WO2006104025A1 - ろう材、ろう付け用複合材およびそれらを用いてろう付け接合されたろう付け構造 - Google Patents
ろう材、ろう付け用複合材およびそれらを用いてろう付け接合されたろう付け構造 Download PDFInfo
- Publication number
- WO2006104025A1 WO2006104025A1 PCT/JP2006/305914 JP2006305914W WO2006104025A1 WO 2006104025 A1 WO2006104025 A1 WO 2006104025A1 JP 2006305914 W JP2006305914 W JP 2006305914W WO 2006104025 A1 WO2006104025 A1 WO 2006104025A1
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- Prior art keywords
- layer
- brazing
- mass
- alloy
- pure
- Prior art date
Links
- 238000005219 brazing Methods 0.000 title claims abstract description 652
- 239000000463 material Substances 0.000 title claims abstract description 222
- 239000000945 filler Substances 0.000 title claims abstract description 45
- 239000002131 composite material Substances 0.000 title claims description 41
- 229910018487 Ni—Cr Inorganic materials 0.000 claims abstract description 223
- 229910045601 alloy Inorganic materials 0.000 claims abstract description 223
- 239000000956 alloy Substances 0.000 claims abstract description 223
- 229910000990 Ni alloy Inorganic materials 0.000 claims abstract description 23
- 229910001069 Ti alloy Inorganic materials 0.000 claims abstract description 12
- 229910052759 nickel Inorganic materials 0.000 claims description 74
- 229910052719 titanium Inorganic materials 0.000 claims description 53
- 239000002184 metal Substances 0.000 claims description 45
- 229910052751 metal Inorganic materials 0.000 claims description 45
- 229910052750 molybdenum Inorganic materials 0.000 claims description 38
- 238000005304 joining Methods 0.000 claims description 27
- 239000000758 substrate Substances 0.000 claims description 14
- 229910000831 Steel Inorganic materials 0.000 claims description 7
- 239000010959 steel Substances 0.000 claims description 7
- 230000007704 transition Effects 0.000 claims 1
- 238000007254 oxidation reaction Methods 0.000 abstract description 61
- 230000003647 oxidation Effects 0.000 abstract description 60
- 238000005260 corrosion Methods 0.000 abstract description 17
- 230000007797 corrosion Effects 0.000 abstract description 17
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 441
- 238000006243 chemical reaction Methods 0.000 description 155
- 239000000203 mixture Substances 0.000 description 87
- 239000002253 acid Substances 0.000 description 56
- 230000000052 comparative effect Effects 0.000 description 44
- 230000005496 eutectics Effects 0.000 description 44
- 238000012360 testing method Methods 0.000 description 34
- 229910000599 Cr alloy Inorganic materials 0.000 description 33
- KHYBPSFKEHXSLX-UHFFFAOYSA-N iminotitanium Chemical compound [Ti]=N KHYBPSFKEHXSLX-UHFFFAOYSA-N 0.000 description 32
- 239000007791 liquid phase Substances 0.000 description 28
- 238000005096 rolling process Methods 0.000 description 28
- 229910004337 Ti-Ni Inorganic materials 0.000 description 27
- 229910011209 Ti—Ni Inorganic materials 0.000 description 27
- 229910052804 chromium Inorganic materials 0.000 description 26
- 238000000137 annealing Methods 0.000 description 25
- 238000000034 method Methods 0.000 description 20
- 229910001220 stainless steel Inorganic materials 0.000 description 20
- 239000010935 stainless steel Substances 0.000 description 16
- 239000007789 gas Substances 0.000 description 11
- 238000002474 experimental method Methods 0.000 description 10
- 239000007788 liquid Substances 0.000 description 10
- 230000015572 biosynthetic process Effects 0.000 description 9
- 230000002829 reductive effect Effects 0.000 description 9
- 230000000694 effects Effects 0.000 description 8
- 238000004519 manufacturing process Methods 0.000 description 8
- 239000002994 raw material Substances 0.000 description 8
- 229910000765 intermetallic Inorganic materials 0.000 description 7
- 239000012071 phase Substances 0.000 description 7
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 7
- 230000007423 decrease Effects 0.000 description 6
- 238000009792 diffusion process Methods 0.000 description 6
- 239000007790 solid phase Substances 0.000 description 6
- 238000003466 welding Methods 0.000 description 6
- 239000011230 binding agent Substances 0.000 description 5
- 229910001000 nickel titanium Inorganic materials 0.000 description 5
- 229910019589 Cr—Fe Inorganic materials 0.000 description 4
- 229910010380 TiNi Inorganic materials 0.000 description 4
- 239000012300 argon atmosphere Substances 0.000 description 4
- 229910000963 austenitic stainless steel Inorganic materials 0.000 description 4
- 238000010586 diagram Methods 0.000 description 4
- 239000011261 inert gas Substances 0.000 description 4
- 239000000155 melt Substances 0.000 description 4
- 230000002093 peripheral effect Effects 0.000 description 4
- 238000007712 rapid solidification Methods 0.000 description 4
- 229910000601 superalloy Inorganic materials 0.000 description 4
- 229910052720 vanadium Inorganic materials 0.000 description 4
- 229910018054 Ni-Cu Inorganic materials 0.000 description 3
- 229910018481 Ni—Cu Inorganic materials 0.000 description 3
- 229910010169 TiCr Inorganic materials 0.000 description 3
- GWEVSGVZZGPLCZ-UHFFFAOYSA-N Titan oxide Chemical compound O=[Ti]=O GWEVSGVZZGPLCZ-UHFFFAOYSA-N 0.000 description 3
- 229910052782 aluminium Inorganic materials 0.000 description 3
- 238000010438 heat treatment Methods 0.000 description 3
- 150000002739 metals Chemical class 0.000 description 3
- 238000002156 mixing Methods 0.000 description 3
- 229910052710 silicon Inorganic materials 0.000 description 3
- 239000007787 solid Substances 0.000 description 3
- 229910052726 zirconium Inorganic materials 0.000 description 3
- 238000004458 analytical method Methods 0.000 description 2
- 230000003247 decreasing effect Effects 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 238000011156 evaluation Methods 0.000 description 2
- 230000008018 melting Effects 0.000 description 2
- 238000002844 melting Methods 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 238000005498 polishing Methods 0.000 description 2
- 238000002360 preparation method Methods 0.000 description 2
- 239000011347 resin Substances 0.000 description 2
- 229920005989 resin Polymers 0.000 description 2
- 239000012298 atmosphere Substances 0.000 description 1
- 229910052802 copper Inorganic materials 0.000 description 1
- 239000013078 crystal Substances 0.000 description 1
- 238000010894 electron beam technology Methods 0.000 description 1
- 238000004453 electron probe microanalysis Methods 0.000 description 1
- 230000007613 environmental effect Effects 0.000 description 1
- 239000012065 filter cake Substances 0.000 description 1
- 239000012530 fluid Substances 0.000 description 1
- 239000000446 fuel Substances 0.000 description 1
- 229910000856 hastalloy Inorganic materials 0.000 description 1
- 230000020169 heat generation Effects 0.000 description 1
- 229910001026 inconel Inorganic materials 0.000 description 1
- 230000002401 inhibitory effect Effects 0.000 description 1
- 230000002452 interceptive effect Effects 0.000 description 1
- 229910052748 manganese Inorganic materials 0.000 description 1
- 238000004452 microanalysis Methods 0.000 description 1
- 230000001151 other effect Effects 0.000 description 1
- 239000000843 powder Substances 0.000 description 1
- 238000005476 soldering Methods 0.000 description 1
- 238000012546 transfer Methods 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B15/00—Layered products comprising a layer of metal
-
- 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
- B23K35/3033—Ni as the principal constituent
-
- 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
- B23K35/3033—Ni as the principal constituent
- B23K35/304—Ni as the principal constituent with Cr as the next major constituent
-
- 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
- B23K35/32—Selection of soldering or welding materials proper with the principal constituent melting at more than 1550 degrees C
- B23K35/325—Ti as the principal constituent
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B15/00—Layered products comprising a layer of metal
- B32B15/04—Layered products comprising a layer of metal comprising metal as the main or only constituent of a layer, which is next to another layer of the same or of a different material
- B32B15/043—Layered products comprising a layer of metal comprising metal as the main or only constituent of a layer, which is next to another layer of the same or of a different material of metal
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B15/00—Layered products comprising a layer of metal
- B32B15/18—Layered products comprising a layer of metal comprising iron or steel
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B3/00—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form
- B32B3/26—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form characterised by a particular shape of the outline of the cross-section of a continuous layer; characterised by a layer with cavities or internal voids ; characterised by an apertured layer
- B32B3/28—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form characterised by a particular shape of the outline of the cross-section of a continuous layer; characterised by a layer with cavities or internal voids ; characterised by an apertured layer characterised by a layer comprising a deformed thin sheet, i.e. the layer having its entire thickness deformed out of the plane, e.g. corrugated, crumpled
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C14/00—Alloys based on titanium
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C19/00—Alloys based on nickel or cobalt
- C22C19/03—Alloys based on nickel or cobalt based on nickel
- C22C19/05—Alloys based on nickel or cobalt based on nickel with chromium
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F28—HEAT EXCHANGE IN GENERAL
- F28F—DETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
- F28F21/00—Constructions of heat-exchange apparatus characterised by the selection of particular materials
- F28F21/08—Constructions of heat-exchange apparatus characterised by the selection of particular materials of metal
- F28F21/089—Coatings, claddings or bonding layers made from metals or metal alloys
-
- 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
- B23K2101/00—Articles made by soldering, welding or cutting
- B23K2101/04—Tubular or hollow articles
- B23K2101/14—Heat exchangers
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2255/00—Coating on the layer surface
- B32B2255/06—Coating on the layer surface on metal layer
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2255/00—Coating on the layer surface
- B32B2255/20—Inorganic coating
- B32B2255/205—Metallic coating
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2255/00—Coating on the layer surface
- B32B2255/28—Multiple coating on one surface
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2307/00—Properties of the layers or laminate
- B32B2307/70—Other properties
- B32B2307/714—Inert, i.e. inert to chemical degradation, corrosion
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F28—HEAT EXCHANGE IN GENERAL
- F28D—HEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT
- F28D9/00—Heat-exchange apparatus having stationary plate-like or laminated conduit assemblies for both heat-exchange media, the media being in contact with different sides of a conduit wall
- F28D9/0062—Heat-exchange apparatus having stationary plate-like or laminated conduit assemblies for both heat-exchange media, the media being in contact with different sides of a conduit wall the conduits for one heat-exchange medium being formed by spaced plates with inserted elements
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F28—HEAT EXCHANGE IN GENERAL
- F28F—DETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
- F28F3/00—Plate-like or laminated elements; Assemblies of plate-like or laminated elements
- F28F3/02—Elements or assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with recesses, with corrugations
- F28F3/025—Elements or assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with recesses, with corrugations the means being corrugated, plate-like elements
-
- Y—GENERAL 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/12—All metal or with adjacent metals
- Y10T428/12493—Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.]
- Y10T428/12771—Transition metal-base component
- Y10T428/12806—Refractory [Group IVB, VB, or VIB] metal-base component
-
- Y—GENERAL 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/12—All metal or with adjacent metals
- Y10T428/12493—Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.]
