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CN115519198A - Titanium-aluminum/nickel-based high-temperature alloy heterogeneous porous sandwich structure product and preparation method thereof - Google Patents

Titanium-aluminum/nickel-based high-temperature alloy heterogeneous porous sandwich structure product and preparation method thereof Download PDF

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Publication number
CN115519198A
CN115519198A CN202210092389.1A CN202210092389A CN115519198A CN 115519198 A CN115519198 A CN 115519198A CN 202210092389 A CN202210092389 A CN 202210092389A CN 115519198 A CN115519198 A CN 115519198A
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nickel
panel
porous
titanium
noble metal
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宋晓国
罗云
胡胜鹏
刘亚洲
付伟
杨敏旋
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Harbin Institute of Technology Weihai
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Harbin Institute of Technology Weihai
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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23KSOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K1/00Soldering, e.g. brazing, or unsoldering
    • B23K1/008Soldering within a furnace
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23KSOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K1/00Soldering, e.g. brazing, or unsoldering
    • B23K1/0008Soldering, e.g. brazing, or unsoldering specially adapted for particular articles or work
    • B23K1/0014Brazing of honeycomb sandwich structures
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23KSOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K20/00Non-electric welding by applying impact or other pressure, with or without the application of heat, e.g. cladding or plating
    • B23K20/02Non-electric welding by applying impact or other pressure, with or without the application of heat, e.g. cladding or plating by means of a press ; Diffusion bonding
    • B23K20/023Thermo-compression bonding
    • B23K20/026Thermo-compression bonding with diffusion of soldering material
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23KSOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K20/00Non-electric welding by applying impact or other pressure, with or without the application of heat, e.g. cladding or plating
    • B23K20/26Auxiliary equipment
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C45/00Amorphous alloys
    • C22C45/04Amorphous alloys with nickel or cobalt as the major constituent
    • CCHEMISTRY; METALLURGY
    • C23COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23CCOATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C14/00Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material
    • C23C14/06Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material characterised by the coating material
    • C23C14/14Metallic material, boron or silicon
    • C23C14/16Metallic material, boron or silicon on metallic substrates or on substrates of boron or silicon
    • CCHEMISTRY; METALLURGY
    • C23COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23CCOATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C14/00Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material
    • C23C14/22Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material characterised by the process of coating
    • C23C14/34Sputtering
    • C23C14/35Sputtering by application of a magnetic field, e.g. magnetron sputtering

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  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Materials Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Laminated Bodies (AREA)

Abstract

The invention relates to the technical field of porous structure strengthening, in particular to a titanium aluminum/nickel-based superalloy heterogeneous porous sandwich structure product and a preparation method thereof, wherein the method comprises the following steps: obtaining a porous structure, a panel, a noble metal and a nickel-based amorphous thin strip, and putting the panel and the porous structure into an acetone solution for cleaning; the porous structure is made of nickel-based high-temperature alloy, and the panel is made of titanium-aluminum alloy; plating noble metal on the surface to be connected of the panel by adopting magnetron sputtering to form a noble metal layer; sequentially laminating and assembling a panel, a noble metal layer, a nickel-based amorphous thin strip, a porous structure layer, a nickel-based amorphous thin strip, a noble metal layer and the panel into a sandwich structure to obtain an assembly part; and placing the assembly part in a vacuum diffusion furnace, heating and preserving heat to obtain a product, wherein the added noble metal does not react with other elements in the joint to form a brittle phase, but is completely dissolved in the nickel matrix in the brazing seam in a solid solution manner and is in dispersed distribution to form a solid solution strengthening effect, and the strength of the joint is effectively improved.

Description

钛铝/镍基高温合金异质多孔夹层结构制品及制备方法Titanium-aluminum/nickel-based superalloy heterogeneous porous sandwich structure product and preparation method

技术领域technical field

本发明涉及多孔夹层结构强化技术领域,具体涉及一种钛铝/镍基高温合金异质多孔夹层结构制品及制备方法。The invention relates to the technical field of porous interlayer structure strengthening, in particular to a titanium-aluminum/nickel-based superalloy heterogeneous porous interlayer structure product and a preparation method.

背景技术Background technique

热防护系统是运载器的关键技术,热防护系统要求隔热效果好,金属热防护结构以其特有的优势成为了可重复使用运载器的热防护系统首选,其典型代表为美国X-33上所设计的金属热防护系统。The thermal protection system is the key technology of the carrier. The thermal protection system requires good heat insulation effect. The metal thermal protection structure has become the first choice for the thermal protection system of the reusable carrier due to its unique advantages. Its typical representative is the US X-33 The designed metal thermal protection system.

传统的金属热防护结构是由两块高温合金面板及其中间的高温合金芯体组成,高温合金芯体大多采用多孔结构,目前高温合金多孔夹层结构的制备主要采用真空钎焊技术。由于同质多孔夹层结构无法更好的实现减重与性能双优的结果,异质多孔夹层结构有望部分取代同质多孔夹层结构应用于超高速飞行器的热防护系统。The traditional metal thermal protection structure is composed of two superalloy panels and a superalloy core in the middle. Most of the superalloy cores adopt a porous structure. At present, the preparation of the superalloy porous sandwich structure mainly adopts vacuum brazing technology. Since the homogeneous porous sandwich structure cannot better achieve the results of weight reduction and performance, the heterogeneous porous sandwich structure is expected to partially replace the homogeneous porous sandwich structure in the thermal protection system of ultra-high-speed aircraft.

