EP3109337B1 - Method for the preparation of tial forged components - Google Patents
Method for the preparation of tial forged components Download PDFInfo
- Publication number
- EP3109337B1 EP3109337B1 EP16175160.7A EP16175160A EP3109337B1 EP 3109337 B1 EP3109337 B1 EP 3109337B1 EP 16175160 A EP16175160 A EP 16175160A EP 3109337 B1 EP3109337 B1 EP 3109337B1
- Authority
- EP
- European Patent Office
- Prior art keywords
- tial
- finished product
- cast
- semi
- cast semi
- 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.)
- Not-in-force
Links
- 238000000034 method Methods 0.000 title claims description 25
- 229910010038 TiAl Inorganic materials 0.000 claims description 77
- 239000011265 semifinished product Substances 0.000 claims description 38
- 238000009750 centrifugal casting Methods 0.000 claims description 27
- 229910045601 alloy Inorganic materials 0.000 claims description 24
- 239000000956 alloy Substances 0.000 claims description 24
- 238000005242 forging Methods 0.000 claims description 16
- 238000005266 casting Methods 0.000 claims description 12
- 238000004519 manufacturing process Methods 0.000 claims description 10
- 229910052758 niobium Inorganic materials 0.000 claims description 10
- 239000010955 niobium Substances 0.000 claims description 10
- GUCVJGMIXFAOAE-UHFFFAOYSA-N niobium atom Chemical compound [Nb] GUCVJGMIXFAOAE-UHFFFAOYSA-N 0.000 claims description 10
- 239000000203 mixture Substances 0.000 claims description 9
- ZOKXTWBITQBERF-UHFFFAOYSA-N Molybdenum Chemical compound [Mo] ZOKXTWBITQBERF-UHFFFAOYSA-N 0.000 claims description 7
- 229910052750 molybdenum Inorganic materials 0.000 claims description 7
- 239000011733 molybdenum Substances 0.000 claims description 7
- 238000005520 cutting process Methods 0.000 claims description 4
- 238000010438 heat treatment Methods 0.000 claims description 3
- 239000000155 melt Substances 0.000 claims description 3
- 238000003754 machining Methods 0.000 claims description 2
- 238000007493 shaping process Methods 0.000 claims 1
- 239000000463 material Substances 0.000 description 20
- 239000010936 titanium Substances 0.000 description 7
- 229910052719 titanium Inorganic materials 0.000 description 7
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 6
- 239000000470 constituent Substances 0.000 description 6
- 238000001816 cooling Methods 0.000 description 6
- 239000010949 copper Substances 0.000 description 6
- 229910052802 copper Inorganic materials 0.000 description 6
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 5
- 229910052782 aluminium Inorganic materials 0.000 description 5
- 229910006281 γ-TiAl Inorganic materials 0.000 description 5
- 239000011159 matrix material Substances 0.000 description 4
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 3
- 230000006698 induction Effects 0.000 description 3
- 238000012545 processing Methods 0.000 description 3
- 238000005204 segregation Methods 0.000 description 3
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 3
- 229910001040 Beta-titanium Inorganic materials 0.000 description 2
- ZOXJGFHDIHLPTG-UHFFFAOYSA-N Boron Chemical compound [B] ZOXJGFHDIHLPTG-UHFFFAOYSA-N 0.000 description 2
- 229910052796 boron Inorganic materials 0.000 description 2
- 230000029142 excretion Effects 0.000 description 2
- 239000012530 fluid Substances 0.000 description 2
- 230000017525 heat dissipation Effects 0.000 description 2
- 230000002093 peripheral effect Effects 0.000 description 2
- 239000002244 precipitate Substances 0.000 description 2
- 239000002243 precursor Substances 0.000 description 2
- 241000446313 Lamella Species 0.000 description 1
- 229910000831 Steel Inorganic materials 0.000 description 1
- 229910001069 Ti alloy Inorganic materials 0.000 description 1
- 229910004349 Ti-Al Inorganic materials 0.000 description 1
- 229910004692 Ti—Al Inorganic materials 0.000 description 1
- 230000002411 adverse Effects 0.000 description 1
- 229910021325 alpha 2-Ti3Al Inorganic materials 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 239000000110 cooling liquid Substances 0.000 description 1
- 230000001419 dependent effect Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 230000002349 favourable effect Effects 0.000 description 1
- 230000005484 gravity Effects 0.000 description 1
- 239000012535 impurity Substances 0.000 description 1
- 238000007373 indentation Methods 0.000 description 1
- 230000001939 inductive effect Effects 0.000 description 1
- 239000007788 liquid Substances 0.000 description 1
- 238000002844 melting Methods 0.000 description 1
- 230000008018 melting Effects 0.000 description 1
- 238000001000 micrograph Methods 0.000 description 1
- 238000003801 milling Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012805 post-processing Methods 0.000 description 1
- 238000000926 separation method Methods 0.000 description 1
- 238000007711 solidification Methods 0.000 description 1
- 230000008023 solidification Effects 0.000 description 1
- 239000007858 starting material Substances 0.000 description 1
- 239000010959 steel Substances 0.000 description 1
Images
Classifications
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22F—CHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
- C22F1/00—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
- C22F1/16—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of other metals or alloys based thereon
- C22F1/18—High-melting or refractory metals or alloys based thereon
- C22F1/183—High-melting or refractory metals or alloys based thereon of titanium or alloys based thereon
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21J—FORGING; HAMMERING; PRESSING METAL; RIVETING; FORGE FURNACES
- B21J5/00—Methods for forging, hammering, or pressing; Special equipment or accessories therefor
- B21J5/002—Hybrid process, e.g. forging following casting
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21K—MAKING FORGED OR PRESSED METAL PRODUCTS, e.g. HORSE-SHOES, RIVETS, BOLTS OR WHEELS
- B21K3/00—Making engine or like machine parts not covered by sub-groups of B21K1/00; Making propellers or the like
- B21K3/04—Making engine or like machine parts not covered by sub-groups of B21K1/00; Making propellers or the like blades, e.g. for turbines; Upsetting of blade roots
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22D—CASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
- B22D13/00—Centrifugal casting; Casting by using centrifugal force
- B22D13/02—Centrifugal casting; Casting by using centrifugal force of elongated solid or hollow bodies, e.g. pipes, in moulds rotating around their longitudinal axis
- B22D13/023—Centrifugal 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 horizontal
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22D—CASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
- B22D13/00—Centrifugal casting; Casting by using centrifugal force
- B22D13/04—Centrifugal casting; Casting by using centrifugal force of shallow solid or hollow bodies, e.g. wheels or rings, in moulds rotating around their axis of symmetry
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22D—CASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
- B22D13/00—Centrifugal casting; Casting by using centrifugal force
- B22D13/06—Centrifugal casting; Casting by using centrifugal force of solid or hollow bodies in moulds rotating around an axis arranged outside the mould
- B22D13/066—Centrifugal 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22D—CASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
- B22D13/00—Centrifugal casting; Casting by using centrifugal force
- B22D13/10—Accessories for centrifugal casting apparatus, e.g. moulds, linings therefor, means for feeding molten metal, cleansing moulds, removing castings
- B22D13/101—Moulds
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22D—CASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
- B22D21/00—Casting non-ferrous metals or metallic compounds so far as their metallurgical properties are of importance for the casting procedure; Selection of compositions therefor
- B22D21/002—Castings of light metals
- B22D21/005—Castings of light metals with high melting point, e.g. Be 1280 degrees C, Ti 1725 degrees C
-
- 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
Definitions
- the invention relates to a method for producing forged components from TiAl alloys for turbomachines, such as stationary gas turbines or aircraft engines.
