Unit Cell Titanium Casting

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 ).

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 plurality of titanium alloy ingots 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 plurality of titanium alloy ingots within the ceramic crucible utilizing induction heating generated by an induction coil;   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 position the induction coil relative to the titanium alloy ingots;   wherein the melting of the plurality of titanium alloy ingots prolongs the total time that the induction coil continues to act upon the target material, thus raising the melt temperature of the target material prior to mold evacuation and allowing for improved pattern mold fill;   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 the plurality of titanium alloy ingots ranges from 2 to 6 ingots. 
     
     
         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 crucible is a single Yttria-based barium infused shell layer having a thickness ranging from 0.015 inch to 0.060 inch, and comprised of a binder with a slurry ratio between 1:1.5 and 1:3.5. 
     
     
         6 . The method according to  claim 1  wherein a power level to the induction coil is more than 70 kiloWatts. 
     
     
         7 . The method according to  claim 1  wherein each of the plurality of titanium alloy ingots has a thickness ranging from 1 mm to 10 mm, and a height ranging from 2 cm to 20 cm. 
     
     
         8 . The method according to  claim 1  wherein a 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 the ceramic crucible;   an internal chamber positioned within the external chamber; and   a mold positioned within the internal chamber;   wherein a ceramic crucible containing a plurality of titanium alloy ingots is positioned therein;   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 a pressurized gas is injected into the evacuated external chamber to create a pressurized external chamber;   wherein the melting of the plurality of titanium alloy ingots prolongs the total time that the induction coil continues to act upon the target material, thus raising the melt temperature of the target material prior to mold evacuation and allowing for improved pattern mold fill;   wherein the plurality of titanium alloy ingots is melted within the ceramic crucible utilizing induction heating generated by an induction coil;   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 plurality of titanium alloy ingots 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 plurality of titanium alloy ingots within the ceramic crucible utilizing induction heating generated by an induction coil;   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;   wherein the melting of the plurality of titanium alloy ingots prolongs the total time that the induction coil continues to act upon the target material, thus raising the melt temperature of the target material prior to mold evacuation and allowing for improved pattern mold fill.   
     
     
         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 a power level to the induction coil is more than 60 kiloWatts.