- Y10T428/12771—Transition metal-base component
- Y10T428/12861—Group VIII or IB metal-base component
- Y10T428/12937—Co- or Ni-base component next to Fe-base component
-
- Y—GENERAL 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/12—All metal or with adjacent metals
- Y10T428/12493—Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.]
- Y10T428/12771—Transition metal-base component
- Y10T428/12861—Group VIII or IB metal-base component
- Y10T428/12944—Ni-base component
-
- Y—GENERAL 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/12—All metal or with adjacent metals
- Y10T428/12493—Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.]
- Y10T428/12771—Transition metal-base component
- Y10T428/12861—Group VIII or IB metal-base component
- Y10T428/12951—Fe-base component
- Y10T428/12972—Containing 0.01-1.7% carbon [i.e., steel]
- Y10T428/12979—Containing more than 10% nonferrous elements [e.g., high alloy, stainless]
Definitions
- brazing material, brazing composite material, and brazing structure brazed and bonded using them
- the present invention relates to a brazing material, a brazing composite material, and a brazing structure that is brazed and joined using the brazing material, and more particularly, a filter material that forms a heat exchange channel such as a radiator or a gas cooler,
- the present invention relates to a brazing composite material and a brazing structure brazed and bonded using the composite material.
- a brazing material composed of a laminated structure of an Mn-based metal layer and an Ni-based metal layer that also has an Mn-Ni-Cu alloy force by using rolling joining without using the liquid rapid solidification method described above.
- a technology for brazing stainless steel using the brazing material has been proposed.
- Such a technique is disclosed in, for example, International Publication No. WOOOZ18537.
- the Mn—Ni—Cu alloy contains Cr, Ti, etc. in a total amount of 5% by mass or less. Improves acid resistance.
- the Mn-Ni-Cu alloy constituting a part of the conventional brazing material disclosed in the above-mentioned International Publication No. WOOOZ18537 contains Mn and Cu having low corrosion resistance. Therefore, there is a problem that it is difficult to improve the corrosion resistance of the joint by brazing.
- the conventional Ti-Ni brazing material disclosed in the above-mentioned JP-A-2003-117678 has high corrosion resistance, while a Cr 2 O oxide film (
- the Ni-Cr-Fe corrosion-resistant and heat-resistant superalloys listed in JP-A-2003-117678 are also used as the Ni alloy. Is high (about 1800 ° C to about 2000 ° C), the reaction rate between the brazing material and the Ni-Cr-Fe corrosion-resistant heat-resistant superalloy during brazing becomes slow. As a result, the diffusion rate of Cr from the Ni—Cr—Fe-based corrosion-resistant heat-resistant superalloy to the brazed joint becomes slow, so there is a disadvantage that Cr is not sufficiently supplied to the brazed joint. As a result, a sufficient amount of Cr 2 O 3 oxide film (passive film) is not formed on the surface of the joint by brazing.
- the present invention has been made in order to solve the above-described problems.
- An object is to provide a brazed structure that is brazed and joined.
- the brazing material according to the first aspect of the present invention comprises a Ni-Cr brazing layer having a Ni-Cr alloy layer force and a Ti brazing layer having a Ti layer or Ti alloy layer force.
- Ni—Cr It consists of at least a three-layer structure with a brazing layer and a Ni brazing layer placed between the Ti brazing layer and a Ni brazing layer that also has Ni alloy layer strength.
- a brazing material is constituted by a Ni—Cr brazing layer, a Ti brazing layer, and a Ni brazing layer. Since Ti-Ni-Cr alloy is formed at the joint, the Cr O oxide film (
- Passive film can be formed. Thereby, it is possible to improve the acid resistance of the joint portion by brazing joint.
- a brazing material with a Ni-Cr brazing layer, a Ti brazing layer, and a Ni brazing layer, Ti, Ni, and Cr, which have high corrosion resistance, are included in the joint by brazing.
- the corrosion resistance of the joint by brazing can be improved.
- the Ni brazing layer between the Ni-Cr brazing layer and the Ti brazing layer, in the process of brazing and joining, the Ti contained in the Ti brazing layer and the Ni-Cr alloy layer It is possible to shorten the time when Cr contained in is mixed. This suppresses the formation of brittle TiCr due to the reaction between Ti contained in the Ti brazing layer and Cr contained in the Ni-Cr alloy layer. But
- the brazing material is layered by forming the brazing material with the Ni-Cr brazing layer, the Ti brazing layer, and the Ni brazing layer. It is possible to suppress the manufacturing process from becoming complicated.
- the brazing material is layered, a binder to be mixed is not necessary when a powdered brazing material is used. As a result, when brazing is performed using a layered brazing material, it is not necessary to remove the binder after brazing and joining, so that the manufacturing process can be simplified.
- the Cr content of the Ni—Cr brazing layer made of the Ni—Cr alloy layer is 20% by mass or more and 40% by mass or less.
- an oxide film (not having a sufficient thickness) of Cr 2 O is formed on the surface of the joint by brazing.
- the Ni brazing layer is preferable when the total amount of Ti in the Ti brazing layer and the amount of Ni in the Ni brazing layer is 100% by mass.
- the Ni content is 21.5% to 37.5% by mass.
- the amount of Ni in the Ni brazing layer is 28.
- the amount is around 3% by mass.
- the ratio t2Ztl between the thickness tl of the Ti brazing layer and the thickness t2 of the Ni brazing layer may be 1Z8 or more and 2Z7 or less.
- the thickness ratio between the Ti brazing layer and the Ni brazing layer is only set to 1Z8 or more and 2Z7 or less, and the temperature in the Ti brazing layer is about 1220 ° C or less, which does not require a special furnace.
- Ti and Ni in the Ni brazing layer can be melted, and it is possible to suppress the formation of brittle TiM intermetallic compounds at the joint by brazing.
- composition ratio (mass%) of Ti and Ni can be controlled.
- the ratio t2Ztl between the thickness tl of the Ti brazing layer and the thickness t2 of the Ni brazing layer may be substantially 1Z5.
- the amount of Ti in the Ti brazing layer and Ni brazing When the total amount of Ni in the layer is 100% by mass, the amount of Ni in the Ni brazing layer should be about 28.3% by mass, which is the eutectic composition at the initial stage of brazing. it can.
- a Ti—Ni alloy with a eutectic composition can be easily obtained at the initial stage of brazing simply by setting the thickness ratio between the Ti brazing layer and the Ni brazing layer to 1Z5.
- the Ti brazing layer is composed of a first ITi brazing layer made of the first ITi layer or the second ITi alloy layer, and a second Ti brazing made of the second Ti layer or the second Ti alloy layer.
- the Ni brazing layer includes an INi brazing layer made of the INi layer or the INi alloy layer, and a second Ni brazing layer that also has the second Ni layer or the second Ni alloy layer force.
- the INi brazing layer is disposed between the brazing layer and the first ITi brazing layer, and the second Ni brazing layer is disposed between the Ni-Cr brazing layer and the second Ti brazing layer. It may be made of a five-layer structure in which is placed.
- the portion in contact with the member to be brazed is the ITi layer (second Ti layer) or the ITi alloy layer (first layer). 2Ti alloy layer).
- At least one of the Ni—Cr brazing layer, the Ti brazing layer, and the Ni brazing layer is Mo or Co. Contains at least one of the following.
- the acid resistance of the joint portion by brazing joint can be further improved.
- the brazing material containing at least one of Mo and Co preferably, at least one of a Ni—Cr brazing layer, a Ti brazing layer, and a Ni brazing layer
- the total Mo content in is 2.0% by mass or more and 4.5% by mass or less. If comprised in this way, the oxidation resistance of a junction part can be fully and effectively improved.
- the brazing material containing at least one of Mo and Co preferably, at least one of a Ni—Cr brazing layer, a Ti brazing layer, and a Ni brazing layer 1
- the total Co content in one layer is 2.0% by mass or more and 10.0% by mass or less. If comprised in this way, the oxidation resistance of a junction part can be fully and effectively improved.
- a brazing composite material includes a substrate formed of steel, a Ni-Cr brazing layer that is rolled and joined to the surface of the substrate and has Ni-Cr alloy layer strength, At least three-layer structure of Ti brazing layer with Ti layer or Ti alloy layer force and Ni brazing layer with Ni layer or Ni alloy layer force between Ni-Cr brazing layer and Ti brazing layer It is equipped with brazing material that also has strength.
- a brazing material comprising a Ni-Cr brazing layer, a Ti brazing layer, and a Ni brazing layer is provided. Since a Ti—Ni—Cr alloy is formed at the joint by brazing, a Cr 2 O oxide film (passive film) can be easily formed on the surface of the joint. As a result,
- the corrosion resistance of the joint by brazing can be improved.
- the Ni brazing layer between the Ni-Cr brazing layer and the Ti brazing layer, the Ti brazing layer and Ni contained in the Ti brazing layer can be used during the brazing process.
- the time for mixing with Cr contained in the Cr alloy layer can be shortened. As a result, it is possible to suppress the formation of brittle TiCr due to the reaction between Ti contained in the Ti brazing layer and Cr contained in the Ni-Cr alloy layer.
- a brazing composite material by rolling and bonding a layered brazing material having a structural force of at least three layers of a Ni-Cr brazing layer, a Ti brazing layer, and a Ni brazing layer to a substrate.
- a powdery brazing material formed by a liquid rapid solidification method it is possible to suppress the complexity of the brazing material manufacturing process. Thereby, it is possible to prevent the manufacturing process of the brazing composite material from being complicated.
- the brazing material is layered, a noinder to be mixed is not necessary when a powdered brazing material is used. This eliminates the need to remove the binder after brazing and joining when brazing using a layered brazing material. Therefore, the manufacturing process can be simplified.
- the Cr content of the Ni-Cr brazing layer made of the Ni-Cr alloy layer is 20 mass% or more and 40 mass% or less.
- the Cr content of the Ni-Cr alloy layer is set to 20% by mass or more, a sufficiently thick Cr 2 O force can be applied to the surface of the joint by brazing.
- the brazing composite material according to the second aspect preferably, when the total amount of Ti in the Ti brazing layer and the amount of Ni in the Ni brazing layer is 100% by mass, Ni The amount of Ni in the brazing layer is 21.5 mass% or more and 37.5 mass% or less. With this configuration, by making the amount of Ni in the Ni brazing layer 21.5% by mass or more, Ti in the Ti brazing layer and the Ni brazing layer at a temperature of about 1220 ° C or less. Ni and can be melted. This makes it possible to melt Ti in the Ti brazing layer and Ni in the Ni brazing layer without using a special furnace that outputs a high temperature of about 1220 ° C or higher. Also, by making the Ni content in the Ni brazing layer 37.5% by mass or less, unlike the case where the Ni content is larger than 37.5% by mass, Ti N is also formed in the joint by brazing. Inhibiting the formation of intermetallic compounds
- the amount of Ni in the Ni brazing layer is 28.
- the amount is around 3% by mass.
- the ratio t2Ztl between the thickness tl of the Ti brazing layer and the thickness t2 of the Ni brazing layer is 1Z8 or more and 2Z7 or less.
- the amount of Ni in the Ni brazing layer relative to the amount of Ti in the Ti brazing layer can be 21.5 mass% or more and 37.5 mass% or less.
