[go: up one dir, main page]

US20030213575A1 - Melting crucible and method - Google Patents

Melting crucible and method Download PDF

Info

Publication number
US20030213575A1
US20030213575A1 US10/146,461 US14646102A US2003213575A1 US 20030213575 A1 US20030213575 A1 US 20030213575A1 US 14646102 A US14646102 A US 14646102A US 2003213575 A1 US2003213575 A1 US 2003213575A1
Authority
US
United States
Prior art keywords
liner body
melted
chamber section
metallic charge
melting
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.)
Abandoned
Application number
US10/146,461
Inventor
Thomas Todaro
Mark Tarby
Jason Andruchowitz
John Astrab
Robert Bayles
Edward Bornemann
James Maslen
Evan Miller
George Normann
Albert Osagie-Erese
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.)
Howmet Corp
Original Assignee
Howmet Research Corp
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 Howmet Research Corp filed Critical Howmet Research Corp
Priority to US10/146,461 priority Critical patent/US20030213575A1/en
Assigned to HOWMET RESEARCH CORPORATION reassignment HOWMET RESEARCH CORPORATION ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: TODARO, THOMAS J., ASTRAB, JOHN M., ANDRUCHOWITZ, JASON S., BAYLES, ROBERT H., BORNEMANN, EDWARD W., MASLEN, JAMES D., MILLER, EVAN R., NORMANN, GEORGE J., OSAGIE-ERESE, ALBERT, TARBY, MARK K.
Priority to JP2003124639A priority patent/JP2003343979A/en
Priority to EP03010450A priority patent/EP1365201A1/en
Publication of US20030213575A1 publication Critical patent/US20030213575A1/en
Abandoned legal-status Critical Current

Links

Images

Classifications

    • CCHEMISTRY; METALLURGY
    • C21METALLURGY OF IRON
    • C21CPROCESSING OF PIG-IRON, e.g. REFINING, MANUFACTURE OF WROUGHT-IRON OR STEEL; TREATMENT IN MOLTEN STATE OF FERROUS ALLOYS
    • C21C5/00Manufacture of carbon-steel, e.g. plain mild steel, medium carbon steel or cast steel or stainless steel
    • C21C5/52Manufacture of steel in electric furnaces
    • C21C5/5241Manufacture of steel in electric furnaces in an inductively heated furnace
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22BPRODUCTION AND REFINING OF METALS; PRETREATMENT OF RAW MATERIALS
    • C22B9/00General processes of refining or remelting of metals; Apparatus for electroslag or arc remelting of metals
    • C22B9/003General processes of refining or remelting of metals; Apparatus for electroslag or arc remelting of metals by induction
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F27FURNACES; KILNS; OVENS; RETORTS
    • F27BFURNACES, KILNS, OVENS OR RETORTS IN GENERAL; OPEN SINTERING OR LIKE APPARATUS
    • F27B14/00Crucible or pot furnaces
    • F27B14/04Crucible or pot furnaces adapted for treating the charge in vacuum or special atmosphere
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F27FURNACES; KILNS; OVENS; RETORTS
    • F27BFURNACES, KILNS, OVENS OR RETORTS IN GENERAL; OPEN SINTERING OR LIKE APPARATUS
    • F27B14/00Crucible or pot furnaces
    • F27B14/06Crucible or pot furnaces heated electrically, e.g. induction crucible furnaces with or without any other source of heat
    • F27B14/061Induction furnaces
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F27FURNACES; KILNS; OVENS; RETORTS
    • F27BFURNACES, KILNS, OVENS OR RETORTS IN GENERAL; OPEN SINTERING OR LIKE APPARATUS
    • F27B14/00Crucible or pot furnaces
    • F27B14/08Details specially adapted for crucible or pot furnaces
    • F27B14/10Crucibles
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F27FURNACES; KILNS; OVENS; RETORTS
    • F27DDETAILS OR ACCESSORIES OF FURNACES, KILNS, OVENS OR RETORTS, IN SO FAR AS THEY ARE OF KINDS OCCURRING IN MORE THAN ONE KIND OF FURNACE
    • F27D1/00Casings; Linings; Walls; Roofs
    • F27D1/0003Linings or walls
    • F27D1/0006Linings or walls formed from bricks or layers with a particular composition or specific characteristics
    • HELECTRICITY
    • H05ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
    • H05BELECTRIC HEATING; ELECTRIC LIGHT SOURCES NOT OTHERWISE PROVIDED FOR; CIRCUIT ARRANGEMENTS FOR ELECTRIC LIGHT SOURCES, IN GENERAL
    • H05B6/00Heating by electric, magnetic or electromagnetic fields
    • H05B6/02Induction heating
    • H05B6/22Furnaces without an endless core
    • H05B6/24Crucible furnaces
    • H05B6/26Crucible furnaces using vacuum or particular gas atmosphere
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F27FURNACES; KILNS; OVENS; RETORTS
    • F27DDETAILS OR ACCESSORIES OF FURNACES, KILNS, OVENS OR RETORTS, IN SO FAR AS THEY ARE OF KINDS OCCURRING IN MORE THAN ONE KIND OF FURNACE
    • F27D3/00Charging; Discharging; Manipulation of charge
    • F27D3/14Charging or discharging liquid or molten material
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F27FURNACES; KILNS; OVENS; RETORTS
    • F27DDETAILS OR ACCESSORIES OF FURNACES, KILNS, OVENS OR RETORTS, IN SO FAR AS THEY ARE OF KINDS OCCURRING IN MORE THAN ONE KIND OF FURNACE
    • F27D3/00Charging; Discharging; Manipulation of charge
    • F27D3/15Tapping equipment; Equipment for removing or retaining slag
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02PCLIMATE CHANGE MITIGATION TECHNOLOGIES IN THE PRODUCTION OR PROCESSING OF GOODS
    • Y02P10/00Technologies related to metal processing
    • Y02P10/25Process efficiency