- Components made of TiAl materials which comprise titanium and aluminum as their main components, are very interesting for applications in which components have to be moved quickly, for example as blades of turbomachinery, since they have high strength at a low specific weight.
- such materials are difficult to process, since to achieve the desired property profile of the components, the materials must have a defined microstructure with a specific microstructure.
- the invention proposes to produce TiAl components from TiAl materials by forging, using as semifinished product for forging a TiAl cast semi-finished product which is produced by horizontal centrifugal casting. It has been shown that TiAl cast semi-finished products produced by horizontal centrifugal casting can advantageously be used for further processing by forging in order to provide TiAl components with a particularly advantageous property profile for use in turbomachines in a simple and efficient manner.
- the horizontal centrifugal casting which is to be used according to the present invention for the production of TiAl - cast semi-finished products for the subsequent forging, is characterized in that a mold, in which the melt of the material to be cast is filled and provides the corresponding shapes for the semi-finished products is rotated about a horizontal axis.
- Horizontal means that the axis is aligned transversely, in particular perpendicular to the direction of gravity, with deviations by a few degrees in the context of technical implementation accuracy are allowed, ie, for example, deviations of up to +/- 10 °, preferably +/- 5 °.
- TiAl alloy is understood to mean a material comprising as its main components titanium and aluminum, so that they form the largest alloy constituents.
- materials which have intermetallic phases such as ⁇ 2 -Ti 3 Al and ⁇ -TiAl, and preferably also as constituents, which account for the largest part of a component made from such a material in terms of volume.
- the TiAl alloy can be a so-called TNM alloy, which contains niobium and molybdenum as further constituents, since such alloys have particularly good mechanical properties for use in turbomachines.
- it can be a TNM alloy having the composition 43.5% by weight of aluminum, 4% by weight of niobium, 1% by weight of molybdenum and 0.1% by weight of boron and the remainder titanium and unavoidable impurities and / or alloy constituents with fractions of in each case ⁇ 0.5% by weight up to a total amount of ⁇ 5% by weight, in particular ⁇ 2% by weight.
- the aluminum content of such an alloy may be in the range from 40 to 50% by weight, in particular 42 to 45% by weight, while the niobium content may be in the range from 2 to 6% by weight and in particular 3 to 5% by weight.
- the molybdenum content may range from 0.5 to 2 weight percent, while boron may range from 0.05 weight percent to 0.15 weight percent.
- the TiAl cast semi-finished product produced by horizontal centrifugal casting has the shape of a ring, since this form is a favorable starting material for the subsequent forging process.
- the TiAl cast semi-finished product can be cast by centrifugal casting so that the corresponding shapes, namely rings, are produced as separate cast semi-finished products.
- the cast semi-finished product can be produced with a microstructure which has colonies of .alpha.-titanium and .gamma.-TiAl in a .beta.-titanium matrix, where .beta -TiAl excretions may be present.
- the ⁇ -TiAl precipitates in the ⁇ -titanium matrix can be lenticular and / or the colonies of ⁇ -titanium and ⁇ -TiAl can have an elongated shape. Further, the ⁇ -TiAl may be provided in the colonies in the form of fine fins.
- the phase composition of the TiAl cast semi-finished product may already be close to the equilibrium phase composition at room temperature and may vary only up to 10% by volume, and more preferably up to 8% by volume, from the equilibrium composition at room temperature. This means that the cast semi-finished product has phases other than on the order of up to 10% by volume and up to 8% by volume, respectively, than should be the case for the equilibrium composition at room temperature.
- the TiAl cast semi - finished product After the TiAl cast semi - finished product has been produced by forging and optionally with at least one heat treatment, it is manufactured into a TiAl component or TiAl semifinished product which can only be produced by slight reworking into the desired TiAl component Post-processing, in particular the corresponding surface processing or deburring or Entkanten may include.
- a TiAl cast semi-finished product in the form of a ring is forged to form an annular disk, from which corresponding blades for turbomachines are cut out.
- the TiAl melt is heated at a sufficiently high temperature, i. in an overheated state can be introduced into the mold
- an inductively heatable feeder in the apparatus for horizontal centrifugal casting, by means of which the melt is introduced into the mold.
- the feeder can be surrounded by at least one coil.
- the feeder may be embodied as an open-topped trough, which may be cooled by a fluid, such as water, and which may preferably be formed from copper, niobium or molybdenum materials. Copper, niobium or molybdenum materials are understood to mean those materials which contain copper, niobium or molybdenum as the main constituent.
- the mold may be formed of a steel and / or copper and / or niobium material to allow rapid heat dissipation. Copper and niobium materials are in turn understood to mean materials which contain copper or niobium as the main constituent. To improve heat dissipation from the mold, the mold may also include suitable cooling channels for fluids such as water and the like.
- FIG. 1 shows a schematic sectional view of an apparatus and a method for centrifugal casting of semi-finished TiAl castings, from which subsequently by forming by forging TiAl - components are produced, which can be used in particular in turbomachines, such as aircraft engines.
- the apparatus comprises a mold 1 having a plurality of molds 3, 3 'into which the casting material is filled.
- the mold 1 of the embodiment, which in FIG. 1 is shown it is in the forms 3, 3 'to molds for the production of cones and Cylinders, which are arranged along the longitudinal axis 2 of the mold 1 and along the peripheral wall of the mold 1 spaced from each other.
- the mold 1 is in centrifugal casting, with which the molds 3, 3 'of the mold 1 are filled with appropriate molten liquid, rotated about the Kokillenl Kunststoffsachse 2, so that the casting material, for. in the form of a TiAl alloy, which is molten introduced into the mold 1, by which centrifugal force is forced into the molds 3, 3 '.
- the molten TiAl alloy 9 is provided from a crucible 6, which can be heated by a heater 7, wherein the molten TiAl alloy is introduced into the mold 1 via a feeder 5.
- FIG. 1 can be seen, the feeder 5 is moved in the mold 1 along the longitudinal axis 2, so that successively arranged along the longitudinal axis 2 spaced molds 3, 3 'can be filled.
- cooling channels 4 are provided in the mold 1 through which cooling liquid, such as water, can flow.
- the feeder 5 is provided with an induction heater 8, wherein a coil is provided for the induction heater 8 is, which is arranged around an upwardly open channel of the feeder 5.
