EP2342365A1 - Method for producing a ss- -tial base alloy - Google Patents
Method for producing a ss- -tial base alloyInfo
- Publication number
- EP2342365A1 EP2342365A1 EP10765988A EP10765988A EP2342365A1 EP 2342365 A1 EP2342365 A1 EP 2342365A1 EP 10765988 A EP10765988 A EP 10765988A EP 10765988 A EP10765988 A EP 10765988A EP 2342365 A1 EP2342365 A1 EP 2342365A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- tial
- electrode
- titanium
- 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.)
- Granted
Links
- 239000000956 alloy Substances 0.000 title claims abstract description 103
- 229910045601 alloy Inorganic materials 0.000 title claims abstract description 101
- 238000004519 manufacturing process Methods 0.000 title claims abstract description 17
- 239000010936 titanium Substances 0.000 claims abstract description 44
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 claims abstract description 38
- 229910052719 titanium Inorganic materials 0.000 claims abstract description 35
- 238000000034 method Methods 0.000 claims abstract description 17
- 229910010038 TiAl Inorganic materials 0.000 claims abstract description 12
- 238000010313 vacuum arc remelting Methods 0.000 claims abstract description 5
- 238000009827 uniform distribution Methods 0.000 claims abstract description 3
- 229910006281 γ-TiAl Inorganic materials 0.000 claims description 41
- 238000002844 melting Methods 0.000 claims description 31
- 230000008018 melting Effects 0.000 claims description 31
- 239000000463 material Substances 0.000 claims description 12
- 239000002131 composite material Substances 0.000 claims description 9
- 230000002950 deficient Effects 0.000 claims description 8
- 229910052720 vanadium Inorganic materials 0.000 claims description 8
- 229910052782 aluminium Inorganic materials 0.000 claims description 7
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims description 7
- 238000003825 pressing Methods 0.000 claims description 5
- 238000005266 casting Methods 0.000 claims description 4
- 229910052804 chromium Inorganic materials 0.000 claims description 4
- 229910052750 molybdenum Inorganic materials 0.000 claims description 4
- 229910052748 manganese Inorganic materials 0.000 claims description 3
- 229910052758 niobium Inorganic materials 0.000 claims description 3
- 229910052715 tantalum Inorganic materials 0.000 claims description 3
- 230000007812 deficiency Effects 0.000 claims description 2
- 230000000087 stabilizing effect Effects 0.000 claims description 2
- 229910052726 zirconium Inorganic materials 0.000 claims description 2
- 238000003466 welding Methods 0.000 claims 2
- 229910052796 boron Inorganic materials 0.000 claims 1
- 238000009826 distribution Methods 0.000 claims 1
- 238000005495 investment casting Methods 0.000 claims 1
- 229910052710 silicon Inorganic materials 0.000 claims 1
- 238000000365 skull melting Methods 0.000 claims 1
- 238000005275 alloying Methods 0.000 abstract description 3
- 230000006735 deficit Effects 0.000 abstract description 3
- 238000003723 Smelting Methods 0.000 abstract 4
- 239000000203 mixture Substances 0.000 description 13
- 229910052802 copper Inorganic materials 0.000 description 9
- 239000010949 copper Substances 0.000 description 9
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 8
- 238000005336 cracking Methods 0.000 description 5
- 239000000155 melt Substances 0.000 description 5
- 239000007858 starting material Substances 0.000 description 5
- LEONUFNNVUYDNQ-UHFFFAOYSA-N vanadium atom Chemical compound [V] LEONUFNNVUYDNQ-UHFFFAOYSA-N 0.000 description 4
- 239000000470 constituent Substances 0.000 description 3
- 230000006698 induction Effects 0.000 description 3
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 3
- 230000015572 biosynthetic process Effects 0.000 description 2
- 150000001875 compounds Chemical class 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 238000000265 homogenisation Methods 0.000 description 2
- 238000010309 melting process Methods 0.000 description 2
- 238000002360 preparation method Methods 0.000 description 2
- 238000007711 solidification Methods 0.000 description 2
- 230000008023 solidification Effects 0.000 description 2
- 239000000126 substance Substances 0.000 description 2
- 230000009466 transformation Effects 0.000 description 2
- 238000000844 transformation Methods 0.000 description 2
- 229910000838 Al alloy Inorganic materials 0.000 description 1
- ZOKXTWBITQBERF-UHFFFAOYSA-N Molybdenum Chemical compound [Mo] ZOKXTWBITQBERF-UHFFFAOYSA-N 0.000 description 1
- 229910004349 Ti-Al Inorganic materials 0.000 description 1
- 229910004692 Ti—Al Inorganic materials 0.000 description 1
- UQZIWOQVLUASCR-UHFFFAOYSA-N alumane;titanium Chemical compound [AlH3].[Ti] UQZIWOQVLUASCR-UHFFFAOYSA-N 0.000 description 1
- 230000002051 biphasic effect Effects 0.000 description 1
- 238000009750 centrifugal casting Methods 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
- 238000005253 cladding Methods 0.000 description 1
- 238000010924 continuous production Methods 0.000 description 1
- 238000001816 cooling Methods 0.000 description 1
- 150000001879 copper Chemical class 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 239000007772 electrode material Substances 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 230000008020 evaporation Effects 0.000 description 1
- 238000001704 evaporation Methods 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- 239000012761 high-performance material Substances 0.000 description 1
- 230000001939 inductive effect Effects 0.000 description 1
- 229910000765 intermetallic Inorganic materials 0.000 description 1
- 238000005259 measurement Methods 0.000 description 1
- 238000010310 metallurgical process Methods 0.000 description 1
- 238000002156 mixing Methods 0.000 description 1
- 239000011733 molybdenum Substances 0.000 description 1
- 239000002994 raw material Substances 0.000 description 1
- 238000005245 sintering Methods 0.000 description 1
- 210000003625 skull Anatomy 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 230000006641 stabilisation Effects 0.000 description 1
- 238000011105 stabilization Methods 0.000 description 1
- 239000010935 stainless steel Substances 0.000 description 1
- 229910001220 stainless steel Inorganic materials 0.000 description 1
- 230000007847 structural defect Effects 0.000 description 1
- 239000000725 suspension Substances 0.000 description 1
- 239000013077 target material Substances 0.000 description 1
- 230000000930 thermomechanical effect Effects 0.000 description 1
- 229910021324 titanium aluminide Inorganic materials 0.000 description 1
Classifications
-
- 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
- C22B—PRODUCTION AND REFINING OF METALS; PRETREATMENT OF RAW MATERIALS
- C22B34/00—Obtaining refractory metals
- C22B34/10—Obtaining titanium, zirconium or hafnium
- C22B34/12—Obtaining titanium or titanium compounds from ores or scrap by metallurgical processing; preparation of titanium compounds from other titanium compounds see C01G23/00 - C01G23/08
- C22B34/1295—Refining, melting, remelting, working up of titanium
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22B—PRODUCTION AND REFINING OF METALS; PRETREATMENT OF RAW MATERIALS
- C22B9/00—General processes of refining or remelting of metals; Apparatus for electroslag or arc remelting of metals
- C22B9/16—Remelting metals
- C22B9/20—Arc remelting
-
- 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
Definitions
- the invention relates to a process for the production of ⁇ -TiAl base alloys by means of vacuum arc melting (VA) which solidify completely or at least partially primarily via the ⁇ -phase.
- VA vacuum arc melting
- target alloys will hereinafter be referred to as ⁇ - ⁇ -TiAl base alloy.
- the technical field of the present invention is the melt metallurgical production of ⁇ - ⁇ -TiAl alloys by means of vacuum arc melting (VAR).
- VAR vacuum arc melting
- step (ii) at least one remelting of the electrodes obtained in step (i) by a conventional melt metallurgical process
- Diameter. DE 195 81 384 TI describes intermetallic TiAl compounds and processes for their preparation, wherein the alloy by heat treatment of an alloy having a Ti concentration of 42 to 48 atom%, an Al concentration of 44 to 47 atomic%, a Nb concentration of 6 to 10 atom% and a Cr concentration of 1 to 3 atom% at a temperature in the range of 1300 to 1400 ° C is prepared.