Definitions

  • the present invention relates to melting of a metal or alloy in a crucible and to a crucible assembly for such melting.
  • Induction melting crucibles are known in the metal casting art for melting a charge of metal or alloy.
  • An induction melting crucible typically includes a ceramic crucible around which an induction coil is disposed to heat and melt a solid metal or alloy charge.
  • a refractory material is packed on the inside of the induction coil to form a recess for receiving the crucible.
  • the crucible may be mounted on trunnions and tilted about the trunnion axis to pour a molten metal charge over a lip of the crucible into an underlying mold or other molten metal receiving vessel.
  • the crucible may include a discharge opening in the bottom wall thereof and a stopper rod, plug or other closure mechanism to prevent release of the molten metal from the crucible through the discharge opening to an underlying mold or other molten metal receiving vessel until the molten metal or alloy is at a proper casting temperature.
  • the melt of superalloy contained in the crucible can include dross and other contaminants floating on the melt surface.
  • Dross typically comprises metal oxides that migrate to and float on the melt surface.
  • Other contaminants on or in the melted charge can include non-metallic inclusions, such as metal nitrides, sulfides and the like and unreacted crucible particulate material. It is desirable to reduce the amount of dross and other contaminants floating on the melt surface that are poured from the crucible into the investment mold where they ultimately may adversely affect the quality of the superalloy casting produced in the investment mold.
  • the present invention provides in one embodiment a method of melting and pouring successive metallic charges, such as for example oxygen-reactive nickel base superalloys or cobalt base superalloys, comprising positioning a metallic charge in a disposable, self-supporting refractory vessel, melting the metallic charge in the vessel under vacuum or a protective atmosphere such as for example an inert gas, nitrogen, etc., pouring the melted metallic charge from the vessel, discarding the vessel, and melting the next metallic charge in a clean, new refractory vessel.
  • metallic charges such as for example oxygen-reactive nickel base superalloys or cobalt base superalloys
  • the present invention provides in another embodiment a melting method and a melting crucible assembly that involve positioning a disposable (non-reusable), self-supporting refractory liner body in a refractory host crucible and melting a metallic charge such as, for example, a solid nickel or cobalt base superalloy charge in the liner residing in the host crucible.
  • a metallic charge such as, for example, a solid nickel or cobalt base superalloy charge in the liner residing in the host crucible.
  • the melted metallic charge is poured from the refractory liner body into a mold, and the used (spent) refractory liner body is removed from the host crucible for discarding and replaced with a clean, new (unused) refractory liner body in the host crucible for melting the next metallic charge therein.
  • the disposable refractory liner body comprises a tubular body having a closed bottom wall to form an internal chamber.
  • a partition wall is present in the internal chamber of the liner body to provide a melting chamber section and a pouring chamber section communicated to one another at a location disposed below an existing level of melted metallic charge (melt level) in the liner body.
  • a pour opening is disposed in a cover that partially overlies the pouring chamber section and is connected to the uppermost end of the partition wall.
  • the partition wall is configured such that clean melted metallic charge below the existing melt level flows to the pouring chamber section when the crucible assembly is tilted, while dross and other contaminants floating on the melt surface in the melting chamber section remain confined in that chamber section.
  • FIG. 1 is a sectional view of a melting crucible assembly, with the liner body shown in elevation, taken along lines 1 - 1 of FIG. 2 in accordance with an illustrative embodiment of the invention.
  • FIG. 2 is a plan view of a melting crucible assembly in accordance with an illustrative embodiment of the invention.
  • the support tray for the melting crucible assembly is omitted for convenience.
  • FIG. 3 is a plan view of the refractory liner body.
  • FIG. 4 is a sectional view taken along lines 4 - 4 of FIG. 3 of the refractory liner body.
  • FIG. 5 is an isometric view of the refractory liner body.
  • FIG. 6 is a sectional view of the crucible assembly with a solid ingot shown in elevation received in a recess on the partition wall of the refractory liner body tilted to a near horizontal position.
  • FIG. 7 is a view showing melted metallic material being poured from the liner body into a mold.
  • FIG. 8 is a longitudinal sectional view of a melting vessel in accordance with another illustrative embodiment of the invention.
  • FIGS. 1 - 7 illustrate schematically a melting crucible assembly 10 for melting a solid metallic charge, such as a metal or alloy.
  • the solid metallic charge can be in the form an ingot, billet, sponge, particulates, and other available material forms.
  • the melting crucible assembly 10 is especially useful and beneficial to heat and melt a solid metallic charge (e.g. an ingot or billet) comprising an oxygen-reactive nickel base superalloy or cobalt base superalloy in chamber C.
  • Nickel base superalloys and cobalt base superalloys are well known and widely used in making investment cast gas turbine engine components having an equiaxed grain microstructure or a directionally solidified microstructure that includes a columnar grain microstructure or single crystal. Such superalloys are described herein as oxygen-reactive in the sense that the superalloys usually include alloying elements that are prone to react with or have a high affinity for oxygen at melting temperatures employed.
  • nickel base and cobalt base superalloys include, but are not limited to, CMSX-3, CMSX-4, INCONEL 625, STELLITE 25, and STELLITE 31 superalloys and others (see for example U.S. Pat. Nos.
  • the chamber C can have a vacuum (subambient pressure) of about 100 microns and below, such as about 1 to about 10 microns, therein or a substantially oxygen-free protective atmosphere, such as inert gas, nitrogen, and the like that is non-reactive with the melted superalloy.
  • the protective atmosphere may be present in chamber C at a partial pressure less than atmospheric pressure, at or near atmospheric pressure, or at a positive pressure greater than atmospheric pressure for melting a superalloy charge.
  • the melting crucible assembly 10 is shown including an induction coil 12 disposed about a refractory host crucible 14 and a refractory liner body 16 disposed in the host crucible and functioning a melting vessel in which a solid charge CH of a metallic material is heated and melted.
  • the induction coil 12 is supported on a metal or other support tray 13 , which is rotatable about axis A of a shaft 13 a connected to the support tray to position the crucible assembly in a near horizontal position to receive a solid metallic charge (e.g.
  • a solid ingot or billet CH to be melted and to an upstanding position where the solid metallic charge is melted in the refractory liner body (melting vessel) 16 by energizing the induction coil 12 .
