Patent US4078951A successfully refreshed from Google Patents.
US4078951A
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Method of improving fatigue life of cast nickel based superalloys and composition
Assignee: University Patents Inc
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Filing: 1976-03-31
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Granted: 1978-03-14
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Expires: 1996-03-31
Abstract
Abstract The invention consists of a method of producing a fine equiaxed grain structure (ASTM 2-4) in cast nickel-base superalloys which increases low cycle fatigue lives without detrimental effects on stress rupture properties to temperatures as high as 1800 DEG F. These superalloys are variations of the basic nickel-chromium matrix, hardened by gamma prime [Ni3 (Al, Ti)] but with optional additions of cobalt, tungsten, molybdenum, vanadium, columbium, tantalum, boron, zirconium, carbon and hafnium. The invention grain refines these alloys to ASTM 2 to 4 increasing low cycle fatigue life by a factor of 2 to 5 (i.e. life of 700 hours would be increased to 1400 to 3500 hours for a given stress) as a result of the addition of 0.01% to 0.2% of a member of the group consisting of boron, zirconium and mixtures thereof to aid heterogeneous nucleation. The alloy is vacuum melted and heated to 250 DEG -400 DEG F. above the melting temperature, cooled to partial solidification, thus resulting in said heterogeneous nucleation and fine grains, then reheated and cast at about 50 DEG -100 DEG F. of superheat. Additions of 0.1% boron and 0.1% zirconium (optional) are the preferred nucleating agents.
Inventors
- 👤 Allen F. Denzine
- 👤 Thomas A. Kolakowski
- 👤 John F. Wallace
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-03 22:18
CPC Classifications
C; C22; C22F; C22F1/00; C22F1/10
Claims Analysis
Total Claims: 20
Claim 1
Independent Claim
169 words
A method for producing heterogeneous nuclei in test nickel-base superalloys which results in the grain refinement of said superalloys and in the improvement of the low cycle fatigue properties in said superalloys while mantaining the present stress rupture properties of said superalloys, comprising: charging a nickel-base superalloy in a crucible; adding to said superalloy from 0.01 to 0.20 percent of a member selected from the group consisting of boron, zirconium and mixtures thereof for causing the formation of a substrate for heterogeneous nucleation; melting said charged nickel-base superalloy and said selected member in a vacuum furnace; superheating said charged nickel-base superalloy and said selected member to a temperature of about 250° F. to about 400° F. above said melting temperature in a period of about two minutes to about eight minutes to form heterogeneous nuclei in said nickel-base superalloy; and cooling until partial solidification, reheating and pouring said superalloy with about 50° F. to about 100° F. of superheat, whereby an equiaxed fine grain structure results in said superalloy.
Claim 2
Independent Claim
169 words
A method for producing heterogeneous nuclei in test nickel-base superalloys which results in the grain refinement of said superalloys and in the improvement of the low cycle fatigue properties in said superalloys while mantaining the present stress rupture properties of said superalloys, comprising: charging a nickel-base superalloy in a crucible; adding to said superalloy from 0.01 to 0.20 percent of a member selected from the group consisting of boron, zirconium and mixtures thereof for causing the formation of a substrate for heterogeneous nucleation; melting said charged nickel-base superalloy and said selected member in a vacuum furnace; superheating said charged nickel-base superalloy and said selected member to a temperature of about 250° F. to about 400° F. above said melting temperature in a period of about two minutes to about eight minutes to form heterogeneous nuclei in said nickel-base superalloy; and cooling until partial solidification, reheating and pouring said superalloy with about 50° F. to about 100° F. of superheat, whereby an equiaxed fine grain structure results in said superalloy.
Claim 3
Dependent Claim
59 words
The method as described in claim 1 wherein said nickel-base superalloy is: carbon; 0.02 - 0.35 chromium; 6.0 - 17.0 molybdenum; 2.5 columbium, Tantalum; 0.25 - 3.0 aluminum; 2.0 - 8.0 titanium; 0.1 - 3.0 boron; 0.001 - .2 zirconium; 0.001 - .5 cobalt; 2.0 - 15.0 tungsten; 5.0 - 20.0 nickel; Balance plus impurities as low as possible.
