Creep and corrosion-resistant cast alumina-forming alloys for high temperature service in industrial and petrochemical applications

Patent metadata

Field	Value
Publication number	US-11866809-B2
Application number	US-202117162917-A
Country	US
Kind code	B2
Filing date	Jan 29, 2021
Priority date	Jan 29, 2021
Publication date	Jan 9, 2024
Grant date	Jan 9, 2024

Abstract

An austenitic Ni-base alloy, consisting essentially of, in weight percent: 2.5 to 4.75 Al; 21 to 26 Cr; 20 to 40 Fe; 0.75 to 2.5 total of at least one element elected from the group consisting of Nb and Ta; 0 to 0.25 Ti; 0.09 to 1.5 Si; 0 to 0.5 V; 0 to 2 Mn; 0 to 3 Cu; 0 to 2 of at least one element selected from the group consisting of Mo and W; 0 to 1 of at least one element selected from the group consisting of Zr and Hf; 0 to 0.15 Y; 0.3 to 0.55 C; 0.005 to 0.1 B; 0 to 0.05 P; less than 0.06 N and balance Ni (30 to 46 Ni), wherein the weight percent Ni is greater than the weight percent Fe, and wherein the ratio Ni/(Fe+2*C) is between 1.02 and 1.067.

First claim

We claim:

1. An austenitic Ni-base cast alloy, consisting essentially of, in weight percent:
2.5 to 4.75 Al;
21 to 26 Cr;
20 to 40 Fe;
0.75 to 2.5 total of at least one element selected from
the group consisting of Nb and Ta;
0 to 0.25 Ti;
0.09 to 1.5 Si;
0 to 0.5 V;
0 to 2 Mn;
0 to 3 Cu;
0 to 2 of at least one element selected from the group consisting of Mo and W;
0 to 1 of at least one element selected from the group consisting of Zr and Hf;
0 to 0.15 Y;
0.3 to 0.55 C;
0.005 to 0.1 B;
0 to 0.05 P;
0.002 to less than 0.06 N and
balance Ni (30 to 46 Ni),
wherein the weight percent Ni is greater than the weight percent Fe, wherein the ratio Ni/(Fe+2*C) is between 1.02 and 1.067, wherein said alloy forms an external continuous scale comprising alumina, and has a stable phase FCC austenitic matrix microstructure, said austenitic matrix being essentially delta-ferrite-free and essentially BCC-phase free, consisting of one or more carbide strengthening phases, and exhibits a creep rupture lifetime of at least 200 h at 900° C. and 50 MPa.

2. The alloys of claim 1 , wherein the mass change after 2000 hours of testing in 500 hour cycles at 900° C. in Air+10% water vapor environment is ±2 mg/cm 2 .

3. The alloys of claim 1 , wherein the mass change after 2000 hours of testing in 500 hour cycles at 900° C. in Air+10% water vapor environment is ±1 mg/cm 2 .

4. The alloys of claim 1 , wherein the mass change during oxidation testing in 500 hour cycles at 1000° C. in Air+10% water vapor environment after 1000 hour testing is ±2 mg/cm 2 .

5. The alloy of claim 1 , wherein a calculated MC carbide contents after solidification are between 0.5 and 3.0 wt. %, M 23 C 6 is between 2 and 6 wt. % and M 7 C 3 is between 0 and 3 wt. % with total carbide contents between 2.0 wt. % and 12 wt. %.

6. The alloy of claim 1 , wherein a calculated equilibrium contents of MC carbide is between 0.25 and 3.0 wt. %, M 23 C 6 is between 2 and 9 wt. % with total calculated carbide equilibrium contents between 2.0 wt. % and 12.0 wt. % at 900° C.

7. The alloy of claim 1 , wherein a calculated change in M 23 C 6 contents after 900° C. exposure is between 0.2 to 6 wt. %.

8. The alloy of claim 1 , wherein a calculated change in M 23 C 6 contents after 900° C. exposure is between 0.2 to 4 wt. %.

9. The alloy of claim 1 , wherein a calculated change in M 23 C 6 contents after 900° C. exposure is between 1.2 to 4 wt. %.

10. The alloy of claim 1 , wherein the calculated change in total carbide contents after 900° C. exposure is between 0.1 to 3.0 wt. %.

11. The alloy of claim 1 , wherein the change in total carbide contents after 900° C. exposure is between 0.1 and 1.5 wt. %, for a creep rupture lifetime of at least 100 h at 900° C. and 50 MPa.

12. The alloy of claim 1 , wherein the mass change during oxidation testing in 100 hour cycles at 1100° C. in Air+10% water vapor environment after 1000 hour testing is ±2 mg/cm 2 .

13. The alloy of claim 1 , wherein the mass change during oxidation testing in 100 hour cycles at 1100° C. in Air+10% water vapor environment after 1000 hour testing is ±1 mg/cm 2 .

14. The alloy of claim 1 , wherein the creep rupture lifetime at 1150° C., 7.17 MPa are between 200 and 1500 hours.

15. The alloy of claim 1 , wherein a calculated equilibrium contents of MC carbide is between 0.25 and 3 wt. %, M 23 C 6 is between 2 and 8 wt. % with total calculated carbide equilibrium contents between 2.0 wt. % and 9.0 wt. % at 1150° C.

16. The alloy of claim 1 , wherein a calculated change in M 23 C 6 contents after 1150° C. exposure is between 0.1 and 5.0 wt. %.

17. The alloy of claim 1 , wherein the calculated change in total carbide contents after 1150° C. exposure is between 0.0 to 2 wt. %.

18. The alloy of claim 1 , wherein the mass change during oxidation testing in 100 hour cycles at 1150° C. in Air+10% water vapor environment after 1000 hour testing is ±2 mg/cm 2 .

Assignees

• Ut Battelle Llc

Inventors

• Muralidharan Govindarajan
• Brady Michael P
• Yamamoto Yukinori

Classifications

• C22C30/00 Primary

  Alloys containing less than 50% by weight of each constituent · CPC title

• B32B9/00

  Layered products comprising a {layer of a} particular substance not covered by groups B32B11/00 - B32B29/00 · CPC title

• C22C19/055 Primary

  with the maximum Cr content being at least 20% but less than 30% · CPC title

• B32B2315/02

  Ceramics · CPC title