High temperature niobium-bearing superalloys

Patent metadata

Field	Value
Publication number	US-9938610-B2
Application number	US-201414490103-A
Country	US
Kind code	B2
Filing date	Sep 18, 2014
Priority date	Sep 20, 2013
Publication date	Apr 10, 2018
Grant date	Apr 10, 2018

Abstract

Nickel-base superalloys having gamma prime strengthening precipitates in a gamma matrix and little or no tertiary incoherent phases, such as delta, delta variants and eta.

First claim

What is claimed is:

1. A nickel-based niobium bearing superalloy including about of 2.2 to 4 wt. % aluminum, about 0.01 to 0.05 wt. % boron, about 0.02 to 0.06 wt. % carbon, about 6 to 15 wt. % chromium, about 0 to 20 wt. % cobalt, about 0 to 0.5 wt. % hafnium, about 1 to 3 wt. % molybdenum, about 7.2 to 16 wt. % niobium, about 0 to 0.6 wt. % silicon, about 1 to 5 wt. % tantalum, about 0 to 1.5 wt. % titanium, about 1 to 3 wt. % tungsten, about 0.04 to 0.1 wt. % zirconium and the balance nickel and incidental impurities,
wherein the nickel-based niobium bearing superalloy has a microstructure of essentially gamma phase and gamma prime phase, and wherein the volume percentage of gamma prime phase is about 45% to about 50% and the balance of the microstructure is gamma phase.

2. A niobium bearing superalloy according to claim 1 including about 3.3 wt. % aluminum, about 9.0 wt. % chromium and about 9.6 wt. % niobium.

3. A niobium bearing superalloy according to claim 1 including about 3.8 wt. % aluminum, about 9.1 wt. % chromium and about 8.1 wt. % niobium.

4. A niobium bearing superalloy according to claim 1 including about 2.8 wt. % aluminum, about 8.9 wt. % chromium and about 11.1 wt. % niobium.

5. A niobium bearing superalloy according to claim 1 including about 3.3 wt. % aluminum, about 13.6 wt. % chromium and about 9.7 wt. % niobium.

6. A niobium bearing superalloy according to claim 1 including about 3.3 wt. % aluminum, about 9.0 wt. % chromium and about 9.6 wt. % niobium.

7. A niobium bearing superalloy according to claim 1 including about 3.2 wt. % aluminum, about 8.8 wt. % chromium and about 8.7 wt. % niobium.

8. A nickel-based niobium bearing superalloy consisting of 2.5 to 5 wt. % aluminum, 0.01 to 0.05 wt. % boron, 0.02 to 0.06 wt. % carbon, 8 to 15 wt. % chromium, 0 to 20 wt. % cobalt, 0 to 0.5 wt. % hafnium, 1 to 3 wt. % molybdenum, 6 to 12 wt. % niobium, 0 to 0.6 wt. % silicon, 1 to 5 wt. % tantalum, 0 to 1.5 wt. % titanium, 1 to 3 wt. % tungsten, 0.04-0.1 wt % zirconium and the balance nickel and incidental impurities,
wherein the nickel-based niobium bearing superalloy has a microstructure of essentially gamma phase and gamma prime phase, and wherein the volume percentage of gamma prime phase is about 45% to about 50% and the balance of the microstructure is gamma phase.

9. A nickel-based niobium bearing superalloy according to claim 8 consisting of 3 to 4.5 wt. % aluminum, 0.01 to 0.05 wt. % boron, 0.02 to 0.06 wt. % carbon, 10 to 15 wt. % chromium, 8 to 20 wt. % cobalt, 0 to 0.5 wt. % hafnium, 1 to 3 wt. % molybdenum, 6 to 9.5 wt. % niobium, 0 to 0.6 wt. % silicon, 1 to 5 wt. % tantalum, 0 to 0.5 wt. % titanium, 1 to 3 wt. % tungsten, 0.04-0.1 wt % zirconium and the balance nickel and incidental impurities.

10. A nickel-based niobium bearing superalloy according to claim 8 consisting of 3.5 to 4.5 wt. % aluminum, 0.01 to 0.05 wt. % boron, 0.02 to 0.06 wt. % carbon, 11 to 13.5 wt. % chromium, 10 to 18 wt. % cobalt, 0 to 0.5 wt. % hafnium, 1 to 3 wt. % molybdenum, 6.5 to 8.5 wt. % niobium, 0 to 0.6 wt. % silicon, 1 to 5 wt. % tantalum, 0 to 0.5 wt. % titanium, 1 to 3 wt. % tungsten, 0.04-0.1 wt % zirconium and the balance nickel and incidental impurities.