发明人在实践中,发现上述现有技术存在以下缺陷:In practice, the inventor finds that the above-mentioned prior art has the following defects:

在异质多孔夹层结构的钎焊连接过程中,接头中形成大量金属间化合物,并且钎料在两种母材上的润湿性不同,易形成溶蚀等缺陷,接头成为结构的薄弱区,成为异质多孔夹层结构在高温环境下服役的隐患。During the brazing connection process of the heterogeneous porous sandwich structure, a large number of intermetallic compounds are formed in the joint, and the wettability of the solder on the two base materials is different, which is easy to form defects such as dissolution, and the joint becomes the weak area of the structure, becoming Hidden dangers of heterogeneous porous sandwich structure serving in high temperature environment.

发明内容Contents of the invention

为了解决上述技术问题,本发明的目的在于提供钛铝/镍基高温合金异质多孔夹层结构制品及制备方法,所采用的技术方案具体如下:In order to solve the above-mentioned technical problems, the object of the present invention is to provide a titanium-aluminum/nickel-based superalloy heterogeneous porous sandwich structure product and a preparation method, and the adopted technical scheme is specifically as follows:

第一方面,本发明一个实施例提供了一种钛铝/镍基高温合金异质多孔夹层结构制备方法,该制备方法包括以下步骤:In the first aspect, an embodiment of the present invention provides a method for preparing a titanium-aluminum/nickel-based superalloy heterogeneous porous sandwich structure, the preparation method comprising the following steps:

获取多孔结构、面板、贵金属和镍基非晶薄带,将所述面板和多孔结构放入丙酮溶液中清洗;其中所述多孔结构的材质为镍基高温合金,所述面板的材质为钛铝合金;Obtain the porous structure, panel, noble metal and nickel-based amorphous strip, put the panel and porous structure into an acetone solution for cleaning; wherein the material of the porous structure is a nickel-based superalloy, and the material of the panel is titanium aluminum alloy;

采用磁控溅射将所述贵金属镀在面板的待连接面,形成贵金属层;Plating the noble metal on the surface to be connected of the panel by magnetron sputtering to form a noble metal layer;

依次按照面板、贵金属层、镍基非晶薄带、多孔结构层、镍基非晶薄带、贵金属层和面板的顺序层叠装配为夹层结构,得到装配件;The sandwich structure is obtained by stacking and assembling the panel, the noble metal layer, the nickel-based amorphous strip, the porous structure layer, the nickel-based amorphous strip, the noble metal layer and the panel in sequence;

将所述装配件放置于真空扩散炉中,加热温度至1020~1080℃,保温1~30min后,得到钛铝/镍基高温合金异质多孔夹层结构制品。The assembly is placed in a vacuum diffusion furnace, heated to 1020-1080° C., and kept warm for 1-30 minutes to obtain a titanium-aluminum/nickel-based superalloy heterogeneous porous sandwich structure product.

进一步,所述贵金属为金、铂或者钯中的任意一种。Further, the noble metal is any one of gold, platinum or palladium.

进一步,所述贵金属层的质量占钎料总质量的0.5wt.%~5wt.%。Further, the mass of the precious metal layer accounts for 0.5wt.%-5wt.% of the total mass of the solder.

进一步,所述镍基非晶薄带的厚度为50μm~200μm。Further, the thickness of the nickel-based amorphous ribbon is 50 μm-200 μm.

进一步,所述镍基非晶薄带的化学成分包括Cr:6%-8%、Si:4%-5%、B:Further, the chemical composition of the nickel-based amorphous strip includes Cr: 6%-8%, Si: 4%-5%, B:

2.75%-3.5%、Fe:2.5%-3.5%、Ni:余量。2.75%-3.5%, Fe: 2.5%-3.5%, Ni: balance.

进一步,所述多孔结构为蜂窝多孔结构、泡沫多孔结构、矩形多孔结构、三角形多孔结构、菱形多孔结构中的任意一种。Further, the porous structure is any one of a honeycomb porous structure, a foam porous structure, a rectangular porous structure, a triangular porous structure, and a rhombus porous structure.

进一步,在真空扩散炉中,真空度小于3.0×10-3Pa后,以20℃/min的升温速度升至1020~1080℃,保温1~30min,5℃/min的降温速度降至600℃,随炉冷却至室温,得到制品。Further, in the vacuum diffusion furnace, after the vacuum degree is less than 3.0×10 -3 Pa, the temperature is raised to 1020-1080°C at a rate of 20°C/min, kept for 1-30min, and the temperature is lowered to 600°C at a rate of 5°C/min , cooled to room temperature with the furnace to obtain the product.

另一方面,本发明另一个实施例还提供了一种钛铝/镍基高温合金异质多孔夹层结构制品,采用上述任意一项所述的方法制备。On the other hand, another embodiment of the present invention also provides a titanium-aluminum/nickel-based superalloy heterogeneous porous sandwich structure product, which is prepared by any one of the methods described above.

本发明具有如下有益效果:The present invention has following beneficial effects:

根据上述制备方法所添加的贵金属未与接头中其它元素反应形成脆性相,而是完全固溶于钎缝中的镍基体,呈弥散分布,形成固溶强化效果,有效提升接头强度。同时,由于采用多孔结构层的平面抗拉强度有效提升了70%以上,断裂位置从芯体与面板的界面转移至芯体中部,有效的提高钎焊接头的力学性能,有效的解决了现有技术中镍基钎料钎焊镍基高温合金芯体与钛铝合金面板时钎缝界面处大量化合物析出富集严重和易形成溶蚀导致性能下降的问题。The precious metal added according to the above preparation method does not react with other elements in the joint to form a brittle phase, but is completely dissolved in the nickel matrix in the brazing joint, and is dispersedly distributed, forming a solid solution strengthening effect and effectively improving the strength of the joint. At the same time, since the planar tensile strength of the porous structure layer is effectively increased by more than 70%, the fracture position is transferred from the interface between the core and the panel to the middle of the core, which effectively improves the mechanical properties of the brazed joint and effectively solves the existing problem. In the technology, when brazing the nickel-based superalloy core body and the titanium-aluminum alloy panel with nickel-based brazing filler metal, a large number of compounds are precipitated and enriched at the interface of the brazing seam, which is prone to corrosion and leads to performance degradation.

