High temperature, damage tolerant superalloy, an article of manufacture made from the alloy, and process for making the alloy
A nickel-base alloy is disclosed that has the following weight percent composition. C about 0.005 to about 0.06 Cr about 13 to about 17 Fe about 4 to about 20 Mo about 3 to about 9 W up to about 8 Co up to about 12 Al about 1 to about 3 Ti about 0.6 to about 3 Nb up to about 5.5 B about 0.001 to about 0.012 Mg about 0.0010 to about 0.0020 Zr about 0.01 to about 0.08 Si up to about 0.7 P up to about 0.05 and the balance is nickel, usual impurities, and minor amounts of other elements as residuals from alloying additions during melting. The alloy provides a combination of high strength, good creep resistance, and good resistance to crack growth. A method of heat treating a nickel base superalloy to improve the tensile ductility of the alloy is also disclosed. An article of manufacture made from the nickel base superalloy described herein is also disclosed.
1. A process for improving the tensile ductility of a precipitation hardenable nickel-base superalloy comprising the steps of:
providing an intermediate product form made from a precipitation hardenable, nickel-base alloy;
determining the solvus temperature of γ′ phase in the precipitation hardenable, nickel-base alloy;
heating the intermediate product form at a supersolvus temperature for a time sufficient to solution the γ′ phase in the alloy; then
heating the intermediate product form at a subsolvus temperature for a time sufficient to cause precipitation and coarsening of γ′ precipitate in the alloy; and then
aging the intermediate product form at temperature and time conditions selected to precipitate γ′ phase in the alloy without further coarsening of the γ′ phase, said aging step comprising the steps of heating the intermediate product form at a temperature of about 1500° F. to about 1550° F. for about 4 hours, cooling the heated intermediate product form to room temperature, then heating the intermediate product form at a temperature of about 1350° F. to about 1400° F. for about 16 hours, and then air cooling the heated intermediate product form to room temperature.
2. The process as claimed in claim 1 wherein the subsolvus temperature is 10 to 150° F. below the γ′ solvus temperature.
3. The process as claimed in claim 1 wherein the supersolvus temperature is about 1850-2100° F.
4. The process as claimed in claim 1 comprising the step of cooling the intermediate product form at a rate of 100° F. per hour after the intermediate product form is heated at the subsolvus temperature.
5. The process as claimed in claim 1 wherein the step of cooling the heated intermediate product form consists of quenching the intermediate product form in water.
6. The process as claimed in claim 1 wherein the step of cooling the heated intermediate product form consists of cooling the intermediate product form in air.
7. The process as claimed in claim 1 wherein the precipitation hardenable nickel-base superalloy consists essentially of, in weight percent,
C about 0.005 to about 0.06
Cr about 13 to about 17
Fe about 4 to about 20
Mo about 3 to about 9
W up to about 8
Co up to about 12
Al about 1 to about 3
Ti about 0.6 to about 3
Nb up to about 5.5
B about 0.001 to about 0.012
Mg about 0.0010 to about 0.0020
Zr about 0.01 to about 0.08
Si up to about 0.7
P up to about 0.05
and the balance is nickel, usual impurities, and minor amounts of other elements as residuals from alloying additions during melting.
8. A process for improving the tensile ductility of a precipitation hardenable nickel-base superalloy comprising the steps of:
providing an intermediate product form made from a precipitation hardenable, nickel-base alloy;
determining the solvus temperature of γ′ phase in the precipitation hardenable, nickel-base alloy;
heating the intermediate product form at a supersolvus temperature for a time sufficient to solution the γ′ phase in the alloy; then
heating the intermediate product form at a subsolvus temperature for a time sufficient to cause precipitation and coarsening of γ′ precipitate in the alloy; and then
aging the intermediate product form by heating at about 1400° F. for about 16 hours to precipitate γ′ phase in the alloy without further coarsening of the γ′ phase and then air cooling the heated intermediate product form to room temperature.
9. The process as claimed in claim 8 wherein the subsolvus temperature is 10 to 150° F. below the γ′ solvus temperature.
10. The process as claimed in claim 8 wherein the supersolvus temperature is about 1850-2100° F.
11. The process as claimed in claim 8 comprising the step of cooling the intermediate product form at a rate of 100° F. per hour after the intermediate product form is heated at the subsolvus temperature.
12. The process as claimed in claim 8 wherein the precipitation hardenable nickel-base superalloy consists essentially of, in weight percent,
C about 0.005 to about 0.06
Cr about 13 to about 17
Fe about 4 to about 20
Mo about 3 to about 9
W up to about 8
Co up to about 12
Al about 1 to about 3
Ti about 0.6 to about 3
Nb up to about 5.5
B about 0.001 to about 0.012
Mg about 0.0010 to about 0.0020
Zr about 0.01 to about 0.08
Si up to about 0.7
P up to about 0.05
and the balance is nickel, usual impurities, and minor amounts of other elements as residuals from alloying additions during melting.