EP0357664A1 - Plymetal brazing strip - Google Patents
Plymetal brazing stripInfo
- Publication number
- EP0357664A1 EP0357664A1 EP88904044A EP88904044A EP0357664A1 EP 0357664 A1 EP0357664 A1 EP 0357664A1 EP 88904044 A EP88904044 A EP 88904044A EP 88904044 A EP88904044 A EP 88904044A EP 0357664 A1 EP0357664 A1 EP 0357664A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- alloy
- substrate
- foil
- product
- multilayered
- 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.)
- Withdrawn
Links
- 238000005219 brazing Methods 0.000 title claims abstract description 57
- 229910045601 alloy Inorganic materials 0.000 claims abstract description 65
- 239000000956 alloy Substances 0.000 claims abstract description 65
- 239000000758 substrate Substances 0.000 claims abstract description 65
- 230000015556 catabolic process Effects 0.000 claims abstract description 11
- 238000006731 degradation reaction Methods 0.000 claims abstract description 11
- 239000011888 foil Substances 0.000 claims description 65
- 238000000034 method Methods 0.000 claims description 37
- 239000000463 material Substances 0.000 claims description 25
- 239000000945 filler Substances 0.000 claims description 17
- 229910052802 copper Inorganic materials 0.000 claims description 14
- 239000000203 mixture Substances 0.000 claims description 11
- 238000002844 melting Methods 0.000 claims description 10
- 230000008018 melting Effects 0.000 claims description 10
- 238000001816 cooling Methods 0.000 claims description 9
- 239000002184 metal Substances 0.000 claims description 8
- 229910052751 metal Inorganic materials 0.000 claims description 8
- 238000010438 heat treatment Methods 0.000 claims description 7
- 229910000831 Steel Inorganic materials 0.000 claims description 5
- 239000010959 steel Substances 0.000 claims description 5
- 238000002425 crystallisation Methods 0.000 claims description 4
- 230000008025 crystallization Effects 0.000 claims description 4
- 229910052742 iron Inorganic materials 0.000 claims description 3
- 230000001590 oxidative effect Effects 0.000 claims description 2
- 239000000112 cooling gas Substances 0.000 claims 2
- 229910017770 Cu—Ag Inorganic materials 0.000 claims 1
- 229910000808 amorphous metal alloy Inorganic materials 0.000 claims 1
- 230000000694 effects Effects 0.000 claims 1
- 239000007789 gas Substances 0.000 claims 1
- 238000004519 manufacturing process Methods 0.000 abstract description 7
- 238000010030 laminating Methods 0.000 abstract 1
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 14
- 239000010949 copper Substances 0.000 description 13
- 238000005096 rolling process Methods 0.000 description 11
- 238000007712 rapid solidification Methods 0.000 description 5
- XEEYBQQBJWHFJM-UHFFFAOYSA-N iron Substances [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 3
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 description 2
- 238000002441 X-ray diffraction Methods 0.000 description 2
- 238000007596 consolidation process Methods 0.000 description 2
- PSFDQSOCUJVVGF-UHFFFAOYSA-N harman Chemical compound C12=CC=CC=C2NC2=C1C=CN=C2C PSFDQSOCUJVVGF-UHFFFAOYSA-N 0.000 description 2
- 230000003647 oxidation Effects 0.000 description 2
- 238000007254 oxidation reaction Methods 0.000 description 2
- 238000010791 quenching Methods 0.000 description 2
- 229910001208 Crucible steel Inorganic materials 0.000 description 1
- 229910000767 Tm alloy Inorganic materials 0.000 description 1
- 238000013459 approach Methods 0.000 description 1
- 238000005452 bending Methods 0.000 description 1
- 239000011230 binding agent Substances 0.000 description 1
- 238000005266 casting Methods 0.000 description 1
- 238000005253 cladding Methods 0.000 description 1
- 239000000470 constituent Substances 0.000 description 1
- KUNSUQLRTQLHQQ-UHFFFAOYSA-N copper tin Chemical compound [Cu].[Sn] KUNSUQLRTQLHQQ-UHFFFAOYSA-N 0.000 description 1
- 230000001419 dependent effect Effects 0.000 description 1
- 238000000151 deposition Methods 0.000 description 1
- 238000004455 differential thermal analysis Methods 0.000 description 1
- 230000008030 elimination Effects 0.000 description 1
- 238000003379 elimination reaction Methods 0.000 description 1
- 230000002708 enhancing effect Effects 0.000 description 1
- 239000011261 inert gas Substances 0.000 description 1
- 229910000765 intermetallic Inorganic materials 0.000 description 1
- 150000001247 metal acetylides Chemical class 0.000 description 1
- 229910001092 metal group alloy Inorganic materials 0.000 description 1
- 229910052752 metalloid Inorganic materials 0.000 description 1
- 229910052759 nickel Inorganic materials 0.000 description 1
