EP0968065B1 - Method and apparatus for producing directionally solidified castings - Google Patents

Method and apparatus for producing directionally solidified castings Download PDF

Info

Publication number
EP0968065B1
EP0968065B1 EP98946047A EP98946047A EP0968065B1 EP 0968065 B1 EP0968065 B1 EP 0968065B1 EP 98946047 A EP98946047 A EP 98946047A EP 98946047 A EP98946047 A EP 98946047A EP 0968065 B1 EP0968065 B1 EP 0968065B1
Authority
EP
European Patent Office
Prior art keywords
mold
water
tank
cooled
heating zone
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
EP98946047A
Other languages
German (de)
French (fr)
Other versions
EP0968065A1 (en
Inventor
Vegeny Nikolaevich Kablov
Viktor Vladimirovich Gerasimov
Joseph Markovich Demonis
Viatcheslav Alexeevitch Nikolaev
Elena Mikhailovna Visik
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.)
All Russian Scientific Research Institute of Aviation Materials
General Electric Co
Original Assignee
All Russian Scientific Research Institute of Aviation Materials
General Electric Co
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 All Russian Scientific Research Institute of Aviation Materials, General Electric Co filed Critical All Russian Scientific Research Institute of Aviation Materials
Publication of EP0968065A1 publication Critical patent/EP0968065A1/en
Application granted granted Critical
Publication of EP0968065B1 publication Critical patent/EP0968065B1/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • 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
    • B22D27/04Influencing the temperature of the metal, e.g. by heating or cooling the mould
    • B22D27/045Directionally solidified castings