- the molten TiAl alloy 9 can be held inductively at temperature on its way via the feeder 5 to the molds 3, 3 '.
- FIG. 2 shows the mold 1 after the horizontal centrifugal casting, wherein all molds 3, 3 'are filled with the cast TiAl material and the TiAl cast semi-finished products in the form of cones 10 and cylinders 11 can be removed, wherein the mold 1, as later in In another embodiment, can be decomposed into corresponding items to remove the TiAl - cast semi-finished products.
- FIG. 3 shows the mold 1 in a perspective view, in which case the individual forms 3, 3 'and their spaced arrangement in the circumferential direction and longitudinal direction of the cylindrical mold 1 can be clearly seen.
- a plurality of cooling channels 4 are arranged side by side in the peripheral wall of the mold 1 and run in the longitudinal direction of the mold 1.
- FIGS. 4 to 7 show a further exemplary embodiment of the method according to the invention and the device not according to the invention for the production of centrifugally cast TiAl cast semi-finished products as a precursor for the production of forged TiAl components.
- the second embodiment differs from the previous embodiment only in that differently shaped TiAl cast semi-finished products 12 are formed and, correspondingly, the mold 1 has other shapes 3 "Instead of the cones and cylinders as used in the exemplary embodiment of FIGS FIGS. 1 to 3 are made according to the embodiment of the FIG. 4 a plurality of rings or tubes 12 (see FIG. 5 ), wherein the corresponding molds 3 "are formed by circumferential indentations in the mold wall 1.
- the method or device differs according to FIG FIG. 4 not further compared to the embodiment of FIG. 1 so that the same components are given the same reference numerals and a repeated description of these identical components is omitted.
- FIG. 7 illustrates in a compilation in the diagrams a) to e) the sequence of the inventive method with respect to the centrifugal casting for the production of semi-finished Ti-Al casting as a precursor for the forging of TiAl - components from the TiAl - cast semi-finished products.
- the partial images a) to d) correspond to the representations of FIGS. 4 to 6 , in the partial image a) the beginning of the centrifugal casting is shown, in which the feeder 5, the first row of molds 3 "filled with the casting material, while in the partial image b) the feeder 5 has already been moved along the longitudinal axis 2 of the mold 1 and fill the third row of molds 3 "with molten TiAl alloy.
- the drawing e) of the FIG. 7 shows how the mold 1 is constructed of several parts, namely different ring segments 13 to 15, which are disassembled for removing the finished TiAl - cast semi-finished products in the form of rings 12.
- the mold 1 is in the illustrated embodiment of the invention FIG. 7 e) each of an end plate 13 and a plurality of annular mold segments 14 and separating segments 15, which are arranged alternately side by side so as to form the molds 3 " FIG. 7 e) five forms are provided for the formation of rings 12, wherein the mold 1 with more ring segments 14, 15 may be formed longer to form more rings 12.
- FIG. 8 schematically shows a micrograph to illustrate the microstructure of a TiAl - cast semi-finished product after centrifugal casting.
- the microstructure off a plurality of colonies 16 of ⁇ - titanium and ⁇ - TiAl, wherein the ⁇ - TiAl is in the form of lamellae 18 in the colonies 16.
- the colonies 16 are elongated and embedded in a ⁇ -titanium matrix 17, which additionally has lenticular ⁇ -TiAl precipitates 19.
- the structure has no globular ⁇ - TiAl grains and gives the material a tensile strength of 650 to 800 MPa with a total elongation of 0.2 to 0.9%.
- the microstructure is already very close to the equilibrium phase composition at room temperature, with the deviation from the equilibrium phase composition at room temperature only up to 10% by volume, preferably up to 8% by volume of the microstructure.
- the TiAl cast semi - finished products produced by horizontal centrifugal casting are outstandingly suitable for further processing into TiAl forged components, as described in US Pat FIG. 9 is shown.
- the TiAl cast semi-finished products are produced in the form of rings 12, as described, for example, in accordance with the method FIG. 7 in a forge with corresponding forging tools 20, 21 to a TiAl forging component in the form of an annular disc 22 (see drawing b) FIG. 9 ), from which according to the illustration in FIG. 9c) corresponding TiAl - components 23, such as blades or the like can be separated out, as indicated by the dashed lines in FIG. 9c) is indicated.
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Materials Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Physics & Mathematics (AREA)
- Thermal Sciences (AREA)
- Crystallography & Structural Chemistry (AREA)
- Forging (AREA)
Description
Die vorliegende Erfindung betrifft ein Verfahren zur Herstellung von geschmiedeten Bauteilen aus TiAl - Legierungen für Strömungsmaschinen, wie stationäre Gasturbinen oder Flugtriebwerke.The invention relates to a method for producing forged components from TiAl alloys for turbomachines, such as stationary gas turbines or aircraft engines.
Bauteile aus TiAl - Werkstoffen, die also als Hauptbestandteile Titan und Aluminium umfassen, sind für Anwendungen, bei denen Bauteile schnell bewegt werden müssen, wie beispielsweise als Schaufeln von Strömungsmaschinen, sehr interessant, da sie bei einem niedrigen spezifischen Gewicht eine hohe Festigkeit aufweisen. Allerdings sind derartige Werkstoffe schwierig zu verarbeiten, da zur Erzielung des gewünschten Eigenschaftsprofils der Bauteile, die Werkstoffe ein definiertes Gefüge mit einer bestimmten Mikrostruktur aufweisen müssen.Components made of TiAl materials, which comprise titanium and aluminum as their main components, are very interesting for applications in which components have to be moved quickly, for example as blades of turbomachinery, since they have high strength at a low specific weight. However, such materials are difficult to process, since to achieve the desired property profile of the components, the materials must have a defined microstructure with a specific microstructure.
Beim Gießen von TiAl-Werkstoffen kann es jedoch zu Seigerungen und Aluminiumsegregationen kommen, sodass sich eine inhomogene Mikrostruktur einstellen kann. Außerdem können sich grobe Gefüge ausbilden, die die mechanischen Eigenschaften negativ beeinflussen.However, when casting TiAl materials, segregation and aluminum segregation can occur, resulting in an inhomogeneous microstructure. In addition, coarse structures can form, which adversely affect the mechanical properties.
Aus der
Entsprechend ist es Aufgabe der vorliegenden Erfindung ein Verfahren zur Herstellung von TiAl - Bauteilen anzugeben, welches eine effiziente Herstellung von Bauteilen aus TiAl - Legierungen mit einem definierten Eigenschaftsprofil und einer gewünschten Mikrostruktur ermöglicht, wobei insbesondere geschmiedete TiAl - Bauteile für den Einsatz in Strömungsmaschinen bereitgestellt werden soll.Accordingly, it is an object of the present invention to provide a method for the production of TiAl components, which enables an efficient production of components made of TiAl alloys with a defined property profile and a desired microstructure, in particular forged TiAl components being provided for use in turbomachines should.
