US2072910A - Alloy - Google Patents

Alloy Download PDF

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Publication number
US2072910A
US2072910A US21938A US2193835A US2072910A US 2072910 A US2072910 A US 2072910A US 21938 A US21938 A US 21938A US 2193835 A US2193835 A US 2193835A US 2072910 A US2072910 A US 2072910A
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Prior art keywords
beryllium
alloy
nickel
cobalt
chromium
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US21938A
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Enrique G Touceda
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Consolidated Car Heating Co Inc
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Consolidated Car Heating Co Inc
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Publication date
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Priority to US21938A priority Critical patent/US2072910A/en
Priority to US83078A priority patent/US2072911A/en
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    • 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
    • C22C19/058Alloys based on nickel or cobalt based on nickel with chromium without Mo and W

Definitions

  • My invention is a new alloy having novel characteristics which adapt it for practically all uses where extremely high resistance to corrosion is essential.
  • One of the objects of my invention is to provide an alloy in which the three principal ingredients are chromium, nickel and cobalt but which, by other additions, is endowed with many novel and desirable characteristics entirely lack- 10 ing in other alloys containing chromium, nickel and cobalt in the same proportions.
  • the essential ingredients of my alloy and their percentages of the total composition, by weight, are- Per cent Cr 10 to 35 Ni to 50 C0 20 to 50 Be 0.1 to 5 20 Nl+C 55 b0 80
  • the preferred ranges of my essential ingredients are-- 30 Per cent Cr 20. to 30 Ni- 30 to 40 C0-" to 40 Be from 0.1% to about 1.4% and from 1.8% to I find that alloys of this character containing beryllium in the neighborhood of about 1.6% are somewhat less desirable than those containing beryllium either below or above this percentage in that the ultimate strength of the composition with this quantity of beryllium is substantially reduced.
  • the nickel content plus the cobalt content should not be less than 55% nor more than 80%.
  • beryllium which has a very low specific gravity and is readily oxidizable is thereafter added. Due to the lightness of the beryllium it should be prealloyed with a heavier metal such as nickel or copper and the addition made by tying the nickel-beryllium or copper-beryllium to a rod and plunging it into the molten mass.
  • Another very desirable characteristic is the marked improvement in the'surface of the material as cast. substantial reduction in the melting point, a reducticn in the specific gravity, and a reduction in the shrinkage of cast specimens makes the composition particularly desirable for east dentures and the like.
  • the reduction in the melting point is of particular importance because the melting point of alloys of this character is unusually high.
  • the' melting points of some of the alloys containing chromium, nickel and cobalt within the above ranges, but without beryllium are as high as 2640 F. to 2750 F.
  • the addition of beryllium within the limits contemplated by this invention will reduce the final melting point of most of the alloys to between 2300 F. and 2500 F.
  • titanium is not an essential ingredient of my alloy, additions up to say 1% or slightly more, preferably in the form of manganese titanium, may be made. Such additions facilitate the soldering and welding of the composition.
  • metal such, for example as copper
  • the tilium has a hardness of C-l3 whereas melt No. a
  • the addition of beryllium does not in any way appreciably afiect this highly desirable characteristic of the base alloy yet it makes possible the casting of lactic acid-resisting articles tanium, when employed, is preferably added as a manganese-titanium alloy, and molybdenum and silicon are permissible additions within the limits stated, it will be apparent that in addition to' the principal alloying elements, chromium, nickel and cobalt and minor but effective quantities of beryllium, my alloy may contain other elements in quantities somewhat exceeding those ordinarily encountered as impurities but which do not materially affect the desirable characteristics of the composition as above set forth.
  • the phrase, the balance being substantially nickel and cobalt, used in the claims, is to be understood as including elements other than nickel and cobalt to
  • An alloy comprising chromium, nickel, cobalt and beryllium as essential alloying ingredients, the chromium content being from 10% to 35%, the beryllium content being from 0.1%. to 5%, and the balance being substantially nickel and cobalt each between 20% and 50% with a combined-nickel and cobalt content of from 55% to 80%; said alloy being characterized by a higher yield point, a substantially greater fluidity at casting temperatures, and a cleaner surface in the as cast condition than it would otherwise have without the beryllium.
  • An alloy comprising chromium, nickel, cobalt and beryllium as essential alloying ingredients, the chromium content being from 20% to 30%, the beryllium content being from 0.1% to 5%, and the balance being substantially nickel and cobalt; the nickel content being from 35% to 40% and the cobalt content being from 25% to 40%; said alloy being characterized by a higher yield point, a substantially greater fluidity at casting temperatures, and a cleaner surface in the as cast condition than it would otherwise have without the beryllium.
  • An alloy comprising chromium, nickel, cobalt and beryllium as essential alloying ingredients, the chromium content being from 10% to cleaner surface in the as cast condition than it would otherwise have without the beryllium,
  • An alloy comprising chromium, nickel, cobalt and beryllium as essential alloying ingredients, the chromium content being from 20% to 30%, the beryllium content being from more than 1.6% to and the balance being substantialiy nickel and cobalt: the nickel content being from 35% to 40% and the cobmt content being from to 40%; said alloy being characterized by a higher yield point, a substantially greater fluidity at casting temperatures, and a cleaner surface in the as cast condition than it would otherwise have without the beryllium.
  • An alloy comprising chromium, nickel, c0- balt and beryllium as essential alloying ingredients, the chromium content being from 25% to 32%, the beryllium content being from 0.1% to 5%, and the balance being substantially nickel and cobalt; the nickel content. being from to 40% and the cobalt content being from 25% to said alloy being characterized by a higher yield point, a substantially greater fluidity at casting temperatures, and a cleaner surface in the as cast condition than it would otherwise have without the beryllium.
  • An alloy comprising chromium, nickel, cobait and beryllium as essential alloying ingredients, the chromium content being from 25% to 32%, the beryllium content being from more than 1.6% to 5%, and the balance being substantially nickel and cobaltythe nickel content being from 30% to and the cobalt content being from 25% to 35%; said alloybeing characterized by a higher yield point, a substantially greater fluidity at casting temperatures, and cleaner surface in the as cast" condition than it would otherwise have without the beryllium.

