CN107354331B - The method for controlling TiAl-base alloy oriented freezing organization lamellar orientation as substrate seed crystal using refractory metal - Google Patents
The method for controlling TiAl-base alloy oriented freezing organization lamellar orientation as substrate seed crystal using refractory metal Download PDFInfo
- Publication number
- CN107354331B CN107354331B CN201710575889.XA CN201710575889A CN107354331B CN 107354331 B CN107354331 B CN 107354331B CN 201710575889 A CN201710575889 A CN 201710575889A CN 107354331 B CN107354331 B CN 107354331B
- Authority
- CN
- China
- Prior art keywords
- tial
- refractory metal
- directional solidification
- seed crystal
- base alloy
- 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.)
- Expired - Fee Related
Links
Classifications
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C1/00—Making non-ferrous alloys
- C22C1/02—Making non-ferrous alloys by melting
- C22C1/03—Making non-ferrous alloys by melting using master alloys
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22D—CASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
- B22D27/00—Treating the metal in the mould while it is molten or ductile ; Pressure or vacuum casting
- B22D27/04—Influencing the temperature of the metal, e.g. by heating or cooling the mould
- B22D27/045—Directionally solidified castings
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C14/00—Alloys based on titanium
Abstract
The method for controlling TiAl-base alloy oriented freezing organization lamellar orientation as substrate seed crystal using refractory metal, it is related to a kind of TiAl-base alloy directional freeze method, and in particular to a kind of method for being oriented solidification control TiAl-base alloy oriented freezing organization lamellar orientation as substrate seed crystal material using refractory metal.The present invention is to solve the problems, such as that Composition Transient is longer in conventional seed-grain method directional solidification process.This method: one, foundry alloy melting;Two, refractory metal and directional solidification bar connect;Three, start directional solidification.The present invention is compared with traditional seed-grain method, and when doing substrate seed crystal material directional solidification using refractory metal, this method has many advantages, such as shorter Composition Transient, the technique of simplification and higher growth stability.The invention belongs to TiAl-base alloy directional solidification fields.
Description
Technical field
It is related to that the present invention relates to a kind of TiAl-base alloy directional freeze methods, and in particular to make using a kind of refractory metal
The method for being oriented solidification control TiAl-base alloy oriented freezing organization lamellar orientation for substrate seed crystal material.
Background technique
TiAl-base alloy is a kind of high temperature structural material in the great application prospect of aerospace field, uses temperature
Range is between 650 DEG C~1000 DEG C.The room temperature texture of TiAl-base alloy is usually by γ phase (TiAl) and α2Phase (Ti3Al it) constitutes,
Studies have shown that complete lamellar structure (α2+ γ) there is optimal comprehensive mechanical property.But the lamella of full sheet layer TiAl-base alloy
Orientation has apparent anisotropy, and when lamellar orientation is consistent with alloy Impact direction, full sheet layer TiAl alloy can express
Optimal strong plasticity.
Research heat both at home and abroad is had become using the lamellar orientation in directional solidification technique control TiAl alloy based alloy at present
Point, still, since TiAl alloy itself is used as a kind of intermetallic compound, the complexity of process of setting results in directional solidification
Its lamellar structure is controlled with very big difficulty.Its meeting after undergoing the solid-solid phase change process after a series of complex liquid-solid-phase changeable
Form γ/α2Lamellar structure, in liquid/solid phase transition process, different primary phases leads to subsequent solidification path and final lamellar orientation
Difference, people will use directional solidification technique control using solidification path different corresponding to two different primary phases as boundary's point
Lamellar orientation processed is divided into two methods, i.e. control solidification path method and seed-grain method.