Definitions

  • the present invention relates to metal casting and can be used in producing castings with directional and single crystal structure.
  • the invention relates to a metal casting apparatus with a water-cooled tank having a truncated cone shape.
  • An apparatus for directional solidification generally comprises a vacuum chamber inside which there are disposed a mold heating zone, a baffle system, a water-cooled chill plate usually made of copper, an induction furnace, and a thermocouple system that automatically controlls and maintains the temperature in a cooling zone and in a heating zone within the furnace.
  • a vacuum chamber inside which there are disposed a mold heating zone, a baffle system, a water-cooled chill plate usually made of copper, an induction furnace, and a thermocouple system that automatically controlls and maintains the temperature in a cooling zone and in a heating zone within the furnace.
  • cooling zone is a liquid cooling bath with a material that melts easily to serve the role of the cooling medium.
  • the liquid metal bath is disclosed in U.S. Patent Nos 3763926 and 3915761, and Russian Federation Patent No 2010672.
  • the closest prior art to the present invention is an apparatus disclosed in French Patent Application 2604378, being accepted as a prototype.
  • This prototype apparatus comprises a vacuum chamber with a heating member inside where there is disposed a ceramic mold fixed on a water-cooled metallic plate which is moved up and down with the help of a rod and of an actuator for vertical transportation.
  • a horizontal baffle separates a heating zone and a cooling zone.
  • In the cooling zone concentrically with the chill plate, there is disposed an additional circular water-cooled cavity with the inner diameter exceeding the mold's maximal size.
  • Below the cavity there is disposed a container which is utilized for capturing the poured casting metal in the event of mold breakage.
  • the above apparatuses can function only when they comprise a crystallizer. It is impossible to use such installation for directional solidification processing with a liquid metal coolant and it is difficult to utilize the expensive alloys used in directional solidification castings in the event of mold breakage. Thus there is a need for a casting apparatus that provides a means that efficiently cools the molten cast alloy while protecting the equipment from damage in the event that the ceramic mold breaks while containing the molten cast alloy material.
  • the technical aim of this invention is to produce castings having the directional and single crystal structure by the method of radiation cooling without using the above-mentioned crystallizer.
  • Another aim of the invention is to be able to reconstruct easily the invented apparatus for both radiation crystallization processing and liquid metal cooling crystallization processing.
  • the inventive apparatus also increases the reliability and economic profit due to the apparatus' performance.
  • the invention comprises an apparatus in accordance with claim 1 hereof and a method in accordance with claim 9.
  • the inventive apparatus comprises a vacuum chamber inside which there is disposed an induction melting furnace, a mold preheating furnace with a ceramic mold, a drive assembly for mold transportation and a water-cooled tank.
  • the drive assembly comprises a rod on which the mold is fixed with the help of a hanger and a regulating actuator for vertical movement being positioned above the vacuum chamber.
  • the water-cooled tank is shaped as a truncated cone. Its upper portion is opened towards the heating zone, and its bottom portion has a smaller base than the upper portion.
  • a baffle separates the heating zone inside the induction furnace from the cooling zone; said baffle moves in a horizontal plane and closely adjoins the mold during the solidification process. It consists of the segments or sectors (not less than 2 from each side).
  • the apparatus performs as follows: the mold (1) is disposed on the hanger (2) and is fixed on the movable rod (3).
  • the hanger (2), the movable rod (3), and the regulating actuator comprise the drive assembly (14).
  • the mold (1) is placed into the mold preheater furnace (9) with the help of the actuator while regulating the mold position relative to the heater (4).
  • the heat baffle (5) is disposed under the heating zone (10).
  • the top butt end of the water-cooled tank (6) adjoins the baffle's (5) lower surface and is positioned coaxially with the heater (4) and (11).
  • the vacuum chamber (12) is evacuated to 1 x 10 -3 mm m.c.
  • the mold preheating furnace (9) is switched on.
  • the induction furnace's heater (11) Upon reaching the mold temperature of 100-150 °C higher than the liquidus temperature of the alloy being cast, the induction furnace's heater (11) is switched on, the alloy (7) being cast melts and is poured into the heated ceramic mold at the predetermined temperature. After that, the actuator for vertical transportation lowers the mold from the heating zone (10) into the cooling zone (13) at the required rate. Solidification of the molten cast alloy occurs by radiation onto the cold walls of the water-cooled tank. Due to this fact it becomes possible to produce large sized castings with directional and single crystal microstructure. Large size castings can include blades, nozzles, buckets, airfoils, and the like, that are used both in aircraft and land-based turbine engines. The castings are often greater than 30 inches in overall height.
  • the heater (4 and 11) is switched off.
  • the temperature is decreased to 300-400 °C, the mold with the solidified casting alloy is extracted from the installation which has been previously decompressed. Then the process is repeated for the next mold.
  • a single crystal seed with proper orientation is positioned into the top of the starting zone (8) of the ceramic mold before it is disposed in the vacuum chamber. Then the mold position is strictly fixed relative to the heater. In such event the seed and the solidified portion of the starting zone serve as a cooling medium, and further solidification of the melt is caused by radiation cooling in the water-cooled tank as stated above.
  • the use of the water-cooled tank instead of a chill plate allows the same or better working efficiency of said tank than that of a chill plate or of the prototype circular water-cooled cavity. At the same time the water-cooled tank of this invention does not require the use of a complex drive assembly with airtight seals.
  • the heat baffle (5) is used for raising the axial temperature gradient at the solidification front.
  • Said baffle moves in a horizontal plane, closely adjoins the ceramic mold according to its geometry during the solidification process and consists of the segments or sectors (not less than 2 from each side).
  • the water-cooled tank may be made of stainless steel and contain a double layer wall surrounding the perimeter of the tank. A vacuum atmosphere is created in the tank to further aid in the cooling of the cast parts.
  • the tank may also effectively function as a mold catch basin in the event of mold breakage, and the expensive, poured casting alloy may be easily removed from the tapered tank and be remelted.
  • the apparatus of this invention allows one to produce high quality castings having the directional and single crystal structure, including the large sized castings used in the land based turbine industry, by the method of radiation cooling without using the crystallizers of the prior art.
  • the invention also gives the possibility to reconstruct easily the disclosed apparatus for liquid metal cooling crystallization processing, to use successively the invented water-cooled tank as a mold catch basin in the event of mold breakage, and to increase the reliability and economic profitability of the apparatus' performance.

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Crystals, And After-Treatments Of Crystals (AREA)
  • Moulding By Coating Moulds (AREA)

Abstract

The present invention relates to an apparatus for metal casting and can be used in producing castings with directional and single crystal structure. The apparatus comprises a vacuum chamber (12) inside which there is disposed an induction melting furnace (15), a mold preheating furnace (9) with a ceramic mold (1), and a water-cooled tank (6) being shaped as a truncated cone having a bottom portion (16) and an upper portion (17) which is opened towards a heating zone (10). The heating zone (10) and the cooling zone (13) are separated by a baffle (5) articulating in a horizontal plane and consisting of segments or sectors. The apparatus allows the production of high quality castings having the directional and single crystal structure including the large sized castings by both the method of radiation cooling and the method of liquid metal cooling. Said invention gives the possibility to use successively the disclosed apparatus as a mold catch basin in the event of mold breakage and to increase the reliability and economic profitability of the apparatus' performance.