- DE 196 31 583 A1 discloses a method for producing a TiAl-Nb product from an alloy, in which first an alloy electrode is produced from the alloy components. The formation of the alloy electrode is carried out by pressing and / or sintering the alloy components to the electrode. The latter is melted off by an induction coil.
- JP 02277736 A discloses a heat-resistant TiAl-based alloy in which specific amounts of V and Cr are introduced into an intermetallic Ti-Al compound to improve heat resistance and ductility.
- DE 1 179 006 A discloses ternary or higher titanium-aluminum alloys with such elements which stabilize the ⁇ - and ⁇ -phase of the titanium.
- the usual process for remelting is vacuum-arc melting with self-consuming electrode, since the plasma melting plants are generally not designed for the supply of compact ingots as starting material.
- biphasic in the form of lamellar colonies of the a2-Ti 3 Al phase and the ⁇ -TiAl phase constructed ⁇ -TiAl base alloys remelting takes place in the vacuum arc furnace (VAR furnace) easily and leads to the desired result (see V. Guether: "Status and Prospects of ⁇ -TiAl Intote Production", International Symp. on Gamma Titanium Aluminides 2003, ed. H. Clemens, Y.-W. Kim and AH Rosenberger, San Diego, TMS 2004).
- a new generation of ⁇ -TiAl high performance materials has a structural design different from conventional TiAl alloys.
- ß-stabilizing elements such as Cr, Cu, Hf, Mn, Mo, Nb, V , Ta and Zr
- a primary solidification path is established over the ⁇ -Ti phase. This results in very fine microstructures, in addition to lamellar ⁇ 2 / ⁇ - Colonies also include globular ⁇ grains and globular ⁇ grains, sometimes including globular 012 grains.
- the disadvantage is that cracking occurs again during the remelting of electrodes from this material in the VAR furnace, the result of which is frequently the flaking off of constituents of the self-consumable alloy electrode from the primary melting zone. These chipped parts fall into the molten bath and are no longer completely remelted therein. This causes structural defects in the ingot, making the ingot material unusable. Remelting in the VAR furnace is no longer technically reproducible under these conditions.
- the cause of the disturbing chipping behavior is considered to be massive phase transformations in the temperature range between the eutectoid temperature and the phase boundary temperature to the ⁇ -phase region.
- the curve represents the During VAR melting, based on the length of the self-consumable electrode, a temperature field extends from the melting temperature (about 1570 ° C.) at the bottom of the electrode to near room temperature at the electrode suspension between 1000 and 1200 ° C.
- the relatively poor ductility of the intermetallic material then leads in this zone to the formation of the S Tear discharges in the form of cracks, which in turn lead to the described chipping of unmelted pieces of the electrode.
- the present invention seeks to provide a method for producing a solidifying over the ⁇ -phase ⁇ -TiAl base alloy - hereinafter referred to as ⁇ - ⁇ -TiAl base alloy - specify that Avoiding the cracking problem leads to a reliable production of such a target alloy.
- the successive remelting steps during the vacuum arc melting are thus subdivided into the melting of a primary alloy in the first remelting steps, wherein a base melt electrode is produced from a conventional ⁇ -TiAl primary alloy, and the melting of the target alloy in the form of the desired ⁇ - ⁇ -TiAl base alloy in the last remelting step.
- the primary alloy has a deficit of titanium and / or a deficiency of ß-stabilizing elements such as Nb, Mo, Cr, Mn, V, and Ta.
- the alloy is a defined amount of titanium and / or ß deprived of stabilizing elements, so that an aluminum content of the primary alloy preferably between 45 at .-% (particularly preferably 45.5 at .-%) and 50 at .-% sets.
- the contents of aluminum and ß-stabilizing elements are chosen so that the solidification path of the primary alloy is at least partially via the peritectic conversion. It is thus set a structure analogous to conventional TiAl alloys, which can be processed easily in VA oven.
- the target alloy is readjusted by the addition of the materials originally removed from the press electrode.
- these materials are welded as cladding to form a composite electrode firmly on the outer surface of the Abschmelzelektrode to safely exclude a solid state drop into the molten bath. It is also possible to accomplish this by a sheath insert of the deficient alloy content on the inside of the Umschmelzkokille the VAR furnace.
- 1 is a schematic diagram of a vacuum arc melting furnace
- 2 is a perspective view of a composite electrode in a first embodiment
- Fig. 3 is a perspective view of a composite electrode in a second embodiment
- Fig. 4 is a diagram of the linear expansion coefficient as
- the VAR furnace 1 has a copper crucible 4 with a bottom plate 5. Around this copper crucible 4 around a water jacket 6 with water inlet 7 and 8 water outlet is arranged. The copper crucible 4 is also closed at the top of a vacuum bell 9, passes through the top of a lifting bar 10 vertically displaceable. At this lifting bar 10 sits the holder 1 1, where the actual electrode 2 is suspended.
- a DC voltage is applied between the copper crucible 4 and the lifting rod 10, due to which a high-current arc is ignited and maintained between the electrode 2 electrically connected to the lifting rod 10 and the copper crucible 4.
- the electrode 2 is successively remelted to ingot 3 under homogenization of the alloy components.
- the target composition of the ⁇ - ⁇ -TiAl alloy is Ti - 43.5A1 - 4.0Nb - ⁇ , ⁇ - 0.1B (at .-%) or Ti - A128.6 - Nb9, l - Mo2, 3 - B0.03 (m-%).
- the composition of the primary alloy for the base melt electrode is determined by a reduction of the titanium content to Ti - 45.93A1 - 4.22Nb - l, 06Mo - 0.1 1B (at .-%).
- a ingot 3 of the primary alloy of 200 mm in diameter and a length of 1.4 m by 2-fold VAR melting as described above is produced from a pressing electrode 2, without the occurrence of a cracking problem.
- titanium sponge pure aluminum and master alloys are used.
- the entire surface area of the ingot 3 becomes of the primary alloy Pure titanium sheet 15 with a thickness of 3 mm (mass 12 kg) wound and partially welded to the lateral surface 16 of the ingot 3, as shown in Fig. 2.
- the upper edge 17 of the titanium sheet 15 is completely welded over the circumference of the ingot 3 with this.
- weld spots 18 are set distributed over the lateral surface 16.
- the thus assembled self-consumable electrode is remelted as a composite electrode 19 in a final melting step in the VAR furnace 1 to a ingot 3 with a diameter of 280 mm and the composition of the target alloy.
- the target composition, the feeds used and the composition of the primary alloy correspond to the exemplary embodiment 1.
- an ingot 3 having a diameter of 140 mm and a length of 1.8 m is produced by simple VAR melting of press electrodes 2.
- the mass of the ingot is 1 15 kg.
- a sheet of pure titanium with the dimensions circumference 628 mm x height 880 mm x thickness 3 mm (mass 7.6 kg) in the inserted inner surface.
- the composition of the primary alloy ingot forming the base melt electrode 2 and the titanium sheet thus provide the target composition.
- the target composition, the starting materials used and the composition of the primary alloy correspond to the embodiment 1, likewise the production of the composite electrode 19.
- the last remelting takes place in what is known as a VAR skull melter, ie a vacuum arc - Melting device with a water-cooled, tiltable crucible made of copper.
- the target material's molten alloy material is poured into permanent molds made of stainless steel, which are attached to a rotating casting wheel.
- the casting bodies thus produced by centrifugal casting are used as starting material for the production of components from the target alloy.
- Exemplary Embodiment 4 A ⁇ - ⁇ -TiAl alloy according to US Pat. No. 6,669,791 has a composition (target alloy) Ti-43,0A1-6,0V (at.%) Or Ti-A129,7-V7,8 (m-%). ).
- the composition of the primary alloy is determined by the complete reduction of the strongly ⁇ -stabilizing element vanadium to Ti-45J5A1 (at .-%) or Ti-A132.2 (m-%).