Die oben genannte Aufgabenstellung wird gelöst durch ein Verfahren mit den Merkmalen des Anspruchs 1. Vorteilhafte Ausgestaltungen sind Gegenstand der abhängigen Ansprüche.The above object is achieved by a method having the features of
Die Erfindung schlägt vor, TiAl - Bauteile aus TiAl - Werkstoffen durch Schmieden zu erzeugen, wobei als Halbzeug für das Schmieden ein TiAl - Gusshalbzeug verwendet wird, welches durch horizontalen Schleuderguss erzeugt wird. Es hat sich gezeigt, dass durch horizontalen Schleuderguss hergestellte TiAl - Gusshalbzeuge vorteilhaft für die weitere Verarbeitung durch Schmieden verwendet werden können, um so auf einfache und effiziente Weise TiAl - Bauteile mit insbesondere vorteilhaftem Eigenschaftsprofil für den Einsatz in Strömungsmaschinen bereitzustellen.The invention proposes to produce TiAl components from TiAl materials by forging, using as semifinished product for forging a TiAl cast semi-finished product which is produced by horizontal centrifugal casting. It has been shown that TiAl cast semi-finished products produced by horizontal centrifugal casting can advantageously be used for further processing by forging in order to provide TiAl components with a particularly advantageous property profile for use in turbomachines in a simple and efficient manner.
Das horizontale Schleudergießen, welches gemäß der vorliegenden Erfindung zur Herstellung von TiAl - Gusshalbzeugen für das nachfolgende Schmieden eingesetzt werden soll, zeichnet sich dadurch aus, dass eine Kokille, in die die Schmelze des abzugießenden Werkstoffs eingefüllt wird und die die entsprechenden Formen für die Halbzeuge bereitstellt, um eine horizontale Achse gedreht wird. Horizontal bedeutet hierbei, dass die Achse quer, insbesondere senkrecht zur Richtung der Schwerkraft ausgerichtet ist, wobei Abweichungen um einige Grad im Rahmen der technischen Durchführungsgenauigkeit zulässig sind, also beispielsweise Abweichungen von bis zu +/- 10°, vorzugsweise +/- 5°. Durch das horizontale Schleudergießen lassen sich bei hohen Rotationsgeschwindigkeiten der Kokille hohe Abkühlraten erzielen, sodass Entmischungen in der TiAl - Legierung vermieden werden können und ein feines Gefüge erzeugt werden kann. Außerdem können materialsparend Halbzeug mit großen Wanddicken bzw. Halbzeuge in Form von Zylindern und Kegeln hergestellt werden.The horizontal centrifugal casting, which is to be used according to the present invention for the production of TiAl - cast semi-finished products for the subsequent forging, is characterized in that a mold, in which the melt of the material to be cast is filled and provides the corresponding shapes for the semi-finished products is rotated about a horizontal axis. Horizontal here means that the axis is aligned transversely, in particular perpendicular to the direction of gravity, with deviations by a few degrees in the context of technical implementation accuracy are allowed, ie, for example, deviations of up to +/- 10 °, preferably +/- 5 °. By means of horizontal centrifugal casting, high cooling rates can be achieved at high rotational speeds of the mold, so that segregations in the TiAl alloy can be avoided and a fine microstructure can be produced. In addition, material-saving semi-finished products can be produced with large wall thicknesses or semi-finished products in the form of cylinders and cones.
Unter TiAl - Legierung wird bei der vorliegenden Erfindung ein Werkstoff verstanden, der als Hauptbestandteile Titan und Aluminium umfasst, sodass diese die größten Legierungsbestandteile bilden. Insbesondere werden darunter Werkstoffe verstanden, die intermetallische Phasen, wie α2-Ti3Al und γ-TiAl aufweisen und zwar vorzugsweise ebenfalls als Bestandteile, die volumenmäßig den größten Anteil eines aus einem derartigen Werkstoff gefertigten Bauteils ausmachen.In the present invention, TiAl alloy is understood to mean a material comprising as its main components titanium and aluminum, so that they form the largest alloy constituents. In particular, it is understood as meaning materials which have intermetallic phases, such as α 2 -Ti 3 Al and γ-TiAl, and preferably also as constituents, which account for the largest part of a component made from such a material in terms of volume.
Insbesondere kann die TiAl - Legierung eine sogenannte TNM - Legierung sein, die als weitere Bestandteile Niob und Molybdän aufweist, da derartige Legierungen besonders gute mechanische Eigenschaften für den Einsatz in Strömungsmaschinen aufweisen. Insbesondere kann es sich um eine TNM - Legierung mit der Zusammensetzung 43,5 Gew.% Aluminium, 4 Gew.% Niob, 1 Gew.% Molybdän sowie 0,1 Gew.% Bor und der Rest Titan sowie unvermeidbare Verunreinigungen und/oder Legierungsbestandteile mit Anteilen von jeweils < 0,5 Gew.% bis zu einem Gesamtteil von ≤ 5 Gew.%, insbesondere ≤ 2 Gew.% handeln. Der Aluminiumanteil einer derartigen Legierung kann im Bereich von 40 bis 50 Gew. %, insbesondere 42 bis 45 Gew.% liegen, während der Niobanteil im Bereich von 2 bis 6 Gew.% und insbesondere 3 bis 5 Gew.% liegen kann. Der Molybdänanteil kann wiederum in einem Bereich von 0,5 bis 2 Gew.% liegen, während Bor in einem Bereich von 0,05 Gew.% bis 0,15 Gew.% vorliegen kann.In particular, the TiAl alloy can be a so-called TNM alloy, which contains niobium and molybdenum as further constituents, since such alloys have particularly good mechanical properties for use in turbomachines. In particular, it can be a TNM alloy having the composition 43.5% by weight of aluminum, 4% by weight of niobium, 1% by weight of molybdenum and 0.1% by weight of boron and the remainder titanium and unavoidable impurities and / or alloy constituents with fractions of in each case <0.5% by weight up to a total amount of ≦ 5% by weight, in particular ≦ 2% by weight. The aluminum content of such an alloy may be in the range from 40 to 50% by weight, in particular 42 to 45% by weight, while the niobium content may be in the range from 2 to 6% by weight and in particular 3 to 5% by weight. Again, the molybdenum content may range from 0.5 to 2 weight percent, while boron may range from 0.05 weight percent to 0.15 weight percent.
Das TiAl - Gusshalbzeug, das durch den horizontalen Schleuderguss hergestellt wird, weist die Form eines Ringes auf, da diese Form ein günstiges Vormaterial für den nachfolgenden Schmiedeprozess darstellt.The TiAl cast semi-finished product produced by horizontal centrifugal casting has the shape of a ring, since this form is a favorable starting material for the subsequent forging process.