- the thickness ratio between the Ti brazing layer and the Ni brazing layer is simply set to 1Z8 or more and 2Z7 or less, and the Ti brazing layer does not require a special furnace at a temperature of about 1220 ° C or less.
- Ti and Ni in the Ni brazing layer can be melted, and an intermetallic compound consisting of brittle Ti Ni is formed at the joint by brazing
- It can be the composition (mass 0/0) ratio between Ti and Ni, which can be inhibited.
- the ratio t2Ztl between the thickness tl of the Ti brazing layer and the thickness t2 of the Ni brazing layer may be substantially 1Z5.
- the amount of Ni in the Ni brazing layer is The amount can be in the vicinity of 28.3% by mass which is the eutectic composition in the initial stage.
- a Ti—Ni alloy with a eutectic composition can be easily obtained at the initial stage of brazing simply by setting the thickness ratio between the Ti brazing layer and the Ni brazing layer to 1Z5.
- At least one of the Ni—Cr brazing layer, the Ti brazing layer, and the Ni brazing layer is Mo. Or at least one of Co.
- the brazing material preferably contains 2.0 mass% or more and 4.5 mass% or less Mo. If comprised in this way, the oxidation resistance of a junction part can be improved sufficiently and effectively.
- the brazing material preferably contains 2.0 mass% or more and 10.0 mass% or less of Co. If comprised in this way, the oxidation resistance of a junction part can be improved sufficiently and effectively.
- a brazing structure includes a substrate formed of steel, a Ni-Cr brazing layer, a Ti layer, which is rolled and joined to the surface of the substrate and is a Ni-Cr alloy layer. Or Ti brazing layer with Ti alloy layer force, and arranged between Ni-Cr brazing layer and Ti brazing layer It is preferably formed by brazing and joining using a brazing composite material having a brazing material having at least three layers of structural strength of a Ni brazing layer that also has Ni layer or Ni alloy layer strength.
- At least a brazed joint portion includes a Ti—Ni—Cr alloy.
- a CrO oxide film passive film
- the brazed joint contains Ti, Ni, and Cr, which have high corrosion resistance. It can be improved.
- the Ti-Ni-Cr alloy preferably, when the total amount of Ti and Ni in the Ti-Ni-Cr alloy is 100% by mass, the Ti Ni-Cr alloy The amount of Ni in the steel is 59.5 mass% or more and 70.0 mass% or less.
- the Ti—Ni—Cr alloy can be melted at a temperature of about 1220 ° C. or less.
- the brazing structure of the third aspect can be formed without using a special furnace that outputs a high temperature of about 1220 ° C or higher.
- the Ni content in the Ti-Ni-Cr alloy is around 64.4% by mass. Is the amount.
- a Ti-Ni alloy with a eutectic composition can be obtained in the brazed Ti-Ni-Cr alloy. Therefore, at the eutectic temperature of Ti-Ni alloy of 1110 ° C, Ti and Ni in the Ti-Ni-Cr alloy, which is in the liquid phase, can be changed to the solid phase without going through the state of solid-liquid coexistence.
- solid Ti can be easily formed by lowering the temperature of the Ti—Ni—Cr alloy below the eutectic temperature of 1110 ° C.
- the solid-liquid coexistence state does not exist in the process of brazing and joining, unlike the case where the Ti-Ni-Cr alloy coexists with the solid-liquid coexistence state. It can suppress that it falls.
- the brazing material having a Ti—Ni—Cr alloy strength can easily flow into the joint.
- the brazed structure according to the third aspect preferably 1 ⁇ 0: 0: The content is 11% by mass or more.
- a sufficient amount of Cr is contained in the Ti-Ni-Cr alloy, so a Cr O oxide film (passive film) having a sufficient thickness on the surface of the brazed joint portion. Can be generated. This was brazed and joined
- the acid resistance of the portion can be further improved.
- the brazed portion preferably contains at least one of Mo and Co.
- the brazed joint portion contains at least one of Mo and Co
- the brazed joint portion is 2.0 mass% or more and 4.5 mass%. Contains the following Mo. If comprised in this way, the oxidation resistance of a junction part can be improved sufficiently and effectively.
- the brazed part contains at least one of Mo and Co
- the brazed part is preferably 2.0% by mass or more and 10.0% by mass or less. Contains Co. If comprised in this way, the oxidation resistance of a junction part can be improved sufficiently and effectively.
- FIG. 1 is a cross-sectional view showing a configuration of a brazing material according to a first embodiment of the present invention.
- FIG. 2 is a cross-sectional view partially showing a heat exchanger formed using the brazing material according to the first embodiment shown in FIG.
- FIG. 3 is an enlarged cross-sectional view showing a joint portion of the heat exchanger according to the first embodiment shown in FIG. 2.
- FIG. 4 A state diagram of a Ni—Ti based alloy.
- FIG. 5 is a schematic diagram for explaining a eutectic reaction of the brazing material according to the first embodiment shown in FIG. 1.
- FIG. 6 is a schematic diagram for explaining the eutectic reaction of the brazing material according to the first embodiment shown in FIG. 1.
- FIG. 7 is a schematic diagram for explaining the eutectic reaction of the brazing material according to the first embodiment shown in FIG. 1.
- FIG. 8 is a cross-sectional view for explaining a brazing joining process when forming the heat exchanger according to the first embodiment shown in FIG. 2.
- FIG. 9 is a cross-sectional view for explaining a brazing joining process when forming the heat exchanger according to the first embodiment shown in FIG. 2.
- FIG. 10 is a cross-sectional view showing a configuration of a brazing composite material according to a second embodiment of the present invention.
- FIG. 11 is a cross-sectional view for explaining the process of brazing and joining when forming heat exchange according to the second embodiment shown in FIG. 10.
- FIG. 12 is a cross-sectional view for explaining the process of brazing and joining when forming the heat exchange according to the second embodiment shown in FIG.
- FIG. 13 is a cross-sectional view showing a configuration of a brazing material according to a third embodiment of the present invention.
- FIG. 14 is a cross-sectional view partially showing a heat exchange formed using the brazing material according to the third embodiment shown in FIG. 13.
- FIG. 15 is a cross-sectional view showing a configuration of a brazing composite material according to a fourth embodiment of the present invention.
- FIG. 16 is a cross-sectional view showing the structure of a brazing composite material according to a modification of the present invention.
- the brazing material 1 includes a Ni—Cr alloy layer 2, a Ti layer 3 a disposed on one side of the Ni—Cr alloy layer 2, and a Ni Cr alloy.
- Ti layer 3b disposed on the other side of layer 2, Ni layer 4a disposed between Ni—Cr alloy layer 2 and Ti layer 3a, and between Ni—Cr alloy layer 2 and Ti layer 3b And a Ni layer 4b.
- the Ni layers 4a and 4b are roll-bonded to the Ni—Cr alloy layer 2.
- the Ti layers 3a and 3b are roll-bonded to Ni layers 4a and 4b that are roll-bonded to the Ni—Cr alloy layer 2.
- the rolling joining for example, hot welding, cold welding, vacuum welding, or the like can be used.
- Ni— The Cr alloy layer 2 is an example of the “Ni—Cr brazing layer” in the present invention.
- the Ti layer 3a is an example of the “Ti brazing layer” and “ITi brazing layer” of the present invention, and the Ti layer 3b is the “Ti brazing layer” and “second Ti brazing layer” of the present invention. It is an example of a “layer”.
- the Ni layer 4a is an example of the “Ni brazing layer” and “INi brazing layer” of the present invention, and the Ni layer 4b is the “Ni brazing layer” and “second Ni brazing layer” of the present invention. It is an example of a “layer”.
- the Ni-Cr alloy layer 2 is composed only of Ni and Cr.
- the Cr content of this Ni—Cr alloy layer 2 is about 20 mass% or more and about 40 mass% or less.
- Ti layers 3a and 3b are composed of pure Ti only. Further, each of the Ti layers 3a and 3b has a thickness of tl.
- the Ni layers 4a and 4b are also composed of pure Ni only. Each of the Ni layers 4a and 4b has a thickness of t2.
- the amount of Ni in the Ni layer 4a when the total amount of Ti in the Ti layer 3a and the amount of Ni in the Ni layer 4a is 100 mass%, the amount of Ni in the Ni layer 4a is 21. 5 mass% or more and 37.5 mass% or less, and preferably about 28.3 mass%, which is the eutectic composition of the TiNi alloy in the initial stage of brazing.
- the amount of Ni in the Ni layer 4b when the total amount of Ti in the Ti layer 3b and the amount of Ni in the Ni layer 4b is 100% by mass, the amount of Ni in the Ni layer 4b is 21.5% by mass or more and 37.5% by mass or less.
- it is about 28.3 mass% which becomes the eutectic composition of the TiNi alloy in the initial stage of brazing.
- the ratio t2Ztl between the thickness tl of the Ti layers 3a and 3b and the thickness t2 of the Ni layers 4a and 4b is 1 Z8 or more and 2Z7 or less, and preferably about
- the heat exchange lOO formed using the brazing filler metal 1 according to the first embodiment includes a pair of plates 11 formed of stainless steel and six waves formed of stainless steel as shown in FIG.
- a fin 12 having a shape and five plates 13 formed of stainless steel are provided.
- the plate 13 is an example of the “substrate” in the present invention.
- As stainless steel SUS410 and SUS430, which are ferritic stainless steels, SUS304 and SUS316, which are austenitic stainless steels, and the like can be used.
- the pair of plates 11 constitutes the outer frame of the heat exchanger 100. Also 6 fins 12 and 5 The plates 13 are arranged so as to be alternately stacked between the pair of plates 11.
- the inside of the heat exchanger ⁇ 100 is divided into six layers by five plates 13, and the exhaust gas and water flow alternately every other layer in the six layers.
- the fins 12 are provided to slow down the flow rates of exhaust gas and water flowing through the six layers.
- the heat exchange ⁇ 100 includes a Ti—Ni—Cr alloy la formed by brazing and joining described later between the fins 12 and the plates 13 and 11. Yes. That is, a plate 13 and a pair of Ti—Ni—Cr alloy la are formed between adjacent fins 12, and a Ti—Ni—Cr alloy la is formed between plate 11 and fins 12. Is formed. As shown in FIG. 3, this Ti—Ni—Cr alloy la has a function for joining the outer peripheral surface of the bent portion of the fin 12 to the plates 13 and 11 (see FIG. 2). The content of Cr in the Ti—Ni—Cr alloy la is about 11% by mass or more.
- the amount of Ni in the Ti Ni—Cr alloy la is 59.5% by mass or more and 70.0%. It is about 64.4% by mass or less, which is the eutectic composition of the Ti—Ni alloy in the Ti Ni—Cr alloy la after brazing.
- the temperature of the exhaust gas flowing inside the heat exchanger 100 is about 700 ° C.
- the eutectic reaction used when forming the heat exchanger 100 by the brazing material 1 of the first embodiment will be described with reference to FIGS.
- the eutectic reaction is a reaction in which two or more types of solid phases are simultaneously precipitated and solidified or melted when two or more types of alloys are cooled from a molten state or melted from a solid state.
- the temperatures of the eutectic points of the Ni-Ti alloy after brazing and after brazing are about 955 ° C and about 1110 ° C, respectively, as shown in Fig. 4.
