CN111496417A - Ti-Ni-Nb-Zr brazing material of Nb-Si-based ultrahigh-temperature structural material and brazing connection process - Google Patents

Ti-Ni-Nb-Zr brazing material of Nb-Si-based ultrahigh-temperature structural material and brazing connection process Download PDF

Info

Publication number
CN111496417A
CN111496417A CN202010392447.3A CN202010392447A CN111496417A CN 111496417 A CN111496417 A CN 111496417A CN 202010392447 A CN202010392447 A CN 202010392447A CN 111496417 A CN111496417 A CN 111496417A
Authority
CN
China
Prior art keywords
brazing
temperature structural
temperature
high temperature
brazing material
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
CN202010392447.3A
Other languages
Chinese (zh)
Other versions
CN111496417B (en
Inventor
任新宇
熊华平
静永娟
程耀永
尚泳来
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
AECC Beijing Institute of Aeronautical Materials
Original Assignee
AECC Beijing Institute of Aeronautical Materials
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by AECC Beijing Institute of Aeronautical Materials filed Critical AECC Beijing Institute of Aeronautical Materials
Priority to CN202010392447.3A priority Critical patent/CN111496417B/en
Publication of CN111496417A publication Critical patent/CN111496417A/en
Application granted granted Critical
Publication of CN111496417B publication Critical patent/CN111496417B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Classifications

    • 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
    • B23K35/00Rods, electrodes, materials, or media, for use in soldering, welding, or cutting
    • B23K35/22Rods, electrodes, materials, or media, for use in soldering, welding, or cutting characterised by the composition or nature of the material
    • B23K35/24Selection of soldering or welding materials proper
    • B23K35/32Selection of soldering or welding materials proper with the principal constituent melting at more than 1550 degrees C
    • B23K35/325Ti as the principal constituent
    • 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
    • B23K1/20Preliminary treatment of work or areas to be soldered, e.g. in respect of a galvanic coating
    • B23K1/206Cleaning

Abstract

The invention belongs to the technical field of welding, and particularly relates to a Ti-Ni-Nb-Zr brazing material of an Nb-Si-based ultrahigh-temperature structural material and a brazing connection process. At present, a special brazing material for connecting Nb-Si based ultra-high temperature structural materials is lacked, the content of brittle phases in the joint can be reduced, and the brazed joint with higher strength is obtained. The Ti-Ni-Nb-Zr brazing solder of the Nb-Si based ultrahigh temperature structural material comprises the following chemical components in percentage by weight: ni: 15.0-20.0, Nb: 12.0 to 18.0, Zr: 18.0 to 25.0, and the balance Ti. The brazing solder has good spreading performance, can be well wetted and spread on the Nb-Si base surface, has good plasticity, can be processed into different brazing solder forms, and is beneficial to adding and assembling the brazing solder before welding.

