CN106007773B - A kind of vacuum brazing method of porous silicon nitride ceramic and TiAl-base alloy - Google Patents

A kind of vacuum brazing method of porous silicon nitride ceramic and TiAl-base alloy Download PDF

Info

Publication number
CN106007773B
CN106007773B CN201610347362.7A CN201610347362A CN106007773B CN 106007773 B CN106007773 B CN 106007773B CN 201610347362 A CN201610347362 A CN 201610347362A CN 106007773 B CN106007773 B CN 106007773B
Authority
CN
China
Prior art keywords
silicon nitride
powder
tial
base alloy
porous silicon
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.)
Active
Application number
CN201610347362.7A
Other languages
Chinese (zh)
Other versions
CN106007773A (en
Inventor
宋晓国
赵一璇
檀财旺
赵洪运
刘多
曹健
冯吉才
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.)
Harbin Institute of Technology Weihai
Original Assignee
Harbin Institute of Technology Weihai
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 Harbin Institute of Technology Weihai filed Critical Harbin Institute of Technology Weihai
Priority to CN201610347362.7A priority Critical patent/CN106007773B/en
Publication of CN106007773A publication Critical patent/CN106007773A/en
Application granted granted Critical
Publication of CN106007773B publication Critical patent/CN106007773B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • CCHEMISTRY; METALLURGY
    • C04CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04BLIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B37/00Joining burned ceramic articles with other burned ceramic articles or other articles by heating
    • C04B37/02Joining burned ceramic articles with other burned ceramic articles or other articles by heating with metallic articles
    • C04B37/023Joining burned ceramic articles with other burned ceramic articles or other articles by heating with metallic articles characterised by the interlayer used
    • C04B37/026Joining burned ceramic articles with other burned ceramic articles or other articles by heating with metallic articles characterised by the interlayer used consisting of metals or metal salts
    • CCHEMISTRY; METALLURGY
    • C04CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04BLIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B2237/00Aspects relating to ceramic laminates or to joining of ceramic articles with other articles by heating
    • C04B2237/02Aspects relating to interlayers, e.g. used to join ceramic articles with other articles by heating
    • C04B2237/12Metallic interlayers
    • CCHEMISTRY; METALLURGY
    • C04CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04BLIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B2237/00Aspects relating to ceramic laminates or to joining of ceramic articles with other articles by heating
    • C04B2237/02Aspects relating to interlayers, e.g. used to join ceramic articles with other articles by heating
    • C04B2237/12Metallic interlayers
    • C04B2237/122Metallic interlayers based on refractory metals
    • CCHEMISTRY; METALLURGY
    • C04CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04BLIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B2237/00Aspects relating to ceramic laminates or to joining of ceramic articles with other articles by heating
    • C04B2237/02Aspects relating to interlayers, e.g. used to join ceramic articles with other articles by heating
    • C04B2237/12Metallic interlayers
    • C04B2237/126Metallic interlayers wherein the active component for bonding is not the largest fraction of the interlayer
    • CCHEMISTRY; METALLURGY
    • C04CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04BLIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B2237/00Aspects relating to ceramic laminates or to joining of ceramic articles with other articles by heating
    • C04B2237/02Aspects relating to interlayers, e.g. used to join ceramic articles with other articles by heating
    • C04B2237/12Metallic interlayers
    • C04B2237/126Metallic interlayers wherein the active component for bonding is not the largest fraction of the interlayer
    • C04B2237/127The active component for bonding being a refractory metal
    • CCHEMISTRY; METALLURGY
    • C04CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04BLIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B2237/00Aspects relating to ceramic laminates or to joining of ceramic articles with other articles by heating
    • C04B2237/30Composition of layers of ceramic laminates or of ceramic or metallic articles to be joined by heating, e.g. Si substrates
    • C04B2237/32Ceramic
    • C04B2237/36Non-oxidic
    • C04B2237/368Silicon nitride
    • CCHEMISTRY; METALLURGY
    • C04CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04BLIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B2237/00Aspects relating to ceramic laminates or to joining of ceramic articles with other articles by heating
    • C04B2237/30Composition of layers of ceramic laminates or of ceramic or metallic articles to be joined by heating, e.g. Si substrates
    • C04B2237/40Metallic
    • CCHEMISTRY; METALLURGY
    • C04CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04BLIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B2237/00Aspects relating to ceramic laminates or to joining of ceramic articles with other articles by heating
    • C04B2237/50Processing aspects relating to ceramic laminates or to the joining of ceramic articles with other articles by heating
    • C04B2237/52Pre-treatment of the joining surfaces, e.g. cleaning, machining

