GB1592123A – Nickel-base alloys
– Google Patents
GB1592123A – Nickel-base alloys
– Google Patents
Nickel-base alloys
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Publication number
GB1592123A
GB1592123A
GB12962/78A
GB1296278A
GB1592123A
GB 1592123 A
GB1592123 A
GB 1592123A
GB 12962/78 A
GB12962/78 A
GB 12962/78A
GB 1296278 A
GB1296278 A
GB 1296278A
GB 1592123 A
GB1592123 A
GB 1592123A
Authority
GB
United Kingdom
Prior art keywords
alloy
nickel
chromium
weight
powder
Prior art date
1977-04-04
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
Application number
GB12962/78A
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.)
Eutectic Corp
Original Assignee
Eutectic Corp
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.)
1977-04-04
Filing date
1978-04-03
Publication date
1981-07-01
1978-04-03
Application filed by Eutectic Corp
filed
Critical
Eutectic Corp
1981-07-01
Publication of GB1592123A
publication
Critical
patent/GB1592123A/en
Status
Expired
legal-status
Critical
Current
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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
C22C19/058—Alloys based on nickel or cobalt based on nickel with chromium without Mo and W
B—PERFORMING OPERATIONS; TRANSPORTING
B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
B23K35/00—Rods, electrodes, materials, or media, for use in soldering, welding, or cutting
B23K35/22—Rods, electrodes, materials, or media, for use in soldering, welding, or cutting characterised by the composition or nature of the material
B23K35/24—Selection of soldering or welding materials proper
B23K35/30—Selection of soldering or welding materials proper with the principal constituent melting at less than 1550 degrees C
B23K35/3033—Ni as the principal constituent
B23K35/304—Ni as the principal constituent with Cr as the next major constituent
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
C22C19/053—Alloys based on nickel or cobalt based on nickel with chromium and Mo or W with the maximum Cr content being at least 30% but less than 40%
Description
PATENT SPECIFICATION ( 11) 1 592 123
n ( 21) Application No 12962/78 ( 22) Filed 3 Apr 1978 ( 19) ( 31) Conventions Application No 784376 ( 32) Filed 4 Apr 1977 in ( 33) United States of America (US)
Z,, ( 44) Complete Specification Published 1 Jul 1981
U ( 51) INT CL 3 C 22 C 19/05 _ B 23 K 35/30 ( 52) Index at Acceptance C 7 A 711 A 23 Y A 247 A 249 A 250 A 253 A 25 X A 25 Y A 299 A 307 A 309 A 30 Y A 311 A 313 A 316 A 319 A 31 X A 32 D A 323 A 326 A 329 A 339 A 349 A 350 A 35 X A 35 Y A 389 A 409 A 414 A 416 A 418 A 41 Y A 422 A 425 A 428 A 42 X A 432 A 435 A 437 A 439 A 43 X A 459 A 509 A 529 A 53 X A 53 Y A 557 A 559 A 55 Y A 562 A 565 A 568 A 56 X A 571 A 574 A 577 A 579 A 57 Y A 599 A 609 A 615 A 617 A 61 X A 61 Y A 671 A 673 A 675 A 677 A 679 A 67 X A 681 A 683 A 685 A 687 A 689 A 68 X A 693 A 695 A 697 A 699 A 69 X A 70 X B 3 R 32 G ( 72) Inventors: OTTO KNOTEK ERICH LUGSCHEIDER ( 54) NICKEL-BASE ALLOYS ( 71) We, EUTECTIC CORPORATION, a corporation organised and existing under the laws of the State of New York, United States of America, of 40-40 172nd Street, Flushing, New York 11358, United States of America, do hereby declare the invention for which we pray that a patent may be granted to us, and the method by which it is to be performed, to be particularly described in and by the following statement: 5
This invention relates to a wear resistant and corrosion resistant nickelbase alloy and to articles of manufacture made of said alloy, such as welding consumables, P/M (powder metallurgy) preforms for producing hard surface elements on metal substrates, e g valve seats, and wear and corrosion resistant castings, and the like.
Wear and corrosion resistant alloys are known for hard facing metal substrates, for valve 10 seats, and for the production of wear resistant castings, among other uses.
