US3015885A - Cladding of steel plates with titanium - Google Patents

Cladding of steel plates with titanium Download PDF

Info

Publication number
US3015885A
US3015885A US719928A US71992858A US3015885A US 3015885 A US3015885 A US 3015885A US 719928 A US719928 A US 719928A US 71992858 A US71992858 A US 71992858A US 3015885 A US3015885 A US 3015885A
Authority
US
United States
Prior art keywords
titanium
pack
plate
steel
cladding
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
Application number
US719928A
Inventor
Kenneth W Mceuen
Eugene M Smith
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Lukens Steel Co
Original Assignee
Lukens Steel Co
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Lukens Steel Co filed Critical Lukens Steel Co
Priority to US719928A priority Critical patent/US3015885A/en
Application granted granted Critical
Publication of US3015885A publication Critical patent/US3015885A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • 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
    • B23K20/00Non-electric welding by applying impact or other pressure, with or without the application of heat, e.g. cladding or plating
    • B23K20/22Non-electric welding by applying impact or other pressure, with or without the application of heat, e.g. cladding or plating taking account of the properties of the materials to be welded
    • B23K20/227Non-electric welding by applying impact or other pressure, with or without the application of heat, e.g. cladding or plating taking account of the properties of the materials to be welded with ferrous layer
    • 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
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B15/00Layered products comprising a layer of metal
    • B32B15/01Layered products comprising a layer of metal all layers being exclusively metallic
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00Metal working
    • Y10T29/30Foil or other thin sheet-metal making or treating
    • Y10T29/301Method
    • Y10T29/302Clad or other composite foil or thin metal making
    • 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
    • Y10T428/12861Group VIII or IB metal-base component
    • Y10T428/12937Co- or Ni-base component next to Fe-base component

