US20180141115A1 - Unit Cell Titanium Casting - Google Patents

Unit Cell Titanium Casting Download PDF

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Publication number
US20180141115A1
US20180141115A1 US15/816,017 US201715816017A US2018141115A1 US 20180141115 A1 US20180141115 A1 US 20180141115A1 US 201715816017 A US201715816017 A US 201715816017A US 2018141115 A1 US2018141115 A1 US 2018141115A1
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Prior art keywords
chamber
internal chamber
evacuated
pressure
external chamber
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US15/816,017
Inventor
Norm Smith
Jan Paraiso
Francisco Dosal
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Topgolf Callaway Brands Corp
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Callaway Golf Co
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Priority to US15/816,017 priority Critical patent/US20180141115A1/en
Publication of US20180141115A1 publication Critical patent/US20180141115A1/en
Abandoned legal-status Critical Current

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    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B22—CASTING; POWDER METALLURGY
    • B22D—CASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
    • B22D21/00—Casting non-ferrous metals or metallic compounds so far as their metallurgical properties are of importance for the casting procedure; Selection of compositions therefor
    • B22D21/002—Castings of light metals
    • B22D21/005—Castings of light metals with high melting point, e.g. Be 1280 degrees C, Ti 1725 degrees C
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B22—CASTING; POWDER METALLURGY
    • B22D—CASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
    • B22D18/00—Pressure casting; Vacuum casting
    • B22D18/06—Vacuum casting, i.e. making use of vacuum to fill the mould
    • A—HUMAN NECESSITIES
    • A63—SPORTS; GAMES; AMUSEMENTS
    • A63B—APPARATUS FOR PHYSICAL TRAINING, GYMNASTICS, SWIMMING, CLIMBING, OR FENCING; BALL GAMES; TRAINING EQUIPMENT
    • A63B53/00—Golf clubs
    • A63B53/04—Heads
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B22—CASTING; POWDER METALLURGY
    • B22D—CASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
    • B22D25/00—Special casting characterised by the nature of the product
    • B22D25/02—Special casting characterised by the nature of the product by its peculiarity of shape; of works of art

