Nickel-base superalloys especially useful as compatible protective environmental coatings for advanced superaloys

• US 5,035,958 A
• Filed: 10/11/1989
• Issued: 07/30/1991
• Est. Priority Date: 12/27/1983
• Status: Expired due to Term

• Current Assignee: General Electric Company
• Original Assignee: General Electric Company
• Inventors: Yang, Swe-Wong, Prugar, Mark L., Jackson, Melvin R., Gigliotti, Michael F. X. Jr., Rairden, John R. III
• Primary Examiner(s): Lechert, Jr., Stephen J.
• Application Number:
  US07/420,708
• Time in Patent Office: 657 Days
• Field of Search: 420/443, 420/445, 420/448, 420/553, 428/414, 428/478
• US Class Current: 428/553
• CPC Class Codes: C22C 19/056 with the maximum Cr content being at least 10% but less than 20%
• CPC Class Codes: C22C 49/08 Iron group metals
• CPC Class Codes: Y10T 428/12063 Nonparticulate metal component
• CPC Class Codes: Y10T 428/12486 Laterally noncoextensive components [e.g., embedded, etc.]
• CPC Class Codes: Y10T 428/12931 Co-, Fe-, or Ni-base components, alternative to each other

Abstract

There is provided by the present invention an alloy which is mechanically and chemically compatible with advanced nickel-base superalloys and nickel-base eutectic superalloys and which possesses excellent resistance to high temperature oxidation. The alloy of the invention is, therefore, particularly useful as a protective environmental coating for the external surfaces of hot-stage aircraft gas turbine engine components, e.g., rotating blades and stationary vanes, made from such advanced superalloys.

Claims

1. A composition for application to nickel-base superalloy substrates consisting essentially of, by weight, 1 to 10% cobalt, 6 to 12% chromium, 5 to 8% aluminum, 1 to 10% tantalum, 1 to 10% tungsten, 0 to 3% rhenium, 0 to 2% molybdenum, 0.1 to 2% hafnium, 0.005 to 0.1% boron, 0.005 to 0.25% carbon, the balance nickel and incidental impurities.

2. The composition of claim 1 consisting essentially of, by weight, 1 to 6% cobalt, 7 to 10% chromium, 5 to 7% aluminum, 4 to 6% tantalum, 3.5 to 5.5% tungsten, 0 to 3% rhenium, 0 to 2% molybdenum, 0.5 to 1.5% hafnium, 0.005 to 0.025% boron, 0.005 to 0.025% carbon, the balance nickel and incidental impurities.

3. The composition of claim 2 consisting essentially of, weight, 3.8 to 4.2% cobalt, 8.3 to 8.7% chromium, 5.8 to 6.2% aluminum, 4.7 to 5.3% tantalum, 4.2 to 4.8% tungsten, 1.2 to 1.8% rhenium, 1.3 to 1.7% molybdenum, 0.7 to 1.1% hafnium, 0.005 to 0.02% boron, 0.005 to 0.02% carbon, the balance nickel and incidental impurities.

4. A high temperature oxidation and corrosion resistant coated nickel-base superalloy article characterized by high coating-substrate compatibility, said article comprising:

(a) a nickel-base superalloy or nickel-base eutictic superalloy substrate, and

(b) a coating providing at least a portion of the outer surface of said article, said coating consisting essentially of, by weight, 1 to 10% cobalt, 6 to 12% chromium, 5 to 8% aluminum, 1 to 10% tantalum, 1 to 10% tungsten, 0 to 3% rhenium, 0 to 2% molybdenum, 0.1 to 2% hafnium, 0.005 to 0.1% boron, 0.005 to 0.25% carbon, the balance nickel and incidental impurities.

5. The article of claim 4 wherein said coating consists essentially of, by weight, 1 to 6% cobalt, 7 to 10% chromium, 5 to 7% aluminum, 4 to 6% tantalum, 3.5 to 5.5% tungsten, 0 to 5% rhenium, 0 to 2% molybdenum, 0.5 to 1.5% hafnium, 0.005 to 0.025% boron, 0.005 to 0.25% carbon, the balance nickel and incidental impurities.

6. The article of claim 5 wherein said coating consists essentially of, by weight, 3.8 to 4.2% cobalt, 8.3 to 8.7% chromium, 5.8 to 6.2% aluminum, 4.7 to 5.3% tantalum, 4.2 to 4.8% tungsten, 1.2 to 1.8% rhenium, 1.3 to 1.7% molybdenum, 0.7 to 1.1% hafnium, 0.005 to 0.02% boron, 0.005 to 0.2% carbon, the balance nickel and incidental impurities.

7. The article of claim 4 wherein said substrate comprises a composite of a nickel-base superalloy matrix and an aligned fibrous monocarbide eutectic reinforcing phase embedded in said matrix, the substrate consisting essentially of, by weight, at least an amount in excess of an impurity amount up to 0.02% of boron, 0 to 9% rhenium, 0 to <

0.8% titanium, 0 to 20% chromium, 0 to 10% aluminum, 3 to 15% tantalum, 0.1 to 1% carbon, 0 to 20% cobalt, 0 to 20% tungsten, 0 to 7% vanadium, 0 to 10% molybdenum, 0 to 3% columbium, 0 to 3% hafnium, 0 to 1.5% zirconium, the balance nickel and incidental impurities.