It is leading phase that seed-grain method directional solidification TiAl alloy, which is to control α phase, and satisfactory seed crystal is placed on fusing
The bottom of alloy grows directional solidificating alloy on the basis of seed crystal, so that α phase is formed under the adductive crystallization of bottom seed crystal
The lamellar structure parallel with the direction of growth.But in seed-grain method directional solidification process, seed crystal alloy and directional solidificating alloy
Ingredient is often different, most common seed crystal alloy Ti-43Al-3Si alloy, the seed crystal alloy and current excellent combination property
And the TiAl-base alloy component difference with prospect of the application is larger, such as Ti-48Al-2Cr-2Nb, Ti-48Al-5Nb.Therefore,
In seed-grain method directional solidification process, often there is longer Composition Transient between seed crystal alloy and directional solidificating alloy.?
In directional solidification process, Composition Transient is often also the critical stage of microstructure transformation, and longer Composition Transient may
The fringe time of microstructure heredity can be made to elongate, reduce the stability of lamellar orientation.
Summary of the invention
The purpose of the present invention is to solve the longer problem in Composition Transient in conventional seed-grain method directional solidification process,
Provide a kind of method that TiAl-base alloy oriented freezing organization lamellar orientation is controlled as substrate seed crystal using refractory metal.
Using refractory metal as substrate seed crystal control TiAl-base alloy oriented freezing organization lamellar orientation method according to
Lower step carries out:
One, foundry alloy melting: melting is carried out to TiAl-base alloy using vacuum induction water jacketed copper crucible, and pours and casts out female conjunction
Ingot;
Two, refractory metal and directional solidification bar connect: being cut from mother alloy ingot using spark cutting method
The refractory metal of same diameter and cylindrical rod material reason are bonded to together, are put into ceramic tube by cylinder bar, then will pottery
Porcelain tube is incorporated in the Bridgman directional solidification furnace of high-purity argon gas protection, and the linkage interface of refractory metal and cylinder bar
Lower than the freezing interface of directional solidification starting;
Three, start directional solidification: starting Bridgman directional solidification furnace is heated to 1500 DEG C~1800 DEG C and carries out hot steady
Fixedization handle 15 minutes~30 minutes, start directional solidification drawing device, directional solidification growth rate be 10 μm/s~50 μm/
S, it is oriented solidification under 10 DEG C/mm~30 DEG C/mm temperature gradient, until rapid quenching is carried out when directional solidification 40mm, when fixed
When being reduced to 200 DEG C or less to solidification room temperature, directional solidification room is opened, directional solidificating alloy ingot casting is obtained.
TiAl-base alloy described in step 1 is by atomic percentage content by 47% Al, 1.0% W, 0.5% Si and remaining
The Ti of amount is formed;Or the TiAl-base alloy is made of by atomic percentage content 47% Al and the Ti of surplus.
Refractory metal described in step 2 is Ti or Nb.
The diameter of cylinder bar described in step 2 is 6mm.
" Bridgman device for directionally solidifying " of the present invention comes from Liu Tong, Luo Liangshun, Su Yanqing et al. in 2016,31
(5): 618-626 is published in entitled " the Effect of growth rate of Journal of Material Research
on microstructures and microhardness in directionally solidified Ti–47Al–
1.0W–0.5Si alloy》。
The present invention is substituted using high-melting-point pure metal Ti, Nb as substrate seed crystal in seed-grain method directional solidification process
Conventional seed crystal alloy, since the temperature of directional solidification heating is 1600 DEG C, and the fusing point of pure Ti is 1680 DEG C, and the fusing point of Nb is
2468 DEG C, therefore the heating temperature of directional solidification can not be by high-melting-point pure metal seed crystal alloy melting, and directional solidificating alloy
Start to orient in high-melting-point pure metal seed crystal alloy interface forward position after starting directional solidification pull system for molten condition
Growth, so that Composition Transient be not present between seed crystal alloy and directional solidificating alloy, and Ti, Nb be as strong β phase stable element,
Alloy can be made to come into being leading phase β phase in directional solidification simultaneously, to achieve the purpose that controlling alloy sheet interlayer is orientated.
