Single crystal seed alloy
First Claim
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1. A single crystal seed alloy composition comprising:
- nickel; and
, in the proportion of 5 to 50 weight, % a further metal selected from the Transition Series of elements in Period VI of the Periodic Table of elements.
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Abstract
An alloy composition suitable for use as a single crystal seed comprises nickel and, in the proportion of 5 to 50 weight %, a further metal selected from the Transition Series of elements in Period VI of the Periodic Table of Elements. The further metal may be tungsten or tantalum. The alloy composition contains no component which forms an oxide layer at elevated temperatures, and in particular contains no aluminium or titanium. The alloy composition is suitable for use as a seed alloy for the casting of single crystal components such as aerofoils for gas turbine engines.
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Citations
18 Claims
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1. A single crystal seed alloy composition comprising:
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nickel; and
,in the proportion of 5 to 50 weight, % a further metal selected from the Transition Series of elements in Period VI of the Periodic Table of elements. - View Dependent Claims (2, 3, 4, 5, 6, 7, 8, 9, 11, 12, 14, 15, 16, 17)
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10. A single crystal seed alloy composition comprising;
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nickel; and
,in the proportion of 5 to 50 weight, % a further metal selected from the Transition Series of elements in Period VI of the Periodic Table of elements, wherein the alloy composition has a solidification temperature which is not less than 1300°
C. and not greater than 1400°
C., and a solidification temperature range which is not greater than 20°
C.
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13. A single crystal seed alloy composition consisting essentially of:
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nickel; and
,tungsten in the proportion of 13 to 40 weight %, wherein the alloy composition has a solidification temperature which is not less than 1300°
C. and not greater than 1400°
C., and a solidification temperature range which is not greater than 20°
C.
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18. A single crystal seed alloy composition consisting essentially of:
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nickel; and
,tantalum in the proportion of 25 to 35 weight %, wherein the alloy composition has a solidification temperature which is not less than 1300°
C. and not greater than 1400°
C., and a solidification temperature range which is not greater than 20°
C.
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Specification