US3678988A - Incorporation of dispersoids in directionally solidified castings - Google Patents

Incorporation of dispersoids in directionally solidified castings Download PDF

Info

Publication number
US3678988A
US3678988A US51793A US3678988DA US3678988A US 3678988 A US3678988 A US 3678988A US 51793 A US51793 A US 51793A US 3678988D A US3678988D A US 3678988DA US 3678988 A US3678988 A US 3678988A
Authority
US
United States
Prior art keywords
alloy
mold
particles
solidification
molten
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
US51793A
Inventor
John K Tien
Stephen M Copley
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.)
Raytheon Technologies Corp
Original Assignee
United Aircraft 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 United Aircraft Corp filed Critical United Aircraft Corp
Application granted granted Critical
Publication of US3678988A publication Critical patent/US3678988A/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
    • B22D27/08Shaking, vibrating, or turning of moulds

Definitions

  • ABSTRACT Inert particles are uniformly dispersed within a molten alloy while it is being directionally solidified in a mold to cause a uniform dispersion within the casting, the dispersion being produced by ultrasonic waves within the molten alloyduring solidification.
  • One feature of the invention is a process for mixing the particles uniformly in the alloy and for maintaining the uniformed dispersion of the particles during the directional solidification. Another feature is the use of ultrasonic waves generated in the liquid phase of the alloy to maintain a uniform dispersion and to force the particles against the solidification front to incorporate such particles within the solid phase.
  • Another feature of the invention is a mold apparatus by which the inert particles may be kept in a substantially uniform dispersion while the alloy in the mold is being directionally solidified.
  • the particles which may be nonwettable by the alloy are mixed with the alloy as by a flow of an inert gas stream carrying the particles.
  • the particles are caused to be uniformly dispersed by ultrasonic waves generated in the molten alloy and are kept mixed during directional solidification of the alloy toward the source of the waves, this source being at the end of the mold opposite to the chill plate from which the directional solidification starts and progresses toward the ultrasonic probe which is positioned in the molten alloy and is the source of the waves. These waves force the particles and into the solid liquid interface.
  • FIG. I is a diagrammatic view of a mold apparatus for casting the alloy.
  • FIG. 2 is a diagrammatic showing of the system.
  • the mold that may be used in the incorporation of dispersed particles in the casting includes a growth portion 2 resting on a chill plate 4 and communicating at its upper end with a root portion 8 of the mold.
  • the mold shown is used in casting a turbine blade and the mold provides as well as the root forcing portion 8 a platform portion 10, an airfoil shaped blade portion 12, and a shroud forming portion 14 at the upper end of the blade portion. Above the shroud is the open upper end 16 of the mold which permits filling of the mold in the casting process.
  • the mold is positioned within a susceptor l8 surrounded in turn by a heating coil 20.
  • the latter may be an induction coil preferably tapped midway of its ends as at 22 in order to provide a separate temperature control for the top and bottom portions of the mold.
  • the susceptor rests on the chill plate, being insulated therefrom by a suitable insulating ring 26.
  • a probe 28 Positioned in the upper end of the mold during the casting of the article therein is a probe 28 by which ultrasonic waves may be generated within the molten alloy during the solidification process. Obviously the probe 28 is in such a position that it may be removed from the liquid alloy before the solidification front reaches a point to encompass the probe. Also shown, but in dotted lines, is a tube 30 which is projected downwardly into the mold and is used for the distribution of the particles into the poured alloy before solidification of the alloy begins. This tube is removed after the particles have been dispersed within the molten alloy so that it is not a pan of the mold and does not remain therein during the solidification.
  • a suitable alloy which has been melted and raised to a super heat of about 50 F above the melting point is poured into the mold after the latter has in turn been heated by the surrounding heating coils to a temperature above the melting point of the alloy also preferably at least 50 F above the melting point.
  • the tube 30 is inserted in the molten alloy and the particles are forced into the molten alloy as for example by a stream of inert gas under pressure in which the particles are carried in suspension.
  • the ultrasonic waves established by the probe 28 serve to mix the particles uniformly throughout the molten alloy in the mold.
  • the ultrasonic waves serve to keep the particles uniformly dispersed within the molten alloy and also serve to force the particles against and into the liquid solid interface as the interface progresses upwardly from the chill plate toward the top of the mold.
  • FIG. 2 the apparatus by which the invention may be carried out is shown as applied to a mold 32 for making an ingot although obviously an article mold as in FIG. 1 may as readily be used.
  • This mold is positioned on a chill plate 34 and is surrounded by the susceptor 36 which in turn is heated by axially aligned induction coils 38 and 40.
  • the induction coils are separately heated as shown for controlling the cooling of the mold.
  • the particles to be mixed with the molten metal are supplied from a hopper 42 through an aspirator 44 such that argon or other inert gas supplied through a pipe 46 having a valve 48 therein will pick up the individual particles and deliver them through a refractory tube 48 into the molten metal within the ingot mold 32.
  • the tube is shown as projecting nearly to the bottom of the ingot and it is apparent that the effect of the inert gas carrying the particles is to assure a mixing to some extent of the particles within the molten metal.
  • the tube 48 is withdrawn and an ultrasonic vibration is set up by a refractory probe 50 immersed in the molten alloy. It has been found that approximately a 20 kilocycle frequency is acceptable. Higher power levels are used during the mixing than are used during the solidification after the mixing is completed.
  • the probe may be supported with its tip in the molten alloy from a retracting support structure 52 providing for removal of the probe as the liquid-solid interface approached the tip of the probe during solidification.
  • the probe may be energized from a variable frequency and power generator and controller 54.