- insert materials titanium sponge, aluminum and vanadium are used.
- a base melt electrode 2 is prepared as an ingot of the binary TiAl primary alloy having a diameter of 200 mm and a length of 1 m by double VAR melting (mass 126 kg).
- vanadium rods 20 with a diameter of 16.7 mm and a length of 1 m (total mass 10.7 kg) are each offset by 45 ° relative to one another along the entire lateral surface 16 of the base melt electrode 2, and thus uniformly welded over the circumference of the electrode 2 welded.
- the resulting composite electrode 19 'from the binary primary alloy and the welded vanadium rods 20 is in the final third
- the target composition of the ⁇ -TiAl alloy corresponds to that of Embodiment 1 (Ti - 43.5A1 - 4.0Nb - ⁇ , ⁇ - 0.1B at .-%).
- the composition of the primary alloy is determined by a complete reduction of the molybdenum content and a partial reduction of the titanium content to Ti - 49.63A1 - 4.57Nb - 0.1 1B (at .-%).
- a base melt electrode 2 having a diameter of 200 mm and a length of 1 m is produced by double VAR melting.
- the ingot mass is 126 kg.
- the electrode 2 On the lateral surface 16 of the electrode 2, eight rods made of the commercial TiMol5 alloy are welded on, parallel to the longitudinal axis parallel to exemplary embodiment 4.
- the diameter of the rods is 26 mm, the length of the rods corresponds to the ingot length.
- the total mass of the TiMol5 rods is 19.6 kg.
- the resulting composite electrode consisting of one ingot of the primary alloy and eight TiMol5 rods is remelted in the final third melting process to an ingot of the target alloy with a diameter of 300 mm in the VAR furnace 1.
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- Chemical & Material Sciences (AREA)
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- Mechanical Engineering (AREA)
- Organic Chemistry (AREA)
- Metallurgy (AREA)
- Materials Engineering (AREA)
- Manufacturing & Machinery (AREA)
- Physics & Mathematics (AREA)
- Plasma & Fusion (AREA)
- Life Sciences & Earth Sciences (AREA)
- Environmental & Geological Engineering (AREA)
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Abstract
Description
Verfahren zur Herstellung einer β-γ-TiAl-Basislegierung Process for producing a β-γ-TiAl base alloy
Die Erfindung betrifft ein Verfahren zur Herstellung von γ-TiAl Basislegierungen mittels Vakuum-Lichtbogen-Schmelzen (VA ), die vollständig oder zumindest teilweise primär über die ß -Phase erstarren. Derartige Ziellegierungen sollen im Folgenden als β-γ-TiAl-Basislegierung bezeichnet werden. The invention relates to a process for the production of γ-TiAl base alloys by means of vacuum arc melting (VA) which solidify completely or at least partially primarily via the β-phase. Such target alloys will hereinafter be referred to as β-γ-TiAl base alloy.
Das technische Gebiet der vorliegenden Erfindung ist die schmelzmetallur- gische Herstellung von β-γ-TiAl-Legierungen mittels Vakuum- Lichtbogen- Schmelzen (VAR). Ursprünglich werden dabei ausgehend von den Rohstoffen Titanschwamm, Aluminium sowie Legierungselementen und Vorlegierungen kompakte Körper gepresst, in denen die gewünschten Legierungsbestandteile in der stöchiometrisch passenden Form vorliegen. Gege- benenfalls werden hierbei durch das spätere Schmelzen verursachte Abdampfverluste vorgehalten. Die Presskörper werden entweder direkt mittels Plasmaschmelzen zu sogenannten Ingots eingeschmolzen (PAM) oder zu selbstverzehrenden Elektroden zusammengebaut und zu Ingots abgeschmolzen (VAR). In beiden Fällen entstehen Materialien, deren chemi- sehe und strukturelle Homogenität für eine technische Verwendung ungeeignet ist und die demzufolge noch mindestens einmal umgeschmolzen werden müssen (s. V. Guether:„Micro strueture and Defects in γ-TiAl ba- sed Vacuum Are Remelted Ingot Materials", 3rd Int. Symp. on Structural Intermetallics, September 2001, Jackson Hole WY, USA). Aus der DE 101 56 336 A1 ist ein Verfahren zur Herstellung von Legie- rungs-Ingots bekannt, das folgende Stufen aufweist: The technical field of the present invention is the melt metallurgical production of β-γ-TiAl alloys by means of vacuum arc melting (VAR). Originally, starting from the raw materials titanium sponge, aluminum and alloying elements and master alloys compact bodies are pressed in which the desired alloying constituents are present in the stoichiometrically appropriate form. If necessary, evaporation losses caused by the later melting are stored here. The compacts are either melted directly by means of plasma melts into so-called ingots (PAM) or assembled to self-consuming electrodes and melted down to ingots (VAR). In both cases, materials are formed whose chemical and structural homogeneity is unsuitable for industrial use and which consequently must be remelted at least once (see V. Guether: Microstructures and Defects in γ-TiAl ba- sed Vacuum Are Remelted Ingot Materials ", 3 nd International Symp on Structural Intermetallics, September 2001, Jackson Hole WY, USA). From DE 101 56 336 A1 a process for the production of alloy ingots is known which comprises the following steps:
(i) Herstellung von Elektroden durch übliches Vermischen und Verpres- sen der ausgewählten Ausgangsstoffe, (i) preparation of electrodes by customary mixing and pressing of the selected starting materials,
(ii) mindestens einmaliges Umschmelzen der in Stufe (i) erhaltenen Elektroden durch ein übliches schmelzmetallurgisches Verfahren, (ii) at least one remelting of the electrodes obtained in step (i) by a conventional melt metallurgical process,
(iii) induktives Abschmelzen der in Stufe (i) oder (ii) erhaltenen Elektroden in einer Hochfrequenz-Spule, (iii) inductive melting of the electrodes obtained in step (i) or (ii) in a high-frequency coil,
(iv) Homogenisieren der in Stufe (iii) erhaltenen Schmelze in einem Kalt- wandinduktionstiegel und (iv) homogenizing the melt obtained in step (iii) in a cold wall induction crucible and
(v) Abziehen der Schmelze unter Kühlung aus dem Kaltwandinduktionstiegel von Stufe (iv) in Form von Blöcken mit frei einstellbarem (v) withdrawing the melt under cooling from the cold wall induction crucible of step (iv) in the form of blocks with freely adjustable
Durchmesser. Die DE 195 81 384 Tl beschreibt intermetallische TiAl- Verbindungen und Verfahren zu ihrer Herstellung, wobei die Legierung durch Wärmebehandlung einer Legierung mit einer Ti-Konzentration von 42 bis 48 Atom-%, einer AI-Konzentration von 44 bis 47 Atom-%, einer Nb-Konzentration von 6 bis 10 Atom-% und einer Cr-Konzentration von 1 bis 3 Atom-% bei einer Temperatur im Bereich von 1.300 bis 1.400° C hergestellt wird. Diameter. DE 195 81 384 TI describes intermetallic TiAl compounds and processes for their preparation, wherein the alloy by heat treatment of an alloy having a Ti concentration of 42 to 48 atom%, an Al concentration of 44 to 47 atomic%, a Nb concentration of 6 to 10 atom% and a Cr concentration of 1 to 3 atom% at a temperature in the range of 1300 to 1400 ° C is prepared.
Die DE 196 31 583 AI offenbart ein Verfahren zur Herstellung eines TiAl- Nb-Erzeugnisses aus einer Legierung, bei dem zunächst aus den Legierungskomponenten eine Legierungselektrode hergestellt wird. Die Ausbil- dung der Legierungselektrode erfolgt durch Pressung und/oder Sintern der Legierungskomponenten zu der Elektrode. Letztere wird durch eine Induktionsspule abgeschmolzen. Aus der JP 02277736 A ist eine hitzebeständige TiAl-Basislegierung bekannt, bei der zur Verbesserung der Wärmebeständigkeit und Duktilität spezifische Mengen von V und Cr in eine intermetallische Ti- AI- Verbindung eingebracht werden. DE 196 31 583 A1 discloses a method for producing a TiAl-Nb product from an alloy, in which first an alloy electrode is produced from the alloy components. The formation of the alloy electrode is carried out by pressing and / or sintering the alloy components to the electrode. The latter is melted off by an induction coil. JP 02277736 A discloses a heat-resistant TiAl-based alloy in which specific amounts of V and Cr are introduced into an intermetallic Ti-Al compound to improve heat resistance and ductility.