Definitions

  • the present invention relates to precision titanium casting. More specifically, the present invention relates to an apparatus and method for precision titanium casting utilizing induction heating.
  • Vacuum electric arc smelting is another method in which a titanium ingot is melted by substantial heat generated by mutual discharging in a high current state by respectively using a titanium ingot crucible and a water-cooled copper crucible as a positive electrode and a negative electrode, thereby forming a molten liquid metal in the crucible and completing the casting of the titanium.
  • Another method is vacuum induction smelting in which an induction coil is wrapped outside a split-type water-cooled copper crucible.
  • the electromagnetic force generated by the induction coil passes through a nonmetal isolation portion between splits of the copper crucible and then acts on a titanium ingot placed inside the crucible. Then the molten metal forms a molten metal liquid inside the crucible and the casting of the titanium is completed.
  • Vacuum induction smelting and vacuum electric arc smelting require the use of a water-cooled copper crucible which results in the loss of substantial heat.
  • the actual power consumed is very little (only 20% to 30% of the power actually acts on the titanium).
  • the preparation of the molding shell is very complex and time consuming, which adds to the costs.
  • the operation time of a single furnace is usually 60 to 80 minutes, and the loading and discharge process requires the coordination of many people.
  • the process from the preparation of the wax pattern to the clearing of the molding shell can take ten days.
  • Titanium is an extremely reactive metal. During melting via traditional casting processes, a water cooling environment is required. The molten titanium liquid will come into direct contact with water if the crucible cracks, resulting in a fierce reaction, or even explosion, which poses a great threat to production safety.
  • a new kind of titanium alloy induction melting vacuum suction casting device is urgently needed, to solve the problems with existing titanium alloy casting, such as low efficiency, high cost, complicated technology, heavy workload, difficulty with preparing high-quality molding shells, long cycle and potential hazard.
  • one of the primary tenets is the use of an induction coil in order to melt the desired material within the crucible.
  • the induction coil will utilize a set power level between 15 and 50 kW in order to melt the target material.
  • the power level is varied during the course of the melt. Optimally, the power begins relatively low with a transition to higher power levels prior to the complete melting of the ingot. The change in power is controlled by a Programmable Logic Controller (PLC), and the transition or transitions in power is/are based off of the melt temperature of the target material.
  • PLC Programmable Logic Controller
  • This process allows for a smooth controllable melt, followed by a period where a significant additional amount of energy can be transferred into the target material before the material is evacuated from the crucible resulting. This allows for a better pattern mold fill, better material properties, and reduced equipment cycle times.
  • One aspect of the present invention is a method for unit cell casting of titanium or titanium-alloys.
  • the method includes positioning a mold within an internal chamber.
  • the method also includes evacuating an external chamber to create an evacuated external chamber wherein a ceramic crucible containing a titanium alloy ingot is positioned therein.
  • the method also includes evacuating the internal chamber to create an evacuated internal chamber having a pressure no greater than 3 ⁇ 10 ⁇ 2 atmosphere.
  • the method also includes injecting a pressurized gas into the evacuated external chamber to create a pressurized external chamber with a pressure in excess of 1 atm.
  • the method also includes melting the titanium alloy ingot within the ceramic crucible utilizing induction heating generated by an induction coil positioned around the ceramic crucible, wherein a power for the induction coil is commences at a first power level of 15 kiloWatts and increases to a second power level greater than 50 kiloWatts.
  • the method also includes transferring the completely melted titanium alloy material into the mold from the crucible using a pressure differential created between the external chamber and the internal chamber. A high pressure differential in maintained between the external chamber and the internal chamber during the transfer of the melted titanium alloy material.
  • the PLC controls power to the induction coil to superheat the titanium alloy ingot in the ceramic crucible.
  • the pressure of the internal chamber and the pressure of the external chamber are monitored and communicated to the PLC during the casting process, and wherein the PLC controls the casting process based on the pressure of the internal chamber and the pressure of the external chamber.
  • Another aspect of the present invention is a system method for unit cell casting of titanium or titanium-alloys.
  • the system comprises an external chamber, a ceramic crucible positioned within the external chamber, an induction coil positioned around a bottom section of the ceramic crucible, an internal chamber positioned within the external chamber, a mold positioned within the internal chamber, a first vacuum gauge positioned within the internal chamber, a second vacuum gauge positioned within the external chamber, a PLC in communication with the first vacuum gauge, the second vacuum gauge, and the induction coil.
  • the pressure of the internal chamber and the pressure of the external chamber are monitored and communicated to the PLC during the casting process, and wherein the PLC controls the casting process based on the pressure of the internal chamber and the pressure of the external chamber.
  • the external chamber is evacuated to create an evacuated external chamber wherein the ceramic crucible contains a titanium alloy ingot positioned therein.
  • a pressurized gas is injected into the evacuated external chamber to create a pressurized external chamber.
  • the titanium alloy ingot is melted within the ceramic crucible utilizing induction heating generated by the induction coil positioned around the ceramic crucible, wherein a power for the induction coil is commences at a first power level of 15 kiloWatts and increases to a second power level greater than 50 kiloWatts.
  • the internal chamber is evacuated to create an evacuated internal chamber.
  • the titanium alloy material is completely transferred into the mold from the crucible using a maximum pressure differential created between the external chamber and the internal chamber.
  • Yet another aspect of the present invention is a method for unit cell casting of titanium or titanium-alloys.
  • the method includes evacuating an external chamber to create an evacuated external chamber wherein a ceramic crucible containing a titanium alloy ingot is positioned therein.
  • the method also includes evacuating the internal chamber to create an evacuated internal chamber having a pressure no greater than 3 ⁇ 10 ⁇ 2 atmosphere.
  • the method also includes melting the titanium alloy ingot within the ceramic crucible utilizing induction heating generated by an induction coil positioned around the ceramic crucible, wherein a power for the induction coil is commences at a first power level of 15 kiloWatts and increases to a second power level greater than 50 kiloWatts.
  • the method also includes injecting a pressurized gas into the evacuated external chamber to create a pressurized external chamber with a pressure in excess of 1 atmosphere, wherein the pressure differential is at a maximum.