Description

FIELD OF THE INVENTION
The present invention relates to metal casting and can be used in producing castings with directional and single crystal structure. In particular the invention relates to a metal casting apparatus with a water-cooled tank having a truncated cone shape.
BACKGROUND OF THE INVENTION
An apparatus for directional solidification generally comprises a vacuum chamber inside which there are disposed a mold heating zone, a baffle system, a water-cooled chill plate usually made of copper, an induction furnace, and a thermocouple system that automatically controlls and maintains the temperature in a cooling zone and in a heating zone within the furnace. Such features are disclosed in U.S. Patent Nos 3680625, 4804311, and 4412577.
Also known in the art is an apparatus for directional solidification, in which the cooling zone is a liquid cooling bath with a material that melts easily to serve the role of the cooling medium. The liquid metal bath is disclosed in U.S. Patent Nos 3763926 and 3915761, and Russian Federation Patent No 2010672.
Apparatuses in which both types of the above mentioned assemblies are combined (i.e., the copper chill plate and the liquid metal cooling bath) are also known. But those apparatuses comprise two actuators for vertical transportation of a mold with a metal casting. These actuators are disposed above and beneath the vacuum chamber housing. For that reason the dimensions of the apparatuses are enlarged and the service of the installations become complicated while the reliability of the apparatuses is decreased (see U.S. Patent 5197531, and the publication Singer R.F. "Directional and Single Crystal Solidification Using LMC").
The closest prior art to the present invention is an apparatus disclosed in French Patent Application 2604378, being accepted as a prototype. This prototype apparatus comprises a vacuum chamber with a heating member inside where there is disposed a ceramic mold fixed on a water-cooled metallic plate which is moved up and down with the help of a rod and of an actuator for vertical transportation. A horizontal baffle separates a heating zone and a cooling zone. In the cooling zone, concentrically with the chill plate, there is disposed an additional circular water-cooled cavity with the inner diameter exceeding the mold's maximal size. Below the cavity there is disposed a container which is utilized for capturing the poured casting metal in the event of mold breakage.
The above apparatuses, including the prototype, can function only when they comprise a crystallizer. It is impossible to use such installation for directional solidification processing with a liquid metal coolant and it is difficult to utilize the expensive alloys used in directional solidification castings in the event of mold breakage. Thus there is a need for a casting apparatus that provides a means that efficiently cools the molten cast alloy while protecting the equipment from damage in the event that the ceramic mold breaks while containing the molten cast alloy material.
SUMMARY OF THE INVENTION
The technical aim of this invention is to produce castings having the directional and single crystal structure by the method of radiation cooling without using the above-mentioned crystallizer. Another aim of the invention is to be able to reconstruct easily the invented apparatus for both radiation crystallization processing and liquid metal cooling crystallization processing. The inventive apparatus also increases the reliability and economic profit due to the apparatus' performance.
To achieve said aim the invention comprises an apparatus in accordance with claim 1 hereof and a method in accordance with claim 9. In one embodiment, the inventive apparatus comprises a vacuum chamber inside which there is disposed an induction melting furnace, a mold preheating furnace with a ceramic mold, a drive assembly for mold transportation and a water-cooled tank. The drive assembly comprises a rod on which the mold is fixed with the help of a hanger and a regulating actuator for vertical movement being positioned above the vacuum chamber. The water-cooled tank is shaped as a truncated cone. Its upper portion is opened towards the heating zone, and its bottom portion has a smaller base than the upper portion. A baffle separates the heating zone inside the induction furnace from the cooling zone; said baffle moves in a horizontal plane and closely adjoins the mold during the solidification process. It consists of the segments or sectors (not less than 2 from each side).