The present invention uses high-melting-point pure metal Ti and Nb as seed crystal base material, using common Bridgman directional solidification
System controls TiAl-base alloy oriented freezing organization lamellar orientation, eliminates original as substrate seed crystal by using refractory metal
Beginning as cast condition area's microstructure to starting interface microstructure adverse effect, while ensure alloy leading phase be β phase, to reach
Control the purpose of alloy sheet interlayer orientation.
It is binary Ti-47Al (at.%) by directional solidification TiAl alloy ingredient prepared by refractory metal seed crystal material
With polynary Ti-47Al-1.0W-0.5Si (at.%) alloy.The present invention is done compared with traditional seed-grain method using refractory metal
When substrate seed crystal material directional solidification, this method has shorter Composition Transient, the technique of simplification and higher growth steady
The advantages that qualitative.
Detailed description of the invention
Fig. 1 is using high-melting-point pure metal Ti in embodiment 1 as substrate seed crystal material directional solidification Ti-47Al-1.0W-
0.5Si alloy seeding interface micro-organization chart;
Fig. 2 is using high-melting-point pure metal Ti in embodiment 1 as substrate seed crystal material directional solidification Ti-47Al-1.0W-
0.5Si alloy seeding interface seeding Interface composition line scanning figure, a indicates that Al, b indicate that Si, c indicate that W, d indicate Ti in figure;
Fig. 3 is using high-melting-point pure metal Ti in embodiment 1 as substrate seed crystal material directional solidification Ti-47Al-1.0W-
Micro-organization chart of 0.5Si alloy steady-state growth area;
Fig. 4 is using high-melting-point pure metal Nb in embodiment 2 as substrate seed crystal material directional solidification Ti-47Al-1.0W-
0.5Si alloy seeding interface micro-organization chart;
Fig. 5 is using high-melting-point pure metal Nb in embodiment 2 as substrate seed crystal material directional solidification Ti-47Al-1.0W-
0.5Si alloy seeding interface seeding Interface composition line scanning figure, a indicates that Ti, b indicate that Al, c indicate that W, d indicate Si, e in figure
Indicate Nb;
Fig. 6 is using high-melting-point pure metal Nb in embodiment 2 as substrate seed crystal material directional solidification Ti-47Al-1.0W-
Micro-organization chart of 0.5Si alloy steady-state growth area;
Fig. 7 is drawn using high-melting-point pure metal Ti as substrate seed crystal material directional solidification Ti-47Al alloy in embodiment 3
Brilliant interface micro-organization chart;
Fig. 8 is drawn using high-melting-point pure metal Ti as substrate seed crystal material directional solidification Ti-47Al alloy in embodiment 3
Brilliant interface seeding Interface composition line scanning figure;
Fig. 9 is steady as substrate seed crystal material directional solidification Ti-47Al alloy using high-melting-point pure metal Ti in embodiment 3
State vitellarium micro-organization chart;
Figure 10 is using high-melting-point pure metal Nb in embodiment 4 as substrate seed crystal material directional solidification Ti-47Al alloy
Seeding interface micro-organization chart;
Figure 11 is using high-melting-point pure metal Nb in embodiment 4 as substrate seed crystal material directional solidification Ti-47Al alloy
Seeding interface seeding Interface composition line scanning figure;
Figure 12 is using high-melting-point pure metal Nb in embodiment 4 as substrate seed crystal material directional solidification Ti-47Al alloy
Micro-organization chart of steady-state growth area.
Specific embodiment
The technical solution of the present invention is not limited to the following list, further includes between each specific embodiment
Any combination.