- the eutectic composition el of the Ni-Ti alloy at about 955 ° C in the initial stage of brazing is about 28.3 mass% Ni about 71.7 mass% Ti, and about 11 10 after brazing.
- the eutectic composition e2 of Ni-Ti alloy at ° C is about 64.4 wt% Ni about 35.6 wt% Ti. In the initial stage of brazing, it melts at a temperature of about 1220 ° C or less, and The composition range in which an intermetallic compound composed of Ti Ni does not occur is about 21.5 mass% Ni—about 78.5
- the composition range of the melting in the following state for about 1220 ° C is about 59.5 weight 0 / ONi- about 40.5 weight 0/0 Ti (be2) ⁇ about 70.0 weight 0 / it has been shown that 0 Ni- about 30.0 weight 0/0 (ae2). That is, in the first embodiment, based on the range of bel to ael including the eutectic composition el of the Ti—Ni alloy at the initial stage of brazing, 1 amount in Tifi3a (3b) and?
- the total amount of Ni in the Ni layer 4a (4b) when the total amount of Ni is 100% by mass is about 21.5% to 37.5% by mass. Also, based on the range of be2 to ae2 including the eutectic composition e2 of Ti-Ni alloy in Ti-Ni-Cr alloy la (see Fig. 2 and Fig. 3) after brazing! /, Ti Ni-
- Ti Ni- The amount of Ni in TiNi—Cr alloy 1a when the sum of the amount of Ti in Cr alloy 1a and the amount of Ni in TiNi—Cr alloy 1a is 100% by mass is approximately 59.5 as described above. More than mass% and less than 70.0 mass%.
- the principle of brazing according to the first embodiment is as follows: Ni—Cr alloy layer 2 shown in FIG. 5 and Ni layer 4a disposed on one side and the other side of Ni—Cr alloy layer 2 respectively. And 4b, and the brazing material that also acts as a force with the Ti layers 3a and 3b disposed on the outer surfaces of the Ni layers 4a and 4b, respectively, are heated to about 1220 ° C or less.
- Ti layer 3a (3b) and Ni layer 4a (4b) in the composition range of bel to ael (see Fig. 4) located on the surface side of the brazing material shown in Fig. 5 are used.
- the brazing material 1 (see Fig. 1) is placed between the plate 11 (see Fig. 2) and the fins 12 (see Fig. 2).
- the brazing material 1 is disposed between the fins 12 and the plate 13.
- the outer peripheral surface of the bent portion of the fin 12 is in contact with the Ti layer 3a constituting the brazing material 1, and the plate 13 and the Ti layer 3b constituting the brazing material 1 are in contact. From this state, it is heated for about 10 minutes at a temperature of about 1110 ° C. or more and about 1220 ° C. or less in an inert gas or vacuum.
- the 1 layer 3a (Ti layer 3b) and the Ni layer 4a (Ni Layer 4b) changes from the solid phase to the liquid phase to form a Ti-Ni liquid phase lb (see Fig. 6) (composition range: bel to ael (see Fig. 4)).
- the Ti-Ni liquid phase lb in the liquid phase reacts with the Ni-Cr alloy layer 2 to form a Ti-Ni-Cr liquid phase lc (with a composition range of be2 to a e2 (see Fig. 4)).
- Form Fig. 7 ).
- the temperature after brazing! ! ⁇ ⁇ ⁇ ⁇ !
- Li-phase When the temperature of ⁇ decreases, the Ti-Ni-Cr liquid phase lc is in the composition range from be2 to ae2 (see Fig. 4) from the liquid phase to the solid phase Ti-Ni-Cr alloy It changes to la (see Fig. 2 and Fig. 3). As a result, the outer peripheral surface of the bent portion of the fin 12 and the plates 13 and 11 are brazed and joined by the force Ti—Ni—Cr alloy la, so that the heat exchanger 100 shown in FIG. 2 is formed.
- a brazing material is constituted by the Ni—Cr alloy layer 2, the Ti layers 3a and 3b, and the Ni layers 4a and 4b.
- Ti—Ni — Cr alloy la is formed on the surface of the joint.
- the brazing material is constituted by the Ni-Cr alloy layer 2, the Ti layers 3a and 3b, and the Ni layers 4a and 4b, so that the joint portion by brazing is high. Since corrosion-resistant Ti, Ni and Cr are included, the corrosion resistance of the joint by brazing can be improved.
- the Ni layer 4a (Ni layer 4b) is disposed between the Ni—Cr alloy layer 2 and the Ti layer 3a (Ti layer 3b), thereby performing the brazing joint process.
- the time for mixing Ti contained in the Ti layers 3a and 3b and Cr contained in the Ni—Cr alloy layer 2 can be shortened.
- Ti contained in Ti layers 3a and 3b and Cr contained in Ni-Cr alloy layer 2 It is possible to suppress the formation of brittle TiCr by reacting with
- the amount in the Ni layers 4a and 4b is By setting the Ni content to 21.5 mass% or more, the Ti layers 3a and 3b and the Ni layers 4a and 4b can be melted at a temperature of about 1220 ° C or less. This makes it possible to melt Ti in the Ti layers 3a and 3b and Ni in the Ni layers 4a and 4b without using a special furnace that outputs a high temperature of about 1220 ° C or higher.
- the amount in the Ni layers 4a and 4b is By making the Ni content 37.5% by mass or less, unlike the case where the Ni content is larger than 37.5% by mass, an intermetallic compound consisting of Ti Ni is generated at the joint by brazing. Can be suppressed
- Ti Ni-Cr Ti-Ni alloy with eutectic composition e2 can be obtained in Ti-Ni-Cr alloy la after brazing by setting the amount of Ni in alloy la to about 64.4% by mass.
- the Ti-Ni-Cr liquid phase lc is transferred to the solid phase without interfering with the solid-liquid coexisting state.
- the Ti-Ni-Cr alloy la (see Fig. 2 and Fig.
- the temperature of the Ti-Ni-Cr liquid phase lc is lowered from the eutectic temperature of about 1110 ° C, so that it can be solidified uniformly.
- there is no solid-liquid coexistence state in the Ti Ni-Cr liquid phase lc so unlike the case where the Ti Ni-Cr liquid phase lc is in the solid-liquid coexistence state! ! - ⁇ -It is possible to suppress a decrease in the fluid wettability of the liquid phase.
- the brazing material 1 composed of the Ti—Ni—Cr liquid phase lc can be easily flowed to the joint.
- the first embodiment described above is used.
- a brazing composite material 50 in which a brazing material 51 having a three-layer structural force is roll-bonded to the substrate 13 will be described.
- the brazing composite material 50 according to the second embodiment of the present invention is rolled and joined to the plate 13 formed of stainless steel and one side and the other side of the plate 13. A pair of brazing materials 51!
- the pair of brazing materials 51 are the Ni-Cr alloy layer 2, the Ti layer 3, the Ni-Cr alloy layer 2 and the Ti layer that are roll-bonded to the plate 13, respectively. 3 layer structure with a Ni layer 4 disposed between them.
- the amount of Ni in Ni layer 4 is 21.5% by mass or more and 37.5% by mass or less.
- it is about 28.3 mass% which becomes the eutectic composition of the initial Ti—Ni alloy at the time of brazing.
- the brazing material 51 composed of the three-layer structure of the Ni—Cr alloy layer 2, the Ti layer 3, and the Ni layer 4 is rolled and joined to the plate 13, the Ti layer 3 and the Ni layer 4
- the eutectic reaction may occur in the vicinity of about 955 ° C (see Fig. 4), so the condition for rolling joining the brazing material 51 to the plate 13 is less than about 955 ° C.
- the brazing filler metal 51 is rolled and joined to the substrate 13 made of SUS304 or SUS316, which is an austenitic stainless steel, approximately 1050 ° to prevent sigma brittleness (brittle phenomenon) in the austenitic stainless steel. It is necessary to anneal at C or higher.
- the substrate 13 having a ferritic stainless steel strength such as SUS430 or SUS410.
- the brazing composite is brought into contact with the bent portion of the fin 12. Arrange material 50. Then, brazing and joining under the same conditions as in the first embodiment (heating in an inert gas or vacuum at a temperature of about 1110 ° C to about 1220 ° C for about 10 minutes) I do. At this time, as shown in FIG. 11 and FIG. 12, the Ti layer 3 and the Ni layer 4 constituting the brazing material 51 change to a solid phase force and a liquid phase state, and the composition range of bel to ael (see FIG. 4) Ti Ni liquid phase 51a is formed.
- the Ti Ni liquid phase 51a becomes Ni-Cr alloy layer 2 And Ti-Ni-Cr alloy la (see Fig. 2 and Fig. 3) in the composition range of be2 to ae2 (see Fig. 4) is formed.
- the temperature force eutectic point of the Ti—Ni—Cr alloy la reaches about 1110 ° C. (see FIG. 4)
- the Ti Ni—Cr alloy 1 a changes from a molten state to a solid state.
- the outer peripheral surface of the bent portion of the fin 12, the plates 11 and 13, and the force Ti—Ni—Cr alloy la are brazed to form a heat exchanger.
- Examples 1-9 and Comparative Example 1 were obtained by calculating and comparing the increase in the amount of acid in the reaction layer of the clad material according to Examples 1-9 and Comparative Examples 1-4 (joint part by brazing joint). The oxidation resistance of the reaction layer (joint part by brazing joint) of the clad material by ⁇ 4 was evaluated. This will be described in detail below.
- a Ni—Cr alloy layer containing 60 mass% Ni and 40 mass% Cr, a pure Ni layer, and a pure Ti layer were used as a brazing material.
- a pure Ni layer was rolled and joined to one side and the other side of the Ni—Cr alloy layer, respectively, and then subjected to diffusion annealing at a temperature of 800 ° C. for 1 minute in an argon atmosphere. Then, finish rolling and annealing were performed, and the thicknesses of the Ni-Cr alloy layer and the pure Ni layer were adjusted to 25.0 m and 2.1 m, respectively.
- the content (% by mass) of Ni in the pure Ni layer relative to the sum of Ti in the pure Ti layer before brazing and Ni in the pure Ni layer is the eutectic composition el (about 28.3
- the mass ratio of Ni in the Ti Ni—Cr alloy to the total of Ti and Ni in the brazed Ti Ni—Cr alloy is equal to the eutectic composition e2 (approximately 64.4 mass). %).
- the thickness of the Ni—Cr alloy layer, pure Ni layer, and pure Ti layer was adjusted to 23.4 / ⁇ ⁇ , 1.6 / zm, and 11.7 m by finish rolling and annealing. Except for the above, a brazing material according to Example 2 having a five-layer structure of pure Ti layer Z pure Ni layer / Ni Cr alloy layer Z pure Ni layer Z pure Ti layer was produced in the same manner as in Example 1 above. In this way, the content (% by mass) of Ni in the pure Ni layer relative to the sum of Ti in the pure Ti layer before brazing and Ni in the pure Ni layer is bel (about 21.5 mass 0). / 0 ), and the content of Ni in the Ti—Ni—Cr alloy (mass%) force e2 (approximately 59.5 mass%) relative to the sum of Ti and Ni in the Ti—Ni—Cr alloy after brazing ).
