Brazing sheet, articles formed from brazing sheet, and methods of forming articles

Abstract

A brazing sheet, an article formed from or including all or a portion of the brazing sheet, and a method of forming the article are provided. The brazing sheet includes a core layer, a brazing layer, and an interliner layer intermediate the core layer and the brazing layer. The core layer includes a first aluminum alloy, the core layer being at least partially recrystallized. The brazing layer includes a 4XXX series aluminum alloy. The interliner layer includes a second aluminum alloy, the interliner layer being not recrystallized.

Description

[Technical field]

[0001] <Cross reference> This application claims the benefit under 35 U.S.C. § 119(e) of U.S. Provisional Patent Application No. 63 / 228,740, filed August 3, 2021, and U.S. Provisional Patent Application No. 63 / 266,367, filed January 4, 2022, the entire disclosures of which are incorporated herein by reference.

[0002] The present disclosure relates to brazing sheets, articles of manufacture formed from or including all or a portion of a brazing sheet, and methods of forming the articles of manufacture. [Background technology]

[0003] For example, various devices such as heat exchangers can be formed from specially designed metal plates that are stacked. Plate type heat exchangers function by circulating two fluids (e.g., liquids, refrigerants, or a combination thereof) on either side of the plates, allowing heat exchange between the fluids across the plates. To ensure that plate type heat exchangers have acceptable corrosion resistance, the devices can be designed to resist corrosive attack along the joints between the plates and through the thickness of the sheet material used to form the plates. Increasing resistance to corrosive attack in plate type heat exchangers can present significant challenges. Summary of the Invention

[0004] One non-limiting aspect according to the present disclosure is directed to a brazing sheet including a core layer, a brazing layer, and an interliner layer intermediate the core layer and the brazing layer. In various non-limiting embodiments, the brazing sheet has a structure suitable for at least one of controlled atmosphere brazing and vacuum brazing. The core layer of the brazing sheet may be, for example, 1 cm thick. 2The interliner layer of the brazing sheet is at least partially recrystallized to contain a dislocation density of 10,000,000 or less per cm. The interliner layer of the brazing sheet is not recrystallized, so that, for example, the interliner layer is 2 The brazing sheet core layer includes a first aluminum alloy, such as a 3XXX series aluminum alloy or a 6XXX series aluminum alloy. For example, in certain non-limiting embodiments, the first aluminum alloy includes, in weight percent based on the total weight of the first aluminum alloy, 0-1.2 silicon, 0-1.0 copper, 0-0.25 zirconium, 0-0.8 iron, 0-2.0 manganese, 0-3.0 zinc, 0-1.5 magnesium, 0-0.25 titanium, 0-0.3 chromium, 0-0.5 bismuth, aluminum, and impurities. The brazing sheet interliner includes a second aluminum alloy. In various non-limiting embodiments, the second aluminum alloy includes, in weight percent based on the total weight of the second aluminum alloy, at least 0.01 zirconium. In various non-limiting embodiments, the first aluminum alloy has a first recrystallization temperature and the second aluminum alloy has a second recrystallization temperature, the second recrystallization temperature being greater than the first recrystallization temperature. The brazing layer of the brazing sheet comprises a 4XXX series aluminum alloy. In various non-limiting embodiments, the brazing layer comprises a 4XXX series aluminum alloy including, in weight percent based on the total weight of the 4XXX series aluminum alloy, 5-15 silicon, 0-2.0 magnesium, 0-1.0 iron, 0-3.0 zinc, 0-2.0 copper, 0-1.0 manganese, 0-0.2 titanium, 0-0.3 bismuth, aluminum, and impurities. As used herein, the "recrystallization temperature" of a material is the lowest temperature at which at least 90% of the material is fully recrystallized when the material is heated at that temperature for a period of one hour or less. The recrystallization temperature may depend on the material composition of the sheet material and the amount of strain in the grains of the sheet material.

[0005] Yet another non-limiting aspect according to the present disclosure is directed to a method for forming a brazing sheet according to the present disclosure. The method includes homogenizing a core layer to form a homogenized core layer and hot working a workpiece including a 3XXX series aluminum alloy to form at least one interliner layer. The method further includes hot rolling the at least one brazing layer, the at least one interliner layer, and the homogenized core layer together to form a brazing sheet.

[0006] In certain non-limiting embodiments of a brazing sheet according to the present disclosure, the core layer of the brazing sheet comprises a first thickness in the range of 60%-90% of the total thickness of the brazing sheet, the interliner layer of the brazing sheet comprises a second thickness in the range of 3%-20% of the total thickness of the brazing sheet, and the brazing layer of the brazing sheet comprises a third thickness in the range of 3%-20% of the total thickness of the brazing sheet. In various non-limiting embodiments, the brazing sheet further comprises a second brazing layer and / or a second interliner layer.

[0007] An additional non-limiting aspect of the present disclosure is directed to a heat exchanger that includes all or a portion of an embodiment of a brazing sheet according to the present disclosure. In certain non-limiting embodiments, the heat exchanger is an oil cooler or a liquid cooled condenser.

[0008] Yet another non-limiting aspect according to the present disclosure is directed to a method for forming an article. The method includes contacting a first portion including a first material with a second portion including all or a portion of an embodiment of a brazing sheet according to the present disclosure. The first portion is bonded to the second portion by a process including at least one of controlled atmosphere brazing and vacuum brazing. In various non-limiting embodiments, the first material includes aluminum or an aluminum alloy. In certain non-limiting embodiments, the article is a heat exchanger, such as, for example, an oil cooler or a liquid cooled condenser.

[0009] It is to be understood that the invention disclosed and described herein is not limited to the aspects summarized in this Summary, and the reader will appreciate the foregoing details as well as other details in light of the following detailed description of various non-limiting and non-exhaustive aspects hereof. [Brief description of the drawings]

[0010] The features and advantages of the embodiments described herein, and the manner in which they are accomplished, will become more apparent and the embodiments will be better understood by referring to the following description in conjunction with the accompanying drawings, in which:

[0011] [Figure 1] FIG. 1 is a schematic side view of a non-limiting embodiment of a brazing sheet according to the present disclosure.

[0012] [Diagram 2] FIG. 1 is a schematic side view of a non-limiting embodiment of a brazing sheet according to the present disclosure.

[0013] [Diagram 3] FIG. 1 is a schematic side view of a non-limiting embodiment of a brazing sheet according to the present disclosure.

[0014] [Figure 4] FIG. 2 is a schematic perspective view illustrating a non-limiting embodiment of cold rolling an embodiment of a material layer according to the present disclosure.

[0015] [Figure 5A] 1 is a photomicrograph showing a cross-sectional side view of a portion of a layer of material including an aluminum alloy that has not been recrystallized.

[0016] [Figure 5B] 1 is a photomicrograph illustrating a cross-sectional side view of a portion of a layer of material that includes an aluminum alloy and that has been at least partially recrystallized.

[0017] [Figure 5C]1 is a photomicrograph showing a cross-sectional side view of a portion of a layer of material that includes an aluminum alloy and is fully recrystallized.

[0018] [Figure 6] FIG. 1 is a block diagram of a non-limiting embodiment of a method according to the present disclosure for forming an article from a material including a brazing sheet.

[0019] [Figure 7A] 1 is a photomicrograph showing a cross-sectional side view of a portion of a comparative brazing sheet including an interliner layer that has been at least partially recrystallized.

[0020] [Figure 7B] 7B provides a photomicrograph showing a cross-sectional side view of a portion of the comparative brazing sheet of FIG. 7A.

[0021] [Figure 8A] 1 is a photomicrograph showing a cross-sectional side view of a portion of a non-limiting embodiment of a brazing sheet according to the present disclosure, including a non-recrystallized interliner layer.

[0022] [Figure 8B] 8B provides a photomicrograph showing a cross-sectional side view of a portion of the brazing sheet of FIG. 8A.

[0023] [Figure 9A] 1 is a grain orientation map of a first sample that has not been recrystallized.

[0024] [Figure 9B] FIG. 9B is a kernel average orientation difference (KAM) map of the first sample shown in FIG. 9A.

[0025] [Figure 10A] 13 is a grain orientation map of a second sample that has not been recrystallized.

[0026] [Figure 10B]FIG. 10B is a KAM map of the first sample shown in FIG. 10A.

[0027] [Figure 11A] 13 is a grain orientation map of a third sample that has been at least partially recrystallized.