Abstract

Inert particles are uniformly dispersed within a molten alloy while it is being directionally solidified in a mold to cause a uniform dispersion within the casting, the dispersion being produced by ultrasonic waves within the molten alloy during solidification.

Description

United States Patent Tien et al.
[ 51 July 25,1972
INCORPORATION OF DISPERSOIDS IN DIRECTIONALLY SOLIDIFIED CASTINGS Inventors: John K. Tlen, Rocky Hill; Stephen M. Copley, Madison, both of Conn.
United Aircraft Corporation, East Hartford, Conn.
Filed: July 2, 1970 Appl. No.: 51,793
Assignee:
US. Cl ..l64/49, 164/55, 164/97 Int. Cl ..B22d 27/02 Field of Search ..l64/48, 49, 97, 250, 55
References Cited UNITED STATES PATENTS 7/1966 Ver Snyder 164/60 X @QQQQQ 3,045,302 7/l962 Patton 164/49 OTHER PUBLICATIONS Hiedemann, Metallurgical Effects of Ultrasonic Waves, .lournal of the Acoustical Society of America, Vol. 26, No. 45, Sept. I954 pp. 83 l- 842 Primary Examiner-J. Spencer Overholser Assistant Examiner-John E. Roethel Attorney-Charles A. Warren [57] ABSTRACT Inert particles are uniformly dispersed within a molten alloy while it is being directionally solidified in a mold to cause a uniform dispersion within the casting, the dispersion being produced by ultrasonic waves within the molten alloyduring solidification.
7 Claims, 2 Drawing Figures INCORPORATION OF DISPERSOIDS IN DIRECTIONALLY SOLIDIFIED CASTINGS BACKGROUND OF THE INVENTION Metals and alloys have been strengthened by a dispersion of inert particles within the alloy, one example of which is a nickel alloy within which thoria particles have been dispersed. Several methods have been used without complete success in obtaining uniformity of particle dispersion particularly when such particles are not wettable by the alloy in which they are embedded. This is particularly true in the plane front mode of solidification or in the cellular front mode.
STATEMENT OF THE INVENTION One feature of the invention is a process for mixing the particles uniformly in the alloy and for maintaining the uniformed dispersion of the particles during the directional solidification. Another feature is the use of ultrasonic waves generated in the liquid phase of the alloy to maintain a uniform dispersion and to force the particles against the solidification front to incorporate such particles within the solid phase.
Another feature of the invention is a mold apparatus by which the inert particles may be kept in a substantially uniform dispersion while the alloy in the mold is being directionally solidified.
According to the invention the particles which may be nonwettable by the alloy are mixed with the alloy as by a flow of an inert gas stream carrying the particles. The particles are caused to be uniformly dispersed by ultrasonic waves generated in the molten alloy and are kept mixed during directional solidification of the alloy toward the source of the waves, this source being at the end of the mold opposite to the chill plate from which the directional solidification starts and progresses toward the ultrasonic probe which is positioned in the molten alloy and is the source of the waves. These waves force the particles and into the solid liquid interface.
BRIEF DESCRIPTION OF THE DRAWINGS FIG. I is a diagrammatic view of a mold apparatus for casting the alloy.
FIG. 2 is a diagrammatic showing of the system.
Referring first to FIG. 1, the mold that may be used in the incorporation of dispersed particles in the casting includes a growth portion 2 resting on a chill plate 4 and communicating at its upper end with a root portion 8 of the mold. The mold shown is used in casting a turbine blade and the mold provides as well as the root forcing portion 8 a platform portion 10, an airfoil shaped blade portion 12, and a shroud forming portion 14 at the upper end of the blade portion. Above the shroud is the open upper end 16 of the mold which permits filling of the mold in the casting process.
The mold is positioned within a susceptor l8 surrounded in turn by a heating coil 20. The latter may be an induction coil preferably tapped midway of its ends as at 22 in order to provide a separate temperature control for the top and bottom portions of the mold. The susceptor rests on the chill plate, being insulated therefrom by a suitable insulating ring 26.
Positioned in the upper end of the mold during the casting of the article therein is a probe 28 by which ultrasonic waves may be generated within the molten alloy during the solidification process. Obviously the probe 28 is in such a position that it may be removed from the liquid alloy before the solidification front reaches a point to encompass the probe. Also shown, but in dotted lines, is a tube 30 which is projected downwardly into the mold and is used for the distribution of the particles into the poured alloy before solidification of the alloy begins. This tube is removed after the particles have been dispersed within the molten alloy so that it is not a pan of the mold and does not remain therein during the solidification.
In the casting process, a suitable alloy which has been melted and raised to a super heat of about 50 F above the melting point is poured into the mold after the latter has in turn been heated by the surrounding heating coils to a temperature above the melting point of the alloy also preferably at least 50 F above the melting point. Before solidification begins, the tube 30 is inserted in the molten alloy and the particles are forced into the molten alloy as for example by a stream of inert gas under pressure in which the particles are carried in suspension. During the supply of the particles tothe molten alloy and after the particles have been mixed with the alloy, the ultrasonic waves established by the probe 28 serve to mix the particles uniformly throughout the molten alloy in the mold. As the solidification of the alloy begins and progresses upwardly through the article forming portion of the mold the ultrasonic waves serve to keep the particles uniformly dispersed within the molten alloy and also serve to force the particles against and into the liquid solid interface as the interface progresses upwardly from the chill plate toward the top of the mold.
