[go: up one dir, main page]

US3475165A - Nickel-base alloys - Google Patents

Nickel-base alloys Download PDF

Info

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
Application number
US666143A
Inventor
Arthur T Cape
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Coast Metals Inc
Original Assignee
Coast Metals Inc
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Coast Metals Inc filed Critical Coast Metals Inc
Application granted granted Critical
Publication of US3475165A publication Critical patent/US3475165A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C19/00Alloys based on nickel or cobalt
    • C22C19/03Alloys based on nickel or cobalt based on nickel
    • C22C19/05Alloys based on nickel or cobalt based on nickel with chromium
    • C22C19/051Alloys based on nickel or cobalt based on nickel with chromium and Mo or W
    • C22C19/056Alloys 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.

Landscapes

  • 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
US666143A 1967-09-07 1967-09-07 Nickel-base alloys Expired - Lifetime US3475165A (en)

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)

* Cited by examiner, † Cited by third party
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)

* Cited by examiner, † Cited by third party
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

Patent Citations (3)

* Cited by examiner, † Cited by third party
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)

* Cited by examiner, † Cited by third party
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

Similar Documents

Publication Publication Date Title
US2430419A (en) Welding rod
US2920954A (en) Stainless steel alloy of high hardness
US3475165A (en) Nickel-base alloys
US2756489A (en) Metal alloy
US2328580A (en) Ruthenium alloy pen point
US3539307A (en) Welding rod
US2306667A (en) Alloy
US2109285A (en) Alloy
US3012881A (en) Iron-base alloys
US1449338A (en) Alloy and process of making the same
US2072911A (en) Alloy
US3925070A (en) Brazing alloy
US2757084A (en) Alloy compositions
US2944891A (en) Brazing alloys
US1568224A (en) Bearing metal
SE8007443L (en) AN EROSION-resistant alloy
US2070451A (en) Hard metal alloy
US3563731A (en) Cobalt-base alloys containing chromium,carbon,tungsten and nickel
US2803538A (en) Self-hardening alloys
US3125446A (en) Zirconium base alloy
US1057828A (en) Metal alloy.
US2072910A (en) Alloy
US4249942A (en) Copper base alloy containing manganese and cobalt
JPS5773146A (en) Wear resistant aluminum bronze alloy
US2212017A (en) Cuprous alloy