[0028] [Figure 11B] FIG. 11B is a KAM map of the third sample shown in FIG. 11A.

[0029] [Figure 12A] 13 is a grain orientation map of a fourth sample that is significantly recrystallized.

[0030] [Figure 12B] FIG. 12B is a KAM map of the fourth sample shown in FIG. 12A.

[0031] [Figure 13] FIG. 1 is a system diagram illustrating how the electron beam of a scanning electron microscope scans the surface of a sample layer to obtain a Kikuchi pattern from each discrete sampling spot.

[0032] [Figure 14] FIG. 13 is a system diagram illustrating how EBSD can be used to create a KAM map based on the orientation difference between data points to determine the strain of a sample.

[0033] [Figure 15A] 1 is a grain orientation map of a non-limiting embodiment of a brazing sheet according to the present disclosure.

[0034] [Figure 15B] 15B is a KAM map of the brazing sheet shown in FIG. 15A.

[0035] [Figure 16A] 1 is a grain orientation map of a non-limiting embodiment of a brazing sheet according to the present disclosure.

[0036] [Figure 16B] 16B is a KAM map of the brazing sheet shown in FIG. 16A.

[0037] [Figure 17] FIG. 2 is a block diagram of a non-limiting embodiment of a method according to the present disclosure for forming a brazing sheet.

[0038] [Figure 18A] 1 is a grain orientation map of a comparative brazing sheet produced that includes an O-tempered interliner layer that is at least partially recrystallized.

[0039] [Figure 18B] 18A provides a photomicrograph showing a cross-sectional side view of a portion of two comparative brazing sheets of FIG. 18A after the brazing process with dashed lines indicating the joint width.

[0040] [Figure 19A] 1 is a grain orientation map of a non-limiting embodiment of a fabricated brazing sheet including a non-recrystallized H-tempered interliner layer.

[0041] [Figure 19B] FIG. 19B is a photomicrograph showing a cross-sectional side view of a portion of the two brazing sheets of FIG. 19A after the brazing process with the dashed brown bands showing.

[0042] The examples set forth herein illustrate particular embodiments in one or more forms, and such examples should not be construed in any manner as limiting the scope of the appended claims. DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS

[0043] Various embodiments are described and illustrated herein to provide a general understanding of the structure, function, and use of the disclosed articles and methods. The various embodiments described and illustrated herein are non-limiting and non-exhaustive. Therefore, the present invention is not limited by the description of the various non-limiting and non-exhaustive embodiments disclosed herein. Rather, the present invention is defined only by the claims. The features and characteristics illustrated and / or described in connection with the various embodiments may be combined with the features and characteristics of other embodiments. Such modifications and variations are intended to be included within the scope of the present specification. Accordingly, the claims may be amended to recite any feature or characteristic explicitly or inherently described or otherwise explicitly or inherently supported herein. Furthermore, applicants reserve the right to amend the claims to affirmatively disclaim any feature or characteristic that may exist in the prior art. The various embodiments disclosed and described herein may comprise, consist of, or consist essentially of the features and characteristics variously described herein.

[0044] Reference herein to "various embodiments," "some embodiments," "one embodiment," "embodiment," "non-limiting embodiment," or similar phrases means that a particular feature, structure, or characteristic described in connection with the examples is included in at least one embodiment. Thus, appearances of the phrases "various embodiments," "some embodiments," "in one embodiment," "in an embodiment," "non-limiting embodiment," or similar phrases herein do not necessarily refer to the same embodiment. Furthermore, particular described features, structures, or characteristics may be combined in any suitable manner in one or more embodiments. Thus, a particular feature, structure, or characteristic illustrated or described in connection with one embodiment may be combined, in whole or in part, without limitation, with the feature, structure, or characteristic of one or more other embodiments. Such modifications and variations are intended to be included within the scope of the present embodiments.

[0045] The H-tempered core layer in the brazing sheet is not typically homogenized and can develop brown bands that may be resistant to corrosion. As used herein, H-temper has the meaning given in ANSI H35.1 / H35.1(M)-2017. The brown bands can form in the core layer when silicon diffuses from the brazing layer into the core layer and precipitates with the manganese and iron in solid solution during the brazing process. The brown bands in the core layer are caused by small-scale Al-containing deposits that form a band near the interface between the brazing layer and the core layer. x Mn y S z Or Al x (Mn, Fe) y S z The formation of a dispersion at the interface pulls the manganese out of solid solution and creates a more electrochemically negative area in the brazing sheet that is anodic relative to the center of the brazing sheet, thereby increasing the overall corrosion resistance of the H-tempered core layer. However, the H-tempered core layer can have relatively poor formability characteristics, which can create challenges when incorporating the brazing sheet into a manufactured product.

[0046] An O-tempered core layer in a brazing sheet may be easier to form (e.g., softer) than an H-tempered core layer, facilitating the manufacture of products incorporating the brazing sheet. As used herein, O-tempered has the meaning given in ANSI H35.1 / H35.1(M)-2017. One example of a brazing sheet including an O-tempered core layer is described in U.S. Pat. No. 7,255,932, which is incorporated herein by reference. Although having relatively favorable formability properties, an O-tempered core layer may be more susceptible to corrosion than an H-tempered core layer.

[0047] The present disclosure provides a brazing sheet that may have advantageous formability properties, corrosion resistance, and liquid film transfer resistance. The brazing sheet may include a core layer, a brazing layer, and an interliner layer intermediate the core layer and the brazing layer. The core layer may include a first aluminum alloy and may be at least partially recrystallized. The brazing layer includes a 4XXX series aluminum alloy. The interliner layer may include a second aluminum alloy and may not be recrystallized.

[0048] The term "core layer" as used herein refers to a substrate layer of a brazing sheet. In various non-limiting embodiments, the "core layer" can be disposed substantially at the center of the brazing sheet. However, the location of the core layer in a brazing sheet according to the present disclosure is not limited to the center of the brazing sheet. The core layer may or may not be covered on both sides with another layer of the brazing sheet, for example, the core layer may be disposed on one side of the brazing sheet and exposed. Thus, in various non-limiting embodiments of the brazing sheet herein, the core layer may be surrounded by other layers of the brazing sheet, may have at least one side at least partially exposed, or may have at least one side completely exposed.

[0049] 1, a brazing sheet 100 is provided. The brazing sheet 100 includes a core layer 102, a brazing layer 104, and an interliner layer 106 disposed intermediate the core layer 102 and the brazing layer 104. In various non-limiting embodiments, the core layer 102, the interliner layer 106, and the brazing layer 104 are bonded together to form the brazing sheet 100. The brazing sheet 100 can have a composition and thickness suitable for at least one of controlled atmosphere brazing and vacuum brazing.

[0050] The brazing layer 104 of the brazing sheet 100 includes an aluminum alloy, such as, for example, a 4XXX series aluminum alloy. In various non-limiting embodiments, the brazing layer 104 includes an aluminum alloy including, in weight percent based on the total weight of the aluminum alloy, 5.0-15 silicon, 0-2.0 magnesium, 0-1.0 iron, 0-3.0 zinc, 0-2.0 copper, 0-1.0 manganese, 0-0.2 titanium, 0-0.3 bismuth, aluminum, and impurities.

[0051] The core layer 102 of the brazing sheet 100 includes an aluminum alloy, such as, for example, a 3XXX series aluminum alloy or a 6XXX series aluminum alloy. In various non-limiting embodiments, the core layer 102 includes a first aluminum alloy including, in weight percent based on the total weight of the first aluminum alloy, 0-1.2 silicon, 0-1.0 copper, 0-0.25 zirconium, 0-0.8 iron, 0-2.0 manganese, 0-3.0 zinc, 0-1.5 magnesium, 0-0.25 titanium, 0-0.3 chromium, 0-0.5 bismuth, aluminum, and impurities.

[0052] The concentration of silicon present in the aluminum alloy can affect the recrystallization temperature of the aluminum alloy. In certain non-limiting embodiments, the first aluminum alloy includes 0-0.6 silicon, 0-0.2 silicon, 0.05-1.2 silicon, 0.05-0.6 silicon, or 0.05-0.2 silicon, in weight percent based on the total weight of the first aluminum alloy. The core layer 102 can be at least partially recrystallized, and in various non-limiting embodiments, the core layer 102 can be an O-tempered core layer and / or homogenized.