Die DE 1 179 006 A schließlich offenbart ternäre oder höhere Titan- Aluminium- Legierungen mit solchen Elementen, die die a- und ß-Phase des Titans stabilisieren. Übliches Verfahren zum Umschmelzen ist das Vakuum-Lichtbogen- Schmelzen mit selbstverzehrender Elektrode, da die Anlagen zum Plasma- Schmelzen in der Regel nicht für die Zuführung von kompakten Ingots als Ausgangsmaterial ausgelegt sind. Im Falle von herkömmlichen, zweiphasig in Form lamellarer Kolonien aus der a2-Ti3Al-Phase und der γ-TiAl-Phase aufgebauten γ-TiAl-Basislegierungen geschieht das Umschmelzen im Vakuum-Lichtbogen-Schmelzofen (VAR-Ofen) problemlos und führt zum gewünschten Ergebnis (s. V. Guether:„Status and Prospects of γ-TiAl In- got Production", Int. Symp. on Gamma Titanium Aluminides 2003, Hrsg. H. Clemens, Y.-W. Kim and A.H. Rosenberger, San Diego, TMS 2004). Finally, DE 1 179 006 A discloses ternary or higher titanium-aluminum alloys with such elements which stabilize the α- and β-phase of the titanium. The usual process for remelting is vacuum-arc melting with self-consuming electrode, since the plasma melting plants are generally not designed for the supply of compact ingots as starting material. In the case of conventional, biphasic in the form of lamellar colonies of the a2-Ti 3 Al phase and the γ-TiAl phase constructed γ-TiAl base alloys remelting takes place in the vacuum arc furnace (VAR furnace) easily and leads to the desired result (see V. Guether: "Status and Prospects of γ-TiAl Intote Production", International Symp. on Gamma Titanium Aluminides 2003, ed. H. Clemens, Y.-W. Kim and AH Rosenberger, San Diego, TMS 2004).
Eine neue Generation von γ-TiAl-Hochleistungswerkstoffen, z.B. die so bezeichneten TNM®-Legierungen der Anmelderin, besitzt einen von herkömmlichen TiAl-Legierungen abweichenden strukturellen Aufbau. Insbesondere aufgrund der Absenkung des Aluminium-Gehaltes auf üblicher- weise 40 at.-% bis 45,5 Atom-%, aber auch aufgrund des Zulegierens von ß-stabilisierenden Elementen wie beispielsweise Cr, Cu, Hf, Mn, Mo, Nb, V, Ta und Zr wird ein primärer Erstarrungspfad über die ß-Ti-Phase eingestellt. Es entstehen dadurch sehr feine Gefüge, die neben lamellaren α2/γ- Kolonien auch globulare ß -Körner und globulare γ-Körner, mitunter auch globulare 012-Körner enthalten. Werkstoffe mit derartigen Gefügen besitzen entscheidende Vorteile bezüglich der thermo-mechanischen Eigenschaften und der Prozessierbarkeit mittels Umformtechnologien (s. H. Clemens: „Design of Novel ß-Solidifying TiAl Alloys with Adjustable ß/B2-Phase Fraction and Excellent Hot-Workability", Advanced Engineering Materials 2008, 10, No.8, p. 707-713). Derartige Legierungen werden - wie eingangs bereits festgehalten - im Folgenden als β-γ-TiAl-Basislegierungen bezeichnet. A new generation of γ-TiAl high performance materials, such as Applicant's designated TNM® alloys, has a structural design different from conventional TiAl alloys. In particular, due to the lowering of the aluminum content to usually 40 at .-% to 45.5 atom%, but also due to the addition of ß-stabilizing elements such as Cr, Cu, Hf, Mn, Mo, Nb, V , Ta and Zr, a primary solidification path is established over the β-Ti phase. This results in very fine microstructures, in addition to lamellar α 2 / γ- Colonies also include globular β grains and globular γ grains, sometimes including globular 012 grains. Materials with such structures have significant advantages in terms of thermo-mechanical properties and processability by means of forming technologies (see H. Clemens: "Design of Novel ß-Solidifying TiAl Alloys with Adjustable ß / B2 Phase Fraction and Excellent Hot Workability", Advanced Engineering Materials 2008, 10, No.8, pp. 707-713) Such alloys are referred to below as β-γ-TiAl base alloys, as already stated above.
Nachteilig ist, dass es beim erneuten Umschmelzen von Elektroden aus diesem Material im VAR-Ofen zu Rissbildungen kommt, deren Resultat häufig das Abplatzen von Bestandteilen der selbstverzehrenden Legierungselektrode aus der Erstschmelzzone ist. Diese abgeplatzten Teile fallen in das Schmelzbad und werden darin nicht mehr vollständig wieder aufgeschmolzen. Dadurch entstehen strukturelle Defekte im Ingot, wodurch das Ingotmaterial unbrauchbar wird. Das Umschmelzen im VAR-Ofen ist unter diesen Verhältnissen nicht mehr technisch reproduzierbar möglich. Als Ursache für das störende Abplatzverhalten werden massive Phasenumwandlungen im Temperaturbereich zwischen der eutektoiden Temperatur und der Phasengrenztemperatur zum ß -Einphasengebiet angesehen. Durch die unterschiedlichen linearen Ausdehnungskoeffizienten der verschiedenen Phasenbestandteile kommt es insbesondere bei Phasenumwand- lungen zu sprungartigen Veränderungen des integralen linearen Wärmeausdehnungskoeffizienten der Legierung und als Folge davon zu inneren Spannungen, die die Festigkeit des Materials im gegebenen Temperaturbereich übersteigen. Entsprechende Dilatometermessungen an einer TNM -Bl -Legierung (Ti - 43,5A1 - 4,0Nb - Ι,ΟΜο - Ο,ΙΒ at.-%) zeigen, dass sich der lineare Ausdehnungskoeffizient einer entsprechenden Legierungsprobe im Tempe- raturintervall zwischen 1.000 °C und 1.200°C von 9 x 10"6 auf 40 x 10"6 K"1 mehr als vervierfacht. Dieses Verhalten ist in der beigefügten Fig. 4 dargestellt, in der die Kurve A den linearen Ausdehnungskoeffizienten dieser Legierung wiedergibt. Die Kurve stellt die Aufheizrate der Probe dar. Während des VAR- Schmelzens zieht sich bezogen auf die Länge der selbstverzehrenden Elektrode ein Temperaturfeld von Schmelztemperatur (ca. 1570 °C) an der Elektrodenunterseite bis nahezu Raumtemperatur an der Elektrodenaufhängung durch das Material. Unweit der Schmelzfront wird das kritische Temperaturintervall zwischen 1000 und 1200 °C er- reicht. Die relativ schlechte Duktilität des intermetallischen Werkstoffes führt dann in dieser Zone dazu, dass sich die dort bildenden Spannungen in Form von Rissen entladen, die wiederum zu dem geschilderten Abplatzen von ungeschmolzenen Stücken von der Elektrode führen. Ausgehend von dieser geschilderten Problematik des Standes der Technik liegt der Erfindung die Aufgabe zugrunde, ein Verfahren zur Herstellung einer über die ß-Phase erstarrenden γ-TiAl-Basislegierung - im Folgenden kurz als β-γ-TiAl-Basislegierung bezeichnet - anzugeben, dass unter Umgehung der Rissbildungsproblematik zu einer zuverlässigen Produktion einer solchen Ziellegierung führt. The disadvantage is that cracking occurs again during the remelting of electrodes from this material in the VAR furnace, the result of which is frequently the flaking off of constituents of the self-consumable alloy electrode from the primary melting zone. These chipped parts fall into the molten bath and are no longer completely remelted therein. This causes structural defects in the ingot, making the ingot material unusable. Remelting in the VAR furnace is no longer technically reproducible under these conditions. The cause of the disturbing chipping behavior is considered to be massive phase transformations in the temperature range between the eutectoid temperature and the phase boundary temperature to the β-phase region. Due to the different linear expansion coefficients of the various phase components, in particular during phase transformations, sudden changes in the integral linear thermal expansion coefficient of the alloy and, as a consequence, internal stresses which exceed the strength of the material in the given temperature range occur. Corresponding dilatometer measurements on a TNM-B1 alloy (Ti - 43.5A1 - 4.0Nb - Ι, ΟΜο - Ο, ΙΒ at .-%) show that the linear expansion coefficient of a corresponding alloy sample in the temperature range between 1000 ° C and 1200 ° C of 9 x 10 "6 to 40 x 10" 6 K "1 more than quadrupled. this behavior is illustrated in the accompanying Fig. 4, in which the curve A represents the linear expansion coefficient of this alloy. the curve represents the During VAR melting, based on the length of the self-consumable electrode, a temperature field extends from the melting temperature (about 1570 ° C.) at the bottom of the electrode to near room temperature at the electrode suspension between 1000 and 1200 ° C. The relatively poor ductility of the intermetallic material then leads in this zone to the formation of the S Tear discharges in the form of cracks, which in turn lead to the described chipping of unmelted pieces of the electrode. Based on this described problem of the prior art, the present invention seeks to provide a method for producing a solidifying over the β-phase γ-TiAl base alloy - hereinafter referred to as β-γ-TiAl base alloy - specify that Avoiding the cracking problem leads to a reliable production of such a target alloy.