Referring now to FIG. 2 the apparatus by which the invention may be carried out is shown as applied to a mold 32 for making an ingot although obviously an article mold as in FIG. 1 may as readily be used. This mold is positioned on a chill plate 34 and is surrounded by the susceptor 36 which in turn is heated by axially aligned induction coils 38 and 40. The induction coils are separately heated as shown for controlling the cooling of the mold.
The particles to be mixed with the molten metal are supplied from a hopper 42 through an aspirator 44 such that argon or other inert gas supplied through a pipe 46 having a valve 48 therein will pick up the individual particles and deliver them through a refractory tube 48 into the molten metal within the ingot mold 32. The tube is shown as projecting nearly to the bottom of the ingot and it is apparent that the effect of the inert gas carrying the particles is to assure a mixing to some extent of the particles within the molten metal.
After the particles are dispersed within the molten metal the tube 48 is withdrawn and an ultrasonic vibration is set up by a refractory probe 50 immersed in the molten alloy. It has been found that approximately a 20 kilocycle frequency is acceptable. Higher power levels are used during the mixing than are used during the solidification after the mixing is completed.
The probe may be supported with its tip in the molten alloy from a retracting support structure 52 providing for removal of the probe as the liquid-solid interface approached the tip of the probe during solidification. The probe may be energized from a variable frequency and power generator and controller 54.
After sufficient time is allowed for uniform distribution of the particles through the molten alloy, directional solidification is initiated within the ingot by reducing or terminating the energy supply to the lower heating coil and allowing the effect of the water-cooled chill plate to establish columnar grain growth upwardly from the plate. As solidification proceeds the ultrasonic waves force the particles against the liquid-solid interface while maintaining a uniform distribution of the particles within the bulk of the liquid phase of the alloy. Although it is not established why there is a force acting on the particles at the interface the existence of this force has been demonstrated and the existence of the force has also be measured experimentally. Obviously as solidification proceeds, the probe is kept above the liquid-solid interface so that it does not become a part of the casting. Furthermore the tube through which the particles are introduced to the molten alloy will have been removed prior to the start of solidification.
We claim 1. In the dispersion of inert particles in a casting during solidification of the alloy of the casting the steps which involve mixing the particles into the molten alloy,
generating ultrasonic waves in the molten alloy to obtain a uniform dispersion of the particles in the molten alloy, and thereafter maintaining a uniform dispersion of the particles by generating ultrasonic waves at a lower level in the molten portion of the alloy during solidification.
2. In the dispersion of inert particles in a directionally solidified casting during solidification of the alloy of the casting within the mold the steps of adding the inert particles to the molten alloy,
generating ultrasonic waves in the molten portion of the alloy to obtain and to maintain a uniform dispersion of the particles in the alloy, and
causing a directional solidification of the alloy from one end of the mold to the other to obtain an oriented grain structure in the cast article.
3. The process of claim 2 with the added steps of causing the directional solidification to occur upwardly by the use of a chill plate at the bottom end of the mold, and
positioning the source of the ultrasonic waves in the molten alloy remote from the chill plate.
4. The process of casting a directionally solidified alloy with inert particles therein including the steps of melting the alloy,
pouring the alloy into the mold,
introducing inert particles into the alloy and mixing the particles in the molten alloy,
generating ultrasonic waves in the molten alloy at one end of the mold as the alloy issolidified, and
simultaneously causing a directional solidification of the alloy from the opposite end in a direction toward the source of the generated waves.
5. The process as in claim 4 in which the directional solidification of the alloy is caused by heat removal from the alloy by a chill plate located at one end of the mold and with the source of the ultrasonic waves located at the end of the mold remote from the-chill plate and external to the part of the casting used as the cast article.
6. The process as in claim 1 including the step of solidifying the alloy within the mold in a direction toward the source of the waves to force the inert particles in the molten alloy against the solidification front.
7. The process as in claim 3 including the step of causing the solidification front to move from the chill plate toward the wave generator such that the particles in the molten alloy are forced against the solidification front to be uniformly embedded within the solidified alloy.