[0053] 1, the interliner layer 106 of the brazing sheet 100 includes an aluminum alloy, such as a second aluminum alloy, including at least 0.01 zirconium, aluminum, and impurities, in weight percent based on the total weight of the second aluminum alloy. The zirconium in the aluminum alloy of the interliner layer 106 can inhibit recrystallization in the interliner layer 106. In various non-limiting embodiments, the interliner layer 106 of the brazing sheet 100 includes a second aluminum alloy including, in weight percent based on the total weight of the aluminum alloy, 0.05-1.5 silicon, 0-2 copper, 0.01-0.5 zirconium, 0-0.8 iron, 0-2.0 manganese, 0-3.0 zinc, 0-2.0 magnesium, 0-0.3 titanium, 0-1.0 chromium, 0-0.5 bismuth, aluminum, and impurities. The interliner layer 106 can be homogenized or non-homogenized. In certain non-limiting embodiments, the interliner layer 106 includes a composition suitable for forming a brown band. The interliner layer 106 can be an amorphous and / or H-tempered interliner layer.

[0054] Silicon can reduce the resistance of the aluminum alloy to recrystallization. The inventors of the present disclosure have determined that there are various factors that can affect the recovery and recrystallization kinetics of the aluminum alloy and thereby the recrystallization temperature of the aluminum alloy (e.g., reducing the recovery and recrystallization kinetics increases the recrystallization temperature of the aluminum alloy). For example, stabilizing the dislocation core through reduction of the core stress field can affect the slip process and the resulting recovery and recrystallization kinetics. In various non-limiting embodiments, solutes that can inhibit recrystallization can include atomic radii larger than aluminum (118 picometers (pm)), such as, for example, manganese (161 pm), chromium (166 pm), vanadium (171 pm), and zirconium (206 pm). While not intending to be bound by any particular theory, it is believed that solutes with large atomic radii can decorate the dislocation core, thereby reducing tensile stress, increasing the activation barrier for dislocation slip, and reducing the recovery and recrystallization kinetics. In various non-limiting embodiments, silicon may be less effective at reducing the slip process compared to manganese, chromium, vanadium, and zirconium because the atomic radius of silicon (111 pm) is actually smaller than the atomic radius of aluminum (118 pm). The inventors of the present disclosure have determined that solutes that diffuse slower in aluminum than silicon may inhibit the recrystallization of aluminum alloys. Slower diffusing solutes may reduce dislocation climb processes in aluminum alloys, thereby reducing recovery and recrystallization kinetics. Increased core stress fields may further destabilize dislocation glide. Silicon may be a faster diffuser compared to manganese, chromium, vanadium, and zirconium, thereby enhancing the climb process which further increases recovery and recrystallization kinetics.

[0055] The recovery of the aluminum alloy may require the relocation of dislocation cores into a defined cell structure through slip and climb process kinetics. The defined cell structure may act as a nucleation site for the formation of new crystal orientations within the deformed parent grains of the aluminum alloy. The recovery of the aluminum alloy may then lead to the recrystallization of the aluminum alloy. The slower the diffusion rate and the larger the atomic radius of the solute present in the dislocation core, the more enhanced the stabilization of the dislocation core may be, and the slower the recovery of the aluminum alloy. This may allow the use of heat treatments on the aluminum alloy while maintaining the aluminum alloy in a non-recrystallized form.

[0056] Fast diffusing solute atoms (e.g., diffusion distance of at least 60 μm at 600° C. in aluminum after 100 minutes), such as magnesium and zinc, may not be very effective in reducing dislocation climb kinetics. Fast diffusing solutes may therefore not contribute significantly to inhibiting recrystallization. Slow diffusing solute atoms (e.g., diffusion distance of 10 μm or less at 600° C. in aluminum after 100 minutes), such as manganese, chromium, vanadium, zirconium, and titanium, can reduce dislocation climb kinetics if the slow diffusing solutes are segregated to the dislocation core by reduced mobility.

[0057] In various non-limiting embodiments, zirconium can form nanoscale L12 order simple cubic Al3Zr phases that can be effective in preventing the motion and pinning of linear grain boundary segments so that recrystallization in aluminum alloys can be inhibited.

[0058] In certain non-limiting embodiments, the interliner layer 106 of the brazing sheet 100 includes a 3XXX series aluminum alloy, which may include a composition suitable for inhibiting recrystallization of the interliner layer 106. For example, the 3XXX series aluminum alloy may include, in weight percent based on the total weight of the 3XXX series aluminum alloy, 0.01-0.2 silicon, 0-0.6 copper, 0.8-1.9 manganese, 0-0.2 chromium, 0-0.15 zirconium, 0-0.4 iron, 0-3.0 zinc, 0-0.2 magnesium, 0-0.3 titanium, 0-0.1 vanadium, 0-0.5 bismuth, aluminum, and impurities. In various non-limiting embodiments, the 3XXX series aluminum alloys include, in weight percent based on the total weight of the 3XXX series aluminum alloy, 0.02-0.2 silicon, 0.3-0.6 copper, 1.75-1.9 manganese, 0.1-0.2 chromium, 0-0.15 zirconium, 0.05-0.4 iron, 0-1.0 zinc, 0.01-0.1 magnesium, 0-0.3 titanium, 0-0.1 vanadium, 0-0.5 bismuth, aluminum, and impurities. In certain non-limiting embodiments, the 3XXX series aluminum alloys include, in weight percent based on the total weight of the aluminum alloy, at least 0.8 manganese, at least 1.0 manganese, at least 1.2 manganese, at least 1.4 manganese, at least 1.55 manganese, or at least 1.75 manganese.

[0059] As used herein, a brazing sheet layer that is "at least partially recrystallized" contains at least one recrystallized grain (e.g., the layer is greater than 0% recrystallized). The recrystallized grain is substantially undeformed and free of distortion.

[0060] As used herein, a "non-recrystallized" brazing sheet layer does not contain recrystallized grains, i.e., the layer is 1 cm 2The "non-crystallized" layer does not contain grains with a dislocation density of 10,000,000 or less per unit area. In certain non-limiting embodiments, the morphology of the grains in the "non-crystallized" layer can be as processed. For example, non-recrystallized grains can be elongated in the as-cold rolled state and have the same crystal orientation as the rolling direction (longitudinal direction, L). Also, for example, non-crystallized material can contain only deformed and distorted grains.

[0061] Layers of material (e.g., sheets) suitable for incorporation into a brazing sheet are typically cold worked during manufacture to reduce the thickness of the material, e.g., reduce the thickness of the material by at least 80%, prior to annealing. For example, as illustrated in FIG. 4, layer of material 450 is cold rolled by rollers 452. To accommodate the reduced thickness of layer of material 450, the grains of layer of material 450 become elongated, resulting in an increase in the aspect ratio of the grains relative to their longitudinal direction L (e.g., in the L-S-T plane). As a result of the cold working, the grains change crystal orientation (e.g., forming a crystallographic cold rolled texture) relative to the longitudinal direction L (e.g., in the L-S-T plane) and the grains become thinner and thinner, e.g., thinner and thinner, ... 2 Less than 10,000,000 pieces per cm 2 The alloy experiences an increase in dislocation density to over 10 billion per well.

[0062] Since the deformation is typically a metastable and high energy state of the material layer 450, the strain in the material layer 450 can be reduced during the final anneal. The reduction in strain can be in the form of recovery only, where the grain morphology (e.g., elongated grains) and cold rolled texture are preserved, but the strain inside the grains is reduced. The dislocations rearrange themselves and form sub-cell structures inside the grains. Although the overall dislocation density can be reduced, a defect-free volume of new grain orientations is not formed.

[0063] For long anneals or anneals with temperature gradients, material layer 450 may recrystallize after recovery. During recrystallization, substantially defect-free volumes of new crystal orientations may nucleate from the interior subcells of the recovered grains and / or from high angle grain boundary segments adjacent to high strain concentrations that become mobile or form dispersions. These nuclei then grow, consuming the defect-rich grains to produce substantially defect-free, low dislocation density (>10,000,000 / cm). 2 less than 100 nm), forming recrystallized grains with new crystal orientation (e.g., forming a crystallographic recrystallization texture).

[0064] For example, Figure 5A illustrates a cross-section in the L-ST plane of a layer of material containing only non-recrystallized grains after cold rolling, Figure 5B illustrates a cross-section in the L-ST plane of a layer of material that is at least partially recrystallized after cold rolling and annealing, and Figure 5C illustrates a cross-section in the L-ST plane of a fully recrystallized material after cold rolling and annealing.