BRIEF DESCRIPTION OF THE DRAWING
  • Fig.1 shows a schematic drawing of the apparatus where I is the ceramic mold, 2 is the hanger to fix the mold to the drive assembly, 3 is the rod, 4 is the heater of the mold preheating furnace, 5 is the heat baffle, 6 is the water cooled tank, 7 is the molten superalloy, and 8 is the starting zone with a seed.
  • DESCRIPTION OF THE INVENTION
    The apparatus performs as follows: the mold (1) is disposed on the hanger (2) and is fixed on the movable rod (3). The hanger (2), the movable rod (3), and the regulating actuator comprise the drive assembly (14). The mold (1) is placed into the mold preheater furnace (9) with the help of the actuator while regulating the mold position relative to the heater (4). The heat baffle (5) is disposed under the heating zone (10). The top butt end of the water-cooled tank (6) adjoins the baffle's (5) lower surface and is positioned coaxially with the heater (4) and (11). The vacuum chamber (12) is evacuated to 1 x 10-3 mm m.c. The mold preheating furnace (9) is switched on. Upon reaching the mold temperature of 100-150 °C higher than the liquidus temperature of the alloy being cast, the induction furnace's heater (11) is switched on, the alloy (7) being cast melts and is poured into the heated ceramic mold at the predetermined temperature. After that, the actuator for vertical transportation lowers the mold from the heating zone (10) into the cooling zone (13) at the required rate. Solidification of the molten cast alloy occurs by radiation onto the cold walls of the water-cooled tank. Due to this fact it becomes possible to produce large sized castings with directional and single crystal microstructure. Large size castings can include blades, nozzles, buckets, airfoils, and the like, that are used both in aircraft and land-based turbine engines. The castings are often greater than 30 inches in overall height.
    Once the mold with the casting alloy has been lowered along its complete height into the cooling zone, the heater (4 and 11) is switched off. When the temperature is decreased to 300-400 °C, the mold with the solidified casting alloy is extracted from the installation which has been previously decompressed. Then the process is repeated for the next mold.
    In another aspect of this invention, in order to produce blades having single crystal structure with desired orientation, a single crystal seed with proper orientation is positioned into the top of the starting zone (8) of the ceramic mold before it is disposed in the vacuum chamber. Then the mold position is strictly fixed relative to the heater. In such event the seed and the solidified portion of the starting zone serve as a cooling medium, and further solidification of the melt is caused by radiation cooling in the water-cooled tank as stated above. The use of the water-cooled tank instead of a chill plate allows the same or better working efficiency of said tank than that of a chill plate or of the prototype circular water-cooled cavity. At the same time the water-cooled tank of this invention does not require the use of a complex drive assembly with airtight seals.
    As stated above, the heat baffle (5) is used for raising the axial temperature gradient at the solidification front. Said baffle moves in a horizontal plane, closely adjoins the ceramic mold according to its geometry during the solidification process and consists of the segments or sectors (not less than 2 from each side).
    In the inventive apparatus the water-cooled tank may be made of stainless steel and contain a double layer wall surrounding the perimeter of the tank. A vacuum atmosphere is created in the tank to further aid in the cooling of the cast parts. The tank may also effectively function as a mold catch basin in the event of mold breakage, and the expensive, poured casting alloy may be easily removed from the tapered tank and be remelted.
    The apparatus of this invention allows one to produce high quality castings having the directional and single crystal structure, including the large sized castings used in the land based turbine industry, by the method of radiation cooling without using the crystallizers of the prior art. The invention also gives the possibility to reconstruct easily the disclosed apparatus for liquid metal cooling crystallization processing, to use successively the invented water-cooled tank as a mold catch basin in the event of mold breakage, and to increase the reliability and economic profitability of the apparatus' performance.