附图说明Description of drawings

为了更清楚地说明本发明实施例或现有技术中的技术方案和优点,下面将对实施例或现有技术描述中所需要使用的附图作简单的介绍,显而易见地,下面描述中的附图仅仅是本发明的一些实施例,对于本领域普通技术人员来讲,在不付出创造性劳动的前提下,还可以根据这些附图获得其它附图。In order to more clearly illustrate the technical solutions and advantages in the embodiments of the present invention or in the prior art, the following will briefly introduce the accompanying drawings that need to be used in the description of the embodiments or the prior art. Apparently, the appended The drawings are only some embodiments of the present invention, and those skilled in the art can also obtain other drawings based on these drawings without creative work.

图1为本发明一个实施例所提供的制品的结构示意图;Fig. 1 is a schematic structural view of a product provided by an embodiment of the present invention;

图2为本发明一个实施例所提供的一种钛铝/镍基高温合金异质多孔夹层结构的制备方法流程图。Fig. 2 is a flowchart of a method for preparing a titanium-aluminum/nickel-based superalloy heterogeneous porous sandwich structure provided by an embodiment of the present invention.

具体实施方式detailed description

为了更进一步阐述本发明为达成预定发明目的所采取的技术手段及功效,以下结合附图及较佳实施例,对依据本发明提出的一种钛铝/镍基高温合金异质多孔夹层结构制品及制备方法,其具体实施方式、结构、特征及其功效,详细说明如下。在下述说明中,不同的“一个实施例”或“另一个实施例”指的不一定是同一实施例。此外,一或多个实施例中的特定特征、结构、或特点可由任何合适形式组合。In order to further explain the technical means and effects of the present invention to achieve the intended purpose of the invention, a kind of titanium-aluminum/nickel-based superalloy heterogeneous porous sandwich structure product proposed according to the present invention will be described below in conjunction with the accompanying drawings and preferred embodiments. And preparation method, its specific embodiment, structure, feature and effect thereof, detailed description is as follows. In the following description, different "one embodiment" or "another embodiment" do not necessarily refer to the same embodiment. Furthermore, the particular features, structures, or characteristics of one or more embodiments may be combined in any suitable manner.

除非另有定义,本文所使用的所有的技术和科学术语与属于本发明的技术领域的技术人员通常理解的含义相同。Unless otherwise defined, all technical and scientific terms used herein have the same meaning as commonly understood by one of ordinary skill in the technical field of the invention.

下面结合附图具体的说明本发明所提供的一种钛铝/镍基高温合金异质多孔夹层结构制品及制备方法的具体方案。The specific scheme of a titanium-aluminum/nickel-based superalloy heterogeneous porous sandwich structure product and its preparation method provided by the present invention will be described in detail below with reference to the accompanying drawings.

请参阅图1,本发明一个实施例提供了一种钛铝/镍基高温合金异质多孔夹层结构制品,包括多孔结构、面板、贵金属和镍基非晶薄带。Please refer to FIG. 1 , an embodiment of the present invention provides a titanium-aluminum/nickel-based superalloy heterogeneous porous sandwich structure product, including a porous structure, a panel, a precious metal and a nickel-based amorphous strip.

其中,多孔结构、面板、贵金属和镍基非晶薄带依次按照面板10、贵金属层20、镍基非晶薄带30、多孔结构层40、镍基非晶薄带30、贵金属层20和面板10的顺序层叠设置。Among them, the porous structure, the panel, the noble metal and the nickel-based amorphous strip are in order according to the panel 10, the noble metal layer 20, the nickel-based amorphous strip 30, the porous structure layer 40, the nickel-based amorphous strip 30, the noble metal layer 20 and the panel. 10 sequential cascading settings.

其中,多孔结构层40可以为蜂窝结构层、泡沫多孔结构、矩形多孔结构、三角形多孔结构和菱形多孔结构中的任意一种,材质为镍基高温合金。Wherein, the porous structure layer 40 can be any one of a honeycomb structure layer, a foam porous structure, a rectangular porous structure, a triangular porous structure and a diamond porous structure, and the material is a nickel-based superalloy.

其中,面板10的材质为钛铝合金。Wherein, the material of the panel 10 is titanium aluminum alloy.

其中,贵金属的材质可以为金、铂或者钯。Wherein, the material of the noble metal may be gold, platinum or palladium.

请参阅图2,本发明一个实施例还提供的一种钛铝/镍基高温合金异质多孔夹层结构的制备方法,该制备方法包括以下步骤:Referring to Fig. 2, an embodiment of the present invention also provides a method for preparing a titanium-aluminum/nickel-based superalloy heterogeneous porous sandwich structure, the preparation method comprising the following steps:

步骤S001,获取多孔结构、面板、贵金属和镍基非晶薄带,将所述面板和多孔结构放入丙酮溶液中清洗;其中所述多孔结构的材质为镍基高温合金。Step S001, obtaining a porous structure, a panel, a noble metal, and a nickel-based amorphous strip, and cleaning the panel and the porous structure in an acetone solution; wherein the material of the porous structure is a nickel-based superalloy.