- the content (% by mass) of Ni in the Ti Ni—Cr alloy with respect to the total of Ti and Ni in the Ti—Ni—Cr alloy after brazing is ae2 (about 70.0% by mass) I tried to become.
- pure Ti before brazing And Ti in the layer with the content of Ni in the pure Ni layer to the total of Ni of pure Ni layer (wt%) is a el (about 37.5 weight 0/0), after brazing
- the content ratio (mass%) of Ni in the Ti—Ni—Cr alloy to the total of Ti and Ni in the Ti—Ni—Cr alloy was set to e2 (about 59.5 mass%).
- the content (% by mass) of Ni in the Ti Ni—Cr alloy with respect to the total of Ti and Ni in the Ti—Ni—Cr alloy after brazing is ae2 (about 70.0% by mass) I tried to become.
- a Ni-Cr alloy layer containing 80% by mass of Ni and 20% by mass of Cr is used, and by performing finish rolling and annealing, a Ni-Cr alloy layer, a pure Ni layer and The pure Ti layer and the pure Ni layer were the same as in Example 1 except that the thickness of each of the pure Ti layer was adjusted to 21.6 / ⁇ ⁇ , 2.4 m and 11.8 m.
- ZNi—Cr alloy layer Z pure Ni layer Z pure Ti layer A brazing material according to Example 6 having a five-layer structure was prepared.
- the content (% by mass) of Ni in the pure Ni layer relative to the sum of Ti in the pure Ti layer before brazing and Ni in the pure Ni layer is the eutectic composition el (about 28. 3% by mass), and the content (% by mass) of Ni in the Ti Ni—Cr alloy with respect to the sum of Ti and Ni in the Ti—Ni—Cr alloy after brazing is the eutectic composition e2 (about 64%). 4% by mass).
- a Ni-Cr alloy layer containing 80% by mass of Ni and 20% by mass of Cr is used, and by performing finish rolling and annealing, a Ni-Cr alloy layer, a pure Ni layer and And pure Ti layer, respectively, except that the thickness of each of the pure Ti layer was adjusted to 20.6 / ⁇ ⁇ , 1.8 / zm and 12.9 m.
- Layer ZNi—Cr alloy layer Z Pure Ni layer Z A brazing material according to Example 7 having a five-layer structure of pure Ti layers was produced.
- the Ni content of the pure Ni layer to the total of Ni of pure Ni layer (mass 0/0) bel (about 21.5 mass 0/0), while the content of Ni in the Ti Ni- Cr alloy with respect to the sum of Ti and Ni in the Ti- Ni- Cr alloys after brazing (mass%) of be2 (about 59.5 mass %).
- a Ni-Cr alloy layer containing 80% by mass of Ni and 20% by mass of Cr is used, and by performing finish rolling and annealing, a Ni-Cr alloy layer, a pure Ni layer and Pure Ti layer Z Pure Ni layer ZNi— Similar to Example 1 except that the thickness of each of the pure Ti layer was adjusted to 26.6 m, 1.4 m and 10.3 m.
- a brazing material according to Example 8 having a five-layer structure of Cr alloy layer Z pure Ni layer Z pure Ti layer was produced.
- the Ni content of the pure Ni layer to the total of Ni of pure Ni layer bel (about 21.5 mass 0/0), while the content of Ni in the Ti Ni- Cr alloy with respect to the sum of Ti and Ni in the Ti- Ni- Cr alloys after brazing (mass%) of ae2 (about 70.0 mass %).
- a Ni-Cr alloy layer containing 80% by mass of Ni and 20% by mass of Cr is used, and by performing finish rolling and annealing, a Ni-Cr alloy layer, a pure Ni layer and Pure Ti layer Z Pure Ni layer ZNi— Similar to Example 1 except that the thickness of each of the pure Ti layer was adjusted to 23.2 m, 2.9 m and 10.5 m.
- a brazing material according to Example 9 having a five-layer structure of Cr alloy layer Z pure Ni layer Z pure Ti layer was produced. In this way, the Ni content (mass%) in the pure Ni layer relative to the total of Ti in the pure Ti layer before brazing and Ni in the pure Ni layer is ael (approximately 37.5% by mass). ) And the content (% by mass) of Ni in the Ti Ni—Cr alloy with respect to the total of Ti and Ni in the Ti—Ni—Cr alloy after brazing becomes ae2 (about 70.0% by mass). I did it.
- a Ni-Cr alloy layer containing 80% by mass of Ni and 20% by mass of Cr is used, and finish rolling and annealing are performed.
- Pure Ti layer Z Pure Ni layer / Ni Cr In the same manner as in Example 1 except that the thickness of each i layer was adjusted to 16.4 / ⁇ ⁇ , 3.7 m and 13.1 m. Alloy layer Z pure Ni layer A brazing material according to Comparative Example 1 having a five-layer structure of Z pure Ti layer was prepared.
- the content (% by mass) of Ni in the pure Ni layer relative to the total of Ti in the pure Ti layer before brazing and Ni in the pure Ni layer is ael (approximately 37.5% by mass) together it becomes, the content of Ni in the Ti Ni- Cr alloys to the sum of Ti and Ni in the Ti- Ni- Cr alloys after brazing (mass 0/0) force e2 (about 59.5 mass %).
- a Ni-Cr alloy layer containing 60% by mass of Ni and 40% by mass of Cr is used, and by finish rolling and annealing, a Ni-Cr alloy layer, a Ni layer, and Ti Pure Ti layer Z Pure Ni layer / Ni Cr alloy layer Z As in Example 1 above, except that the thickness of each layer was adjusted to 27.4 / ⁇ ⁇ , 1. and 10.1 m.
- a brazing material according to Comparative Example 2 having a five-layer structure of a pure Ni layer and a Z pure Ti layer was produced.
- the content (% by mass) of Ni in the pure Ni layer with respect to the sum of Ti in the pure Ti layer before brazing and Ni in the pure Ni layer is bel (about 21.5% by mass).
- the content (% by mass) of Ni in the Ti—Ni—Cr alloy with respect to the sum of Ti and Ni in the Ti—Ni—Cr alloy after brazing is equal to the eutectic composition e 2 (about 64.4). Mass%).
- a Ni-Cr alloy layer containing 60% by mass of Ni and 40% by mass of Cr is used, and by finish rolling and annealing, a Ni-Cr alloy layer, a Ni layer, and Ti Pure Ti layer Z Pure Ni layer / Ni Cr alloy In the same manner as in Example 1 except that the thickness of each layer was adjusted to 30.8 / ⁇ ⁇ , 1.6 m and 8.0 m.
- Layer Z pure Ni layer A brazing material according to Comparative Example 3 having a five-layer structure of Z pure Ti layer was produced.
- the content (% by mass) of Ni in the pure Ni layer relative to the sum of Ti in the pure Ti layer before brazing and Ni in the pure Ni layer is equal to the eutectic composition el (about 28.3 Mass%), and the content (% by mass) of Ni in the Ti—Ni—Cr alloy with respect to the sum of Ti and Ni in the Ti—Ni—Cr alloy after brazing is ae2 (about 70.0% by mass). ) To be bigger.
- the content (% by mass) of Ni in the pure Ni layer relative to the sum of Ti in the pure Ti layer before brazing and Ni in the pure Ni layer is equal to the eutectic composition el (about 28.3 %), And the content of Ni in the Ti-Ni-Cr alloy (mass./.) Force 3 ⁇ 4e2 (about 59.5) with respect to the sum of Ti and Ni in the Ti-Ni-Cr alloy after brazing Mass%).
- composition (mass%) of the pure 1 layer and the pure Ni layer calculated based on the thickness (m) of each layer of the brazing filler metal and the thickness of each layer of the brazing filler metal Tables 1 to 3 below show the correspondence with the ratio.
- a 40% Cr—Ni alloy layer was used, while in Examples 6 to 9 shown in Table 2, a 20% Cr—Ni alloy layer was used.
- Comparative Example 1 in Table 3 a 20% Cr—Ni alloy layer was used, and in Comparative Examples 2 to 4, a 40% Cr—Ni alloy layer was used.
- Example 1 The ratio of the thickness of each layer (m) pure Ti layer and the pure Ni layer (wt 0/0) of pure Ti layer pure Ni layer 40 ⁇ 1 ⁇ 2Cr-Ni alloy SoJun Ni layer pure Ti layer net Ti layer Pure Ni layer
- Example 1 10.4 2.1 25.0 2.1 10.4 71.7 28.3
- Example 2 11.7 1.6 23.4 1.6 11.7 78.7 21.3
- Example 3 8.7 1.2 30.2 1.2 8.7 78.6 21.4
- Example 4 12.0 3.4 19.2 3.4 12.0 64.1 35.9
- Example 5 9.1 2.5 26.8 2.5 9.1 64.7 35.3
- the composition of the reaction layer of the clad material obtained by reacting the brazing materials according to Examples 1 to 9 and Comparative Examples 1 to 4 produced as described above was analyzed. Specifically, the brazing materials according to Examples 1 to 9 and Comparative Examples 1 to 4 were reacted under predetermined conditions (temperature: about 1220 ° C., time: 10 minutes). Then, the reaction layer of the clad material obtained by the above reaction was regarded as a joint portion by brazing joint according to the first embodiment, and after polishing the cross section of the reaction layer with resin, polishing was performed. And the content rate (mass%) of Ni, Cr, and Ti in the cross section of the reaction layer was analyzed using EPMA (electron beam microanalysis). In addition, the reaction ratio of Ti and Ni in the reaction layer of the clad material obtained by experiments was analyzed. The results are shown in Table 4 to Table 6 below.
- Example 6 31.3 1 1 .2 57.5 35.3 64.7
- Example 7 35.2 1 1.0 53.8 39.6 60.4
- Example 8 26.5 13.3 60.2 30.5 69.5
- Example 9 27.0 1 1 .7 61.3 30.5 69.5
- the composition (mass%) ratio of the reaction layer obtained by reacting the brazing material according to Example 1 was 26.7 mass% for Ti, 25.0 mass% for Cr, Ni was 48.3 mass%. Further, the composition ratio of Ti and Ni in the reaction layer according to Example 1 was 35.6% by mass: 64.4% by mass, and the eutectic composition e2 (see FIG. 4) was obtained. In addition, the composition (mass%) ratio of the reaction layer obtained by reacting the brazing filler metal according to Example 2 was 31.0 mass% for Ti, 24.3 mass% for Ti, and 44.7 mass% for ⁇ . It was.
- the yield ratio of Ti and Ni in the reaction layer according to Example 2 was 40.9 mass%: 59.1 mass%, and the composition was almost be2 (see FIG. 4).
- the composition (mass%) ratio of the reaction layer obtained by reacting the brazing filler metal according to Example 3 was 21.4 mass% for Ti, 29.1 mass% for Cr, and 49.5 mass 0 for Ni. /. Met.
- the composition ratio of Ti and Ni in the reaction layer according to Example 3 was 30.2% by mass: 69.8% by mass, which was almost ae2 (see FIG. 4).
- the composition (mass%) ratio of the reaction layer obtained by reacting the brazing material according to Example 4 Ti is 32.0 mass%, Cr is 20.0 mass 0/0, Ni is 48.0 mass %Met.
- the composition ratio of Ti and Ni in the reaction layer according to Example 4 was 40.0% by mass: 60.0% by mass, and the composition was almost be2 (see FIG. 4).