Description

Ti-Ni-Nb-Zr brazing material of Nb-Si-based ultrahigh-temperature structural material and brazing connection process
Technical Field
The invention belongs to the technical field of welding, and particularly relates to a Ti-Ni-Nb-Zr brazing material of an Nb-Si-based ultrahigh-temperature structural material and a brazing connection process.
Background
Advanced aircraft engines have higher turbine temperatures, which require higher temperature capability of the blade material. At present, the temperature bearing capacity of the fifth generation nickel-based single crystal superalloy, which is the most advanced blade material, still does not exceed 1150 ℃, and reaches more than 80% of the melting point of the fifth generation nickel-based single crystal superalloy, and the fifth generation nickel-based single crystal superalloy approaches the limit use temperature of the fifth generation nickel-based single crystal superalloy, so that the use requirement of a future high-performance engine is difficult to meet.
The Nb-Si based ultra-high temperature structural material mainly consists of a solid solution of Nb (Nb)SS) And an intermetallic compound Nb5Si3Two-phase composition of NbSSHas good room temperature toughness and intermetallic compound phase Nb5Si3The high-temperature-resistant material has excellent high-temperature strength, large unit cell lattice constant, difficulty in dislocation and creep, good creep resistance and thermodynamic stability at 1600-1800 ℃. The Nb-Si based ultra-high temperature structural material with a tough/brittle two-phase structure is formed by NbSSProviding room temperature ductility of the material, Nb5Si3The high-temperature strength is provided, the excellent high-temperature strength is ensured, and meanwhile, the high-temperature strength has certain room temperature plasticity, and is expected to become a next-generation advanced aeroengine blade material. Generally speaking, the service temperature can be as high as 1200-1400 ℃.
The Nb-Si based ultra-high temperature structural material has high melting point, high rigidity, low density and excellent high temperature strength, has great potential to replace the existing Ni based high temperature alloy and is applied to the aerospace field. Soldering/joining is one of the indispensable key manufacturing techniques to achieve its engineering applications. At present, few relevant documents are reported about the connection of the materials. The connection of Nb-Si-based ultrahigh-temperature structural materials can be realized by adopting traditional Ni-based brazing materials BNi-2(Ni-7Cr-5Si-3B-3Fe, mass percent), BNi-5(Ni-19Cr-10Si, mass percent) and the like, but the excessively high Ni content in the brazing materials enables a large amount of Ni-Nb and Ni-B brittle intermetallic compound phases to be generated in a joint, so that the defects of microcracks, unwelded joints and the like are generated in the joint, and the joint strength is low.
Therefore, the special brazing material for connecting Nb-Si based ultra-high temperature structural materials is lacked, the content of brittle phases in the joint can be reduced, and the brazed joint with higher strength is obtained.
Disclosure of Invention
The invention aims to specially design a Ti-Ni-Nb-Zr brazing material of an Nb-Si-based ultrahigh-temperature structural material and a brazing connection process aiming at the technical defects, so that the effective brazing connection of the Nb-Si-based ultrahigh-temperature structural material is realized, and a brazed joint with excellent room temperature and high temperature strength is obtained.
The purpose of the invention is realized by the following technical scheme:
a Ti-Ni-Nb-Zr brazing solder of an Nb-Si based ultrahigh temperature structure material comprises the following chemical components in percentage by weight: ni: 15.0-20.0, Nb: 12.0 to 18.0, Zr: 18.0 to 25.0, and the balance Ti.
Optionally, the brazing material comprises the following chemical components in percentage by weight: ni: 15.0 to 17.0, Nb: 12.0 to 18.0, Zr: 18.0 to 25.0, and the balance Ti.
Optionally, the brazing material comprises the following chemical components in percentage by weight: ni: 17.0 to 20.0, Nb: 12.0 to 18.0, Zr: 18.0 to 25.0, and the balance Ti.
Optionally, the brazing material comprises the following chemical components in percentage by weight: ni: 16.0, Nb: 12.0 to 18.0, Zr: 18.0 to 25.0, and the balance Ti.
Optionally, the brazing material comprises the following chemical components in percentage by weight: ni: 15.0-20.0, Nb: 14.0 to 18.0, Zr: 18.0 to 25.0, and the balance Ti.
Optionally, the brazing material comprises the following chemical components in percentage by weight: ni: 15.0-20.0, Nb: 12.0 to 18.0, Zr: 20.0, and the balance being Ti.