[0065] The partial recrystallization of the interliner layer 106 can be difficult to control. The interface constitutes a discontinuity in the microstructure and is therefore also typically a region of high strain. It would be expected that the partial recrystallization would occur preferentially at the interface between the brazing layer 104 and the interliner layer 106. The forming strain may then be insufficient to ensure that the recrystallized grains of the interliner layer 106 recrystallize again during the heating of the brazing cycle, and thus heating may result in an interliner layer 106 with poor corrosion resistance. The interliner layer 106 is therefore not crystallized.

[0066] In various non-limiting embodiments, the at least partially recrystallized core layer 102 may be, for example, 1 cm 2 5,000,000 or less per 、 or 1 cm 2 1,000,000 or less per cm 2For example, the at least partially recrystallized core layer 102 may have a dislocation density of, for example, 100,000 / cm 2 ~10,000,000 / cm 2 , or 100,000 / cm 2 ~1,000,000 / cm 2 Such as, 10,000~10,000,000 / cm 2 The dislocation density may range from 0.01 to 0.1.

[0067] As used herein, "dislocation density" refers to the average average dislocation density of a material. Dislocation density can be measured using a transmission electron microscope applying the line intercept method as described in Martin et al., "The quantitative measurement of dislocation density in the transmission electron microscope", Parkt. Metallogr. 32 (1995), p. 467, or the line length measurement method as described in Kruml et al., "Dislocation density in Ni3(Al,Hf)", Intermetallics 8 (2000), p. 729, both of which are incorporated herein by reference in their entirety.

[0068] In various non-limiting embodiments, the unrecrystallized interliner layer 106 may be, for example, 1 cm 2 Over 1,000,000,000 pieces per cm 2 More than 10,000,000,000 pieces per cm 2 More than 100,000,000,000 pieces per cm 2 For example, the non-recrystallized interliner layer 106 may have an average dislocation density of greater than 100,000,000 per cm. 2 1,000,000,000~1cm per 2 1,000,000,000,000 per cm 2 10,000,000,000~1cm per 21,000,000,000,000 etc. per cm 2 100,000,000~1cm per 2 The dislocation density may range from 1,000,000,000,000 per

[0069] In certain non-limiting embodiments, electron backscatter diffraction (EBSD) utilizing a scanning electron microscope (SEM) can be used to determine whether a layer is recrystallized or at least partially recrystallized. In EBSD, as illustrated in the system diagram example of FIG. 13, the electron beam of the SEM scans the surface of the sample layer and obtains a Kikuchi pattern from each discrete sampling spot. Each orientation of crystals that is symmetrically unique within the sample layer can have a unique Kikuchi pattern, and each Kikuchi pattern can be indexed by comparing the resulting Kikuchi pattern to a database of Kikuchi patterns. Areas of the same orientation based on the Kikuchi pattern within the defined orientation spread are then identified as contiguous grains. An orientation map is then created by assigning a color to each grain based on its orientation.

[0070] The distortion of the sample layer can create lattice rotations that can be measured by EBSD. If there is a lattice rotation, the sample layer is recrystallized if the lattice rotation is minimal. In various non-limiting embodiments, EBSD can be used to create a kernel average orientation difference (KAM) map based on the orientation difference between data points to determine the distortion of the sample layer, as illustrated in the system diagram example of FIG. 14. For the KAM map, the orientation difference between data points is quantified based on the orientation spread (OS) and color-coded in the map based on the OS. For example, a layer with an OS of 2.5 degrees or less can be considered recrystallized, and a layer with an OS of more than 2.5 degrees can be considered uncrystallized. In various non-limiting embodiments, a layer with an OS of 2.0 degrees or less can be considered recrystallized, and a layer with an OS of more than 2.0 degrees can be considered uncrystallized. In certain non-limiting embodiments, the quantitative orientation difference can be obtained from line trace analysis.

[0071] As illustrated in Figures 9A, 10A, 11A, and 12A, the grain orientation map may include a legend illustrating the color of each grain orientation. As illustrated in Figures 9B, 10B, 11B, and 12B, the scale of the KAM map is 0OS (yellow), indicating minimal, if any, distortion in the sample layer, and 4.99999OS (black), indicating significant distortion in the sample layer. The data in Figures 9A and 9B, 10A and 10B, 11A and 11B, and 12A and 12B were obtained using a step size of 0.5 microns.

[0072] For example, a grain orientation map of the non-recrystallized first sample (cold rolled composite) is shown in Figure 9A, and a KAM map of the first sample is shown in Figure 9B. As illustrated in Figures 9A and 9B, the grains in the first sample are primarily elongated, and as illustrated in Figure 9B, the KAM map shows predominantly high OS (orange-red) regions, indicating that the first sample is not recrystallized.

[0073] The grain orientation map of the second sample that was not recrystallized (cold rolled and annealed) is shown in Figure 10A, and the KAM map of the second sample is shown in Figure 10B. As illustrated in Figures 10A and 10B, the grains in the second sample are primarily elongated, and as illustrated in Figure 10B, the KAM map shows areas of high OS (orange), but exhibits less OS than that of Figure 9B, indicating that the second sample is not recrystallized and is recovered.

[0074] A grain orientation map of the third sample, which has been at least partially recrystallized, is shown in Figure 11A, and a KAM map of the third sample is shown in Figure 11B. As illustrated in Figures 11A and 11B, the grains are a mixture of smaller elongated grains that are primarily recovered. In Figure 11B, the KAM map shows some OS (orange) and some crystals grown with essentially no distortion and minimal OS (yellow).

[0075] A grain orientation map of the fourth sample, which is significantly recrystallized, is shown in Figure 12A, and a KAM map of the fourth sample is shown in Figure 12B. As illustrated in Figures 12A and 12B, the grains are large and have regrown. In Figure 12B, the KAM map shows minimal OS (yellow), indicating that the fourth sample is significantly recrystallized.

[0076] A grain orientation map of a non-limiting embodiment of a first brazing sheet 1500 according to the present disclosure is shown in FIG. 15A, and a KAM map of the first brazing sheet 1500 is shown in FIG. 15B. As shown by FIG. 15A and FIG. 15B, the core layer 1502 of the first brazing sheet 1500 is at least partially recrystallized. The interliner layer 1506 is intermediate the core layer 1502 and the brazing layer 1506. The interliner layer 1506 is not recrystallized. The core layer 1502 comprises a first aluminum alloy, the brazing layer 1504 comprises a 4XXX series aluminum alloy, and the interliner layer 1506 comprises a second aluminum alloy.

[0077] A grain orientation map of a non-limiting embodiment of a second brazing sheet 1600 according to the present disclosure is shown in Figure 16A, and a KAM map of the second brazing sheet 1600 is shown in Figure 16B. As shown by Figures 16A and 16B, the core layer 1602 of the first brazing sheet 1600 is at least partially recrystallized. The interliner layer 1606 is intermediate the core layer 1602 and the brazing layer 1604. The interliner layer 1606 is at least partially recrystallized. The core layer 1602 comprises a first aluminum alloy, the brazing layer 1604 comprises a 4XXX series aluminum alloy, and the interliner layer 1606 comprises a second aluminum alloy.

[0078] 18A, a grain orientation map of a fabricated comparative brazing sheet 1800 comprising a first O-tempered interliner layer 1806a that is at least partially recrystallized, a second O-tempered interliner layer 1806b that is at least partially recrystallized, an O-tempered core layer 1802, a first brazing layer 1804a comprising a 4XXX series aluminum alloy, and a second brazing layer 1804b comprising a 4XXX series aluminum alloy. Referring to FIG. 18B, two of the brazing sheets 1800 were brought into contact and subjected to a brazing process resulting in a brazing joint 1850.

[0079] Referring to Figure 19A, a grain orientation map of a fabricated comparative brazing sheet 1900 according to the present disclosure, comprising a first non-recrystallized H-tempered interliner layer 1906a, a second non-recrystallized H-tempered interliner layer 1906b, an O-tempered core layer 1902, a first brazing layer 1904a comprising a 4XXX series aluminum alloy, and a second brazing layer 1904b comprising a 4XXX series aluminum alloy. Referring to Figure 19B, two of the brazing sheets 1900 were brought into contact and subjected to a brazing process, resulting in a brazing joint 1950. The interliner layer 1904a remains discernable in Figure 19B after the brazing process, where the interliner layer 1804a can no longer be discerned from the remainder of the comparative brazing sheet 1800 in Figure 18B. The interliner layer 1904a in Figure 19B was observed to contain a fine dispersion of liquid and brown branding. The bond width in Figure 19B is substantially narrower than that in Figure 19A, indicating less liquid film transfer in Figure 19B compared to Figure 19A.