- the yield ratio of Ti and Ni in the reaction layer of Example 6 was 35.3% by mass: 64.7% by mass, which was almost the eutectic composition e2 (see FIG. 4).
- the composition (mass%) ratio of the reaction layer obtained by reacting the brazing filler metal according to Example 7 was 35.2 mass% for Ti, 11.0 mass% for Cr, and 3.8 mass% for Ni force. there were. Further, the composition ratio between Ti and Ni in the reaction layer according to Example 7, 39.6 wt 0/0: 60. a 4 wt%, and the composition of almost be2 (see FIG. 4).
- the composition (mass%) ratio of the reaction layer obtained by reacting the brazing filler metal according to Example 8 was 26.5 mass% for Ti, 13.3 mass% for Cr, and 60.2 mass for Ni. %Met. Moreover, the yarn ⁇ ratio between Ti and Ni in the reaction layer according to Example 8, 30.5 parts by mass 0/0: 69. a 5 wt%, has fallen and thread ⁇ approximately ae2 (see FIG. 4) . Further, the composition (mass%) ratio of the reaction layer obtained by reacting the brazing filler metal according to Example 9 was as follows: Ti 27.0 mass%, Cr 11.7 mass%, Ni 61.3 mass% there were.
- the composition ratio between Ti and Ni in the reaction layer according to Example 9 30.5 parts by mass 0/0: 69. a 5 wt%, and the composition of almost ae2 (see FIG. 4).
- the reaction layer also has Ti—Ni—Cr alloy strength.
- the composition (mass%) ratio of the reaction layer obtained by reacting the brazing material according to Comparative Example 1 was 35.9 mass% for Ti and 8. for Cr. 8 mass%, Ni was 55.3 mass%.
- the reaction layer also had a Ti—Ni—Cr alloy strength containing 8.8 mass% of Cr.
- reaction layer obtained by reacting the brazing filler metal according to Comparative Example 2 did not melt at about 1220 ° C. or less (see FIG. 4). It was also found that the Ni-Cr alloy layer remained unmelted in the reaction layer obtained by reacting the filter medium according to Comparative Example 3 at about 1220 ° C or less (see Fig. 4). In addition, it was found that an intermetallic compound containing Ti N was deposited in the reaction layer obtained by reacting the brazing material according to Comparative Example 4.
- reaction layers obtained by reacting the brazing materials according to Examples 1 to 9 and Comparative Example 1 An acid test was conducted to evaluate the acid resistance of the joint by brazing). Specifically, the reaction layers obtained by reacting the brazing materials according to Examples 1 to 9 and Comparative Example 1 were cut into 50 mm ⁇ 50 mm squares, and the weight of the reaction layer before the oxidation test was measured. And heated at 700 ° C. for 100 hours. Then, the weight of the reaction layer after the oxidation test was measured, and the change ability of the weight of the reaction layer before and after the oxidation test was calculated. The increase in the amount of acid in the reaction layer was calculated, and the oxidation resistance of the reaction layer was evaluated.
- Comparative Examples 5 and 6 the acid-rich test performed on the reaction layers obtained by reacting the brazing materials according to Examples 1 to 9 and Comparative Example 1 was also performed on SUS316L and SUS304. . That is, it comparison [SUS316L by J5 and SUS304 by Comparative Example 6 were cut into 50 mm ⁇ 50 mm squares, weighed before the oxidation test, and then heated in the atmosphere at a temperature of 700 ° C. for 100 hours. Then, the weight after the oxidation test was measured, and the increase in oxidation was calculated from the change in weight before and after the oxidation test. Table 7 shows the results. In Comparative Examples 2 to 4, the acid layer test was not performed because the reaction layer was mixed uniformly.
- a reaction layer containing 31.3 mass% of Ti, 11.2 mass% of Cr, and 57.5 mass% of Ni obtained by reacting the brazing material according to Example 6 was used.
- the increase in oxidation before and after the oxidation test was 0.213 mgZcm 2 .
- an oxidation test of the reaction layer containing 35.2% by mass of Ti, 11.0% by mass of Cr, and 53.8% by mass of Ni obtained by reacting the brazing material according to Example 7 The increase in acid concentration before and after was 0.228 mgZcm 2 .
- the reaction of the brazing material according to Comparative example 1 It was found that the oxidation resistance of the reaction layer obtained by the above treatment was smaller than that of 0.451 mgZcm 2 and had high acid resistance. This is because the reaction layer obtained by reacting the brazing material according to Comparative Example 1 contained only 8.8% by mass of Cr, whereas the brazing material according to Examples 1 to 9 was reacted. Since the reaction layer obtained by this treatment contains 11.0% by mass or more of Cr, the surface of the reaction layer obtained by reacting the brazing filler metal according to Examples 1 to 9 on the surface of the Cr O oxide film It is thought that this is because it was sufficiently formed
- the joint part obtained by brazing and brazing the brazing materials according to Examples 1 to 5 including the 40% Cr—Ni alloy layer has higher oxidation resistance than stainless steels such as S US316L and SUS304. It is thought that it does not oxidize faster than stainless steel.
- the brazing material according to Examples 1 to 5 including a 40% Cr—Ni alloy layer is considered to be more preferable as a brazing material for stainless steel and the like.
- the oxidation increase (0.213 mgZcm 2 , 0.228 mg / cm 2 , 0.201 mg) of the reaction layer obtained by reacting the brazing material according to Examples 6 to 9 containing the 20% Cr—Ni alloy layer.
- the joint joined by brazing using the brazing material according to Examples 6 to 9 including the 20% Cr—Ni alloy layer has lower oxidation resistance than SUS316L, so that it is oxidized faster than stainless steel SUS316L. It is considered to be ashamed. As a result, it was found that the brazing material according to Examples 6 to 9 was not very preferable as a brazing material for stainless steel SUS316L.
- the brazing material Id includes a Ni—Cr alloy layer 2a, a Ti layer 3c disposed on one side of the Ni—Cr alloy layer 2a, and a Ni—Cr alloy. Ti layer 3d disposed on the other side of alloy layer 2a, Ni layer 4c disposed between Ni—Cr alloy layer 2a and Ti layer 3c, and Ni—Cr alloy layer 2a and Ti layer 3d. With Ni layer 4d placed between!
- Mo or Co is added to at least one of the Ni—Cr alloy layer 2a, the Ti layers 3c and 3d, and the Ni layers 4c and 4d. It has been overwhelmed.
- Mo or Co is contained so that the content of the brazing filler metal Id is about 10% by mass or less. If the Ti-Ni-Cr alloy le contains Mo, a content of about 2.0% to about 4.5% by mass is preferred! ! ⁇ ⁇ ⁇ Alloy! When Co is contained in ⁇ , a content of about 2.0% by mass to about 10% by mass is preferable.
- the Ni layers 4c and 4d are roll-bonded to the Ni—Cr alloy layer 2a. Ti layers 3c and 3d are rolled and bonded to Ni layers 4c and 4d that are rolled and bonded to Ni—Cr alloy layer 2a. Further, as the rolling joining, for example, hot welding, cold welding, vacuum welding, or the like can be used.
- the Ni—Cr alloy layer 2a is the “Ni—Cr brazing layer” of the present invention. It is an example.
- the Ti layer 3c is an example of the “Ti brazing layer” and the “first ITi brazing layer” of the present invention, and the Ti layer 3d is the “Ti brazing layer” and the “second Ti brazing layer” of the present invention. Is an example.
- the Ni layer 4c is an example of the “Ni brazing layer” and the “second INi brazing layer” of the present invention, and the Ni layer 4d is the “Ni brazing layer” and the “second Ni brazing layer” of the present invention. Is an example.
- the Ni-Cr alloy layer 2a is composed of Ni and Cr.
- the Ni—Cr alloy layer 2a may be doped with Mo or Co.
- the Cr content of the Ni—Cr alloy layer 2a is about 20 mass% or more and about 40 mass% or less.
- Ti layers 3c and 3d are also composed of Ti force.
- the Ti layers 3c and 3d may be added with Mo or Co.
- the Ti layers 3c and 3d each have a thickness of t3.
- the Ni layers 4c and 4d are composed of M.
- the Ni layers 4c and 4d may be supplemented with Mo or Co.
- the Ni layers 4c and 4d each have a thickness of t4.
- the amount of Ni in the Ni layer 4c when the total amount of Ti in the Ti layer 3c and the amount of Ni in the Ni layer 4c is 100 mass%, the amount of Ni in the Ni layer 4c is 21. 5 mass% or more and 37.5 mass% or less, and preferably about 28.3 mass%, which is the eutectic composition of the Ti—Ni alloy at the initial stage of brazing.
- the amount of Ni in the Ni layer 4d when the total amount of Ti in the Ti layer 3d and the amount of Ni in the Ni layer 4d is 100% by mass, the amount of Ni in the Ni layer 4d is 21.5% by mass or more and 37.5% by mass or less. Preferably, it is about 28.3 mass% which becomes the eutectic composition of the TiNi alloy in the initial stage of brazing.
- the ratio t4Zt3 between the thickness t3 of the Ti layers 3c and 3d and the thickness t4 of the Ni layers 4c and 4d is 1 Z8 or more and 2Z7 or less, and
- the heat exchange 100a formed using the brazing filler metal Id (see Fig. 13) according to the third embodiment is brazed between the fin 12 and the plates 13 and 11, as shown in Fig. 14.
- the brazing material Id (see FIG. 13) is arranged between the plate 11 and the fin 12, and the brazing material Id is arranged between the fin 12 and the plate 13. .
- heating is performed at a temperature of about 1110 ° C. or more and about 1150 ° C. or less for about 10 minutes.
- Other processes of the brazing joint using the brazing material Id according to the third embodiment are the same as the processes of the brazing joint using the brazing material 1 according to the first embodiment.
- brazing can be performed at a temperature of about 1150 ° C or lower, so that the crystals of plates 11 and 13 and fins 12 that are powerful, such as SUS304 and SUS316, are prevented from coarsening from the hot brazing during brazing. can do.
- the strength of the plates 11 and 13 and the fins 12 can be improved, so that the thickness of the plates 11 and 13 and the fins 12 can be reduced.
- the heat exchange 100a can be reduced in weight, and the heat exchange efficiency of the heat exchange ioo a can be improved by making it easier to transfer the heat of the exhaust gas flowing through the heat exchange 100a to the water.
- the brazing composite material 50a in which the brazing material 51a having a three-layer structural force is roll-bonded to the substrate 13 will be described.
- a brazing composite material 50a according to the fourth embodiment of the present invention
- a plate 13 made of less steel and a pair of brazing materials 5 la rolled and joined to one side and the other side of the plate 13 are provided.
- the pair of brazing materials 51a includes the Ni-Cr alloy layer 2a, the Ti layer 3e, the Ni-Cr alloy layer 2a, and the Ti layer that are roll-bonded to the plate 13, respectively. It consists of a three-layer structure with a Ni layer 4e placed between them.
- the amount of Ni in the Ni layer 4e is 21.5% by mass or more and 37.5% by mass or less. Preferably, it is about 28.3 mass%, which is the eutectic composition of the initial TiNi alloy at the time of brazing.