Claims (6)

  1. 2. In the dispersion of inert particles in a directionally solidified casting during solidification of the alloy of the casting within the mold the steps of adding the inert particles to the molten alloy, generating ultrasonic waves in the molten portion of the alloy to obtain and to maintain a uniform dispersion of the particles in the alloy, and causing a directional solidification of the alloy from one end of the mold to the other to obtain an oriented grain structure in the cast article.
  2. 3. The process of claim 2 with the added steps of causing the directional solidification to occur upwardly by the use of a chill plate at the bottom end of the mold, and positioning the source of the ultrasonic waves in the molten alloy remote from the chill plate.
  3. 4. The process of casting a directionally solidified alloy with inert particles therein including the steps of melting the alloy, pouring the alloy into the mold, introducing inert particles into the alloy and mixing the particles in the molten alloy, generating ultrasonic waves in the molten alloy at one end of the mold as the alloy is solidified, and simultaneously causing a directional solidification of the alloy from the opposite end in a direction toward the source of the generated waves.
  4. 5. The process as in claim 4 in which the directional solidification of the alloy is caused by heat removal from the alloy by a chill plate located at one end of the mold and with the source of the ultrasonic waves located at the end of the mold remote from the chill plate and external to the part of the casting used as the cast article.
  5. 6. The process as in claim 1 including the step of solidifying the alloy within the mold in a direction toward the source of the waves to force the inert particles in the molten alloy against the solidification front.
  6. 7. The process as in claim 3 including the step of causing the solidification front to move from the chill plate toward the wave generator such that the particles in the molten alloy are forced against the solidification front to be uniformly embedded within the solidified alloy.
US51793A 1970-07-02 1970-07-02 Incorporation of dispersoids in directionally solidified castings Expired - Lifetime US3678988A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US5179370A 1970-07-02 1970-07-02