Specific embodiment 1: present embodiment controls TiAl-base alloy directional solidification by substrate seed crystal of refractory metal
The method of tissue lamellar orientation follows the steps below:
One, foundry alloy melting: melting is carried out to TiAl-base alloy using vacuum induction water jacketed copper crucible, and pours and casts out female conjunction
Ingot;
Two, refractory metal and directional solidification bar connect: being cut from mother alloy ingot using spark cutting method
The refractory metal of same diameter and cylindrical rod material reason are bonded to together, are put into ceramic tube by cylinder bar, then will pottery
Porcelain tube is incorporated in the Bridgman directional solidification furnace of high-purity argon gas protection, and the linkage interface of refractory metal and cylinder bar
Lower than the freezing interface of directional solidification starting;
Three, start directional solidification: starting Bridgman directional solidification furnace is heated to 1500 DEG C~1800 DEG C and carries out hot steady
Fixedization handle 15 minutes~30 minutes, start directional solidification drawing device, directional solidification growth rate be 10 μm/s~50 μm/
S, it is oriented solidification under 10 DEG C/mm~30 DEG C/mm temperature gradient, until rapid quenching is carried out when directional solidification 40mm, when fixed
When being reduced to 200 DEG C or less to solidification room temperature, directional solidification room is opened, directional solidificating alloy ingot casting is obtained.
Specific embodiment 2: the present embodiment is different from the first embodiment in that TiAl base described in step 1 is closed
Gold by atomic percentage content by 47% Al, 1.0%~W, 0.5% Si and the Ti of surplus form;Or the TiAl base
Alloy is made of by atomic percentage content 47% Al and the Ti of surplus.It is other same as the specific embodiment one.
Specific embodiment 3: unlike one of present embodiment and specific embodiment one or two described in step 2
Refractory metal be Ti or Nb.It is other identical as one of specific embodiment one or two.
Specific embodiment 4: unlike one of present embodiment and specific embodiment one to three described in step 2
The diameter of cylinder bar is 6mm.It is other identical as one of specific embodiment one to three.
Specific embodiment 5: being heated in step 3 unlike one of present embodiment and specific embodiment one to four
To 1700 DEG C and carry out thermostabilization processing 18 minutes~25 minutes.It is other identical as one of specific embodiment one to four.
Specific embodiment 6: being heated in step 3 unlike one of present embodiment and specific embodiment one to five
To 1600 DEG C and carry out thermostabilization processing 20 minutes.It is other identical as one of specific embodiment one to five.
Specific embodiment 7: pull in step 3 unlike one of present embodiment and specific embodiment one to six
Rate is 40 μm/s.It is other identical as one of specific embodiment one to six.
Specific embodiment 8: pull in step 3 unlike one of present embodiment and specific embodiment one to seven
Rate is 30um/s.It is other identical as one of specific embodiment one to seven.
Specific embodiment 9: unlike one of present embodiment and specific embodiment one to eight 15 in step 3
DEG C/mm~25 DEG C/mm temperature gradient under be oriented solidification.It is other identical as one of specific embodiment one to eight.1
Specific embodiment 10: unlike one of present embodiment and specific embodiment one to nine 20 in step 3
DEG C/temperature gradient of mm under be oriented solidification.It is other identical as one of specific embodiment one to nine.
