Methods for reducing carbon contamination when melting highly reactive alloys

• US 7,582,133 B2
• Filed: 12/27/2006
• Issued: 09/01/2009
• Est. Priority Date: 12/27/2006
• Status: Expired due to Fees

• Current Assignee: General Electric Company
• Original Assignee: General Electric Company
• Inventors: Gigliotti, Michael Francis Xavier Jr., Bewlay, Bernard Patrick, Kelly, Thomas Joseph, Weimer, Michael James
• Primary Examiner(s): Kerns; Kevin P
• Application Number:
  US11/646,025
• Publication Number:
  US 20080156147A1
• Time in Patent Office: 979 Days
• Field of Search: 164/72, 164/335, 164/267, 266/44, 266/282, 266/275, 75/101.8, 432/262, 432/264, 432/265
• US Class Current: 75/10.18
• CPC Class Codes: C22C 14/00 Alloys based on titanium
• CPC Class Codes: F27B 14/10 Crucibles

Abstract

Methods for reducing carbon contamination when melting highly reactive alloys involving providing a graphite crucible having an interior, applying at least a first protective layer to the interior of the graphite crucible, placing a highly reactive alloy into the crucible having the first protective layer, and melting the highly reactive alloy to obtain a melted alloy having reduced carbon contamination.

Claims

1. A method for reducing carbon contamination when melting highly reactive titanium aluminide alloys comprising:

providing a graphite crucible having an interior;

applying a first protective layer comprising a foil liner to the interior of the graphite crucible;

applying a second protective layer comprising a carbide coating to the interior of the graphite crucible on top of the first protective layer;

placing a highly reactive titanium aluminide alloy into the crucible having the first protective layer and the second protective layer; and

melting the highly reactive titanium aluminide alloy to a temperature of from about 1370°

C. to about 1700°

C. to obtain a melted titanium aluminide alloy having reduced carbon contamination.

2. The method of claim 1 wherein the foil liner is fabricated from a high melting point alloy element selected from the group consisting of niobium, tantalum, tungsten, and molybdenum.

3. The method of claim 2 wherein the carbide coating is formed by applying a high melting point alloy element selected from the group consisting of niobium, tantalum, tungsten, molybdenum, and combinations thereof, to the interior of the crucible and heat treating the high melting point alloy element in a carborizing atmosphere.

4. The method of claim 3 wherein the foil liner comprises a thickness of from about 0.005 mm to about 2 mm.

5. A method for reducing carbon contamination when melting highly reactive titanium aluminide alloys comprising:

providing a graphite crucible having an interior;

applying a first protective layer comprising a carbide coating to the interior of the graphite crucible;

applying a second protective layer comprising a foil liner to the interior of the graphite crucible on top of the first protective layer;

placing a highly reactive titanium aluminide alloy into the crucible having the first protective layer and the second protective layer; and

melting the highly reactive titanium aluminide alloy to a temperature of from about 1370°

C. to about 1700°

C. to obtain a melted titanium aluminide alloy having reduced carbon contamination.

6. The method of claim 5 wherein the carbide coating is formed by applying a high melting point alloy element selected from the group consisting of niobium, tantalum, tungsten, and molybdenum, to the interior of the crucible and heat treating the high melting point alloy element in a carborizing atmosphere and wherein the foil liner is fabricated from a high melting point alloy element selected from the group consisting of niobium, tantalum, tungsten, and molybdenum.

7. The method of claim 6 wherein the foil liner comprises a thickness of from about 0.005 mm to about 2 mm.