其中,多孔结构可以为蜂窝结构、泡沫多孔结构、矩形多孔结构、三角形多孔结构和菱形多孔结构中的任意一种,材质为镍基高温合金。Wherein, the porous structure can be any one of honeycomb structure, foam porous structure, rectangular porous structure, triangular porous structure and diamond porous structure, and the material is nickel-based superalloy.

其中,贵金属作为靶材,可以为金、铂或者钯中的任意一种;贵金属层的质量占钎料总质量的0.5wt.%~5wt.%。Wherein, the noble metal as the target material can be any one of gold, platinum or palladium; the mass of the noble metal layer accounts for 0.5wt.%-5wt.% of the total mass of the solder.

其中,镍基非晶薄带的厚度为50μm~200μm。镍基非晶薄带也称为BNi-2非晶薄带,按照质量百分比计,其化学成分包括Cr:6%-8%、Si:4%-5%、B:Wherein, the thickness of the nickel-based amorphous strip is 50 μm to 200 μm. Nickel-based amorphous strips are also called BNi-2 amorphous strips. According to mass percentage, its chemical composition includes Cr: 6%-8%, Si: 4%-5%, B:

2.75%-3.5%、Fe:2.5%-3.5%、Ni:余量。2.75%-3.5%, Fe: 2.5%-3.5%, Ni: balance.

其中,面板的材质为钛铝合金。Wherein, the material of the panel is titanium aluminum alloy.

具体的,首先将面板和多孔结构进行电火花线切割加工,得到合适尺寸的面板和多孔芯;然后将处理好的面板和多孔芯放入丙酮溶液中超声清洗10min。Specifically, firstly, the panel and the porous structure are subjected to wire electric discharge processing to obtain a panel and a porous core of a suitable size; then, the processed panel and the porous core are ultrasonically cleaned in an acetone solution for 10 minutes.

步骤S002,采用磁控溅射将贵金属镀在面板的待连接面,形成贵金属层。Step S002, using magnetron sputtering to plate noble metal on the surface to be connected of the panel to form a noble metal layer.

面板的待连接面是指形成夹层结构之后,与其他结构连接在一起的侧面,在该待连接面上镀上贵金属层,而后依次与镍基非晶薄带、多孔结构层构成夹层结构。The surface to be connected of the panel refers to the side that is connected with other structures after forming the sandwich structure. The surface to be connected is plated with a noble metal layer, and then forms a sandwich structure with nickel-based amorphous strip and porous structure layer in turn.

步骤S003,依次按照面板、贵金属层、镍基非晶薄带、多孔结构层、镍基非晶薄带、贵金属层和面板的顺序层叠装配为夹层结构,得到装配件。Step S003 , sequentially stacking and assembling the panel, the precious metal layer, the nickel-based amorphous strip, the porous structure layer, the nickel-based amorphous strip, the noble metal layer and the panel into a sandwich structure to obtain an assembly.

步骤S004,将所述装配件放置于真空扩散炉中,加热温度至1020~1080℃,保温1~30min后,得到制品。Step S004, placing the assembly in a vacuum diffusion furnace, heating the temperature to 1020-1080° C., and keeping it warm for 1-30 minutes to obtain the product.

其中,在真空扩散炉中,真空度小于3.0×10-3Pa后,以20℃/min的升温速度升至1020~1080℃,保温1~30min,5℃/min的降温速度降至600℃,随炉冷却至室温,取出制品。Among them, in the vacuum diffusion furnace, after the vacuum degree is less than 3.0×10 -3 Pa, the temperature is raised to 1020-1080°C at a rate of 20°C/min, kept for 1-30min, and the temperature is reduced to 600°C at a rate of 5°C/min. , cool down to room temperature with the furnace, and take out the product.

根据上述方法所添加的贵金属未与接头中其它元素反应形成脆性相,而是完全固溶于钎缝中的镍基体,呈弥散分布,形成固溶强化效果,有效提升接头强度。其中,本发明实施例中的接头是指多孔结构与面板之间的连接处,芯体是指多孔结构层,下文不再声明。同时,由于采用多孔结构层的平面抗拉强度有效提升了70%以上,断裂位置从芯体与面板的界面转移至芯体的中部,有效的提高接头的力学性能,有效的解决了现有技术中镍基钎料钎焊镍基高温合金芯体与钛铝合金面板时钎缝界面处大量化合物析出富集严重和易形成溶蚀导致性能下降的问题。The precious metal added according to the above method does not react with other elements in the joint to form a brittle phase, but is completely dissolved in the nickel matrix in the brazing joint, and is distributed in a dispersed manner, forming a solid solution strengthening effect and effectively improving the strength of the joint. Wherein, the joint in the embodiment of the present invention refers to the connection between the porous structure and the panel, and the core refers to the porous structure layer, which will not be stated below. At the same time, since the planar tensile strength of the porous structure layer is effectively increased by more than 70%, the fracture position is transferred from the interface between the core and the panel to the middle of the core, which effectively improves the mechanical properties of the joint and effectively solves the problem of the existing technology. When brazing nickel-based superalloy core body and titanium-aluminum alloy panel with medium-nickel-based brazing filler metal, a large number of compounds at the interface of the brazing seam are seriously precipitated and enriched, and it is easy to form corrosion and cause performance degradation.