Das TiAl - Gusshalbzeug kann so im Schleudergussverfahren abgegossen werden, dass die entsprechenden Formen, nämlich Ringe, als separate Gusshalbzeuge entstehen. Darüber hinaus ist es auch möglich aus einem einzelnen Gussstück oder mehreren Gussstücken die gewünschten TiAl - Gusshalbzeuge durch Trennen, insbesondere Zerteilen oder Zerspanen herzustellen. Beispielsweise ist es möglich ein zylindrisches Rohr durch horizontalen Schleuderguss herzustellen und dieses anschließend durch mechanische Trennverfahren, wie Schneiden, Sägen, Fräsen oder dergleichen in entsprechende Ringstücke zu zerteilen bzw. zu trennen und diese Ringstücke als TiAl - Gusshalbzeuge für das nachfolgende Schmieden zu verwenden.The TiAl cast semi-finished product can be cast by centrifugal casting so that the corresponding shapes, namely rings, are produced as separate cast semi-finished products. Moreover, it is also possible to produce the desired semi-finished TiAl castings from a single casting or several castings by cutting, in particular cutting or machining. For example, it is possible to produce a cylindrical tube by horizontal centrifugal casting and then to divide this by mechanical separation processes, such as cutting, sawing, milling or the like into corresponding ring pieces and to use these ring pieces as TiAl - cast semi-finished products for subsequent forging.
Durch das horizontale Schleudergussverfahren können TiAl - Gusshalbzeuge in Form von Ringen mit einer Länge von 5 bis 300 cm und/oder Wandstärken von 4 bis 30 cm und/oder Innendurchmessern von 10 bis 100 cm als einzelne Gussstücke abgegossen werden.By means of the horizontal centrifugal casting process, semi-finished TiAl castings in the form of rings with a length of 5 to 300 cm and / or wall thicknesses of 4 to 30 cm and / or internal diameters of 10 to 100 cm can be poured off as individual castings.
Durch die schnelle Abkühlung, die mittels des Schleudergussverfahrens möglich ist, kann das Gusshalbzeug mit einer Mikrostruktur hergestellt werden, die Kolonien aus α - Titan und γ-TiAl in einer β - Titan - Matrix aufweist, wobei in der β - Titan - Matrix zusätzlich γ-TiAl Ausscheidungen vorliegen können. Die γ-TiAl Ausscheidungen in der β - Titan - Matrix können linsenförmig ausgebildet sein und/oder die Kolonien aus α - Titan und γ - TiAl können eine langgestreckte Form aufweisen. Ferner kann das γ - TiAl in den Kolonien in Form von feinen Lamellen vorgesehen sein.Due to the rapid cooling, which is possible by means of the centrifugal casting process, the cast semi-finished product can be produced with a microstructure which has colonies of .alpha.-titanium and .gamma.-TiAl in a .beta.-titanium matrix, where .beta -TiAl excretions may be present. The γ-TiAl precipitates in the β-titanium matrix can be lenticular and / or the colonies of α-titanium and γ-TiAl can have an elongated shape. Further, the γ-TiAl may be provided in the colonies in the form of fine fins.
Die Phasenzusammensetzung des TiAl - Gusshalbzeugs kann bereits nahe der Gleichgewichtsphasenzusammensetzung bei Raumtemperatur sein und lediglich bis zu 10 Vol.% und insbesondere bis zu 8 Vol.% von der Gleichgewichtszusammensetzung bei Raumtemperatur abweichen. Dies bedeutet, dass das Gusshalbzeug lediglich in der Größenordnung von bis zu 10 Vol.% bzw. bis zu 8 Vol.% andere Phasen aufweist als dies für die Gleichgewichtszusammensetzung bei Raumtemperatur der Fall sein sollte.The phase composition of the TiAl cast semi-finished product may already be close to the equilibrium phase composition at room temperature and may vary only up to 10% by volume, and more preferably up to 8% by volume, from the equilibrium composition at room temperature. This means that the cast semi-finished product has phases other than on the order of up to 10% by volume and up to 8% by volume, respectively, than should be the case for the equilibrium composition at room temperature.
Nach dem Herstellen des TiAl - Gusshalbzeugs wird dieses mit einem oder mehreren Umformschritten durch Schmieden und optional mit mindestens einer Wärmebehandlung zu einem TiAl - Bauteil bzw. TiAl - Halbzeug gefertigt, welches lediglich durch geringfügige Nacharbeit zum gewünschten TiAl - Bauteil gefertigt werden kann, wobei die Nachbearbeitung insbesondere die entsprechende Oberflächenbearbeitung bzw. das Entgraten oder Entkanten umfassen kann.After the TiAl cast semi - finished product has been produced by forging and optionally with at least one heat treatment, it is manufactured into a TiAl component or TiAl semifinished product which can only be produced by slight reworking into the desired TiAl component Post-processing, in particular the corresponding surface processing or deburring or Entkanten may include.
Es wird ein TiAl - Gusshalbzeug in Form eines Ringes zu einer Ringscheibe geschmiedet, aus welcher entsprechende Schaufeln für Strömungsmaschinen herausgetrennt werden.A TiAl cast semi-finished product in the form of a ring is forged to form an annular disk, from which corresponding blades for turbomachines are cut out.
Um sicherzustellen, dass die TiAl - Schmelze mit ausreichend hoher Temperatur, d.h. in einem überhitzten Zustand in die Kokille eingeführt werden kann, wird zudem vorgeschlagen, bei der Vorrichtung für den horizontalen Schleuderguss einen induktiv beheizbaren Speiser vorzusehen, mittels dem die Schmelze in die Kokille eingebracht wird. Zur induktiven Beheizung kann der Speiser von mindestens einer Spule umgeben sein.To ensure that the TiAl melt is heated at a sufficiently high temperature, i. in an overheated state can be introduced into the mold, it is also proposed to provide an inductively heatable feeder in the apparatus for horizontal centrifugal casting, by means of which the melt is introduced into the mold. For inductive heating, the feeder can be surrounded by at least one coil.
Der Speiser kann als eine oben offene Rinne ausgeführt sein, die durch ein Fluid, wie beispielsweise Wasser kühlbar sein kann und die vorzugsweise aus Kupfer-, Niob- oder Molybdänwerkstoffen gebildet sein kann. Unter Kupfer -, Niob - oder Molybdänwerkstoffen werden diejenigen Werkstoffe verstanden, die als Hauptbestandteil Kuper, Niob oder Molybdän aufweisen.The feeder may be embodied as an open-topped trough, which may be cooled by a fluid, such as water, and which may preferably be formed from copper, niobium or molybdenum materials. Copper, niobium or molybdenum materials are understood to mean those materials which contain copper, niobium or molybdenum as the main constituent.
Die Kokille kann aus einem Stahl - und/oder Kupfer - und/oder Niobwerkstoff gebildet sein, um eine schnelle Wärmeableitung zu ermöglichen. Unter Kupfer - und Niobwerkstoffen werden wiederum Werkstoffe verstanden, die als Hauptbestandteil Kupfer bzw. Niob aufweisen. Zur Verbesserung der Wärmeableitung aus der Kokille kann die Kokille auch geeignete Kühlkanäle für Fluide, wie Wasser und dergleichen, umfassen.The mold may be formed of a steel and / or copper and / or niobium material to allow rapid heat dissipation. Copper and niobium materials are in turn understood to mean materials which contain copper or niobium as the main constituent. To improve heat dissipation from the mold, the mold may also include suitable cooling channels for fluids such as water and the like.