Claim 4
Dependent Claim
53 words
The method as described in claim 1 wherein said nickel-base superalloy is: carbon; 0.03 - 0.07 chronium; 11.0 - 13.0 molybdenum; 3.8 - 5.20 columbium, tantalum; 1.50 - 2.50 aluminum; 5.50 - 6.50 titanium; 0.40 - 1.00 boron; 0.005 - 0.015 zirconium; 0.05 - 0.15 nickel; Balance plus impurities as low as possible.
Claim 5
Dependent Claim
65 words
The method as described in claim 1 wherein said nickel-base superalloy is: carbon; 0.14 - 0.18 chromium; 11.2 - 11.8 molybdenum; 1.75 - 2.25 columbium, tantalum; 4.80 - 5.20 aluminum; 3.30 - 3.70 titanium; 3.80 - 4.20 boron; 0.010 - 0.020 zirconium; 0.05 - 0.12 cobalt; 8.0 - 9.0 tungsten; 4.8 - 5.2 hafnium; 0.80 - 1.202 nickel; Balance plus impurities as low as possible.
Claim 6
Dependent Claim
16 words
The method as described in claim 1 wherein said casting takes place in an inert atmosphere.
Claim 7
Dependent Claim
16 words
The method as described in claim 1 wherein said added selected member is 0.1 percent boron.
Claim 8
Dependent Claim
23 words
The method as described in claim 1 wherein said added selected member is a combination of 0.1 percent boron and 0.1 percent zirconium.
Claim 9
Independent Claim
104 words
A method of grain refining cast nickel-base superalloys which comprises: combining said superalloy with 0.01 percent to 0.20 percent of a member selected from the group consisting of boron, zirconium and mixtures thereof; melting said superalloy and said selected member in a furnace; superheating said superalloy and said selected member to a temperature of about 250° to about 400° F. above said melting temperature in a period of about 2 minutes to about 8 minutes; and cooling until partial solidification, reheating and pouring said superalloy with about 50° F. to about 100° F. superheat, whereby an equiaxed fine grain structure results in said superalloy.
Claim 10
Independent Claim
104 words
A method of grain refining cast nickel-base superalloys which comprises: combining said superalloy with 0.01 percent to 0.20 percent of a member selected from the group consisting of boron, zirconium and mixtures thereof; melting said superalloy and said selected member in a furnace; superheating said superalloy and said selected member to a temperature of about 250° to about 400° F. above said melting temperature in a period of about 2 minutes to about 8 minutes; and cooling until partial solidification, reheating and pouring said superalloy with about 50° F. to about 100° F. superheat, whereby an equiaxed fine grain structure results in said superalloy.
Claim 11
Dependent Claim
13 words
The method of claim 8 in which said furnace is a vacuum furnace.
Claim 12
Dependent Claim
15 words
The method of claim 8 in which an inert atmosphere is used in said furnace.
Claim 13
Dependent Claim
14 words
The method of claim 8 in which said selected member is 0.1 percent boron.
Claim 14
Dependent Claim
21 words
The method of claim 8 in which said selected member is a combination of 0.1 percent boron and 0.1 percent zirconium.
Claim 15
Dependent Claim
175 words
A new, improved cast nickel-base superalloy consisting essentially of the following approximate composition: Carbon; 0.02 - 0.17 Chromium; 6.0 - 20.0 Cobalt; 2.0 - 15.0 Molybdenum; 1.7 - 6.0 Tungsten (W); 2.5 - 20.0 Columbium, Tantalum; 0.9 - 6.5 Iron; 0 - 4.5 Titanium; 0.1 - 4.7 Aluminum; 2.0 - 8.0 Boron; 0.001 - 0.20 Zirconium; 0.001 - 0.50 Nickel; Balance plus impurities as low as possible, the improvement of which consists of a grain refining agent having 0.01 percent to 0.20 percent selected from the group consisting of boron, zirconium and mixtures thereof, and further being characterized by a fine equiaxed grain structure with an ASTM grain size of two or finer and by improved fatigue life at both room and elevated temperatures (1400° F.) by a factor of at least four in terms of strain reversals to failure in the range of 0.001 to 0.008 strain amplitude without deterioration of stress rupture life to temperatures as high as 1800° F. when compared to the same cast nickel-base superalloy in the non-grain refined condition.
