plain carbon or the stainless variety. The initial sandwich assembly must preclude the admission of air during rolling, for both vanadium and titanium are quite reactive with various components of air at the rolling temperature. This exclusion is most conveniently accomplished by welding the vanadium to the titanium and the vanadium to the steel, being careful not to form a titanium-steel fusion bond. Another air exclusion method is to form a cavity in the steel for the insertion of the vanadium and titanium covering with a steel plate and welding shut. After the sandwich is formed hot rolling is performed in the usual manner. Rolling is performed at a temperature range from about 750 to 1000 centigrade. The thickness reduction per rolling pass seems to be of no consequence. Experiments were run where reductions of 0.025 and 0.100 inch per pass yielded clads of similar quality. The minimum reduction for bonding seems to be about 60%, although the quality of the clad may not be very good until a reduction of near has been accomplished. Even greater reductions (80-95%) have provided better clads.
The above example introduces a diffusion barrier which prevents the formation of damaging brittle intermetallic compounds. However, due to the carbon content of the steel there is apparently some formation of discontinuous complex carbides. This carbide formation does not seriously affect the bend ductility of the clad or the stability of the interface union. We have found that it is possible to prevent the formation even of these carbides by the use of a second intervening layer, such layer being of pure copper. The fabrication of such a four tiered clad is the same as that for the tripartite material discussed above. The copper is interposed between the steel and vanadium of Example I. Copper sheet 0.007 inch thick was employed, it of course being understood that here again varying thickness may be utilized.
It will be understood that modification and variations may be effected without departing from the spirit and scope of the instant invention.
We claim as our invention:
The process of cladding titanium onto plain carbon steel comprising the steps of: forming a four-layer composite of titanium, vanadium, copper and plain carbon steel, the vanadium layer being positioned between the titanium and the copper and the copper layer being positioned between the vanadium and the steel whereby the formation of intermetallic compounds between the titanium and steel is prevented; uniting the edges of said composite to prevent the introduction of air between the layers; and rolling said composite at a temperature from 750 C. to 1000" C. under adequate pressure to insure the interbonding of the composite.
References Cited in the file of this patent UNITED STATES PATENTS Hensel -Jan. 23, 1951 6 Ulam Aug. 14, 1956 Keay Mar. 26, 1957 Slomin July 9, 1957 Keay Nov. 19, 1957 Gray Oct. 7, 1958 OTHER REFERENCES Brazing Titanium to Titanium and to Mild and Stainless Steels, WADC Report 52-313, part No. 2, published December 1953, pp. 1 and 22-23.
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Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3121949A (en) * 1961-12-14 1964-02-25 Lukens Steel Co Method for manufacturing titanium clad steel
US3798747A (en) * 1972-06-06 1974-03-26 Du Pont Conversion-rolling of titanium/steel bonded composite
WO1986003704A1 (en) * 1984-12-17 1986-07-03 Dow Chemical Co A method for welding a titanium sheet to a ferrous metal
US4765530A (en) * 1984-12-17 1988-08-23 The Dow Chemical Company Method for forming a titanium lined electrochemical cell
US4839242A (en) * 1986-02-24 1989-06-13 Sumitomo Metal Industries, Ltd. Titanium-clad steel and a method for the manufacture thereof
US5190831A (en) * 1991-11-05 1993-03-02 Explosive Fabricators, Inc. Bonded titanium/steel components
US20050156014A1 (en) * 2002-08-09 2005-07-21 Korea Institute Of Science And Technology Clad sheets for corrosion resistance and fabricating method thereof
US20090136778A1 (en) * 2005-03-09 2009-05-28 Carbone Lorraine Equipements Genie Chimique (S.A.S.U) Zirconium-coated steel plates and chemical device elements produced with such plates
FR2936178A1 (en) * 2008-09-24 2010-03-26 Snecma ASSEMBLY OF TITANIUM AND STEEL PARTS BY WELDING DIFFUSION
US20240075709A1 (en) * 2022-09-06 2024-03-07 Ems Engineered Materials Solutions, Llc Deep Drawable Clad Systems and Methods Thereof

