WO2006109602A1 - アルミニウム合金製ブレージングシートおよび熱交換器用アルミニウム合金製チューブ - Google Patents
アルミニウム合金製ブレージングシートおよび熱交換器用アルミニウム合金製チューブ Download PDFInfo
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- WO2006109602A1 WO2006109602A1 PCT/JP2006/307031 JP2006307031W WO2006109602A1 WO 2006109602 A1 WO2006109602 A1 WO 2006109602A1 JP 2006307031 W JP2006307031 W JP 2006307031W WO 2006109602 A1 WO2006109602 A1 WO 2006109602A1
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- WIPO (PCT)
- Prior art keywords
- alloy
- aluminum alloy
- brazing
- ray diffraction
- tube
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Classifications
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- 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
-
- 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 or brazing
- B23K35/0233—Sheets or foils
-
- 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 or brazing
- B23K35/0233—Sheets or foils
- B23K35/0238—Sheets or 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
- B23K35/28—Selection of soldering or welding materials proper with the principal constituent melting at less than 950°C
- B23K35/286—Al 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
- B23K35/28—Selection of soldering or welding materials proper with the principal constituent melting at less than 950°C
- B23K35/286—Al as the principal constituent
- B23K35/288—Al as the principal constituent with Sn or Zn
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- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C1/00—Making non-ferrous alloys
- C22C1/11—Making amorphous alloys
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C21/00—Alloys based on aluminium
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C21/00—Alloys based on aluminium
- C22C21/02—Alloys based on aluminium with silicon as the next major constituent
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C21/00—Alloys based on aluminium
- C22C21/10—Alloys based on aluminium with zinc as the next major constituent
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22F—CHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
- C22F1/00—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
- C22F1/04—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of aluminium or alloys based thereon
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- 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
-
- 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
- F28F21/081—Heat exchange elements made from metals or metal alloys
- F28F21/084—Heat exchange elements made from metals or metal alloys from aluminium or aluminium alloys
-
- 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
-
- 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
- F28D1/00—Heat-exchange apparatus having stationary conduit assemblies for one heat-exchange medium only, the media being in contact with different sides of the conduit wall, in which the other heat-exchange medium is a large body of fluid, e.g. domestic or motor car radiators
- F28D1/02—Heat-exchange apparatus having stationary conduit assemblies for one heat-exchange medium only, the media being in contact with different sides of the conduit wall, in which the other heat-exchange medium is a large body of fluid, e.g. domestic or motor car radiators with heat-exchange conduits immersed in the body of fluid
- F28D1/03—Heat-exchange apparatus having stationary conduit assemblies for one heat-exchange medium only, the media being in contact with different sides of the conduit wall, in which the other heat-exchange medium is a large body of fluid, e.g. domestic or motor car radiators with heat-exchange conduits immersed in the body of fluid with plate-like or laminated conduits
- F28D1/0391—Heat-exchange apparatus having stationary conduit assemblies for one heat-exchange medium only, the media being in contact with different sides of the conduit wall, in which the other heat-exchange medium is a large body of fluid, e.g. domestic or motor car radiators with heat-exchange conduits immersed in the body of fluid with plate-like or laminated conduits a single plate being bent to form one or more conduits
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F28—HEAT EXCHANGE IN GENERAL
- F28F—DETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
- F28F1/00—Tubular elements; Assemblies of tubular elements
- F28F1/10—Tubular elements and assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with projections, with recesses
- F28F1/12—Tubular elements and assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with projections, with recesses the means being only outside the tubular element
- F28F1/126—Tubular elements and assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with projections, with recesses the means being only outside the tubular element consisting of zig-zag shaped fins
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- 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
- Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10S165/00—Heat exchange
- Y10S165/905—Materials of manufacture
-
- 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.]
- Y10T428/12736—Al-base component
- Y10T428/12764—Next to Al-base component
Definitions
- the present invention relates to an aluminum alloy brazing sheet used for manufacturing a heat exchanger, and an aluminum alloy tube for heat exchange constituted by using a strong aluminum alloy brazing sheet.
- a plurality of flat tubular tubes 111 are provided with radiating fins 112 that are formed in a corrugated shape.
- the tube 111 is integrally formed, and both ends of the tube 111 are open to spaces formed by a header 113 and a tank (not shown).