[0080] In various non-limiting embodiments, the interliner layer of the brazing sheet (e.g., brazing sheet 100) according to the present disclosure is configured to inhibit liquid film migration. For example, the interliner layer (e.g., interliner layer 106) can be a heterogenized material having distortions that can inhibit liquid film migration (e.g., dissolution into the brazing layer upon liquefaction) during the brazing cycle. For example, the deformed and distorted grains of the interliner layer (e.g., interliner layer 106) can recrystallize during the heating of the brazing cycle before the brazing liner begins to melt, thereby protecting the core layer (e.g., core layer 102) from liquid film migration even if the core layer does not completely recrystallize. In various non-limiting embodiments, if the interliner layer is not homogenized and contains at least 0.01 weight percent manganese in solid solution, Al x Mn y S z Dispersions and brown bands can form in the interliner layer during the brazing cycle. Thus, a brazing sheet (e.g., brazing sheet 100) can include formability of O-tempered material for a homogenized O-tempered core layer (e.g., core layer 102), which is typically the thickest portion of the brazing sheet, and can include enhanced corrosion protection of non-homogenized, non-recrystallized material for an interliner layer (e.g., interliner layer 106), which can inhibit corrosion of the core layer.

[0081] In certain non-limiting embodiments of a brazing sheet (e.g., brazing sheet 100) according to the present disclosure, the grains of the core layer (e.g., core layer 102) include a first aspect ratio and the grains of the interliner layer (e.g., interliner layer 106) include a second aspect ratio in the final temper (e.g., after fabrication is completed after final heat treatment). In various non-limiting embodiments of the brazing sheet, the second aspect ratio can be greater than the first aspect ratio, e.g., at least 0.1 greater, at least 0.5 greater, at least 1 greater, or at least 2 greater than the first aspect ratio. As used herein, the "aspect ratio" of a material refers to the ratio of the average length to the grain height measured in the long-short cross-sectional (L-ST) plane. In various non-limiting embodiments, the grains of the core layer of a brazing sheet according to the present disclosure are approximately equilibrated or equilibrated in the final temper.

[0082] In various non-limiting embodiments of a brazing sheet (e.g., brazing sheet 100) according to the present disclosure, a core layer (e.g., core layer 102) can include an aluminum alloy having a first recrystallization temperature, and an interliner layer (e.g., interliner layer 106) of the brazing sheet can include an aluminum alloy having a second recrystallization temperature. In various embodiments of a brazing sheet according to the present disclosure, the second recrystallization temperature can be higher than the first recrystallization temperature, such as at least 5 degrees Celsius higher, at least 10 degrees Celsius higher, at least 25 degrees Celsius higher, at least 50 degrees Celsius higher, or at least 100 degrees Celsius higher than the first recrystallization temperature. An annealing heat treatment temperature can be applied to a brazing sheet according to the present disclosure such that the core layer can fully recrystallize, while the interliner layer may not recrystallize (e.g., remain unrecrystallized), but may recover during the annealing heat treatment.

[0083] The thickness of each layer in various embodiments of a brazing sheet according to the present disclosure (e.g., brazing sheet 100) can be configured based on the desired structural characteristics of the article of manufacture to be made from or incorporating all or a portion of the brazing sheet. For example, in various non-limiting embodiments, the core layer (e.g., core layer 102) is less than the total thickness of the brazing sheet (i.e., t total In various non-limiting embodiments, the interliner layer (e.g., interliner layer 106) may include a first thickness t1 that may be in the range of 60% to 90% of the total thickness (t total In various non-limiting embodiments, the brazing layer (e.g., brazing layer 104) may include a second thickness t2 that is in the range of 3% to 20% of the total thickness (t total ) in the range of 3% to 20% of the total thickness (t1). In various non-limiting embodiments, the first thickness t1 is greater than the second thickness t2 and greater than the third thickness t3. In certain non-limiting embodiments, the total thickness (t1) of a brazing sheet (e.g., brazing sheet 100) according to the present disclosure may include a third thickness t3 in the range of 3% to 20% of the total thickness (t2). total ) is in the range of 100 μm to 5 mm, for example in the range of 200 μm to 1 mm.

[0084] In various non-limiting embodiments, the brazing sheet according to the present disclosure may comprise, in addition to the core layer, an interliner layer and a brazing layer. For example, referring to the non-limiting embodiment shown in FIG. 2, the brazing sheet 200 comprises a core layer 202, a first interliner layer 206a, a first brazing layer 204a, a second brazing layer 204b, and a second interliner layer 206b. In various non-limiting embodiments, the core layer 202, the first interliner layer 206a, the second interliner layer 206b, the first brazing layer 204a, and the second brazing layer 204b are bonded together to form the brazing sheet 200. The brazing sheet 200 may be suitable for at least one of controlled atmosphere brazing and vacuum brazing. For example, the brazing sheet 200 may comprise layers having a composition such that the brazing sheet is suitable for controlled atmosphere brazing and / or vacuum brazing.

[0085] 2, the second brazing layer 204b is disposed on the second side 202b of the core layer 202, and the first brazing layer 204a is disposed on the first side 202a of the core layer 202. The second side 202b of the core layer 202 is disposed opposite the first side 202a of the core layer 202. In various non-limiting embodiments, the first brazing layer 204a and / or the second brazing layer 204b can be composed of a composition as described herein with respect to the brazing layer 104. In various non-limiting embodiments, the composition of the second brazing layer 204b can be the same or different from the composition of the first brazing layer 204a. For example, the second brazing layer 204b can include a 1XXX series aluminum alloy, a 3XXX series aluminum alloy, a 3XXX series aluminum alloy (e.g., a 3XXX series aluminum alloy with an intentional addition of zinc (e.g., 0.1-4 weight percent based on the total weight of the aluminum alloy), a 3XXX series aluminum alloy without an intentional addition of zinc), a 4XXX series aluminum alloy, or a 7XXX series aluminum alloy. Similarly, the first interliner layer 206a and / or the second interliner layer 206b can be composed of a composition as described herein with respect to the interliner layer 106. In various non-limiting embodiments, the composition of the second interliner layer 206b can be the same or different from the composition of the first interliner layer 206a.

[0086] The second interliner layer 206b can be disposed intermediate the core layer 202 and the second brazing layer 204b. The second interliner layer 206b can be non-recrystallized, and in various non-limiting embodiments, the second interliner layer 206b can be non-homogenized.

[0087] The thickness of each layer within the brazing sheet 200 can be configured based on the desired structural characteristics of the article to be made from or incorporating all or a portion of the brazing sheet 200. For example, in various non-limiting embodiments, the core layer 202 is less than the total thickness (t total In various non-limiting embodiments, the first interliner layer 206a and the second interliner layer 206b may include a first thickness t1 that may be in the range of 60% to 90% of the total thickness (t total In various non-limiting embodiments, the first brazing layer 204a and the second brazing layer 204b may have a combined thickness t2+t4 that is within a range of 3% to 20% of the total thickness (t total In certain non-limiting embodiments, the brazing sheet 200 may include a combined thickness t3+t5 that is in the range of 3% to 20% of the total thickness (t total ) is in the range of 100 μm to 5 mm, for example in the range of 200 μm to 1 mm.

[0088] In various non-limiting embodiments, the brazing sheet may not include a second interliner layer, and the second brazing layer may be in direct contact with the core layer. Referring to the non-limiting embodiment shown generally in FIG. 3, the brazing sheet 300 includes a core layer 302, an interliner layer 306, a first brazing layer 304a, and a second brazing layer 304b. In various non-limiting embodiments, the core layer 302, the interliner layer 306, the first brazing layer 304a, and the second brazing layer 304b are bonded together to form the brazing sheet 300. The brazing sheet 300 may be suitable for at least one of controlled atmosphere brazing and vacuum brazing. For example, the brazing sheet 300 may include layers having a composition such that the brazing sheet is suitable for controlled atmosphere brazing and / or vacuum brazing.