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Ceramic Engineering (AREA)
  • Materials Engineering (AREA)
  • Structural Engineering (AREA)
  • Organic Chemistry (AREA)
  • Ceramic Products (AREA)

Abstract

The invention discloses the vacuum brazing methods of a kind of porous silicon nitride ceramic and TiAl-base alloy, Step 1: the nano silicon nitride silicon particle, the Ti powder that mass fraction is 2 ~ 4wt.% and AgCu powder that mass fraction is 1.5 ~ 3wt.% are carried out 4 ~ 6h of mechanical ball mill, composite soldering is mentioned;Step 2: the composite soldering after ball milling is assembled with pretreated TiAl-base alloy and porous silicon nitride base material, keep solder powder thickness between 50 ~ 200 μm;Step 3: the soldered fitting assembled is put into vacuum drying oven, it is heated to 840 DEG C ~ 900 DEG C under vacuum conditions, keep the temperature 5min ~ 30min, realize effective connection high-intensitive between porous ceramics and alloy substrate, technical solution of the present invention can effectively solve the problem that the connectivity problem of porous ceramics and TiAl-base alloy, obtain the soldered fitting of good mechanical performance.

Description

A kind of vacuum brazing method of porous silicon nitride ceramic and TiAl-base alloy
Technical field
The present invention relates to radome manufacturing technology fields, and in particular to a kind of porous silicon nitride ceramic and TiAl base close The vacuum brazing method of gold.
Background technique
It is known that porous silicon nitride ceramic because of its good wave, all has outstanding in room temperature and hot environment Mechanical performance and lower dielectric constant and the cover material for being applied to manufacture radome, and radar antenna cover It needs in application process and there is high specific strength, specific stiffness, good inoxidizability and excellent mechanical behavior under high temperature TiAl-base alloy bracket is effectively connected.However thermal expansion coefficient and Young's modulus etc. between ceramics and metal exist compared with Big difference is also easy to produce biggish residual stress during the connection process and influences the performance of jointing between base material.To understand Certainly this problem, researcher introduces the concept of composite soldering in the connection of ceramics and metal, i.e., in common metal base pricker Second Phase Particle or fiber etc. are introduced in material, it is made to produce the similar interface group with metal-based compound solder during the connection process It knits to alleviate the difference of the thermal expansion coefficient between dissimilar material base material, Young's modulus.The thinking of this composite soldering is introduced into And be applied among the present invention, to obtain effective soldering connection of porous silicon nitride ceramic and TiAl-base alloy.
Summary of the invention
It can be realized effective connection high-intensitive between porous ceramics and alloy substrate the object of the present invention is to provide a kind of, The porous silicon nitride ceramic of soldered fitting good mechanical performance and the vacuum brazing method of TiAl-base alloy.
In order to achieve the above objectives, the technical scheme adopted by the invention is that:
A kind of vacuum brazing method of porous silicon nitride ceramic and TiAl-base alloy, includes the following steps:
Step 1: nano silicon nitride silicon particle, Ti powder and AgCu powder 4 ~ 6h of mechanical ball mill are obtained into composite soldering, it is described Composite soldering in containing weight fraction be 1.5 ~ 3wt.% nano silicon nitride silicon particle, weight fraction be 2 ~ 4wt.% Ti powder, Surplus is AgCu powder;
Step 2: the composite soldering after ball milling is filled with pretreated TiAl-base alloy and porous silicon nitride base material Match, keep solder powder thickness between 50 ~ 200 μm,
Step 3: the soldered fitting assembled is put into vacuum drying oven, it is heated to 840 DEG C ~ 900 DEG C under vacuum conditions, Keep the temperature 5min ~ 30min.
