High strength, corrosion resistant austenitic alloys
원문보기
IPC분류정보
국가/구분
United States(US) Patent
등록
국제특허분류(IPC7판)
C22C-038/00
C22C-038/42
C22C-038/44
C22C-038/46
C22C-038/48
C22C-038/52
C22C-038/58
C22C-038/02
C22C-038/04
출원번호
US-0331135
(2011-12-20)
등록번호
US-9347121
(2016-05-24)
발명자
/ 주소
Forbes Jones, Robin M.
Evans, C. Kevin
Lippard, Henry E.
Mills, Adrian R.
Riley, John C.
Dunn, John J.
출원인 / 주소
ATI PROPERTIES, INC.
대리인 / 주소
K&L Gates LLP
인용정보
피인용 횟수 :
2인용 특허 :
13
초록▼
An austenitic alloy may generally comprise, in weight percentages based on total alloy weight: up to 0.2 carbon; up to 20 manganese; 0.1 to 1.0 silicon; 14.0 to 28.0 chromium; 15.0 to 38.0 nickel; 2.0 to 9.0 molybdenum; 0.1 to 3.0 copper; 0.08 to 0.9 nitrogen; 0.1 to 5.0 tungsten; 0.5 to 5.0 cobalt;
An austenitic alloy may generally comprise, in weight percentages based on total alloy weight: up to 0.2 carbon; up to 20 manganese; 0.1 to 1.0 silicon; 14.0 to 28.0 chromium; 15.0 to 38.0 nickel; 2.0 to 9.0 molybdenum; 0.1 to 3.0 copper; 0.08 to 0.9 nitrogen; 0.1 to 5.0 tungsten; 0.5 to 5.0 cobalt; up to 1.0 titanium; up to 0.05 boron; up to 0.05 phosphorus; up to 0.05 sulfur; iron; and incidental impurities.
대표청구항▼
1. An austenitic alloy comprising, in weight percentages: up to 0.2 carbon;3.5 to 10.0 manganese;0.1 to 1.0 silicon;14.0 to 28.0 chromium;15.0 to 38.0 nickel;2.0 to 9.0 molybdenum;0.1 to 3.0 copper;0.08 to 0.9 nitrogen;0.1 to 5.0 tungsten;0.5 to 5.0 cobalt;up to 1.0 titanium;up to 0.05 boron;up to 0
1. An austenitic alloy comprising, in weight percentages: up to 0.2 carbon;3.5 to 10.0 manganese;0.1 to 1.0 silicon;14.0 to 28.0 chromium;15.0 to 38.0 nickel;2.0 to 9.0 molybdenum;0.1 to 3.0 copper;0.08 to 0.9 nitrogen;0.1 to 5.0 tungsten;0.5 to 5.0 cobalt;up to 1.0 titanium;up to 0.05 boron;up to 0.05 phosphorus;up to 0.05 sulfur;iron; andincidental impurities. 2. The alloy of claim 1 further comprising at least one of columbium and tantalum, wherein a combined weight percentage of columbium and tantalum is up to 0.3. 3. The alloy of claim 1 further comprising up to 0.2 weight percent vanadium. 4. The alloy of claim 1 further comprising up to 0.1 weight percent aluminum. 5. The alloy of claim 1 further comprising at least one of cerium and lanthanum, wherein a combined weight percentage of cerium and lanthanum is no greater than 0.1. 6. The alloy of claim 1 further comprising up to 0.5 weight percent ruthenium. 7. The alloy of claim 1 further comprising up to 0.6 weight percent zirconium. 8. The alloy of claim 1, wherein the iron is up to 60 weight percent. 9. The alloy of claim 1 comprising a cobalt/tungsten ratio, based on weight percentages, from 2:1 to 4:1. 10. The alloy of claim 1 having a PRE N16 value of greater than 40. 11. The alloy of claim 1 having a PRE N16 value from 40 to 60. 12. The alloy of claim 1, wherein the alloy is non-magnetic. 13. The alloy of claim 1 having a magnetic permeability value of less than 1.01. 