Using following experimental verifications effect of the present invention:
Embodiment 1:
The present embodiment is using high-melting-point pure metal Ti as seed crystal base material directional solidification Ti-47Al-1.0W-0.5Si
Alloy is realized by following step:
One, by the Ti-47Al-1.0W-0.5Si alloy cast ingot of the Φ 6mm × 100mm cut from master alloy and Φ 6mm ×
The pure Ti bar physical adhesion of 20mm has then been put into Y to together2O3The Al of coating2O3In ceramic tube, it is connected to directional solidification
System pumping rod;
Two, start directional solidification vacuum system, vacuumize, and be passed through high-purity argon gas, then start heating device, be heated to
Temperature at directional solidification startup interface is 1600 DEG C, then carries out the thermostabilization processing of 30min, guarantees directional solidificating alloy
The stability of melt;
Three, start directional solidification drawing device, directional solidification growth rate control is 10 μm/s;
Four, when pull is to 40mm, rapid quenching, solid/liquid interfaces when can retain alloy oriented growth are carried out;
Five, directional solidification heating system is closed, when directional solidification room temperature is reduced to 200 DEG C or less, opens orientation
Room is solidified, directional solidificating alloy ingot casting is obtained;
It is longitudinally slit along directional solidification ingot casting using Electric Discharge Wire-cutting Technology, it is obtained by standard metallographic preparation method of sample
Take the macro microstructure in directional solidification ingot casting seed crystal seeding interface, it can be seen that obtain and grow in front of seed crystal seeding interface
The parallel lamellar structure in direction is shown in Fig. 1, and show that alloying component transition region is only 1.2mm by component lines scanning, sees Fig. 2, and
And the lamellar structure parallel with the direction of growth grows to always the steady-state growth stage of directional solidificating alloy, sees Fig. 3.
Embodiment 2:
The present embodiment is using high-melting-point pure metal Nb as seed crystal base material directional solidification Ti-47Al-1.0W-0.5Si
Alloy is realized by following step:
One, by the Ti-47Al-1.0W-0.5Si alloy cast ingot of the Φ 6mm × 100mm cut from master alloy and Φ 6mm ×
The pure Ti bar physical adhesion of 20mm has then been put into Y to together2O3The Al of coating2O3In ceramic tube, it is connected to directional solidification
System pumping rod;
Two, start directional solidification vacuum system, vacuumize, and be passed through high-purity argon gas, then start heating device, be heated to
Temperature at directional solidification startup interface is 1600 DEG C, then carries out the thermostabilization processing of 15min, guarantees directional solidificating alloy
The stability of melt;
Three, start directional solidification drawing device, directional solidification growth rate control is 30 μm/s;
Four, when pull is to 40mm, rapid quenching is carried out, solid/liquid interfaces when retaining alloy oriented growth;
Five, directional solidification heating system is closed, when directional solidification room temperature is reduced to 200 DEG C or less, opens orientation
Room is solidified, directional solidificating alloy ingot casting is obtained;
It is longitudinally slit along directional solidification ingot casting using Electric Discharge Wire-cutting Technology, it is obtained by standard metallographic preparation method of sample
Directional solidification ingot casting seed crystal seeding interface macrostructure is taken, it can be seen that about five columns are obtained in front of seed crystal interface
Crystalline substance, lamellar structure and the direction of growth are shown in Fig. 4 close to parallel in each column crystal.And by component lines scanning obtain alloy at
Point transition region is only 0.6mm, sees Fig. 5.And lamellar structure of the directional solidificating alloy in the steady-state growth stage also inherits seeding circle
Microstructure at face, is shown in Fig. 6.
Embodiment 3:
The present embodiment is passed through using high-melting-point pure metal Ti as seed crystal base material directional solidification Ti-47Al alloy following
Step is realized:
One, by the Ti-47Al-1.0W-0.5Si alloy cast ingot of the Φ 6mm × 100mm cut from master alloy and Φ 6mm ×
The pure Ti bar of 20mm docks, and has then been put into Y2O3The Al of coating2O3In ceramic tube, it is connected to directional solidification system pumping rod;
Two, start directional solidification vacuum system, vacuumize, and be passed through high-purity argon gas, then start heating device, be heated to
Temperature at directional solidification startup interface is 1600 DEG C, then carries out the thermostabilization processing of 15min, guarantees directional solidificating alloy
The stability of melt;
Three, start directional solidification drawing device, directional solidification growth rate control is 30 μm/s;
Four, when pull is to 40mm, rapid quenching is carried out, solid/liquid interfaces when retaining alloy oriented growth;
Five, directional solidification heating system is closed, when directional solidification room temperature is reduced to 200 DEG C or less, opens orientation
Room is solidified, directional solidificating alloy ingot casting is obtained;
It is longitudinally slit along directional solidification ingot casting using Electric Discharge Wire-cutting Technology, it is obtained by standard metallographic preparation method of sample
Directional solidification ingot casting seed crystal seeding interface macrostructure has been taken, has been obtained in front of seed crystal seeding interface close with the direction of growth
Parallel lamellar structure, is shown in Fig. 7, and show that alloying component transition region is only 1.0mm by component lines scanning, sees Fig. 8, and with
The parallel lamellar orientation of the direction of growth grows to always the steady-state growth stage, sees Fig. 9.