Publications (1)

Publication Number Publication Date
US3678988A true US3678988A (en) 1972-07-25

Family

ID=21973409

Family Applications (1)

Application Number Title Priority Date Filing Date
US51793A Expired - Lifetime US3678988A (en) 1970-07-02 1970-07-02 Incorporation of dispersoids in directionally solidified castings

Country Status (1)

Country Link
US (1) US3678988A (en)

Cited By (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
USB511885I5 (en) * 1974-10-03 1976-01-27
US4582117A (en) * 1983-09-21 1986-04-15 Electric Power Research Institute Heat transfer during casting between metallic alloys and a relatively moving substrate
US4683936A (en) * 1984-05-16 1987-08-04 Trw Inc. Controlled solidification, method of distributing strengthening additives and maintaining a constant melt level
FR2666819A1 (en) * 1990-09-19 1992-03-20 Inst Aluminievoi Magnievoi METHOD AND DEVICE FOR MANUFACTURING A COMPOSITE MATERIAL FROM A BASE METAL.
US5228494A (en) * 1992-05-01 1993-07-20 Rohatgi Pradeep K Synthesis of metal matrix composites containing flyash, graphite, glass, ceramics or other metals
US20040016318A1 (en) * 2002-07-23 2004-01-29 General Electric Company Method for making materials having artificially dispersed nano-size phases and articles made therewith
WO2005017220A1 (en) * 2003-08-04 2005-02-24 General Electric Company Method for making materials having artificially dispersed nano-size phases and articles made therewith
US20060157219A1 (en) * 2005-01-18 2006-07-20 Bampton Clifford C Method and system for enhancing the quality of deposited metal
US20080292259A1 (en) * 2007-02-01 2008-11-27 The Boeing Company Multi-color curved multi-light generating apparatus
US7509993B1 (en) * 2005-08-13 2009-03-31 Wisconsin Alumni Research Foundation Semi-solid forming of metal-matrix nanocomposites
EP2241392A1 (en) * 2009-04-16 2010-10-20 General Electric Company Casting Method for super-Alloy and stainless Steel
US20130236352A1 (en) * 2012-03-12 2013-09-12 Xiaochun Li Nanomaterial-based methods and apparatuses
US20140255620A1 (en) * 2013-03-06 2014-09-11 Rolls-Royce Corporation Sonic grain refinement of laser deposits
US9481031B2 (en) 2015-02-09 2016-11-01 Hans Tech, Llc Ultrasonic grain refining
EP2606994A3 (en) * 2011-12-20 2017-08-23 General Electric Company Induction stirred, ultrasonically modified investment castings and apparatus for producing
US10022786B2 (en) 2015-09-10 2018-07-17 Southwire Company Ultrasonic grain refining

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3045302A (en) * 1958-10-20 1962-07-24 Int Nickel Co Casting of metals and alloys
US3260505A (en) * 1963-10-21 1966-07-12 United Aircraft Corp Gas turbine element

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3045302A (en) * 1958-10-20 1962-07-24 Int Nickel Co Casting of metals and alloys
US3260505A (en) * 1963-10-21 1966-07-12 United Aircraft Corp Gas turbine element

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
Hiedemann, Metallurgical Effects of Ultrasonic Waves, Journal of the Acoustical Society of America, Vol. 26, No. 45, Sept. 1954 pp. 831 842 *