- 229910052757 nitrogen Inorganic materials 0.000 description 1
- 230000000704 physical effect Effects 0.000 description 1
- 239000000843 powder Substances 0.000 description 1
- 230000002028 premature Effects 0.000 description 1
- 238000012545 processing Methods 0.000 description 1
- 239000010453 quartz Substances 0.000 description 1
- 229910052710 silicon Inorganic materials 0.000 description 1
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N silicon dioxide Inorganic materials O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 description 1
- 238000012360 testing method Methods 0.000 description 1
- 239000011800 void material Substances 0.000 description 1
- 238000003466 welding Methods 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
- B23K35/00—Rods, electrodes, materials, or media, for use in soldering, welding, or cutting
- B23K35/02—Rods, electrodes, materials, or media, for use in soldering, welding, or cutting characterised by mechanical features, e.g. shape
- B23K35/0222—Rods, electrodes, materials, or media, for use in soldering, welding, or cutting characterised by mechanical features, e.g. shape for use in soldering, brazing
- B23K35/0233—Sheets, foils
- B23K35/0238—Sheets, foils layered
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
- B23K35/00—Rods, electrodes, materials, or media, for use in soldering, welding, or cutting
- B23K35/22—Rods, electrodes, materials, or media, for use in soldering, welding, or cutting characterised by the composition or nature of the material
- B23K35/24—Selection of soldering or welding materials proper
- B23K35/30—Selection of soldering or welding materials proper with the principal constituent melting at less than 1550 degrees C
Definitions
- This invention relates to the production of flexible multilayered strip and, in particular, to the production of flexible multilayered brazing foils formed of rapidly solidified homogeneous metal foil joined to a ductile substrate.
- Brazing is a process for metallurgically bonding materials, often of dissimilar compositions, to each others at temperatures above about 450°C.
- a filler metal that has a melting point lower than that of the base material parts to be joined is interposed herebetween and the assembly is then heated to a temperature sufficient to melt the filler metal. Upon cooling, a strong joint is formed.
- brazing is commonly employed in the manufacture of a wide variety of products such as heat exchangers, cemented carbide tipped tools, bicycle frames, electrical products, etc.
- brazing fillers are employed in powder, ribbon, wire or wrought form.
- Improved brazing foils have been formed by rapid solidification techniques. These foils possess the ability to substantially reduce the number of failed joints because of improved homogeneity resulting from the rapid solidification process. Examples of such improved materials are disclosed in U.S. Patent Nos. 4,448,852 and 4,489,136.
- rapidly solidified brazing foils exhibit loses in relative ductility as the foil thickness increases and especially at foil thicknesses of greater than about 75-100 ⁇ m. Accordingly, there are applications which, because of the configurations of the brazed joint (especially those requiring a brazing filler-metal thickness larger than about 75 ⁇ m) require either special handling of the rapidly solidified brazing foil or, in some instances, require the selection of an alternative, inferior brazing material.
- the present invention is directed to multilayered products, in particular multilayered brazing foils, which comprise a rapidly solidified, homogeneous alloy foil metallically bonded to a substrate, wherein the substrate is capable of undergoing a substantial degree of plastic deformation without any substantial degradation of its ductility, and wherein the integrity of the foil layer is maintained.
- the present invention is directed to a process for producing multilayered products, in particular multilayered brazing foils, which comprises the steps of: arranging a rapidly solidified, homogeneous alloy in contact with a substrate capable of undergoing a substantial degree of plastic deformationswithout experiencing a substantial degradation of the ductility thereof; and applying heat and pressure to the alloy and substrate at a temperature and pressure in an amount and for a time sufficient to cause the substrate to undergo plastic deformation and to create metallic bonding between the alloy and the substrate.
- bonding is accomplished by a roll bonding process to produce continuous, multilayered brazing strip.
