EP3706934A1 - Vorrichtung und verfahren zur herstellung eines metalllegierungsrohlings durch schleudergiessen - Google Patents

Vorrichtung und verfahren zur herstellung eines metalllegierungsrohlings durch schleudergiessen

Info

Publication number
EP3706934A1
EP3706934A1 EP18804376.4A EP18804376A EP3706934A1 EP 3706934 A1 EP3706934 A1 EP 3706934A1 EP 18804376 A EP18804376 A EP 18804376A EP 3706934 A1 EP3706934 A1 EP 3706934A1
Authority
EP
European Patent Office
Prior art keywords
rotation
metal alloy
axis
mold
centrifugal casting
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
EP18804376.4A
Other languages
English (en)
French (fr)
Other versions
EP3706934B1 (de
Inventor
Laurent Ferrer
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Safran Aircraft Engines SAS
Original Assignee
Safran Aircraft Engines SAS
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Safran Aircraft Engines SAS filed Critical Safran Aircraft Engines SAS
Publication of EP3706934A1 publication Critical patent/EP3706934A1/de
Application granted granted Critical
Publication of EP3706934B1 publication Critical patent/EP3706934B1/de
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22DCASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
    • B22D13/00Centrifugal casting; Casting by using centrifugal force
    • B22D13/06Centrifugal casting; Casting by using centrifugal force of solid or hollow bodies in moulds rotating around an axis arranged outside the mould
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22DCASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
    • B22D27/00Treating the metal in the mould while it is molten or ductile ; Pressure or vacuum casting
    • B22D27/02Use of electric or magnetic effects
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22DCASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
    • B22D13/00Centrifugal casting; Casting by using centrifugal force
    • B22D13/02Centrifugal casting; Casting by using centrifugal force of elongated solid or hollow bodies, e.g. pipes, in moulds rotating around their longitudinal axis
    • B22D13/026Centrifugal casting; Casting by using centrifugal force of elongated solid or hollow bodies, e.g. pipes, in moulds rotating around their longitudinal axis the longitudinal axis being vertical
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22DCASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
    • B22D13/00Centrifugal casting; Casting by using centrifugal force
    • B22D13/06Centrifugal casting; Casting by using centrifugal force of solid or hollow bodies in moulds rotating around an axis arranged outside the mould
    • B22D13/066Centrifugal casting; Casting by using centrifugal force of solid or hollow bodies in moulds rotating around an axis arranged outside the mould several moulds being disposed in a circle
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22DCASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
    • B22D21/00Casting non-ferrous metals or metallic compounds so far as their metallurgical properties are of importance for the casting procedure; Selection of compositions therefor
    • B22D21/002Castings of light metals
    • B22D21/005Castings of light metals with high melting point, e.g. Be 1280 degrees C, Ti 1725 degrees C