- Mo or Co is added to at least one of the Ni—Cr alloy layer 2a, the Ti layer 3e, and the Ni layer 4e.
- Mo or Co is contained so that the content of the brazing material 51a is about 10% by mass or less.
- Mo is contained in the brazing material 5 la
- a content of about 2.0% by mass to about 4.5% by mass is preferred.
- Co is contained in the brazing material 51a, about 2.
- a content of 0% to about 10% by weight is preferred.
- the composite material 50a (FIG brazing so as to be in contact with the bent portion of the fin 12 15)). Then, the brazing joint is performed under the same conditions as in the third embodiment (heating in an inert gas or vacuum at a temperature of about 1110 ° C to about 1150 ° C for about 10 minutes). Do.
- a brazing material according to Example 1 was produced in the same manner as the comparative experiment conducted to confirm the effect of the first embodiment described above.
- a Ni—Cr alloy layer containing 60% by mass of Ni and 40% by mass of Cr, a Ni layer added with 5% by mass of Mo, and a pure Ti layer were used as a brazing material.
- the Ni layer was rolled and joined to one side and the other side of the Ni—Cr alloy layer, respectively, and then subjected to diffusion annealing at a temperature of 800 ° C. for 1 minute in an argon atmosphere. Then, finish rolling and annealing were performed to adjust the thickness of the Ni-Cr alloy layer and the Ni layer to 24.2 111 and 1.9 m, respectively.
- a pure Ti layer was rolled and bonded to each Ni layer roll-bonded to both surfaces of the Ni Cr alloy layer, and then diffusion annealing was performed at a temperature of 800 ° C. for 1 minute in an argon atmosphere. Then, by performing finish rolling and annealing, and adjusting the thickness of each pure Ti layer to 11.0 m, the pure Ti layer ZNi layer ZNi-Cr alloy layer ZNi layer Z pure Ti layer has a five-layer structure A brazing material according to Example 10 was produced. In this way, the content (% by mass) of Ni in the Ni layer relative to the total of Ti in the pure Ti layer before brazing and Ni in the Ni layer was adjusted to 24.5% by mass. .
- a brazing material As a brazing material, a Ni—Cr alloy layer containing 60% by mass of Ni and 40% by mass of Cr, a Ni layer added with 10% by mass of Mo, and a pure Ti layer were used. And, by performing finish rolling and annealing, the thickness of each of the Ni-Cr alloy layer, Ni layer and pure Ti layer was adjusted to 23.6 m, 2. O / zm and 11.2 m. Except for the above, a brazing material according to Example 11 having a five-layer structure of a pure Ti layer, a ZNi layer, a ZNi—Cr alloy layer, a ZNi layer, and a Z pure Ti layer was produced in the same manner as in Example 1 above. In this way, the content (% by mass) of Ni in the Ni layer relative to the total of Ti in the pure Ti layer before brazing and Ni in the Ni layer was adjusted to 24.1% by mass.
- Example 12 As the brazing material, a Ni—Cr alloy layer containing 60% by mass of Ni and 40% by mass of Cr, a Ni layer added with 20% by mass of Mo, and a pure Ti layer were used. And, by performing finish rolling and annealing, the thicknesses of the Ni-Cr alloy layer, Ni layer and pure Ti layer were adjusted to 24.2 m, 2.0 m and 10.9 m, respectively. In the same manner as in Example 1, a brazing material according to Example 12 having a five-layer structure of a pure Ti layer, a ZNi layer, a ZNi—Cr alloy layer, a ZNi layer, and a Z pure Ti layer was produced. In this way, the content (% by mass) of Ni in the Ni layer relative to the total of Ti in the pure Ti layer before brazing and Ni in the Ni layer was adjusted to 22.5% by mass.
- a brazing material As a brazing material, a Ni—Cr alloy layer containing 60% by mass of Ni and 40% by mass of Cr, a Ni layer added with 35% by mass of Mo, and a pure Ti layer were used. And, by performing finish rolling and annealing, the thicknesses of the Ni-Cr alloy layer, Ni layer and pure Ti layer were adjusted to 24.4 ⁇ m, 2. and 10.4 m, respectively.
- a brazing material according to Example 13 having a five-layer structure of a pure Ti layer, a ZNi layer, a ZNi—Cr alloy layer, a ZNi layer, and a Z pure Ti layer was produced. In this way, the content (% by mass) of Ni in the Ni layer with respect to the total of Ti in the pure Ti layer before brazing and Ni in the Ni layer was adjusted to 22.9% by mass.
- the brazing material contains 60% by mass of Ni and 40% by mass of Cr, a Ni—Cr alloy layer to which 5% by mass of Mo is added, a Ni layer to which 35% by mass of Mo is added, and a pure layer Ti layer was used. After finishing rolling and annealing, the thickness of each of the Ni-Cr alloy layer, Ni layer and pure Ti layer was adjusted to 24.8 m, 2.5 m and 10.1 ⁇ m.
- the brazing material according to Example 14 having a five-layer structure of pure Ti layer, ZNi layer, ZNi—Cr alloy layer, ZNi layer, and Z pure Ti layer was prepared in the same manner as in Example 1 above. In this way, the content (% by mass) of Ni in the Ni layer relative to the total of Ti in the pure Ti layer before brazing and Ni in the Ni layer was adjusted to 24.1% by mass. .
- a brazing material As a brazing material, a Ni—Cr alloy layer containing 60% by mass of Ni and 40% by mass of Cr, a Ni layer added with 12% by mass of Co, and a pure Ti layer were used. By performing finish rolling and annealing, the thickness of each of the Ni-Cr alloy layer, Ni layer and pure Ti layer was reduced to 23.6 ⁇ m. Except for adjusting to m, 2. l / zm, and 11.1 m, it has the same five-layer structure as the pure Ti layer, ZNi layer, ZNi—Cr alloy layer, ZNi layer, and Z pure Ti layer, as in Example 1 above. A filter cake according to Example 15 was produced. In this way, the content (% by mass) of Ni in the Ni layer relative to the total of Ti in the pure Ti layer before brazing and Ni in the Ni layer was adjusted to 24.8% by mass.
- a brazing material As a brazing material, a Ni-Cr alloy layer containing 60 mass% Ni and 40 mass% Cr, a Ni layer added with 40 mass% or more of Mo, a pure Ti layer, When is used, cracks occur in the brazing material during rolling. In this experiment, Mo was added to the Ni layer up to 35% by mass.
- the plate thickness m) of each layer of the brazing filler metal and the composition (mass%) ratio of the pure Ti layer to the Ni layer calculated based on the plate thickness of each layer of the brazing filler metal The relationship is shown in Table 8 below.
- the composition of the reaction layer of the clad material obtained by reacting the brazing material according to Examples 1 and 10 to 15 produced as described above was analyzed. Specifically, the brazing filler metals according to Examples 1 and 10 to 15 were reacted under predetermined conditions (temperature: about 1150 ° C., time: 10 minutes). Then, the reaction layer of the clad material obtained by the above reaction was regarded as a joint portion by brazing joint according to the third embodiment, and the cross section of the reaction layer was filled with resin and then polished. Then, the content (mass%) of Ti, Cr, Ni, Mo and Co in the cross section of the reaction layer was analyzed using EPM A. Furthermore, the composition (mass%) ratio of Ti and Ni in the reaction layer of the clad material obtained by experiments was analyzed. The results are shown in Table 9 below. [0127] [Table 9]
- the composition (mass%) ratio of the reaction layer obtained by reacting the brazing material according to Example 1 was 26.7 mass% for Ti, 25.0 mass% for Cr, Ni was 48.3 mass%, and Mo and Co were 0 mass%. Further, the yield ratio of Ti and Ni in the reaction layer according to Example 1 was 35.6% by mass: 64.4% by mass, and the eutectic composition e2 (see FIG. 4) was obtained.
- the composition (mass%) ratio of the reaction layer obtained by reacting the brazing material according to Example 10 was as follows: Ti was 28.6 mass%, Cr was 24.6 mass%, Ni was 46.2 mass%, Mo was 0.5% by mass, and Co was 0% by mass.
- the composition ratio of Ti and Ni in the reaction layer according to Example 10 was 38.2% by mass: 61.8% by mass. Further, the composition (mass%) ratio of the reaction layer obtained by reacting the brazing filler metal according to Example 11 was as follows: Ti force 3 mass%, Cr 24.1 mass%, Ni 45.5 mass%, Mo 1. 0% by mass, Co was 0% by mass. Further, the yield ratio of Ti and Ni in the reaction layer according to Example 11 was 39.2% by mass: 60.8% by mass.
- the composition (mass%) ratio of the reaction layer obtained by reacting the brazing filler metal according to Example 12 was as follows: Ti was 28.3 mass%, Cr was 24.6 mass%, Ni was 45.1 mass 0 / 0 , Mo was 2.1% by mass, and Co was 0% by mass.
- the composition ratio of Ti and Ni in the reaction layer according to Example 12 was 38.6% by mass: 61.4% by mass.
- the composition (mass%) ratio of the reaction layer obtained by reacting the brazing material according to Example 13 was as follows: Ti was 26.7 mass%, Cr was 24.5 mass%, and Ni was 44.6 mass%. Mo was 4.3% by mass and Co was 0% by mass.
- the yield ratio of Ti and Ni in the reaction layer according to Example 13 was 37.4% by mass: 62.6% by mass.
- the composition (mass%) ratio of the reaction layer obtained by reacting the brazing filler metal according to Example 14 was 25.7 mass% for Ti, 24.7 mass% for Cr, and 42.1 mass% for Ni. Mo was 7.5% by mass and Co was 0% by mass.
- composition (mass%) ratio of the reaction layer obtained by reacting the brazing filler metal according to Example 15 was 29.0 mass% for Ti, 24.1 mass% for Cr, 45.7 mass% for Ni, Mo was 0% by mass and Co was 1.3% by mass. Further, the composition ratio between Ti and Ni in the reaction layer according to Example 15, 38.8 wt 0/0: became 61.2 mass 0/0. Thus, it was found from the composition of the reaction layer obtained by reacting the brazing filler metal according to Examples 1 and 10 to 15 that the reaction layer had a Ti—Ni—Cr alloy strength.
- an acid test was conducted to evaluate the acid resistance of the reaction layer (joint part by brazing joint) obtained by reacting the brazing material according to Examples 1 and 10 to 15 described above.
- the reaction layer obtained by reacting the brazing material according to Examples 1 and 10 to 15 was cut into a 50 mm ⁇ 50 mm square, and the weight of the reaction layer before the oxidation test was measured. Heated at a temperature of ° C for 100 hours. Then, the weight of the reaction layer after the acid test was measured, and the change in the weight of the reaction layer before and after the oxidation test was calculated. The increase in the acid layer in the reaction layer was calculated, and the acid resistance of the reaction layer was evaluated. .
- Table 10 The results are shown in Table 10.
- Ti obtained by reacting the brazing material according to Example 1 was 26.7 mass%, Cr was 25.0 mass%, Ni was 48.3 mass%, Mo and The increase in the amount of acid before and after the acid test of the reaction layer containing Co at a ratio of 0% by mass was 0.042 mgZcm 2 . Further, Ti obtained by reacting the brazing material according to Example 10 was 28.6% by mass, Cr was 24.6% by mass, Ni was 46.2% by mass, Mo was 0.5% by mass, and Co was 0%. Of the reaction layer contained at a rate of mass%. The amount of increase in acid before and after the acid test was 0.026 mg / cm 2 .