本申请技术方案不局限于以下所举例的具体实施方式,还包括各具体实施方式之间的任意组合。The technical solution of the present application is not limited to the specific implementation manners exemplified below, but also includes any combination of the specific implementation manners.

实施例1Example 1

钛铝/镍基高温合金异质多孔夹层结构的制备方法,包括:A method for preparing a titanium-aluminum/nickel-based superalloy heterogeneous porous sandwich structure, including:

获取多孔结构、面板、贵金属和镍基非晶薄带,其中,面板材料选用TiAl合金,多孔结构为蜂窝多孔结构,选用的材质为GH3536镍基高温合金,尺寸是40mm×30mm×12mm,芯格内切圆直径为1.6mm,芯体壁厚为0.05mm。镍基非晶薄带也称为BNi-2非晶薄带,该镍基非晶薄带的尺寸为40mm×30mm×0.1mm;Obtain porous structure, panels, precious metals and nickel-based amorphous thin strips. Among them, the panel material is TiAl alloy, the porous structure is a honeycomb porous structure, and the material selected is GH3536 nickel-based superalloy, with a size of 40mm×30mm×12mm. The diameter of the inscribed circle is 1.6mm, and the wall thickness of the core is 0.05mm. The nickel-based amorphous ribbon is also called BNi-2 amorphous ribbon, and the size of the nickel-based amorphous ribbon is 40mm×30mm×0.1mm;

将所述面板和多孔结构进行电火花线切割加工,得到合适尺寸的面板和多孔结构,然后将处理好的面板和多孔结构放入丙酮溶液中超声清洗10min;The panel and the porous structure are subjected to wire electric discharge processing to obtain a panel and the porous structure of a suitable size, and then the processed panel and the porous structure are ultrasonically cleaned in an acetone solution for 10 minutes;

采用磁控溅射将金镀在面板的待连接面,形成贵金属层;金的添加量为2wt.%;Magnetron sputtering is used to plate gold on the surface to be connected of the panel to form a noble metal layer; the amount of gold added is 2wt.%.

依次按照面板、贵金属层、镍基非晶薄带、多孔结构层、镍基非晶薄带、贵金属层和面板的顺序层叠装配为夹层结构,得到装配件;其中镍基非晶薄带的厚度为100μm;The assembly is obtained by stacking and assembling the panel, the noble metal layer, the nickel-based amorphous strip, the porous structure layer, the nickel-based amorphous strip, the noble metal layer and the panel in sequence to form a sandwich structure; the thickness of the nickel-based amorphous strip is 100μm;

将所述装配件放置于真空扩散炉中,当真空度低于3.0×10-3Pa后,以20℃/min的升温速度升至1030℃,保温5min,然后随炉冷却至室温后,取出制品。Place the assembly in a vacuum diffusion furnace. When the vacuum degree is lower than 3.0×10 -3 Pa, raise the temperature to 1030°C at a rate of 20°C/min, keep it warm for 5 minutes, and then cool to room temperature with the furnace, then take it out products.

试验结果表明,试验实现了钛铝/镍基高温合金异质多孔夹层结构制品的接头的强化,接头组织为典型镍基固溶体基体、弥散的硼化物分布于钎缝,金完全固溶于钎缝中的镍基体,并呈现均匀分布,钛铝/镍基高温合金异质多孔夹层结构平拉强度为40.5MPa,断裂于芯体的中部,相比于未添加金的强度提升了80.8%。The test results show that the test has achieved the strengthening of the joints of titanium-aluminum/nickel-based superalloy heterogeneous porous sandwich structure products. The joint structure is a typical nickel-based solid solution matrix, dispersed borides are distributed in the brazing seam, and gold is completely dissolved in the brazing seam. The nickel matrix in the core is evenly distributed. The flat tensile strength of the titanium-aluminum/nickel-based superalloy heterogeneous porous sandwich structure is 40.5MPa, and the fracture is in the middle of the core, which is 80.8% higher than that without gold addition.

实施例2Example 2

钛铝/镍基高温合金异质多孔夹层结构的制备方法,包括:A method for preparing a titanium-aluminum/nickel-based superalloy heterogeneous porous sandwich structure, including:

获取多孔结构、面板、贵金属和镍基非晶薄带,其中,面板材料选用TiAl合金,多孔结构为蜂窝多孔结构,选用的材质为GH3536镍基高温合金,尺寸是40mm×30mm×12mm,芯格内切圆直径为1.6mm,芯体壁厚为0.05mm。镍基非晶薄带也称为BNi-2非晶薄带,该镍基非晶薄带的尺寸为40mm×30mm×0.1mm;Obtain porous structure, panels, precious metals and nickel-based amorphous thin strips. Among them, the panel material is TiAl alloy, the porous structure is a honeycomb porous structure, and the material selected is GH3536 nickel-based superalloy, with a size of 40mm×30mm×12mm. The diameter of the inscribed circle is 1.6mm, and the wall thickness of the core is 0.05mm. The nickel-based amorphous ribbon is also called BNi-2 amorphous ribbon, and the size of the nickel-based amorphous ribbon is 40mm×30mm×0.1mm;

将所述面板和多孔结构进行电火花线切割加工,得到合适尺寸的面板和多孔结构,然后将处理好的面板和多孔结构放入丙酮溶液中超声清洗10min;The panel and the porous structure are subjected to wire electric discharge processing to obtain a panel and the porous structure of a suitable size, and then the processed panel and the porous structure are ultrasonically cleaned in an acetone solution for 10 minutes;

采用磁控溅射将铂镀在面板的待连接面,形成贵金属层;铂的添加量为1wt.%;Magnetron sputtering is used to plate platinum on the surface to be connected of the panel to form a noble metal layer; the amount of platinum added is 1wt.%.