Definitions

  • Metals such as steel clad with titanium have been found to be highly desirable for many uses. However, it has been found that titanium has certain properties which make it difiicult to bond to steel by the use of the conventional pack rolling procedures. This diificulty is particularly apparent when the clad product is exposed to a subsequent heating operation, as for example, when it must be welded to another metallic member.
  • titanium which make it difficult to clad this metal are its atfinities for oxygen, nitrogen, hydrogen, water vapor, and carbonaceous gases at temperatures above approximately 1300" F., the high rate of interdiffusion between titanium and most other metals having melting points compatible with those used in the making of steel, such as copper, nickel, iron, molybdenum and silver, and the existence of brittle inter-metallic compounds in the alloy systems of these metals.
  • the reaction of titanium with most gases which are not inert is not the only source of difficulty in cladding titanium notwithstanding the fact that solution of these gases in titanium results in brittle bonds.
  • the atmosphere inside the pack must be free of oxygen, nitrogen, hydrogen and water vapor to promote a good bond and to prevent the embrittling of the titanium layer by these gases.
  • the pack is flushed during the heating period with argon, helium or other inert gas.
  • the gas is purified by passing it through a section of titanium sponge mounted in the gas inlet pipe and heated in the range of 1600" F. to 1800" F., and it has been found that this practice resulted in a larger yield of bonded area than previously obtained.
  • the principal object of this invention is the provision of novel improvements in the cladding of other metals with titanium.
  • a further object is the provision of improved procedures for satisfactorily cladding steel with titanium.
  • FIGURE 1 is a sectional view of one form of pack in which a single titanium clad steel plate is made.
  • FIGURE 2 is a view similar to FIGURE 1 but showing a pack from which a pair of titanium clad steel plates are made, and
  • FIGURE 3 is an exploded fragmentary view of the plates of FIGURE 1 before they are assembled but after the base plate has been plated.
  • FIGURES 1 and 3 of the drawing 1 indicates a rectangular steel base plate which has a coating 2 of nickel plated on its upper face.
  • a rectangular titanium plate 3 which is separated from the rectangular steel cover plate 4 by a layer of parting compound 5.
  • the edges of the plate 3 terminate short of the corresponding edges of the plates 1 and 4 to provide spaces 6 for spacer bars 7 which are mounted between the edge portions of the plates 1 and 4 on all four sides of the pack.
  • the bars '7 do not completely fill the spaces 6 to provide gas passages through the pack when the plates and spacer bars have been completely assembled, and the pack welded as indicated at 8.
  • the welds 8 serve to seal hermetically the periphery of the pack.
  • a pipe mounted at each of two opposite sides of the pack and in communication with the peripheral space is a pipe, the pipe 9 being an inlet pipe for gas and the pipe 10 a gas outlet.
  • an inert gas may be passed through the pack, as desired.
  • a portion of the inlet pipe adjacent the pack is provided with a quantity of titanium or other active metal sponge or porous mass 11 held in place by plugs 12 of stainless steel wool and heated to a temperature of 1500 F. to 1800 F. If the gas is not sufficiently pure, it has been found that there is a tendency for the impurities therein to react with the titanium insert and the nickel plated steel plate causing them to tarnish.
  • the pack After the pack has been flushed by the gas, it is charged into a preheated furnace, heated in the range of 1400" F. to 1800 F. until uniform in temperature and then compressed by pressing. While pressing is preferred, rolling may also be used. The reduction in thickness may vary from 7% to 50% or more.
  • titanium clad steel plate withstood bending 180 at room temperatures over a radius of approximately one and one-half times its thickness Bends were made in which the titanium layer was in tension, and others with the titanium in compression, and still others with the bond zone in shear.
  • this pack is substantially the same as that of FIGURE 1 in that it shows a space 6' around the titanium plates and the spacing and sealing bars 7 secured to the base and cover plates by the welds 8.
  • the pack is provided with an inlet pipe 9' and the outlet pipe 111', the inlet pipe being provided with a titanium sponge section 11', and holding plugs 12 of steel wool to maintain the sponge in place.
  • a process for producing a composite metal pack including a metallic base plate, a titanium cladding plate and a cover plate which comprises bonding a coating of nickel on the upper face of the base plate, placing a plate of titanium on said coating, applying a parting material to the upper surface of said titanium plate, placing a cover plate over and in contact with said parting material, hermetically sealing the peripheral edges of said pack, providing the interior of said pack with an inlet means and an outlet means, filling a part of said inlet means with an active metal porous mass, heating the mass in said inlet means to a temperature of between 1500 F.-1800 F., then flushing the pack with a gas which is inert to said titanium plate when heated to thereby heat said pack to a temperature range of from 1400 F. to 1800 F., compressing said pack to reduce the thickness of the pack and to bond the plates to each other except those which are separated by said parting material.

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Pressure Welding/Diffusion-Bonding (AREA)