- the powerful radiator 100 sends the high-temperature refrigerant from the space of one tank through the inside of the tube 111 to the space on the other tank side, and exchanges heat between the tube 111 and the radiating fin 1 12 to lower the temperature. Recirculate the refrigerant again.
- this tube 111 is made of aluminum in which one side surface of the core material 102 is clad with a skin material (also called a sacrificial anode material) 103, and the other side surface of the core material 102 is clad with a brazing material 104.
- the brazing sheet 101 made of aluminum alloy (see Fig. 5) is formed into a flat tubular shape with a forming roll, etc., and brazed sheet 101 made of aluminum alloy is brazed by electro-welding or by brazing heating.
- the fluid passage of the tube 111 is formed.
- the core material 102 is made of an Al-Mn alloy such as alloy number 3003 specified in JISH4000 from the viewpoint of corrosion resistance and strength.
- the skin material 103 that is constantly in contact with the refrigerant has alloy number 7072.
- Al—Zn and Al—Zn—Mg alloys such as Al—2 to 5% Zn—2 to 4% Mg are used, and the brazing filler metal 104 has an Al— Si-based alloys are used.
- the radiator 100 includes a tube 111 having the above-described configuration and a heat dissipation frame that has been corrugated.
- the IN 112 and other members are used to assemble them together by brazing.
- Brazing methods include the flux brazing method and the noclock brazing method using non-corrosive flux, which are brazed by heating to a high temperature of around 600 ° C.
- the present invention has been made in view of the above problems, and an aluminum alloy brazing sheet for heat exchange which has improved life including fatigue in a plastic region, and using the same It is an object of the present invention to provide an aluminum alloy tube for heat exchange that is configured.
- An aluminum alloy brazing sheet for a heat exchanger of the present invention that has solved the above-mentioned problems Is an Al-Mn alloy core and an Al-Zn alloy clad on one side of the core, A1 — Zn—Mg alloy, Al—Si—Mn—Zn alloy, or Al—Si—Mn — An aluminum alloy brazing sheet composed of an Mg—Zn alloy skin material and an A1—Si alloy brazing material clad on the other side of this core material! X-ray diffraction intensity ratio is I
- the aluminum alloy brazing sheet of the present invention satisfies the above-described relational expression, so that in the deformation in the plastic region, the plastic deformation in the direction parallel to the rolling direction of the aluminum alloy brazing sheet. Can be easily generated uniformly. As a result, deformation does not concentrate locally and the progress of cracks in the thickness direction can be delayed, so that the life including fatigue in the plastic region can be improved.
- the aluminum alloy tube for a heat exchanger according to the present invention that has solved the above-described problems includes an A 1 Mn-based alloy core material, an A1-Zn-based alloy clad on one side of the core material, Al-Zn-Mg.
- the heat after heating at 585 to 620 ° C The X-ray diffraction intensity ratio of the aluminum alloy tube for the exchanger is I /
- the configuration satisfies (I +1 +1 +1) ⁇ 0.3.
- the aluminum alloy tube of the present invention satisfies the above-described relational expression, so that plastic deformation in a direction parallel to the rolling direction of the aluminum alloy brazing sheet occurs in deformation in the plastic region. It tends to occur uniformly. As a result, even when repeated tensile or compressive stress is applied in the rolling direction, the deformation does not concentrate locally and the progress of the crack in the thickness direction can be delayed, so fatigue in the plastic region can be prevented. Including life can be improved.
- the aluminum alloy brazing sheet for a heat exchanger according to the present invention was able to improve the life including fatigue in the plastic region. This makes it possible to improve the fatigue life of heat exchangers for automobiles. Further, the aluminum alloy tube for heat exchanger according to the present invention was able to improve the life including fatigue in the plastic region. This makes it possible to improve the fatigue life of automotive heat exchangers.
- FIG. 1 is a cross-sectional view of an aluminum alloy brazing sheet for a heat exchanger according to the present invention.
- FIG. 2 is a cross-sectional view of an essential part of an automotive heat exchanger using the aluminum alloy brazing sheet for heat exchanger of the present invention (aluminum alloy tube for heat exchanger).
- FIG. 3 is an explanatory diagram for explaining a single swing plane bending fatigue test.
- FIG. 4 is a longitudinal sectional view of a main part of a conventional general automotive heat exchanger.
- FIG. 5 is a cross-sectional view of a conventional aluminum alloy brazing sheet for heat exchangers.