[0089] As shown in FIG. 3, the second brazing layer 304b is disposed on the second side 302b of the core layer 302, and the first brazing layer 304a is disposed on the first side 302a of the core layer 302. The second side 302b of the core layer 302 is disposed opposite the first side 302a of the core layer 302. In various non-limiting embodiments, the first brazing layer 304a and / or the second brazing layer 304b can be of a composition as described herein for the brazing layer 104. In various non-limiting embodiments, the composition of the second brazing layer 304b can be the same or different from the composition of the first brazing layer 304a. Similarly, the interliner layer 306 can be of a composition as described herein for the interliner layer 106.

[0090] 17 is a block diagram of a non-limiting embodiment of a method according to the present disclosure for forming a non-limiting embodiment of a brazing sheet according to the present disclosure. The method can include homogenizing a core layer to form a homogenized core layer (step 1702). A workpiece including a 3XXX series aluminum alloy can be hot worked (e.g., hot rolled into intermediate gauge sheet material) to form an interliner layer (step 1704). The method can further include hot rolling together a stack or assembly including the homogenized core layer from step 1702, one or more interliner layers from step 1704, and one or more brazing layers to form a brazing sheet (step 1706). For example, a stack including the homogenized core layer from step 1702, at least one interliner layer from step 1704, and at least one brazing layer can be assembled in the appropriate order, heated, and then hot rolled to bond the layers together to form a brazing sheet. During the process, a conventional interliner layer is more likely than a conventional core layer to be at least partially recrystallized during fabrication of the brazing sheet. Embodiments of an interliner layer according to the present disclosure treated in this manner may remain non-recrystallized during creation of the brazing sheet.

[0091] In various non-limiting embodiments, an article of manufacture, such as a heat exchanger, can include a structural element that includes all or a portion of an embodiment of a brazing sheet according to the present disclosure (e.g., any of brazing sheets 100, 200, 300). In various embodiments, a heat exchanger, such as an oil cooler or a liquid cooled condenser, includes all or a portion of an embodiment of a brazing sheet according to the present disclosure (e.g., any of brazing sheets 100, 200, 300).

[0092] FIG. 6 is a block diagram of a non-limiting embodiment of a method according to the present disclosure for forming an article of manufacture, such as a heat exchanger. The method embodiment includes contacting a first portion including a first material with a second portion including all or a portion of an embodiment of a brazing sheet according to the present disclosure. For example, a non-limiting embodiment of a method according to the present disclosure may include contacting a first portion including a first material with a second portion including all or a portion of brazing sheet 100, brazing sheet 200, brazing sheet 300, and / or a different embodiment of a brazing sheet according to the present disclosure (FIG. 6, step 602). In various non-limiting embodiments, the first portion can be brazed to the second portion by a process including at least one of controlled atmosphere brazing and vacuum brazing (FIG. 6, step 604). In various embodiments, step 604 includes controlled atmosphere brazing, and a flux may or may not be used. For example, if the core layer and one or more interliner layers of a brazing sheet according to the present disclosure include magnesium, a flux may not be required when performing controlled atmosphere brazing. However, if the core layer and one or more interliner layers of a brazing sheet according to the present disclosure do not include magnesium, a flux may be required when performing controlled atmosphere brazing. As illustrated in Figure 6, in various non-limiting embodiments of the method, the first material includes aluminum or an aluminum alloy. EXAMPLES

[0093] A comparative brazing sheet and a non-limiting embodiment of a brazing sheet according to the present disclosure were prepared. Both brazing sheets included five layers bonded together, including a first brazing layer, a first interliner layer, a core layer, a second interliner layer, and a second brazing layer. The first interliner layer was intermediate the core layer and the first brazing layer, and the second interliner layer was intermediate the core layer and the second brazing layer. Both brazing sheets included the same brazing layer including a 4XXX series alloy and the same core layer including an at least partially recrystallized 3003 series aluminum alloy. The interliner layer in both the comparative brazing sheet and the brazing sheet according to the present disclosure contained, in weight percent, silicon up to 0.25, iron up to 0.6, copper from 0.2 to 0.4, manganese from 0.8 to 1.3, magnesium up to 0.1, zinc up to 0.05, titanium up to 0.35, zirconium up to 0.12, aluminum, and impurities. The interliner layer of the comparative brazing sheet was heat treated to be at least partially recrystallized and have an O temper. The interliner layer of the brazing sheet according to the present disclosure was heat treated to be neither recrystallized nor homogenized.

[0094] FIG. 7A is a micrograph of a cross section of the microstructure of the comparative brazing sheet of this example in a pre-brazing state. FIG. 7B is a micrograph of a cross section of the microstructure of the comparative brazing sheet of this example in a post-brazing state. FIG. 8A is a micrograph of a cross section of the microstructure of the brazing sheet embodiment according to the present disclosure of this example in a pre-brazing state. FIG. 8B is a micrograph of a cross section of the microstructure of the brazing sheet embodiment according to the present disclosure of this example in a post-brazing state. With reference to FIG. 7B and FIG. 8B, the retained combined thickness of the core layer and interliner layer of the brazing sheet embodiment of the present disclosure after brazing is 30-50 μm thicker than the combined thickness of the core layer and interliner layer of the comparative brazing sheet of this example after brazing. As illustrated in FIG. 7B and FIG. 8B, a greater amount of liquid film transfer occurs at the interface 750 between the brazing layer and the liner layer in the comparative brazing sheet compared to the interface 850 in the brazing sheet embodiment according to the present disclosure. In addition, the interliner layer of the comparative brazing sheet of this example was observed to have a higher eutectic phase content, indicating liquid film migration, and the retained thickness of the core layer in the comparative brazing sheet of this example after brazing was 20% lower than the retained thickness of the core layer in the brazing sheet according to the present disclosure of this example after brazing.

[0095] Additionally, the comparative brazing sheets and the brazing sheets according to the present disclosure evaluated in this example were tested for ultimate tensile strength, tensile yield strength, and tensile elongation in the pre-brazing state. Table 1 provides the results. [Table 1]

[0096] As shown in Table 1, the measured mechanical properties of the brazing sheet according to the present disclosure and the comparative brazing sheet evaluated in this example were only slightly different. This indicates that the brazing sheet according to the present disclosure in this example exhibits formability comparable to that of a fully O-tempered brazing sheet. Figures 8A and 8B illustrate the reduction in liquid film migration that occurs with the brazing sheet according to the present disclosure in this example compared to the comparative brazing sheet. This indicates that the brazing sheet according to the present disclosure evaluated in this example has enhanced corrosion resistance compared to the comparative brazing sheet.

[0097] The following numbered sections are directed to various non-limiting embodiments and aspects according to the disclosure. Item 1. A brazing sheet, a core layer comprising a first aluminum alloy, the core layer being at least partially recrystallized; a brazing layer comprising a 4XXX series aluminum alloy; an interliner layer intermediate the core layer and the brazing layer and including a second aluminum alloy, the interliner layer being not recrystallized. Item 2. The brazing sheet of item 1, wherein the first aluminum alloy has a first recrystallization temperature, the second aluminum alloy has a second recrystallization temperature, and the second recrystallization temperature is greater than the first recrystallization temperature. Item 3. The brazing sheet according to item 1 or 2, wherein the core layer is homogenized. Item 4. The interliner layer is 1 cm 2 The brazing sheet according to any one of items 1 to 3, having a dislocation density of at least 100,000,000 per square inch. Item 5. The interliner layer is 1 cm 2 5. The brazing sheet according to any one of items 1 to 4, which does not contain recrystallized grains having a dislocation density of 10,000,000 or less per unit area. 。 Item 6. The core layer is 1 cm 26. The brazing sheet according to any one of items 1 to 5, having a dislocation density of 10,000,000 or less per square inch. Item 7. The brazing sheet of any of paragraphs 1-6, wherein the grains of the core layer have a first aspect ratio and the grains of the interliner layer have a second aspect ratio, the second aspect ratio being greater than the first aspect ratio, each aspect ratio referring to the ratio between the average grain length and grain height for the long and short cross sections. Item 8. The brazing sheet according to any one of Items 1 to 7, wherein the interliner layer is not homogenized. Item 9. The brazing sheet of any one of items 1 to 8, wherein the interliner layer is configured to inhibit liquid film migration. Item 10. The brazing sheet of any one of items 1 to 9, wherein the second aluminum alloy contains at least 0.01 weight percent zirconium based on the total weight of the second aluminum alloy. Item 11. The brazing sheet of any one of items 1 to 10, wherein the core layer, the interliner layer, and the brazing layer are bonded together. Item 12. The brazing sheet according to any one of items 1 to 11, wherein the first aluminum alloy is a 3XXX series aluminum alloy or a 6XXX series aluminum alloy. Item 13. The first aluminum alloy is, in weight percent based on the total weight of the first aluminum alloy, Silicone from 0 to 1.2, 0 to 1.0 copper and 0 to 0.25 zirconium, 0 to 0.8 iron, Manganese from 0 to 2.0, 0 to 3.0 zinc, 0 to 1.5 magnesium, 0~0.25 titanium and 0 to 0.3 chromium, 0 to 0.5 bismuth, Aluminum and 13. The brazing sheet according to any one of items 1 to 12, further comprising impurities.