Diese Aufgabe wird durch die im Patentanspruch 1 angegebenen Verfahrensschritte wie folgt gelöst: - Erschmelzen einer Basisschmelzelektrode einer herkömmlichen γ- TiAl-Primärlegierung mit einem defizitären Gehalt an Titan und/oder an mindestens einem ß -stabilisierenden Element gegenüber der herzustellenden β-γ-TiAl-Basislegierung in mindestens einem ersten Vakuum-Lichtbogen-Umschmelzschritt, This object is achieved by the method steps indicated in claim 1 as follows: Melting a base melt electrode of a conventional γ-TiAl primary alloy with a deficient content of titanium and / or on at least one β-stabilizing element in relation to the β-γ-TiAl base alloy to be produced in at least one first vacuum arc remelting step,
- Zuordnen einer dem defizitären Gehalt des Titans und/oder ß- stabilisierenden Elements entsprechenden Menge an Titan und/oder ß-stabilisierendem Element zur Basisschmelzelektrode in gleichmäßiger Verteilung über deren Länge und Umfang, und - Assigning a deficient content of the titanium and / or ß-stabilizing element corresponding amount of titanium and / or ß-stabilizing element to the base melt electrode in a uniform distribution over the length and circumference, and
- Zulegieren der zugeordneten Menge des Titans und/oder ß- stabilisierenden Elements in die Basisschmelzelektrode zur Bildung der homogenen β-γ-TiAl-Basislegierung in einem letzten Vakuum- Lichtbogen-Schmelzschritt. - Adding the associated amount of the titanium and / or ß-stabilizing element in the base melt electrode to form the homogeneous β-γ-TiAl-based alloy in a last vacuum arc melting step.
Die aufeinanderfolgenden Umschmelzschritte während des Vakuum- Lichtbogen- Schmelzens werden also unterteilt in das Schmelzen einer Pri- mär-Legierung in den ersten Umschmelzschritten, wobei eine Basisschmelzelektrode aus einer herkömmlichen γ-TiAl-Primärlegierung hergestellt wird, und das Schmelzen der Ziellegierung in Form der gewünschten β-γ-TiAl-Basislegierung im jeweils letzten Umschmelzschritt. Die Primärlegierung besitzt ein Defizit an Titan und/oder ein Defizit an ß- stabilisierenden Elementen wie z.B. Nb, Mo, Cr, Mn, V, und Ta. Dabei wird der Legierung beim Herstellen der gepressten Basisschmelzelektrode eine definierte Menge an Titan und/oder ß -stabilisierenden Elementen entzogen, so dass sich ein Aluminium-Gehalt der Primärlegierung vorzugsweise zwischen 45 at.-% (besonders bevorzugt 45,5 at.-%) und 50 at.-% einstellt. Die Gehalte an Aluminium und an ß -stabilisierenden Elementen werden so gewählt, dass der Erstarrungsweg der Primärlegierung zumindest teilweise über die peritektische Umwandlung erfolgt. Es wird damit ein Gefüge analog zu konventionellen TiAl Legierungen eingestellt, das sich problemlos im VA -Ofen prozessieren lässt. The successive remelting steps during the vacuum arc melting are thus subdivided into the melting of a primary alloy in the first remelting steps, wherein a base melt electrode is produced from a conventional γ-TiAl primary alloy, and the melting of the target alloy in the form of the desired β-γ-TiAl base alloy in the last remelting step. The primary alloy has a deficit of titanium and / or a deficiency of ß-stabilizing elements such as Nb, Mo, Cr, Mn, V, and Ta. In the production of the pressed base melt electrode, the alloy is a defined amount of titanium and / or ß deprived of stabilizing elements, so that an aluminum content of the primary alloy preferably between 45 at .-% (particularly preferably 45.5 at .-%) and 50 at .-% sets. The contents of aluminum and ß-stabilizing elements are chosen so that the solidification path of the primary alloy is at least partially via the peritectic conversion. It is thus set a structure analogous to conventional TiAl alloys, which can be processed easily in VA oven.
Im letzten Schmelzschritt wird durch die Zugabe der ursprünglich der Presselektrode entzogenen Materialien die Ziellegierung wieder eingestellt. Vorzugsweise werden diese Materialien als Mantel unter Bildung einer Komposit-Elektrode fest auf die Mantelfläche der Abschmelzelektrode aufgeschweißt, um ein Abfallen im festen Zustand in das Schmelzbad sicher auszuschließen. Auch ist es möglich, dies durch eine Manteleinlage des defizitären Legierungsanteils an der Innenseite der Umschmelzkokille des VAR-Ofens zu bewerkstelligen. Überraschenderweise zeigt sich, dass sich bei geeigneter Auswahl und geeignet gleichverteiltem Anbringen der defizitären Legierungsbestandteile auf der Elektrodenmantelfläche keine negativen Folgen für die lokale chemische Homogenität des entstehenden Ingots der herzustellenden β-γ-ΤιΑ1- Basislegierung als Ziellegierung ergeben. In the last melting step, the target alloy is readjusted by the addition of the materials originally removed from the press electrode. Preferably, these materials are welded as cladding to form a composite electrode firmly on the outer surface of the Abschmelzelektrode to safely exclude a solid state drop into the molten bath. It is also possible to accomplish this by a sheath insert of the deficient alloy content on the inside of the Umschmelzkokille the VAR furnace. Surprisingly, it has been found that, with a suitable selection and suitably evenly distributed attachment of the deficient alloy constituents on the electrode jacket surface, there are no negative consequences for the local chemical homogeneity of the resulting ingot of the produced β-γ-ιιι1 base alloy as target alloy.