  • induction coil 12 instead of using induction coil 12 to heat and melt the metallic charge in the refractory liner body, electrical resistance heating/melting, gas fired heating/melting, electron beam heating/melting, or any other means for heating and melting the metallic charge in the refractory liner body 16 can be cooperatively positioned in chamber C relative to the metallic charge in practice of the invention.
  • the host crucible 12 resides in a bed of packed refractory grog particulates 18 .
  • the grog particulates 18 in turn are received in refractory shell 20 applied to the interior of the induction coil 12 .
  • the refractory shell 20 can be formed by manually applying a refractory mud or grout to the interior of the induction coil 12 and hardening the refractory mud by curing a resin binder or other type of binder therein in conventional manner.
  • the refractory shell 20 is first formed on the interior of the induction coil 12 .
  • the bottom of grog particulates 18 is placed on the bottom of shell 20 followed by positioning of the host crucible 14 on the grog particulates 18 .
  • Additional grog particulates then are introduced and packed into the annular space between the upstanding wall of the host crucible 14 and the upstanding wall of the refractory shell 20 with the grog particulates topped off with a layer 22 of thermal insulation, such as KAOWOOL insulation.
  • the disposable refractory liner body (melting vessel) 16 is received in the host crucible 14 in a manner that the liner body 16 can be readily placed in the host crucible and subsequently removed from the host crucible after a metallic charge has been melted and poured from the crucible assembly.
  • the refractory liner body 16 thus comprises a disposable (non-reusable or throw-away) liner body that is used only one time to melt a metallic charge, then removed, and replaced with a clean, new refractory liner body 16 in the host crucible.
  • the used (spent) refractory liner body 16 will contain a small amount of the unpoured, melted metallic charge with dross and other contaminants such that the used (spent) liner body is discarded and not reused.
  • the refractory liner body (melting vessel) 16 can comprise any suitable refractory material selected in dependence on the metal or alloy to be melted therein.
  • the refractory body liner 16 in melting a conventional nickel base superalloy, can comprise alumina silicate ceramic.
  • the host crucible 14 can comprise zircon or alumina silicate ceramic, while the grog particulates can comprise zirconia particles of ⁇ 10+35 mesh size meaning the grog particles are less than 10 mesh and greater than 35 mesh size using U.S. Standard Sieve system.
  • the refractory shell 20 can comprise castable alumina. The invention is not limited to any particular refractory materials which, as mentioned, are selected in dependence on the metal or alloy to be melted in the liner body 16 .
  • the disposable (non-reusable), refractory liner body (melting vessel) 16 is self-supporting in that it supports its own weight as well as the weight the metallic charge melted therein at the particular melting temperature employed without the need for any mechanical support from the host crucible 14 , which serves only to receive and position the liner body 16 .
  • the refractory liner body 16 is shown having a cylindrical tubular shape with a closed end, although any suitable body shape can be used.
  • the liner body 16 is received with radial clearance G in the host crucible 14 such that the liner body 16 can be readily placed in the host crucible and subsequently removed from the host crucible after a metallic charge has been melted and poured from the crucible assembly.
  • the outer diameter of the liner body 16 is less than the inner diameter of the cylindrical side wall 14 a of the host crucible 14 .
  • the liner body 16 is not connected to the host crucible 14 other than being received therein.
  • the refractory liner body 16 includes annular, cylindrical side wall 16 a and an integral bottom wall 16 b that closes off the end the liner body to form an internal chamber 16 c in the liner body 16 .
  • the liner body includes an integral partition wall 16 d that extends downwardly in the internal chamber 16 c to define or provide a melting chamber section MS and a pouring chamber section PS communicated to one another at a location disposed below the existing level of melted metallic charge (melt level) in the liner body.
  • the liner body 16 includes integral walls 16 w that intersect with partition wall 16 d to form pouring chamber section PS.
  • the partition wall 16 d is shown terminating at its lowermost end a distance above the bottom wall 16 b such that a through-passage 16 p is formed between the melting chamber section MS and a pouring chamber section PS for flow of clean melted metallic material from the melting chamber section MS to the pouring chamber section PS.
  • the partition wall may include openings (not shown) extending therethrough to this same end.
  • the partition wall 16 d is configured to form a scallop or recess 16 r along the side thereof facing the melting chamber section MS.
  • the recess 16 r widens in the direction toward the lowermost end of the partition wall as best shown in FIG. 4.
  • This recess 16 r is adapted to receive and position a cylindrical ingot or billet of solid metallic charge to be melted.
  • the melting crucible assembly 10 can be tilted to place the liner body 16 in a near horizontal position.
  • the cylindrical ingot or billet then can be placed in the recess 16 r on partition wall 16 d , FIG. 6.
  • the melting crucible assembly 10 then can be tilted to place the liner body 16 in an upstanding vertical position for melting of the ingot or billet.
  • the refractory liner 16 includes a cover 16 e that overlies the partition wall 16 d and is connected to the uppermost end of the partition wall 16 d by ceramic cement for example.
  • the cover 16 e includes a discharge or pouring opening 160 through which melted metallic material in the pouring chamber section PS is poured when the crucible assembly 10 is tilted to this end by rotation of support tray 13 by any suitable rotary actuator (not shown) connected to shaft 13 a , FIG. 1.
  • the partition wall 16 d is positioned and configured such that clean melted metallic charge below the existing melt level in melting chamber section MS flows to the pouring chamber section PS when the melting crucible assembly 10 is tilted, while dross and other contaminants floating on the melt surface in the melting chamber section MP remain confined in that chamber section.
  • the cylindrical liner body comprising sidewall 16 a and bottom wall 16 b can be made using conventional ceramic fabrication techniques that include pressed powder and sintering.
  • the walls 16 d , 16 w and cover 16 e are similarly made and connected to the cylindrical body by cementing.
  • the refractory liner body 16 can be used alone as a melting vessel and surrounded by induction coil 12 or otherwise cooperatively positioned relative to any other heating means such as electrical resistance heating elements, gas fired heating elements, electron beam(s) and the like, that can heat and melt the metallic charge CH residing therein as illustrated in FIG. 8.
  • the refractory liner body 16 used as a melting vessel is tilted by rotating tray 13 to pour melted metallic charge therefrom such as, for example, into a mold.
  • the invention is described above with respect to certain embodiments, those skilled in the art will appreciate that modifications and changes can be made therein without departing from the spirit and scope of the invention set forth in the appended claims.