- an improved process for brazing parts comprising the steps of arranging at least two parts relative to each other to define a gap therebetween, interposing in the gap between the parts a multilayered brazing filler material comprising a layer of rapidly solidified, homogeneous alloy foil metallically bonded to a substrate capable of undergoing substantial plastic deformation without substantial degradation of the ductility thereof, heating at least the filler material to melt at least the foil and to cause the parts to be joined, and then cooling the filler material to produce a brazement.
- the brazing material In any brazing process, the brazing material must meet a variety of criteria in order to be acceptable for use in the process.
- the brazing material must have a melting point that is sufficiently high to maintain its integrity and physical properties over the entire range of service requirements of the metal parts being brazed.
- the melting point must not be so high as to make difficult the brazing operation.
- the filler material must be compatible, both chemicallly and metallurgically, with the parts being brazed. Morever, the brazing material should be homogeneous; that is, it should have a substantially uniform composition in all dimensions.
- the brazing material must be ductile to enable it to be formed to accommodate the size and shape of the joint gap to be brazed. Finally, the brazing material must be thick enough to provide sufficient filler metal to fill completely the gap.
- Multilayered metallic products are generally referred to as "plymetal" parts. Rapidly solidified, homogeneous alloy foils have been produced for a number of years by a process referred to as rapid solidification technique. See, for example. U.S. Patent Nos. 4,448,852 and 4,489,136.
- the process comprises the steps of selecting a particular composition of the requisite elements in the desired proportions, melting and homogenizing the same, and depositing the molten compositions onto a chill surface, such as rapidly rotating cylinder, to quench the composition.
- Rapid solidification as used herein means the application of a quench rate of at least about 10 5 °C/sec.
- the products resulting from this process may be crystalline or amorphous, but regardless of their structure, they are homogeneous.
- the products are in foil form; that is, they have a thickness that is small relative to the width and length of the product. Most preferably, the foil is in the form of ribbon.
- the rapidly solidified, homogeneous foil is metallically bonded to a substrate.
- the substrate is formed of a material which is capable of undergoing a substantial degree of plastic deformation without substantial degradation of its ductility.
- the degree of plastic deformation ranges from a few percent to
- Substrates within the scope of the invention include Cu and Cu-base alloys, Cu-Ag-base alloy. Fe and Fe-base alloys and Ni and Ni-base alloys. Most preferably, the substrate is matched to the foil to which it is to be bonded. For example, Cu-base alloy foils would most preferably be bonded to Cu or Cu-base alloy substrates.
- Metallic bonds are created by the sharing of electrons by groups of atoms, creating what is sometimes referred to as an electron cloud of free moving electrons.
- the existance of a composition gradient between the foil and substrate, which enhances the creation of such electron cloud, coupled with plastic deformation of the substrate at an elevated temperature yields an essentially void free, continuous interface between the foil and substrate and creates to produce a strong metallic bond at the interface.
- Multilayered products within the scope of the invention are, most preferably, brazing strips.
- the brazing strips of the present invention overcome a long-felt need in the industry to produce thick, ductile brazing strip from compositions which are inherently brittle in conventional form or in thick (A 100 ⁇ m) rapidly solidified foil from.
- Most brazing alloys contain a large concentration of metalloid elements such as Si, B, and P which form brittle intermetallic compounds upon crystallization.
- the present invention advantageously utilizes the plasticity and inherent ductility in the substrate to produce a multilayered product which has ductility substantially equal to he ductility of the substrate.
- the invention is particularly useful in brazing applications which require filling a gap of 100 ⁇ m or more.
- the multilayered brazing strip enhance the ability to braze certain dissimilar materials. For example.
- the prior art employed expensive silver-base brazing filler metal to braze the carbide to the steel.
- the thermal expansion coefficient of the carbides and steel are so different, internal stresses in the brazement are quite high and can lead to premature failure.
- a three-layered strip of a substrate, such as copper, sandwiched between rapidly solidified homogeneous-brazing alloy is used because the substrate accommodates the difference in stresses between the carbide and the steel while maintaining the service thermal and strength requirements of the tool.
- Another advantage to the production of thick brazing filler products is the elimination of the need for adhering together multiple strips of rapidly solidified material through the use of binders which could contaminate the brazement and/or create voids therein.
- the present invention one can, for the first time, produce brazing filler strips of rapidly solidified brazing foil in thickness of 100 ⁇ m or greater. Morever, because of the loss in ductility of rapidly solidified alloys as they approach 100 u m or more in thickness, the present invention provides thick brasing strip which has all the advantages associated with rapidly solidified brazing foil.