The brazing connection process of the Nb-Si based ultrahigh-temperature structural material adopts the Ti-Ni-Nb-Zr brazing material and comprises the following steps:
cleaning the surfaces of a first Nb-Si-based ultrahigh-temperature structure material and a second Nb-Si-based ultrahigh-temperature structure material to be brazed, and assembling, wherein the fit clearance of the first Nb-Si-based ultrahigh-temperature structure material and the second Nb-Si-based ultrahigh-temperature structure material is 0.02-0.09 mm;
fixing the brazing solder at the fitting angle of the first Nb-Si base ultra-high temperature structure material and the second Nb-Si base ultra-high temperature structure material to be welded or between the first Nb-Si base ultra-high temperature structure material and the second Nb-Si base ultra-high temperature structure material to be welded, and ensuring close fitting;
step three, uniformly coating aluminum oxide flow resisting agents on the top and the bottom of a welding seam, and then placing a combination of the first Nb-Si-based ultrahigh-temperature structural material and the second Nb-Si-based ultrahigh-temperature structural material to be welded and the brazing material in a vacuum heating furnace for brazing;
step four, adjusting the vacuum degree in the furnace to be better than 8 × 10-3And when Pa is needed, heating, wherein the heating speed is not more than 15 ℃/min, the brazing connection temperature is 1250-1290 ℃, the heat preservation time is 50-100 min, and furnace cooling is carried out after the heat preservation is finished.
Optionally, the braze is in the form of a block, a strip, a wire, or an alloy powder.
Optionally, the first Nb-Si-based ultra-high temperature structural material and the second Nb-Si-based ultra-high temperature structural material are assembled and combined by adopting a butt joint or splicing method.
Alternatively, the braze joint temperature is 1270 ℃.
The technical scheme of the invention has the advantages and beneficial effects that:
1. the solder has good spreading performance, can be well wetted and spread on the surface of the Nb-Si-based alloy, has good plasticity, can be processed into different solder forms such as blocks, strips, wires or alloy powder, and is beneficial to adding and assembling the solder before welding;
2. in the invention, a certain content of Ni is added for reducing the melting point of the brazing solder, but the content of the Ni element in the brazing solder is controlled to be not more than 20 percent by mass, so that the generation tendency and the content of Ni-Nb and Ni-Ti brittle compound phases in the joint can be reduced; the other elements Nb and Ti in the brazing material are constituent elements of Nb-Si alloy base metal, and the element Zr and Nb are completely mutually soluble, so that the brazing material has good compatibility with the welded Nb-Si base metal, and the joint performance is improved;
3. the brazing filler metal disclosed by the invention is combined with related binary alloy phase diagram theoretical calculation and repeated test optimization to obtain brazing filler metal components with reasonable Ti-Ni-Nb-Zr component distribution ratio, the melting temperature range is 1194-1223 ℃, the connection can be carried out within the brazing temperature range of 1230-1300 ℃, the recommended brazing connection temperature is 1250-1290 ℃, the heat treatment temperature is lower than that of Nb-Si base metal (1450-1500 ℃), and the performance of the base metal is not damaged; moreover, under the condition that the brazing connection temperature is 1250-1290 ℃, and the fit clearance of the materials to be welded is 0.02-0.09 mm, the welding seam can be welded at one time without repair welding, and the defects of corrosion, fusion, microcrack and the like in the brazing seam can be ensured;
4. the brazing filler metal and the joint obtained under the process condition have high performance, the joint structure obtained by interdiffusion of the brazing filler metal and the base metal is close to the base metal, and the joint mainly comprises (Nb, Ti) solid solution phase and Nb5Si3Phase composition, and Ti, Zr and Ni elements in the brazing filler metal are dissolved in (Nb, Ti)SSAnd (Nb, Ti, Zr)5Si3In the phase, the connecting joint does not have residual brazing filler metal with the melting temperature of 1194-1223 ℃ or brittle intermetallic compound phases such as Ni-Nb, Ni-Ti and the like. When the Ni-based brazing filler metal is adopted, a large amount of brittle intermetallic compound phases such as Nb-Ni, Ni-Si, Ni-B and the like are generated in a joint due