[0098] Section 14. the brazing layer being a first brazing layer disposed on a first side of the core layer; 14. The brazing sheet of any one of items 1 to 13, wherein a second brazing layer is disposed on a second side of the core layer opposite the first side of the core layer, and the second brazing layer comprises a 1XXX series aluminum alloy, a 3XXX series aluminum alloy, a 3XXX series aluminum alloy, a 4XXX series aluminum alloy, or a 7XXX series aluminum alloy. Section 15. the brazing layer being a first brazing layer disposed on a first side of the core layer; the interliner layer is a first interliner layer; a second brazing layer is disposed on a second side of the core layer opposite the first side of the core layer, the second brazing layer comprising a 1XXX series aluminum alloy, a 3XXX series aluminum alloy, a 3XXX series aluminum alloy, a 4XXX series aluminum alloy, or a 7XXX series aluminum alloy; 15. The brazing sheet according to any one of items 1 to 14, wherein the second interliner layer is disposed between the core layer and the second brazing layer. Item 16. The brazing sheet according to any one of Items 1 to 15, wherein the brazing sheet is suitable for at least one of controlled atmosphere brazing and vacuum brazing. Item 17. The weight percent of the 4XXX series aluminum alloy in each brazing layer is based on the total weight of the 4XXX series aluminum alloy. 5 to 15 silicon, 0 to 2.0 magnesium, 0 to 1.0 iron, 0 to 3.0 zinc, 0 to 2.0 copper, Manganese from 0 to 1.0, 0~0.2 titanium and 0 to 0.3 Bismuth, Aluminum and 17. The brazing sheet according to any one of items 1 to 16, further comprising impurities. Section 18. the core layer comprises a first thickness in a range of 60% to 90% of a total thickness of the brazing sheet; the interliner layer includes a second thickness in the range of 3% to 20% of the total thickness of the brazing sheet; 18. The brazing sheet of any one of items 1 to 17, wherein the brazing layer includes a third thickness in the range of 3% to 20% of the total thickness of the brazing sheet. Item 19. A heat exchanger comprising a structural element comprising all or a portion of the brazing sheet according to any one of items 1 to 18.

[0099] Item 20. A method for forming an article, comprising: Contacting a first portion including a first material with a second portion including all or a portion of the brazing sheet according to any one of items 1 to 18; and brazing the first portion to the second portion by a process comprising at least one of controlled atmosphere brazing and vacuum brazing. Item 21. The method of item 20, wherein the first material comprises aluminum or an aluminum alloy. Item 22. The method of any one of items 20 or 21, wherein the article is a heat exchanger.

[0100] Item 23. A brazing sheet, a core layer comprising a first aluminum alloy having a first recrystallization temperature; and a brazing layer comprising a 4XXX series aluminum alloy. an interliner layer intermediate the core layer and the brazing layer, the interliner layer comprising a 3XXX series aluminum alloy having a second recrystallization temperature, the interliner layer having a second recrystallization temperature, the second recrystallization temperature being in weight percent based on the total weight of the 3XXX series aluminum alloy: Silicone 0.01 to 0.2 0~0.6 copper, Manganese, 0.8-1.9 0 to 0.2 chromium, Zirconium, 0 to 0.15 0-0.4 iron, 0-3 zinc, Magnesium, 0-0.2 0~0.3 titanium, Vanadium, 0 to 0.1 0 to 0.5 Bismuth, Aluminum, and an interliner layer containing impurities; The brazing sheet, wherein the second recrystallization temperature is greater than the first recrystallization temperature. The brazing sheet of paragraph 23, wherein the sum of the weight percents of manganese, chromium, titanium, zirconium, and vanadium in the 3XXX series aluminum alloy is at least 2.0. The brazing sheet of any of paragraphs 23 or 24, wherein the sum of the weight percents of manganese, chromium, titanium, zirconium, and vanadium in the 3XXX series aluminum alloy is at least 2.1. Item 26. The 3XXX series aluminum alloy of the interliner layer is, in weight percent based on the total weight of the 3XXX series aluminum alloy, 0.02 to 0.1 silicon, 0.3 to 0.6 copper, Manganese, 1.75-1.9; 0.1 to 0.2 chromium, 0 to 0.15 zirconium, 0.05 to 0.4 iron, 0-1 zinc and 0.01 to 0.1 magnesium, 0~0.3 titanium and 0 to 0.1 vanadium, 0 to 0.5 bismuth, Aluminum and 26. The brazing sheet according to any one of items 23 to 25, further comprising impurities.

[0101] Item 27. The brazing sheet of any one of items 23 to 26, wherein the core layer is at least partially recrystallized and the interliner layer is not recrystallized. Item 28. The brazing sheet of any one of items 23 to 27, wherein a first sum of weight percentages of manganese, chromium, and vanadium in the interliner layer is greater than a second sum of weight percentages of manganese, chromium, and vanadium in the core layer. Item 29. The brazing sheet of any one of items 23 to 28, wherein the core layer, the interliner layer, and the brazing layer are bonded together into the brazing sheet. Item 30. The first aluminum alloy is, in weight percent based on the total weight of the first aluminum alloy, Silicone from 0 to 1.2, 0 to 1.0 copper and 0 to 0.25 zirconium, 0 to 0.8 iron, 0-2 manganese, 0-3 zinc, 0 to 1.5 magnesium, 0~0.25 titanium and 0 to 0.3 chromium, 0 to 0.5 bismuth, Aluminum and 30. The brazing sheet according to any one of items 23 to 29, further comprising impurities.

[0102] Section 31. the interliner layer being a first interliner layer disposed on the first side of the core layer; 31. The brazing sheet of any one of items 23 to 30, wherein a second brazing layer is disposed on a second side of the core layer opposite the first side of the core layer, and the second brazing layer comprises a 1XXX series aluminum alloy, a 3XXX series aluminum alloy, a 3XXX series aluminum alloy, a 4XXX series aluminum alloy, or a 7XXX series aluminum alloy. Section 32. the brazing layer being a first brazing layer disposed on a first side of the core layer; the interliner layer is a first interliner layer; a second brazing layer is disposed on a second side of the core layer opposite the first side of the core layer, the second brazing layer comprising a 1XXX series aluminum alloy, a 3XXX series aluminum alloy, a 3XXX series aluminum alloy, a 4XXX series aluminum alloy, or a 7XXX series aluminum alloy; 31. The brazing sheet according to any one of items 23 to 30, wherein the second interliner layer is disposed between the core layer and the second brazing layer. Item 33. The brazing sheet according to any one of Items 23 to 32, wherein the brazing sheet is suitable for at least one of controlled atmosphere brazing and vacuum brazing. Item 34. The weight percent of the 4XXX series aluminum alloy in each brazing layer based on the total weight of the 4XXX series aluminum alloy is: 5 to 15 silicon, 0 to 2.0 magnesium, 0 to 1.0 iron, Zinc from 0 to 3.0, 0 to 2.0 copper, Manganese from 0 to 1.0, 0~0.2 titanium and 0 to 0.3 Bismuth, Aluminum and Item 34. The brazing sheet according to any one of items 23 to 33, comprising impurities. Section 35. the core layer comprises a first thickness in a range of 60% to 90% of a total thickness of the brazing sheet; each interliner layer includes a second thickness in the range of 3% to 20% of the total thickness of the brazing sheet; 35. The brazing sheet of any one of paragraphs 23 to 34, wherein each brazing layer includes a third thickness in the range of 3% to 20% of the total thickness of the brazing sheet. Item 36. The brazing sheet according to any one of items 23 to 35, wherein the core layer is homogenized.