  • the method also includes utilizing a high pressure differential between the external chamber and the internal chamber to flow the completely melted titanium alloy material into the mold from the crucible.
  • the pressurized gas is preferably argon.
  • the mold is preferably covered in a kaolin wool insulating material.
  • the mold is preferably for a thin-walled golf club head.
  • the mold is alternatively for an article having a wall thickness less than 0.250 inch.
  • the induction melting time preferably ranges from 30 seconds to 90 seconds.
  • the ceramic crucible is preferably composed of two yttria-based primary crucible layers, wherein a first primary crucible layer has a thickness ranging from 0.010 inch to 0.060 inch, and a second primary crucible layer has a thickness ranging from 0.001 inch to 0.020 inch.
  • the ceramic crucible further comprises a silica based backup layer.
  • the induction coil is preferably positioned around a bottom section of the ceramic crucible.
  • the induction coil is alternatively positioned around an upper section of the ceramic crucible.
  • FIG. 1 is an illustration of a unit-cell casting system.
  • FIG. 2 is an isolated view of an interior chamber, crucible, induction coils and mold of the unit-cell casting system, showing placement of the induction coils at a lower section of the crucible.
  • FIG. 2A is an isolated view of an interior chamber, crucible, induction coils and mold of the unit-cell casting system, showing placement of the induction coils at an upper section of the crucible.
  • FIG. 2B is an isolated view of an interior chamber, crucible, induction coils and mold of the unit-cell casting system, showing an insulation material wrapped around the mold.
  • FIG. 3A is an illustration of a technician pre-heating a mold in an oven.
  • FIG. 3B is an illustration of a technician attaching the pre-heated mold to a lid of the internal container.
  • FIG. 3C is an illustration of a technician attaching the lid to the internal container.
  • FIG. 3D is an isolated view of the internal container.
  • FIG. 3E is an isolated view of the lid of the internal container.
  • FIG. 3F is an isolated view of the internal chamber of the internal container showing infrared heaters.
  • FIG. 4 is an illustration of a unit-cell casting system during an external chamber evacuation step.
  • FIG. 4A is an illustration of a unit-cell casting system during an external chamber pressurization step.
  • FIG. 4B is an illustration of a unit-cell casting system during an ingot melting step.
  • FIG. 5 is an illustration of a PLC unit and computer for a unit cell casting system.
  • FIG. 6 is a block diagram of a unit cell casting method.
  • FIG. 7 is an isolated view of a crucible for a unit cell casting system.
  • FIG. 8 is a flow chart of a method for unit cell titanium casting.
  • FIG. 9 is a flow chart of a method for unit cell titanium casting.
  • FIG. 10 is a flow chart of a method for unit cell titanium casting.
  • FIG. 11 is an illustration of a PLC unit, an operator's computer for a unit cell casting system, an internal chamber with monitoring connections.
  • FIG. 12 is an illustration of a PLC unit, an operator's computer for a unit cell casting system, an internal chamber with monitoring connections.
  • a unit cell titanium casting system 5 comprises an external container 44 , an internal container 39 , a vacuum mechanism 60 , a crucible 10 , an induction coil 15 , a coil electrical generation mechanism 25 , and a mold 30 .
  • the external container 44 defines an external chamber 45 .
  • the internal container 39 defines an internal chamber 40 .
  • the vacuum mechanism 60 includes a vacuum line 71 , a vacuum connector 70 and pressure gauges 75 a and 75 b . The vacuum mechanism 60 is utilized to evacuate and pressurize the external chamber 45 and the internal chamber 40 in order to create a pressure differential between the internal chamber 40 and the external chamber 45 .
  • the crucible 10 is preferably composed of a ceramic material.
  • the crucible 10 is composed of a first layer 11 a , a second layer 11 b and a silica based third layer 11 c , as shown in FIG. 7 .
  • a metal ingot 20 is placed within the interior of the crucible 10 .
  • the metal ingot 20 is preferably a titanium alloy material.
  • the volume of the crucible 10 preferably corresponds to the amount of metal necessary for forming the article.
  • the interior of the crucible 10 preferably has a diameter ranging from 15 centimeters (“cm”) to 90 cm, more preferably from 35 cm to 60 cm.
  • a height of the crucible 10 preferably ranges 30 cm to 200 cm, and more preferably from 60 cm to 100 cm.
  • connection nozzle 27 is connected between a bottom opening (not shown) of the crucible 10 and an opening to the mold 30 .
  • the connection nozzle 27 allows the melted metal material from the ingot 20 to flow into the mold 30 for casting of the article.
  • the size of connection nozzle 27 is determined based on the size and shape of the cavity of the mold 30 , and is preferably from 5 cm to 100 cm, and more preferably from 15 cm to 50 cm.
  • the induction coil 15 is wrapped around the crucible 10 .
  • the induction coil 15 is energized to generate an electromagnetic force to melt the metal ingot 20 (e.g., titanium alloy ingot) within the crucible 10 .
  • the coil electrical generation mechanism 25 provides the electricity to the induction coil 15 .
  • the induction coil 15 is wrapped around a bottom section 10 b of the crucible 10 . This melts the bottom of the ingot 20 first.
  • the induction coil 15 is wrapped around an upper section 10 a of the crucible 10 . This melts the top of the ingot 20 first.
  • the induction coil 15 is preferably centered on the upper third of the ingot 20 . This positioning allows the induction coil 15 to first act on the upper portion of the ingot 20 (melting the material from the top down), causing molten material to cascade around the still-solid ingot 20 and forming a seal before the electromagnetic forces of the induction coil 15 affect the remaining material.
  • the induction coil 15 is positioned towards the bottom 10 b of the ceramic crucible 10 . This positioning allows for a uniform melt as molten material cascades onto itself and also increased homogeneity of the pour as the electromagnetic forces can better act on the molten material prior to it being evacuated from the crucible 10 .
  • Melting of the ingot 20 of titanium alloy is carried out in a vacuum condition for induction melting.
  • the induction coil 15 is connected to the coil electrical generation mechanism 25 .
  • the ceramic crucible 10 is utilized for vacuum induction melting of the titanium alloy.
  • the ceramic material does not interfere with the fielding effect of the electromagnetic force, and the electro-magnetic induction energy generated by the induction coil 15 is fully focused on melting the ingot of titanium alloy.
  • an insulating material 31 is wrapped around the mold 30 .
  • molds are preheated prior to use in order to improve the flow of material into the mold itself and to better allow the mold 30 to fill completely.
  • pattern mold heat is retained through the use of an insulating material 31 (e.g.: Kaolin wool) thereby extending the useful period of the mold 30 prior to the pour and allowing for better fill, including filling of more difficult molds (e.g., thin walled castings).
  • an insulating material 31 e.g.: Kaolin wool
  • the mold 30 is preheated in an oven 80 .
  • pattern molds 30 are preheated prior to use in order to improve the flow of material into the mold 30 itself and to better allow the mold 30 to fill completely. Due to the nature of titanium materials, and the melting process itself, there is a likely correlation between the temperature of the mold 30 and the ability to fill complex and/or thin walled pattern molds 30 . Temperatures testing include 1050° C., 1060° C., 1100° C., 1150° C., 1200° C., 1250° C. and 1260° C. The pre-heated mold is removed from the 80 and attached to a lid 35 of the internal container 39 .