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • General Engineering & Computer Science (AREA)
  • Metallurgy (AREA)
  • Materials Engineering (AREA)
  • Manufacturing & Machinery (AREA)
  • Organic Chemistry (AREA)
  • Physics & Mathematics (AREA)
  • Electromagnetism (AREA)
  • Crucibles And Fluidized-Bed Furnaces (AREA)
  • Casting Support Devices, Ladles, And Melt Control Thereby (AREA)
  • Furnace Details (AREA)

Abstract

A melting method and a melting crucible assembly involve positioning a disposable (non-reusable), self-supporting refractory liner body in a refractory host crucible and melting a metallic charge in the liner residing in the host crucible. The melted metallic charge is poured from the refractory liner body, and the used refractory liner body is removed from the host crucible for discarding and replaced with a clean, new (unused) refractory liner body in the host crucible for melting the next metallic charge therein.

Description

    FIELD OF THE INVENTION
  • The present invention relates to melting of a metal or alloy in a crucible and to a crucible assembly for such melting. [0001]
  • BACKGROUND OF THE INVENTION
  • Induction melting crucibles are known in the metal casting art for melting a charge of metal or alloy. An induction melting crucible typically includes a ceramic crucible around which an induction coil is disposed to heat and melt a solid metal or alloy charge. A refractory material is packed on the inside of the induction coil to form a recess for receiving the crucible. The crucible may be mounted on trunnions and tilted about the trunnion axis to pour a molten metal charge over a lip of the crucible into an underlying mold or other molten metal receiving vessel. Alternatively, the crucible may include a discharge opening in the bottom wall thereof and a stopper rod, plug or other closure mechanism to prevent release of the molten metal from the crucible through the discharge opening to an underlying mold or other molten metal receiving vessel until the molten metal or alloy is at a proper casting temperature. [0002]
  • In the vacuum induction melting of oxygen-reactive nickel base superalloys and cobalt base superalloys used to investment cast gas turbine engine components, such as turbine blades, vanes and other components, the melt of superalloy contained in the crucible can include dross and other contaminants floating on the melt surface. Dross typically comprises metal oxides that migrate to and float on the melt surface. Other contaminants on or in the melted charge can include non-metallic inclusions, such as metal nitrides, sulfides and the like and unreacted crucible particulate material. It is desirable to reduce the amount of dross and other contaminants floating on the melt surface that are poured from the crucible into the investment mold where they ultimately may adversely affect the quality of the superalloy casting produced in the investment mold. [0003]
  • SUMMARY OF THE INVENTION
  • The present invention provides in one embodiment a method of melting and pouring successive metallic charges, such as for example oxygen-reactive nickel base superalloys or cobalt base superalloys, comprising positioning a metallic charge in a disposable, self-supporting refractory vessel, melting the metallic charge in the vessel under vacuum or a protective atmosphere such as for example an inert gas, nitrogen, etc., pouring the melted metallic charge from the vessel, discarding the vessel, and melting the next metallic charge in a clean, new refractory vessel. [0004]
  • The present invention provides in another embodiment a melting method and a melting crucible assembly that involve positioning a disposable (non-reusable), self-supporting refractory liner body in a refractory host crucible and melting a metallic charge such as, for example, a solid nickel or cobalt base superalloy charge in the liner residing in the host crucible. The melted metallic charge is poured from the refractory liner body into a mold, and the used (spent) refractory liner body is removed from the host crucible for discarding and replaced with a clean, new (unused) refractory liner body in the host crucible for melting the next metallic charge therein. [0005]
  • In a particular embodiment of the invention, the disposable refractory liner body comprises a tubular body having a closed bottom wall to form an internal chamber. A partition wall is present in the internal chamber of the liner body to provide a melting chamber section and a pouring chamber section communicated to one another at a location disposed below an existing level of melted metallic charge (melt level) in the liner body. A pour opening is disposed in a cover that partially overlies the pouring chamber section and is connected to the uppermost end of the partition wall. The partition wall is configured such that clean melted metallic charge below the existing melt level flows to the pouring chamber section when the crucible assembly is tilted, while dross and other contaminants floating on the melt surface in the melting chamber section remain confined in that chamber section. Use of a clean, new refractory liner body for melting each respective metallic charge and the flow of the melted metallic charge from the melting chamber section to the pouring chamber section reduces the amount of dross and other contaminants that will be poured from the pouring chamber section into a mold. [0006]
  • The above and other objects and advantages of the present invention will become more readily apparent from the following drawings taken in conjunction with the following detailed description.[0007]
  • DESCRIPTION OF THE DRAWINGS
  • FIG. 1 is a sectional view of a melting crucible assembly, with the liner body shown in elevation, taken along lines [0008] 1-1 of FIG. 2 in accordance with an illustrative embodiment of the invention.
  • FIG. 2 is a plan view of a melting crucible assembly in accordance with an illustrative embodiment of the invention. The support tray for the melting crucible assembly is omitted for convenience. [0009]