The size of nano silicon nitride silicon particle described in step 1 is 20nm ~ 50nm, Ti powder and AgCu eutectic in the present invention The size of powder is 10 μm ~ 50 μm.
The porosity of porous silicon nitride base material is 45% ~ 60% in step 2 of the present invention.
Pretreated TiAl-base alloy refers to that chemical constituent is the TiAl of Ti-46Al-2Nb-2Cr in step 2 of the present invention Alloy.
Pretreated porous silicon nitride base material refers to that group is divided into 92%Si in step 2 of the present invention3N4 +6% Y2 O3 +2% Al2 O3Porous ceramics.
The surface to be welded of TiAl-base alloy and porous silicon nitride base material 200#, 400#, 800#SiC sand in step 2 of the present invention Paper is polished, and is cleaned by ultrasonic 15min ~ 20min in acetone soln.
In step 3 of the present invention, to guarantee coming into full contact between solder and base material, on the fitting side apply 0.5MPa ~ The axial compressive force of 2MPa, the more preferably axial compressive force of 1.5MPa, to improve joint quality.
Further, method for welding of the invention guarantees that vacuum degree is 10 in furnace in brazing process-2~10-4Pa, soldering rise Warm rate is 5 DEG C/min ~ 10 DEG C/min, and cooling rate is 1 DEG C/min ~ 5 DEG C/min.
In step 3 of the present invention, to guarantee coming into full contact between solder and base material, side applies 1.5MPa on the fitting Axial compressive force, guarantee that vacuum degree is 10 in furnace in brazing process-4Pa, soldering heating rate are 10 DEG C/min, cooling rate 1 ℃/min。
The present invention realizes effective connection high-intensitive between porous ceramics and alloy substrate, and the mechanical property of soldered fitting is excellent Good, the expansion for improving porous ceramics and solder bonding metal connector is extensively applied.
Detailed description of the invention
Fig. 1 is a kind of back scattering photo of jointing of the invention.
Specific embodiment
Following will be combined with the drawings in the embodiments of the present invention, and technical solution in the embodiment of the present invention carries out clear, complete Site preparation description, it is clear that described embodiments are only a part of the embodiments of the present invention, instead of all the embodiments.It is based on Embodiment in the present invention, it is obtained by those of ordinary skill in the art without making creative efforts all other Embodiment shall fall within the protection scope of the present invention.
A kind of vacuum brazing method of porous silicon nitride ceramic and TiAl-base alloy, includes the following steps:
Step 1: nano silicon nitride silicon particle, Ti powder and AgCu powder 4 ~ 6h of mechanical ball mill are obtained into composite soldering, it is described Composite soldering in containing weight fraction be 1.5 ~ 3wt.% nano silicon nitride silicon particle, weight fraction be 2 ~ 4wt.% Ti powder, Surplus is AgCu powder;
Step 2: the composite soldering after ball milling is filled with pretreated TiAl-base alloy and porous silicon nitride base material Match, keep solder powder thickness between 50 ~ 200 μm,
Step 3: the soldered fitting assembled is put into vacuum drying oven, it is heated to 840 DEG C ~ 900 DEG C under vacuum conditions, Keep the temperature 5min ~ 30min;The size of the nano silicon nitride silicon particle is 20nm ~ 50nm, the size of Ti powder and AgCu eutectic powder It is 10 μm ~ 50 μm;The porosity of porous silicon nitride base material is 45% ~ 60% in rapid two;Pretreated TiAl base closes in step 2 Gold refers to that chemical constituent is the TiAl alloy of Ti-46Al-2Nb-2Cr;Pretreated porous silicon nitride base material is in step 2 Finger group is divided into 92%Si3N4 +6% Y2 O3 +2%Al2 O3Porous ceramics;TiAl-base alloy and porous silicon nitride are female in step 2 The surface to be welded of material is polished with 200#, 400#, 800#SiC sand paper, and is cleaned by ultrasonic 15min ~ 20min in acetone soln; In step 3, to guarantee coming into full contact between solder and base material, side applies the axial pressure of 0.5MPa ~ 2MPa on the fitting Power, to improve joint quality;Guarantee that vacuum degree is 10 in furnace in brazing process-2~10-4Pa, soldering heating rate be 5 DEG C/min ~ 10 DEG C/min, cooling rate is 1 DEG C/min ~ 5 DEG C/min, in addition, in step 3 of the present invention, to guarantee between solder and base material It comes into full contact with, side applies the axial compressive force of 1.5MPa on the fitting, guarantees that vacuum degree is 10 in furnace in brazing process-4Pa, pricker Weldering heating rate is 10 DEG C/min, and cooling rate is 1 DEG C/min.
