NL2031237B1 - “THERMAL-ELECTRIC” COUPLING PREPARATION METHOD OF TiAl ALLOY SHEET WITHOUT-CANNING - Google Patents
“THERMAL-ELECTRIC” COUPLING PREPARATION METHOD OF TiAl ALLOY SHEET WITHOUT-CANNING Download PDFInfo
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- NL2031237B1 NL2031237B1 NL2031237A NL2031237A NL2031237B1 NL 2031237 B1 NL2031237 B1 NL 2031237B1 NL 2031237 A NL2031237 A NL 2031237A NL 2031237 A NL2031237 A NL 2031237A NL 2031237 B1 NL2031237 B1 NL 2031237B1
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- tial alloy
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- 239000000956 alloy Substances 0.000 title claims abstract description 54
- 229910045601 alloy Inorganic materials 0.000 title claims abstract description 53
- 229910010038 TiAl Inorganic materials 0.000 title claims abstract description 48
- 230000008878 coupling Effects 0.000 title claims abstract description 17
- 238000010168 coupling process Methods 0.000 title claims abstract description 17
- 238000005859 coupling reaction Methods 0.000 title claims abstract description 17
- 238000009924 canning Methods 0.000 title abstract description 20
- 238000002360 preparation method Methods 0.000 title abstract description 12
- 238000000034 method Methods 0.000 claims abstract description 28
- 239000002994 raw material Substances 0.000 claims abstract description 11
- 238000005266 casting Methods 0.000 claims abstract description 8
- 238000005303 weighing Methods 0.000 claims abstract description 7
- 238000000829 induction skull melting Methods 0.000 claims abstract description 4
- 238000010438 heat treatment Methods 0.000 claims description 22
- 238000001816 cooling Methods 0.000 claims description 13
- CSCPPACGZOOCGX-UHFFFAOYSA-N Acetone Chemical compound CC(C)=O CSCPPACGZOOCGX-UHFFFAOYSA-N 0.000 claims description 12
- 238000005507 spraying Methods 0.000 claims description 9
- 239000011248 coating agent Substances 0.000 claims description 8
- 238000000576 coating method Methods 0.000 claims description 8
- 238000005242 forging Methods 0.000 claims description 7
- 238000001035 drying Methods 0.000 claims description 6
- 238000001513 hot isostatic pressing Methods 0.000 claims description 6
- 238000002844 melting Methods 0.000 claims description 6
- 230000008018 melting Effects 0.000 claims description 6
- 238000005498 polishing Methods 0.000 claims description 6
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 claims description 5
- 230000003064 anti-oxidating effect Effects 0.000 claims description 5
- 229910052802 copper Inorganic materials 0.000 claims description 5
- 239000010949 copper Substances 0.000 claims description 5
- 238000005520 cutting process Methods 0.000 claims description 4
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 claims description 3
- 238000000265 homogenisation Methods 0.000 claims description 3
- 239000000155 melt Substances 0.000 claims description 3
- 238000005058 metal casting Methods 0.000 claims description 3
- 238000004506 ultrasonic cleaning Methods 0.000 claims description 3
- 238000005406 washing Methods 0.000 claims description 3
- 239000010439 graphite Substances 0.000 claims description 2
- 229910002804 graphite Inorganic materials 0.000 claims description 2
- 238000004321 preservation Methods 0.000 claims description 2
- 238000003754 machining Methods 0.000 claims 3
- 238000003825 pressing Methods 0.000 claims 1
- 238000005096 rolling process Methods 0.000 abstract description 26
- 238000005272 metallurgy Methods 0.000 abstract description 9
- 239000000463 material Substances 0.000 abstract description 7
- 239000012535 impurity Substances 0.000 abstract description 5
- 238000004663 powder metallurgy Methods 0.000 abstract description 5
- 238000004519 manufacturing process Methods 0.000 abstract description 2
- 229910052751 metal Inorganic materials 0.000 abstract description 2
- 239000002184 metal Substances 0.000 abstract description 2
- XKRFYHLGVUSROY-UHFFFAOYSA-N Argon Chemical compound [Ar] XKRFYHLGVUSROY-UHFFFAOYSA-N 0.000 description 36
- 229910052786 argon Inorganic materials 0.000 description 19
- 239000012298 atmosphere Substances 0.000 description 8
- 239000012300 argon atmosphere Substances 0.000 description 6
- 239000011888 foil Substances 0.000 description 6
- 238000007254 oxidation reaction Methods 0.000 description 6
- 238000012545 processing Methods 0.000 description 6
- 239000010936 titanium Substances 0.000 description 6
- ZOXJGFHDIHLPTG-UHFFFAOYSA-N Boron Chemical compound [B] ZOXJGFHDIHLPTG-UHFFFAOYSA-N 0.000 description 3
- 229910001257 Nb alloy Inorganic materials 0.000 description 3
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 3
- 229910000946 Y alloy Inorganic materials 0.000 description 3
- 229910052782 aluminium Inorganic materials 0.000 description 3
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 3