- the process of making the products of the present invention comprises the steps of arranging the foil in contact with the substrate and. thereafter, applying heat and pressure to the foil and substrate to cause the substrate to undergo plastic deformation and create metallic bonding between the foil and the substrate.
- the foil and substrate can be brought into contact in any of a variety of ways such as by laying the foil on top of the substrate by hand or, in the most preferred embodiment, by providing the substrate and foil as continuous spools from which strip is continuously fed into contacting relationship at a location at which bonding is to occur.
- Bonding can be created by means of any suitable apparatus which is capable of applying heat and pressure in accordance with the teachings hereinafter.
- conventional cladding equipment can be employed.
- roll bonding apparatus employing heated rolls is used to produce continuous brazing strip.
- the substrate and foil are fed continuously past heated rolls designed and arranged to provide substantially constant temperature and pressure to the substrate and foil in order to bond the same.
- the temperature at which bonding is effected is dependent upon the structure of the rapidly solidified foils.
- amorphous foil i.e., foil which is at least 50% amorphous by x-ray diffraction
- the temperature of bonding must be equal to or greater than the crystallization of the amorphous foil.
- the temperature of bonding must be at least about 0.4T, where T is the melting temperature of the alloy in degree Kelvin. K.
- the pressure applied to the layers must be sufficient to cause plastic deformation of the substrate in an amount necessary to create an essentially continuous, void-free interface between the f oil and the substrate . Accordingly, while the pressure will vary depending upon the substrate material employed, it is preferred that a force of at least about 0.75 MN be used. In particular, for roll bonding (500 mm O.D. rolls), we prefer to employ a separating force of between 0.75 MN and about 2.5 MN. although lower and higher pressures can be used.
- An additional feature of the process is the step of cooling the bonded product.
- the product is cooled by employing air or a non-oxidizing medium such as nitrogen or an inert gas. The cooling most preferably occurs immediately after completion of the bonding step to avoid oxidation of the surface of the product which may affect product utility as a brazing strip.
- processes for brazing parts comprise the steps of arranging at least two parts relative to each other to define a gap therebetween, interposing in the gap a multilayered brazing filler material comprising a layer of rapidly solidified, homogeneous alloy foil metallically bonded to a substrate capable of undergoing substantial plastic deformation without substantial degradation of the ductility thereof, heating at least the filler material to melt at least the brazing foil layer of the strip and to cause the parts to be joined, and thus cooling the filler material to produce a brazement.
- the multilayered products of the present invention are superior to prior art products employed as brazing foils for all of the reasons described heretofore. While the invention has been described primarily by reference to two layered products, it should be quite evident that particularly useful products are those which include more than two layers. e.g., three layers composed of a substrate sandwiched between two rapidly solidified foils as described heretofore.
- Example 1 is provided in order to illustrate the scope of the inventions but are not intended to limit the scope of the invention to anything less than is disclosed hereinabove.
- Example 1 is provided in order to illustrate the scope of the inventions but are not intended to limit the scope of the invention to anything less than is disclosed hereinabove.
- a multilayered brazing strip was produced using an electrolytic tough-pitch copper substrate and a BAg-3 (American Welding Society Designation) microcrystalline alloy.
- BAg-3 microcrystalline alloy was produced by remelting Handy and Harman's Easy Flo-free TM alloy in a quartz crucible and casting by a planar flow rapid solidification technique.
- the center was 2 plies of 25 ram x 75 w m thick copper ribbon.
- the outer layers were made from 25 mm x 75 ⁇ m ribbon of BAg-3 brazing alloy.
- There BAg-3 layers had, prior to rolling, microhardness of 230 and 260 HV (Vickers microhardness units), respectively.
- the copper ribbon had a microhardness of 120 HV. In this case, the copper ribbon is about twice as ductile and malleable as the BAg-3 alloy.
- the strip was produced by high temperature consolidation on a Stanat 6" x 6" rolling mill. At 178 kN force, well bonded material was produced at rolls temperature of 380-400°C and at .03-.05 m/s rolling rate. By using two copper plies together as the substrate, a strip with the commercially desired thickness of 300 m was produced. Strips of 360 mm length were produced.