Embodiment 4:
The present embodiment is passed through using high-melting-point pure metal Nb as seed crystal base material directional solidification Ti-47Al alloy following
Step is realized:
One, by the Ti-47Al-1.0W-0.5Si alloy cast ingot of the Φ 6mm × 100mm cut from master alloy and Φ 6mm ×
The pure Ti bar of 20mm docks, and has then been put into Y2O3The Al of coating2O3In ceramic tube, it is connected to directional solidification system pumping rod;
Two, start directional solidification vacuum system, vacuumize, and be passed through high-purity argon gas, then start heating device, be heated to
Temperature at directional solidification startup interface is 1600 DEG C, then carries out the thermostabilization processing of 15min, guarantees directional solidificating alloy
The stability of melt;
Three, start directional solidification drawing device, directional solidification growth rate control is 50 μm/s;
Four, when pull is to 40mm, rapid quenching is carried out, solid/liquid interfaces when retaining alloy oriented growth;
Five, directional solidification heating system is closed, when directional solidification room temperature is reduced to 200 DEG C or less, opens orientation
Room is solidified, directional solidificating alloy ingot casting is obtained;
It is longitudinally slit along directional solidification ingot casting using Electric Discharge Wire-cutting Technology, it is obtained by standard metallographic preparation method of sample
The macro microstructure in directional solidification ingot casting seed crystal seeding interface has been taken, has obtained in front of seed crystal seeding interface and is connect with the direction of growth
Subparallel lamellar structure, is shown in Figure 10.And show that alloying component transition region is only 0.6mm by component lines scanning, see Figure 11.And
And the lamellar orientation parallel with the direction of growth grows to always the steady-state growth stage, sees Figure 12.
Claims (8)
1. in the method that refractory metal controls TiAl-base alloy oriented freezing organization lamellar orientation as substrate seed crystal, feature exists
In using refractory metal as substrate seed crystal control TiAl-base alloy oriented freezing organization lamellar orientation method according to the following steps
It carries out:
One, foundry alloy melting: melting is carried out to TiAl-base alloy using vacuum induction water jacketed copper crucible, and pours and casts out master alloy
Ingot;
Two, refractory metal and directional solidification bar connect: cylinder is cut from mother alloy ingot using spark cutting method
The refractory metal of same diameter and cylindrical rod material reason are bonded to together, are put into ceramic tube, then by ceramic tube by bar
It is incorporated in the Bridgman directional solidification furnace of high-purity argon gas protection, and the linkage interface of refractory metal and cylinder bar is lower than
The freezing interface of directional solidification starting;
Three, start directional solidification: starting Bridgman directional solidification furnace is heated to 1500 DEG C~1800 DEG C and carries out thermostabilization
Processing 15 minutes~30 minutes starts directional solidification drawing device, is 10 μm/s~50 μm/s, 10 in directional solidification growth rate
DEG C/mm~30 DEG C/mm temperature gradient under be oriented solidification, until when directional solidification 40mm, rapid quenching is carried out, when orientation is solidifying
Gu room temperature is reduced to 200 DEG C or less, directional solidification room is opened, directional solidificating alloy ingot casting is obtained;
Refractory metal described in step 2 is Nb;TiAl-base alloy described in step 1 is by atomic percentage content by 47%
The Ti composition of Al, 1.0% W, 0.5% Si and surplus;Or the TiAl-base alloy presses atomic percentage content by 47%
The Al and Ti of surplus composition.