Definitions

  • the present invention relates to the manufacture of metal alloy blanks by centrifugal casting of a molten metal alloy, and in particular blade blanks for turbomachines, in particular blades for aeronautical turbojet engines.
  • Figure 1 shows a known manufacturing device that can be used for this manufacture.
  • the manufacturing device 100 comprises, in a chamber 150 closed and sealed, a crucible 110 and a centrifugal casting wheel 120.
  • the crucible 110 is adapted to perform the melting of the metal alloy, which is for example provided in the form of a metal alloy ingot 116. Once this fusion has been performed, the molten metal alloy is poured into the wheel centrifugal casting 120.
  • the centrifugal casting wheel 120 is rotatable about an axis of rotation A and comprises a mold 122 for receiving the molten metal alloy.
  • the mold 122 extends in a radial direction R with respect to the axis of rotation A.
  • the centrifugal casting wheel 120 is rotated about its axis of rotation A. During this rotation, the molten metal alloy is rapidly driven by the centrifugal force at the bottom of the mold 122.
  • the rotational speed of the casting wheel Centrifugal 120 is chosen such that this centrifugal force is significantly greater than the force of gravity.
  • the molten metal alloy solidifies gradually, at a solidification rate lower than the filling rate of the mold 122; thus, the solidification takes place on the entire mold 122, until the desired metal alloy blank.
  • the blank metal alloy is then extracted from the mold 122, and can subsequently undergo subsequent industrial steps (heat treatment, machining, forging ...) to reach a final piece.
  • the foundry step that has just been described has the advantage of reducing the porosity due to the removal of the metal alloy during the solidification of the metal alloy blank. However, it also has drawbacks, which will be understood with reference to FIGS. 2 and 3.
  • FIG. 2 schematically represents the solidified metal blank in section along the plane C-C of Figure 1 and allows to observe the metallurgical microstructure (the walls of the mold 122 and the centrifugal wheel 120 have been omitted to simplify the drawing).
  • the solidified metal blank 146 has a central region B1 consisting of coarsely equiaxed grains.
  • the blank 146 Near its walls, the blank 146 has a "skin" B3 consisting of equiaxial grains of smaller dimensions than in the central region B1.
  • the blank 146 has an intermediate region B2 consisting of columnar grains (also known as basaltic grains).
  • This intermediate region B2 is better visible in FIGS. 3A and 3B, which are photographs of cuts in the radial direction R of two metal blanks made of TA6V (titanium-based alloy comprising by weight 6% of aluminum and 4% of vanadium ) obtained according to the method just described, and where the regions B1, B2 and B3 have been indicated.
  • TA6V titanium-based alloy comprising by weight 6% of aluminum and 4% of vanadium
  • the columnar grains of the intermediate region B2 induce a very strong anisotropy, which is problematic for subsequent industrial stages.
  • the mechanical and dynamic properties of the blank in the intermediate region B2 are very different in the direction considered (perpendicular to the axis of the columnar grains or parallel to their axis), the responses of the material to the forces of the different machining as a function of the angle of cut with respect to the columnar grain axis.
  • the relaxations of the constraints of the machining are also anisotropic.
  • the machining of the blank must be designed to take into account the foregoing factors, which tends to complicate it.
  • the parts that one wishes to achieve by machining the blank must also be sized to take into account the factors that above, which frequently leads to a non-optimal use of the material of the blank.
  • the directions of the axes of the columnar grains may vary from one region of the blank to the other (as can be seen for example in FIG. 3B): in this case, the mechanical and dynamic properties of the The blank, even in a given direction, may differ from one region to another of the same blank and / or blank to another. The design of the machining is then even more complex. It may even be that some of the blanks are totally unusable for machining, in which case they must be discarded.
  • the blank since the blank has a complex and varied metallurgical microstructure, its use properties (especially mechanical) are widely dispersed. Parts made from this blank must be dimensioned accordingly, which tends to weigh them down. This is particularly undesirable when the part to be manufactured is a dawn for an aeronautical turbojet, because such vanes must be as light as possible in the interest of the turbojet engine's performance.