14. The alloy of claim 1 having an ultimate tensile strength of at least 110 ksi, a yield strength of at least 50 ksi, and a percent elongation of at least 15%. 15. The alloy of claim 1 having an ultimate tensile strength in the range of 90 ksi to 150 ksi, a yield strength in the range of 50 ksi to 120 ksi, and a percent elongation in the range of 20% to 65%. 16. The alloy of claim 1 having an ultimate tensile strength in the range of 100 ksi to 240 ksi, a yield strength in the range of 110 ksi to 220 ksi, and a percent elongation in the range of 15% to 30%. 17. The alloy of claim 1 having a critical pitting temperature of at least 45° C. 18. The alloy of claim 1 comprising, in weight percentages based on total alloy weight: up to 0.05 carbon;3.5 to 10.0 manganese;0.1 to 1.0 silicon;18.0 to 26.0 chromium;19.0 to 37.0 nickel;3.0 to 7.0 molybdenum;4 to 2.5 copper;0.1 to 0.55 nitrogen;0.2 to 3.0 tungsten;0.8 to 3.5 cobalt;up to 0.6 titanium;a combined weight percentage of columbium and tantalum no greater than 0.3;up to 0.2 vanadium;up to 0.1 aluminum;up to 0.05 boron;up to 0.05 phosphorus;up to 0.05 sulfur;iron; andincidental impurities. 19. The alloy of claim 18, wherein the manganese is 3.5 to 8.0 weight percent. 20. The alloy of claim 18, wherein the chromium is 19.0 to 25.0 weight percent. 21. The alloy of claim 18, wherein the nickel is 20.0 to 35.0 weight percent. 22. The alloy of claim 18, wherein the molybdenum is 3.0 to 6.5 weight percent. 23. The alloy of claim 18, wherein the copper is 0.5 to 2.0 weight percent. 24. The alloy of claim 18, wherein the tungsten is 0.3 to 2.5 weight percent. 25. The alloy of claim 18, wherein the cobalt is 1.0 to 3.5 weight percent. 26. The alloy of claim 18, wherein the iron is 20 to 50 weight percent. 27. The alloy of claim 1 comprising, in weight percentages based on total alloy weight: up to 0.05 carbon;3.5 to 8.0 manganese;0.1 to 0.5 silicon;19.0 to 25.0 chromium;20.0 to 35.0 nickel;3.0 to 6.5 molybdenum;0.5 to 2.0 copper;0.2 to 0.5 nitrogen;0.3 to 2.5 tungsten;1.0 to 3.5 cobalt;up to 0.6 titanium;a combined weight percentage of columbium and tantalum no greater than 0.3;up to 0.2 vanadium;up to 0.1 aluminum;up to 0.05 boron;up to 0.05 phosphorus;up to 0.05 sulfur;iron;trace elements; andincidental impurities. 28. The alloy of claim 27, wherein the manganese is 4.0 to 6.0. 29. The alloy of claim 27, wherein the chromium is 20.0 to 22.0 weight percent. 30. The alloy of claim 27, wherein the molybdenum is 6.0 to 6.5 weight percent. 31. The alloy of claim 27, wherein the iron is 40 to 45 weight percent. 32. The alloy of claim 1, wherein the nitrogen is 0.1 to 0.55 weight percent. 33. The alloy of claim 1, wherein the nitrogen is 0.2 to 0.5 weight percent. 34. The alloy of claim 18, wherein the nitrogen is 0.2 to 0.5 weight percent. 35. The alloy of claim 1, wherein the manganese is 3.5 to 6.5 weight percent. 36. The alloy of claim 1, wherein the manganese is 4.0 to 6.0 weight percent. 37. The alloy of claim 18, wherein the manganese is 3.5 to 6.5 weight percent.
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