  • infrared heaters 50 a and 50 b are used to maintain the heat of the mold 30 within the internal chamber 40 . Due to the nature of titanium materials, and the melting process itself, the more that heat loss is minimized, the greater time the material can flow and fill the mold 30 prior to solidification. To this end, pattern mold heat is retained through the use of infrared heaters 50 a and 50 b placed within the internal walls of the internal chamber 40 of the internal container 39 in order to minimize pattern mold cool down and improve the ability to cast complex and/or thin-walled parts.
  • FIGS. 4, 4A and 4B illustrate the casting process using a pressure differential between the external chamber 45 and the internal chamber 40 to assist in the flow of melted titanium alloy materials into a mold 30 .
  • FIG. 5 illustrates a programmable logic computer (“PLC”) and operator computer 91 utilized with the unit cell casting system 5 .
  • PLC programmable logic computer
  • FIG. 6 is a block diagram of a unit cell casting method 600 .
  • an ingot 20 is prepared for casting.
  • the single ingot 20 is utilized to manufacture a single article such as a golf club head 29 .
  • the present invention manufactures only a single article in each process.
  • the mold 30 is preheated in an oven.
  • the external chamber 45 is evacuated.
  • the external chamber 45 is pressurized with an argon gas.
  • the internal chamber 40 is evacuated.
  • the induction coil 15 is energized and at step 607 the ingot 20 is melted within the crucible 10 .
  • the melted material flows into mold 30 .
  • the de-molding process occurs.
  • the article (golf club head) 29 is finished.
  • a frequency generated in the induction coil ranges from 1 kilo-Hertz to 50 kilo-Hertz, and a power ranges from 15 kilo-Watts to 50 kilo-Watts.
  • An atmospheric pressure of the evacuated internal chamber ranges from 3 ⁇ 1 ⁇ 2 atmosphere to 9.87 ⁇ 10 ⁇ 7 atmosphere.
  • An atmospheric pressure of the evacuated internal chamber ranges from 9.87 ⁇ 10 ⁇ 7 atmosphere to 9.87 ⁇ 10 ⁇ 13 atmosphere.
  • the first layer 11 a and the second layer 11 b are preferably composed of yttrium oxide and other materials.
  • Yttrium oxide is highly inert to titanium in a high-temperature environment resulting in no chemical reaction between the two materials.
  • Yttrium oxide also isolates the ceramic material from the titanium during the melting process to prevent reaction between them to ensure the smooth melting of the titanium-alloy.
  • the third layer 11 c of the crucible 10 is preferably composed of silicon dioxide and other materials. The silicon dioxide resists the metallic expansion and thermal stress during the melting process to ensure strength of the crucible.
  • a preferred thickness of the first layer 11 a is from 0.5 mm to 1.5 mm and the preferred thickness range of the crucible 10 is from 5 mm to 15 mm.
  • a method 800 for unit cell casting of titanium or titanium-alloys is shown in FIG. 8 .
  • a pressure of an internal chamber is monitored utilizing a first vacuum gauge.
  • a pressure of an external chamber is monitored utilizing a second vacuum gauge.
  • the pressure of the internal chamber and the pressure of the external chamber are transmitted to a programmable logic controller (PLC).
  • PLC programmable logic controller
  • a mold is positioned within the internal chamber.
  • an external chamber is evacuated to create an evacuated external chamber having a pressure no greater than 3 ⁇ 10 ⁇ 2 atmosphere, wherein a ceramic crucible containing a titanium alloy ingot is positioned therein.
  • the internal chamber is evacuated to create an evacuated internal chamber having a pressure no greater than 3 ⁇ 10 ⁇ 2 atmosphere, wherein the external chamber and the internal chamber have an equal pressurization.
  • the titanium alloy ingot is melted within the ceramic crucible utilizing induction heating generated by an induction coil positioned around the ceramic crucible.
  • the completely melted titanium alloy material is transferred into the mold from the crucible using a pressure equalization between the external chamber and the internal chamber.
  • a pressure equalization is maintained between the external chamber and the internal chamber during the melting of the titanium alloy ingot.
  • the pressure of the internal chamber and the pressure of the external chamber are monitored and communicated to the PLC during the casting process, and wherein the PLC controls the casting process based on the pressure of the internal chamber and the pressure of the external chamber.
  • a method 900 for unit cell casting of titanium or titanium-alloys is shown in FIG. 9 .
  • a pressure of an internal chamber is monitored utilizing a first vacuum gauge.
  • a pressure of an external chamber is monitored utilizing a second vacuum gauge.
  • the pressure of the internal chamber and the pressure of the external chamber are transmitted to a programmable logic controller (PLC).
  • PLC programmable logic controller
  • a mold is positioned within the internal chamber.
  • an external chamber is evacuated to create an evacuated external chamber having a pressure no greater than 3 ⁇ 10 ⁇ 2 atmosphere, wherein a ceramic crucible containing a titanium alloy ingot is positioned therein.
  • the internal chamber is evacuated to create an evacuated internal chamber having a pressure no greater than 3 ⁇ 10 ⁇ 2 atmosphere, wherein the external chamber and the internal chamber have an equal pressurization.
  • the titanium alloy ingot is melted within the ceramic crucible utilizing induction heating generated by an induction coil positioned around the ceramic crucible.
  • a pressurized gas is injected into the evacuated external chamber to create a pressurized external chamber with a pressure in excess of 1 atm, wherein the pressure differential between the external chamber and the internal chamber is maximized.
  • the completely melted titanium alloy material is transferred into the mold from the crucible using a pressure equalization between the external chamber and the internal chamber.
  • a high pressure differential in maintained between the external chamber and the internal chamber during the transfer of the melted titanium alloy material is monitored and communicated to the PLC during the casting process, and wherein the PLC controls the casting process based on the pressure of the internal chamber and the pressure of the external chamber.
  • a method 1000 for unit cell casting of titanium or titanium-alloys is shown in FIG. 10 .
  • a mold is positioned within an internal chamber of a casting chamber.
  • an external chamber is evacuated to create an evacuated external chamber wherein a ceramic crucible containing a titanium alloy ingot is positioned therein.
  • the internal chamber is evacuated to create an evacuated internal chamber having a pressure no greater than 3 ⁇ 10 ⁇ 2 atmosphere.
  • the titanium alloy ingot is melted within the ceramic crucible utilizing induction heating generated by an induction coil positioned around the ceramic crucible, wherein the external chamber and the internal chamber are at an equal pressurization.
  • a pressurized gas is injected into the evacuated external chamber to create a pressurized external chamber with a pressure in excess of 1 atmosphere.
  • a high pressure differential is utilized between the external chamber and the internal chamber to flow the completely melted titanium alloy material into the mold from the crucible.
  • FIG. 11 illustrates a PLC 90 , an operator's computer 91 and an apparatus 5 for a system for unit cell titanium casting.
  • FIG. 12 illustrates a PLC 90 , an operator's computer 91 and an internal chamber with an optical pyrometer for a system for unit cell titanium casting.
  • the optical pyrometer monitors the temperature of the internal chamber.