  • FIG. 3 is a plan view of the refractory liner body. [0010]
  • FIG. 4 is a sectional view taken along lines [0011] 4-4 of FIG. 3 of the refractory liner body.
  • FIG. 5 is an isometric view of the refractory liner body. [0012]
  • FIG. 6 is a sectional view of the crucible assembly with a solid ingot shown in elevation received in a recess on the partition wall of the refractory liner body tilted to a near horizontal position. [0013]
  • FIG. 7 is a view showing melted metallic material being poured from the liner body into a mold. [0014]
  • FIG. 8 is a longitudinal sectional view of a melting vessel in accordance with another illustrative embodiment of the invention.[0015]
  • DESCRIPTION OF THE INVENTION
  • FIGS. [0016] 1-7 illustrate schematically a melting crucible assembly 10 for melting a solid metallic charge, such as a metal or alloy. The solid metallic charge can be in the form an ingot, billet, sponge, particulates, and other available material forms. For purposes of illustration and not limitation, the melting crucible assembly 10 is especially useful and beneficial to heat and melt a solid metallic charge (e.g. an ingot or billet) comprising an oxygen-reactive nickel base superalloy or cobalt base superalloy in chamber C. Nickel base superalloys and cobalt base superalloys are well known and widely used in making investment cast gas turbine engine components having an equiaxed grain microstructure or a directionally solidified microstructure that includes a columnar grain microstructure or single crystal. Such superalloys are described herein as oxygen-reactive in the sense that the superalloys usually include alloying elements that are prone to react with or have a high affinity for oxygen at melting temperatures employed. For purposes of illustration and not limitation, nickel base and cobalt base superalloys include, but are not limited to, CMSX-3, CMSX-4, INCONEL 625, STELLITE 25, and STELLITE 31 superalloys and others (see for example U.S. Pat. Nos. 4,582,548 and 4,643,782). The chamber C can have a vacuum (subambient pressure) of about 100 microns and below, such as about 1 to about 10 microns, therein or a substantially oxygen-free protective atmosphere, such as inert gas, nitrogen, and the like that is non-reactive with the melted superalloy. The protective atmosphere may be present in chamber C at a partial pressure less than atmospheric pressure, at or near atmospheric pressure, or at a positive pressure greater than atmospheric pressure for melting a superalloy charge.
  • The [0017] melting crucible assembly 10 is shown including an induction coil 12 disposed about a refractory host crucible 14 and a refractory liner body 16 disposed in the host crucible and functioning a melting vessel in which a solid charge CH of a metallic material is heated and melted. The induction coil 12 is supported on a metal or other support tray 13, which is rotatable about axis A of a shaft 13 a connected to the support tray to position the crucible assembly in a near horizontal position to receive a solid metallic charge (e.g. a solid ingot or billet) CH to be melted and to an upstanding position where the solid metallic charge is melted in the refractory liner body (melting vessel) 16 by energizing the induction coil 12. In lieu of using induction coil 12 to heat and melt the metallic charge in the refractory liner body, electrical resistance heating/melting, gas fired heating/melting, electron beam heating/melting, or any other means for heating and melting the metallic charge in the refractory liner body 16 can be cooperatively positioned in chamber C relative to the metallic charge in practice of the invention.
  • The host crucible [0018] 12 resides in a bed of packed refractory grog particulates 18. The grog particulates 18 in turn are received in refractory shell 20 applied to the interior of the induction coil 12. The refractory shell 20 can be formed by manually applying a refractory mud or grout to the interior of the induction coil 12 and hardening the refractory mud by curing a resin binder or other type of binder therein in conventional manner. The refractory shell 20 is first formed on the interior of the induction coil 12. Then, the bottom of grog particulates 18 is placed on the bottom of shell 20 followed by positioning of the host crucible 14 on the grog particulates 18. Additional grog particulates then are introduced and packed into the annular space between the upstanding wall of the host crucible 14 and the upstanding wall of the refractory shell 20 with the grog particulates topped off with a layer 22 of thermal insulation, such as KAOWOOL insulation.
  • The disposable refractory liner body (melting vessel) [0019] 16 is received in the host crucible 14 in a manner that the liner body 16 can be readily placed in the host crucible and subsequently removed from the host crucible after a metallic charge has been melted and poured from the crucible assembly. The refractory liner body 16 thus comprises a disposable (non-reusable or throw-away) liner body that is used only one time to melt a metallic charge, then removed, and replaced with a clean, new refractory liner body 16 in the host crucible. The used (spent) refractory liner body 16 will contain a small amount of the unpoured, melted metallic charge with dross and other contaminants such that the used (spent) liner body is discarded and not reused.
  • The refractory liner body (melting vessel) [0020] 16 can comprise any suitable refractory material selected in dependence on the metal or alloy to be melted therein. For example, for purposes of illustration and not limitation, in melting a conventional nickel base superalloy, the refractory body liner 16 can comprise alumina silicate ceramic. The host crucible 14 can comprise zircon or alumina silicate ceramic, while the grog particulates can comprise zirconia particles of −10+35 mesh size meaning the grog particles are less than 10 mesh and greater than 35 mesh size using U.S. Standard Sieve system. The refractory shell 20 can comprise castable alumina. The invention is not limited to any particular refractory materials which, as mentioned, are selected in dependence on the metal or alloy to be melted in the liner body 16.