- Example 2
- Ribbon, 38 ⁇ m thick, of an alloy designated as MBF-2005 (having a composition within the range of compositions disclosed in U.S. 4,489,136) was bonded to both sides of a 406 u rn thick (16 gauge) copper strip.
- the consolidation was carried out in a Canadian Iron Foundry, 2-high, heated rolling mill with 500 mm diameter cast steel rolls.
- the 101 mm wide brazing alloy formed the outer layers while the 108 mm wide, soft copper composed the center core.
- Roll speed was held at 5 m/rain, roll temperature at 490°C. while rolling pressure was 2.0 MN.
- a well bonded multilayered strip was produced.
- Example 5 Using the same heating rolling mill as described in Example 2. above. 100 mm wide x 38 ⁇ m thick ribbons of alloy MBF-2005 were clad on both sides of a 150 mm wide x 127 ⁇ m thick copper core. At conditions of 5 m/min rolling speed. 490°C rolls temperature and 1.6 MN rolling pressure, twenty well bonded strips of plymetal were produced. Good metallurgical bonding between the copper substrate and MBF-2005 alloy and a fine uniform crystalline structure of the MBF-2005 alloy layers resulted. Differential thermal analysis of this plymetal strip was done on a Perkin-Elmer 1700 DTA analyzer in order to determine the melting characteristics of this strip. The strip characteristics are essentially the same as the characteristics of an MBF-2005 single ribbon when measured in the brazing temperature range. The presence of a metallurgically-bonded copper core does not change the strip melting behavior of the low melting MBF-2005 constituent layers.
- Example 5 Example 5
- Example 6 In the same equipment and under similar conditions as in Example 3, separate 25 and 50 mm wide x .38 ⁇ m thick ribbons of MBF-2005 alloy were bonded to both sides of a 25 mm wide x 127 ⁇ m thick copper core. At conditions of 5 m/rain rolling speed, 520°C roll temperature and 1.3 MN force, twenty well-bonded, 300 mm long strips of plymetal were produced.
- Example 6 Two 100 mm wide, 50 ⁇ m thick ribbons of copper-tin (90/10) brazing alloy (designated MBF-2004B) were clad on both sides of a 100 mm wide. 37 ⁇ m thick copper strip.
- Example 3 The same equipment as in Example 3 was used and the production conditions were 3.0 m/min rolling speed, 525oC rolls temperature and 1.45 MN roll pressure. During some tests, the exiting strip was cooled by compressed air. The addition of the cooling step produced a brighter, shinier, oxidation free strip surface, strong metallurgical bonding was achieved with this process as well.
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Pressure Welding/Diffusion-Bonding (AREA)
- Laminated Bodies (AREA)
Abstract
Produit ductile multicouche comprenant une feuille d'alliage homogène rapidement solidifiée, soudée métalliquement à un substrat, dans lequel le substrat est susceptible de subir un degré élevé de déformation plastique sans dégradation sensible de sa ductilité. Le produit est particulièrement utile en tant que bande de brasage. Un procédé de fixation par laminage permettant de produire une bande de brasage ductile continue est également divulgué.Multilayer ductile product comprising a homogeneous rapidly solidified alloy sheet, metallically welded to a substrate, in which the substrate is liable to undergo a high degree of plastic deformation without appreciable degradation of its ductility. The product is particularly useful as a brazing strip. A laminating fastening method for producing a continuous ductile brazing strip is also disclosed.