  • the anisotropy induced by the columnar grains of the intermediate region B2, and the interfaces between the intermediate region B2 with columnar grains and the regions B1 and B3 with equiaxial grains make it very difficult or even impractical to perform simple operations. hot shaping of the blank, such as forging, rolling or extruding. However, these operations can bring new mechanical properties to the material of the blank. There is therefore a need for a new process for manufacturing a metal alloy blank by centrifugal casting which makes it possible to reduce the anisotropy of the blank and to simplify and make less costly the subsequent operations to be performed on the blank.
  • the present invention provides a device for manufacturing a metal alloy blank by centrifugal casting of a molten metal alloy, comprising a centrifugal casting wheel, the centrifugal casting wheel being rotatable about an axis of rotation and comprising a mold for receiving the molten metal alloy, the mold extending in a radial direction relative to the axis of rotation, the device comprising at least one magnet arranged to induce a electric current in the mold during the rotation of the centrifugal casting wheel about the axis of rotation.
  • the electrical current induced by the magnet creates a Laplace force that tends to stir the molten metal alloy within the mold. Thanks to this stirring, the metal alloy blank has, after solidification, a homogeneous macrostructure, almost free of columnar grains, and therefore almost isotropic, which eliminates the disadvantages described above.
  • the blank has virtually no residual porosity after cooling. This avoids having to subject the blank to a hot isostatic pressing (HIP) step, which also makes it possible to reduce these residual porosities but has the disadvantage of being long and very expensive.
  • HIP hot isostatic pressing
  • the centrifugal casting wheel comprises a winding surrounding an internal volume of the mold and configured so that the magnet induces an electric current in the winding during said rotation of the centrifugal casting wheel around the axis of rotation.
  • an induced current is generated not only in the molten metal alloy (and possibly in the structure of the centrifugal casting wheel), but also in the winding.
  • the Laplace force acting on the molten metal alloy is more intense.
  • the mixing of the molten metal alloy inside the mold is more intense, which further improves the homogeneity of the metal alloy blank.
  • it is not necessary to connect the winding to a source of electricity since an induced current is generated remotely in the winding. This avoids providing a particular connection of the winding to a source of electricity not secured to the centrifugal casting wheel, which would be complex from the mechanical point of view (risk of blocking the centrifugal casting wheel by the supply son).
  • the magnet is an annular or circular magnet whose axis is parallel to the axis of rotation.
  • the magnetic field generated by the magnet is substantially uniform over the entire volume swept by the mold during the rotation of the centrifugal casting wheel.
  • the device comprises a plurality of magnets arranged spaced around the axis of rotation.
  • the magnetic field acting on the mold varies during the rotation of the centrifugal casting wheel. It follows that the electric current induced in the mold, and thus the Laplace force acting on the molten metal alloy, is variable during the rotation of the centrifugal casting wheel, which improves the stirring of the molten metal alloy within the mold.
  • the magnets are even in number, and the polarities of said magnets alternate regularly around the axis of rotation.
  • the magnetic field acting on the mold periodically changes direction during the rotation of the centrifugal casting wheel, which further improves the stirring of the molten metal alloy within the mold.
  • the magnet is not secured to the centrifugal casting wheel, and the device further comprises a permanent magnet integral with the centrifugal casting wheel and extending partly through the coil.
  • the magnet is an annular or circular magnet whose axis is parallel to the axis of rotation.
  • the poles of the permanent magnet and the magnet facing each other have opposite names.
  • the device comprises a plurality of magnets not integral with the centrifugal casting wheel and arranged spaced about the axis of rotation.
  • the non-integral magnets of the centrifugal casting wheel are even in number, and the polarities of said magnets alternate regularly around the axis of rotation.
  • the axis of rotation is vertical.