Claim 16
Dependent Claim
175 words
A new, improved cast nickel-base superalloy consisting essentially of the following approximate composition: Carbon; 0.02 - 0.17 Chromium; 6.0 - 20.0 Cobalt; 2.0 - 15.0 Molybdenum; 1.7 - 6.0 Tungsten (W); 2.5 - 20.0 Columbium, Tantalum; 0.9 - 6.5 Iron; 0 - 4.5 Titanium; 0.1 - 4.7 Aluminum; 2.0 - 8.0 Boron; 0.001 - 0.20 Zirconium; 0.001 - 0.50 Nickel; Balance plus impurities as low as possible, the improvement of which consists of a grain refining agent having 0.01 percent to 0.20 percent selected from the group consisting of boron, zirconium and mixtures thereof, and further being characterized by a fine equiaxed grain structure with an ASTM grain size of two or finer and by improved fatigue life at both room and elevated temperatures (1400° F.) by a factor of at least four in terms of strain reversals to failure in the range of 0.001 to 0.008 strain amplitude without deterioration of stress rupture life to temperatures as high as 1800° F. when compared to the same cast nickel-base superalloy in the non-grain refined condition.
Claim 17
Dependent Claim
15 words
The improved composition of claim 13 wherein said grain refining agent is 0.1 percent boron.
Claim 18
Dependent Claim
22 words
The improved composition of claim 13 wherein said grain refining agent is a combination of 0.1 percent boron and 0.1 percent zirconium.
Claim 19
Dependent Claim
154 words
A new, improved cast nickel-base superalloy having a fine equiaxed grain structure and improved fatigue life at both room and elevated temperatures (1400° F.), formed by a process involving: charging a nickel-base superalloy in a crucible; adding to said superalloy from 0.01 to 0.20 percent of a member selected from the group consisting of boron, zirconium and mixtures thereof for causing the formation of a substrate for heterogeneous nucleation; melting said charged nickel-base superalloy and said selected member in a vacuum furnace; superheating said charged nickel-base superalloy and said selected member to a temperature of about 250° F. to about 400° F. above said melting temperature in a period of about 2 minutes to about 8 minutes to form heterogeneous nuclei in said nickel-base superalloy; and cooling until partial solidification, reheating and pouring said superalloy with about 50° to about 100° F. of superheat, whereby an equiaxed fine grain structure results in said superalloy.
Claim 20
Dependent Claim
154 words
A new, improved cast nickel-base superalloy having a fine equiaxed grain structure and improved fatigue life at both room and elevated temperatures (1400° F.), formed by a process involving: charging a nickel-base superalloy in a crucible; adding to said superalloy from 0.01 to 0.20 percent of a member selected from the group consisting of boron, zirconium and mixtures thereof for causing the formation of a substrate for heterogeneous nucleation; melting said charged nickel-base superalloy and said selected member in a vacuum furnace; superheating said charged nickel-base superalloy and said selected member to a temperature of about 250° F. to about 400° F. above said melting temperature in a period of about 2 minutes to about 8 minutes to form heterogeneous nuclei in said nickel-base superalloy; and cooling until partial solidification, reheating and pouring said superalloy with about 50° to about 100° F. of superheat, whereby an equiaxed fine grain structure results in said superalloy.
References Cited (Backward Citations)
US3459545A
Cited
US3620719A
Cited
USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1981-03-13 | 1981-09-12 | 1982-03-14 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1985-03-13 | 1985-09-12 | 1986-03-14 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1989-03-13 | 1989-09-12 | 1990-03-14 | $7700.00 | Window Closed / Lapsed |