2. controlling TiAl-base alloy oriented freezing organization lamella as substrate seed crystal using refractory metal according to claim 1 to take
To method, it is characterised in that the diameter of cylinder bar described in step 2 be 6mm.
3. controlling TiAl-base alloy oriented freezing organization lamella as substrate seed crystal using refractory metal according to claim 1 to take
To method, it is characterised in that be heated in step 3 1700 DEG C and carry out thermostabilization handle 18 minutes~25 minutes.
4. controlling TiAl-base alloy oriented freezing organization lamella as substrate seed crystal using refractory metal according to claim 1 to take
To method, it is characterised in that be heated in step 3 1600 DEG C and carry out thermostabilization handle 20 minutes.
5. controlling TiAl-base alloy oriented freezing organization lamella as substrate seed crystal using refractory metal according to claim 1 to take
To method, it is characterised in that in step 3 withdrawing rate be 40 μm/s.
6. controlling TiAl-base alloy oriented freezing organization lamella as substrate seed crystal using refractory metal according to claim 1 to take
To method, it is characterised in that in step 3 withdrawing rate be 30um/s.
7. controlling TiAl-base alloy oriented freezing organization lamella as substrate seed crystal using refractory metal according to claim 1 to take
To method, it is characterised in that be oriented solidification under 15 DEG C/mm~25 DEG C/mm temperature gradient in step 3.
8. controlling TiAl-base alloy oriented freezing organization lamella as substrate seed crystal using refractory metal according to claim 1 to take
To method, it is characterised in that solidification is oriented in step 3 under the temperature gradient of 20 DEG C/mm.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201710575889.XA CN107354331B (en) | 2017-07-14 | 2017-07-14 | The method for controlling TiAl-base alloy oriented freezing organization lamellar orientation as substrate seed crystal using refractory metal |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201710575889.XA CN107354331B (en) | 2017-07-14 | 2017-07-14 | The method for controlling TiAl-base alloy oriented freezing organization lamellar orientation as substrate seed crystal using refractory metal |
Publications (2)
Publication Number | Publication Date |
---|---|
CN107354331A CN107354331A (en) | 2017-11-17 |
CN107354331B true CN107354331B (en) | 2019-01-08 |
Family
ID=60292611
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201710575889.XA Expired - Fee Related CN107354331B (en) | 2017-07-14 | 2017-07-14 | The method for controlling TiAl-base alloy oriented freezing organization lamellar orientation as substrate seed crystal using refractory metal |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN107354331B (en) |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN112916831B (en) * | 2021-01-25 | 2022-07-26 | 中国科学院金属研究所 | Preparation method of gamma-TiAl alloy with lamellar interface preferred orientation and fine lamellar characteristics |
Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN1570224A (en) * | 2003-07-16 | 2005-01-26 | 中国科学院金属研究所 | Method for suppressing stray crystal forming and growing at seed crystal starting end, and casting case construction thereof |
CN103789598A (en) * | 2014-02-28 | 2014-05-14 | 南京理工大学 | Directional TiAl-based alloy and preparation method thereof |
CN104651650A (en) * | 2015-02-02 | 2015-05-27 | 西北工业大学 | Method for preparing TiAl-base alloy directional fully lamellar structure |
-
2017
- 2017-07-14 CN CN201710575889.XA patent/CN107354331B/en not_active Expired - Fee Related
Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN1570224A (en) * | 2003-07-16 | 2005-01-26 | 中国科学院金属研究所 | Method for suppressing stray crystal forming and growing at seed crystal starting end, and casting case construction thereof |
CN103789598A (en) * | 2014-02-28 | 2014-05-14 | 南京理工大学 | Directional TiAl-based alloy and preparation method thereof |