  • the balancing device of the centrifugal casting wheel is simpler.
  • the construction and operation of the device are therefore simplified.
  • the stirring of the molten metal alloy inside the mold is less disturbed. Indeed, during the rotation of the wheel, the molten metal alloy inside the mold is subjected to the centrifugal force and the force of gravity.
  • the centrifugal force is always radial to the axis of rotation. If the axis of rotation is vertical, the direction of the force of gravity also does not vary during the rotation of the wheel, so that the stirring is less disturbed.
  • the radial direction is parallel to the horizontal. In this way, the construction of the centrifugal casting wheel is simpler, especially if the axis of rotation is vertical.
  • the present invention also provides a method of manufacturing a metal alloy blank comprising the steps of:
  • centrifugal casting wheel pouring the molten metal alloy into a centrifugal casting wheel, the centrifugal casting wheel being rotatable about an axis of rotation and comprising a mold for receiving the metal alloy melting, the mold extending in a radial direction relative to the axis of rotation;
  • the centrifugal casting wheel comprises a coil surrounding an interior volume of the mold, and during the rotation step, the magnetic field induces an electric current in the coil.
  • the method according to the invention provides the same advantages as the device according to the invention.
  • the metal alloy is an alloy based on titanium or nickel.
  • titanium-based titanium (respectively “nickel-based) is meant that titanium (respectively nickel) is substantially, by weight, the majority element of the alloy.
  • Titanium-based or nickel-based metal alloys are among the alloys commonly used to make blanks of mechanically stressed parts, such as blades for a turbomachine, and more particularly blades for an aeronautical turbojet engine.
  • the metal alloy blank is a blade blank for a turbomachine, in particular a blade for an aeronautical turbojet engine.
  • FIG. 1 shows schematically a known centrifugal casting manufacturing device
  • FIG. 2 shows schematically the solidified metal blank obtained by the device of Figure 1, in section along the plane CC of Figure 1;
  • FIGS. 3A and 3B are photographs of sections of two metal blanks obtained by the device of FIG. 1, in the direction of FIG. 1;
  • FIG. 4 schematically represents a device for manufacturing by centrifugal casting according to the invention
  • FIG. 5 is a partial perspective view and cut away of the device of Figure 4.
  • FIG. 6 is a top view of the centrifugal casting wheel and the magnet, according to another embodiment of the invention.
  • Figure 7 is a top view similar to Figure 6, according to yet another embodiment of the invention.
  • FIG. 8 is a top view similar to Figure 7, according to yet another variant of the invention.
  • FIG. 9 is a side view of a portion of the centrifugal casting wheel, according to yet another embodiment of the invention.
  • FIG. 10 is a perspective view of FIG. 9, showing a first possibility of implementing the variant of FIG. 9;
  • FIG. 11 is a perspective view of FIG. 9, showing another possibility of implementing the variant of FIG. 9.
  • FIG. 4 schematically represents a device 10 for manufacturing a metal alloy blank by centrifugal casting of a molten metal alloy.
  • the manufacturing device 10 comprises, in a closed and sealed enclosure 50, a melting device 610, a centrifugal casting wheel 20 (hereinafter referred to as “the wheel 20" for convenience) and a magnet 40.
  • the melter 610 is adapted to provide a molten metal alloy.
  • the merge device 610 performs the melting of a metal alloy provided in the form of a metal alloy ingot 616.
  • the various constituents of the metal alloy are introduced individually into the melter 610, and then melted together so as to obtain the molten metal alloy.
  • the metal alloy is selected from suitable alloys for the final piece to be made from the blank.
  • the metal alloy may be, for example, a ceramic-based alloy, a steel, a titanium-based alloy, or a nickel-based alloy.
  • Titanium-based alloys include:
  • conventional titanium alloys having a crystallographic structure identical to that of pure titanium, for example: TA6V, Ti-17, Ti 10-2-3, Ti-5553, ⁇ 16, ⁇ 21;; and
  • titanium-based intermetallic alloys having one or more crystallographic structure phases different from that of pure titanium.
  • titanium aluminides are particularly contemplated, among which:
  • phase titanium aluminides and ⁇ 2 columnar such as:
  • Ti-48AI-1V-0.3C Ti-48AI-2Cr-2Nb (also known as “GE 48-2-2") or Ti-48AI-2Nb-0.75Cr-0.3Si (also known as “Daido RNT650");