Embodiment 1:
Step 1: the porosity of porous silicon nitride be 45% ~ 60%, by mass fraction be 1.5 ~ 3wt.% having a size of 20nm ~ Nano silicon nitride silicon particle, the mass fraction of 50nm is 2 ~ 4wt.% mechanical having a size of 10 μm ~ 50 μm of Ti powder and AgCu powder progress 4 ~ 6h of ball milling.
Step 2: the surface to be welded of TiAl-base alloy and porous silicon nitride base material is carried out with 200#, 400#, 800#SiC sand paper Polishing, and it is cleaned by ultrasonic 15min ~ 20min in acetone soln.Composite soldering after ball milling is closed with pretreated TiAl base Gold and porous silicon nitride base material are assembled, and keep solder powder thickness between 50 ~ 200 μm.
Step 3: side applies the axis of 0.5MPa ~ 2MPa on the fitting to guarantee coming into full contact between solder and base material To pressure, the soldered fitting assembled is put into vacuum drying oven, in vacuum degree 10-2~10-4With heating rate for 5 under Pa environment DEG C/min ~ 10 DEG C/min is heated to 840 DEG C ~ 900 DEG C, 5min ~ 30min is kept the temperature, then with 1 DEG C/min ~ 5 DEG C/min cooling rate It is cooled to room temperature.
Embodiment 2:
The difference of the present embodiment and embodiment 1 is that the porosity of porous silicon nitride in step 1 is 50%.Other steps It is identical as specific embodiment 1.
Embodiment 3:
Difference of the present embodiment from embodiment 2 is that the mass percent of nano silicon nitride silicon particle in step 1 is The mass percent of 2wt.%, Ti powder is 2wt.%.Other steps are identical as specific embodiment 2.
Embodiment 4:
The difference of the present embodiment and embodiment 3 is in step 3 that brazing process parameter is 10 DEG C/min of heating rate, Brazing temperature be 860 DEG C, soaking time 10min, after be cooled to room temperature with 1 DEG C/min.Other steps and 3 phase of specific embodiment Together.
Embodiment 5:
The difference of the present embodiment and embodiment 3 is in step 3 that brazing process parameter is 10 DEG C/min of heating rate, Brazing temperature be 880 DEG C, soaking time 20min, after be cooled to room temperature with 3 DEG C/min.Other steps and 3 phase of specific embodiment Together.
Embodiment 6:
The difference of the present embodiment and embodiment 3 is in step 3 that brazing process parameter is 5 DEG C/min of heating rate, pricker Weld temperature be 900 DEG C, soaking time 10min, after be cooled to room temperature with 5 DEG C/min.Other steps and 3 phase of specific embodiment Together.
Embodiment 7:
The difference of the present embodiment and embodiment 2 be solder powder in step 2 with a thickness of 100 μm.Other steps and tool Body embodiment 2 is identical.
Embodiment 8:
The difference of the present embodiment and embodiment 2 is in step 3, to guarantee coming into full contact between solder and base material, Side applies the axial compressive force of 1.5MPa on the fitting, guarantees that vacuum degree is 10 in furnace in brazing process-4Pa is brazed heating rate For 10 DEG C/min, cooling rate is 1 DEG C/min.
It is provided for the embodiments of the invention the vacuum brazing side of a kind of porous silicon nitride ceramic and TiAl-base alloy above Method is described in detail, and used herein a specific example illustrates the principle and implementation of the invention, above The explanation of embodiment is merely used to help understand method and its core concept of the invention;Meanwhile for the general skill of this field Art personnel, according to the thought of the present invention, there will be changes in the specific implementation manner and application range, in conclusion this Description should not be construed as limiting the invention.