to high elements such as Si, B and the like, so that the joint strength is low, and even microcracks occur in the joint. The room-temperature bending strength of the connection joint obtained by the brazing material reaches 330-363 MPa, reaches 60-66% of the room-temperature bending strength (550MPa) of a base material, and is 40-45% higher than that of a Ni-based brazing filler metal joint. Due to the main phase (Nb, Ti) in the soldered jointSSAnd (Nb, Ti, Zr)5Si3The melting temperature of the phase is up to more than 2000 ℃, so that the connecting joint has satisfactory high-temperature strength, the high-temperature bending strength of the joint reaches 152-168 MPa at 1200 ℃, 54-60% of the high-temperature bending strength (280MPa) of the base material is reached, and the performance of the connecting joint exceeds that of other conventional brazing materials;
5. the brazing material is green and environment-friendly, does not contain toxic elements, and does not contain noble metal elements such as Ag, Au, Pd, Pt and the like.
Drawings
FIG. 1 is a schematic view of a weld configuration of an embodiment of a butt joint;
fig. 2 is a schematic view of a welding structure of an embodiment of the plug connector.
In the figure: 1 is a first Nb-Si based ultra-high temperature structural material to be brazed, 2 is a second Nb-Si based ultra-high temperature structural material to be brazed, and 3 is brazing solder.
Detailed Description
The technical scheme of the invention is further detailed in the following by combining the drawings and the embodiment:
referring to fig. 1 for the butt-joint brazing position and fig. 2 for the splicing brazing position, the brazing material 3 is fixed at the fitting angle of the first and second Nb-Si based ultra-high temperature structural materials 1 and 2 to be welded or is arranged between the two materials, and close fitting is ensured.
Table 1 shows the components and weight percentage compositions of the Ti-Ni-Nb-Zr brazing material for the Nb-Si based ultra high temperature structural material according to the technical solution of the present invention, and lists examples of 16 Ti-Ni-Nb-Zr brazing materials.
TABLE 1 compositions and weight percentages of brazing materials in examples of the invention
Figure BDA0002486310770000051
Figure BDA0002486310770000061
The following 11 components (all atomic ratios) Nb-Si based ultra-high temperature structural materials are brazed and connected by adopting the brazing materials with the compositions of examples 1 to 16 shown in Table 1 and respectively used as blocks, strips, wires or alloy powder at the brazing temperature of 1250-1290 ℃ for the heat preservation time of 50-100 min:
(1)Nb-17Si-23Ti;
(2)Nb-18Si-24Ti-2Cr-2Al-2Hf;
(3)Nb-16Si-22Ti-3Cr-2Al-2Hf;
(4)NB-17Si-20Ti-8Zr-2Al-2Hf;
(5)Nb-18Si-20Ti-12Zr-3Mo-2Al;
(6)Nb-26Si-22Ti-6Cr-3Al-2Hf;
(7)Nb-16Si-22Ti-3Cr-3Al-2Hf;
(8)Nb-12Si-24Ti-4Cr-4Al-2Hf;
(9)Nb-20Si-24Ti-2Cr-2Al;
(10)Nb-16Si-10Ti-10Zr-3Cr-3Al-2Hf;
(11)Nb-16Si-20Ti-4V-3Cr-3Al-2Hf。
verification of connection effect of each embodiment: the joint structure obtained by interdiffusion of the brazing filler metal and the base metal is close to the base metal and mainly comprises (Nb, Ti) solid solution phase and Nb5Si3Phase composition, and Ti, Zr and Ni elements in the brazing filler metal are dissolved in (Nb, Ti)SSAnd (Nb, Ti, Zr)5Si3In the phase, the connecting joint does not have residual brazing filler metal with the melting temperature of 1194-1223 ℃ or brittle intermetallic compound phases such as Ni-Nb, Ni-Ti and the like. The room-temperature bending strength of the connection joint obtained by the brazing material reaches 330-363 MPa, reaches 60-66% of the room-temperature bending strength (550MPa) of a base material, and is 40-45% higher than that of a Ni-based brazing filler metal joint. Due to the main phase (Nb, Ti) in the soldered jointSSAnd (Nb, Ti, Zr)5Si3The melting temperature of the phase is up to more than 2000 ℃, so that the connecting joint has satisfactory high-temperature strength, the high-temperature bending strength of the joint reaches 152-168 MPa at 1200 ℃, 54-60% of the high-temperature bending strength (280MPa) of the base material is reached, and the performance of the connecting joint exceeds that of other conventional brazing materials.
It should be noted that, in the embodiments described in the present invention, the formula of the brazing material, the name of the process, the name and specific components of the material to be brazed, etc. may be different. All equivalent or simple changes of the structure, the characteristics and the principle based on the patent conception of the invention are included in the protection scope of the invention.