  • titanium aluminas with ⁇ and 2 equiaxed phases such as T-45Al-2Nb-2Mn + 0.8TiB 2 (also known as "Howmet
  • aluminides with ⁇ , ⁇ and ⁇ 2 equiaxed phases such as Ti-47.3-Al-2,2Nb-0,5Mn-0,4W-0,4Mo-0,23Si, Ti-46,5AI -3Nb-2Cr-0.2W-0,2Si-0, IC
  • the Ti-48Al-2 Cr-2 NB alloy comprises, in atomic percentage, 48% of Al, 2% of Cr, 2% of Nb, and titanium (Ti) in addition to 100%.
  • nickel-based alloys conventional nickel alloys such as René 77 or DS 200, or nickel superalloys such as AMI, are particularly contemplated.
  • the fusion device 610 can be, for example:
  • VAR Vacuum Arc Remelting
  • VIM Vacuum Induction Melting
  • EB Electro Bombardment
  • the enclosure 50 is controlled to provide the required atmosphere:
  • the molten metal alloy leaving the melting device 610 is poured into the wheel 20.
  • the wheel 20 comprises a hub 30 at least one mold 22 fixed to the hub 30.
  • the hub 30 comprises a central channel 32 and several supply channels 33 each communicating with a mold 22.
  • the hub 30 may be provided with a funnel 31 opening onto the central channel 32.
  • the hub 30 is capable of being rotated about an axis of rotation A, for example by means of a motor (not shown).
  • the wheel 20 is rotatable about the axis of rotation A.
  • the axis A is preferably vertical.
  • FIG. 5 shows in perspective a mold 22 fixed to the hub 30
  • the mold 22 extends in a radial direction R1 with respect to the axis A (see FIG. 4).
  • this radial direction RI is perpendicular to the axis A.
  • the radial direction RI is parallel to the horizontal.
  • the mold 22 is adapted to receive the molten metal alloy, here in a cavity 22B.
  • the mold 22 is typically made of a metal, a metal alloy or a ceramic sufficiently resistant to withstand the thermal stresses associated with contact with the molten mechanical alloy.
  • the cavity 22B may have a rectangular or cylindrical section. This section may advantageously be constant over the entire length of the cavity 22B.
  • the cavity 22B typically has a length substantially greater than the maximum dimension of its section, for example at least 3 times, and preferably at least 5 times greater than the maximum dimension of its section.
  • the metal alloy blank After solidification, the metal alloy blank then has the general shape of a bar.
  • the cavity 22B communicates with a supply channel 33 via a feed 22A, which is optionally of smaller section than the cavity 22B.
  • molds 22 may be attached to the hub 30 as can be seen in FIGS. 4 and 5. For example, several molds 22 may be evenly spaced about the axis A. The molds 22 may also be superimposed to form a plurality of molds 22. (two in FIGS. 4 and 5) mold levels 22. The molds 22 can be separable from the hub 30, so that they can be replaced individually and / or separated one by one from the hub 30 in order to extract the metal alloy blank after solidification.
  • the manufacturing device 10 also comprises at least one magnet.
  • the magnet designated by the reference 40; it should be noted, however, that the features presented in the following with respect to the magnet 40 may be applied to a single, all or some of the magnets.
  • the magnetic field generated by the magnet 40 is denoted H.
  • magnet includes both permanent magnets and electromagnets, unless otherwise stated.
  • the magnetic field H induces an electric current in the mold 22.
  • This electric current is induced in the walls 23 of the mold 22 (especially if it is made of a metal or a metal alloy), and also in the molten metal alloy contained in the cavity 22B.
  • This electric current generates a magnetic field induced in the mold 22.
  • this induced magnetic field creates a Laplace force.
  • This Laplace force tends to stir the molten metal alloy being solidified in the cavity 22B.
  • the stirring of the molten metal alloy in the cavity 22B has the following effects:
  • the stirring of the molten metal alloy considerably favors the formation of equiaxial grains with respect to the formation of columnar grains. Therefore, the alloy metal blank has a homogeneous macrostructure, almost without of columnar grains, and therefore almost isotropic, which eliminates the disadvantages discussed above.
  • the stirring makes it possible to constantly re-homogenize the chemical composition of the molten metal alloy, both in front of the solidification front and at the level of the solidification front. This makes it possible to avoid any local segregation, and consequently any aligned positive segregation or exudation in the blank.
  • the manufacturing device 10 thus makes it possible to obtain a metal blank with improved mechanical and structural properties, which can be more easily machined and / or subjected to hot forming operations (forging, rolling, extrusion, etc.). Furthermore, the subsequent operations to be performed on the blank are less expensive because the hot isostatic pressing step is no longer necessary.