Description

Jan. 9, 1962 K. w. MCEUEN ETAL 3,015,885
CLADDING OF STEEL PLATES WITH TITANIUM Filed March 7, 1958 INVENTOR5.
A. W. M05060,
firm/mam.
3,015,885 CLADDING OF STEEL PLATES WITH TITANIUM Kenneth W. McEuen, Malvern, and Eugene M. Smith, Coatesville, Pa., assignors to Luk-ens Steel Company, Coatesville, Pa., a corporation of Pennsylvania Filed Mar. 7, 1953, Ser. No. 719,928 5 Claims. (Cl. 29-4709) This invention relates to the production of composite metal products and, more particularly, to improvements in the cladding of steel plates with titanium.
Metals such as steel clad with titanium have been found to be highly desirable for many uses. However, it has been found that titanium has certain properties which make it difiicult to bond to steel by the use of the conventional pack rolling procedures. This diificulty is particularly apparent when the clad product is exposed to a subsequent heating operation, as for example, when it must be welded to another metallic member. The properties of titanium which make it difficult to clad this metal are its atfinities for oxygen, nitrogen, hydrogen, water vapor, and carbonaceous gases at temperatures above approximately 1300" F., the high rate of interdiffusion between titanium and most other metals having melting points compatible with those used in the making of steel, such as copper, nickel, iron, molybdenum and silver, and the existence of brittle inter-metallic compounds in the alloy systems of these metals. The reaction of titanium with most gases which are not inert is not the only source of difficulty in cladding titanium notwithstanding the fact that solution of these gases in titanium results in brittle bonds. Another difliculty experienced in cladding titanium to steel is that diffusion is very rapid between titanium and other metals when they are brought into contact at temperatures of approximately 1300 F. and above. This contact at these temperatures results in the formation of weak and brittle bonds due to the formation of inter-metallic compounds between the bonding metal and the titanium or the steel. Accordingly, it has been found that if an attempt is made to clad steel with titanium by rolling a pack of these metals in the usual manner, a weak alloy will form somewhere in the diffusion zone between the titanium and steel during the rollmg or heating of the pack, and an unsatisfactory bond will result.
After much experimental work, we have found that strong and ductile bonds between titanium and steel separated by an interlayer of nickel can be made if the nickel is bonded to the steel, as by plating, and the titanium plate is applied directly to the nickel layer or plating. The bonds between titanium and nickel plated backing steel have been found to possess the highest mechanical properties and to be superior to bonds obtained between titanium and uncoated low carbon steel, titanium and chromium plated steel, titanium and chromium-iron alloys containing 11.5% to 35% chromium, and titanium and nickel-chromium-molybdenum stainless steel in shear strength and bend ductility.
The atmosphere inside the pack must be free of oxygen, nitrogen, hydrogen and water vapor to promote a good bond and to prevent the embrittling of the titanium layer by these gases. The pack is flushed during the heating period with argon, helium or other inert gas. The gas is purified by passing it through a section of titanium sponge mounted in the gas inlet pipe and heated in the range of 1600" F. to 1800" F., and it has been found that this practice resulted in a larger yield of bonded area than previously obtained.
The diffusion of iron, chromium and nickel into titanium results in the formation of inter-metallic compounds of these metals with titanium, and these compounds make the nited States Patent ice bonds weak and brittle. In the case of titanium and nickel plated steel, such as disclosed in this application, such diffusion can be minimized by limiting the heating of the pack to a temperature of 1700 F. for thirty minutes or 1600 F. for one hour. It has been found that even if bonds made according to our method contain minor amounts of inter-metallic compounds, they are capable of withstanding reheating to 1400" F. for periods up to two hours without decreasing their strength or ductility. Parting compounds commonly used in stainless steel packs are satisfactory for titanium, and roll bonding of this metal to nickel plated steel within the range of 1600 F. to 1700 F. is practicable.
The principal object of this invention is the provision of novel improvements in the cladding of other metals with titanium.
A further object is the provision of improved procedures for satisfactorily cladding steel with titanium.
Other objects will appear hereinafter throughout the specification.
Referring to the drawing:
FIGURE 1 is a sectional view of one form of pack in which a single titanium clad steel plate is made.
FIGURE 2 is a view similar to FIGURE 1 but showing a pack from which a pair of titanium clad steel plates are made, and
FIGURE 3 is an exploded fragmentary view of the plates of FIGURE 1 before they are assembled but after the base plate has been plated.