[0103] Item 37. A method for forming the brazing sheet of any one of items 1 to 36, wherein the brazing sheet includes a core layer, at least one brazing layer, and at least one interliner layer, the method comprising: homogenizing the core layer to form a homogenized core layer; hot working a workpiece comprising said 3XXX series aluminum alloy to form said at least one interliner layer; and hot rolling the at least one brazing layer, the at least one interliner layer, and the homogenized core layer together to form a brazing sheet. Item 38. A brazing sheet formed by the method of item 37. Item 39. A heat exchanger comprising a structural element comprising all or a portion of the brazing sheet of any one of items 23 to 36 and 38.

[0104] Item 40. A method for forming an article of manufacture, comprising: Contacting a first portion including a first material with a second portion including all or a portion of the brazing sheet of any one of items 23 to 36 and 38; and brazing the first portion to the second portion by a process comprising at least one of controlled atmosphere brazing and vacuum brazing. Item 41. The method of item 40, wherein the first material comprises aluminum or an aluminum alloy. Item 42. The method of any of items 40 or 41, wherein the article is a heat exchanger.

[0105] As used herein, unless otherwise indicated, all numerical parameters should be understood in all instances to be modified by the term "about," given the inherent variability of the underlying measurement method used to determine the numerical value of the parameter. At the very least, and not as an attempt to limit the application of the doctrine of equivalents to the scope of the claims, each numerical parameter set forth herein should at the very least be construed in light of the number of reported significant digits and by applying ordinary rounding techniques.

[0106] Also, any numerical range recited herein includes all subranges subsumed within the recited range. For example, the range "1 to 10" includes all subranges between (and including) the recited minimum value of 1 and the recited maximum value of 10, i.e., having a minimum value of 1 or more and a maximum value of 10 or less. Also, all ranges recited herein include the endpoints of the recited range. For example, the range "1 to 10" includes the endpoints 1 and 10. Any maximum numerical limitation recited herein is intended to include all lower numerical limitations subsumed therein, and any minimum numerical limitation recited herein is intended to include all higher numerical limitations subsumed therein. Accordingly, applicants reserve the right to amend this specification, including the claims, to explicitly recite subranges that are explicitly subsumed within the recited ranges. All such ranges are inherently described herein.

[0107] As used herein, the grammatical articles "a," "an," and "the" are intended to include "at least one" or "one or more," unless otherwise noted, even though "at least one" or "one or more" may be expressly used in some cases. Thus, the foregoing grammatical articles are used herein to refer to one or more (i.e., "at least one") of the particular identified elements. Furthermore, the use of a singular noun includes the plural and the use of a plural noun includes the singular, unless the context of use requires otherwise.

[0108] Those skilled in the art will recognize that the articles and methods described herein and the accompanying discussion are used as examples for conceptual clarity, and various configuration modifications are contemplated. As a result, as used herein, the specific examples / embodiments described and the accompanying discussion are intended to represent their more general class. In general, the use of any specific example is intended to represent its class, and does not include specific components, devices, operations / acts, and objects, and should not be taken as limiting. While the present disclosure provides descriptions of various specific aspects for the purpose of illustrating various aspects of the disclosure and / or its potential applications, those skilled in the art will recognize that variations and modifications occur. Thus, the invention(s) described herein should be understood to be at least as broad as they are claimed, and not more narrowly defined by the specific illustrative aspects provided herein.

Claims

1. A brazing sheet, a core layer comprising a first aluminum alloy, the core layer being at least partially recrystallized; a brazing layer comprising a 4xxx series aluminum alloy; an interliner layer intermediate the core layer and the brazing layer and comprising a second aluminum alloy; the interliner layer having a weight percent based on the total weight of the second aluminum alloy of: Silicon of 0.02 to 0.2; 0.3 to 0.6 copper; Manganese of 1.75 to 1.9; 0.1 to 0.2% chromium; 0 to 0.15 zirconium; 0.05 to 0.4 iron, Zinc between 0 and 1.0; 0.01 to 0.1% magnesium; Titanium 0 to 0.3, 0 to 0.1 vanadium; Bismuth between 0 and 0.5; Aluminum and impurities, A brazing sheet, wherein the interliner layer is not recrystallized.

2. 2. The brazing sheet of claim 1, wherein the first aluminum alloy has a first recrystallization temperature and the second aluminum alloy has a second recrystallization temperature, the second recrystallization temperature being greater than the first recrystallization temperature.

3. The brazing sheet of claim 1 , wherein the core layer is homogenized.

4. The interliner layer is 1 cm ２ 2. The brazing sheet of claim 1 having a dislocation density of at least 100,000,000 per square inch.

5. The interliner layer is 1 cm ２ 2. The brazing sheet of claim 1, which is free of recrystallized grains having a dislocation density of 10,000,000 or less per square inch. 。

6. The core layer is 1 cm ２ 2. The brazing sheet of claim 1 having a dislocation density of 10,000,000 or less per square inch.

7. 2. The brazing sheet of claim 1, wherein the grains of the core layer have a first aspect ratio and the grains of the interliner layer have a second aspect ratio, the second aspect ratio being greater than the first aspect ratio, each aspect ratio referring to the ratio between the average grain length and grain height for the long and short cross sections.

8. The brazing sheet of claim 1 , wherein the interliner layer is not homogenized.

9. The brazing sheet of claim 1 , wherein the interliner layer is configured to inhibit liquid film migration.

10. 2. The brazing sheet of claim 1, wherein the second aluminum alloy comprises at least 0.01 weight percent zirconium, based on a total weight of the second aluminum alloy.

11. The brazing sheet of claim 1 , wherein the core layer, the interliner layer, and the brazing layer are adhered together.

12. 2. The brazing sheet according to claim 1, wherein the first aluminum alloy is a 3xxx series aluminum alloy or a 6xxx series aluminum alloy.

13. the first aluminum alloy comprising, in weight percent based on a total weight of the first aluminum alloy: Silicon of 0 to 1.2, 0 to 1.0 copper, 0 to 0.25 zirconium; 0 to 0.8 iron, Manganese between 0 and 2.0; Zinc between 0 and 3.0; 0 to 1.5 magnesium, 0 to 0.25 titanium, 0 to 0.3 chromium; Bismuth between 0 and 0.5; Aluminum and The brazing sheet according to claim 1 , further comprising:

14. the brazing layer being a first brazing layer disposed on a first side of the core layer; 2. The brazing sheet of claim 1, wherein a second brazing layer is disposed on a second side of the core layer opposite the first side of the core layer, the second brazing layer comprising a 1XXX series aluminum alloy, a 3XXX series aluminum alloy, a 3XXX series aluminum alloy, a 4XXX series aluminum alloy, or a 7XXX series aluminum alloy.

15. the brazing layer being a first brazing layer disposed on a first side of the core layer; the interliner layer is a first interliner layer, a second brazing layer is disposed on a second side of the core layer opposite the first side of the core layer, the second brazing layer comprising a 1xxx series aluminum alloy, a 3xxx series aluminum alloy, a 4xxx series aluminum alloy, or a 7xxx series aluminum alloy; The brazing sheet of claim 1 , wherein a second interliner layer is disposed intermediate the core layer and the second brazing layer.

16. 10. The brazing sheet of claim 1, wherein the brazing sheet is suitable for at least one of controlled atmosphere brazing and vacuum brazing.

17. The 4xxx series aluminum alloy of each brazing layer is, in weight percent based on the total weight of the 4xxx series aluminum alloy: 5 to 15 silicon, 0 to 2.0 magnesium, 0 to 1.0 iron, Zinc between 0 and 3.0; 0 to 2.0 copper, Manganese between 0 and 1.0; 0 to 0.2 titanium, Bismuth between 0 and 0.3; Aluminum and The brazing sheet according to claim 1 , further comprising:

18. the core layer comprises a first thickness in the range of 60% to 90% of a total thickness of the brazing sheet; the interliner layer comprises a second thickness in the range of 3% to 20% of the total thickness of the brazing sheet; The brazing sheet of claim 1 , wherein the brazing layer comprises a third thickness in the range of 3% to 20% of the total thickness of the brazing sheet.

19. A heat exchanger comprising a structural element comprising all or part of the brazing sheet according to any one of claims 1 to 5.

20. 1. A method for forming an article, the method comprising: contacting a first portion including a first material with a second portion including all or a portion of the brazing sheet of claim 1; and brazing the first portion to the second portion by a process comprising at least one of controlled atmosphere brazing and vacuum brazing.

21. The method of claim 20 , wherein the first material comprises aluminum or an aluminum alloy.

22. The method of claim 20, wherein the article is a heat exchanger.

Images