- FIG. 6 is a sectional view of an aluminum alloy tube for a heat exchanger according to the present invention.
- FIG. 1 is a cross-sectional view of an aluminum alloy brazing sheet for heat exchanger of the present invention
- FIG. 2 is an aluminum alloy brazing sheet for heat exchanger of the present invention (aluminum alloy tube for heat exchanger).
- FIG. 2 is a cross-sectional view of a main part of a heat exchanger for an automobile using a slab.
- the brazing sheet 1 made of an aluminum alloy for a heat exchanger comprises an Al—Mn alloy core material 2 and an Al—Zn alloy clad on one side of the core material 2, A1 —Zn—.
- This aluminum alloy brazing sheet 1 for heat exchangers has an X-ray diffraction intensity ratio of I
- the configuration satisfies 200 Z (I + 1 + 1 + 1) ⁇ 0.4.
- I 1, 1, 1, 1 are equivalent plane groups ⁇ 200 ⁇ , ⁇ 1 11 ⁇ , ⁇ 220 ⁇ and ⁇ 311 ⁇ represent the intensity of X-ray diffraction.
- Al (Au, Cu, Ni, Ag, etc.) having a face-centered cubic lattice crystal structure has a small angle (2 ⁇ ) when X-ray diffraction intensity is measured by the ⁇ -2 ⁇ method.
- Equivalent plane group ⁇ 111 ⁇ , ⁇ 200 ⁇ , ⁇ 220 ⁇ , ⁇ 311 ⁇ , ⁇ 222 ⁇ , ⁇ 400 ⁇ , ⁇ 331 ⁇ , ⁇ 420 ⁇ Calculate the X-ray diffraction intensity ratio of ⁇ 200 ⁇ out of the four X-ray diffraction intensities on the first side.
- the X-ray diffraction strength of each surface group was measured and measured as shown in the following formula (1) ⁇ 200 ⁇ , ⁇ 11 1 ⁇ , ⁇ 220 ⁇ and ⁇ 311 ⁇ , find the sum of the X-ray diffraction intensities (I, 1, I, I)
- the ratio of the X-ray diffraction intensity (I) of ⁇ 200 ⁇ to the sum is the X-ray diffraction intensity ratio.
- this X-ray diffraction intensity ratio needs to be 0.4 or more.
- the X-ray diffraction intensity can be measured using a general-purpose X-ray diffraction apparatus.
- the X-ray diffraction intensity ratio is 0.4 or more, it is easy to uniformly generate plastic deformation in a direction parallel to the rolling direction of the aluminum alloy brazing sheet 1 for heat exchangers. Even when repeated stress is applied, deformation does not concentrate locally, and the progress of cracks in the thickness direction can be delayed, so that it is possible to improve the life including fatigue in the plastic region. Become. On the other hand, when the X-ray diffraction intensity ratio is less than 0.4, the above-described effect cannot be obtained.
- the X-ray diffraction strength ratio of the aluminum alloy brazing sheet 1 for heat exchanger of the present invention is 0.4 or more.
- ⁇ 100 ⁇ of the aluminum alloy can be strongly oriented in parallel with the plate surface, so that in deformation in the plastic region, easily generates plastic deformation in a direction parallel to the rolling direction of the brazing sheet.
- ⁇ 100 ⁇ is strongly oriented parallel to the surface of the plate, which makes it easier to activate multiple sliding surfaces at the same time. It becomes possible to delay the progress of cracks in the direction.
- the core material 2 of the brazing sheet 1 made of an aluminum alloy for a heat exchanger according to the present invention is configured using an Al-Mn alloy.
- the core material 2 that can be used in the present invention is not limited to this.
- An A1-Mn alloy containing Cu or Si can also be used.
- the core material 2 can be used in an amount of 0.2 to 0.8 mass%.
- An Al—Mn alloy containing Mg, or an A1—Mn alloy further containing 0.2 to 0.8 mass% Mg, and Cu or Si can be used.
- an aluminum alloy provided with an intermediate layer (not shown) containing no Mg between the brazing material 4 and the core material 2 or between the core material 2 and the skin material 3 can also be used. .
- the skin material 3 of the brazing sheet 1 made of an aluminum alloy for a heat exchanger according to the present invention includes an Al—Zn alloy, an Al—Zn—Mg alloy, an Al—Si—Mn—Zn alloy as described above.