In FIGURES 1 and 3 of the drawing, 1 indicates a rectangular steel base plate which has a coating 2 of nickel plated on its upper face. Mounted on the nickel plated face of the base plate is a rectangular titanium plate 3 which is separated from the rectangular steel cover plate 4 by a layer of parting compound 5. As clearly shown in FIGURE 1, the edges of the plate 3 terminate short of the corresponding edges of the plates 1 and 4 to provide spaces 6 for spacer bars 7 which are mounted between the edge portions of the plates 1 and 4 on all four sides of the pack. As indicated in FIGURE 1, the bars '7 do not completely fill the spaces 6 to provide gas passages through the pack when the plates and spacer bars have been completely assembled, and the pack welded as indicated at 8. The welds 8 serve to seal hermetically the periphery of the pack. Mounted at each of two opposite sides of the pack and in communication with the peripheral space is a pipe, the pipe 9 being an inlet pipe for gas and the pipe 10 a gas outlet. By this arrangement of the pipes 9 and 10 an inert gas may be passed through the pack, as desired. In order to purify thoroughly the gas passed through the pack, a portion of the inlet pipe adjacent the pack is provided with a quantity of titanium or other active metal sponge or porous mass 11 held in place by plugs 12 of stainless steel wool and heated to a temperature of 1500 F. to 1800 F. If the gas is not sufficiently pure, it has been found that there is a tendency for the impurities therein to react with the titanium insert and the nickel plated steel plate causing them to tarnish.
After the pack has been flushed by the gas, it is charged into a preheated furnace, heated in the range of 1400" F. to 1800 F. until uniform in temperature and then compressed by pressing. While pressing is preferred, rolling may also be used. The reduction in thickness may vary from 7% to 50% or more.
It has been found that titanium clad steel plate withstood bending 180 at room temperatures over a radius of approximately one and one-half times its thickness. Bends were made in which the titanium layer was in tension, and others with the titanium in compression, and still others with the bond zone in shear.
While the plates used to make up the pack have been described as being rectangular in shape, it will be understood that any suitable shape of plate may be used.
In the pack of FIGURE 2, the steel base plate 1', the nickel plating 2, the titanium plate 3', and the parting material are the same as in FIGURE 1, but a second layer of nickel plating 2' has been added to the cover plate 4, and a second titanium plate 3 has been placed between the nickel plating on the plate 4' and the parting material 5. By using this method, two clad steel plates may be formed at the same time. Otherwise, this pack is substantially the same as that of FIGURE 1 in that it shows a space 6' around the titanium plates and the spacing and sealing bars 7 secured to the base and cover plates by the welds 8. As in FIGURE 1, the pack is provided with an inlet pipe 9' and the outlet pipe 111', the inlet pipe being provided with a titanium sponge section 11', and holding plugs 12 of steel wool to maintain the sponge in place.
The above description and drawings disclose two embodiments of the invention, and specific language has been employed in describing the figures. It will, nevertheless, be understood that no limitations of the scope of the invention are thereby contemplated, and that various alterations and modifications may be made as would occur to one skilled in the art to which the invention relates.
We claim:
1. A process for producing a composite metal pack including a metallic base plate, a titanium cladding plate and a cover plate which comprises bonding a coating of nickel on the upper face of the base plate, placing a plate of titanium on said coating, applying a parting material to the upper surface of said titanium plate, placing a cover plate over and in contact with said parting material, hermetically sealing the peripheral edges of said pack, providing the interior of said pack with an inlet means and an outlet means, filling a part of said inlet means with an active metal porous mass, heating the mass in said inlet means to a temperature of between 1500 F.-1800 F., then flushing the pack with a gas which is inert to said titanium plate when heated to thereby heat said pack to a temperature range of from 1400 F. to 1800 F., compressing said pack to reduce the thickness of the pack and to bond the plates to each other except those which are separated by said parting material.
2. A process as defined in claim 1, wherein said base plate is made of steel, and said coating of nickel is plated on said base plate.
3. A process as defined in claim 2, wherein said cover plate is steel, and said metallic mass in said inlet means is a titanium sponge.
4. A process as defined in claim 3, wherein said gas is argon, and said inlet means and said outlet means are formed as pipes.
5. A process as defined in claim 3, wherein said pack is reduced in thickness by the compressing step from 7% to References Cited in the tile of this patent UNITED STATES PATENTS 1,956,818 Arce May 1, 1934 2,727,834 Cape et a1. Dec. 20, 1955 2,745,172 Townsend May 15, 1956 2,747,066 Brace May 22, 1956 2,786,265 Keay Mar. 26, 1957 2,813,332 Keay Nov. 19, 1957 2,908,969 Wagner Oct. 20, 1959 2,914,848 Blum et al. Dec. 1, 1959' OTHER REFERENCES WADC Technical Report 53502, December 1953,
5 pages 1-7 and 16. Published by Wright Air Development Center, Wright-Patterson Air Force Base, Ohio.