Abstract

A system (5) and method (800) for unit cell casting of titanium or titanium-alloys is disclosed herein. The system (5) comprises an external chamber (45), a crucible (10) positioned within the external chamber (45), an induction coil (15) positioned around the crucible, an internal chamber (40) positioned within the external chamber (45), and a mold (30) positioned within the internal chamber (40). The external chamber (45) is evacuated and a pressurized gas is injected into the evacuated external chamber (45) to create a pressurized external chamber (45). An ingot (20) is melted within the crucible utilizing induction heating generated by the induction coil (15). The internal chamber (40) is evacuated to create an evacuated internal chamber (40). The titanium alloy material of the ingot (20) is completely transferred into the mold (30) from the crucible (10) using a pressure differential created between the external chamber (45) and the internal chamber (40).

Description

    CROSS REFERENCES TO RELATED APPLICATIONS
  • The present application claims priority to U.S. Provisional Patent Application No. 62/425989, filed on Nov. 23, 2016, which is hereby incorporated by reference in its entirety.
    • STATEMENT REGARDING FEDERALLY SPONSORED RESEARCH OR DEVELOPMENT
  • Not Applicable
    • BACKGROUND OF THE INVENTION Field of the Invention
  • The present invention relates to precision titanium casting. More specifically, the present invention relates to an apparatus and method for precision titanium casting utilizing induction heating.
    • Description of the Related Art
  • Various methods of titanium casting are well-known. One such method is investment casting which involves a lost wax procedure.
  • Vacuum electric arc smelting is another method in which a titanium ingot is melted by substantial heat generated by mutual discharging in a high current state by respectively using a titanium ingot crucible and a water-cooled copper crucible as a positive electrode and a negative electrode, thereby forming a molten liquid metal in the crucible and completing the casting of the titanium.
  • Another method is vacuum induction smelting in which an induction coil is wrapped outside a split-type water-cooled copper crucible. The electromagnetic force generated by the induction coil passes through a nonmetal isolation portion between splits of the copper crucible and then acts on a titanium ingot placed inside the crucible. Then the molten metal forms a molten metal liquid inside the crucible and the casting of the titanium is completed.
  • Vacuum induction smelting and vacuum electric arc smelting require the use of a water-cooled copper crucible which results in the loss of substantial heat. The actual power consumed is very little (only 20% to 30% of the power actually acts on the titanium). Furthermore, the preparation of the molding shell is very complex and time consuming, which adds to the costs. In the traditional casting technology, the operation time of a single furnace is usually 60 to 80 minutes, and the loading and discharge process requires the coordination of many people. In the traditional casting technology, the process from the preparation of the wax pattern to the clearing of the molding shell can take ten days.
  • Titanium is an extremely reactive metal. During melting via traditional casting processes, a water cooling environment is required. The molten titanium liquid will come into direct contact with water if the crucible cracks, resulting in a fierce reaction, or even explosion, which poses a great threat to production safety.
  • To solve the above problems, a new kind of titanium alloy induction melting vacuum suction casting device is urgently needed, to solve the problems with existing titanium alloy casting, such as low efficiency, high cost, complicated technology, heavy workload, difficulty with preparing high-quality molding shells, long cycle and potential hazard.
    • BRIEF SUMMARY OF THE INVENTION
  • Utilizing the two chamber casting system, one of the primary tenets is the use of an induction coil in order to melt the desired material within the crucible. Typically, the induction coil will utilize a set power level between 15 and 50 kW in order to melt the target material. In order to allow for the most uniform melt in addition to having the ability to superheat the material (allowing for improved flow) and maximize the efficiency of the equipment, the power level is varied during the course of the melt. Optimally, the power begins relatively low with a transition to higher power levels prior to the complete melting of the ingot. The change in power is controlled by a Programmable Logic Controller (PLC), and the transition or transitions in power is/are based off of the melt temperature of the target material. This process allows for a smooth controllable melt, followed by a period where a significant additional amount of energy can be transferred into the target material before the material is evacuated from the crucible resulting. This allows for a better pattern mold fill, better material properties, and reduced equipment cycle times.
  • One aspect of the present invention is a method for unit cell casting of titanium or titanium-alloys. The method includes positioning a mold within an internal chamber. The method also includes evacuating an external chamber to create an evacuated external chamber wherein a ceramic crucible containing a titanium alloy ingot is positioned therein. The method also includes evacuating the internal chamber to create an evacuated internal chamber having a pressure no greater than 3×10−2 atmosphere. The method also includes injecting a pressurized gas into the evacuated external chamber to create a pressurized external chamber with a pressure in excess of 1 atm. The method also includes melting the titanium alloy ingot within the ceramic crucible utilizing induction heating generated by an induction coil positioned around the ceramic crucible, wherein a power for the induction coil is commences at a first power level of 15 kiloWatts and increases to a second power level greater than 50 kiloWatts. The method also includes transferring the completely melted titanium alloy material into the mold from the crucible using a pressure differential created between the external chamber and the internal chamber. A high pressure differential in maintained between the external chamber and the internal chamber during the transfer of the melted titanium alloy material. The PLC controls power to the induction coil to superheat the titanium alloy ingot in the ceramic crucible. The pressure of the internal chamber and the pressure of the external chamber are monitored and communicated to the PLC during the casting process, and wherein the PLC controls the casting process based on the pressure of the internal chamber and the pressure of the external chamber.
  • Another aspect of the present invention is a system method for unit cell casting of titanium or titanium-alloys. The system comprises an external chamber, a ceramic crucible positioned within the external chamber, an induction coil positioned around a bottom section of the ceramic crucible, an internal chamber positioned within the external chamber, a mold positioned within the internal chamber, a first vacuum gauge positioned within the internal chamber, a second vacuum gauge positioned within the external chamber, a PLC in communication with the first vacuum gauge, the second vacuum gauge, and the induction coil. The pressure of the internal chamber and the pressure of the external chamber are monitored and communicated to the PLC during the casting process, and wherein the PLC controls the casting process based on the pressure of the internal chamber and the pressure of the external chamber. The external chamber is evacuated to create an evacuated external chamber wherein the ceramic crucible contains a titanium alloy ingot positioned therein. A pressurized gas is injected into the evacuated external chamber to create a pressurized external chamber. The titanium alloy ingot is melted within the ceramic crucible utilizing induction heating generated by the induction coil positioned around the ceramic crucible, wherein a power for the induction coil is commences at a first power level of 15 kiloWatts and increases to a second power level greater than 50 kiloWatts. The internal chamber is evacuated to create an evacuated internal chamber. The titanium alloy material is completely transferred into the mold from the crucible using a maximum pressure differential created between the external chamber and the internal chamber.
  • Yet another aspect of the present invention is a method for unit cell casting of titanium or titanium-alloys. The method includes evacuating an external chamber to create an evacuated external chamber wherein a ceramic crucible containing a titanium alloy ingot is positioned therein. The method also includes evacuating the internal chamber to create an evacuated internal chamber having a pressure no greater than 3×10−2 atmosphere. The method also includes melting the titanium alloy ingot within the ceramic crucible utilizing induction heating generated by an induction coil positioned around the ceramic crucible, wherein a power for the induction coil is commences at a first power level of 15 kiloWatts and increases to a second power level greater than 50 kiloWatts. The method also includes injecting a pressurized gas into the evacuated external chamber to create a pressurized external chamber with a pressure in excess of 1 atmosphere, wherein the pressure differential is at a maximum. The method also includes utilizing a high pressure differential between the external chamber and the internal chamber to flow the completely melted titanium alloy material into the mold from the crucible.