- An alloy or an Al—Si—Mn—Mg—Zn alloy is used.
- the skin material 3 that can be used in the present invention is not limited to this Al—Zn alloy, In—Sn—Mg alloy, Al—Si—Mn— containing In or Sn.
- Zn-based, Al-Si-Mn-Mg-Zn-based alloys can be used.
- composition range for use as a skin material of the present invention for example, A1- 2. 5 ⁇ 5. 5 wt% Zn, A1- 0. 2 ⁇ 1. 2 mass 0/0 Si- 0. 1 ⁇ 1 . 5 mass% Mn, 2. 5 to 5. 5 mass 0/0 Zn, A1- 0. 2 ⁇ 1 . 2 wt% Si- 0. 2 to 3. 5 wt% Mg, 1. 5 to 5. 5 mass% Zn etc. are mentioned.
- the thickness of the skin material is not particularly limited, but is usually 30 to: LOOmm.
- the brazing material 4 of the aluminum alloy brazing sheet 1 for a heat exchanger according to the present invention is configured using the A1-S engagement gold as described above.
- the brazing material 4 that can be used in the present invention is not limited to this, and an Al—Si alloy containing Cu, Zn, or the like having a low melting point can also be used.
- the aluminum alloy brazing sheet 1 for a heat exchanger has the skin material 3 disposed on one side surface of the core material 2 and the brazing material 4 disposed on the other side surface of the core material 2, and this is homogeneous. After the chemical treatment, it is hot-rolled and clad, appropriately subjected to intermediate annealing at 210 to 300 ° C, and finish cold rolling with a finish cold rolling rate of 5% or more and less than 22% can be produced. [0025] [Aluminum alloy tube for heat exchanger]
- an aluminum alloy tube 11 for a heat exchanger includes an A1-Mn alloy core 2 and an A1-Zn alloy clad on one side of the core 2, A1-Zn— Mg alloy, Al—Si—Mn—Zn, Al—Si—Mn—Mg—Zn alloy skin 3 and A1—S engagement gold brazing material 4 clad on the other side of the core 2
- the aluminum alloy brazing sheet 1 for heat exchangers is produced using, and the aluminum alloy brazing sheet 1 for heat exchangers is bent in the width direction by a forming roll or the like, and the skin material 3 is arranged on the inner surface side of the pipe.
- the tube tube After being formed into a flat tube so as to be placed, this is electro-welded and formed into a flat tube.
- the tube tube is formed into a flat tube shape as shown in FIG. 6, for example, by a forming roll, and the tube is brazed and closed in the brazing process.
- a flat tubular tube 11 ′ may be used.
- this aluminum alloy tube 11 for heat exchanger is assembled by brazing together using radiating fins 12 subjected to corrugation processing and other members such as header 13, and 585 to 620 °
- Heat exchange such as the radiator 10 can be produced by brazing by heating to a high temperature of C, preferably 590 to 600 ° C.
- the heating temperature in the present invention is 585 ° C or higher, preferably 590 ° C or higher.
- the heating temperature in the present invention is set to 620 ° C. or less.
- the aluminum alloy tube 11 for heat exchanger of the present invention needs to satisfy the following formula (2) in the X-ray diffraction intensity ratio when brazing heating at 585 to 620 ° C is performed.
- the X-ray diffraction intensity ratio of the aluminum alloy tube 11 for heat exchanger of the present invention is 0.3 or more.
- the aluminum alloy composition of the core material and the skin material and the production conditions can be appropriately adjusted.
- Sample materials A, B, and C all have the same composition.
- Test materials A, B, C of the core material Si;. 0 81 wt%, Fe;. 0 18 wt%, Cu;. 0 82 mass 0/0
- Mn Mn; l. 5% by mass, Mg; 0.04% by mass, Ti; 0.12% by mass, and the balance being Al.
- test materials A, B, and C an aluminum alloy containing Si: 0.79% by mass, Mn: 1.1% by mass, Zn: 4.0% by mass and the balance being A1 was used. .
- test materials A, B, and C an aluminum alloy containing Si: 10.5% by mass and the balance being A1 was used.
- Test materials A, B, and C having such a composition are fabricated by a conventional method (temperature: 680 to 750 ° C for both the core material, the skin material, and the brazing material), and then homogenized (for example, the core material and the skin).