A known wear resistant composition is a cobalt-base alloy containing by weight 0 9 1.6 % C, 5 % Mn max, 8 1 5 % Si, 26 29 % Cr, 4 6 % W, 2 % max Fe and the balance cobalt This alloy has been recommended for applications involving room and high temperature abrasive action, galling in metal-to-metal wear, and a moderate degree of 15 impact, thermal shock or stress loading The foregoing alloy generally exhibits a hardness ranging from about 40 to 49 Rockwell C.
Another known composition is a nickel-base alloy containing by weight 0 25 0 75 % C, 3 to 5 % Si, 10 to 15 % Cr, 3 to 5 % Fe, 1 5 to 4 % B, 0 2 % Co max and the balance at least 77 % nickel This alloy is particularly adapted for producing centrifugally cast shapes, 20 exhibits a hardness of about 42 to 52 Rockwell C and has a melting point of about 1065 C ( 1950 F) The alloy is preferably cobalt-free (e g not exceeding 0 2 % Co by weight) where the danger of radioactive contamination exists, such as in equipment employed in nuclear power applications This alloy is suggested for liners, thrust shoes, bushings and other valve components for nuclear applications 25 Another known wear resistant cobalt-base alloy is a composition containing by weight 1 8 2 2 % C, 0 5 1 % Mn, 0 8 1 5 % Si, 30 33 % Cr, 3 % max Ni, 11 13 % W, 2 % max Fe and the balance cobalt The hardness of this alloy may range from about 54 to 58 Rockwell C.
A problem which arises in the production of hard face coatings and/or cast shapes using 2 1 592 123 2 complex wear and corrosion resistant alloys, such as high chromium, high carbon nickel-base alloys, is the tendency of such alloys in the molten state to segregate on freezing due to the relatively large liquidus-solidus temperature range over which solidification occurs This is particularly important in the production of castings for wear resistant applications in which the surface hardness of a bushing, a sleeve, etc, is important 5 We have now found a nickel-base alloy in which the solidus-liquidus temperature range of the alloy system is narrow and thereby minimizes the amount of segregation of the alloy during freezing from the liquid to the solid state This alloy is a high chromium-containing, high carbon-containing nickel-base alloy characterized by resistance to wear and corrosion and by high hardness 10 The alloy can be used to make welding consumables whose deposit is characterized by resistance to wear and corrosion, and it can also be used to make other wear and corrosion resistant articles and coatings The alloy can be used in powder form, e g in the manufacture of preforms.
Thus in one embodiment the invention provides a nickel-base wear and corrosion 15 resistant alloy containing by weight 20 % to 35 % Cr, 1 % to 8 % Si, 1 7 % to 3 5 % C, 0 to % W and at least 40 % nickel as the balance (excluding impurities), the carbon being present in said alloy as carbides of the formula M 7 C 3 (where M is chromium or a mixture of chromium and minor amounts of one or more of the other metals present), the amount of chromium in said M 7 C 3 compound being at least 65 % but less than 100 % of the total 20 chromium in said alloy, and the melting point of said alloy being less than 1350 MC.
The invention also includes mixtures of the constituent elements of the alloys of the invention, in powder form.
All percentages given herein are by weight on the basis of the total composition.
Alloys produced from the foregoing composition are characterized by high hardness 25 ranging from about 35 to 55 Rockwell C The alloy is rendered particularly acid resistant by the presence of copper and/or molybdenum, as described below.
By having a major amount of the chromium in the composition tied up as M 7 C 3, an alloy composition is provided having a relatively narrow melting range which aids in minimizing segregation of the alloy during solidification, either as a casting, as a weld deposit, or as a 30 coating on a metal substrate.
While the M 7 C 3 compound comprises essentially chromium carbide, that is, about 65 % to less than 100 % of the total chromium present, small amounts of other metals may be present in the compound to provide variations thereof, such as (Cr W)7 C 3, (Cr Ni)7 C 3 or (Cr W Ni)7 C 3 Thus, reference to M 7 C 3 in the disclosure is meant to include the foregoing 35 variations of the carbide in which chromium is an essential ingredient, the amount of chromium comprising at least 65 % of the total chromium content of the alloy composition and ranging up to less than about 100 %, preferably between 75 % and 100 % of the total chromium content.
As will be appreciated, according to the law of mass action, some of the chromium will 40 enter the nickel matrix and form a solid solution therewith and confer resistance to corrosion to the final alloy, the remainder of the chromium (at least 65 %), forming the compound M 7 C 3.
The foregoing alloy is particularly useful for forming welding consumables, alloy spraypowder for producing hard facing coatings, P/M preforms for use in the production of wear 45 resistant valve seats and wear and abrasion resistant castings, such as sleeves, bushings, wear rings, grooving rolls and the like.