Cited By (24)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
USB511885I5 (en) * 1974-10-03 1976-01-27
US3981346A (en) * 1974-10-03 1976-09-21 United Technologies Corporation Method and apparatus for directional solidification
US4582117A (en) * 1983-09-21 1986-04-15 Electric Power Research Institute Heat transfer during casting between metallic alloys and a relatively moving substrate
US4683936A (en) * 1984-05-16 1987-08-04 Trw Inc. Controlled solidification, method of distributing strengthening additives and maintaining a constant melt level
FR2666819A1 (en) * 1990-09-19 1992-03-20 Inst Aluminievoi Magnievoi METHOD AND DEVICE FOR MANUFACTURING A COMPOSITE MATERIAL FROM A BASE METAL.
US5228494A (en) * 1992-05-01 1993-07-20 Rohatgi Pradeep K Synthesis of metal matrix composites containing flyash, graphite, glass, ceramics or other metals
US7465365B1 (en) 2002-07-23 2008-12-16 General Electric Company Method for making materials having artificially dispersed nano-size phases and articles made therewith
US6939388B2 (en) 2002-07-23 2005-09-06 General Electric Company Method for making materials having artificially dispersed nano-size phases and articles made therewith
US20080289727A1 (en) * 2002-07-23 2008-11-27 Thomas Martin Angeliu Method for making materials having artificially dispersed nano-size phases and articles made therewith
US20040016318A1 (en) * 2002-07-23 2004-01-29 General Electric Company Method for making materials having artificially dispersed nano-size phases and articles made therewith
WO2005017220A1 (en) * 2003-08-04 2005-02-24 General Electric Company Method for making materials having artificially dispersed nano-size phases and articles made therewith
US20060157219A1 (en) * 2005-01-18 2006-07-20 Bampton Clifford C Method and system for enhancing the quality of deposited metal
US7509993B1 (en) * 2005-08-13 2009-03-31 Wisconsin Alumni Research Foundation Semi-solid forming of metal-matrix nanocomposites
US20080292259A1 (en) * 2007-02-01 2008-11-27 The Boeing Company Multi-color curved multi-light generating apparatus
US7603017B2 (en) 2007-02-01 2009-10-13 The Boeing Company Multi-color curved multi-light generating apparatus
EP2241392A1 (en) * 2009-04-16 2010-10-20 General Electric Company Casting Method for super-Alloy and stainless Steel
EP2606994A3 (en) * 2011-12-20 2017-08-23 General Electric Company Induction stirred, ultrasonically modified investment castings and apparatus for producing
US20130236352A1 (en) * 2012-03-12 2013-09-12 Xiaochun Li Nanomaterial-based methods and apparatuses
US9273375B2 (en) * 2012-03-12 2016-03-01 Wisconsin Alumni Research Foundation Nanomaterial-based methods and apparatuses
US20140255620A1 (en) * 2013-03-06 2014-09-11 Rolls-Royce Corporation Sonic grain refinement of laser deposits
US9481031B2 (en) 2015-02-09 2016-11-01 Hans Tech, Llc Ultrasonic grain refining
US10441999B2 (en) 2015-02-09 2019-10-15 Hans Tech, Llc Ultrasonic grain refining
US10022786B2 (en) 2015-09-10 2018-07-17 Southwire Company Ultrasonic grain refining
US10639707B2 (en) 2015-09-10 2020-05-05 Southwire Company, Llc Ultrasonic grain refining and degassing procedures and systems for metal casting

Similar Documents

Publication Publication Date Title
US3678988A (en) Incorporation of dispersoids in directionally solidified castings
US9839958B2 (en) Method for induction stirred, ultrasonically modified investment castings
US3690367A (en) Apparatus for the restructuring of metals
US5335711A (en) Process and apparatus for metal casting
US3841384A (en) Method and apparatus for melting and casing metal
US3620289A (en) Method for casting directionally solified articles
GB1369270A (en) Casting of directionally solidified articles
CA1049222A (en) Method of and apparatus for producing metallic castings
JP2003501272A (en) Directional solidification method and apparatus
US3700023A (en) Casting of directionally solidified articles
GB2516992A (en) Applying heat to form a component
US3754592A (en) Method for producing directionally solidified cast alloy articles
CN110421144B (en) Pressure-regulating precision casting method for high-temperature alloy floating wall tile under action of external electromagnetic field
KR100435000B1 (en) Die-casting process for rheocasting method and apparatus thereof
US3667533A (en) Making directionally solidified castings
US3598172A (en) Process of casting with downward-unidirectional solidification
JP3209099B2 (en) Casting apparatus, casting method and turbine blade
US5309976A (en) Continuous pour directional solidification method
US3669180A (en) Production of fine grained ingots for the advanced superalloys
EP0293960B1 (en) Process and apparatus for metal casting
US3625275A (en) Apparatus and method for single-crystal casting
US3712368A (en) Apparatus for making directionally solidified castings
JP3194354B2 (en) Precision casting method and precision casting device
US4683936A (en) Controlled solidification, method of distributing strengthening additives and maintaining a constant melt level
US3543284A (en) Process for casting single crystal shapes