Weitere bevorzugte Ausführungsformen des erfindungsgemäßen Herstellungsverfahrens sind in weiteren Unteransprüchen angegeben, deren Einzelheiten und Merkmale sich aus der nachfolgenden Beschreibung von Ausführungsbeispielen anhand der beigefügten Zeichnungen ergeben. Es zeigen: Further preferred embodiments of the manufacturing method according to the invention are specified in further subclaims, whose details and features will become apparent from the following description of embodiments with reference to the accompanying drawings. Show it:
Fig.l eine Prinzipskizze eines Vakuum-Lichtbogen-Schmelzofens, Fig. 2 eine perspektivische Ansicht einer Komposit-Elektrode in einer ersten Ausführungsform, 1 is a schematic diagram of a vacuum arc melting furnace, 2 is a perspective view of a composite electrode in a first embodiment,
Fig. 3 eine perspektivische Ansicht einer Komposit-Elektrode in einer zweiten Ausführungsform und Fig. 3 is a perspective view of a composite electrode in a second embodiment and
Fig. 4 ein Diagramm des linearen Ausdehnungskoeffizienten als Fig. 4 is a diagram of the linear expansion coefficient as
Funktion der Temperatur einer TNM®-B 1 -Legierung. Anhand von Fig. 1 soll grundsätzlich ein Vakuum-Lichtbogen- Schmelzofen 1 und das Verfahren zum Umschmelzen einer entsprechenden Elektrode 2 zu einem Ingot 3 erläutert werden. So weist der VAR-Ofen 1 einen Kupfertiegel 4 mit einer Bodenplatte 5 auf. Um diesen Kupfertiegel 4 herum ist ein Wasserkühlmantel 6 mit Wasserzulauf 7 und Wasserablauf 8 angeordnet. Der Kupfertiegel 4 ist ferner oben von einer Vakuumglocke 9 abgeschlossen, durch die an der Oberseite eine Hebestange 10 vertikal verschiebbar durchgreift. An dieser Hebestange 10 sitzt der Halter 1 1, an dem die eigentliche Elektrode 2 aufgehängt ist. Über eine Gleichstromversorgung 12 wird zwischen Kupfertiegel 4 und Hebestange 10 eine Gleichspannung angelegt, aufgrund derer ein Hochstrom-Lichtbogen zwischen der mit der Hebestange 10 elektrisch verbundenen Elektrode 2 und dem Kupfertiegel 4 gezündet und aufrecht erhalten wird. Dieser führt zum Abschmelzen der Elektrode 2, wobei sich das abge- schmolzene Legierungsmaterial im Kupfertiegel 4 sammelt und dort erstarrt. In einem kontinuierlichen Prozess, bei dem zwischen der sich selbst verzehrenden Elektrode 2 über den Elektrodenlichtbogenspalt 13 der Lichtbogen zum geschmolzenen Reservoir 14 an der Oberseite des Ingots 3 läuft, wird die Elektrode 2 sukzessive zum Ingot 3 unter Homogenisierung der Legierungsbestandteile umgeschmolzen. Function of the temperature of a TNM®-B 1 alloy. 1, a vacuum arc melting furnace 1 and the method for remelting a corresponding electrode 2 to form an ingot 3 will be explained in principle. Thus, the VAR furnace 1 has a copper crucible 4 with a bottom plate 5. Around this copper crucible 4 around a water jacket 6 with water inlet 7 and 8 water outlet is arranged. The copper crucible 4 is also closed at the top of a vacuum bell 9, passes through the top of a lifting bar 10 vertically displaceable. At this lifting bar 10 sits the holder 1 1, where the actual electrode 2 is suspended. Via a DC power supply 12, a DC voltage is applied between the copper crucible 4 and the lifting rod 10, due to which a high-current arc is ignited and maintained between the electrode 2 electrically connected to the lifting rod 10 and the copper crucible 4. This leads to the melting of the electrode 2, wherein the molten alloy material collects in the copper crucible 4 and solidifies there. In a continuous process in which, between the self-consuming electrode 2 via the electrode arc gap 13, the arc to the molten reservoir 14 at the top of the ingot 3 runs, the electrode 2 is successively remelted to ingot 3 under homogenization of the alloy components.
Dieser Vorgang kann mit im Durchmesser jeweils größeren Schmelztiegeln 4 mehrfach wiederholt werden, wobei der Ingot des einen Umschmelz- schrittes zur Elektrode des nächsten Umschmelzschrittes wird. Damit wird der Homogenisierungsgrad der herzustellenden Ingots mit jedem Um- schmelzschritt verbessert. Im Folgenden werden nun verschiedene Ausführungsbeispiele zur Herstellung einer β-γ-TiAl-Basislegierung beschrieben: This process can be repeated several times with larger diameter crucibles 4, wherein the ingot of a Umschmelz- step becomes the electrode of the next Umschmelzschrittes. This improves the degree of homogenization of the ingots to be produced with each remelting step. Various embodiments for producing a β-γ-TiAl base alloy will now be described below:
Ausführungsbeispiel 1 Die Zielzusammensetzung der β-γ-TiAl-Legierung ist Ti - 43,5A1 - 4,0Nb - Ι,ΟΜο - 0,1B (at.-%) bzw. Ti - A128,6 - Nb9,l - Mo2,3 - B0,03 (m-%). Die Zusammensetzung der Primärlegierung für die Basisschmelzelektrode wird durch eine Reduktion des Titangehaltes auf Ti - 45,93A1 - 4,22Nb - l,06Mo - 0,1 1B (at.-%) festgelegt. Zunächst wird konventionell aus einer Presselektrode 2 ein Ingot 3 der Primärlegierung mit 200 mm Durchmesser und einer Länge von 1 ,4 m durch 2-faches VAR-Schmelzen wie oben beschrieben hergestellt, ohne dass eine Rissproblematik auftritt. Als Einsatzmaterialien für die Herstellung der Presselektrode 2 werden Titan- Schwamm, Rein- Aluminium und Vorlegierungen verwendet. Exemplary Embodiment 1 The target composition of the β-γ-TiAl alloy is Ti - 43.5A1 - 4.0Nb - Ι, ΟΜο - 0.1B (at .-%) or Ti - A128.6 - Nb9, l - Mo2, 3 - B0.03 (m-%). The composition of the primary alloy for the base melt electrode is determined by a reduction of the titanium content to Ti - 45.93A1 - 4.22Nb - l, 06Mo - 0.1 1B (at .-%). First, conventionally, a ingot 3 of the primary alloy of 200 mm in diameter and a length of 1.4 m by 2-fold VAR melting as described above is produced from a pressing electrode 2, without the occurrence of a cracking problem. As starting materials for the production of the pressing electrode 2 titanium sponge, pure aluminum and master alloys are used.
Um den reduzierten Titangehalt in der Basisschmelzelektrode auf den gewünschten Wert der β-γ-TiAl-Legierung in der Ziellegierung anzuheben, wird die gesamte Mantelfläche des Ingots 3 aus der Primärlegierung ein Rein-Titanblech 15 mit einer Dicke von 3 mm (Masse 12 kg) gewickelt und teilweise mit der Mantelfläche 16 des Ingots 3 verschweißt, wie dies in Fig. 2 dargestellt ist. Dabei wird die obere Kante 17 des Titanbleches 15 vollständig über den Umfang des Ingots 3 mit diesem verschweißt. Ferner werden Schweißpunkte 18 über die Mantelfläche 16 verteilt gesetzt. Die so zusammengebaute selbstverzehrende Elektrode wird als Komposit- Elektrode 19 in einem letzten Schmelzschritt im VAR-Ofen 1 zu einem Ingot 3 mit einem Durchmesser von 280 mm und der Zusammensetzung der Ziellegierung umgeschmolzen. In order to raise the reduced titanium content in the base melt electrode to the desired value of the β-γ-TiAl alloy in the target alloy, the entire surface area of the ingot 3 becomes of the primary alloy Pure titanium sheet 15 with a thickness of 3 mm (mass 12 kg) wound and partially welded to the lateral surface 16 of the ingot 3, as shown in Fig. 2. In this case, the upper edge 17 of the titanium sheet 15 is completely welded over the circumference of the ingot 3 with this. Furthermore, weld spots 18 are set distributed over the lateral surface 16. The thus assembled self-consumable electrode is remelted as a composite electrode 19 in a final melting step in the VAR furnace 1 to a ingot 3 with a diameter of 280 mm and the composition of the target alloy.