  • The disposable (non-reusable), refractory liner body (melting vessel) [0021] 16 is self-supporting in that it supports its own weight as well as the weight the metallic charge melted therein at the particular melting temperature employed without the need for any mechanical support from the host crucible 14, which serves only to receive and position the liner body 16.
  • For purposes of illustration and not limitation, the [0022] refractory liner body 16 is shown having a cylindrical tubular shape with a closed end, although any suitable body shape can be used. The liner body 16 is received with radial clearance G in the host crucible 14 such that the liner body 16 can be readily placed in the host crucible and subsequently removed from the host crucible after a metallic charge has been melted and poured from the crucible assembly. To this end, the outer diameter of the liner body 16 is less than the inner diameter of the cylindrical side wall 14 a of the host crucible 14. The liner body 16 is not connected to the host crucible 14 other than being received therein.
  • The [0023] refractory liner body 16 includes annular, cylindrical side wall 16 a and an integral bottom wall 16 b that closes off the end the liner body to form an internal chamber 16 c in the liner body 16. The liner body includes an integral partition wall 16 d that extends downwardly in the internal chamber 16 c to define or provide a melting chamber section MS and a pouring chamber section PS communicated to one another at a location disposed below the existing level of melted metallic charge (melt level) in the liner body. The liner body 16 includes integral walls 16 w that intersect with partition wall 16 d to form pouring chamber section PS. For purposes of illustration and not limitation, the partition wall 16 d is shown terminating at its lowermost end a distance above the bottom wall 16 b such that a through-passage 16 p is formed between the melting chamber section MS and a pouring chamber section PS for flow of clean melted metallic material from the melting chamber section MS to the pouring chamber section PS. Alternatively, the partition wall may include openings (not shown) extending therethrough to this same end.
  • The [0024] partition wall 16 d is configured to form a scallop or recess 16 r along the side thereof facing the melting chamber section MS. The recess 16 r widens in the direction toward the lowermost end of the partition wall as best shown in FIG. 4. This recess 16 r is adapted to receive and position a cylindrical ingot or billet of solid metallic charge to be melted. In particular, the melting crucible assembly 10 can be tilted to place the liner body 16 in a near horizontal position. The cylindrical ingot or billet then can be placed in the recess 16 r on partition wall 16 d, FIG. 6. The melting crucible assembly 10 then can be tilted to place the liner body 16 in an upstanding vertical position for melting of the ingot or billet.
  • The [0025] refractory liner 16 includes a cover 16 e that overlies the partition wall 16 d and is connected to the uppermost end of the partition wall 16 d by ceramic cement for example. The cover 16 e includes a discharge or pouring opening 160 through which melted metallic material in the pouring chamber section PS is poured when the crucible assembly 10 is tilted to this end by rotation of support tray 13 by any suitable rotary actuator (not shown) connected to shaft 13 a, FIG. 1.
  • The [0026] partition wall 16 d is positioned and configured such that clean melted metallic charge below the existing melt level in melting chamber section MS flows to the pouring chamber section PS when the melting crucible assembly 10 is tilted, while dross and other contaminants floating on the melt surface in the melting chamber section MP remain confined in that chamber section. Use of a vacuum or protective atmosphere in chamber C together with a clean, new refractory liner body 16 for melting each respective metallic charge as well as the flow of the melted metallic charge from the melting chamber section MS to the pouring chamber section PS under the partition wall 16 d reduces the amount of dross and other contaminants that will be poured from the pouring chamber section into a mold M, such as an investment mold, that will be positioned beneath the melting crucible assembly 10 in chamber C to receive the melted metallic charge as described, for example, in U.S. Pat. No. 5,226,946, which is incorporated herein by reference.
  • The cylindrical liner body comprising sidewall [0027] 16 a and bottom wall 16 b can be made using conventional ceramic fabrication techniques that include pressed powder and sintering. The walls 16 d, 16 w and cover 16 e are similarly made and connected to the cylindrical body by cementing.
  • Although the invention has been described in detail above with respect to the [0028] refractory liner body 16 being disposed in host crucible 14 that resides in refractory particulates 18 and refractory shell 20, the invention is not so limited. The refractory liner body 16 can be used alone as a melting vessel and surrounded by induction coil 12 or otherwise cooperatively positioned relative to any other heating means such as electrical resistance heating elements, gas fired heating elements, electron beam(s) and the like, that can heat and melt the metallic charge CH residing therein as illustrated in FIG. 8. The refractory liner body 16 used as a melting vessel is tilted by rotating tray 13 to pour melted metallic charge therefrom such as, for example, into a mold. Moreover, although the invention is described above with respect to certain embodiments, those skilled in the art will appreciate that modifications and changes can be made therein without departing from the spirit and scope of the invention set forth in the appended claims.