依次按照面板、贵金属层、镍基非晶薄带、多孔结构层、镍基非晶薄带、贵金属层和面板的顺序层叠装配为夹层结构,得到装配件;其中镍基非晶薄带的厚度为100μm;The assembly is obtained by stacking and assembling the panel, the noble metal layer, the nickel-based amorphous strip, the porous structure layer, the nickel-based amorphous strip, the noble metal layer and the panel in sequence to form a sandwich structure; the thickness of the nickel-based amorphous strip is 100μm;

将所述装配件放置于真空扩散炉中,当真空度低于3.0×10-3Pa后,以20℃/min的升温速度升至1040℃,保温5min,然后随炉冷却至室温后,取出制品。Place the assembly in a vacuum diffusion furnace. When the vacuum degree is lower than 3.0×10 -3 Pa, raise the temperature to 1040°C at a rate of 20°C/min, keep it warm for 5 minutes, and then cool to room temperature with the furnace, then take it out products.

试验结果表明,试验实现了钛铝/镍基高温合金异质多孔夹层结构制品的接头的强化,接头组织为典型镍基固溶体基体、弥散的硼化物分布于钎缝,铂完全固溶于钎缝中的镍基体,并呈现均匀分布,钛铝/镍基高温合金异质多孔夹层结构平拉强度为36.5MPa,大部分断裂于芯体,相比于未添加铂的强度提升了63%。The test results show that the test has realized the strengthening of the joints of titanium-aluminum/nickel-based superalloy heterogeneous porous sandwich structure products. The joint structure is a typical nickel-based solid solution matrix, dispersed borides are distributed in the brazing seam, and platinum is completely dissolved in the brazing seam. The nickel matrix in the alloy is evenly distributed, and the flat tensile strength of the titanium-aluminum/nickel-based superalloy heterogeneous porous sandwich structure is 36.5MPa, most of which are broken in the core, which is 63% higher than that without platinum.

实施例3Example 3

钛铝/镍基高温合金异质多孔夹层结构的制备方法,包括:A method for preparing a titanium-aluminum/nickel-based superalloy heterogeneous porous sandwich structure, including:

获取多孔结构、面板、贵金属和镍基非晶薄带,其中,面板材料选用TiAl合金,多孔结构为蜂窝多孔结构,选用的材质为GH3536镍基高温合金,尺寸是40mm×30mm×12mm,芯格内切圆直径为1.6mm,芯体壁厚为0.05mm。镍基非晶薄带也称为BNi-2非晶薄带,该镍基非晶薄带的尺寸为40mm×30mm×0.15mm;Obtain porous structure, panels, precious metals and nickel-based amorphous thin strips. Among them, the panel material is TiAl alloy, the porous structure is a honeycomb porous structure, and the material selected is GH3536 nickel-based superalloy, with a size of 40mm×30mm×12mm. The diameter of the inscribed circle is 1.6mm, and the wall thickness of the core is 0.05mm. The nickel-based amorphous ribbon is also called BNi-2 amorphous ribbon, and the size of the nickel-based amorphous ribbon is 40mm×30mm×0.15mm;

将所述面板和多孔结构进行电火花线切割加工,得到合适尺寸的面板和多孔结构,然后将处理好的面板和多孔结构放入丙酮溶液中超声清洗10min;The panel and the porous structure are subjected to wire electric discharge processing to obtain a panel and the porous structure of a suitable size, and then the processed panel and the porous structure are ultrasonically cleaned in an acetone solution for 10 minutes;

采用磁控溅射将钯镀在面板的待连接面,形成贵金属层;钯的添加量为1.5wt.%;Magnetron sputtering is used to plate palladium on the surface to be connected of the panel to form a noble metal layer; the amount of palladium added is 1.5wt.%.

依次按照面板、贵金属层、镍基非晶薄带、多孔结构层、镍基非晶薄带、贵金属层和面板的顺序层叠装配为夹层结构,得到装配件;其中镍基非晶薄带的厚度为100μm;The assembly is obtained by stacking and assembling the panel, the noble metal layer, the nickel-based amorphous strip, the porous structure layer, the nickel-based amorphous strip, the noble metal layer and the panel in sequence to form a sandwich structure; the thickness of the nickel-based amorphous strip is 100μm;

将所述装配件放置于真空扩散炉中,当真空度低于3.0×10-3Pa后,以20℃/min的升温速度升至1030℃,保温5min,然后随炉冷却至室温后,取出制品。Place the assembly in a vacuum diffusion furnace. When the vacuum degree is lower than 3.0×10 -3 Pa, raise the temperature to 1030°C at a rate of 20°C/min, keep it warm for 5 minutes, and then cool to room temperature with the furnace, then take it out products.

试验结果表明,试验实现了钛铝/镍基高温合金异质多孔夹层结构制品的接头的强化,接头组织为典型镍基固溶体基体、弥散的硼化物分布于钎缝,钯完全固溶于钎缝中的镍基体,并呈现均匀分布,钛铝/镍基高温合金异质多孔夹层结构平拉强度为33.4MPa,断裂于芯体,相比于未添加钯的强度提升了49%。The test results show that the test has realized the strengthening of the joints of titanium-aluminum/nickel-based superalloy heterogeneous porous sandwich structure products. The joint structure is a typical nickel-based solid solution matrix, dispersed borides are distributed in the brazing seam, and palladium is completely dissolved in the brazing seam. The nickel matrix in the alloy is evenly distributed, and the flat tensile strength of the titanium-aluminum/nickel-based superalloy heterogeneous porous sandwich structure is 33.4MPa, which is 49% higher than that without palladium.