Ausführungsbeispiel 2 Embodiment 2
Die Zielzusammensetzung, die verwendeten Einsatzmaterialien und die Zusammensetzung der Primärlegierung entsprechen dem Ausführungsbei- spiel 1. Aus der Primärlegierung wird durch einfaches VAR-Schmelzen von Presselektroden 2 ein Ingot 3 mit einem Durchmesser von 140 mm und einer Länge von 1,8 m hergestellt. Die Masse des Ingots beträgt 1 15 kg. In die vom Kupfertiegel 4 gebildete Kokille des VAR-Ofens 1 wird vor der letzten Schmelze des der Basisschmelzelektrode 2 ein Blech aus Rein-Titan mit den Abmessungen Umfang 628 mm x Höhe 880 mm x Dicke 3 mm (Masse 7,6 kg) in die innere Mantelfläche eingelegt. In Summe ergibt sich somit aus der Zusammensetzung des die Basisschmelzelektrode 2 bildenden Primärlegierungsingots und dem Titanblech die Zielzusammensetzung. Die Umschmelze erfolgt in den mit dem Titanblech ausgekleideten Kupfer- tiegel 4 zu einer Zwischenelektrode derart, dass die Außenhaut des Titanblechs nicht vollständig mit aufgeschmolzen wird und als stabile Hülle bestehen bleibt. Im nachfolgenden letzten VAR-Umschmelzschritt der Zwischenelektrode kann es zwar zu Rissbildungen kommen, die aber aufgrund der mechanischen Stabilisierung durch die duktile Außenhülle nicht zu ei- nem Herunterfallen von Elektrodenmaterial in das Schmelzreservoir 14 führen. The target composition, the feeds used and the composition of the primary alloy correspond to the exemplary embodiment 1. From the primary alloy, an ingot 3 having a diameter of 140 mm and a length of 1.8 m is produced by simple VAR melting of press electrodes 2. The mass of the ingot is 1 15 kg. In the mold formed by the copper crucible 4 of the VAR furnace 1 is before the last melt of the base melt electrode 2, a sheet of pure titanium with the dimensions circumference 628 mm x height 880 mm x thickness 3 mm (mass 7.6 kg) in the inserted inner surface. In sum, the composition of the primary alloy ingot forming the base melt electrode 2 and the titanium sheet thus provide the target composition. The remelting takes place in the copper plate 4 lined with the titanium sheet to form an intermediate electrode in such a way that the outer skin of the titanium sheet is not completely melted with it and remains as a stable shell. In the following last VAR remelting step of the intermediate electrode, cracking may occur, but due to the mechanical stabilization by the ductile outer shell, this does not result in cracking. Drop down of electrode material in the melt reservoir 14 lead.
Ausführungsbeispiel 3 Embodiment 3
Die Zielzusammensetzung, die verwendeten Einsatzmaterialien und die Zusammensetzung der Primärlegierung entsprechen dem Ausführungsbeispiel 1, ebenfalls die Herstellung der Komposit-Elektrode 19. Im Unterschied zu Ausführungsbeispiel 1 erfolgt deren letztes Umschmelzen in ei- nem sogenannten ,VAR skull melter', also einer Vakuum-Lichtbogen- Schmelzeinrichtung mit einem wassergekühlten, kippbaren Schmelztiegel aus Kupfer. Das im , skull' befindliche schmelzflüssige Material der Ziellegierung wird in Permanentkokillen aus Edelstahl abgegossen, die an einem rotierenden Gießrad angebracht sind. Die so im Schleuderguss hergestell- ten Gießkörper werden als Vormaterial für die Herstellung von Bauteilen aus der Ziellegierung verwendet. The target composition, the starting materials used and the composition of the primary alloy correspond to the embodiment 1, likewise the production of the composite electrode 19. In contrast to embodiment 1, the last remelting takes place in what is known as a VAR skull melter, ie a vacuum arc - Melting device with a water-cooled, tiltable crucible made of copper. The target material's molten alloy material is poured into permanent molds made of stainless steel, which are attached to a rotating casting wheel. The casting bodies thus produced by centrifugal casting are used as starting material for the production of components from the target alloy.
Ausführungsbeispiel 4: Eine β-γ-TiAl Legierung gemäß US Patent 6,669,791 besitzt eine Zusammensetzung (Ziellegierung) Ti - 43,0A1 - 6,0V (at.-%) bzw. Ti - A129,7 - V7,8 (m-%). Die Zusammensetzung der Primärlegierung wird durch die vollständige Reduktion des stark ß -stabilisierenden Elementes Vanadium auf Ti - 45J5A1 (at.-%) bzw. Ti - A132,2 (m-%) festgelegt. Als Einsatzma- terialien werden Titan-Schwamm, Aluminium und Vanadium verwendet. Zunächst wird konventionell eine Basisschmelzelektrode 2 als Ingot der binären TiAl-Primärlegierung mit einem Durchmesser von 200 mm und einer Länge von 1 m durch zweifaches VAR-Schmelzen hergestellt (Masse 126 kg). Wie Fig. 3 zeigt, werden entlang der gesamten Mantelfläche 16 der Basisschmelzelektrode 2 längsaxialparallel acht Vanadiumstäbe 20 mit einem Durchmesser von 16,7 mm und einer Länge von 1 m (Masse insgesamt 10,7 kg) jeweils um 45° zueinander versetzt und damit gleichmäßig über den Umfang der Elektrode 2 verteilt aufgeschweißt. Die so entstandene Komposit-Elektrode 19' aus der binären Primärlegierung und den aufgeschweißten Vanadiumstäben 20 wird im abschließenden dritten Exemplary Embodiment 4: A β-γ-TiAl alloy according to US Pat. No. 6,669,791 has a composition (target alloy) Ti-43,0A1-6,0V (at.%) Or Ti-A129,7-V7,8 (m-%). ). The composition of the primary alloy is determined by the complete reduction of the strongly β-stabilizing element vanadium to Ti-45J5A1 (at .-%) or Ti-A132.2 (m-%). As insert materials titanium sponge, aluminum and vanadium are used. First, conventionally, a base melt electrode 2 is prepared as an ingot of the binary TiAl primary alloy having a diameter of 200 mm and a length of 1 m by double VAR melting (mass 126 kg). As shown in FIG. 3, eight vanadium rods 20 with a diameter of 16.7 mm and a length of 1 m (total mass 10.7 kg) are each offset by 45 ° relative to one another along the entire lateral surface 16 of the base melt electrode 2, and thus uniformly welded over the circumference of the electrode 2 welded. The resulting composite electrode 19 'from the binary primary alloy and the welded vanadium rods 20 is in the final third
Schmelzprozess zu einem Ingot der Ziellegierung mit einem Durchmesser von 300 mm im VAR-Ofen 1 umgeschmolzen. Melting process to an ingot of target alloy with a diameter of 300 mm in the VAR furnace 1 remelted.
Ausführungsbeispiel 5 Embodiment 5
Die Zielzusammensetzung der γ-TiAl-Legierung entspricht der des Ausführungsbeispiels 1 (Ti - 43,5A1 - 4,0Nb - Ι,ΟΜο - 0,1B at.-%). Die Zu- sammensetzung der Primärlegierung wird durch eine vollständige Reduktion des Molybdängehaltes und eine teilweise Reduktion des Titangehaltes auf Ti - 49,63A1 - 4,57Nb - 0,1 1B (at.-%) festgelegt. Aus der Primärlegierung wird durch zweifaches VAR-Schmelzen eine Basisschmelzelektrode 2 mit einem Durchmesser von 200 mm und einer Länge von 1 m hergestellt. Die Ingotmasse beträgt 126 kg. Auf die Mantelfläche 16 der Elektrode 2 werden analog zu Ausführungsbeispiel 4 längsaxialparallel acht Stäbe aus der kommerziellen Legierung TiMol5 aufgeschweißt. Der Durchmesser der Stäbe beträgt 26 mm, die Länge der Stäbe entspricht der Ingotlänge. Die Gesamtmasse der TiMol5 Stäbe beträgt 19,6 kg. Die so entstandene Komposit-Elektrode aus einem Ingot der Primärlegierung und acht TiMol5 Stäben wird im abschließenden dritten Schmelzprozess zu einem Ingot der Ziellegierung mit einem Durchmesser von 300 mm im VAR-Ofen 1 umgeschmolzen. The target composition of the γ-TiAl alloy corresponds to that of Embodiment 1 (Ti - 43.5A1 - 4.0Nb - Ι, ΟΜο - 0.1B at .-%). The composition of the primary alloy is determined by a complete reduction of the molybdenum content and a partial reduction of the titanium content to Ti - 49.63A1 - 4.57Nb - 0.1 1B (at .-%). From the primary alloy, a base melt electrode 2 having a diameter of 200 mm and a length of 1 m is produced by double VAR melting. The ingot mass is 126 kg. On the lateral surface 16 of the electrode 2, eight rods made of the commercial TiMol5 alloy are welded on, parallel to the longitudinal axis parallel to exemplary embodiment 4. The diameter of the rods is 26 mm, the length of the rods corresponds to the ingot length. The total mass of the TiMol5 rods is 19.6 kg. The resulting composite electrode consisting of one ingot of the primary alloy and eight TiMol5 rods is remelted in the final third melting process to an ingot of the target alloy with a diameter of 300 mm in the VAR furnace 1.
