US3475165A - Nickel-base alloys - Google Patents
Nickel-base alloys Download PDFInfo
- Publication number
- US3475165A US3475165A US666143A US3475165DA US3475165A US 3475165 A US3475165 A US 3475165A US 666143 A US666143 A US 666143A US 3475165D A US3475165D A US 3475165DA US 3475165 A US3475165 A US 3475165A
- Authority
- US
- United States
- Prior art keywords
- cobalt
- nickel
- alloy
- hardness
- alloys
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
Links
- 229910045601 alloy Inorganic materials 0.000 title description 26
- 239000000956 alloy Substances 0.000 title description 26
- 239000010941 cobalt Substances 0.000 description 21
- 229910017052 cobalt Inorganic materials 0.000 description 21
- GUTLYIVDDKVIGB-UHFFFAOYSA-N cobalt atom Chemical compound [Co] GUTLYIVDDKVIGB-UHFFFAOYSA-N 0.000 description 21
- 235000019589 hardness Nutrition 0.000 description 19
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 12
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 10
- ZOXJGFHDIHLPTG-UHFFFAOYSA-N Boron Chemical compound [B] ZOXJGFHDIHLPTG-UHFFFAOYSA-N 0.000 description 8
- 229910052796 boron Inorganic materials 0.000 description 8
- 238000007792 addition Methods 0.000 description 7
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 description 6
- 229910052804 chromium Inorganic materials 0.000 description 6
- 239000011651 chromium Substances 0.000 description 6
- 229910052742 iron Inorganic materials 0.000 description 6
- WFKWXMTUELFFGS-UHFFFAOYSA-N tungsten Chemical compound [W] WFKWXMTUELFFGS-UHFFFAOYSA-N 0.000 description 6
- 229910052721 tungsten Inorganic materials 0.000 description 6
- 239000010937 tungsten Substances 0.000 description 6
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 description 5
- 239000000203 mixture Substances 0.000 description 5
- 229910052759 nickel Inorganic materials 0.000 description 5
- 229910052710 silicon Inorganic materials 0.000 description 5
- 239000010703 silicon Substances 0.000 description 5
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 4
- 229910052799 carbon Inorganic materials 0.000 description 4
- 229910000531 Co alloy Inorganic materials 0.000 description 2
- 239000004615 ingredient Substances 0.000 description 2
- WWVKQTNONPWVEL-UHFFFAOYSA-N caffeic acid phenethyl ester Natural products C1=C(O)C(O)=CC=C1C=CC(=O)OCC1=CC=CC=C1 WWVKQTNONPWVEL-UHFFFAOYSA-N 0.000 description 1
- 239000011248 coating agent Substances 0.000 description 1
- 238000000576 coating method Methods 0.000 description 1
- 230000003247 decreasing effect Effects 0.000 description 1
- NRUQNUIWEUZVLI-UHFFFAOYSA-O diethanolammonium nitrate Chemical compound [O-][N+]([O-])=O.OCC[NH2+]CCO NRUQNUIWEUZVLI-UHFFFAOYSA-O 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 229910052751 metal Inorganic materials 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 150000002739 metals Chemical class 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- SWUARLUWKZWEBQ-UHFFFAOYSA-N phenylethyl ester of caffeic acid Natural products C1=C(O)C(O)=CC=C1C=CC(=O)OCCC1=CC=CC=C1 SWUARLUWKZWEBQ-UHFFFAOYSA-N 0.000 description 1
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Classifications
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C19/00—Alloys based on nickel or cobalt
- C22C19/03—Alloys based on nickel or cobalt based on nickel
- C22C19/05—Alloys based on nickel or cobalt based on nickel with chromium
- C22C19/051—Alloys based on nickel or cobalt based on nickel with chromium and Mo or W
- C22C19/056—Alloys based on nickel or cobalt based on nickel with chromium and Mo or W with the maximum Cr content being at least 10% but less than 20%
Definitions
- This invention relates generally to nickel-base alloys of the type used for hard surfacing.
- a coating alloy known as Pratt & Whitney Aircraft Specification-PWA 693 has the following composition:
- composition of the basic alloy was as follows:
- composition of the basic alloy was as follows:
- Knoop hardness 0.5 1060 0.75 1162 1.00 1192 1.5 1419 5.0 1450 7.5 135 1 It is apparent from the upper graph that the Knoop hardness increased very rapidly, even with as little as 0.5% cobalt, and on up to 1.5% cobalt with a maximum hardness established at somewhere between 1.5 and 7% cobalt, and the hardness decreasing slightly beyond about 5% cobalt.