Claims (27)

We claim
1. A method of melting and pouring successive metallic charges, comprising positioning a metallic charge in a disposable, self-supporting refractory vessel, melting the metallic charge in said vessel under vacuum or a protective atmosphere, pouring the melted metallic charge from said vessel, discarding said vessel, and melting a next metallic charge in a clean, new refractory vessel under a vacuum or protective atmosphere.
2. The method of claim 1 wherein the metallic charge comprising a nickel base superalloy or a cobalt base superalloy is melted in a melting chamber section in said liner body.
3. The method of claim 2 wherein the melted metallic charge is poured from a pouring chamber section communicated to said melting chamber section in said liner body at a location below a melt level of the melted metallic charge in said liner body.
4. The method of claim 1 wherein said metallic charge is melted by energizing an induction coil disposed about said vessel.
5. The method of claim 1 wherein the melted metallic charge is melted under a protective atmosphere selected from inert gas or nitrogen.
7. A method of melting and pouring a metallic charge, comprising positioning a metallic charge in a disposable refractory liner body residing in a refractory host crucible, melting the metallic charge in said liner body, pouring the melted metallic charge from said liner body, removing said liner body from said host crucible, and placing a clean, new refractory liner body to melt the next metallic charge.
7. The method of claim 6 wherein the metallic charge comprising a nickel base superalloy or cobalt base superalloy is melted in a melting chamber section in said liner body.
8. The method of claim 7 wherein the melted metallic charge is poured from a pouring chamber section communicated to said melting chamber section in said liner body at a location below a level of the melted metallic charge in said liner body.
9. The method of claim 6 wherein said metallic charge is melted by energizing an induction coil disposed about the host crucible.
10. The method of claim 6 wherein the melted metallic charge is poured into a mold.
11. A melting crucible assembly comprising a refractory host crucible, and a disposable, self-supporting refractory liner body disposed in the host crucible and in which a metallic charge is melted, said liner body including a partition wall that forms a melting chamber section and a pouring chamber section communicated to one another at a location disposed below a melt level of a melted metallic charge in said liner body such that melted metallic charge below said level flows from the melting chamber section to the pouring chamber section when said crucible assembly is tilted.
7. The assembly of claim 6 including an induction coil about the host crucible.
8. The assembly of claim 6 wherein said host crucible resides in a bed of refractory grog particulates.
9. The assembly of claim 6 wherein said liner body is received in said host crucible with clearance that allows said liner body to be removed from said host crucible after said metallic charge has been melted and poured.
10. The assembly of claim 6 wherein said liner body has a cylindrical tubular shape.
11. The assembly of claim 10 wherein said liner body has an outer diameter that is less than an inner diameter of a cylindrical side wall of said host crucible.
12. The assembly of claim 6 wherein said partition wall extends downwardly in said liner body when it is oriented in an upstanding position.
13. The assembly of claim 12 wherein said partition wall terminates at its lowermost end a distance above a bottom wall of said liner body such that a passage is formed between said melting chamber section and said pouring chamber section for flow of clean melted metallic material from said melting chamber section to said pouring chamber section.
14. The assembly of claim 6 wherein said partition wall is configured to form a recess along a side thereof facing said melting chamber section.
15. The assembly of claim 14 wherein said recess is adapted to receive and position a cylindrical ingot or billet of said metallic charge material.
16. The assembly of claim 6 wherein said liner body includes a cover that is connected to the uppermost end of said partition wall, said cover including an opening through which melted metallic charge in said pouring chamber section is poured when said crucible assembly is tilted.
17. The combination of a melting vessel in a chamber having a vacuum or a protective atmosphere therein, comprising a disposable, self-supporting refractory vessel in which a metallic charge comprising a nickel base superalloy or cobalt base superalloy is melted, said vessel including a partition wall that forms a melting chamber section and a pouring chamber section communicated to one another at a location disposed below a melt level of melted metallic charge in said vessel such that melted metallic charge below said level flows from the melting chamber section to the pouring chamber section when said vessel is tilted.
18. The combination of claim 17 wherein said vessel is received in said host crucible with clearance that allows said vessel to be removed from said host crucible after said metallic charge has been melted and poured.
19. The combination of claim 17 wherein said partition wall extends downwardly in said liner body when it is oriented in an upstanding position.
20. The combination of claim 19 wherein said partition wall terminates at its lowermost end a distance above a bottom wall of said liner body such that a passage is formed between said melting chamber section and said pouring chamber section for flow of clean melted metallic material from said melting chamber section to said pouring chamber section.
21. The combination of claim 17 wherein said partition wall is configured to form a recess along a side thereof facing said melting chamber section, said recess being adapted to receive and position a cylindrical ingot or billet of said metallic charge material.
22. The combination of claim 17 wherein said vessel includes a cover that is connected to the uppermost end of said partition wall, said cover including an opening through which melted metallic charge in said pouring chamber section is poured when said crucible assembly is tilted.
US10/146,461 2002-05-14 2002-05-14 Melting crucible and method Abandoned US20030213575A1 (en)

Priority Applications (3)

Application Number Priority Date Filing Date Title
US10/146,461 US20030213575A1 (en) 2002-05-14 2002-05-14 Melting crucible and method
JP2003124639A JP2003343979A (en) 2002-05-14 2003-04-30 Melting crucible and its method
EP03010450A EP1365201A1 (en) 2002-05-14 2003-05-09 Melting crucible and method

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US10/146,461 US20030213575A1 (en) 2002-05-14 2002-05-14 Melting crucible and method

Publications (1)

Publication Number Publication Date
US20030213575A1 true US20030213575A1 (en) 2003-11-20

Family

ID=29400470

Family Applications (1)

Application Number Title Priority Date Filing Date
US10/146,461 Abandoned US20030213575A1 (en) 2002-05-14 2002-05-14 Melting crucible and method

Country Status (3)

Country Link
US (1) US20030213575A1 (en)
EP (1) EP1365201A1 (en)
JP (1) JP2003343979A (en)

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102192649A (en) * 2010-10-15 2011-09-21 中国南方航空工业(集团)有限公司 Crucible basket for vacuum smelting furnace and manufacturing method of crucible basket
US20120300806A1 (en) * 2011-05-23 2012-11-29 Prabhu Satyen N Electric Induction Furnace with Lining Wear Detection System
US20140174341A1 (en) * 2011-08-05 2014-06-26 Plansee Se Crucible for growing crystals
US20140369375A1 (en) * 2012-01-23 2014-12-18 Apple Inc. Boat and coil designs
US20150360267A1 (en) * 2013-02-18 2015-12-17 Commissariat à l'énergie atomique et aux énergies alternatives Induction furnace and method for treating metal waste to be stored
US10598439B2 (en) * 2011-05-23 2020-03-24 Inductotherm Corp. Electric induction furnace lining wear detection system
IT202300003093A1 (en) * 2023-02-22 2024-08-22 Orotig S P A INDUCTION CASTING MACHINE