Description

Patented Mar. 9, 1937 PATENT orrics ALLOY Enrique G. Touceda,
Albany, N. Y., auilnor to Consolidated Car-Heating Company, Inc., Albany, N. Y., a corporation of New York No Drawing. Applicatigigggay 17, 1935, Serial 6 Claims.
My invention is a new alloy having novel characteristics which adapt it for practically all uses where extremely high resistance to corrosion is essential.
One of the objects of my invention is to provide an alloy in which the three principal ingredients are chromium, nickel and cobalt but which, by other additions, is endowed with many novel and desirable characteristics entirely lack- 10 ing in other alloys containing chromium, nickel and cobalt in the same proportions.
The essential ingredients of my alloy and their percentages of the total composition, by weight, are- Per cent Cr 10 to 35 Ni to 50 C0 20 to 50 Be 0.1 to 5 20 Nl+C 55 b0 80 In addition to the foregoing, I find that additions of molybdenum in quantities under 8% and preferably in the neighborhood of about 6% are particularly desirable in developing certain characteristics; the alloy with molybdenum additions being specifically claimed in my divisional appli cation Serial No. 83,078.
The preferred ranges of my essential ingredients are-- 30 Per cent Cr 20. to 30 Ni- 30 to 40 C0-" to 40 Be from 0.1% to about 1.4% and from 1.8% to I find that alloys of this character containing beryllium in the neighborhood of about 1.6% are somewhat less desirable than those containing beryllium either below or above this percentage in that the ultimate strength of the composition with this quantity of beryllium is substantially reduced. In any case the nickel content plus the cobalt content should not be less than 55% nor more than 80%.
In making my alloy the nickel, cobalt and chromium, and molybdenum if molybdenum is to be incorporated, are first melted together, and the.
beryllium, which has a very low specific gravity and is readily oxidizable is thereafter added. Due to the lightness of the beryllium it should be prealloyed with a heavier metal such as nickel or copper and the addition made by tying the nickel-beryllium or copper-beryllium to a rod and plunging it into the molten mass. Once loy containing the following ingredients-- Per cent Cr 27.3 N 35.0 C0 28.7 Mo- 6.0 Si 1.0 Ti- 0.7
showed a tensile strength of 100,000 pounds per square inch with a yield point at 43,000 pounds per square inch. Substantially the same alloy with an addition of 4.0% of beryllium showed a tensile strength of 120,000 pounds per square inch with a yield point at 87,000 pounds per square inch. In other words, the yield point was raised more than by the beryllium addition.
Again, 0.8% of beryllium addedto an alloy containing nickel 35.5%, cobalt 29.5%, chromium 28.2% and molybdenum 6% raised the yield point from 45,000 pounds to 53,000 pounds persquare inch.
Another very desirable characteristic is the marked improvement in the'surface of the material as cast. substantial reduction in the melting point, a reducticn in the specific gravity, and a reduction in the shrinkage of cast specimens makes the composition particularly desirable for east dentures and the like.
The reduction in the melting point is of particular importance because the melting point of alloys of this character is unusually high. For example, the' melting points of some of the alloys containing chromium, nickel and cobalt within the above ranges, but without beryllium, are as high as 2640 F. to 2750 F. The addition of beryllium Within the limits contemplated by this invention will reduce the final melting point of most of the alloys to between 2300 F. and 2500 F.
Another desirable characteristic developed by the beryllium addition is a decided reduction in This feature combined with a the speciflc gravity of the material. 'Ihis is a very important factor where the material is used for prosthetic articles.