    Claims (10)

    1. An apparatus for producing castings, with directional and single crystal structure, the apparatus comprising a vacuum chamber (12) inside which there is positioned an induction melting furnace (15), and a mold preheating furnace (9), a ceramic mold (1) being fixed to a transportation drive assembly (14) comprising a rod (3) and an actuator (14) for vertical movement, cooling means, a baffle (5) separating a heating zone (10) and a water-cooled tank (6) having a closed bottom portion (16) and an upper portion (17) opened towards the heating zone (10), characterised in that the cooling means consists of said water-cooled tank (6) and the actuator is positioned above the vacuum chamber.
    2. The apparatus of claim 1 characterized in that the water-cooled tank (6) is shaped as a truncated cone with its bottom portion (16) having a smaller base than the upper portion (17) of the tank (6).
    3. The apparatus of claim 1 characterized in that a baffle (5) articulates in a horizontal plane and consists of at least two sectors or segments, closely adjoining the ceramic mold (1) during a solidification process.
    4. The apparatus of claim 1 where the drive assembly (14) further comprises a mold hanger (2).
    5. The apparatus of claim 1 where said water-cooled tank (6) can be used as a mold catch basin.
    6. The apparatus of claim 1 where said mold (1) contains a starter cavity (8) for a crystal having a defined crystal orientation.
    7. The apparatus of claim 1 where the water-cooled tank (6) has a double wall.
    8. The apparatus of claim 1 where the water-cooled tank (6) is made of stainless steel.
    9. A method of making a directional or single crystal alloy structure comprising the steps of: placing a mold (1) in a mold preheating furnace (9) relative to a heater (4), the mold being fixed to a transportation drive assembly comprising a rod (3) and an actuator (14) for vertical movement positioned above the vacuum chamber; heating the mold (1) to a temperature of about 100 to 150 °C above the liquidus temperature of a casting alloy; melting the casting alloy; pouring the molten alloy (7) into the heated mold (1); lowering the mold (1) with the molten alloy at a required rate from a heating zone (10) into a cooling zone (13) consisting of a water-cooled tank (6) comprising a closed bottom portion and an open upper portion with water-cooled walls extending therebetween; and solidifying the molten alloy by radiation onto the water-cooled walls of the tank (6).
    10. The method of claim 9 where the mold (1) passes through a baffle (5) located between the heating zone (10) and the cooling zone (13).
    EP98946047A 1997-09-12 1998-09-14 Method and apparatus for producing directionally solidified castings Expired - Lifetime EP0968065B1 (en)

    Applications Claiming Priority (3)

    Application Number Priority Date Filing Date Title
    RU97115515 1997-09-12
    RU97115515A RU2117550C1 (en) 1997-09-12 1997-09-12 Apparatus for making castings with directed and monocrystalline structure
    PCT/US1998/019021 WO1999012679A1 (en) 1997-09-12 1998-09-14 Method and apparatus for producing directionally solidified castings

    Publications (2)

    Publication Number Publication Date
    EP0968065A1 EP0968065A1 (en) 2000-01-05
    EP0968065B1 true EP0968065B1 (en) 2004-12-01

    Family

    ID=20197238

    Family Applications (1)

    Application Number Title Priority Date Filing Date
    EP98946047A Expired - Lifetime EP0968065B1 (en) 1997-09-12 1998-09-14 Method and apparatus for producing directionally solidified castings

    Country Status (5)

    Country Link
    EP (1) EP0968065B1 (en)
    AT (1) ATE283746T1 (en)
    DE (1) DE69827932D1 (en)
    RU (1) RU2117550C1 (en)
    WO (1) WO1999012679A1 (en)

    Cited By (3)

    * Cited by examiner, † Cited by third party
    Publication number Priority date Publication date Assignee Title
    CN103394674A (en) * 2013-07-24 2013-11-20 西安工程大学 Vacuum induction furnace for casting thin-wall castings and method of casting thin-wall titanium alloy castings
    US8752611B2 (en) 2011-08-04 2014-06-17 General Electric Company System and method for directional casting
    CN106180589A (en) * 2016-07-19 2016-12-07 柳州三木科技有限公司 A kind of forging method of seeder wheel hub

    Families Citing this family (9)

    * Cited by examiner, † Cited by third party
    Publication number Priority date Publication date Assignee Title
    EP1162016B1 (en) * 2000-05-13 2004-07-21 ALSTOM Technology Ltd Apparatus for casting a directionally solidified article
    KR100416303B1 (en) * 2000-12-28 2004-01-31 이재현 apparatus of a part manufacture used for directionally solidification
    US6896030B2 (en) 2003-07-30 2005-05-24 Howmet Corporation Directional solidification method and apparatus
    CN102278881A (en) * 2011-08-12 2011-12-14 上海理工大学 Vacuum induction melting furnace capable of realizing rapid solidification
    CN112157245B (en) * 2020-09-03 2022-03-29 中国科学院金属研究所 Method for controlling oriented columnar crystal grains in process of preparing large-size oriented blade by utilizing LMC (melt-spinning-casting) oriented solidification technology
    RU2754215C1 (en) * 2020-11-02 2021-08-30 Федеральное государственное унитарное предприятие "Всероссийский научно-исследовательский институт авиационных материалов" (ФГУП "ВИАМ") Device for producing large-sized castings with directional and single-crystal structure
    RU2754333C1 (en) * 2021-03-02 2021-09-01 Акционерное общество «ОДК-Авиадвигатель» Method for manufacturing ceramic shell molds for casting according to smelted models of turbine blades with a directional and single-crystal structure
    CN114734024A (en) * 2022-03-31 2022-07-12 上海元定科技有限公司 Liquid metal cooling vacuum precision casting furnace and working method
    CN114505467B (en) * 2022-04-06 2022-07-01 太原科技大学 Aluminum alloy casting mold and method utilizing electromagnetic induction to supplement temperature