- QNTVPKHKFIYODU-UHFFFAOYSA-N aluminum niobium Chemical compound [Al].[Nb] QNTVPKHKFIYODU-UHFFFAOYSA-N 0.000 description 3
- RFEISCHXNDRNLV-UHFFFAOYSA-N aluminum yttrium Chemical compound [Al].[Y] RFEISCHXNDRNLV-UHFFFAOYSA-N 0.000 description 3
- 230000000694 effects Effects 0.000 description 3
- 239000010955 niobium Substances 0.000 description 3
- 229910052719 titanium Inorganic materials 0.000 description 3
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 2
- 238000003723 Smelting Methods 0.000 description 2
- 239000010425 asbestos Substances 0.000 description 2
- 229910052796 boron Inorganic materials 0.000 description 2
- 239000011651 chromium Substances 0.000 description 2
- 238000013461 design Methods 0.000 description 2
- 238000007599 discharging Methods 0.000 description 2
- 230000003647 oxidation Effects 0.000 description 2
- 229910052895 riebeckite Inorganic materials 0.000 description 2
- 239000004576 sand Substances 0.000 description 2
- 238000009763 wire-cut EDM Methods 0.000 description 2
- 229910052727 yttrium Inorganic materials 0.000 description 2
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 description 1
- 229910001209 Low-carbon steel Inorganic materials 0.000 description 1
- 229910001182 Mo alloy Inorganic materials 0.000 description 1
- 229910000756 V alloy Inorganic materials 0.000 description 1
- UNQHSZOIUSRWHT-UHFFFAOYSA-N aluminum molybdenum Chemical compound [Al].[Mo] UNQHSZOIUSRWHT-UHFFFAOYSA-N 0.000 description 1
- HIMLGVIQSDVUJQ-UHFFFAOYSA-N aluminum vanadium Chemical compound [Al].[V] HIMLGVIQSDVUJQ-UHFFFAOYSA-N 0.000 description 1
- 238000000137 annealing Methods 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 229910052799 carbon Inorganic materials 0.000 description 1
- 239000000919 ceramic Substances 0.000 description 1
- 229910052804 chromium Inorganic materials 0.000 description 1
- 238000013329 compounding Methods 0.000 description 1
- 238000005336 cracking Methods 0.000 description 1
- 239000013078 crystal Substances 0.000 description 1
- 238000007872 degassing Methods 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 230000005674 electromagnetic induction Effects 0.000 description 1
- 238000011010 flushing procedure Methods 0.000 description 1
- 239000007789 gas Substances 0.000 description 1
- 230000006698 induction Effects 0.000 description 1
- 238000009413 insulation Methods 0.000 description 1
- 229910000765 intermetallic Inorganic materials 0.000 description 1
- 239000007769 metal material Substances 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 229910052759 nickel Inorganic materials 0.000 description 1
- 239000000843 powder Substances 0.000 description 1
- 238000011160 research Methods 0.000 description 1
- 238000001878 scanning electron micrograph Methods 0.000 description 1
- 238000007789 sealing Methods 0.000 description 1
- 238000005204 segregation Methods 0.000 description 1
- 238000007711 solidification Methods 0.000 description 1
- 230000008023 solidification Effects 0.000 description 1
- 238000004381 surface treatment Methods 0.000 description 1
- 230000009466 transformation Effects 0.000 description 1
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
-
- 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
-
- 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
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C30/00—Alloys containing less than 50% by weight of each constituent
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22F—CHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
- C22F1/00—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
- C22F1/16—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of other metals or alloys based thereon
- C22F1/18—High-melting or refractory metals or alloys based thereon
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- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Physics & Mathematics (AREA)
- Thermal Sciences (AREA)
- Crystallography & Structural Chemistry (AREA)
- Metal Rolling (AREA)
Abstract
The present disclosure relates to a “thermal-electric” coupling preparation method of a TiAl alloy sheet without-canning, and aims to solve the problems that an existing cast ingot metallurgy canning rolling method of the TiAl alloy sheet is complex in process, high in cost, poor in sheet shape and low in material utilization rate, and overcome the shortcomings that a powder metallurgy method is high in impurity content, high in cost, low in density and low in production efficiency. The “thermal- electric” coupling preparation method comprises the specific steps of: l, weighing all raw material components; 2, preparing a cast ingot through vacuum induction skull melting and metal mold casting, 3, performing first blank pretreatment, 4, performing second blank pretreatment, and 5, performing “thermal-electric” coupling non-canning rolling on the sheet, to obtain a TiAl alloy sheet.