Claims (1)

1. A PROCESS FOR PRODUCING A COMPOSITE METAL PACK INCLUDING A METALLIC BASE PLATE, A TITANIUM CLADDING PLATE AND A COVER PLATE WHICH COMPRISES BONDING A COATING OF NICKEL ON THE UPPER FACE OF THE BASE PLATE, PLACING A PLATE OF TITANIUM ON SAID COATING, APPLYING A PARTING MATERIAL TO THE UPPER SURFACE OF THE SAID TITANIUM PLATE, PLACING A COVER PLATE OVER AND IN CONTACT WITH SAID, PARTING MATERIAL, HERMETICALLY SEALING THE PERIPHERAL EDGES OF SAID PACK, PROVIDING THE INTERIOR OF SAID PACK WITH AN INLET MEANS AND AN OUTLET MEANS, FILLING A PART OF SAID INTLET MEANS WITH AN ACTIVE METAL POROUS MASS, HEATING THE MASS IN SAID INLET MEANS TO A TEMPERATURE OF BETWEEN 1500* F.-1800* F., THEN FLUSHING THE PACK WITH A GAS WHICH IS INERT TO SAID TITANIUM PLATE WHEN HEATED TO THEREBY HEAT SAID PACK TO A TEMPERATURE RANGE OF FROM 1400* F. TO 1800* F., COMPRESSING SAID PACK TO REDUCE THE THICKNESS OF THE PACK AND TO BOND THE PLATES TO EACH OTHER EXCEPT THOSE WHICH ARE SEPARATED BY SAID PARTING MATERIAL.
US719928A 1958-03-07 1958-03-07 Cladding of steel plates with titanium Expired - Lifetime US3015885A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US719928A US3015885A (en) 1958-03-07 1958-03-07 Cladding of steel plates with titanium

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US719928A US3015885A (en) 1958-03-07 1958-03-07 Cladding of steel plates with titanium

Publications (1)

Publication Number Publication Date
US3015885A true US3015885A (en) 1962-01-09

Family

ID=24891954

Family Applications (1)

Application Number Title Priority Date Filing Date
US719928A Expired - Lifetime US3015885A (en) 1958-03-07 1958-03-07 Cladding of steel plates with titanium

Country Status (1)

Country Link
US (1) US3015885A (en)