- the material is 450 to 590 ° CX for 10 hours, the brazing material is 450 to 520 ° C for 10 hours, and then hot-rolled and clad (temperature: 400 ° C or more, finished hot rolled and the thickness is 3 mm), Interim annealing (temperature shown in Table 1) is performed as appropriate, and finish cold rolling at the finish cold rolling rate shown in Table 1 is performed, so that a brazing made of aluminum alloy for a 3-layer heat exchanger with a thickness of 0.2 mm each Sheets (flat specimens A, B, C) were prepared.
- Specimens A, B, C before heating to brazing heating temperature (600 ° C) and Specimens A, B after heating to brazing heating temperature (600 ° C) , C, and X-ray diffraction strength were measured.
- the X-ray diffraction intensity was measured using an X-ray diffractometer (RAD-B system, manufactured by Rigaku Corporation), using a plane perpendicular to the rolling surface from the skin material side, which is an A1-Mn-Si-Zn alloy. And an X-ray is incident in a plane in which the intersecting line between the plane and the rolling plane is parallel to the rolling direction, and an equivalent plane group ⁇ 111 ⁇ , ⁇ 200 ⁇ , ⁇ 220 by the ⁇ -2 ⁇ method ⁇ And ⁇ 311 ⁇ X-ray diffraction intensities I, I
- the X-ray diffraction intensity ratio ⁇ of the specimens A, B, and C obtained by the above equation (4) is determined to be excellent ( ⁇ ) if the X-ray diffraction intensity ratio ⁇ is 0.3 or more. A value of less than 0.3 was judged as defective (X).
- the number of repeated fractures was determined by the single swing plane bending fatigue test shown in FIG. In addition, it is explanatory drawing explaining a single swing plane bending fatigue test.
- test piece set length was adjusted so that the maximum strain amount at the fracture portion was about 0.008. Under such conditions, the number of repetitions until the specimens of specimens A, B, and C broke was obtained.
- the strain gauge cannot be applied directly to the rupture site for the amount of strain at the rupture part, the strain gauge is applied to a predetermined position at a few locations at a slight distance from the rupture site force.
- the strain amount at the fracture site was estimated by interpolating the strain amount at the fracture site from the strain value of the strain gauge at the half length, and the load stress, that is, the test piece set length was adjusted based on this.
- specimen A has an appropriate composition and manufacturing conditions for the aluminum alloy of the core material, skin material, and brazing material, and further, the X-ray diffraction intensity ratio before heating equivalent to brazing and the equivalent of brazing. Since the X-ray diffraction intensity ratio after heating was also appropriate, good evaluation results could be obtained in terms of the number of repeated fractures equivalent to brazing.
- the deformation did not concentrate locally, and the progress of cracks in the thickness direction could be delayed, so the life including fatigue in the plastic region (the number of repetitions of fracture at a strain of 0.008) was improved. .
- test materials B and C although the composition of each aluminum alloy of the core material, the skin material, and the brazing material was appropriate, the manufacturing conditions were not appropriate, and further, before the heating equivalent to brazing. Since the X-ray diffraction strength ratio and the X-ray diffraction intensity ratio after heating equivalent to brazing were also appropriate, the number of repetitions of fracture equivalent to brazing was small, and a force that could not give good evaluation results. I got it.
- the test material B had a high finish annealing ratio and a high intermediate annealing temperature, the intensity ratio of the X-ray diffraction intensity before heating equivalent to brazing and the equivalent of brazing The X-ray diffraction intensity ratio after heating decreased. Therefore, in the deformation in the plastic region due to repeated bending, it was difficult to uniformly generate plastic deformation in the direction parallel to the rolling direction of the specimen B.
- sample C had a high finish cold rolling ratio, so the X-ray diffraction intensity ratio before heating equivalent to brazing and the X-ray diffraction intensity ratio after heating equivalent to brazing were low. Natsuta. For this reason, in the deformation in the plastic region due to repeated bending, plastic deformation in the direction parallel to the rolling direction of specimen C was uniformly generated, which was difficult. In other words, the deformation concentrated locally and the progress of cracks in the thickness direction could not be delayed, so the life including fatigue in the plastic region (the number of repetitions of fracture at a strain of 0.008) was improved. I helped.