Description
“THERMAL-ELECTRIC” COUPLING PREPARATION METHOD OF TiAl ALLOY
SHEET WITHOUT-CANNING
[DI] The present disclosure relates to the field of preparation of alloy materials, and particularly relates to a “thermal-electric” coupling preparation method of a TiAl alloy sheet without-canning.
[02] As a novel high-temperature structural material with light weight, high specific strength and good high-temperature oxidation resistance and creep resistance, the TiAl alloy sheet has great application prospects in the aerospace fields of thermal protection systems of space-ground reciprocating aircrafts, skins of supersonic aircrafts, etc.
However, due to the intrinsic brittleness of intermetallic compounds, the TiAl alloy is poor in high-temperature deformation capacity and narrow in hot working window, which limits the development and engineering application of its sheet.
[03] The existing preparation method of the TiAl alloy sheet mainly includes ingot metallurgy method, powder metallurgy method and foil metallurgy method. According to the ingot metallurgy method, the rolling of the TiAl alloy sheet is achieved through a series of procedures such as ingot cogging, hot isostatic pressing, forging cogging, cutting, surface treatment, canning blank making and rolling. The ingot metallurgy method is complex in procedure, high in canning cost, large in deformation resistance difference between canning and TiAl alloy, poor in deformation coordination and low in material utilization rate. According to the powder metallurgy method, the preparation of the TiAl alloy sheet is achieved through a series of procedures such as TiAl alloy powder making, canning blank making, degassing sealing, hot isostatic pressing and rolling. The powder metallurgy method is high in impurity content such as O and N impurity content, high in raw material cost, low in blank density and low in production efficiency.
According to the foil metallurgy method, Ti foil and Al foil serve as the raw materials and are alternately arranged to form a multi-layer structure, and the TiAl alloy sheet is prepared through rolling compounding and subsequent heat treatment. The foil metallurgy method is complex in procedure, weak in component design capacity and poor in plate uniformity and mechanical property. In summary, a large number of researches are carried out on the preparation methods, and certain achievements are obtained, but there are problems that need to be solved urgently.
[04] The present disclosure provides a “thermal-electric” coupling preparation method of a TiAl alloy sheet without-canning, and aims at solving the problems that an ingot metallurgy canning rolling method is complex in procedure, high in canning cost, poor in deformation coordination and low in material utilization rate, and the challenges that a powder metallurgy method and a foil metallurgy method are difficult in component control and poor in plate uniformity and mechanical property.