- a nickel-base alloy consisting of from 0.005 to 1.0% carbon, 2.5 to 4.75% silicon, 6 to 16% chromium, 7 to 17% tungsten, 2 to 5% iron, 1 to 5% boron, 0.5 to 7.5% cobalt, and the remainder essentially all nickel.
- a nickel-base alloy consisting of from 0.005 to 1.0% carbon, 2.5 to 4.00% silicon, 10 to 13% chromium, 15 to 17% tungsten, 2.5 to 4.3% iron, 1.75 to 3.25% boron, 2 to 5% cobalt, and the remainder essentially all nickel.
- a nickel-base alloy consisting of about 0.5% carbon, about 3.75% silicon, about 12% chromium, about 16% 3 4 tungsten, about 3.75% iron, about 3% boron, 2 to 2.5% References Cited cobalt, and the remainder essentially all nickel.
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- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Laminated Bodies (AREA)
Description
Oct. 28, 1969 A. T. CAPE I NICKEL-BASE ALLOYS Filed Sept v, 1967 INVENTOR.
ARTHUR T. CAPE SSHNOUVH dOONX ATTORNEYS United States Patent 3,475,165 NICKEL-BASE ALLOYS Arthur T. Cape, Monterey, Calif., assiguor to Coast Metals, Inc., Little Ferry, N.J., a corporation of Delaware Filed Sept. 7, 1967, Ser. No. 666,143 Int. Cl. C22c 19/02 US. Cl. 75-171 4 Claims ABSTRACT OF THE DISCLOSURE Effect of additions of cobalt to nickel-base alloys containing chromium, tungsten, iron and boron, and particularly the increase in Knoop hardness caused by such additions.
This invention relates generally to nickel-base alloys of the type used for hard surfacing.
A coating alloy known as Pratt & Whitney Aircraft Specification-PWA 693, has the following composition:
I have found, as the result of extensive tests that the Knoop hardnesses of the foregoing alloy can be greatly improved by incorporating in the aforesaid alloy cobalt, in a controlled amount such that the cobalt constitutes from .5 to 7.5% by weight of the alloy. At the same time, the ranges of several of the other ingredients of the aforesaid alloy may be broadened without detracting from the increased Knoop hardnesses or other desirable properties of .the alloy.
This increase in Knoop hardness is illustrated in the accompanying graph which forms a part of this application, and in which varying amounts of cobalt were incorporated in nickel-base alloys of slightly ditferent compositions, as follows:
In the lower graph, the composition of the basic alloy was as follows:
Without the addition of cobalt, the average Knoop hardness, as indicated in the graph, was 802.
With the addition to such alloy of cobalt in various amounts, the average Knoop hardness were as follows.
Cobalt added (percent) Knoop hardness 2.5 1092 5.0 125 8 10.0 1 168 It is apparent from the lower graph that the maximum hardness of the alloy was established as somewhere between and 7.5% cobalt, or, more strictly, between 4 and 7.5%, and that beyond 7.5% cobalt, the hardness falls off.
ICC
In the upper graph, the composition of the basic alloy was as follows:
Reference to this graph shows that the Knoop hardness of thes alloy, without cobalt, was 915, and that with the addition to the alloy of cobalt in various amounts, the average Knoop hardnesses were as follows.
Cobalt added (percent) Knoop hardness 0.5 1060 0.75 1162 1.00 1192 1.5 1419 5.0 1450 7.5 135 1 It is apparent from the upper graph that the Knoop hardness increased very rapidly, even with as little as 0.5% cobalt, and on up to 1.5% cobalt with a maximum hardness established at somewhere between 1.5 and 7% cobalt, and the hardness decreasing slightly beyond about 5% cobalt.
It further appears from a comparison of the two graphs that since the respective compositions were of substantially similar analysis from the viewpoint of those ingredients which do not enhance the hardness, that the difference in rate of hardness increase was due primarily to the dilference in the boron content of the alloys.
Stated in another way, the variation in hardness in such alloys, due to cobalt additions thereto, is apparently related, in some way to the boron content of the alloy. This relationship has not, as yet, been fully determined, but it is clear that the addition of cobalt to such alloys, in amounts of from 0.5 to 7.5%, does cause a marked increase in the Knoop hardnes.
The alloys, in accordance with the invention, are encompassed within the following ranges:
Broad Range Preferred Range Preferred Analysis Carbon 005-1. 00 0. l-O. 7 0. 5 Silicon 2. 5-4. 2. 54. 00 3. 75 Chromium 6-16 10-13 12 Tungsten 717 15-17 16 Iron 2-5 2. 5-4. 3 3. 75 Boron 1. 00-5. 00 1. 75-3. 25 3. 00 Cobalt 0. 5-7. 5 2-5 2-2. 5 Nickel Remainder Remainder Remainder Having thus described my invention, 1 claim:
1. A nickel-base alloy consisting of from 0.005 to 1.0% carbon, 2.5 to 4.75% silicon, 6 to 16% chromium, 7 to 17% tungsten, 2 to 5% iron, 1 to 5% boron, 0.5 to 7.5% cobalt, and the remainder essentially all nickel.