    Family Cites Families (12)

    * Cited by examiner, † Cited by third party
    Publication number Priority date Publication date Assignee Title
    US3532155A (en) * 1967-12-05 1970-10-06 Martin Metals Co Process for producing directionally solidified castings
    US3680625A (en) * 1970-11-12 1972-08-01 Trw Inc Heat reflector
    US3915761A (en) * 1971-09-15 1975-10-28 United Technologies Corp Unidirectionally solidified alloy articles
    US3763926A (en) * 1971-09-15 1973-10-09 United Aircraft Corp Apparatus for casting of directionally solidified articles
    FR2604378B1 (en) * 1978-06-30 1989-10-27 Snecma FOUNDRY APPARATUS FOR THE MANUFACTURE OF MOLDED METAL PARTS WITH ORIENTED STRUCTURE
    US4804311A (en) * 1981-12-14 1989-02-14 United Technologies Corporation Transverse directional solidification of metal single crystal articles
    US4412577A (en) * 1982-01-27 1983-11-01 United Technologies Corporation Control of seed melt-back during directional solidification of metals
    US5197531A (en) * 1990-06-13 1993-03-30 Leybold Aktiengesellschaft Method of manufacturing directionally solidified castings
    RU2010672C1 (en) * 1991-02-15 1994-04-15 Всероссийский научно-исследовательский институт авиационных материалов Method of producing monocrystalline castings
    EP0631832B1 (en) * 1993-07-02 1998-05-20 ALD Vacuum Technologies GmbH Method and apparatus for directional solidification of a metal melt
    DE19539770A1 (en) * 1995-06-20 1997-01-02 Abb Research Ltd Process for producing a directionally solidified casting and device for carrying out this process
    DE19602554C1 (en) * 1996-01-25 1997-09-18 Ald Vacuum Techn Gmbh Method and device for the simultaneous casting and directional solidification of several castings

    Cited By (5)

    * Cited by examiner, † Cited by third party
    Publication number Priority date Publication date Assignee Title
    US8752611B2 (en) 2011-08-04 2014-06-17 General Electric Company System and method for directional casting
    US9597728B2 (en) 2011-08-04 2017-03-21 General Electric Company System and article of manufacture for directional casting
    CN103394674A (en) * 2013-07-24 2013-11-20 西安工程大学 Vacuum induction furnace for casting thin-wall castings and method of casting thin-wall titanium alloy castings
    CN103394674B (en) * 2013-07-24 2016-01-13 西安工程大学 The method of casting thin foundry goods vaccum sensitive stove and casting thin-wall titanium alloy foundry goods
    CN106180589A (en) * 2016-07-19 2016-12-07 柳州三木科技有限公司 A kind of forging method of seeder wheel hub

    Also Published As

    Publication number Publication date
    EP0968065A1 (en) 2000-01-05
    WO1999012679A1 (en) 1999-03-18
    ATE283746T1 (en) 2004-12-15
    DE69827932D1 (en) 2005-01-05
    RU2117550C1 (en) 1998-08-20