  • The pressurized gas is preferably argon. The mold is preferably covered in a kaolin wool insulating material. The mold is preferably for a thin-walled golf club head. The mold is alternatively for an article having a wall thickness less than 0.250 inch. The induction melting time preferably ranges from 30 seconds to 90 seconds. The ceramic crucible is preferably composed of two yttria-based primary crucible layers, wherein a first primary crucible layer has a thickness ranging from 0.010 inch to 0.060 inch, and a second primary crucible layer has a thickness ranging from 0.001 inch to 0.020 inch. The ceramic crucible further comprises a silica based backup layer. The induction coil is preferably positioned around a bottom section of the ceramic crucible. The induction coil is alternatively positioned around an upper section of the ceramic crucible.
  • Having briefly described the present invention, the above and further objects, features and advantages thereof will be recognized by those skilled in the pertinent art from the following detailed description of the invention when taken in conjunction with the accompanying drawings.
    • BRIEF DESCRIPTION OF THE SEVERAL VIEWS OF THE DRAWINGS
  • FIG. 1 is an illustration of a unit-cell casting system.
  • FIG. 2 is an isolated view of an interior chamber, crucible, induction coils and mold of the unit-cell casting system, showing placement of the induction coils at a lower section of the crucible.
  • FIG. 2A is an isolated view of an interior chamber, crucible, induction coils and mold of the unit-cell casting system, showing placement of the induction coils at an upper section of the crucible.
  • FIG. 2B is an isolated view of an interior chamber, crucible, induction coils and mold of the unit-cell casting system, showing an insulation material wrapped around the mold.
  • FIG. 3A is an illustration of a technician pre-heating a mold in an oven.
  • FIG. 3B is an illustration of a technician attaching the pre-heated mold to a lid of the internal container.
  • FIG. 3C is an illustration of a technician attaching the lid to the internal container.
  • FIG. 3D is an isolated view of the internal container.
  • FIG. 3E is an isolated view of the lid of the internal container.
  • FIG. 3F is an isolated view of the internal chamber of the internal container showing infrared heaters.
  • FIG. 4 is an illustration of a unit-cell casting system during an external chamber evacuation step.
  • FIG. 4A is an illustration of a unit-cell casting system during an external chamber pressurization step.
  • FIG. 4B is an illustration of a unit-cell casting system during an ingot melting step.
  • FIG. 5 is an illustration of a PLC unit and computer for a unit cell casting system.
  • FIG. 6 is a block diagram of a unit cell casting method.
  • FIG. 7 is an isolated view of a crucible for a unit cell casting system.
  • FIG. 8 is a flow chart of a method for unit cell titanium casting.
  • FIG. 9 is a flow chart of a method for unit cell titanium casting.
  • FIG. 10 is a flow chart of a method for unit cell titanium casting.
  • FIG. 11 is an illustration of a PLC unit, an operator's computer for a unit cell casting system, an internal chamber with monitoring connections.
  • FIG. 12 is an illustration of a PLC unit, an operator's computer for a unit cell casting system, an internal chamber with monitoring connections.
    •  DETAILED DESCRIPTION OF THE INVENTION
  • As shown in FIG. 1, a unit cell titanium casting system 5 comprises an external container 44, an internal container 39, a vacuum mechanism 60, a crucible 10, an induction coil 15, a coil electrical generation mechanism 25, and a mold 30. The external container 44 defines an external chamber 45. The internal container 39 defines an internal chamber 40. The vacuum mechanism 60 includes a vacuum line 71, a vacuum connector 70 and pressure gauges 75 a and 75 b. The vacuum mechanism 60 is utilized to evacuate and pressurize the external chamber 45 and the internal chamber 40 in order to create a pressure differential between the internal chamber 40 and the external chamber 45.
  • The crucible 10 is preferably composed of a ceramic material. In a most preferred embodiment, the crucible 10 is composed of a first layer 11 a, a second layer 11 b and a silica based third layer 11 c, as shown in FIG. 7. A metal ingot 20 is placed within the interior of the crucible 10. The metal ingot 20 is preferably a titanium alloy material. The volume of the crucible 10 preferably corresponds to the amount of metal necessary for forming the article. The interior of the crucible 10 preferably has a diameter ranging from 15 centimeters (“cm”) to 90 cm, more preferably from 35 cm to 60 cm. A height of the crucible 10 preferably ranges 30 cm to 200 cm, and more preferably from 60 cm to 100 cm.
  • A connection nozzle 27 is connected between a bottom opening (not shown) of the crucible 10 and an opening to the mold 30. The connection nozzle 27 allows the melted metal material from the ingot 20 to flow into the mold 30 for casting of the article. Specifically, the size of connection nozzle 27 is determined based on the size and shape of the cavity of the mold 30, and is preferably from 5 cm to 100 cm, and more preferably from 15 cm to 50 cm.
  • The induction coil 15 is wrapped around the crucible 10. The induction coil 15 is energized to generate an electromagnetic force to melt the metal ingot 20 (e.g., titanium alloy ingot) within the crucible 10. The coil electrical generation mechanism 25 provides the electricity to the induction coil 15. As shown in FIG. 2, the induction coil 15 is wrapped around a bottom section 10 b of the crucible 10. This melts the bottom of the ingot 20 first. As shown in FIG. 2A, the induction coil 15 is wrapped around an upper section 10 a of the crucible 10. This melts the top of the ingot 20 first.
  • In order to optimize the ability of the target material to seal around the port of a ceramic crucible 10, the induction coil 15is preferably centered on the upper third of the ingot 20. This positioning allows the induction coil 15 to first act on the upper portion of the ingot 20 (melting the material from the top down), causing molten material to cascade around the still-solid ingot 20 and forming a seal before the electromagnetic forces of the induction coil 15 affect the remaining material.
  • Alternatively, in order to fully utilize the electromagnetic forces of the induction coil 15, to include the electromagnetic stirring of the melt, the induction coil 15 is positioned towards the bottom 10 b of the ceramic crucible 10. This positioning allows for a uniform melt as molten material cascades onto itself and also increased homogeneity of the pour as the electromagnetic forces can better act on the molten material prior to it being evacuated from the crucible 10.
  • Melting of the ingot 20 of titanium alloy is carried out in a vacuum condition for induction melting. The induction coil 15 is connected to the coil electrical generation mechanism 25.
  • The ceramic crucible 10 is utilized for vacuum induction melting of the titanium alloy. The ceramic material does not interfere with the fielding effect of the electromagnetic force, and the electro-magnetic induction energy generated by the induction coil 15 is fully focused on melting the ingot of titanium alloy.
  • In an embodiment shown in FIG. 2B, an insulating material 31 is wrapped around the mold 30. During casting pattern molds are preheated prior to use in order to improve the flow of material into the mold itself and to better allow the mold 30 to fill completely.
  • Due to the nature of titanium materials, and the melting process itself, the more that heat loss is minimized, the greater time the material has to flow and fill the mold 30 prior to solidification. To this end, pattern mold heat is retained through the use of an insulating material 31 (e.g.: Kaolin wool) thereby extending the useful period of the mold 30 prior to the pour and allowing for better fill, including filling of more difficult molds (e.g., thin walled castings).
  • As shown in FIGS. 3A, 3B, 3C, 3D and 3E, the mold 30 is preheated in an oven 80. During unit cell casting, pattern molds 30 are preheated prior to use in order to improve the flow of material into the mold 30 itself and to better allow the mold 30 to fill completely. Due to the nature of titanium materials, and the melting process itself, there is a likely correlation between the temperature of the mold 30 and the ability to fill complex and/or thin walled pattern molds 30. Temperatures testing include 1050° C., 1060° C., 1100° C., 1150° C., 1200° C., 1250° C. and 1260° C. The pre-heated mold is removed from the 80 and attached to a lid 35 of the internal container 39.