Claims (1)

1. the vacuum brazing method of a kind of porous silicon nitride ceramic and TiAl-base alloy, it is characterised in that the following steps are included:
Step 1: nano silicon nitride silicon particle, Ti powder and AgCu powder 4 ~ 6h of mechanical ball mill are obtained into composite soldering, it is described The nano silicon nitride silicon particle for being 1.5 ~ 3wt.% containing weight fraction in composite soldering, weight fraction are the Ti of 2 ~ 4wt.% Powder, surplus are AgCu powder, and the partial size of the nano silicon nitride silicon particle is 20nm ~ 50nm, Ti powder and AgCu eutectic powder Partial size be 10 μm ~ 50 μm;
Step 2: the composite soldering after ball milling is assembled with pretreated TiAl-base alloy and porous silicon nitride base material, Guarantee that solder powder thickness carries out polishing surface to be welded with 200#, 400#, 800#SiC sand paper between 50 ~ 200 μm, and in acetone It is cleaned by ultrasonic 15min ~ 20min in solution, the pretreated TiAl-base alloy refers to that chemical constituent is Ti-46Al- The TiAl alloy of 2Nb-2Cr, the porous silicon nitride base material refer to that group is divided into 92%Si3N4+6% Y2O3+2%Al2O3Porous pottery Porcelain, the porosity of porous silicon nitride base material are 45% ~ 60%;
Step 3: the soldered fitting assembled is put into vacuum drying oven, it is heated to 840 DEG C ~ 900 DEG C under vacuum conditions, protects Warm 5min ~ 30min guarantees that vacuum degree is 1 × 10 in furnace in brazing process-2~ 1×10-4Pa, soldering heating rate are 5 DEG C/min ~ 10 DEG C/min, cooling rate is 1 DEG C/min ~ 5 DEG C/min, wherein applies the axial pressure of 1.5MPa above assembly parts Power guarantees coming into full contact between solder and base material.
CN201610347362.7A 2016-05-24 2016-05-24 A kind of vacuum brazing method of porous silicon nitride ceramic and TiAl-base alloy Active CN106007773B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201610347362.7A CN106007773B (en) 2016-05-24 2016-05-24 A kind of vacuum brazing method of porous silicon nitride ceramic and TiAl-base alloy

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201610347362.7A CN106007773B (en) 2016-05-24 2016-05-24 A kind of vacuum brazing method of porous silicon nitride ceramic and TiAl-base alloy

Publications (2)

Publication Number Publication Date
CN106007773A CN106007773A (en) 2016-10-12
CN106007773B true CN106007773B (en) 2019-06-07

Family

ID=57093050

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201610347362.7A Active CN106007773B (en) 2016-05-24 2016-05-24 A kind of vacuum brazing method of porous silicon nitride ceramic and TiAl-base alloy

Country Status (1)

Country Link
CN (1) CN106007773B (en)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108516871B (en) * 2018-04-23 2020-12-22 哈尔滨工业大学(威海) Surface metallization method of porous silicon nitride ceramic
CN108555476B (en) * 2018-04-25 2020-02-07 哈尔滨工业大学 Composite brazing filler metal for brazing quartz fiber reinforced composite ceramic and Invar alloy and preparation method and brazing method thereof
CN108856943B (en) * 2018-06-27 2021-01-01 衢州学院 Brazing method of TiAl and silicon nitride
CN111747769B (en) * 2020-06-30 2022-12-09 哈尔滨工业大学(威海) AlMgB 14 -TiB 2 Vacuum brazing method for composite ceramic and TiAl-based alloy