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Abstract
Description
Claims
Priority Applications (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB0718179A GB2438358B (en) | 2005-04-12 | 2006-04-03 | Aluminum alloy brazing sheet and aluminum alloy heat exchanger tube |
| US11/911,290 US8062764B2 (en) | 2005-04-12 | 2006-04-03 | Aluminum alloy brazing sheet and aluminum alloy tube for heat exchanger |
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP2005115167A JP4056014B2 (ja) | 2005-04-12 | 2005-04-12 | アルミニウム合金製ブレージングシートおよび熱交換器用アルミニウム合金製チューブ |
| JP2005-115167 | 2005-04-12 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| WO2006109602A1 true WO2006109602A1 (ja) | 2006-10-19 |
Family
ID=37086881
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| PCT/JP2006/307031 Ceased WO2006109602A1 (ja) | 2005-04-12 | 2006-04-03 | アルミニウム合金製ブレージングシートおよび熱交換器用アルミニウム合金製チューブ |
Country Status (6)
| Country | Link |
|---|---|
| US (1) | US8062764B2 (ja) |
| JP (1) | JP4056014B2 (ja) |
| CN (1) | CN100529131C (ja) |
| CZ (1) | CZ304647B6 (ja) |
| GB (1) | GB2438358B (ja) |
| WO (1) | WO2006109602A1 (ja) |
Families Citing this family (23)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US8274014B2 (en) | 2006-05-25 | 2012-09-25 | Bellman-Melcor Development, Llc | Filler metal with flux for brazing and soldering and method of making and using same |
| JP4111456B1 (ja) * | 2006-12-27 | 2008-07-02 | 株式会社神戸製鋼所 | 熱交換器用アルミニウム合金ブレージングシート |
| JP4181607B2 (ja) | 2007-03-29 | 2008-11-19 | 株式会社神戸製鋼所 | アルミニウム合金製ブレージングシートおよびその製造方法 |
| JP4473908B2 (ja) * | 2007-12-27 | 2010-06-02 | 株式会社神戸製鋼所 | 熱交換器用アルミニウム合金クラッド材、および、その製造方法 |
| CN102644009B (zh) | 2008-02-12 | 2015-04-01 | 株式会社神户制钢所 | 铝合金层合板 |
| JP5577616B2 (ja) * | 2009-04-06 | 2014-08-27 | 株式会社デンソー | 熱交換器用チューブ及び熱交換器 |
| JP5610714B2 (ja) * | 2009-06-24 | 2014-10-22 | 株式会社Uacj | アルミニウム合金製熱交換器 |
| JP5411649B2 (ja) * | 2009-10-13 | 2014-02-12 | 株式会社神戸製鋼所 | 熱交換器用アルミニウムクラッド材 |
| JP5491927B2 (ja) * | 2010-03-29 | 2014-05-14 | 株式会社神戸製鋼所 | アルミニウム合金ブレージングシート |
| US8247084B2 (en) * | 2010-05-18 | 2012-08-21 | Kobe Steel, Ltd. | Aluminum alloy brazing sheet |
| JP6216964B2 (ja) * | 2011-08-09 | 2017-10-25 | 三菱アルミニウム株式会社 | 冷却器用クラッド材および発熱素子用冷却器 |
| JP5750077B2 (ja) * | 2012-03-16 | 2015-07-15 | 株式会社神戸製鋼所 | 熱交換器用アルミニウム合金ブレージングシート |
| US20150144309A1 (en) * | 2013-03-13 | 2015-05-28 | Brayton Energy, Llc | Flattened Envelope Heat Exchanger |
| DE102013102821A1 (de) * | 2013-03-19 | 2014-09-25 | Hydro Aluminium Rolled Products Gmbh | Verfahren zur Herstellung eines walzplattierten Aluminiumwerkstücks, walzplattiertes Aluminiumwerkstück und Verwendung dafür |
| US9731383B2 (en) | 2014-07-09 | 2017-08-15 | Bellman-Melcor Development, Llc | Filler metal with flux for brazing and soldering and method of using same |
| JP6498911B2 (ja) * | 2014-11-10 | 2019-04-10 | 三菱アルミニウム株式会社 | 高強度・高耐食性・素材高伸びを有するアルミニウム合金ブレージングシート |
| WO2016172674A1 (en) * | 2015-04-24 | 2016-10-27 | Engineered Materials Solutions, Llc | Self brazing material and a method of making the material |
