HEAT-RESISTANT Ni-BASED ALLOY AND METHOD FOR MANUFACTURING SAME
US-2016040276-A1 · Feb 11, 2016 · US
US10094012B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-10094012-B2 |
| Application number | US-201515127348-A |
| Country | US |
| Kind code | B2 |
| Filing date | Mar 23, 2015 |
| Priority date | Mar 28, 2014 |
| Publication date | Oct 9, 2018 |
| Grant date | Oct 9, 2018 |
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The present invention relates to a NiIr-base heat-resistant alloy which includes a Ni—Ir—Al—W-base alloy which contains Ir: 5.0 to 50.0 mass %, Al: 1.0 to 8.0 mass %, W: 5.0 to 20.0 mass %, and the balance is Ni, and a γ′ phase having an L12 structure precipitating and dispersing in a matrix as an essential strengthening phase, and a ratio (Y/X) of a peak intensity (Y) of (201) plane of the Ir3W phase observed in the range of 2θ=48° to 50° to a peak intensity (X) of (111) plane of the γ′ phase observed in the range of 2θ=43° to 45° in X-ray diffraction analysis is 0.5 or less. The alloy exhibits good high-temperature property stably.
Opening claim text (preview).
The invention claimed is: 1. A NiIr-base heat-resistant alloy comprising a Ni—Ir—Al—W-base alloy which contains Ir: 5.0 to 50.0 mass %, Al: 1.0 to 8.0 mass %, W: 5.0 to 20.0 mass %, and the balance being Ni, and a γ′ phase as an essential strengthening phase having an L1 2 structure precipitated and dispersed in a matrix, wherein a ratio (Y/X) of a peak intensity (Y) of (201) plane of the Ir 3 W phase observed in the range of 2θ=48° to 50° to a peak intensity (X) of (111) plane of the γ′ phase observed in the range of 2θ=43° to 45° in X-ray diffraction analysis is 0.5 or less. 2. The NiIr-base heat-resistant alloy according to claim 1 , comprising one or two or more additive elements selected from the following Group I: Group I: B: 0.001 to 0.1 mass %, Co: 5.0 to 20.0 mass %, Cr: 1.0 to 25.0 mass %, Ta: 1.0 to 10.0 mass %, Nb: 1.0 to 5.0 mass %, Ti: 1.0 to 5.0 mass %, V: 1.0 to 5.0 mass %, and Mo: 1.0 to 5.0 mass %. 3. The NiIr-base heat-resistant alloy according to claim 1 , further containing 0.001 to 0.5 mass % of C and carbides being precipitated and dispersed. 4. The NiIr-base heat-resistant alloy according to claim 1 , wherein Ir in the alloy is substituted by Rh or Pt in an amount of 30 mass % or less. 5. The NiIr-base heat-resistant alloy according to claim 2 , further containing 0.001 to 0.5 mass % of C and carbides being precipitated and dispersed. 6. The NiIr-base heat-resistant alloy according to claim 2 , wherein Ir in the alloy is substituted by Rh or Pt in an amount of 30 mass % or less. 7. The NiIr-base heat-resistant alloy according to claim 3 , wherein Ir in the alloy is substituted by Rh or Pt in an amount of 30 mass % or less. 8. A method of producing a NiIr-base heat-resistant alloy, comprising: melting and casting for producing an alloy ingot having the composition according to claim 1 by a melting and casting method and subjecting the alloy ingot to an aging heat treatment in a temperature range of 700 to 1300° C., wherein a cooling rate in the melting and casting is 200° C./min or more. 9. The method of producing a NiIr-base heat-resistant alloy according to claim 8 , wherein the aging heat treatment is carried out by heating the alloy in the temperature range of 700 to 1300° C., and then cooling at a cooling rate of 5 to 80° C./sec. 10. The method of producing a NiIr-base heat-resistant alloy according to claim 8 , wherein the NiIr-base alloy is subjected to a homogenization heat treatment in a temperature range of 1100 to 1800° C., prior to the aging heat treatment. 11. A method of producing a NiIr-base heat-resistant alloy, comprising: melting and casting for producing an alloy ingot having the composition according to claim 2 by a melting and casting method and subjecting the alloy ingot to an aging heat treatment in a temperature range of 700 to 1300° C., wherein a cooling rate in the melting and casting is 200° C./min or more. 12. The method of producing a NiIr-base heat-resistant alloy according to claim 11 , wherein the aging heat treatment is carried out by heating the alloy in the temperature range of 700 to 1300° C., and then cooling at a cooling rate of 5 to 80° C./sec. 13. The method of producing a NiIr-base heat-resistant alloy according to claim 11 , wherein the NiIr-base alloy is subjected to a homogenization heat treatment in a temperature range of 1100 to 1800° C., prior to the aging heat treatment. 14. A method of producing a NiIr-base heat-resistant alloy, comprising: melting and casting for producing an alloy ingot having the composition according to claim 3 by a melting and casting method and subjecting the alloy ingot to an aging heat treatment in a temperature range of 700 to 1300° C., wherein a cooling rate in the melting and casting is 200° C./min or more. 15. The method of producing a NiIr-base heat-resistant alloy according to claim 14 , wherein the aging heat treatment is carried out by heating the alloy in the temperature range of 700 to 1300° C., and then cooling at a cooling rate of 5 to 80° C./sec. 16. The method of producing a NiIr-base heat-resistant alloy according to claim 14 , wherein the NiIr-base alloy is subjected to a homogenization heat treatment in a temperature range of 1100 to 1800° C., prior to the aging heat treatment. 17. A method of producing a NiIr-base heat-resistant alloy, comprising: melting and casting for producing an alloy ingot having the composition according to claim 4 by a melting and casting method and subjecting the alloy ingot to an aging heat treatment in a temperature range of 700 to 1300° C., wherein a cooling rate in the melting and casting is 200° C./min or more. 18. The method of producing a NiIr-base heat-resistant alloy according to claim 17 , wherein the aging heat treatment is carried out by heating the alloy in the temperature range of 700 to 1300° C., and then cooling at a cooling rate of 5 to 80° C./sec. 19. The method of producing a NiIr-base heat-resistant alloy according to claim 17 , wherein the NiIr-base alloy is subjected to a homogenization heat treatment in a temperature range of 1100 to 1800° C., prior to the aging heat treatment.
of nickel or cobalt or alloys based thereon · CPC title
based on nickel · CPC title
Alloys containing less than 50% by weight of each constituent · CPC title
with the maximum Cr content being at least 10% but less than 20% · CPC title
with the maximum Cr content being at least 20% but less than 30% · CPC title
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