As illustrative of welding consumables, reference is made to Figures 1 to 3 of the accompanying drawings, Figure 1 being a tubular welding rod of the type disclosed in U S.
Patent No 3,033,977 The weld rod comprises a metal tube of nickel of relatively small 50 diameter wth a metallic powder therein of a composition taken with the nickel tube to produce by reaction a weld deposit consisting essentially by weight of 20 % to 35 % Cr, 1 % to 8 % Si, 1 7 % to 3 5 % C, 0 to 15 % W and the balance essentially at least 40 % and preferably at least 50 % nickel As indicated hereinabove, the amount of carbon within the foregoing range is stoichiometrically related to the chromium content to provide carbides 55 based on the formula M 7 C 3 in which M comprises essentially chromium.
As will be appreciated, various fluxes may be incorporated with the metallic powder in the nickel tube The ultimate rod may be drawn through a finishing die to compact it and make it uniform in content The finished tube 10 is shown in Figure 1 with a powder mix 11 of chromium, carbon and tungsten to provide with the nickel tube an ultimate composition 60 containing 30 % Cr, 2 4 % C, 5 % W and the balance essentially nickel Some nickel powder may be present with the powder mix as an aid to compaction during tube drawing, the amount of nickel being correlated with the nickel in the tube to provide the desired total nickel in the weld deposit As will be noted, the tube is pinched at opposite ends 12, 13.
Another weld consumable, comprising a hard facing flux-coated electrode 14, is shown in 65 1 592 123 1 592 123 Figures 2 and 3 Such electrodes are disclosed in U S Patent No 3,211,582, also incorporated herein by reference Referring to Figure 2, a weld rod 14 is depicted comprising a core 15 of the alloy coated with a flux 16, the flux coating incorporating active fluxing agents well known in the art (note U S Patent No 3,211,582) The flux coating 16 is shown in Figure 3 surrounding core rod 15 5 The alloy of the invention is also useful as a flame-spray powder for producing coatings on metal substrates The powder is preferably formed by atomizing a molten bath of the alloy to produce flame-spray powder in the desirable size range Flamespraying torches are disclosed in U S Patent Nos 3,226,028 and 3,228,610 In employing the alloy powder of the invention, the metal substrate (e g steel) is first cleaned in the usual manner and the 10 powder sprayed thereon and thereafter fused in place by directing the flame of a torch onto the deposited coating.
In producing a valve seat on a valve part, a P/M preform 17 may be employed of the type shown in Figure 4 A powder of the alloy composition may be employed in producing the compact It may be desirable to use elemental powders in producing the preform since 15 nickel per se is ductile and provides a compact of good green strength Or, if desired, an alloy powder deficient in nickel may be employed and nickel powder sufficient to complete the desired composition mixed with the alloy powder to provide the necessary green strength in producing the P/M preform of Figure 4 The preform is placed on the seat of the valve and torch-fused in place using the usual fluxes employed for that purpose to assure a 20 metallurgical bond to the valve surface.
Figure 5 shows a machined cast bushing or sleeve 18 which may be produced from the alloy of the invention The foregoing casting is preferably produced by centrifugal casting.
The casting is produced by pouring molten metal into a hollow carbon or steel cylindrical mold which spins about its own axis Rapid chilling combined with the centrifugal force 25 produces a fine grained structure and also produces metallic carbides which are fine and uniform Such a product provides markedly superior wear and corrosion resistance.
The composition can be ipade particularly acid resistant by adding thereto at least one of the metals selected from the group consisting of up to 5 % Cu and up to 5 % Mo, the amount of Mo added replacing an equivalent weight of tungsten, with at least 50 % nickel as the 30 balance Preferably, both metals may be present in amounts ranging from 1 % to 4 % Cu and 1 % to 4 % Mo.
A preferred alloy is one containing about 30 % Cr, about 2 to 5 % Si, about 2 4 % C, about % W and the balance essentially nickel (e g about 58 % to 61 %) As stated herein, the stoichiometric relationship in producing the M 7 C 3 compound is important, especially at or 35 near the eutectic melting point of the alloy, in that a narrow liquidussolidus temperature range is obtained, such as 1220 ‘C to 1300 C at 2 % Si and 2 % C and 12300 C to 1280 ‘C at 5 % Si and 2 % C The narrow liquidus-solidus temperature range is desirable in that it minimizes segregation in a casting and in hard facing coatings produced from the alloy The melting point of the alloy is less than 1350 ‘C and generally does not exceed 1300 ‘C 40 In nuclear applications, it is important that the alloy be iron-free, cobalt-free and boron-free Thus, the iron and cobalt contents each should not exceed about 0 2 % by weight and boron maintained below 0 1 %.