Die beigefügten Zeichnungen zeigen in rein schematischer Weise in
- Fig. 1
- eine Darstellung des horizontalen Schleudergussverfahrens zur Herstellung von kegelförmigen oder zylinderförmigen TiAl - Gusshalbzeugen,
- Fig. 2
- eine Schnittdarstellung einer Kokille nach dem Schleuderguss,
- Fig. 3
- eine perspektivische Darstellung der Kokille aus den
undFiguren 12 , - Fig. 4
- eine weitere Darstellung einer Schleudergussvorrichtung zur Durchführung eines Schleudergussverfahrens gemäß einer zweiten Ausführungsform der Erfindung,
- Fig. 5
- eine Schnittdarstellung der Kokille aus
nach Beendigung des Schleudergusses,Figur 4 - Fig. 6
- eine perspektivische Darstellung der Kokille aus den
,Figuren 4 und 5 - Fig. 7
- eine Darstellung des Ablaufs des Schleudergussverfahrens in den Teilbildern a) bis e) bei der Ausführungsform, die in den
dargestellt ist,Figuren 4 bis 6 - Fig. 8
- eine schematische Darstellung des Gefüges eines TiAl - Gusshalbzeugs nach dem Schleuderguss und in
- Fig. 9
- eine Darstellung eines Schmiedeschritts zur Umformung eines Rings zu einer Scheibe.
- Fig. 1
- a representation of the horizontal centrifugal casting process for the production of conical or cylindrical TiAl cast semi-finished products,
- Fig. 2
- a sectional view of a mold after centrifugal casting,
- Fig. 3
- a perspective view of the mold from the
FIGS. 1 and2 . - Fig. 4
- a further illustration of a centrifugal casting apparatus for carrying out a centrifugal casting process according to a second embodiment of the invention,
- Fig. 5
- a sectional view of the mold
FIG. 4 after completion of centrifugal casting, - Fig. 6
- a perspective view of the mold from the
FIGS. 4 and 5 . - Fig. 7
- a representation of the process of the centrifugal casting process in the sub-images a) to e) in the embodiment shown in the
FIGS. 4 to 6 is shown - Fig. 8
- a schematic representation of the structure of a TiAl - cast semi-finished product after centrifugal casting and in
- Fig. 9
- an illustration of a forging step for forming a ring to a disc.
Weiter Vorteile, Kennzeichen und Merkmale der vorliegenden Erfindung werden bei der nachfolgenden detaillierten Beschreibung von Ausführungsbeispielen deutlich, wobei die Erfindung nicht auf die entsprechenden Ausführungsformen beschränkt ist.Further advantages, characteristics and features of the present invention will become apparent in the following detailed description of exemplary embodiments, wherein the invention is not limited to the corresponding embodiments.
Die
Die Vorrichtung umfasst eine Kokille 1, die eine Vielzahl von Formen 3, 3' aufweist, in die der Gusswerkstoff eingefüllt wird. Bei der Kokille 1 der Ausführungsform, die in
Die Kokille 1 wird beim Schleuderguss, mit dem die Formen 3, 3' der Kokille 1 mit entsprechender Schmelzflüssigkeit befüllt werden, um die Kokillenlängsachse 2 gedreht, sodass der Gusswerkstoff z.B. in Form einer TiAl - Legierung, der schmelzflüssig in die Kokille 1 eingeführt wird, durch die Zentrifugalkraft in die Formen 3, 3' gedrückt wird.The
Die schmelzflüssige TiAl - Legierung 9 wird aus einem Schmelztiegel 6, der durch eine Heizung 7 beheizt werden kann, bereitgestellt, wobei die schmelzflüssige TiAl - Legierung über einen Speiser 5 in die Kokille 1 eingeführt wird.The
Wie der
Um eine möglichst schnelle Erstarrung der TiAl - Legierung in der Kokille 1 bzw. in den Formen 3, 3' zu gewährleisten, sind in der Kokille 1 Kühlkanäle 4 vorgesehen, durch die Kühlflüssigkeit, wie beispielsweise Wasser, fließen kann.In order to ensure the fastest possible solidification of the TiAl alloy in the
Um sicherzustellen, dass die geschmolzene TiAl - Legierung 9 in einem geschmolzenen, überhitzten Zustand in die Kokille 1 bzw. die Formen 3, 3' eingebracht werden kann, ist der Speiser 5 mit einer Induktionsheizung 8 versehen, wobei für die Induktionsheizung 8 eine Spule vorgesehen ist, die um eine nach oben offene Rinne des Speisers 5 angeordnet ist. Durch die Spule 8 kann die schmelzflüssige TiAl - Legierung 9 auf ihrem Weg über den Speiser 5 zu den Formen 3, 3' induktiv auf Temperatur gehalten werden.To ensure that the
Die
Die
Die
Die
Die Teilbilder a) bis d) entsprechen den Darstellungen der
Das Teilbild e) der
Die
Die durch horizontalen Schleuderguss hergestellten TiAl - Gusshalbzeuge sind in hervorragender Weise für die Weiterverarbeitung zu TiAl - Schmiedebauteilen geeignet, wie dies in
Obwohl die vorliegende Erfindung anhand der Ausführungsbeispiele detailliert beschrieben worden ist, ist für den Fachmann selbstverständlich, dass die Erfindung nicht auf diese Ausführungsbeispiele beschränkt ist, sondern dass vielmehr Abwandlungen in der Weise möglich sind, dass einzelne Merkmale weggelassen oder andersartige Kombinationen von Merkmalen verwirklicht werden können, solange der Schutzbereich der beigefügten Ansprüche nicht verlassen wird. Die vorliegende Offenbarung schließt sämtliche Kombinationen der vorliegenden Einzelmerkmale mit ein.Although the present invention has been described in detail with reference to the embodiments, it will be understood by those skilled in the art that the invention is not limited to these embodiments, but rather modifications are possible in the manner that individual features omitted or other combinations of features can be realized as long as the scope of protection of the appended claims is not abandoned. The present disclosure includes all combinations of the subject features.