| JP6564620B2 (ja) * | 2015-06-02 | 2019-08-21 | 株式会社ケーヒン・サーマル・テクノロジー | 熱交換器およびその製造方法 |
| JP6570325B2 (ja) * | 2015-06-04 | 2019-09-04 | 株式会社Uacj | アルミニウム合金クラッド材およびろう付け方法 |
| US10744601B2 (en) | 2015-08-07 | 2020-08-18 | Bellman-Melcor Development, Llc | Bonded brazing ring system and method for adhering a brazing ring to a tube |
| CN108290251A (zh) * | 2015-11-13 | 2018-07-17 | 格朗吉斯铝业(上海)有限公司 | 钎焊板材 |
| CN106735660A (zh) * | 2016-12-14 | 2017-05-31 | 无锡银邦防务科技有限公司 | 一种钎焊蜂窝板面板用高强铝合金复合板、芯材、包覆层及皮材 |
| CN111566240B (zh) * | 2018-03-27 | 2021-09-07 | 古河电气工业株式会社 | 铝合金材料以及使用其的导电构件、电池用构件、紧固部件、弹簧用部件及结构用部件 |
Citations (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH108176A (ja) * | 1996-04-25 | 1998-01-13 | Nippon Light Metal Co Ltd | 耐力が低く極限変形能に優れたアルミニウム合金板およびその製造方法 |
Family Cites Families (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US6129143A (en) * | 1996-08-08 | 2000-10-10 | Denso Corporation | Brazing sheet having an excellent corrosion resistance for use in a heat exchanger, and a heat exchanger using the same |
| JP3533434B2 (ja) | 1996-08-09 | 2004-05-31 | 古河スカイ株式会社 | アルミニウム合金製熱交換器用ブレージングシート |
| CZ9902568A3 (cs) * | 1998-01-21 | 2001-06-13 | Alcan Int Ltd | Aktivní část tepelného výměníku na bázi hliníku a způsob jeho výroby |
| JP3494591B2 (ja) * | 1999-06-23 | 2004-02-09 | 株式会社デンソー | 耐食性が良好な真空ろう付け用アルミニウム合金ブレージングシート及びこれを使用した熱交換器 |
| US6555251B2 (en) * | 2000-12-21 | 2003-04-29 | Alcoa Inc. | Multi-layer, heat treatable brazing sheet with aluminum interlayer |
| JP2005016937A (ja) * | 2003-06-06 | 2005-01-20 | Denso Corp | 耐食性に優れたアルミニウム製熱交換器 |
| JP4220411B2 (ja) * | 2004-02-18 | 2009-02-04 | 住友軽金属工業株式会社 | 熱交換器用アルミニウム合金クラッド材 |
| CZ2007387A3 (cs) * | 2007-06-05 | 2008-12-17 | Visteon Global Technologies, Inc. | Zpusob výroby komory pro tepelné výmeníky automobilu a komora vytvorená tímto zpusobem |
-
2005
- 2005-04-12 JP JP2005115167A patent/JP4056014B2/ja not_active Expired - Fee Related
-
2006
- 2006-04-03 GB GB0718179A patent/GB2438358B/en not_active Expired - Fee Related
- 2006-04-03 CN CNB2006800116478A patent/CN100529131C/zh not_active Expired - Fee Related
- 2006-04-03 WO PCT/JP2006/307031 patent/WO2006109602A1/ja not_active Ceased
- 2006-04-03 US US11/911,290 patent/US8062764B2/en not_active Expired - Fee Related
- 2006-04-03 CZ CZ2007-615A patent/CZ304647B6/cs not_active IP Right Cessation
Patent Citations (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH108176A (ja) * | 1996-04-25 | 1998-01-13 | Nippon Light Metal Co Ltd | 耐力が低く極限変形能に優れたアルミニウム合金板およびその製造方法 |
Also Published As
| Publication number | Publication date |
|---|---|
| US20090020276A1 (en) | 2009-01-22 |
| CZ304647B6 (cs) | 2014-08-20 |
| GB2438358B (en) | 2010-10-20 |
| CN101155937A (zh) | 2008-04-02 |
| GB0718179D0 (en) | 2007-10-31 |
| US8062764B2 (en) | 2011-11-22 |
| GB2438358A (en) | 2007-11-21 |
| CN100529131C (zh) | 2009-08-19 |
| CZ2007615A3 (cs) | 2008-03-05 |
| JP2006291311A (ja) | 2006-10-26 |
| JP4056014B2 (ja) | 2008-03-05 |
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