Examples of alloy compositions of the invention are given as follows:
Alloy No % Cr % C % Si % W % Cu % Mo % Ni 1 20 0 1 7 2 0 __ _ 76 3 2 25 0 2 0 1 0 4 0 68 0 3 25 0 2 2 2 5 2 2 66 3 4 30 0 2 4 2 0 5 0 2 58 6 300 30 50 7 62 0 6 35 0 3 0 2 0 3 3 53 5 7 30 0 2 0 2 0 8 0 58 0 8 280 261 1 65 9 28.0 26 1 5 1 592 123 About 10 parts by weight of chromium combines with about 1 part by weight of carbon to form Cr 7 C 3 Thus, in Alloy No 1, about 85 % of the total chromium is reactable with the carbon, the remaining chromium going into solid solution with the nickel In Alloy No 2, about 80 % of the chromium is reactable with the carbon, the remainder entering into solid solution with the nickel In Alloy No 7, about 66 % of the chromium is combinable with the 5 carbon, the remainder entering into solid solution with the nickel In Alloy No 8, about 93 % of the chromium is combinable with the carbon However, as stated hereinbefore, variations of M 7 C 3 may form with chromium as the essential ingredient together with small amounts of tungsten and/or molybdenum, when present.
Claims (1)
WHAT WE CLAIM IS: 10
A nickel-base wear and corrosion resistant alloy containing by weight 20 % to 35 % Cr, 1 % to 8 % Si, 1 7 % to 3 5 % C, 0 to 15 % W and at least 40 % nickel as the balance (excluding impurities), the carbon being present in said alloy as carbides of the formula M 7 C 3 (where M is chromium or a mixture of chromium and minor amounts of one or more of the other metals present), the amount of chromium in said M 7 C 3 compound being at least 15 % but less than 100 % of the total chromium in said alloy, and the melting point of said alloy being less than 1350 ‘C.
2 An alloy as claimed in claim 1 which additionally contains up to 5 % Cu and/or up to % Mo, said Mo replacing a corresponding weight of W and the balance being at least 50 % by weight nickel 20 3 An alloy as claimed in claim 2 which contains 1 % to 4 % Cu and 1 % to 4 % Mo.
4 An alloy as claimed in any one of the preceding claims which contains not more than 0.2 % by weight (each) of iron and cobalt and less than 0 1 % by weight of boron.
An alloy having a composition substantially as described herein for any one of Alloys Nos 1-8 25 6 A welding consumable comprising an alloy as claimed in any one of the preceding claims.
7 A weld rod comprising a nickel tube with a metallic powder contained within said tube, such that the weld deposit produced thereform is an alloy as claimed in any one of claims 1 to 5 30 8 A casting found of an alloy as claimed in any one of claims 1 to 5.
9 A powder metallurgy preform formed of ingredients for producing an alloy as claimed in any one of claims 1 to 5.
A mixture in powder form of the constituent elements of an alloy as claimed in any one of claims 1 to 5 35 11 An alloy as claimed in any one of claims 1 to 5, in powdered form.
For the Applicants, FRANK B DEHN & CO.
Printed for Her Majesty’s Stationery Office, by Croydon Printing Company Limited, Croydon, Surrey, 1981.
Published by The Patent Office, 25 Southampton Buildings, London, WC 2 A l AY, from which copies may be obtained.
GB12962/78A
1977-04-04
1978-04-03
Nickel-base alloys
Expired
GB1592123A
(en)
Applications Claiming Priority (1)
Application Number
Priority Date
Filing Date
Title
US05/784,376
US4118254A
(en)
1977-04-04
1977-04-04
Wear and corrosion resistant nickel-base alloy
Publications (1)
Publication Number
Publication Date
GB1592123A
true
GB1592123A
(en)
1981-07-01
Family
ID=25132272
Family Applications (1)
Application Number
Title
Priority Date
Filing Date
GB12962/78A
Expired
GB1592123A
(en)
1977-04-04
1978-04-03
Nickel-base alloys
Country Status (5)
Country
Link
US
(1)
US4118254A
(en)
JP
(2)
JPS53125208A
(en)
CA
(1)
CA1096660A
(en)
DE
(1)
DE2814350A1
(en)
GB
(1)
GB1592123A
(en)
Cited By (1)
* Cited by examiner, † Cited by third party
Publication number
Priority date
Publication date
Assignee
Title
GB2204059B
(en)
*
1987-05-01
1991-09-11
Haynes Int Inc
Ductile nickel-silicon alloy
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* Cited by examiner, † Cited by third party
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Priority date
Publication date
Assignee
Title
US4331741A
(en)
*
1979-05-21
1982-05-25
The International Nickel Co., Inc.