[05] In order to solve the above technical problems, the technical solution adopted by the present disclosure is as follows: a “thermal-electric” coupling non-canning preparation method of a TiAl alloy sheet comprises the following steps:
[06] step 1, weighing of raw materials: respectively weighing high-purity sponge titanium, high-purity aluminum, high-purity chromium, aluminum-niobium alloy, aluminum-molybdenum alloy, aluminum-yttrium alloy, aluminum-vanadium alloy, high-purity nickel powder, boron powder and carbon powder as raw materials; alloy comprises the following components in atomic percent: 41-44% of Al, 0-9% of Nb, 0- 9% of V, 0-2% of Cr, 0-4% of Mo, 0-0.5% of X and the balance Ti and inevitable impurity elements, wherein X is one or more of B, Y, C and Ni elements;
[07] step 2, ingot casting: adding the raw materials weighed in the step 1 into a water-cooled copper crucible vacuum induction skull melting furnace and melting; and pouring a melt into a pre-heated metal casting mold to obtain a cylindrical TiAl alloy ingot, wherein the diameter of the ingot is greater than or equal to 100 mm, and the height of the ingot is greater than or equal to 180 mm;
[08] step 3, first blank pretreatment:
[09] a, removing a dead head of the TiAl alloy ingot and carrying out hot isostatic pressing; keeping the temperature for 3-4 h; cooling along with the furnace; and discharging from the furnace;
[10] b, carrying out homogenization treatment on the ingot and putting the ingot into a vacuum heat treatment furnace, keeping the temperature of 900-1,100 °C for 24- 48 h, and cooling along with the furnace;
[11] c‚ removing an oxide skin of the annealed ingot and flattening upper and lower end faces; processing the ingot into a standard cylindrical block through a wire cut electrical discharge machining, wherein the height-diameter ratio is 1.5: 1 to 2: 1; polishing the blank with abrasive paper, wherein the roughness RA is 1.6-0.8; then putting the ingot into an acetone solution and carrying out ultrasonic washing for 5-10 min; taking out the ingot and drying to obtain a TiAl alloy cylindrical blank;
[12] d, spraying high-temperature anti-oxidization coating on the circumferential surface, the upper end surface and the lower end surface of the TiAl alloy cylindrical blank; spraying the anti-oxidization coating for two layers, wherein each layer is 50 um in thickness; and after spraying each time, standing in a constant-temperature and constant-humidity chamber for 1 h;
[13] step 4, second blank pretreatment:
[14] a, wrapping the TiAl alloy cylindrical blank coated and sprayed with the high- temperature anti-oxidation using an asbestos felt with thickness of 8-10 mm; and keeping the temperature at 1,200-1,250°C for 60 min;
[15] b, heating an upper anvil and a lower anvil of a press machine to 600-700 °C by using a split cylindrical box type resistance furnace, clamping the blank that is subjected to heat keeping in the step a between the upper anvil and the lower anvil in a resistance furnace cavity, performing non-canning near-isothermal upsetting deformation on the TiAl alloy blank at a strain rate of 0.01-0.05 s™ wherein the total deformation is 70-80%; and then placing the blank that is subjected to upsetting in a vacuum heat treatment furnace, keeping the temperature at 900°C-1,000°C for 2 h, and cooling along with the furnace;
[16] c‚ removing oxide skin from the upset blank, flattening the surface, cutting a forging cake core part, processing the forging cake core part into a standard rectangular block, and processing a chamfer at the deformed front end of the blank; 17] d, polishing the rectangular blank with abrasive paper, wherein the roughness
Rais 1.6-0.8, placing the rectangular blank in an acetone solution, performing ultrasonic cleaning for 5-10 min, then taking out the rectangular blank, and drying the rectangular blank;
[18] step 5, “thermal-electric” coupling rolling:
[19] a, keeping the temperature of the dried TiAl alloy blank obtained in the step 4 in the vacuum box type heat treatment furnace under 1,150°C-1,200°C for 30-60 min;
[20] b, taking out the blank from the furnace, performing “thermal-electric” coupling rolling, wherein the surface temperature of a roller is 300°C-600°C; introducing pulse current from a blank far away from a rolling inlet through a copper conductive clamp with a graphite gasket, wherein the rolling speed is 0.5-1.5 m/s, and the pass reduction rate is 10-20%; and performing pass temperature keeping in the furnace again;
[21] c‚ keeping the temperature of the rolled sheet in the vacuum heat treatment furnace under 900°C-1,000°C for 2 h, and cooling along with the furnace to obtain the
TiAl alloy sheet.
[22] Preferably, in the step 2, the smelting atmosphere is argon atmosphere, the argon pressure is 0.95-1 MPa, the mass purity of argon is 99.99%, and a furnace chamber is washed for three times by adopting a “vacuumizing-argon filling-vacuumizing” mode before smelting; a casting mold material is low-carbon steel, the preheating temperature is 300-500°C, and a casting mold is pre-buried into Al20:3 or ZrO; sand; and furnace cooling is carried out after pouring.
[23] Preferably, in the step 3a, the hot isostatic pressing treatment process is carried out at 1,230-1,260 °C and 100-150 MPa, the argon atmosphere is used for protection, and the mass purity of argon 1s 99.99%; in the step 3b, the heat treatment atmosphere is argon atmosphere, the argon pressure is 0.95-1 MPa, and the mass purity of argon is
99.99%; and in the step 3d, the high-temperature anti-oxidation coating is a commercially available 1,500°C type finished product, the temperature during standing treatment is 50-55°C, and the humidity is 50-60% RH.