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102699572A (en) * 2012-06-21 2012-10-03 哈尔滨工业大学 Nano particle reinforced Ag-base composite brazing filler metal and preparation method thereof
CN103204694A (en) * 2013-04-03 2013-07-17 哈尔滨工业大学 Method for diffusely connecting TiAl-based alloy and Ti3AlC2 ceramic by adopting Zr/Ni composite intermediate layer
CN103240540A (en) * 2013-05-22 2013-08-14 哈尔滨工业大学 Brazing filler metal for connecting SiO2 ceramic and SiO2 ceramic matrix composite materials and preparing method thereof
CN104690386A (en) * 2015-03-25 2015-06-10 哈尔滨工业大学(威海) Method for connecting Cf/LAS composite material via AgCuTi brazing filler metal

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102699572A (en) * 2012-06-21 2012-10-03 哈尔滨工业大学 Nano particle reinforced Ag-base composite brazing filler metal and preparation method thereof
CN103204694A (en) * 2013-04-03 2013-07-17 哈尔滨工业大学 Method for diffusely connecting TiAl-based alloy and Ti3AlC2 ceramic by adopting Zr/Ni composite intermediate layer
CN103240540A (en) * 2013-05-22 2013-08-14 哈尔滨工业大学 Brazing filler metal for connecting SiO2 ceramic and SiO2 ceramic matrix composite materials and preparing method thereof
CN104690386A (en) * 2015-03-25 2015-06-10 哈尔滨工业大学(威海) Method for connecting Cf/LAS composite material via AgCuTi brazing filler metal

Also Published As

Publication number Publication date
CN106007773A (en) 2016-10-12

Similar Documents

Publication Publication Date Title
CN106007773B (en) A kind of vacuum brazing method of porous silicon nitride ceramic and TiAl-base alloy
CN101494322B (en) Tungsten copper connection method
CN108672965A (en) A method of alleviating ceramics and solder bonding metal connector residual stress
CN107649758B (en) A method of porous silicon nitride ceramic and invar alloy are brazed using composite soldering
CN105643038B (en) Brazed porous Si3N4The method of ceramics and Invar alloys
CN103341675B (en) Method for braze welding of Cf/SiC composite material and metal Nb by using Ti-Co-Nb brazing filler metal
CN102513636B (en) Brazing method capable of reducing residual stress on ceramic and metal joints
WO2003047859A1 (en) Ceramic joining
JPH0339993B2 (en)
CN108516871B (en) Surface metallization method of porous silicon nitride ceramic
CN106944695A (en) A kind of method for welding of porous ceramics and metal
CN105418131A (en) Alumina ceramic low temperature brazing connection method
CN108620767B (en) Preparation method of composite solder for brazing quartz short fiber reinforced silicon dioxide composite material and Invar alloy
CN106588064B (en) The solder and connection method of carbon/carbon compound material and nickel base superalloy
CN104711457B (en) High temperature solder and application thereof
CN105728981A (en) Brazing filler metal for welding Si3N4 ceramic-stainless steel and brazing method thereof
CN104496511B (en) A kind of online reaction forming method of ceramic form
JP2012091975A (en) Method for manufacturing joined body of ceramic material and metallic material
CN104741722A (en) TiNi solder vacuum brazing TZM alloy and ZrC/W composite method
CN113070543B (en) Method for brazing carbon material and nickel-based alloy by adopting Ag-Cr composite brazing filler metal
KR101411954B1 (en) Heterostructure for heating and method of fabricating the same
CN108555476B (en) Composite brazing filler metal for brazing quartz fiber reinforced composite ceramic and Invar alloy and preparation method and brazing method thereof
CN106242606B (en) A method of utilizing Zr-Ni base solder brazing ZrB2-SiC composite ceramics
CN105174988A (en) Method for connecting ceramic by adopting porous ceramic middle layer
CN105081503A (en) Soldering method for achieving connection of SiC-based composite ceramic and Invar alloy by means of NiCrSi

Legal Events

Date Code Title Description
C06 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