  • the mold 22 may be provided with a coil 60, which is seen in FIG.
  • the coil 60 comprises one or more typically several turns electrically connected to each other.
  • the turns of the coil 60 surround an interior volume of the mold 22. In the example shown in FIG. 5, this interior volume is the entire cavity 22B. It could also be only part of the cavity 22B.
  • the turns of the coil 60 can be embedded in the walls
  • the turns extend parallel to the radial direction RI. This maximizes the area swept by the coil during the rotation of the wheel 20, particularly if the cavity 22B has a length significantly greater than the maximum dimension of its section as explained above.
  • the magnet 40 may be an annular magnet 40C whose axis is parallel to the axis A. It may also be a circular magnet.
  • the magnet 40C makes it possible to obtain a substantially uniform magnetic field H over the entire volume swept by the mold 22 during the rotation of the wheel 20.
  • the axis of the magnet 40C coincides with the axis A.
  • the magnetic field H is then more uniform over the entire volume swept by the mold 22 during the rotation of the wheel 20.
  • the device comprises a plurality (here three) magnets 40-1, 40-2, 40-3 each arranged to induce an electric current in the mold 22 and possibly in the winding 60.
  • the magnets 40-1, 40-2, 40-3 are arranged spaced about the axis A. In other words, between the magnets 40-1, 40-2, 40-3, there are gaps devoid of magnets. Consequently, the magnetic field H varies according to the angular position of the mold 22. It follows that the electric current induced by the magnet in the mold 22, and therefore the Laplace force, in the mold 22 is variable during the rotation of the wheel 30, which improves the stirring of the molten metal alloy inside the mold 22.
  • the magnets 40-1, 40-2, 40-3 are all identical.
  • magnets 40-1, 40-2, 40-3 are regularly spaced from each other.
  • the magnets 40-1, 40-2, 40-3 may have the shape of annular segments whose axis is parallel to the axis A as shown in Figure 7. It may also be circular segments. As in the variant of Figure 6, it is preferable that the axis of the annular or circular segments is coincident with the axis A.
  • the magnets are even in number (here, four magnets 40-1 to 40-4), and the polarities of the magnets alternate regularly around the axis A.
  • the pole of the magnets 40-1 to 40-4 facing the wheel 20 is alternately North, South, North, South, ....
  • the magnetic field H applying to the mold 22 periodically changes direction during the rotation of the wheel 20, which further improves the stirring of the molten metal alloy inside the mold
  • the magnetic field H is alternating.
  • the device 10 further comprises a permanent magnet 40M integral with the wheel 20.
  • the magnet 40 is in turn in the form of a magnet 40S not secured to the wheel 20.
  • the magnet 40S is fixed relative to the enclosure 50.
  • the permanent magnet 40M extends partly through the coil 60 of the mold 22.
  • the poles of the permanent magnet 40M and the facing magnet 40S have opposite names (i.e., if one of the poles is North, the other is South).
  • the magnetic field H is almost uniform, as shown schematically in FIG. 9.
  • the lines of the magnetic field H are aligned with the turns of the winding, which further increases the intensity of the current induced in the winding 60 and therefore the intensity of the brewing.
  • the magnet 40S may be an annular magnet whose axis is parallel to the axis A. It may also be a circular magnet.
  • annular or circular magnet makes it possible to obtain a substantially uniform magnetic field H over the entire volume swept by the mold 22 during the rotation of the wheel 20.
  • poles of the permanent magnet 40M and the annular or circular magnet 40S facing each other have opposite names.
  • the device comprises a plurality (here three) of magnets 40S-1, 40S-2, 40S-3 not integral with the wheel 20 and each arranged so as to induce an electric current in the mold 22 and possibly in the coil 60.
  • 40S-2, 40S-3 are such that their poles all have a name opposite to that of the 40M magnet they face (that is, if the poles of magnets 40S-1, 40S-2, 40S-3 are North, the pole of magnet 40 they face is South).
  • the non-integral magnets are even in number of the wheel 20 are even in number, and the polarities of said magnets regularly alternate around the axis A. In other words, following the direction of rotation of the wheel 20, the pole of these magnets facing the wheel 20 is alternately North, South, North,