- 11
- Kokillemold
- 22
- KokillenlängsachseKokillenlängsachse
- 3, 3',3"3, 3 ', 3 "
- Formshape
- 44
- Kühlkanalcooling channel
- 55
- SpeiserSpeiser
- 66
- Schmelztiegelmelting pot
- 77
- Heizungheater
- 88th
- Induktionsspuleinduction coil
- 99
- Schmelzemelt
- 1010
- Kegelcone
- 1111
- Zylindercylinder
- 1212
- Ringring
- 1313
- Endplatteendplate
- 1414
- Formsegmentmold segment
- 1515
- Trennsegmentseparating segment
- 1616
- Koloniecolony
- 1717
- Matrixmatrix
- 1818
- Lamellelamella
- 1919
- linsenförmige Ausscheidunglenticular excretion
- 2020
- Schmiedewerkzeugforging tool
- 2121
- Schmiedewerkzeugforging tool
- 2222
- Scheibedisc
- 2323
- Bauteilcomponent
Claims (8)
- Method for producing forged components from TiAl alloys, namely blades (23) for turbomachinery, in which method a melt (9) of a TiAl alloy is provided which is cast in a horizontal centrifugal casting process such that at least one TiAl cast semi-finished product (10, 11, 12) is produced, the TiAl cast semi-finished product being shaped to form a TiAl forged part (22) by means of forging, characterized in that the TiAl cast semi-finished product is in the shape of a ring (12) and is forged to form an annular disc (22) from which blades (23) for turbomachinery are separated.
- Method according to claim 1, characterized in that the TiAl cast semi-finished product is produced by separating, in particular cutting or machining a casting.
- Method according to claim 1, characterized in that the TiAl alloy is cast in a mold (1) to form a plurality of separate TiAl cast semi-finished products.
- Method according to any of the preceding claims, characterized in that the TiAl alloy is cast to form a TiAl cast semi-finished product in the form of rings (12) having a length of 5 to 300 cm and/or wall thicknesses of 4 to 30 cm and/or internal diameters of 10 to 100 cm.
- Method according to any of the preceding claims, characterized in that the TiAl alloy is a TNM alloy comprising components of niobium and molybdenum.
- Method according to any of the preceding claims, characterized in that the TiAl cast semi-finished product has a microstructure formed by colonies (16) of α - Ti and γ - TiAl that are embedded in β - Ti.
- Method according to any of the preceding claims, characterized in that the phase composition of the TiAl cast semi-finished product differs from the equilibrium phase composition at room temperature by up to 10 vol.%, in particular by up to 8 vol.%.
- Method according to any of the preceding claims, characterized in that the TiAl cast semi-finished product is subjected to a plurality of shaping steps by means of forging and/or at least one heat treatment.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE102015211718.9A DE102015211718B4 (en) | 2015-06-24 | 2015-06-24 | Method and device for the production of TiAl forged components |
Publications (2)
Publication Number | Publication Date |
---|---|
EP3109337A1 EP3109337A1 (en) | 2016-12-28 |
EP3109337B1 true EP3109337B1 (en) | 2019-06-05 |
Family
ID=56321742
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP16175160.7A Not-in-force EP3109337B1 (en) | 2015-06-24 | 2016-06-20 | Method for the preparation of tial forged components |
Country Status (4)
Country | Link |
---|---|
US (1) | US10385434B2 (en) |
EP (1) | EP3109337B1 (en) |
DE (1) | DE102015211718B4 (en) |
ES (1) | ES2742206T3 (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102021000614A1 (en) | 2021-02-08 | 2022-08-11 | Access E.V. | Mold for the crack-free production of a metal object with at least one undercut, in particular from intermetallic alloys such as TiAl, FeAl and other brittle or crack-prone materials, as well as a corresponding method. |
Families Citing this family (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20180010468A1 (en) * | 2016-07-07 | 2018-01-11 | United Technologies Corporation | Enhanced temperature capability gamma titanium aluminum alloys |
US20180010213A1 (en) * | 2016-07-07 | 2018-01-11 | United Technologies Corporation | Enhance ductility of gamma titanium aluminum alloys by reducing interstitial contents |
EP3326746A1 (en) * | 2016-11-25 | 2018-05-30 | Helmholtz-Zentrum Geesthacht Zentrum für Material- und Küstenforschung GmbH | Method for joining and/or repairing substrates of titanium aluminide alloys |
JP6744842B2 (en) * | 2017-06-06 | 2020-08-19 | 三菱日立パワーシステムズ株式会社 | Hollow metal component for rotating electric machine stator, rotating electrical machine, and method for manufacturing hollow metal component |
CN109746406B (en) * | 2019-03-14 | 2020-12-15 | 明光天赋智能科技有限公司 | Centrifugal casting machine for special-shaped iron castings |
CN110052595B (en) * | 2019-04-13 | 2021-03-02 | 衢州恒业汽车部件有限公司 | Automobile steering knuckle with anti-transgranular fracture failure mode and manufacturing method thereof |
TWI752740B (en) | 2020-11-26 | 2022-01-11 | 財團法人工業技術研究院 | Aluminum alloy wheel and method for manufacturing the same |
Family Cites Families (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3203794A (en) * | 1957-04-15 | 1965-08-31 | Crucible Steel Co America | Titanium-high aluminum alloys |
DE1301877B (en) | 1964-03-04 | 1969-08-28 | Black Clawson Co | Horizontal centrifugal casting mold |
RO103095B1 (en) * | 1988-09-10 | 1993-01-10 | Matrite Si Piese Din Fonta Odo | Method and installation for centrifugal casting of pipes |
DE4420138C2 (en) | 1994-06-09 | 1997-09-25 | Ald Vacuum Techn Gmbh | Process for producing castings from reactive metals and mold made of metal for carrying out the process |
DE19528291C2 (en) | 1995-08-02 | 1998-06-04 | Ald Vacuum Techn Gmbh | Method and device for producing particles from directionally solidified castings |
DE19639514C1 (en) | 1996-09-26 | 1997-12-18 | Ald Vacuum Techn Gmbh | Production of high-precision centrifugal castings with controlled solidification |
DE19846781C2 (en) | 1998-10-10 | 2000-07-20 | Ald Vacuum Techn Ag | Method and device for producing precision castings by centrifugal casting |
JP2001288517A (en) | 2000-04-05 | 2001-10-19 | Ishikawajima Harima Heavy Ind Co Ltd | Cu-BASED ALLOY, CASTING HAVING HIGH STRENGTH AND HIGH THERMAL CONDUCTIVITY USING THE SAME AND METHOD FOR PRODUCING CASTING |
DE10024343A1 (en) * | 2000-05-17 | 2001-11-22 | Gfe Met & Mat Gmbh | One-piece component used e.g. for valves in combustion engines has a lamella cast structure |
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 |
EP2135694A4 (en) | 2007-03-15 | 2010-08-18 | Honda Motor Co Ltd | Hollow member, cylinder sleeve and methods for producing them |
DE102008021906A1 (en) | 2008-05-02 | 2008-10-30 | Daimler Ag | Method for the centrifugal casting of a hollow shaft with a variable inner diameter comprises positioning a disk or round plate in a mold using a positioning unit, closing the mold and rotating and pouring a molten metal into the mold |
-
2015
- 2015-06-24 DE DE102015211718.9A patent/DE102015211718B4/en not_active Expired - Fee Related
-
2016
- 2016-06-20 EP EP16175160.7A patent/EP3109337B1/en not_active Not-in-force
- 2016-06-20 ES ES16175160T patent/ES2742206T3/en active Active
- 2016-06-23 US US15/191,038 patent/US10385434B2/en not_active Expired - Fee Related
Non-Patent Citations (1)
Title |
---|
None * |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102021000614A1 (en) | 2021-02-08 | 2022-08-11 | Access E.V. | Mold for the crack-free production of a metal object with at least one undercut, in particular from intermetallic alloys such as TiAl, FeAl and other brittle or crack-prone materials, as well as a corresponding method. |
Also Published As
Publication number | Publication date |
---|---|
US10385434B2 (en) | 2019-08-20 |
DE102015211718B4 (en) | 2020-12-03 |
EP3109337A1 (en) | 2016-12-28 |
ES2742206T3 (en) | 2020-02-13 |
US20160376689A1 (en) | 2016-12-29 |
DE102015211718A1 (en) | 2016-12-29 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
EP3109337B1 (en) | Method for the preparation of tial forged components | |
EP1929146B1 (en) | Method for producing a piston for an internal combustion engine and the thus produced piston | |
EP2890519B1 (en) | Method for producing a composite component | |
EP3372700B1 (en) | Method for making forged tial components | |
DE10024343A1 (en) | One-piece component used e.g. for valves in combustion engines has a lamella cast structure | |
DE102014017721A1 (en) | A method for producing a lost core, core and cooling channel pistons made using such a core | |