[24] Preferably, in the step 4b, the treatment atmosphere is argon atmosphere, the 5 argon pressure is 0.95-1 MPa, and the mass purity of argon is 99.99%; and in the step 4c, the chamfer is a fillet, the angle is 45 degrees, and the radius is 3-6 mm.
[25] Preferably, in the step 5, the heat treatment and annealing atmosphere 1s argon atmosphere, the argon pressure is 0.95-1 MPa, the mass purity of argon is 99.99%, and the inert atmosphere environment is guaranteed by introducing high-flow argon when a furnace door is opened and closed; in the step 5b, the roller temperature is realized by a resistance baking or electromagnetic induction surface heating method, the bearing temperature 1s guaranteed to be lower than 70°C by water-cooling transformation, the pulse current frequency is 300-800 Hz, the waveform is rectangular, the voltage is 120
V, the peak current is 100-200 A-mm'?, and the rolling mill rack insulation is realized by a bearing block ceramic insulating gasket.
[26] Preferably, in the step 5b, the heat keeping temperature is 1,150-1,200 °C, the heat preservation time is 10-15 min, and the total rolling deformation is 30-40%.
[27] Compared with the prior art, the present disclosure has the following beneficial effects:
[28] 1. The problem of segregation of high-melting-point B stable elements in deformed TiAl is successfully solved by adopting a vacuum induction melting and preheating metal mold casting mode.
[29] 2. An alloy solidification path is designed from the angle of alloy components, the phase composition of the TiAl alloy solidified by adopting the path at the room temperature and the high temperature is controlled, and the high-temperature deformation capacity of the alloy is improved.
[30] 3. Through large-deformation near-isothermal upsetting pretreatment, the structure form of the TiAl alloy ingot is effectively improved, as-cast dendritic crystals are crushed, grains are refined, and meanwhile, the problem that the components and the grain size in a blank are not uniform is further solved.
[31] 4. The “thermal-electric” coupling rolling method combining pulse current assistance and hot roller near-isothermal rolling is adopted, the promotion effect of the pure plastic effect in pulse current on the metal material dislocation and super- dislocation motion capacity is utilized, the material deformation resistance is reduced, and the plastic deformation capacity is improved, meanwhile, based on the high electrical resistivity of TiAl alloy, the joule heat effect of the pulse current is utilized, electric energy 1s converted into heat energy, the blank temperature is increased, and the temperature needed by thermal deformation is reduced; meanwhile, based on roller heating, the temperature drop of the blank in the rolling process is reduced, a near- isothermal rolling environment is provided, and a large number of body-centered cubic high-temperature B phases brought by component design are combined, thus high- temperature plastic deformation capacity of the TiAl alloy is improved from multiple aspects, and high-quality rolling of the TiAl alloy is achieved. [B2] 5. Non-canning assembly is adopted, the traditional blank canning treatment manner is broken through, the cost is reduced, the process is simplified, the problems that a canning material absorbs rolling deformation, and the compatibility with TiAl alloy deformation is poor are solved, and the rolling efficiency is improved.
[33] 6. The oxidation problem of the TiAl alloy in the heating and rolling process is solved by reducing the rolling temperature and conducting preheating and remelting under inert atmosphere protection, and the obtained sheet has good surface quality and is free of the obvious surface cracking phenomenon.
[34] 7. The obtained sheet is uniform and fine in grain and good in comprehensive mechanical property and can be directly used or subjected to secondary forming.
[35] FIG. 1 is a TiAl alloy sheet obtained in step 5 in Example 1;
[36] FIG. 2 is a SEM image of a TiAl alloy sheet obtained in step 5 in Example 2.
[37] The present disclosure will be further described in conjunction with specific embodiments.
[38] Example 1
[39] A “thermal-electric” coupling non-canning preparation method of a TiAl alloy sheet comprises the following steps:
[40] step 1, weighing of raw materials:
[41] respectively weighing high-purity sponge titanium, high-purity aluminum, aluminum-niobium alloy (Nb content of 54.56%), aluminum-yttrium alloy (Y content of 87.3%), and boron powder totaling 10 Kg as raw materials; the alloy comprises the following components in atomic percent: 44% of Al, 8% of Nb, 0.1% of X (X is a combination of B and Y) and the balance Ti and inevitable impurity elements.