实施例4Example 4

钛铝/镍基高温合金异质多孔夹层结构的制备方法,包括:A method for preparing a titanium-aluminum/nickel-based superalloy heterogeneous porous sandwich structure, including:

获取多孔结构、面板、贵金属和镍基非晶薄带,其中,面板材料选用TiAl合金,多孔结构为蜂窝多孔结构,选用的材质为GH3536镍基高温合金,尺寸是40mm×30mm×12mm,芯格内切圆直径为2.6mm,芯体壁厚为0.05mm。镍基非晶薄带也称为BNi-2非晶薄带,该镍基非晶薄带的尺寸为40mm×30mm×0.1mm;Obtain porous structure, panels, precious metals and nickel-based amorphous thin strips. Among them, the panel material is TiAl alloy, the porous structure is a honeycomb porous structure, and the material selected is GH3536 nickel-based superalloy, with a size of 40mm×30mm×12mm. The diameter of the inscribed circle is 2.6mm, and the wall thickness of the core is 0.05mm. The nickel-based amorphous ribbon is also called BNi-2 amorphous ribbon, and the size of the nickel-based amorphous ribbon is 40mm×30mm×0.1mm;

将所述面板和多孔结构进行电火花线切割加工,得到合适尺寸的面板和多孔结构,然后将处理好的面板和多孔结构放入丙酮溶液中超声清洗10min;The panel and the porous structure are subjected to wire electric discharge processing to obtain a panel and the porous structure of a suitable size, and then the processed panel and the porous structure are ultrasonically cleaned in an acetone solution for 10 minutes;

采用磁控溅射将金镀在面板的待连接面,形成贵金属层;金的添加量为1.5wt.%;Magnetron sputtering is used to plate gold on the surface to be connected of the panel to form a noble metal layer; the amount of gold added is 1.5wt.%.

依次按照面板、贵金属层、镍基非晶薄带、多孔结构层、镍基非晶薄带、贵金属层和面板的顺序层叠装配为夹层结构,得到装配件;其中镍基非晶薄带的厚度为100μm;The assembly is obtained by stacking and assembling the panel, the noble metal layer, the nickel-based amorphous strip, the porous structure layer, the nickel-based amorphous strip, the noble metal layer and the panel in sequence to form a sandwich structure; the thickness of the nickel-based amorphous strip is 100μm;

将所述装配件放置于真空扩散炉中,当真空度低于3.0×10-3Pa后,以20℃/min的升温速度升至1050℃,保温1min,然后随炉冷却至室温后,取出制品。Place the assembly in a vacuum diffusion furnace. When the vacuum degree is lower than 3.0×10 -3 Pa, raise the temperature to 1050°C at a rate of 20°C/min, keep it warm for 1min, and then cool to room temperature with the furnace, then take it out products.

试验结果表明,试验实现了钛铝/镍基高温合金异质多孔夹层结构制品的接头的强化,接头组织为典型镍基固溶体基体,接头处形成良好的钝角,钛铝/镍基高温合金异质多孔夹层结构平拉强度为20.4MPa,断裂于芯体的中部,相比于未添加金的强度提升了90.3%。The test results show that the test has realized the strengthening of the joints of titanium-aluminum/nickel-based superalloy heterogeneous porous sandwich structure products. The joint structure is a typical nickel-based solid solution matrix, and a good obtuse angle is formed at the joint. The tensile strength of the porous sandwich structure is 20.4MPa, and the fracture is in the middle of the core, which is 90.3% higher than that without gold addition.

需要说明的是:上述本发明实施例先后顺序仅仅为了描述,不代表实施例的优劣。且上述对本说明书特定实施例进行了描述。其它实施例在所附权利要求书的范围内。在一些情况下,在权利要求书中记载的动作或步骤可以按照不同于实施例中的顺序来执行并且仍然可以实现期望的结果。另外,在附图中描绘的过程不一定要求示出的特定顺序或者连续顺序才能实现期望的结果。在某些实施方式中,多任务处理和并行处理也是可以的或者可能是有利的。It should be noted that: the order of the above embodiments of the present invention is only for description, and does not represent the advantages and disadvantages of the embodiments. And the above describes the specific embodiments of this specification. Other implementations are within the scope of the following claims. In some cases, the actions or steps recited in the claims can be performed in an order different from that in the embodiments and still achieve desirable results. In addition, the processes depicted in the accompanying figures do not necessarily require the particular order shown, or sequential order, to achieve desirable results. Multitasking and parallel processing are also possible or may be advantageous in certain embodiments.

本说明书中的各个实施例均采用递进的方式描述,各个实施例之间相同相似的部分互相参见即可,每个实施例重点说明的都是与其他实施例的不同之处。Each embodiment in this specification is described in a progressive manner, the same and similar parts of each embodiment can be referred to each other, and each embodiment focuses on the differences from other embodiments.

以上所述仅为本发明的较佳实施例,并不用以限制本发明,凡在本发明的精神和原则之内,所作的任何修改、等同替换、改进等,均应包含在本发明的保护范围之内。The above descriptions are only preferred embodiments of the present invention, and are not intended to limit the present invention. Any modifications, equivalent replacements, improvements, etc. made within the spirit and principles of the present invention shall be included in the protection of the present invention. within range.