The following series of melts using, for comparative purposes, substantially the same percentages of chromium, nickel, cobalt and molybdenum, show the effect of adding various percentages of beryllium either in the form of copperberyllium or nickel-beryl1ium from this typeof alloy which would otherwise be impossible.
While titanium is not an essential ingredient of my alloy, additions up to say 1% or slightly more, preferably in the form of manganese titanium, may be made. Such additions facilitate the soldering and welding of the composition.
Since the beryllium is incorporated in the composition in the form of an alloy with a heavier Melt No Base 33 a4 40 44 40 40 47 40 Co 28.7 29.0 20.0 21.7 28.2 28.0 20.0 20.2 20.0 15 01'... 27.3 28.5 28.0 20.4 27.0 27.0 27.2 28.0 27.8 Ni 35.0 05.0 04.0 01.9 33.8 34.8 36.3 30.0 05.3 M0. 0.0 0.0 a0 0.0 0.0 0.0 0.0 0.0 0.0 Be 0.8 2.4 4.0 1.0 0.4 0.4 1.0 0.8 si 1.0 1.0 1.0 1.0 Ti 0.7 0.7 0.7 0.7 Mn 1. s 1. 3 1.3 1.3 Rockwell C-scale Ol3 C-22 C-60 O-42 O-{i5 C24 C-22 C-34 O26 20 s gr 8.20 8.15 8.07 7.44 7.84 a. 14 01a '7. 01 7.08 Tensile strength 100,000 110, 000 100, 000 120,000 100, 000 80, 000 07, 000 100. 000 Yield point 48,000 .000 ,000 87,000 50,000 00,000 ,000 ,000 Melting points F 2, 450 2, 300 2, 027 2,400 2, 040
25 From the foregoingtable it will be observed, metal such, for example as copper, and the tilium has a hardness of C-l3 whereas melt No. a
43 with an addition of 4% of beryllium shows an increase in hardness to (J-42, while heats Nos. 45 and 46 show that the additionof only .4% of beryllium about doubles the hardness reading.
In short, it may be said that the addition of beryllium to the chromium-nickel cobalt alloys herein described substantially changes the characteristic of the alloy in the following respects- Reduces the melting point;
. Increases the fluidity;
. Reduces the gravity;
. Improves the surface as cast;
. Increases the resistance to high temperature oxidation;
. Increases the yield point;
. Increases the hardness;
. Reduces the elongation;
. Reduces the tendency of the material to react with the casting crucible; and
10. Reduces the coeflicient of expansion.
All additions of beryllium ,within the limits disclosed above produce a substantial increase in the fluidity of the molten composition, and this characteristic is particularly marked with additions in excess of 2%. For example, when 2.4% beryllium was added to an alloy comprising cobalt 29%, chromium 28%, nickel 34% and molybdenum 6% the fluidity was increased to a point where certain thin sections could-be cast which it was impossible to run with the base alloy.
Where a particularly fine surface is desired on articles cast from my alloy, as in the case of dental plates, etc., excellent -results are obtained by melting the composition in an atmosphere of hydrogen and, moreover, the toughness of the casting is very substantially increased.
My base alloy set forth in the above table, and which is within the disclosure of my copending application Serial No. 58,163, is not only extremely resistant to corrosive attack by lactic acid but may be said to be practically inert thereto. The addition of beryllium does not in any way appreciably afiect this highly desirable characteristic of the base alloy yet it makes possible the casting of lactic acid-resisting articles tanium, when employed, is preferably added as a manganese-titanium alloy, and molybdenum and silicon are permissible additions within the limits stated, it will be apparent that in addition to' the principal alloying elements, chromium, nickel and cobalt and minor but effective quantities of beryllium, my alloy may contain other elements in quantities somewhat exceeding those ordinarily encountered as impurities but which do not materially affect the desirable characteristics of the composition as above set forth. Hence, the phrase, the balance being substantially nickel and cobalt, used in the claims, is to be understood as including elements other than nickel and cobalt to the extent aforesaid.