11. A nickel-based niobium bearing superalloy including about of 2.5 to 5 wt. % aluminum, about 0.01 to 0.05 wt. % boron, about 0.02 to 0.06 wt. % carbon, about 8 to 15 wt. % chromium, about 0 to 20 wt. % cobalt, about 0 to 0.5 wt. % hafnium, about 1 to 3 wt. % molybdenum, about 6 to 12 wt. % niobium, about 0 to 0.6 wt. % silicon, about 1 to 5 wt. % tantalum, about 0 to 1.5 wt. % titanium, about 1 to 3 wt. % tungsten, about 0.04 to 0.1 wt. % zirconium and the balance nickel and incidental impurities,
wherein the nickel-based niobium bearing superalloy has a microstructure of essentially gamma phase and gamma prime phase, and wherein the volume percentage of gamma prime phase is about 45% to about 50% and the balance of the microstructure is gamma phase.

12. A nickel-based niobium bearing superalloy according to claim 11 including about 3 to 4.5 wt. % aluminum, about 0.01 to 0.05 wt. % boron, about 0.02 to 0.06 wt. % carbon, about 10 to 15 wt. % chromium, about 8 to 20 wt. % cobalt, about 0 to 0.5 wt. % hafnium, about 1 to 3 wt. % molybdenum, about 6 to 9.5 wt. % niobium, about 0 to 0.6 wt. % silicon, about 1 to 5 wt. % tantalum, about 0 to 0.5 wt. % titanium, about 1 to 3 wt. % tungsten, about 0.04 to 0.1 wt. % zirconium and the balance nickel and incidental impurities.

13. A nickel-based niobium bearing superalloy according to claim 11 including about 3.5 to 4.5 wt. % aluminum, about 0.01 to 0.05 wt. % boron, about 0.02 to 0.06 wt. % carbon, about 11 to 13.5 wt. % chromium, about 10 to 18 wt. % cobalt, about 0 to 0.5 wt. % hafnium, about 1 to 3 wt. % molybdenum, about 6.5 to 8.5 wt. % niobium, about 0 to 0.6 wt. % silicon, about 1 to 5 wt. % tantalum, about 0 to 0.5 wt. % titanium, about 1 to 3 wt. % tungsten, about 0.04 to 0.1 wt. % zirconium and the balance nickel and incidental impurities.

14. A nickel-based niobium bearing superalloy according to claim 11 including about 3.4 wt. % aluminum, about 12.1 wt. % chromium, about 8.5 wt. % niobium, about 2.4 wt. % molybdenum, about 2.3 wt. % tungsten and about 3.0 wt. % tantalum.

15. A nickel-based niobium bearing superalloy according to claim 11 including about 4.1 wt. % aluminum, about 12.2 wt. % chromium, about 8.6 wt. % niobium, about 2.4 wt. % molybdenum, about 2.3 wt. % tungsten and about 3.0 wt. % tantalum.

16. A nickel-based niobium bearing superalloy according to claim 11 including about 4.1 wt. % aluminum, about 10.5 wt. % chromium, about 7.0 wt. % niobium, about 2.4 wt. % molybdenum, about 2.3 wt. % tungsten and about 3.0 wt. % tantalum.

17. A nickel-based niobium bearing superalloy according to claim 11 including about 3.6 wt. % aluminum, about 12.1 wt. % chromium, about 7.0 wt. % niobium, about 2.4 wt. % molybdenum, about 2.3 wt. % tungsten and about 3.0 wt. % tantalum.

18. A niobium bearing superalloy according to claim 11 including about 3.3 wt. % aluminum, about 9.0 wt. % chromium and about 9.6 wt. % niobium.

19. A niobium bearing superalloy according to claim 11 including about 3.8 wt. % aluminum, about 9.1 wt. % chromium and about 8.1 wt. % niobium.

20. A niobium bearing superalloy according to claim 11 including about 3.2 wt. % aluminum, about 8.8 wt. % chromium and about 8.7 wt. % niobium.

Assignees

• Rolls Royce Corp
• Illinois Institute Of Tech

Inventors

• Helmink Randolph C
• Tin Sammy

Classifications

• C22C19/05

  with chromium · CPC title

• C22C19/056 Primary

  with the maximum Cr content being at least 10% but less than 20% · CPC title

• C22C19/057 Primary

  with the maximum Cr content being less 10% · CPC title

• C22C19/007

  with a light metal (alkali metal Li, Na, K, Rb, Cs; earth alkali metal Be, Mg, Ca, Sr, Ba, Al Ga, Ge, Ti) or B, Si, Zr, Hf, Sc, Y, lanthanides, actinides, as the next major constituent · CPC title