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Continuous Casting (AREA)
  • Molds, Cores, And Manufacturing Methods Thereof (AREA)
EP18804376.4A 2017-11-07 2018-11-06 Vorrichtung und verfahren zur herstellung eines metalllegierungsrohlings durch schleudergiessen Active EP3706934B1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1760453A FR3073163B1 (fr) 2017-11-07 2017-11-07 Dispositif et procede de fabrication d'une ebauche en alliage metallique par coulee centrifuge
PCT/FR2018/052736 WO2019092354A1 (fr) 2017-11-07 2018-11-06 Dispositif et procédé de fabrication d'une ébauche en alliage métallique par coulée centrifuge

Publications (2)

Publication Number Publication Date
EP3706934A1 true EP3706934A1 (de) 2020-09-16
EP3706934B1 EP3706934B1 (de) 2021-10-27

Family

ID=61599295

Family Applications (1)

Application Number Title Priority Date Filing Date
EP18804376.4A Active EP3706934B1 (de) 2017-11-07 2018-11-06 Vorrichtung und verfahren zur herstellung eines metalllegierungsrohlings durch schleudergiessen

Country Status (5)

Country Link
US (1) US11433453B2 (de)
EP (1) EP3706934B1 (de)
CN (1) CN111372703B (de)
FR (1) FR3073163B1 (de)
WO (1) WO2019092354A1 (de)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110722123B (zh) * 2019-11-29 2021-04-02 哈尔滨工业大学 薄壁圆环截面合金铸件原位离心铸造设备及离心铸造方法
CN112605369B (zh) * 2020-11-10 2022-05-03 西北矿冶研究院 一种提高铜阳极板质量的浇铸装置
CN114749622A (zh) * 2022-04-27 2022-07-15 中南大学 双轴离心搅拌铸造装置以及混合金属熔炼铸造方法

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2963758A (en) * 1958-06-27 1960-12-13 Crucible Steel Co America Production of fine grained metal castings
JPH084898B2 (ja) * 1990-02-09 1996-01-24 株式会社クボタ 超電導遠心鋳造機
JPH03281052A (ja) * 1990-03-27 1991-12-11 Kubota Corp 遠心鋳造装置
JP3830697B2 (ja) * 1999-09-29 2006-10-04 株式会社クボタ 圧延用複合ロールの製造方法
US6755239B2 (en) * 2001-06-11 2004-06-29 Santoku America, Inc. Centrifugal casting of titanium alloys with improved surface quality, structural integrity and mechanical properties in isotropic graphite molds under vacuum
CN1327992C (zh) * 2004-12-24 2007-07-25 中国科学院金属研究所 卧式真空电磁离心铸造炉
CN100500919C (zh) * 2006-12-21 2009-06-17 清华大学深圳研究生院 一种高碳高钨高速钢轧辊
CN103357839A (zh) * 2012-03-26 2013-10-23 卓然(靖江)设备制造有限公司 旋转式电磁离心铸造机
US9364890B2 (en) * 2013-03-11 2016-06-14 Ati Properties, Inc. Enhanced techniques for centrifugal casting of molten materials
FR3017062B1 (fr) * 2014-01-31 2023-03-17 Snecma Moule centrifuge chemise a inertie thermique controlee
WO2015119449A1 (ko) * 2014-02-07 2015-08-13 한국생산기술연구원 다중 가압 주조 금형 및 이를 이용한 성형물 제조방법
FR3019561B1 (fr) * 2014-04-08 2017-12-08 Snecma Traitement thermique d'un alliage a base d'aluminure de titane

Also Published As

Publication number Publication date
US11433453B2 (en) 2022-09-06
WO2019092354A1 (fr) 2019-05-16
FR3073163A1 (fr) 2019-05-10
CN111372703B (zh) 2022-05-27
EP3706934B1 (de) 2021-10-27
CN111372703A (zh) 2020-07-03
FR3073163B1 (fr) 2022-07-15
US20200316682A1 (en) 2020-10-08

Similar Documents

Publication Publication Date Title
EP3706934B1 (de) Vorrichtung und verfahren zur herstellung eines metalllegierungsrohlings durch schleudergiessen
EP3020055B1 (de) Gesinterter ringmagnet mit radialer magnetisierung, aufweisend ein verstärktes mechanisches verhalten
EP2086704B1 (de) Verfahren zur herstellung von feingussteilen durch schleuderguss
EP3129516B1 (de) Wärmebehandlung einer aluminium-titan-basis-legierung
EP2906374B1 (de) Verfahren zur herstellung mindestens eines metallturbinentriebwerkteils
EP2983849B1 (de) Monokristalline schmelzform
EP3302874B1 (de) Verfahren zur herstellung einer tial-schaufel eines turbinenmotors
EP3268150B1 (de) Verfahren zur herstellung von turbomaschinenkomponenten, rohling und endgültige komponente
EP0005676A2 (de) Elektromagnetisches Rührverfahren beim Stranggiessen
CA2938286C (fr) Moule chemise pour coulee centrifuge
EP3119544B1 (de) Ausgekleidete zentrifugale form mit kontrollierter thermischer trägheit
EP3475012B1 (de) Kühlofen mit gerichteter erstarrung und kühlverfahren mit solch einem ofen
EP3083133B1 (de) Verfahren zur herstellung eines turbinentriebwerkteils sowie resultierende form und zwischenrohling
EP3465873B1 (de) Drehende elektrische maschine versehen mit seltenerdmagneten mit kleinem anteil dysprosium
EP2086705B1 (de) Verfahren zur herstellung von turbinenschaufeln durch schleudergiessen
FR2623210A1 (fr) Procede de production de gelees metalliques thixotropes par rotation electromagnetique
JP2014124641A (ja) 遠心鋳造装置