CN104651650A (en) * | 2015-02-02 | 2015-05-27 | 西北工业大学 | Method for preparing TiAl-base alloy directional fully lamellar structure |
Non-Patent Citations (3)
Title |
---|
Lamellar orientation control of Ti-47Al-0.5W-0.5Si by directional solidification using b seeding technique;Tong Liu et al.;《Intermetallics》;20160227;第73卷;第1-2页引言1第3段,实验2 * |
Lamellar orientation control of Ti-47Al-0.5W-0.5Si by directional solidification using b seeding technique;Tong Liu et al.;《Intermetallics》;20160227;第73卷;第1-2页引言1第3段,实验2,第3页右栏第1段 * |
铸态Ti-47Al(W,Si)合金组织演化及力学性能研究;刘桐等;《特种铸造及有色合金》;20161031;第36卷(第10期);摘要,第1024页左栏第1段 * |
Also Published As
Publication number | Publication date |
---|---|
CN107354331A (en) | 2017-11-17 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CN102011195B (en) | Preparation method of directional solidification high-Nb TiAl alloy single crystal | |
CN103789598B (en) | A kind of directed TiAl-base alloy and preparation method thereof | |
CN109396400B (en) | Large complex thin-wall fine-grain casting integrated forming method and device | |
CN104278173B (en) | A kind of high-strength high-ductility TiAl alloy material and preparation method thereof | |
CN104328501B (en) | Fully controllable TiAl single crystal alloys of a kind of lamellar orientation and preparation method thereof | |
CN103122431A (en) | Magnesium-lithium alloy with enhanced long-period structure phase and preparation method thereof | |
CN103817313B (en) | A kind of preparation method of integral fine crystal radial impeller foundry goods | |
JPH05200529A (en) | Directional coagulation casting of aluminum titanium | |
CN107236913B (en) | A kind of zirconium-base amorphous alloy and preparation method thereof | |
Zheng et al. | The interdendritic-melt solidification control (IMSC) and its effects on the porosity and phase change of a Ni-based superalloy | |
CN107354331B (en) | The method for controlling TiAl-base alloy oriented freezing organization lamellar orientation as substrate seed crystal using refractory metal | |
Cui et al. | Microstructure evolution and corrosion behavior of directionally solidified FeCoNiCrCu high entropy alloy | |
CN108555297B (en) | Method for eliminating primary β grain boundary of TC4 alloy by adding B induction heating during laser additive manufacturing | |
CN105543618B (en) | It is a kind of to reduce directionally solidifying titanium aluminum alloy casting and the optimize technique of casting mold coating reaction | |
Li et al. | Directional solidification of Ti-46Al-8Nb alloy in BaZrO3 coated Al2O3 composite mould | |
CN104264082B (en) | A kind of nitrogen-doping Strengthening and Toughening metal glass composite material and preparation method thereof | |
CN103451577B (en) | Magnesium base amorphous alloy situ composite material of quasicrystal particle strengthening and preparation method thereof | |
CN101942618B (en) | Magnesium-based block metal glass composite material and preparation method thereof | |
CN103060660B (en) | Method for preparing Fe-Ga-In-Tb alloy by double-feeding vacuum induction smelting | |
CN105088329B (en) | A kind of preparation method of the quasi- seed crystal of TiAl alloy | |
CN104878328A (en) | Structure-controllable TiZr-based amorphous composite material and preparation method thereof | |
CN101824570B (en) | AZ series magnesium-beryllium rare earth alloy material and method for preparing same | |
CN109022906A (en) | A kind of preparation method of the TiAl intermetallic compound containing rare earth element er | |
CN102776453B (en) | Method for preparing spherocrystal toughening amorphous-based composite | |
CN107052282B (en) | A kind of preparation method of the twin dendrite of Al-40%Zn alloy |
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 | ||
CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20190108 Termination date: 20210714 |
|
CF01 | Termination of patent right due to non-payment of annual fee |