- Ti obtained by reacting the brazing material according to Example 11 was 29.3 mass%, Cr was 24.1 mass%, Ni was 45.5 mass%, Mo was 1.0 mass%, and Co was The increase in the amount of acid before and after the oxidation test of the reaction layer contained at a rate of 0% by mass was 0.015 mg / cm 2 .
- Ti obtained by reacting the brazing material according to Example 12 was 28.3% by mass, Cr was 24.6% by mass, Ni was 45.1% by mass, Mo was 2.1% by mass, and Co was 0%.
- the amount of increase in oxidation before and after the oxidation test of the reaction layer contained at a ratio of mass% was 0.004 mg / cm 2 .
- Ti obtained by reacting the brazing filler metal according to Example 13 was 26.7% by mass, Cr was 24.5% by mass, Ni was 44.6% by mass, Mo was 4.3% by mass, and Co was 0%.
- the increase in the amount of acid before and after the acid test of the reaction layer contained at a ratio of mass% was 0.003 mgZcm 2 .
- Ti obtained by reacting the brazing material according to Example 14 was 25.7 mass%, Cr was 24.7 mass%, Ni was 42.1 mass%, Mo was 7.5 mass%, and Co was 0
- the amount of increase in oxidation before and after the oxidation test of the reaction layer contained at a ratio of mass% was 0.002 mg / cm 2 .
- Ti obtained by reacting the brazing material according to Example 15 was 29.0 mass%, Cr was 24.1 mass%, Ni was 45.7 mass%, Mo was 0 mass%, and Co was 1.3.
- the increase in the amount of acid before and after the acid test of the reaction layer contained at a ratio of mass% was 0.022 mgZcm 2 .
- the amount of Mo added to the reaction layer was about 2.0% by mass or more (implementation). In Examples 12 to 14), it was found that the increase in acid concentration was about 1Z10 or less compared to the case where Mo was not added to the reaction layer. In addition, when the amount of Mo added to the reaction layer is about 2.0% by mass or more and about 4.5% by mass or less, the increase in the amount of acid in the reaction layer is effectively reduced and the addition of Mo to the reaction layer is also reduced. When the amount is about 7.5% by mass, the amount of Mo added is larger than that of about 2.0% by mass or more and about 4.5% by mass or less. It was found that the increase in drought did not decrease effectively. That is, by adding about 2.0 mass% or more and about 4.5 mass% or less of Mo to the reaction layer, it is possible to sufficiently and effectively improve the acid resistance.
- brazing structure of the present invention is applied to a heat exchanger.
- the present invention is not limited thereto, and high-temperature exhaust gas flows through the brazing structure of the present invention. Therefore, it can also be applied to brazed structures other than heat exchangers that require high acid resistance.
- the present invention is not limited to this, and the plate constituting the brazing composite material is used.
- the rates include Hastelloy (registered trademark) and Inconel (registered trademark) other than stainless steel. Use any steel containing any Ni-base heat-resistant alloy.
- a force showing an example of using a Ti layer made of pure Ti as a brazing material is not limited to this.
- a Ti alloy layer containing at a ratio of at least% may be used.
- Examples of such Ti alloys mainly composed of pure Ti include ⁇ -alloys having a phase (close-packed hexagonal phase) such as Ti-5A1-2.5Sn and ex-phases such as Ti-6A1-4V (most ⁇ + j8 alloy with dense hexagonal phase) and ⁇ phase (body centered cubic phase)
- Ni layers 4a and 4b are rolled and joined to the surface of Ni—Cr alloy layer 2, and Ti layers 4a and 4b are each Ti.
- An example of brazing using a brazing composite material in which the three-layer brazing material 1 in a state where the layers 3a and 3b are rolled and joined is rolled and joined to the plate 13 has been shown.
- a clad material in which a Ni—Cr alloy layer 20a is roll-bonded to one surface of the plate 13 and a clad material in which a Ni—Cr alloy layer 20b is roll-bonded to the other surface of the plate 13 A pair of Ni layers 40a and 40b arranged so as to sandwich the Ti layer 30 may be prepared separately.
- a Ti—Ni—Cr alloy layer can be formed at the brazed joint.
- the brazing material is formed without adding an element.
- the present invention is not limited to this. It is also possible to use a brazing material added with an element that easily forms an oxide such as Al, V, Si and Zr in the Ti layer. If elements that easily form oxides such as Al, V, Si, and Zr are added to the Ti layer in this way, the adhesion of the oxide layer formed on the surface of the reaction layer is improved. It can suppress peeling. As a result, the progress of the oxidation reaction can be suppressed, so that the amount of oxidation increase in the reaction layer can be reduced. When the oxide layer is peeled off, the exposed portion of the reaction layer is newly oxidized, so that the amount of oxidation increase in the reaction layer increases.
- the force shown for the example in which the brazing material is composed of the Ti layer, the ZNi layer, the ZNi-Cr alloy layer, the ZNi layer, the ZTi layer, the present invention is not limited to this, and the brazing material is a Ni-Cr alloy.
- Layer Z Ni layer ZT ring ZNi layer ZNi—Cr alloy layer can be used to achieve the same effect.
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Abstract
Description
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Priority Applications (2)
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JP2006520495A JP5084260B2 (ja) | 2005-03-29 | 2006-03-24 | ろう材、ろう付け用複合材およびそれらを用いてろう付け接合されたろう付け構造 |
EP06729862.0A EP1864749B1 (en) | 2005-03-29 | 2006-03-24 | Brazing filler material, composite material for brazing and brazed structure joined by using those |
Applications Claiming Priority (2)
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JP2005-094323 | 2005-03-29 | ||
JP2005094323 | 2005-03-29 |
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WO2006104025A1 true WO2006104025A1 (ja) | 2006-10-05 |
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PCT/JP2006/305914 WO2006104025A1 (ja) | 2005-03-29 | 2006-03-24 | ろう材、ろう付け用複合材およびそれらを用いてろう付け接合されたろう付け構造 |
Country Status (4)
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US (1) | US8029916B2 (ja) |
EP (1) | EP1864749B1 (ja) |
JP (1) | JP5084260B2 (ja) |
WO (1) | WO2006104025A1 (ja) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2008073738A (ja) * | 2006-09-22 | 2008-04-03 | Neomax Material:Kk | ろう材、ろう付け用複合材およびそれらを用いてろう付け接合されたろう付け構造 |
JP2008238188A (ja) * | 2007-03-26 | 2008-10-09 | Hitachi Cable Ltd | ろう付け用複合材およびそれを用いたろう付け製品 |
JP2009214120A (ja) * | 2008-03-07 | 2009-09-24 | Hitachi Cable Ltd | ろう付け加工用複合材およびろう付け製品 |
CN105499735A (zh) * | 2016-02-19 | 2016-04-20 | 哈尔滨工业大学(威海) | 一种采用TiZrNiCu+B复合钎料连接Ti60与TiBw/TC4的方法 |
Families Citing this family (10)
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DE112004002533T5 (de) * | 2003-12-24 | 2006-12-07 | Neomax Materials Co., Ltd., Suita | Lötverfahren und gelötete Anordnungen |
DE102009055608A1 (de) * | 2009-11-25 | 2011-05-26 | Behr Gmbh & Co. Kg | Gelöteter Aluminium-Wärmeübertrager |
JP5815325B2 (ja) * | 2011-08-09 | 2015-11-17 | 三菱アルミニウム株式会社 | 熱交換器 |
KR20140070012A (ko) * | 2012-11-30 | 2014-06-10 | 엘지전자 주식회사 | 열 교환기 및 그 제조 방법 |
KR102085716B1 (ko) | 2012-12-10 | 2020-03-06 | 엘지전자 주식회사 | 열 교환기 및 그 제조 방법 |
US8640942B1 (en) * | 2013-03-13 | 2014-02-04 | Siemens Energy, Inc. | Repair of superalloy component |
US20140272450A1 (en) * | 2013-03-14 | 2014-09-18 | Siemens Energy, Inc. | Near eutectic composition nickel base sandwich braze foil |
EP2971563A2 (en) | 2013-03-15 | 2016-01-20 | Siemens Energy, Inc. | Component repair using brazed surface textured superalloy foil |
EP2910765B1 (en) * | 2014-02-21 | 2017-10-25 | Rolls-Royce Corporation | Single phase micro/mini channel heat exchangers for gas turbine intercooling and corresponding method |
EP3572758B1 (en) * | 2014-02-21 | 2023-04-05 | Rolls-Royce Corporation | Microchannel heat exchangers for gas turbine intercooling and condensing |
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US4023936A (en) * | 1976-06-14 | 1977-05-17 | Lukens Steel Company | Titanium clad steel and process for making |
DE4003038C1 (ja) * | 1990-02-02 | 1990-08-09 | Mtu Muenchen Gmbh | |
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JP3765533B2 (ja) | 2001-10-11 | 2006-04-12 | 日立電線株式会社 | ろう付け用複合材及びそれを用いたろう付け製品 |
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2006
- 2006-03-24 US US11/578,511 patent/US8029916B2/en not_active Expired - Fee Related
- 2006-03-24 JP JP2006520495A patent/JP5084260B2/ja not_active Expired - Fee Related
- 2006-03-24 WO PCT/JP2006/305914 patent/WO2006104025A1/ja active Application Filing
- 2006-03-24 EP EP06729862.0A patent/EP1864749B1/en not_active Expired - Fee Related
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JPS6054269A (ja) * | 1983-09-02 | 1985-03-28 | Tanaka Kikinzoku Kogyo Kk | 複合線 |
JPH07299592A (ja) * | 1994-03-07 | 1995-11-14 | Texas Instr Inc <Ti> | 自己ろう付け性複合材を作る方法 |
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Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2008073738A (ja) * | 2006-09-22 | 2008-04-03 | Neomax Material:Kk | ろう材、ろう付け用複合材およびそれらを用いてろう付け接合されたろう付け構造 |
JP2008238188A (ja) * | 2007-03-26 | 2008-10-09 | Hitachi Cable Ltd | ろう付け用複合材およびそれを用いたろう付け製品 |
JP2009214120A (ja) * | 2008-03-07 | 2009-09-24 | Hitachi Cable Ltd | ろう付け加工用複合材およびろう付け製品 |
CN105499735A (zh) * | 2016-02-19 | 2016-04-20 | 哈尔滨工业大学(威海) | 一种采用TiZrNiCu+B复合钎料连接Ti60与TiBw/TC4的方法 |
CN105499735B (zh) * | 2016-02-19 | 2018-04-10 | 哈尔滨工业大学(威海) | 一种采用TiZrNiCu+B复合钎料连接Ti60与TiBw/TC4的方法 |
Also Published As
Publication number | Publication date |
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JPWO2006104025A1 (ja) | 2008-09-04 |
EP1864749A1 (en) | 2007-12-12 |
EP1864749A4 (en) | 2010-04-21 |
US8029916B2 (en) | 2011-10-04 |
US20070224445A1 (en) | 2007-09-27 |
JP5084260B2 (ja) | 2012-11-28 |
EP1864749B1 (en) | 2014-01-22 |
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