Claims (10)

1. A Ti-Ni-Nb-Zr brazing solder of an Nb-Si based ultrahigh temperature structure material is characterized in that: the brazing material comprises the following chemical components in percentage by weight: ni: 15.0-20.0, Nb: 12.0 to 18.0, Zr: 18.0 to 25.0, and the balance Ti.
2. The Ti-Ni-Nb-Zr brazing material according to claim 1, characterized in that: the brazing material comprises the following chemical components in percentage by weight: ni: 15.0 to 17.0, Nb: 12.0 to 18.0, Zr: 18.0 to 25.0, and the balance Ti.
3. The Ti-Ni-Nb-Zr brazing material according to claim 1, characterized in that: the brazing material comprises the following chemical components in percentage by weight: ni: 17.0 to 20.0, Nb: 12.0 to 18.0, Zr: 18.0 to 25.0, and the balance Ti.
4. The Ti-Ni-Nb-Zr brazing material according to claim 1, characterized in that: the brazing material comprises the following chemical components in percentage by weight: ni: 16.0, Nb: 12.0 to 18.0, Zr: 18.0 to 25.0, and the balance Ti.
5. The Ti-Ni-Nb-Zr brazing material according to claim 1, characterized in that: the brazing material comprises the following chemical components in percentage by weight: ni: 15.0-20.0, Nb: 14.0 to 18.0, Zr: 18.0 to 25.0, and the balance Ti.
6. The Ti-Ni-Nb-Zr brazing material according to claim 1, characterized in that: the brazing material comprises the following chemical components in percentage by weight: ni: 15.0-20.0, Nb: 12.0 to 18.0, Zr: 20.0, and the balance being Ti.
7. A brazing connection process of an Nb-Si based ultrahigh-temperature structural material is characterized by comprising the following steps: a Ti-Ni-Nb-Zr brazing material according to any one of claims 1 to 6 is used and comprises the steps of:
cleaning the surfaces of a first Nb-Si-based ultrahigh-temperature structural material (1) and a second Nb-Si-based ultrahigh-temperature structural material (2) to be brazed, and assembling, wherein the fit clearance of the first Nb-Si-based ultrahigh-temperature structural material and the second Nb-Si-based ultrahigh-temperature structural material is 0.02-0.09 mm;
fixing the brazing solder (3) at the matching angle of the first Nb-Si base ultra-high temperature structure material (1) and the second Nb-Si base ultra-high temperature structure material (2) to be welded or between the first Nb-Si base ultra-high temperature structure material and the second Nb-Si base ultra-high temperature structure material to be welded, and ensuring close fitting;
step three, uniformly coating an alumina flow inhibitor on the top and the bottom of a welding seam, and then placing a combination of the first Nb-Si-based ultrahigh-temperature structural material (1) and the second Nb-Si-based ultrahigh-temperature structural material (2) to be welded and the brazing solder (3) in a vacuum heating furnace for brazing;
step four, adjusting the vacuum degree in the furnace to be better than 8 × 10-3At Pa, the temperature starts to riseThe speed is not more than 15 ℃/min, the brazing connection temperature is 1250-1290 ℃, the heat preservation time is 50-100 min, and furnace cooling is carried out after the heat preservation is finished.
8. The process for braze joining of Nb-Si based ultra high temperature structural materials as claimed in claim 7, wherein: the brazing material (3) is in the form of a block, a strip, a wire or an alloy powder.
9. The process for braze joining of Nb-Si based ultra high temperature structural materials as claimed in claim 7, wherein: and assembling and combining the first Nb-Si based ultra-high temperature structural material (1) and the second Nb-Si based ultra-high temperature structural material (2) by adopting a butt joint or splicing method.
10. The process for braze joining of Nb-Si based ultra high temperature structural materials as claimed in claim 7, wherein: the braze joint temperature was 1270 ℃.
CN202010392447.3A 2020-05-11 2020-05-11 Ti-Ni-Nb-Zr brazing material of Nb-Si-based ultrahigh-temperature structural material and brazing connection process Active CN111496417B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202010392447.3A CN111496417B (en) 2020-05-11 2020-05-11 Ti-Ni-Nb-Zr brazing material of Nb-Si-based ultrahigh-temperature structural material and brazing connection process

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202010392447.3A CN111496417B (en) 2020-05-11 2020-05-11 Ti-Ni-Nb-Zr brazing material of Nb-Si-based ultrahigh-temperature structural material and brazing connection process

Publications (2)

Publication Number Publication Date
CN111496417A true CN111496417A (en) 2020-08-07
CN111496417B CN111496417B (en) 2021-12-24

Family

ID=71866826

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202010392447.3A Active CN111496417B (en) 2020-05-11 2020-05-11 Ti-Ni-Nb-Zr brazing material of Nb-Si-based ultrahigh-temperature structural material and brazing connection process

Country Status (1)

Country Link
CN (1) CN111496417B (en)

Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS63317276A (en) * 1987-06-18 1988-12-26 Tanaka Kikinzoku Kogyo Kk Gold alloy filler metal for brazing
JPH06228714A (en) * 1993-02-05 1994-08-16 Hitachi Metals Ltd Low thermal expansion superalloy excellent in oxidation resistance
CN1122839A (en) * 1994-11-11 1996-05-22 冶金工业部包头稀土研究院 Process for producing high rare earth content, Cr-Al-rare earth metal-Fe alloy
CN103949802A (en) * 2014-04-23 2014-07-30 华南理工大学 Ti-Zr-Cu-Ni-Co-Mo amorphous brazing filler metal and preparing method thereof
CN104032240A (en) * 2014-03-05 2014-09-10 中国科学院金属研究所 A Zr-Cu-Ni-Al-Ag-Y block amorphous alloy, a preparation method thereof and applications thereof
CN108381057A (en) * 2018-01-22 2018-08-10 北京科技大学 A kind of preparation and method for welding for being brazed the CoTiNb solders of Nb-Ti high temperature alloys
CN110605498A (en) * 2019-05-14 2019-12-24 中国航发北京航空材料研究院 TiNiNbZr high-temperature brazing filler metal for TiAl alloy, preparation method and brazing method thereof
CN110666395A (en) * 2019-10-21 2020-01-10 中国航发北京航空材料研究院 Brazing filler metal for brazing titanium-containing material, preparation method and brazing method