Claims
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE102009050603A DE102009050603B3 (en) | 2009-10-24 | 2009-10-24 | Process for producing a β-γ-TiAl base alloy |
| PCT/EP2010/064306 WO2011047937A1 (en) | 2009-10-24 | 2010-09-28 | Method for producing a ss-γ-tial base alloy |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| EP2342365A1 true EP2342365A1 (en) | 2011-07-13 |
| EP2342365B1 EP2342365B1 (en) | 2013-03-06 |
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| EP10765988A Not-in-force EP2342365B1 (en) | 2009-10-24 | 2010-09-28 | Process for manufacturing a beta-gamma tial-based alloy |
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| US (1) | US8668760B2 (en) |
| EP (1) | EP2342365B1 (en) |
| JP (1) | JP5492982B2 (en) |
| CN (1) | CN102449176B (en) |
| DE (1) | DE102009050603B3 (en) |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102312111B (en) * | 2011-09-07 | 2013-02-06 | 上海交通大学 | Method for Melting TiAl Alloy Using Vacuum Consumable Electric Arc Furnace |
| JP2015526625A (en) * | 2012-05-16 | 2015-09-10 | ゲーコーエヌ エアロスペース スウェーデン アーベー | Method of applying a titanium alloy on a substrate |
| JP5857917B2 (en) * | 2012-08-28 | 2016-02-10 | 新日鐵住金株式会社 | Ni-base superalloy ingot manufacturing method |
| CN103014386B (en) * | 2012-12-10 | 2014-07-09 | 西安诺博尔稀贵金属材料有限公司 | Preparation method of niobium-tungsten-molybdenum-zirconium alloy ingot |
| CN103276229A (en) * | 2013-06-06 | 2013-09-04 | 广西大学 | Melting method for minimizing aluminium burning loss during melting process of high-temperature structural material Ti-40Al-10Fe alloys |
| EP2851445B1 (en) * | 2013-09-20 | 2019-09-04 | MTU Aero Engines GmbH | Creep-resistant TiAl alloy |
| KR101852697B1 (en) * | 2013-10-23 | 2018-04-26 | 비와이디 컴퍼니 리미티드 | Metal forming apparatus |
| CN104532061A (en) * | 2014-12-26 | 2015-04-22 | 北京科技大学 | High-temperature-resistant aluminum titanium oxide alloy and preparation method thereof |
| DE102015103422B3 (en) * | 2015-03-09 | 2016-07-14 | LEISTRITZ Turbinentechnik GmbH | Process for producing a heavy-duty component of an alpha + gamma titanium aluminide alloy for piston engines and gas turbines, in particular aircraft engines |
| CN104976888B (en) * | 2015-06-08 | 2017-03-08 | 重庆钢铁(集团)有限责任公司 | A vacuum consumable smelting furnace |
| DE102015115683A1 (en) * | 2015-09-17 | 2017-03-23 | LEISTRITZ Turbinentechnik GmbH | A method for producing an alpha + gamma titanium aluminide alloy preform for producing a heavy duty component for reciprocating engines and gas turbines, in particular aircraft engines |
| RU2621500C1 (en) * | 2015-12-21 | 2017-06-06 | Федеральное государственное автономное образовательное учреждение высшего образования "Национальный исследовательский технологический университет "МИСиС" | INTERMETALLIC TiAl BASED ALLOY |
| CN107385370B (en) * | 2017-06-23 | 2019-04-05 | 太原理工大学 | Ti-44Al-4Nb-4V-0 ﹒ 3Mo alloy grain refining heat treatment method |
| KR102095463B1 (en) | 2018-05-24 | 2020-03-31 | 안동대학교 산학협력단 | TiAl-BASED ALLOY HAVING EXCELLENT HIGH-TEMPERATURE FORMABILITY AND METHOD FOR MANUFACTURING TiAl-BASED ALLOY MEMBER USING THE SAME |
| CN110814481B (en) * | 2019-10-30 | 2021-07-13 | 西部超导材料科技股份有限公司 | Butt welding method of auxiliary electrode for titanium alloy |
| CN113234960A (en) * | 2021-05-08 | 2021-08-10 | 陕西工业职业技术学院 | Preparation method of alloy |
| CN113351838B (en) * | 2021-05-17 | 2022-11-04 | 西部超导材料科技股份有限公司 | Gas cooling device, control system and control method for preparing titanium alloy ingots |
| CN116334443B (en) * | 2023-02-16 | 2025-05-30 | 鞍钢集团北京研究院有限公司 | A β-solidified γ-TiAl high-temperature titanium alloy and a preparation method thereof |
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| DE1179006B (en) * | 1952-12-18 | 1964-10-01 | Crucible Steel Internat | Titanium alloys |
| JPH02277736A (en) * | 1989-04-19 | 1990-11-14 | Mitsubishi Heavy Ind Ltd | Ti-al base heat-resistant alloy |
| US5332545A (en) * | 1993-03-30 | 1994-07-26 | Rmi Titanium Company | Method of making low cost Ti-6A1-4V ballistic alloy |
| US6051084A (en) * | 1994-10-25 | 2000-04-18 | Mitsubishi Jukogyo Kabushiki Kaisha | TiAl intermetallic compound-based alloys and methods for preparing same |
| DE19631583C2 (en) * | 1996-08-05 | 2002-10-02 | Geesthacht Gkss Forschung | Process for the manufacture of an alloy product |
| JP4287991B2 (en) | 2000-02-23 | 2009-07-01 | 三菱重工業株式会社 | TiAl-based alloy, method for producing the same, and moving blade using the same |
| DE10156336A1 (en) * | 2001-11-16 | 2003-06-05 | Ald Vacuum Techn Gmbh | Process for the production of alloy ingots |
| RU2269584C1 (en) * | 2004-07-30 | 2006-02-10 | Открытое Акционерное Общество "Корпорация Всмпо-Ависма" | Titanium-base alloy |
| DE102007060587B4 (en) * | 2007-12-13 | 2013-01-31 | Helmholtz-Zentrum Geesthacht Zentrum für Material- und Küstenforschung GmbH | titanium aluminide |
| CN101476061B (en) * | 2009-02-06 | 2010-08-25 | 洛阳双瑞精铸钛业有限公司 | High temperature resistant titanium and aluminum based alloy and manufacturing method thereof |
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| JP5492982B2 (en) | 2014-05-14 |
| CN102449176B (en) | 2014-04-16 |
| US20110219912A1 (en) | 2011-09-15 |
| WO2011047937A1 (en) | 2011-04-28 |
| DE102009050603B3 (en) | 2011-04-14 |
| ES2406904T3 (en) | 2013-06-10 |
| US8668760B2 (en) | 2014-03-11 |
| JP2012527533A (en) | 2012-11-08 |
| CN102449176A (en) | 2012-05-09 |
| RU2011143579A (en) | 2013-05-10 |
| EP2342365B1 (en) | 2013-03-06 |
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