What I claim is:
1. An alloy comprising chromium, nickel, cobalt and beryllium as essential alloying ingredients, the chromium content being from 10% to 35%, the beryllium content being from 0.1%. to 5%, and the balance being substantially nickel and cobalt each between 20% and 50% with a combined-nickel and cobalt content of from 55% to 80%; said alloy being characterized by a higher yield point, a substantially greater fluidity at casting temperatures, and a cleaner surface in the as cast condition than it would otherwise have without the beryllium.
2. An alloy comprising chromium, nickel, cobalt and beryllium as essential alloying ingredients, the chromium content being from 20% to 30%, the beryllium content being from 0.1% to 5%, and the balance being substantially nickel and cobalt; the nickel content being from 35% to 40% and the cobalt content being from 25% to 40%; said alloy being characterized by a higher yield point, a substantially greater fluidity at casting temperatures, and a cleaner surface in the as cast condition than it would otherwise have without the beryllium.
3. An alloy comprising chromium, nickel, cobalt and beryllium as essential alloying ingredients, the chromium content being from 10% to cleaner surface in the as cast condition than it would otherwise have without the beryllium,
4. An alloy comprising chromium, nickel, cobalt and beryllium as essential alloying ingredients, the chromium content being from 20% to 30%, the beryllium content being from more than 1.6% to and the balance being substantialiy nickel and cobalt: the nickel content being from 35% to 40% and the cobmt content being from to 40%; said alloy being characterized by a higher yield point, a substantially greater fluidity at casting temperatures, and a cleaner surface in the as cast condition than it would otherwise have without the beryllium.
5. An alloy comprising chromium, nickel, c0- balt and beryllium as essential alloying ingredients, the chromium content being from 25% to 32%, the beryllium content being from 0.1% to 5%, and the balance being substantially nickel and cobalt; the nickel content. being from to 40% and the cobalt content being from 25% to said alloy being characterized by a higher yield point, a substantially greater fluidity at casting temperatures, and a cleaner surface in the as cast condition than it would otherwise have without the beryllium.
6. An alloy comprising chromium, nickel, cobait and beryllium as essential alloying ingredients, the chromium content being from 25% to 32%, the beryllium content being from more than 1.6% to 5%, and the balance being substantially nickel and cobaltythe nickel content being from 30% to and the cobalt content being from 25% to 35%; said alloybeing characterized by a higher yield point, a substantially greater fluidity at casting temperatures, and cleaner surface in the as cast" condition than it would otherwise have without the beryllium.
ENBIQUE G. TOUCEDA.
US21938A 1935-05-17 1935-05-17 Alloy Expired - Lifetime US2072910A (en)

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Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2524661A (en) * 1947-05-03 1950-10-03 Elgin Nat Watch Co Alloy having high elastic strengths
US2973291A (en) * 1957-06-07 1961-02-28 Straumann Inst Ag Manufacture of point bearings in instruments
US3177074A (en) * 1962-04-23 1965-04-06 Duriron Co Cobalt base alloys

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2524661A (en) * 1947-05-03 1950-10-03 Elgin Nat Watch Co Alloy having high elastic strengths
US2973291A (en) * 1957-06-07 1961-02-28 Straumann Inst Ag Manufacture of point bearings in instruments
US3177074A (en) * 1962-04-23 1965-04-06 Duriron Co Cobalt base alloys

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