Patent Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS63317276A (en) * 1987-06-18 1988-12-26 Tanaka Kikinzoku Kogyo Kk Gold alloy filler metal for brazing
JPH06228714A (en) * 1993-02-05 1994-08-16 Hitachi Metals Ltd Low thermal expansion superalloy excellent in oxidation resistance
CN1122839A (en) * 1994-11-11 1996-05-22 冶金工业部包头稀土研究院 Process for producing high rare earth content, Cr-Al-rare earth metal-Fe alloy
CN104032240A (en) * 2014-03-05 2014-09-10 中国科学院金属研究所 A Zr-Cu-Ni-Al-Ag-Y block amorphous alloy, a preparation method thereof and applications thereof
CN103949802A (en) * 2014-04-23 2014-07-30 华南理工大学 Ti-Zr-Cu-Ni-Co-Mo amorphous brazing filler metal and preparing method thereof
CN108381057A (en) * 2018-01-22 2018-08-10 北京科技大学 A kind of preparation and method for welding for being brazed the CoTiNb solders of Nb-Ti high temperature alloys
CN110605498A (en) * 2019-05-14 2019-12-24 中国航发北京航空材料研究院 TiNiNbZr high-temperature brazing filler metal for TiAl alloy, preparation method and brazing method thereof
CN110666395A (en) * 2019-10-21 2020-01-10 中国航发北京航空材料研究院 Brazing filler metal for brazing titanium-containing material, preparation method and brazing method

Also Published As

Publication number Publication date
CN111496417B (en) 2021-12-24

Similar Documents

Publication Publication Date Title
CN109877413B (en) Brazing material for SiC ceramic brazing and brazing method
CN109420862B (en) Powder brazing filler metal for nickel-based single crystal superalloy connection and preparation method and application thereof
CN112008180B (en) High-performance brazing method of Ni3 Al-based single crystal alloy
CN113909610B (en) High-performance brazing method for third-generation single crystal high-temperature alloy
CN105499833A (en) High-temperature brazing material for brazing tungsten-copper alloy and copper or copper alloy and brazing method of high-temperature brazing material
CN106141494B (en) Solder and preparation method and soldering processes for soldering Mo Re alloys foil
CN111438464B (en) Ti-Ni-Nb-Zr-Hf brazing material of Nb-Si-based ultrahigh-temperature structure material and brazing connection process
CN102873422B (en) Aluminum and aluminum alloy and copper diffusion brazing process
CN105965176B (en) For soldering tungsten-copper alloy and the Ni base chilling solders and soldering processes of stainless steel
CN101992331B (en) Vacuum brazing process for super-Ni laminated material and Cr18-Ni8 stainless steel
CN111496417B (en) Ti-Ni-Nb-Zr brazing material of Nb-Si-based ultrahigh-temperature structural material and brazing connection process
CN111438465B (en) Ti-Ni-Nb brazing material of Nb-Si based ultra-high temperature structure material and brazing connection process
CN105618958A (en) Solder used for vacuum active brazing process of W-Cu composite material and stainless steel and method
CN105618957A (en) Solder used for vacuum active brazing process of W-Cu composite material and stainless steel and method
CN107160059A (en) A kind of preparation of Ni base solders for soldering Nb Ti high temperature alloys and method for welding
CN115476012A (en) Application of Cu-Ti brazing filler metal with high Cu atomic ratio in ceramic-metal brazing
CN114749743A (en) High-temperature connection method for brazing C/C composite material and Ni-based alloy by adopting pure Cu
CN112621020B (en) Nickel-based flux-cored brazing filler metal, preparation method and application
CN110369907B (en) Brazing filler metal for connecting high Nb-TiAl alloy and alumina ceramic and connecting method thereof
CN111151864B (en) Welding material and process for connecting tungsten-based powder alloy and low-expansion high-temperature alloy
CN112958865A (en) Method for welding Al-Cu dissimilar materials by preset brazing filler metal
CN115194275B (en) Method for brazing dissimilar metals of titanium alloy and nickel-based superalloy
CN105397339B (en) A kind of brazing material for TiC Ceramic brazings
CN114888388B (en) Method for brazing titanium alloy and nickel-based superalloy
JPH042354B2 (en)

Legal Events

Date Code Title Description
PB01 Publication
PB01 Publication
SE01 Entry into force of request for substantive examination
SE01 Entry into force of request for substantive examination
GR01 Patent grant
GR01 Patent grant