Cited By (21)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3137937A (en) * 1960-10-26 1964-06-23 Du Pont Explosive bonding
US3305922A (en) * 1962-04-10 1967-02-28 Tno Method for explosive welding and explosive welded products
US3466734A (en) * 1967-03-16 1969-09-16 Crucible Steel Co America Metal articles and method
US3497945A (en) * 1966-08-01 1970-03-03 Gen Dynamics Corp Method for solid state welding
US3708866A (en) * 1968-11-25 1973-01-09 Northrop Corp Thin film diffusion brazing of nickel and nickel base alloys
US3735477A (en) * 1971-10-13 1973-05-29 Lukens Steel Co Method of using and removing a parting compound
US3854891A (en) * 1972-09-25 1974-12-17 Allegheny Ludlum Ind Inc Titanium composite
US3909917A (en) * 1973-08-09 1975-10-07 Viktor Fedorovich Lebedev Method of brazing refractory metals and compounds based thereon
US4023936A (en) * 1976-06-14 1977-05-17 Lukens Steel Company Titanium clad steel and process for making
US4065302A (en) * 1975-12-29 1977-12-27 The International Nickel Company, Inc. Powdered metal consolidation method
US4137616A (en) * 1977-01-26 1979-02-06 Vereinigte Osterreichische Eisen- Und Stahlwerke - Alpine Montan Aktiengesellschaft Method of producing a clad shaped body
US4839242A (en) * 1986-02-24 1989-06-13 Sumitomo Metal Industries, Ltd. Titanium-clad steel and a method for the manufacture thereof
US5009966A (en) * 1987-12-31 1991-04-23 Diwakar Garg Hard outer coatings deposited on titanium or titanium alloys
US5060845A (en) * 1989-07-04 1991-10-29 Nkk Corporation Method for manufacture titanium clad steel plate
US5190831A (en) * 1991-11-05 1993-03-02 Explosive Fabricators, Inc. Bonded titanium/steel components
US5253796A (en) * 1991-07-01 1993-10-19 Rockwell International Corporation Retort for gas diffusion bonding of metals under vacuum
US6194088B1 (en) * 1997-11-12 2001-02-27 Daido Steel Co., Ltd. Stainless steel coated with intermetallic compound and process for producing the same
US20070224445A1 (en) * 2005-03-29 2007-09-27 Neomax Materials Co., Ltd. Brazing Filler Metal, Brazing Composite Material and Brazed Structure Brazed/Bonded with the Same
CN102773670A (en) * 2012-07-26 2012-11-14 李向民 Manufacturing method of titanium-steel-titanium two-sided composite plate
CN103231216A (en) * 2013-05-10 2013-08-07 山东亚盛重工股份有限公司 Manufacturing technique and device for composite board
US8727203B2 (en) 2010-09-16 2014-05-20 Howmedica Osteonics Corp. Methods for manufacturing porous orthopaedic implants

Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1956818A (en) * 1931-07-31 1934-05-01 Acre Ray Vacuum process of welding
US2727834A (en) * 1953-09-15 1955-12-20 Superweld Corp Methods of brazing and coating stainless steel parts
US2745172A (en) * 1951-06-06 1956-05-15 Leyshon W Townsend Composite assembly for bonding plates of dissimilar metals
US2747066A (en) * 1949-11-17 1956-05-22 Porter H Brace Heat treating apparatus
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
US2908969A (en) * 1954-05-28 1959-10-20 Horizons Inc Method of cladding steel with titanium or zirconium
US2914848A (en) * 1957-01-11 1959-12-01 Curtiss Wright Corp Method of brazing titanium

Patent Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1956818A (en) * 1931-07-31 1934-05-01 Acre Ray Vacuum process of welding
US2747066A (en) * 1949-11-17 1956-05-22 Porter H Brace Heat treating apparatus
US2745172A (en) * 1951-06-06 1956-05-15 Leyshon W Townsend Composite assembly for bonding plates of dissimilar 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
US2727834A (en) * 1953-09-15 1955-12-20 Superweld Corp Methods of brazing and coating stainless steel parts
US2908969A (en) * 1954-05-28 1959-10-20 Horizons Inc Method of cladding steel with titanium or zirconium
US2914848A (en) * 1957-01-11 1959-12-01 Curtiss Wright Corp Method of brazing titanium