[42] step 2, ingot casting:
[43] adding the high-purity sponge titanium, high-purity aluminum, aluminum- niobium alloy, aluminum-yttrium alloy, and boron powder weighed in the step 1 into a water-cooled copper crucible vacuum induction skull melting furnace for melting, wherein the melting atmosphere is argon atmosphere and the argon pressure is 0.95- 1MPa, the mass purity of argon gas is 99.99%, flushing the furnace chamber three times by the method of “vacuuming-argon filling-vacuuming” before melting; and pouring a melt into a 500°C pre-heated metal casting mold to obtain a cylindrical alloy ingot, wherein the diameter of the ingot is 100 mm, and the height of the ingot is 185 mm. The casting mold is pre-embedded in Al:Os sand; after pouring, cooled along with the furnace.
[44] step 3, first blank pretreatment:
[45] a, removing a dead head of the TiAl alloy ingot and carrying out hot isostatic pressing, wherein the treatment process is 1250°C, 150MPa, with argon protection, and the mass purity of argon is 99.99%; keeping the temperature for 4 h; cooling along with the furnace; and discharging from the furnace;
[46] b, carrying out homogenization treatment on the ingot and putting the ingot into a vacuum heat treatment furnace; keeping the temperature of 1,000 °C for 24 h, and cooling along with the furnace; wherein the heat treatment atmosphere is argon, the argon pressure is 0.95-1MPa, and the mass purity of argon is 99.99%;
[47] c‚ removing an oxide skin of the annealed ingot and flattening upper and lower end faces; processing the ingot into a standard cylindrical block through a wire cut electrical discharge machining, wherein the height-diameter ratio is 1.5: 1; polishing the blank with abrasive paper, wherein the roughness RA is 1.6; then putting the ingot into an acetone solution and carrying out ultrasonic washing for 5 min; taking out the ingot and drying;
[48] d, spraying high-temperature anti-oxidization coating on the circumferential surface, the upper end surface and the lower end surface of the TiAl alloy cylindrical blank; spraying the anti-oxidization coating for two layers, wherein each layer is 50 um in thickness; and after spraying each time, standing in a constant-temperature and constant-humidity chamber for 1 h; wherein the standing temperature is 50°C, and the humidity is 50%RH.
[49] step 4, second blank pretreatment:
[50] a, wrapping the TiAl alloy cylindrical blank using an asbestos felt with thickness of 8 mm; and keeping the temperature at 1,250°C for 30 min;
[51] b, heating an upper anvil and a lower anvil of a press machine to 600°C by using a split cylindrical box type resistance furnace, clamping the blank that is subjected to heat keeping in the step 1 between the upper anvil and the lower anvil in a resistance furnace cavity, performing non-canning near-isothermal upsetting deformation on the
TiAl alloy blank at a strain rate of 0.01 s™, wherein the total deformation is 70%; and then placing the blank that is subjected to upsetting in a vacuum heat treatment furnace, keeping the temperature at 900°C for 2 h, and cooling along with the furnace;
[52] c‚ removing oxide skin from the upset blank, flattening the surface, cutting a forging cake core part, processing the forging cake core part into a standard rectangular block, and processing a chamfer at the deformed front end of the blank; wherein the chamfer is round, the angle is 45°, the radius is Smm;
[53] d, polishing the rectangular blank with abrasive paper, wherein the roughness
Ra is 1.6, placing the rectangular blank in an acetone solution, performing ultrasonic cleaning for 5 min, then taking out the rectangular blank, and drying the rectangular blank.
[54] step 5, “thermal-electric” coupling rolling:
[55] a, keeping the temperature of the TiAl alloy blank obtained in the step 4 in the vacuum box type heat treatment furnace under 1,200°C for 30 min;
[56] b, taking out the TiAl alloy blank from the furnace, performing “thermal- electric” coupling rolling, wherein the surface temperature of a roller is 600°C, the pulse current frequency is 800Hz, the waveform is rectangular, the voltage is 120V, the peak current is 200A-mm™, the rolling speed is 0.5m/s, the pass reduction rate is 15%; and performing pass temperature keeping in the furnace again, wherein the holding temperature is 1200°C, the holding time is 10min, and the total rolling deformation is 30%;
[57] c‚ keeping the temperature of the rolled sheet in the vacuum heat treatment furnace under 900°C for 2 h, and cooling along with the furnace to obtain the TiAl alloy sheet.
[58] The TiAl alloy sheet obtained in the step 5 in the above Example 1 has a good surface quality, without obvious cracks, as shown in FIG.1.
Claims (1)
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