  • In an alternative embodiment shown in FIG. 3F, infrared heaters 50 a and 50 b are used to maintain the heat of the mold 30 within the internal chamber 40. Due to the nature of titanium materials, and the melting process itself, the more that heat loss is minimized, the greater time the material can flow and fill the mold 30 prior to solidification. To this end, pattern mold heat is retained through the use of infrared heaters 50 a and 50 b placed within the internal walls of the internal chamber 40 of the internal container 39 in order to minimize pattern mold cool down and improve the ability to cast complex and/or thin-walled parts.
  • FIGS. 4, 4A and 4B illustrate the casting process using a pressure differential between the external chamber 45 and the internal chamber 40 to assist in the flow of melted titanium alloy materials into a mold 30.
  • FIG. 5 illustrates a programmable logic computer (“PLC”) and operator computer 91 utilized with the unit cell casting system 5.
  • FIG. 6 is a block diagram of a unit cell casting method 600. At step 601, an ingot 20 is prepared for casting. The single ingot 20 is utilized to manufacture a single article such as a golf club head 29. As opposed to manufacturing multiple articles in a single process, which results in the loss of material, the present invention manufactures only a single article in each process. At step 602, the mold 30 is preheated in an oven. At step 603, the external chamber 45 is evacuated. At step 604, the external chamber 45 is pressurized with an argon gas. At step 605, the internal chamber 40 is evacuated. At step 606, the induction coil 15 is energized and at step 607 the ingot 20 is melted within the crucible 10. At the step 608, the melted material flows into mold 30. At step 609, the de-molding process occurs. At step 610, the article (golf club head) 29 is finished. A frequency generated in the induction coil ranges from 1 kilo-Hertz to 50 kilo-Hertz, and a power ranges from 15 kilo-Watts to 50 kilo-Watts. An atmospheric pressure of the evacuated internal chamber ranges from 3×1−2 atmosphere to 9.87×10−7 atmosphere. An atmospheric pressure of the evacuated internal chamber ranges from 9.87×10−7 atmosphere to 9.87×10−13 atmosphere.
  • As shown in FIG. 7, the first layer 11 a and the second layer 11 b are preferably composed of yttrium oxide and other materials. Yttrium oxide is highly inert to titanium in a high-temperature environment resulting in no chemical reaction between the two materials. Yttrium oxide also isolates the ceramic material from the titanium during the melting process to prevent reaction between them to ensure the smooth melting of the titanium-alloy. The third layer 11 c of the crucible 10 is preferably composed of silicon dioxide and other materials. The silicon dioxide resists the metallic expansion and thermal stress during the melting process to ensure strength of the crucible.
  • A preferred thickness of the first layer 11 a is from 0.5 mm to 1.5 mm and the preferred thickness range of the crucible 10 is from 5 mm to 15 mm.
  • A method 800 for unit cell casting of titanium or titanium-alloys is shown in FIG. 8. At block 801, a pressure of an internal chamber is monitored utilizing a first vacuum gauge. At block 802, a pressure of an external chamber is monitored utilizing a second vacuum gauge. At block 803, the pressure of the internal chamber and the pressure of the external chamber are transmitted to a programmable logic controller (PLC). At block 804, a mold is positioned within the internal chamber. At block 805, an external chamber is evacuated to create an evacuated external chamber having a pressure no greater than 3×10−2 atmosphere, wherein a ceramic crucible containing a titanium alloy ingot is positioned therein. At block 806, the internal chamber is evacuated to create an evacuated internal chamber having a pressure no greater than 3×10−2 atmosphere, wherein the external chamber and the internal chamber have an equal pressurization. At block 807, the titanium alloy ingot is melted within the ceramic crucible utilizing induction heating generated by an induction coil positioned around the ceramic crucible. At block 808, the completely melted titanium alloy material is transferred into the mold from the crucible using a pressure equalization between the external chamber and the internal chamber. A pressure equalization is maintained between the external chamber and the internal chamber during the melting of the titanium alloy ingot. The pressure of the internal chamber and the pressure of the external chamber are monitored and communicated to the PLC during the casting process, and wherein the PLC controls the casting process based on the pressure of the internal chamber and the pressure of the external chamber.
  • A method 900 for unit cell casting of titanium or titanium-alloys is shown in FIG. 9. At block 901, a pressure of an internal chamber is monitored utilizing a first vacuum gauge. At block 902, a pressure of an external chamber is monitored utilizing a second vacuum gauge. At block 903, the pressure of the internal chamber and the pressure of the external chamber are transmitted to a programmable logic controller (PLC). At block 904, a mold is positioned within the internal chamber. At block 905, an external chamber is evacuated to create an evacuated external chamber having a pressure no greater than 3×10−2 atmosphere, wherein a ceramic crucible containing a titanium alloy ingot is positioned therein. At block 906, the internal chamber is evacuated to create an evacuated internal chamber having a pressure no greater than 3×10−2 atmosphere, wherein the external chamber and the internal chamber have an equal pressurization. At block 907, the titanium alloy ingot is melted within the ceramic crucible utilizing induction heating generated by an induction coil positioned around the ceramic crucible. At block 908, a pressurized gas is injected into the evacuated external chamber to create a pressurized external chamber with a pressure in excess of 1 atm, wherein the pressure differential between the external chamber and the internal chamber is maximized. At block 909, the completely melted titanium alloy material is transferred into the mold from the crucible using a pressure equalization between the external chamber and the internal chamber. A high pressure differential in maintained between the external chamber and the internal chamber during the transfer of the melted titanium alloy material. The pressure of the internal chamber and the pressure of the external chamber are monitored and communicated to the PLC during the casting process, and wherein the PLC controls the casting process based on the pressure of the internal chamber and the pressure of the external chamber.
  • A method 1000 for unit cell casting of titanium or titanium-alloys is shown in FIG. 10. At block 1001, a mold is positioned within an internal chamber of a casting chamber. At block 1002, an external chamber is evacuated to create an evacuated external chamber wherein a ceramic crucible containing a titanium alloy ingot is positioned therein. At block 1003, the internal chamber is evacuated to create an evacuated internal chamber having a pressure no greater than 3×10−2 atmosphere. At block 1004, the titanium alloy ingot is melted within the ceramic crucible utilizing induction heating generated by an induction coil positioned around the ceramic crucible, wherein the external chamber and the internal chamber are at an equal pressurization. At block 1005, a pressurized gas is injected into the evacuated external chamber to create a pressurized external chamber with a pressure in excess of 1 atmosphere. At block 1006, a high pressure differential is utilized between the external chamber and the internal chamber to flow the completely melted titanium alloy material into the mold from the crucible.
  • FIG. 11 illustrates a PLC 90, an operator's computer 91 and an apparatus 5 for a system for unit cell titanium casting.
  • FIG. 12 illustrates a PLC 90, an operator's computer 91 and an internal chamber with an optical pyrometer for a system for unit cell titanium casting. The optical pyrometer monitors the temperature of the internal chamber.
  • Those skilled in the pertinent art will recognize that materials other than titanium and titanium alloy may be cast in the unit cell casting system without departing from the scope and spirit of the present invention.
  • From the foregoing it is believed that those skilled in the pertinent art will recognize the meritorious advancement of this invention and will readily understand that while the present invention has been described in association with a preferred embodiment thereof, and other embodiments illustrated in the accompanying drawings, numerous changes, modifications and substitutions of equivalents may be made therein without departing from the spirit and scope of this invention which is intended to be unlimited by the foregoing except as may appear in the following appended claims. Therefore, the embodiments of the invention in which an exclusive property or privilege is claimed are defined in the following appended claims.