Cited By (24)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3137937A (en) * 1960-10-26 1964-06-23 Du Pont Explosive bonding
US3305922A (en) * 1962-04-10 1967-02-28 Tno Method for explosive welding and explosive welded products
US3497945A (en) * 1966-08-01 1970-03-03 Gen Dynamics Corp Method for solid state welding
US3466734A (en) * 1967-03-16 1969-09-16 Crucible Steel Co America Metal articles and method
US3708866A (en) * 1968-11-25 1973-01-09 Northrop Corp Thin film diffusion brazing of nickel and nickel base alloys
US3735477A (en) * 1971-10-13 1973-05-29 Lukens Steel Co Method of using and removing a parting compound
US3854891A (en) * 1972-09-25 1974-12-17 Allegheny Ludlum Ind Inc Titanium composite
US3909917A (en) * 1973-08-09 1975-10-07 Viktor Fedorovich Lebedev Method of brazing refractory metals and compounds based thereon
US4065302A (en) * 1975-12-29 1977-12-27 The International Nickel Company, Inc. Powdered metal consolidation method
US4023936A (en) * 1976-06-14 1977-05-17 Lukens Steel Company Titanium clad steel and process for making
US4137616A (en) * 1977-01-26 1979-02-06 Vereinigte Osterreichische Eisen- Und Stahlwerke - Alpine Montan Aktiengesellschaft Method of producing a clad shaped body
US4839242A (en) * 1986-02-24 1989-06-13 Sumitomo Metal Industries, Ltd. Titanium-clad steel and a method for the manufacture thereof
US5009966A (en) * 1987-12-31 1991-04-23 Diwakar Garg Hard outer coatings deposited on titanium or titanium alloys
US5060845A (en) * 1989-07-04 1991-10-29 Nkk Corporation Method for manufacture titanium clad steel plate
US5253796A (en) * 1991-07-01 1993-10-19 Rockwell International Corporation Retort for gas diffusion bonding of metals under vacuum
US5190831A (en) * 1991-11-05 1993-03-02 Explosive Fabricators, Inc. Bonded titanium/steel components
US6194088B1 (en) * 1997-11-12 2001-02-27 Daido Steel Co., Ltd. Stainless steel coated with intermetallic compound and process for producing the same
GB2336376B (en) * 1997-11-12 2002-10-30 Daido Steelco Ltd Intermetallic-compound coated stainless steel and method of producing the same
US20070224445A1 (en) * 2005-03-29 2007-09-27 Neomax Materials Co., Ltd. Brazing Filler Metal, Brazing Composite Material and Brazed Structure Brazed/Bonded with the Same
US8029916B2 (en) * 2005-03-29 2011-10-04 Neomax Materials Co., Ltd. Brazing filler metal, brazing composite material and brazed structure brazed/bonded with the same
US8727203B2 (en) 2010-09-16 2014-05-20 Howmedica Osteonics Corp. Methods for manufacturing porous orthopaedic implants
CN102773670A (en) * 2012-07-26 2012-11-14 李向民 Manufacturing method of titanium-steel-titanium two-sided composite plate
CN103231216A (en) * 2013-05-10 2013-08-07 山东亚盛重工股份有限公司 Manufacturing technique and device for composite board
CN103231216B (en) * 2013-05-10 2015-11-11 山东亚盛重工股份有限公司 The production technology of composite plate and production equipment thereof

Similar Documents

Publication Publication Date Title
US3015885A (en) Cladding of steel plates with titanium
US2786265A (en) Process of producing composite metal products
US2713196A (en) Method for cladding and product resulting therefrom
US2473712A (en) Procedure for making multiply metal stock
US2813332A (en) Process of preparing composite metal products
TWI357444B (en) Zirconium-cladded steel plates, and elements of ch
US5788142A (en) Process for joining, coating or repairing parts made of intermetallic material
US3156976A (en) Method of making composite metal products
GB2134832A (en) Method of etablishing a bond between titanium and an iron-nickel alloy
US2993269A (en) Methods for producing titanium-clad metal
US2908969A (en) Method of cladding steel with titanium or zirconium
HU178946B (en) Process for joining details made of aluminium and irom alloys
US3121949A (en) Method for manufacturing titanium clad steel
US4137616A (en) Method of producing a clad shaped body
JPH02263504A (en) Method for molding metal and lamination metal assembly
US3299503A (en) Process for the production of bonded metal structures
US2169354A (en) Method of and means for producing steel clad with stainless steel
US3055096A (en) Method for cladding and product resulting therefrom
JP2601284B2 (en) Sintered diamond composite and manufacturing method thereof
US2932885A (en) Method and pack for making zirconium-clad steel plate
US3604103A (en) Method of cladding metals and composites thereof
US3052976A (en) Production of wrought titanium
JPH07232284A (en) Joining of titanium alloy and iron base metal using intermediate member
US3417460A (en) Methods of brazing
JPH0360414A (en) Method for joining carbon material, joined body by this method and material using the same