Legal Events

Date Code Title Description
STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: UNKNOWN

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: THE INTERNATIONAL PUBLICATION HAS BEEN MADE

PUAI Public reference made under article 153(3) epc to a published international application that has entered the european phase

Free format text: ORIGINAL CODE: 0009012

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: REQUEST FOR EXAMINATION WAS MADE

17P Request for examination filed

Effective date: 20200504

AK Designated contracting states

Kind code of ref document: A1

Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR

AX Request for extension of the european patent

Extension state: BA ME

DAV Request for validation of the european patent (deleted)
DAX Request for extension of the european patent (deleted)
GRAP Despatch of communication of intention to grant a patent

Free format text: ORIGINAL CODE: EPIDOSNIGR1

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: GRANT OF PATENT IS INTENDED

INTG Intention to grant announced

Effective date: 20210715

GRAS Grant fee paid

Free format text: ORIGINAL CODE: EPIDOSNIGR3

GRAA (expected) grant

Free format text: ORIGINAL CODE: 0009210

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: THE PATENT HAS BEEN GRANTED

AK Designated contracting states

Kind code of ref document: B1

Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR

REG Reference to a national code

Ref country code: GB

Ref legal event code: FG4D

Free format text: NOT ENGLISH

REG Reference to a national code

Ref country code: CH

Ref legal event code: EP

REG Reference to a national code

Ref country code: AT

Ref legal event code: REF

Ref document number: 1441352

Country of ref document: AT

Kind code of ref document: T

Effective date: 20211115

REG Reference to a national code

Ref country code: DE

Ref legal event code: R096

Ref document number: 602018025822

Country of ref document: DE

REG Reference to a national code

Ref country code: IE

Ref legal event code: FG4D

Free format text: LANGUAGE OF EP DOCUMENT: FRENCH

REG Reference to a national code

Ref country code: SE

Ref legal event code: TRGR

REG Reference to a national code

Ref country code: LT

Ref legal event code: MG9D

REG Reference to a national code

Ref country code: NL

Ref legal event code: MP

Effective date: 20211027

REG Reference to a national code

Ref country code: AT

Ref legal event code: MK05

Ref document number: 1441352

Country of ref document: AT

Kind code of ref document: T

Effective date: 20211027

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: RS

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20211027

Ref country code: LT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20211027

Ref country code: FI

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20211027

Ref country code: BG

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20220127

Ref country code: AT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20211027

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: IS

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20220227

Ref country code: PT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20220228

Ref country code: PL

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20211027

Ref country code: NO

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20220127

Ref country code: NL

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20211027

Ref country code: LV

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20211027

Ref country code: HR

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20211027

Ref country code: GR

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20220128

Ref country code: ES

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20211027

REG Reference to a national code

Ref country code: CH

Ref legal event code: PL

REG Reference to a national code

Ref country code: DE

Ref legal event code: R097

Ref document number: 602018025822

Country of ref document: DE

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: SM

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20211027

Ref country code: SK

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20211027

Ref country code: RO

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20211027

Ref country code: MC

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20211027

Ref country code: LU

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20211106

Ref country code: EE

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20211027

Ref country code: DK

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20211027

Ref country code: CZ

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20211027

Ref country code: BE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20211130

REG Reference to a national code

Ref country code: BE

Ref legal event code: MM

Effective date: 20211130

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: LI

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20211130

Ref country code: CH

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20211130

PLBE No opposition filed within time limit

Free format text: ORIGINAL CODE: 0009261

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT

26N No opposition filed

Effective date: 20220728

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: IE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20211106

Ref country code: AL

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20211027

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: SI

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20211027

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: CY

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20211027

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: HU

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT; INVALID AB INITIO

Effective date: 20181106

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: GB

Payment date: 20231019

Year of fee payment: 6

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: SE

Payment date: 20231020

Year of fee payment: 6

Ref country code: IT

Payment date: 20231019

Year of fee payment: 6

Ref country code: FR

Payment date: 20231020

Year of fee payment: 6

Ref country code: DE

Payment date: 20231019

Year of fee payment: 6

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: MK

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20211027