Claims (20)

We claim as our invention the following:
1. A method for unit cell casting of titanium or titanium-alloys, the method comprising:
positioning a mold within an internal chamber;
evacuating an external chamber to create an evacuated external chamber wherein a ceramic crucible containing a titanium alloy ingot is positioned therein;
evacuating the internal chamber to create an evacuated internal chamber having a pressure no greater than 3×10−2 atmosphere;
injecting a pressurized gas into the evacuated external chamber to create a pressurized external chamber with a pressure in excess of 1 atm;
melting the titanium alloy ingot within the ceramic crucible utilizing induction heating generated by an induction coil positioned around the ceramic crucible, wherein a power for the induction coil is commences at a first power level of 15 kiloWatts and increases to a second power level greater than 50 kiloWatts;
transferring the completely melted titanium alloy material into the mold from the crucible using a pressure differential created between the external chamber and the internal chamber;
wherein a high pressure differential in maintained between the external chamber and the internal chamber during the transfer of the melted titanium alloy material;
wherein the PLC controls power to the induction coil to superheat the titanium alloy ingot in the ceramic crucible;
wherein the pressure of the internal chamber and the pressure of the external chamber are monitored and communicated to the PLC during the casting process, and wherein the PLC controls the casting process based on the pressure of the internal chamber and the pressure of the external chamber.
2. The method according to claim 1 wherein the pressurized gas is argon.
3. The method according to claim 1 wherein a frequency generated in the induction coil ranges from 1 kilo-Hertz to 50 kilo-Hertz.
4. The method according to claim 1 wherein an atmospheric pressure of the evacuated internal chamber ranges from 3×10−2 atmosphere to 9.87×10−7 atmosphere.
5. The method according to claim 1 wherein the second power level to the induction coil is more than 60 kiloWatts.
6. The method according to claim 1 wherein the second power level to the induction coil is more than 70 kiloWatts.
7. The method according to claim 1 wherein the second power level to the induction coil is more than 80 kiloWatts.
8. The method according to claim 1 wherein the second power level to the induction coil is more than 90 kiloWatts.
9. The method according to claim 1 wherein an atmospheric pressure of the evacuated internal chamber ranges from 9.87×10−7 atmosphere to 9.87×10−13 atmosphere
10. A system method for unit cell casting of titanium or titanium-alloys, the system comprising:
an external chamber;
a ceramic crucible positioned within the external chamber;
an induction coil positioned around a bottom section of the ceramic crucible;
an internal chamber positioned within the external chamber; and
a mold positioned within the internal chamber;
a first vacuum gauge positioned within the internal chamber;
a second vacuum gauge positioned within the external chamber;
a PLC in communication with the first vacuum gauge, the second vacuum gauge, and the induction coil;
wherein the pressure of the internal chamber and the pressure of the external chamber are monitored and communicated to the PLC during the casting process, and wherein the PLC controls the casting process based on the pressure of the internal chamber and the pressure of the external chamber;
wherein the external chamber is evacuated to create an evacuated external chamber wherein the ceramic crucible contains a titanium alloy ingot positioned therein;
wherein a pressurized gas is injected into the evacuated external chamber to create a pressurized external chamber;
wherein the titanium alloy ingot is melted within the ceramic crucible utilizing induction heating generated by the induction coil positioned around the ceramic crucible, wherein a power for the induction coil is commences at a first power level of 15 kiloWatts and increases to a second power level greater than 50 kiloWatts;
wherein the internal chamber is evacuated to create an evacuated internal chamber;
wherein the titanium alloy material is completely transferred into the mold from the crucible using a maximum pressure differential created between the external chamber and the internal chamber.
11. A method for unit cell casting of titanium or titanium-alloys, the method comprising:
evacuating an external chamber to create an evacuated external chamber wherein a ceramic crucible containing a titanium alloy ingot is positioned therein;
evacuating the internal chamber to create an evacuated internal chamber having a pressure no greater than 3×10−2 atmosphere;
melting the titanium alloy ingot within the ceramic crucible utilizing induction heating generated by an induction coil positioned around the ceramic crucible, wherein a power for the induction coil is commences at a first power level of 15 kiloWatts and increases to a second power level greater than 50 kiloWatts;
injecting a pressurized gas into the evacuated external chamber to create a pressurized external chamber with a pressure in excess of 1 atmosphere, wherein the pressure differential is at a maximum;
and
utilizing a high pressure differential between the external chamber and the internal chamber to flow the completely melted titanium alloy material into the mold from the crucible.
12. The method according to claim 11 wherein the pressurized gas is argon.
13. The method according to claim 11 wherein a frequency generated in the induction coil ranges from 1 kilo-Hertz to 50 kilo-Hertz.
14. The method according to claim 11 wherein an atmospheric pressure of the evacuated internal chamber ranges from 3×10−2 atmosphere to 9.87×10−7 atmosphere.
15. The method according to claim 11 wherein the mold is for a thin-walled golf club head.
16. The method according to claim 11 wherein the internal chamber is preheated at a temperature ranging from 1150° C. to 1250° C.
17. The method according to claim 11 wherein a PLC determines when to melt the titanium alloy based on the pressures of the internal chamber and the external chamber.
18. The method according to claim 11 wherein the PLC determines when to change the pressure of internal chamber and the external chamber.
19. The method according to claim 11 wherein an atmospheric pressure of the evacuated internal chamber ranges from 9.87×10−7 atmosphere to 9.87×10−13 atmosphere
20. The method according to claim 11 wherein the second power level to the induction coil is more than 60 kiloWatts.
US15/816,017 2016-11-23 2017-11-17 Unit Cell Titanium Casting Abandoned US20180141115A1 (en)

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109628897A (en) * 2018-12-06 2019-04-16 新疆众和股份有限公司 A kind of high-purity alusil alloy sputtering target material blank and preparation method thereof

Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3665083A (en) * 1968-10-14 1972-05-23 Trw Inc Apparatus for melting titanium
US3845807A (en) * 1970-04-01 1974-11-05 H Koon Vacuum casting furnace
US4478270A (en) * 1981-04-01 1984-10-23 Interlake, Inc. Apparatus for casting low-density alloys
DE3927998A1 (en) * 1988-08-25 1990-03-01 Reiichi Okuda Precision casting used in mfg. dental and orthopaedic device - comprises application of inert gas pressure to melting chamber, raising inert gas pressure and prodn. of a differential pressure
US5299619A (en) * 1992-12-30 1994-04-05 Hitchiner Manufacturing Co., Inc. Method and apparatus for making intermetallic castings
US6508722B1 (en) * 2000-01-31 2003-01-21 Acushnet Company Golf club head and improved casting method therefor
CN104028729A (en) * 2014-05-09 2014-09-10 西北工业大学 Vacuum low-pressure casting forming device for titanium alloy component
CN104646647A (en) * 2015-01-16 2015-05-27 马旭东 Titanium-based alloy induction melting bottom leakage type vacuum suction casting device and control method
US20170008073A1 (en) * 2014-03-28 2017-01-12 Ihi Corporation CASTING MOLD, METHOD OF MANUFACTURING SAME, TiAl ALLOY CAST PRODUCT, AND METHOD OF CASTING SAME

Patent Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3665083A (en) * 1968-10-14 1972-05-23 Trw Inc Apparatus for melting titanium
US3845807A (en) * 1970-04-01 1974-11-05 H Koon Vacuum casting furnace
US4478270A (en) * 1981-04-01 1984-10-23 Interlake, Inc. Apparatus for casting low-density alloys
DE3927998A1 (en) * 1988-08-25 1990-03-01 Reiichi Okuda Precision casting used in mfg. dental and orthopaedic device - comprises application of inert gas pressure to melting chamber, raising inert gas pressure and prodn. of a differential pressure
US5299619A (en) * 1992-12-30 1994-04-05 Hitchiner Manufacturing Co., Inc. Method and apparatus for making intermetallic castings
US6508722B1 (en) * 2000-01-31 2003-01-21 Acushnet Company Golf club head and improved casting method therefor
US20170008073A1 (en) * 2014-03-28 2017-01-12 Ihi Corporation CASTING MOLD, METHOD OF MANUFACTURING SAME, TiAl ALLOY CAST PRODUCT, AND METHOD OF CASTING SAME
CN104028729A (en) * 2014-05-09 2014-09-10 西北工业大学 Vacuum low-pressure casting forming device for titanium alloy component
CN104646647A (en) * 2015-01-16 2015-05-27 马旭东 Titanium-based alloy induction melting bottom leakage type vacuum suction casting device and control method

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109628897A (en) * 2018-12-06 2019-04-16 新疆众和股份有限公司 A kind of high-purity alusil alloy sputtering target material blank and preparation method thereof

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