Description
Claims
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US3568887A | 1987-04-07 | 1987-04-07 | |
| US35688 | 1987-04-07 |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| EP0357664A1 true EP0357664A1 (en) | 1990-03-14 |
| EP0357664A4 EP0357664A4 (en) | 1991-05-22 |
Family
ID=21884221
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| EP19880904044 Withdrawn EP0357664A4 (en) | 1987-04-07 | 1988-04-04 | Plymetal brazing strip |
Country Status (3)
| Country | Link |
|---|---|
| EP (1) | EP0357664A4 (en) |
| JP (1) | JP2825249B2 (en) |
| WO (1) | WO1988007932A1 (en) |
Families Citing this family (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE10043484A1 (en) * | 2000-09-04 | 2002-03-28 | Vacuumschmelze Gmbh | Film composite body |
| US6587742B2 (en) | 2000-12-20 | 2003-07-01 | Mark Manuel | Method and apparatus for the creation of a tool |
| US7222834B2 (en) | 2001-08-14 | 2007-05-29 | Floodcooling Technologies, Llc | Tool and a method for making a tool |
| US20040038074A1 (en) | 2001-11-01 | 2004-02-26 | Mark Manuel | Tool and a method for creating a tool |
| US7338717B2 (en) * | 2002-11-07 | 2008-03-04 | Floodcooling Technologies, Llc | Tool and a method for creating the tool |
| US7195223B2 (en) | 2002-12-02 | 2007-03-27 | Mark Manuel | System and a method for cooling a tool |
| US7563091B2 (en) | 2005-01-18 | 2009-07-21 | Floodcooling Technologies, L.L.C. | Tool having an ejection assembly, a method for making such a tool, and a method for ejecting a formed object from a tool |
| US7376484B2 (en) | 2005-01-18 | 2008-05-20 | Floodcooling Technologies, Llc | Method for building a tool |
| US7278197B2 (en) | 2005-01-18 | 2007-10-09 | Floodcooling Technologies, Llc | Method for producing a tool |
| US7379787B2 (en) | 2005-04-09 | 2008-05-27 | Floodcooling Technologies, Llc | Method for forming a tangible item and a tangible item formed by the method |
Family Cites Families (17)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS4962363A (en) * | 1972-10-18 | 1974-06-17 | ||
| US3940293A (en) * | 1972-12-20 | 1976-02-24 | Allied Chemical Corporation | Method of producing amorphous cutting blades |
| US4146163A (en) * | 1977-11-09 | 1979-03-27 | Aluminum Company Of America | Production of aluminum brazing sheet |
| US4186245A (en) * | 1978-09-28 | 1980-01-29 | Allied Chemical Corporation | Energy storage flywheel |
| US4365005A (en) * | 1978-10-13 | 1982-12-21 | Massachusetts Institute Of Technology | Method of forming a laminated ribbon structure and a ribbon structure formed thereby |
| US4250229A (en) * | 1979-04-04 | 1981-02-10 | United Technologies Corporation | Interlayers with amorphous structure for brazing and diffusion bonding |
| JPS5626689A (en) * | 1979-08-13 | 1981-03-14 | Furukawa Kinzoku Kogyo Kk | Production for low-melting point metal composite string |
| JPS5645714A (en) * | 1979-09-22 | 1981-04-25 | Terumi Hase | Sand digger |
| US4340650A (en) * | 1980-06-20 | 1982-07-20 | Gte Products Corporation | Multi-layer composite brazing alloy |
| DE3106607C2 (en) * | 1981-02-23 | 1987-08-20 | Fr. Kammerer GmbH, 7530 Pforzheim | Plating process |
| US4448853A (en) * | 1981-04-15 | 1984-05-15 | Bbc Brown, Boveri & Company, Limited | Layered active brazing material and method for producing it |
| US4562951A (en) * | 1982-04-12 | 1986-01-07 | The United States Of America As Represented By The Secretary Of The Army | Method of making metallic glass-metal matrix composites |
| JPS58179582A (en) * | 1982-04-13 | 1983-10-20 | Nippon Steel Corp | Manufacturing method of aluminum coated steel sheet |
| US4529458A (en) * | 1982-07-19 | 1985-07-16 | Allied Corporation | Compacted amorphous ribbon |
| JPS59232693A (en) * | 1983-06-17 | 1984-12-27 | Ngk Spark Plug Co Ltd | Clad brazing filler metal for joining ceramics and metal or the like and composite body composed of ceramics and metal or the like using said brazing filler metal |
| US4568014A (en) * | 1983-09-29 | 1986-02-04 | The United States Of America As Represented By The Secretary Of Interior | Bonding of metallic glass to crystalline metal |
| US4678720A (en) * | 1985-01-04 | 1987-07-07 | Gte Laboratories Incorporated | Silver-copper-titanium brazing alloy |
-
1988
- 1988-04-04 EP EP19880904044 patent/EP0357664A4/en not_active Withdrawn
- 1988-04-04 JP JP63503567A patent/JP2825249B2/en not_active Expired - Lifetime
- 1988-04-04 WO PCT/US1988/001058 patent/WO1988007932A1/en not_active Ceased
Also Published As
| Publication number | Publication date |
|---|---|
| JP2825249B2 (en) | 1998-11-18 |
| WO1988007932A1 (en) | 1988-10-20 |
| JPH02502899A (en) | 1990-09-13 |
| EP0357664A4 (en) | 1991-05-22 |
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