DE112013007406B4 (en) | Process for manufacturing aluminum alloy components | |
EP3581668B1 (en) | Method for producing a component from gamma tial and correspondingly manufactured component | |
WO2017029186A1 (en) | Steel or aluminium piston for a combustion engine, as well as method for producing at least one part of a steel or aluminium piston for a combustion engine | |
DE10058428B4 (en) | Cylinder liner and cylinder block and method for producing the same | |
DE112014003143T5 (en) | Process for the preparation of a starting material for the separation treatment | |
EP3269838A1 (en) | High temperature resistant tial alloy and method for production thereof, and component from a corresponding tial alloy | |
DE102013208151B4 (en) | Process for the manufacture of metal products | |
EP1407056A2 (en) | Moulded piece made from an intermetallic gamma-ti-al material | |
EP1706516B1 (en) | Method for the production of cast components | |
EP3183080B1 (en) | Method for producing a piston for an internal combustion engine | |
EP3427858A1 (en) | Forging at high temperatures, in particular of titanium aluminides | |
DE102007010839B4 (en) | A method of manufacturing a piston and piston having an annular reinforcement comprising a plurality of reinforcing segments | |
EP2173507B1 (en) | Method and device for producing a tubular solid body from a refractory tungsten-heavy metal alloy, particularly as a semi-finished product for the production of a penetrator for a kinetic energy projectile with fragmentation effect | |
CH710105B1 (en) | Nickel-based superalloy article and method of making the superalloy article. | |
DE102012217939A1 (en) | Process for the production of cores for the casting production of workpieces | |
DE102013018944A1 (en) | Method for producing an impeller of an exhaust gas turbocharger and TiAl alloy for an impeller | |
DE3623122C1 (en) | Method of making piston rings | |
DE19621264B4 (en) | Method for producing a cylinder liner | |
DE102018127559A1 (en) | Component of an internal combustion engine, in particular cylinder head, mold assembly and method for producing a component of an internal combustion engine |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
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: THE APPLICATION HAS BEEN PUBLISHED |
|
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 |
|
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: 20170627 |
|
RBV | Designated contracting states (corrected) |
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 |
|
STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: EXAMINATION IS IN PROGRESS |
|
17Q | First examination report despatched |
Effective date: 20180503 |
|
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 |
|
RIC1 | Information provided on ipc code assigned before grant |
Ipc: B22D 13/10 20060101ALI20181120BHEP Ipc: B22D 21/00 20060101ALI20181120BHEP Ipc: C22F 1/18 20060101AFI20181120BHEP Ipc: B22D 13/04 20060101ALI20181120BHEP Ipc: B22D 13/02 20060101ALI20181120BHEP Ipc: C22C 14/00 20060101ALI20181120BHEP |
|
INTG | Intention to grant announced |
Effective date: 20181221 |
|
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: 1140039 Country of ref document: AT Kind code of ref document: T Effective date: 20190615 |
|
REG | Reference to a national code |
Ref country code: IE Ref legal event code: FG4D Free format text: LANGUAGE OF EP DOCUMENT: GERMAN |
|
REG | Reference to a national code |
Ref country code: DE Ref legal event code: R096 Ref document number: 502016004885 Country of ref document: DE |
|
REG | Reference to a national code |
Ref country code: NL Ref legal event code: MP Effective date: 20190605 |
|
REG | Reference to a national code |
Ref country code: LT Ref legal event code: MG4D |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
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: 20190605 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: 20190905 Ref country code: SE 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: 20190605 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: 20190605 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: 20190605 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: 20190605 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
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: 20190905 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: 20190605 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: 20190605 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: 20190906 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
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: 20190605 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: 20190605 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: 20190605 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: 20190605 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: 20191007 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: 20190605 |
|
REG | Reference to a national code |
Ref country code: CH Ref legal event code: PL |
|
REG | Reference to a national code |
Ref country code: ES Ref legal event code: FG2A Ref document number: 2742206 Country of ref document: ES Kind code of ref document: T3 Effective date: 20200213 |
|
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: 20190605 Ref country code: IT 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: 20190605 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: 20191005 |
|
REG | Reference to a national code |
Ref country code: DE Ref legal event code: R097 Ref document number: 502016004885 Country of ref document: DE |
|
REG | Reference to a national code |
Ref country code: BE Ref legal event code: MM Effective date: 20190630 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: TR 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: 20190605 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: 20190605 |
|
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 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
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: 20190605 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: 20190605 Ref country code: IE Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20190620 |
|
26N | No opposition filed |
Effective date: 20200306 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: LU Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20190620 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: 20190605 Ref country code: BE Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20190630 Ref country code: LI Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20190630 Ref country code: CH Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20190630 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: FR Payment date: 20200623 Year of fee payment: 5 Ref country code: DE Payment date: 20200623 Year of fee payment: 5 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: GB Payment date: 20200625 Year of fee payment: 5 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: ES Payment date: 20200717 Year of fee payment: 5 |
|
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: 20190605 |
|
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: 20160620 Ref country code: MT 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: 20190605 |
|
REG | Reference to a national code |
Ref country code: DE Ref legal event code: R119 Ref document number: 502016004885 Country of ref document: DE |
|
GBPC | Gb: european patent ceased through non-payment of renewal fee |
Effective date: 20210620 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: GB Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20210620 Ref country code: DE Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20220101 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: FR Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20210630 |
|
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: 20190605 |
|
REG | Reference to a national code |
Ref country code: ES Ref legal event code: FD2A Effective date: 20220805 |
|
REG | Reference to a national code |
Ref country code: AT Ref legal event code: MM01 Ref document number: 1140039 Country of ref document: AT Kind code of ref document: T Effective date: 20210620 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: ES Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20210621 Ref country code: AT Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20210620 |