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103827048B (en) * 2011-08-05 2017-05-10 科卢斯博知识产权有限公司 Crucible material
WO2014123801A1 (en) * 2013-02-05 2014-08-14 Sachsisolar, Inc. Crucible liner
TW201529203A (en) * 2014-01-28 2015-08-01 jia-long You Method of manufacturing replaceable stove and product thereof
JP6397834B2 (en) * 2016-01-06 2018-09-26 クルーシブル インテレクチュアル プロパティ エルエルシーCrucible Intellectual Property Llc Crucible material
CN106007339B (en) * 2016-05-11 2018-08-28 蔡春祥 A kind of composite material induction electrical crucible
CN106152789A (en) * 2016-08-08 2016-11-23 无锡蠡湖增压技术股份有限公司 A kind of aluminum liquid stove vacuum heat-preserving set

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4444377A (en) * 1982-07-14 1984-04-24 Daniel E. Groteke Molten metal transfer crucible
US5425047A (en) * 1992-06-03 1995-06-13 Leybold Durferrit Gmbh Closed induction furnace with a tilting apparatus

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB578977A (en) * 1944-06-23 1946-07-18 Stone J & Co Ltd Improvements in the treatment of magnesium base alloys and the production of pressure die-castings therefrom
US3401227A (en) * 1966-02-09 1968-09-10 Trw Inc Liner for crucibles
US5226946A (en) * 1992-05-29 1993-07-13 Howmet Corporation Vacuum melting/casting method to reduce inclusions
US5416795A (en) * 1994-05-20 1995-05-16 Kaniuk; John A. Quick change crucible for vacuum melting furnace

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4444377A (en) * 1982-07-14 1984-04-24 Daniel E. Groteke Molten metal transfer crucible
US5425047A (en) * 1992-06-03 1995-06-13 Leybold Durferrit Gmbh Closed induction furnace with a tilting apparatus

Cited By (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102192649A (en) * 2010-10-15 2011-09-21 中国南方航空工业(集团)有限公司 Crucible basket for vacuum smelting furnace and manufacturing method of crucible basket
US20120300806A1 (en) * 2011-05-23 2012-11-29 Prabhu Satyen N Electric Induction Furnace with Lining Wear Detection System
US9400137B2 (en) * 2011-05-23 2016-07-26 Inductotherm Corp. Electric induction furnace with lining wear detection system
US10598439B2 (en) * 2011-05-23 2020-03-24 Inductotherm Corp. Electric induction furnace lining wear detection system
US20140174341A1 (en) * 2011-08-05 2014-06-26 Plansee Se Crucible for growing crystals
US20140369375A1 (en) * 2012-01-23 2014-12-18 Apple Inc. Boat and coil designs
CN104540618A (en) * 2012-01-23 2015-04-22 苹果公司 Boat and coil designs
US9544949B2 (en) * 2012-01-23 2017-01-10 Apple Inc. Boat and coil designs
US20150360267A1 (en) * 2013-02-18 2015-12-17 Commissariat à l'énergie atomique et aux énergies alternatives Induction furnace and method for treating metal waste to be stored
US9662693B2 (en) * 2013-02-18 2017-05-30 Commissariat A L'energie Atomique Et Aux Energies Alternatives Induction furnace and method for treating metal waste to be stored
IT202300003093A1 (en) * 2023-02-22 2024-08-22 Orotig S P A INDUCTION CASTING MACHINE
WO2024176041A1 (en) * 2023-02-22 2024-08-29 Orotig S.P.A. Method for melting methods and induction furnace

Also Published As

Publication number Publication date
JP2003343979A (en) 2003-12-03
EP1365201A1 (en) 2003-11-26

Similar Documents

Publication Publication Date Title
EP0604703B1 (en) Method for Making Intermetallic Castings
US20030213575A1 (en) Melting crucible and method
US8906170B2 (en) Alloy castings having protective layers and methods of making the same
JP5530093B2 (en) A heat-resistant crucible that can manage thermal stress and is suitable for melting highly reactive alloys
US8210240B2 (en) Casting processes, casting apparatuses therefor, and castings produced thereby
US4240495A (en) Method of making cast metal turbine wheel with integral radial columnar grain blades and equiaxed grain disc
US9381569B2 (en) Vacuum or air casting using induction hot topping
RU2146184C1 (en) Method and apparatus for directional crystallization of melt
EP0897769A1 (en) Mold heating vacuum casting furnace
KR20080097137A (en) Reinforced refractory crucibles for melting titanium alloys
US5607007A (en) Directional solidification apparatus and method
US5335717A (en) Oxidation resistant superalloy castings
US4436485A (en) Turbine wheel with integral DS blades and equiaxed hub
JP5925411B2 (en) Casting process and yttria-containing facecoat material therefor
EP1375033A1 (en) Investment casting under pressure
EP2208556B1 (en) Casting molds for use in directional solidification processes and methods of making
Rakoczy et al. Effect of cobalt aluminate content and pouring temperature on macrostructure, tensile strength and creep rupture of Inconel 713C castings
WO2009072217A1 (en) Immersion nozzle and method of continuous casting
JP3194354B2 (en) Precision casting method and precision casting device
RU2142352C1 (en) Method for investment casting
JP2005121289A (en) Melting holding furnace and melting method of material to be melted
JP2007326111A (en) Immersion nozzle and continuous casting method
JP2737130B2 (en) Unidirectional / single crystal solidification equipment
GB2222972A (en) Shroud seal insert
MXPA99006861A (en) INTEGRATED CRUCIBLE AND MOLD FOR LOW COST&ggr;-TiAl CASTINGS

Legal Events

Date Code Title Description
AS Assignment

Owner name: HOWMET RESEARCH CORPORATION, MICHIGAN

Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNORS:TODARO, THOMAS J.;TARBY, MARK K.;ANDRUCHOWITZ, JASON S.;AND OTHERS;REEL/FRAME:013299/0808;SIGNING DATES FROM 20020805 TO 20020816

STCB Information on status: application discontinuation

Free format text: ABANDONED -- FAILURE TO RESPOND TO AN OFFICE ACTION