2. A nickel-base alloy consisting of from 0.005 to 1.0% carbon, 2.5 to 4.00% silicon, 10 to 13% chromium, 15 to 17% tungsten, 2.5 to 4.3% iron, 1.75 to 3.25% boron, 2 to 5% cobalt, and the remainder essentially all nickel.
3. A nickel-base alloy consisting of about 0.5% carbon, about 3.75% silicon, about 12% chromium, about 16% 3 4 tungsten, about 3.75% iron, about 3% boron, 2 to 2.5% References Cited cobalt, and the remainder essentially all nickel.
4. The method of increasing the Knoop hardness of UNITED STATES PATENTS nickelbase alloys consisting of from 0.005 to 1.00% car- 2,481,976 9/ 1949 Cape 75-171 bon, 2.5 to 4.75% silicon, 6 to 16% chromium, 7 to 17% 5 2 53 39 1 1959 Gonser 75 7 tungsten, 2 to 5% iron, 1 to 5% boron, and balance nickel, 2 875 043 N19 75 171 which consists in adding to said alloys cobalt in amounts of from 05 to RICHARD 0. DEAN, Primary Examiner
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US66614367A | 1967-09-07 | 1967-09-07 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US3475165A true US3475165A (en) | 1969-10-28 |
Family
ID=24672999
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US666143A Expired - Lifetime US3475165A (en) | 1967-09-07 | 1967-09-07 | Nickel-base alloys |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US3475165A (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3947269A (en) * | 1970-01-07 | 1976-03-30 | Trw Inc. | Boron-hardened tungsten facing alloy |
| US4101918A (en) * | 1975-11-29 | 1978-07-18 | Hoechst Aktiengesellschaft | Developing apparatus for light-sensitive materials comprising an evaporator for evaporating a developer medium from a solution |
| US4394347A (en) * | 1981-07-09 | 1983-07-19 | Avco Corporation | Brazing filler metal composition and process |
| EP1903121A1 (en) | 2006-09-21 | 2008-03-26 | Honeywell International, Inc. | Nickel-based alloys and articles made therefrom |
| US10563472B2 (en) | 2015-11-02 | 2020-02-18 | Wellbore Integrity Solutions Llc | Rotary milling tool |
Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2481976A (en) * | 1949-01-06 | 1949-09-13 | Coast Metals Inc | Alloy |
| US2868639A (en) * | 1955-10-06 | 1959-01-13 | Wall Colmonoy Corp | Metallic composition |
| US2875043A (en) * | 1956-04-04 | 1959-02-24 | Metallizing Engineering Co Inc | Spray-weld alloys of the boron-silicon-nickel type |
-
1967
- 1967-09-07 US US666143A patent/US3475165A/en not_active Expired - Lifetime
Patent Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2481976A (en) * | 1949-01-06 | 1949-09-13 | Coast Metals Inc | Alloy |
| US2868639A (en) * | 1955-10-06 | 1959-01-13 | Wall Colmonoy Corp | Metallic composition |
| US2875043A (en) * | 1956-04-04 | 1959-02-24 | Metallizing Engineering Co Inc | Spray-weld alloys of the boron-silicon-nickel type |
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3947269A (en) * | 1970-01-07 | 1976-03-30 | Trw Inc. | Boron-hardened tungsten facing alloy |
| US4101918A (en) * | 1975-11-29 | 1978-07-18 | Hoechst Aktiengesellschaft | Developing apparatus for light-sensitive materials comprising an evaporator for evaporating a developer medium from a solution |
| US4394347A (en) * | 1981-07-09 | 1983-07-19 | Avco Corporation | Brazing filler metal composition and process |
| EP1903121A1 (en) | 2006-09-21 | 2008-03-26 | Honeywell International, Inc. | Nickel-based alloys and articles made therefrom |
| US20100028197A1 (en) * | 2006-09-21 | 2010-02-04 | Mark Heazle | Nickel-based alloys and articles made therefrom |
| US7824606B2 (en) | 2006-09-21 | 2010-11-02 | Honeywell International Inc. | Nickel-based alloys and articles made therefrom |
| US10563472B2 (en) | 2015-11-02 | 2020-02-18 | Wellbore Integrity Solutions Llc | Rotary milling tool |
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