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2539247A (en) * 1945-07-31 1951-01-23 Mallory & Co Inc P R Method of bonding aluminum to steel
US2654946A (en) * 1949-09-09 1953-10-13 Int Nickel Co Soldered joint for chromium alloy gas turbine structures
US2758368A (en) * 1951-09-11 1956-08-14 John B Ulam Method of making composite metal bodies of different metals
US2786265A (en) * 1953-02-03 1957-03-26 Lukens Steel Co Process of producing composite metal products
US2798843A (en) * 1953-10-29 1957-07-09 Rohr Aircraft Corp Plating and brazing titanium
US2813332A (en) * 1953-08-14 1957-11-19 Lukens Steel Co Process of preparing composite metal products
US2854738A (en) * 1945-01-09 1958-10-07 Allen G Gray Nickel coated uranium article

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2854738A (en) * 1945-01-09 1958-10-07 Allen G Gray Nickel coated uranium article
US2539247A (en) * 1945-07-31 1951-01-23 Mallory & Co Inc P R Method of bonding aluminum to steel
US2654946A (en) * 1949-09-09 1953-10-13 Int Nickel Co Soldered joint for chromium alloy gas turbine structures
US2758368A (en) * 1951-09-11 1956-08-14 John B Ulam Method of making composite metal bodies of different metals
US2786265A (en) * 1953-02-03 1957-03-26 Lukens Steel Co Process of producing composite metal products
US2813332A (en) * 1953-08-14 1957-11-19 Lukens Steel Co Process of preparing composite metal products
US2798843A (en) * 1953-10-29 1957-07-09 Rohr Aircraft Corp Plating and brazing titanium

Cited By (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3121949A (en) * 1961-12-14 1964-02-25 Lukens Steel Co Method for manufacturing titanium clad steel
US3798747A (en) * 1972-06-06 1974-03-26 Du Pont Conversion-rolling of titanium/steel bonded composite
WO1986003704A1 (en) * 1984-12-17 1986-07-03 Dow Chemical Co A method for welding a titanium sheet to a ferrous metal
US4765530A (en) * 1984-12-17 1988-08-23 The Dow Chemical Company Method for forming a titanium lined electrochemical cell
US4839242A (en) * 1986-02-24 1989-06-13 Sumitomo Metal Industries, Ltd. Titanium-clad steel and a method for the manufacture thereof
US5190831A (en) * 1991-11-05 1993-03-02 Explosive Fabricators, Inc. Bonded titanium/steel components
US20050156014A1 (en) * 2002-08-09 2005-07-21 Korea Institute Of Science And Technology Clad sheets for corrosion resistance and fabricating method thereof
US20090136778A1 (en) * 2005-03-09 2009-05-28 Carbone Lorraine Equipements Genie Chimique (S.A.S.U) Zirconium-coated steel plates and chemical device elements produced with such plates
US8505806B2 (en) * 2005-03-09 2013-08-13 Mersen France Py Sas Zirconium-coated steel plates and chemical device elements produced with such plates
FR2936178A1 (en) * 2008-09-24 2010-03-26 Snecma ASSEMBLY OF TITANIUM AND STEEL PARTS BY WELDING DIFFUSION
WO2010034697A1 (en) * 2008-09-24 2010-04-01 Snecma Assembly of titanium and steel parts by diffusion welding
US20110176911A1 (en) * 2008-09-24 2011-07-21 Snecma Assembling titanium and steel parts by diffusion welding
US8911200B2 (en) * 2008-09-24 2014-12-16 Snecma Assembling titanium and steel parts by diffusion welding
US20240075709A1 (en) * 2022-09-06 2024-03-07 Ems Engineered Materials Solutions, Llc Deep Drawable Clad Systems and Methods Thereof

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