Claims (8)

1.一种钛铝/镍基高温合金异质多孔夹层结构制备方法,其特征在于,该制备方法包括以下步骤:1. A method for preparing a titanium-aluminum/nickel-based superalloy heterogeneous porous sandwich structure, characterized in that the preparation method comprises the following steps: 获取多孔结构、面板、贵金属和镍基非晶薄带,将所述面板和多孔结构放入丙酮溶液中清洗;其中所述多孔结构的材质为镍基高温合金,所述面板的材质为钛铝合金;Obtain the porous structure, panel, noble metal and nickel-based amorphous strip, put the panel and porous structure into an acetone solution for cleaning; wherein the material of the porous structure is a nickel-based superalloy, and the material of the panel is titanium aluminum alloy; 采用磁控溅射将所述贵金属镀在面板的待连接面,形成贵金属层;Plating the noble metal on the surface to be connected of the panel by magnetron sputtering to form a noble metal layer; 依次按照面板、贵金属层、镍基非晶薄带、多孔结构层、镍基非晶薄带、贵金属层和面板的顺序层叠装配为夹层结构,得到装配件;The sandwich structure is obtained by stacking and assembling the panel, the noble metal layer, the nickel-based amorphous strip, the porous structure layer, the nickel-based amorphous strip, the noble metal layer and the panel in sequence; 将所述装配件放置于真空扩散炉中,加热温度至1020~1080℃,保温1~30min后,得到钛铝/镍基高温合金异质多孔夹层结构制品。The assembly is placed in a vacuum diffusion furnace, heated to 1020-1080° C., and kept warm for 1-30 minutes to obtain a titanium-aluminum/nickel-based superalloy heterogeneous porous sandwich structure product. 2.根据权利要求1所述的钛铝/镍基高温合金异质多孔夹层结构制备方法,其特征在于,所述贵金属为金、铂或者钯中的任意一种。2. The method for preparing a titanium-aluminum/nickel-based superalloy heterogeneous porous sandwich structure according to claim 1, wherein the noble metal is any one of gold, platinum or palladium. 3.根据权利要求1所述的钛铝/镍基高温合金异质多孔夹层结构制备方法,其特征在于,所述贵金属层的质量占钎料总质量的0.5wt.%~5wt.%。3. The method for preparing a titanium-aluminum/nickel-based superalloy heterogeneous porous sandwich structure according to claim 1, wherein the mass of the noble metal layer accounts for 0.5wt.%-5wt.% of the total mass of the solder. 4.根据权利要求1所述的钛铝/镍基高温合金异质多孔夹层结构制备方法,其特征在于,所述镍基非晶薄带的厚度为50μm~200μm。4 . The method for preparing a titanium-aluminum/nickel-based superalloy heterogeneous porous sandwich structure according to claim 1 , wherein the thickness of the nickel-based amorphous ribbon is 50 μm to 200 μm. 5.根据权利要求1所述的钛铝/镍基高温合金异质多孔夹层结构制备方法,其特征在于,所述镍基非晶薄带的化学成分包括Cr:6%-8%、Si:4%-5%、B:2.75%-3.5%、Fe:2.5%-3.5%、Ni:余量。5. The method for preparing a titanium-aluminum/nickel-based superalloy heterogeneous porous sandwich structure according to claim 1, wherein the chemical composition of the nickel-based amorphous ribbon includes Cr: 6%-8%, Si: 4%-5%, B: 2.75%-3.5%, Fe: 2.5%-3.5%, Ni: balance. 6.根据权利要求1所述的钛铝/镍基高温合金异质多孔夹层结构制备方法,其特征在于,所述多孔结构为蜂窝多孔结构、泡沫多孔结构、矩形多孔结构、三角形多孔结构、菱形多孔结构中的任意一种。6. The method for preparing a titanium-aluminum/nickel-based superalloy heterogeneous porous sandwich structure according to claim 1, wherein the porous structure is a honeycomb porous structure, a foam porous structure, a rectangular porous structure, a triangular porous structure, a rhombus Any of the porous structures. 7.根据权利要求1所述的钛铝/镍基高温合金异质多孔夹层结构制备方法,其特征在于,在真空扩散炉中,真空度小于3.0×10-3Pa后,以20℃/min的升温速度升至1020~1080℃,保温1~30min,5℃/min的降温速度降至600℃,随炉冷却至室温,得到制品。7. The method for preparing a titanium-aluminum/nickel-based superalloy heterogeneous porous sandwich structure according to claim 1, characterized in that, in the vacuum diffusion furnace, after the vacuum degree is less than 3.0×10 -3 Pa, at 20°C/min The heating rate is raised to 1020-1080°C, the temperature is kept for 1-30 minutes, the cooling rate is 5°C/min to 600°C, and the product is obtained by cooling to room temperature with the furnace. 8.一种钛铝/镍基高温合金异质多孔夹层结构制品,其特征在于,采用权利要求1-7任意一项所述的方法制备。8. A titanium-aluminum/nickel-based superalloy heterogeneous porous sandwich structure product, characterized in that it is prepared by the method described in any one of claims 1-7.
CN202210092389.1A 2022-01-26 2022-01-26 Titanium-aluminum/nickel-based high-temperature alloy heterogeneous porous sandwich structure product and preparation method thereof Pending CN115519198A (en)

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN118548274A (en) * 2024-07-15 2024-08-27 太原理工大学 Assembled high temperature resistant porous material based on nickel-based alloy ultra-thin strip and preparation method

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN118548274A (en) * 2024-07-15 2024-08-27 太原理工大学 Assembled high temperature resistant porous material based on nickel-based alloy ultra-thin strip and preparation method

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