8. The article of claim 7 wherein said substrate consists essentially of about, by weight, 0.01% boron, 6.44% rhenium, 3.84% chromium, 5.34% aluminum, 11.37% tantalum, 0.43% carbon, 3.8% cobalt, 4.33% tungsten, 3.01% molybdenum, the balance nickel and incidental impurities.

9. The article of claim 4 wherein said substrate comprises an improved nickel-base superalloy capable of being cast as a single crystal by directional solidification consisting essentially of, by weight, 7 to 12% chromium, 1 to 5% molybdenum, 3 to 5% titanium, 3 to 5% aluminum, 5 to 15% cobalt, 3 to 12% tungsten, 2 to 6% tantalum, up to 10% rhenium, up to 2% columbium, up to 3% vanadium, up to 2% hafnium, the balance nickel and incidental impurities, further characterized by the substantial absence of carbon, boron, and zirconium, the alloy having an Al:

Ti ratio in the range of abut 0.5 to about 1 while maintaining the Cr;

Al ratio in the range of about 1.5 to 4.

10. The article of claim 9 wherein said substrate consists essentially of, by weight, about 9.3% chromium, 7.5% cobalt, 3.7% aluminum, 4% tantalum, 4.2% titanium, 1.5% molybdenum, 6% aluminum, 0.5% niobium, the balance nickel and incidental impurities.

11. A composite article of manufacture comprising:

(i) a nickel-base superalloy or nickel-base eutectic superalloy substrate, and

(ii) one or more thick, built-up regions integral with said substrate, said regions providing at least a portion of the outer surface of said article, said regions having a composition consisting of, by weight, 1 to 10% cobalt, 6 to 12% chromium, 5 to 8% aluminum, 1 to 10% tantalum, 1 to 10% tungsten, 0 to 3% rhenium, 0 to 2% molybdenum, 0.1 to 2% hafnium, 0.005 to 0.1% boron, 0.005 to 0.25% carbon, the balance nickel and incidental impurities.

12. The composite article of claim 11 wherein said regions have a composition consisting essentially of, by weight, 1 to 6% cobalt, 7 to 10% chromium, 5 to 7% aluminum, 4 to 6% tantalum, 3.5 to 5.5% tungsten, 0 to 3% rhenium, 0 to 2% molybdenum, 0.5 to 1.5% hafnium, 0.005 to 0.025% boron, 0.005 to 0.25% carbon, the balance nickel and incidental impurities.

13. The composite article of claim 12 wherein said regions have a composition consisting essentially of, by weight, 3.8 to 4.2% cobalt, 8.3 to 8.7% chromium, 5.8 to 6.2% aluminum, 4.7 to 5.3% tantalum, 4.2 to 4.8% tungsten, 1.2 to 1.8% rhenium, 1.3 to 1.7% molybdenum, 0.7 to 1.1% hafnium, 0.005 to 0.02% boron, 0.005 to 0.2% carbon, the balance nickel and incidental impurities.

14. The article of claim 11 wherein said substrate comprises a composite of a nickel-base superalloy matrix and an aligned fibrous monocarbide eutectic reinforcing phase embedded in said matrix, the substrate consisting essentially of, by weight, at least an amount in excess of an impurity amount up to 0.02% of boron, 0 to 9% rhenium, 0 to <

0.8% titanium, 0 to 20% chromium, 0 to 10% aluminum, 3 to 15% tantalum, 0.1 to 1% carbon, 0 to 20% cobalt, 0 to 20% tungsten, 0 to 7% vanadium, 0 to 10% molybdenum, 0 to 3% columbium, <

0.15% hafnium, 0 to 1.5% zirconium, the balance essentially nickel and incidental impurities.

15. The article of claim 14 wherein said substrate comprises a composite of a nickel-base superalloy matrix and an aligned fibrous monocarbide eutectic reinforcing phase embedded in said matrix, the substrate consisting essentially of about, by weight, 0.01% boron, 6.44% rhenium, 3.84% chromium, 5.34% aluminum, 11.37% tantalum, 0.43% carbon, 3.8% cobalt, 4.33% tungsten, 3.01% molybdenum, the balance nickel and incidental impurities.

16. The article of claim 11 wherein said substrate comprises an improved nickel-base superalloy capable of being cast as a single crystal by directional solidification consisting essentially of, by weight:

7 to 12% chromium, 1 to 5% molybdenum, 3 to 5% titanium, 3 to 5% aluminum, 5 to 15% cobalt, 3 to 12% tungsten, 2 to 6% tantalum, up to 10% rhenium, up to 2% columbium, up to 3% vanadium, up to 2% hafnium, balance nickel and incidental impurities, and further characterized by the substantial absence of carbon, boron, and zirconium, the alloy having an Al;

Ti ratio in the range of about 0.5 to about 1 while maintaining the Cr;

Al ration in the range of about 1.5 to 4.

17. The article of claim 16 wherein said substrate comprises an improved nickel-base superalloy capable of being cast as a single crystal by directional solidification consisting essentially of, by weight:

about 9.3% chromium, 7.5% cobalt, 3.7% aluminum, 4% tantalum, 4.2% titanium, 1.5% molybdenum, 6% tungsten, 0.5% niobium, the balance nickel and incidental impurities.

18. The claim 11 article wherein said substrate is an aircraft gas turbine engine rotatable blade or stationary vane and said deposit is the tip portion thereof.