Nickel-base hard facing alloy
EP0057242B1
(en)
*
1981-02-04
1987-03-25
EATON AUTOMOTIVE S.p.A.
High temperature alloy
US5141571A
(en)
*
1991-05-07
1992-08-25
Wall Colmonoy Corporation
Hard surfacing alloy with precipitated bi-metallic tungsten chromium metal carbides and process
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*
1992-06-08
1996-08-13
Nippon Tungsten Co., Ltd.
Titanium-base hard sintered alloy
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1997-01-29
1999-08-10
Deloro Stellite Company, Inc
Hardfacing method and nickel based hardfacing alloy
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(en)
*
1999-05-27
2003-12-22
兼次 安彦
Cr based alloy with excellent strength-ductility balance at high temperature
US20040124231A1
(en)
*
1999-06-29
2004-07-01
Hasz Wayne Charles
Method for coating a substrate
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*
1999-06-29
2002-09-17
General Electric Company
Turbine engine component having wear coating and method for coating a turbine engine component
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*
2002-02-14
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Hoeganaes Ab
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*
2013-06-28
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江苏双勤民生冶化设备制造有限公司
Centrifugal casting method for Inconel 600 alloy pipe
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(en)
*
2013-09-29
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西安瑞福莱钨钼有限公司
Preparing method of nickel-silicon alloy cast ingot
US9528171B2
(en)
*
2014-09-16
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Caterpillar Inc.
Alloy for seal ring, seal ring, and method of making seal ring for seal assembly of machine
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2021-08-19
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江苏新航合金科技有限公司
Nickel-based high-temperature alloy welding material for aviation
CN114473288B
(en)
*
2022-01-11
2023-10-20
河北联之捷焊业科技有限公司
Welding wire for low-dilution nickel-based surfacing layer and method for preparing CMT surfacing layer
Family Cites Families (3)
* Cited by examiner, † Cited by third party
Publication number
Priority date
Publication date
Assignee
Title
US1528478A
(en)
*
1924-12-16
1925-03-03
Hadfield Robert Abbott
Alloy
US2219462A
(en)
*
1938-03-11
1940-10-29
Haynes Stellite Co
Welding rod
US2888740A
(en)
*
1952-07-15
1959-06-02
Eaton Mfg Co
Composite ductile wire
1977
1977-04-04
US
US05/784,376
patent/US4118254A/en
not_active
Expired – Lifetime
1978
1978-04-03
DE
DE19782814350
patent/DE2814350A1/en
active
Granted
1978-04-03
GB
GB12962/78A
patent/GB1592123A/en
not_active
Expired
1978-04-03
CA
CA300,293A
patent/CA1096660A/en
not_active
Expired
1978-04-04
JP
JP3886478A
patent/JPS53125208A/en
active
Granted
1990
1990-02-20
JP
JP2037527A
patent/JPH02277740A/en
active
Granted
Cited By (1)
* Cited by examiner, † Cited by third party
Publication number
Priority date
Publication date
Assignee
Title
GB2204059B
(en)
*
1987-05-01
1991-09-11
Haynes Int Inc
Ductile nickel-silicon alloy
Also Published As
Publication number
Publication date
JPH02277740A
(en)
1990-11-14
JPS647145B2
(en)
1989-02-07
DE2814350C2
(en)
1987-11-12
JPS53125208A
(en)
1978-11-01
US4118254A
(en)
1978-10-03
DE2814350A1
(en)
1978-10-12
JPH0351776B2
(en)
1991-08-07
CA1096660A
(en)
1981-03-03
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Legal Events
Date
Code
Title
Description
1981-09-16
PS
Patent sealed [section 19, patents act 1949]
1992-12-02
PCNP
Patent ceased through non-payment of renewal fee