    Similar Documents

    Publication Publication Date Title
    US4838340A (en) Continuous casting of fine grain ingots
    EP1375034A2 (en) Method and apparatus for directional solidification of a metal melt
    EP0968065B1 (en) Method and apparatus for producing directionally solidified castings
    US20110094705A1 (en) Methods for centrifugally casting highly reactive titanium metals
    EP2921244A1 (en) Method of the directional solidification of the castings of gas turbine blades and a device for producing the castings of gas turbine blades of the directional solidified and monocrystalline structure
    US4515204A (en) Continuous metal casting
    EP1531020B1 (en) Method for casting a directionally solidified article
    DE102014113806B4 (en) Method and device for producing DS / SC castings
    US3248764A (en) Method for improving grain structure and soundness in castings
    EP0471798A1 (en) Induction skull melt spinning of reactive metal alloys.
    US6003587A (en) Casting furnace, a casting method and a turbine blade made thereby
    US3939895A (en) Method for casting directionally solidified articles
    US6715534B1 (en) Method and apparatus for producing directionally solidified castings
    CN100406161C (en) Oriented freezing cast method
    EP0209593B1 (en) Continuous casting method
    US4712604A (en) Apparatus for casting directionally solidified articles
    US6557618B1 (en) Apparatus and method for producing castings with directional and single crystal structure and the article according to the method
    JPS61199569A (en) Light alloy ingot direct chilled casting device
    US3921698A (en) Method for the production of metallic ingots
    RU2123909C1 (en) Method of producing castings with oriented crystallization and device for its embodiment
    RU2623941C2 (en) Method of obtaining large-dimensional castings from heat-resistant alloys by directed crystalization
    JP4366705B2 (en) Ingot manufacturing method and apparatus
    RU2754215C1 (en) Device for producing large-sized castings with directional and single-crystal structure
    JPH0531571A (en) Method and apparatus for manufacturing casting
    RU2319752C2 (en) Method for induction melting of metal and apparatus for performing the same

    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

    17P Request for examination filed

    Effective date: 19990920

    AK Designated contracting states

    Kind code of ref document: A1

    Designated state(s): AT BE CH CY DE DK ES FI FR GB GR IE IT LI LU MC NL PT SE

    17Q First examination report despatched

    Effective date: 20020809

    GRAP Despatch of communication of intention to grant a patent

    Free format text: ORIGINAL CODE: EPIDOSNIGR1

    GRAS Grant fee paid

    Free format text: ORIGINAL CODE: EPIDOSNIGR3

    GRAA (expected) grant

    Free format text: ORIGINAL CODE: 0009210

    AK Designated contracting states

    Kind code of ref document: B1

    Designated state(s): AT BE CH CY DE DK ES FI FR GB GR IE IT LI LU MC NL PT SE

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

    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: 20041201

    Ref country code: LI

    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: 20041201

    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 PRE;WARNING: LAPSES OF ITALIAN PATENTS WITH EFFECTIVE DATE BEFORE 2007 MAY HAVE OCCURRED AT ANY TIME BEFORE 2007. THE CORRECT EFFECTIVE DATE MAY BE DIFFERENT FROM THE ONE RECORDED.SCRIBED TIME-LIMIT

    Effective date: 20041201

    Ref country code: FR

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

    Effective date: 20041201

    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: 20041201

    Ref country code: CH

    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: 20041201

    Ref country code: BE

    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: 20041201

    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: 20041201

    REG Reference to a national code

    Ref country code: GB

    Ref legal event code: FG4D

    REG Reference to a national code

    Ref country code: CH

    Ref legal event code: EP

    REG Reference to a national code

    Ref country code: IE

    Ref legal event code: FG4D

    REF Corresponds to:

    Ref document number: 69827932

    Country of ref document: DE

    Date of ref document: 20050105

    Kind code of ref document: P

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

    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: 20050301

    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: 20050301

    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: 20050301

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

    Ref country code: DE

    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: 20050302

    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 FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

    Effective date: 20050312

    NLV1 Nl: lapsed or annulled due to failure to fulfill the requirements of art. 29p and 29m of the patents act
    REG Reference to a national code

    Ref country code: CH

    Ref legal event code: PL

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

    Ref country code: MC

    Payment date: 20050819

    Year of fee payment: 8

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

    Ref country code: GB

    Payment date: 20050908

    Year of fee payment: 8

    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: 20050914

    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: 20050914

    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: 20050930

    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: 20050902

    EN Fr: translation not filed
    REG Reference to a national code

    Ref country code: IE

    Ref legal event code: MM4A

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

    Ref country code: MC

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

    Effective date: 20060930

    GBPC Gb: european patent ceased through non-payment of renewal fee

    Effective date: 20060914

    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: 20060914

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

    Ref country code: PT

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

    Effective date: 20050501