US2072911A - Alloy - Google Patents

Alloy Download PDF

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Publication number
US2072911A
US2072911A US83078A US8307836A US2072911A US 2072911 A US2072911 A US 2072911A US 83078 A US83078 A US 83078A US 8307836 A US8307836 A US 8307836A US 2072911 A US2072911 A US 2072911A
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Prior art keywords
beryllium
alloy
nickel
cobalt
content
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US83078A
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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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Priority claimed from US21938A external-priority patent/US2072910A/en
Application filed by Consolidated Car Heating Co Inc filed Critical Consolidated Car Heating Co Inc
Priority to US83078A priority Critical 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
    • C22C19/051Alloys based on nickel or cobalt based on nickel with chromium and Mo or W
    • C22C19/053Alloys 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%

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 10 which, by other additions, is endowed with many novel and desirable characteristics entirely lacking in other alloys containing chromium, nickel and cobalt in the same proportions.
  • 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.
  • nickel content plus the cobalt content should not be less than 55% nor more than 30%.
  • the nickel, cobalt and chromium and molybdenum 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 copperberyllium to a rod and plunging it into the molten mass. Once the copper or nickel-beryllium is wet it alloys readily. While the beryllium addition alone very greatly increases the fluidity of the material at casting temperatures a small amount or silicon may be added if desired, but this addition should not exceed 1%. Just before the molten mass is poured I prefer to add about 0.05% of calcium as a de-oxidizer.
  • 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 5 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 50 most of the alloys to between 2300 F. and 2500 F.
  • Another desirable characteristic developed by the beryllium addition is a decided reduction in the specific gravity of the material. This is a a5 very important factor where the material is used for prosthetic articles.
  • 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.
  • the beryllium is incorporated in the From the foregoing table it will be observed, among other things, that small additions of 25 beryllium efiect a remarkable increase in the hardness of the material as measured on the Rockwell C-scale.
  • the base alloy without beryllium has a hardness of C13v whereas melt No. 43 with an addition of 4% of beryllium shows an increase in hardness to (3-42, while heats Nos. 45 and 46 show that the addition of only .4% of beryllium about doubles the hardness reading.
  • the addition of beryllium does not in any way appreciably affect this highly desirable characteristic of the base alloy yet it makes possible the casting of lactic acid-resisting articles composition in the form of an alloy with a heavier metal such, for example, as copper, and
  • the titanium when employed, is preferably added as a manganese-titanium alloy, and silicon is a permissible addition within the limits stated, it will be apparent that in addition to the principal alloying elements, chromium, nickel, cobalt and molybdenum and minor but efiective quantitles of beryllium, my alloy may contain other elements in quantities somewhat exceeding those ordinarily encountered as impurities but which do not materially aifect 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.
  • An alloy comprising chromium, nickel, cobalt, molybdenum and beryllium as essential 9.1-. loying ingredients, the chromium content being from 10% to 35%, the beryllium content being from 0.1% to the molybdenum content being from 0.1% to 8%, 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, molybdenum and beryllium as essential alloying ingredients, the chromium content being from 20% to 30%, the beryllium content being from 0.1% to 5%, the molybdenum content being from 0.1% to 8%, 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, molybdenum and beryllium as-essential alloying ingredients, the chromium content being from to 35%, the beryllium content being from more than 1.6% to 5%, the molybdenum content being from 0.1% to 8%, and the balance beingsubstantially 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, molybdenum and beryllium as essential alloying ingredients, the chromium content being from 20% to 30%, the beryllium content being from more than 1.6% to 5%, the molybdenum content being from 0.1% to 8%, and the balance being substantially nickel and cobalt; the nickel content being from 35% to 40% and the cobalt 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, cobait, molybdenum and beryllium as essential alloying ingredients, the chromium content being from 25% to 32%, the beryllium content being from 0.1% to 5%, the molybdenum content being from 0.1% to 8%, 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, cobalt, molybdenum 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%, the molybdenum content being from 0.1% to 8%, and the balance being substantially nickel and cobalt; the nickel content being from 30% to and the cobalt content being from 25% to 35%; said alloy being 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 UNITED STATES PATENT OFFICE ALLOY No Drawing. Original application May 17, 1935,
Serial No. 21,938. Divided and this application June 2, 1936, Serial No. 83,078
6 Claims.
This application is a division of my copending application Serial No. 21,938 filed May 17, 1935.
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 10 which, by other additions, is endowed with many novel and desirable characteristics entirely lacking 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
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 30%.
In making my alloy the nickel, cobalt and chromium and molybdenum 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 copperberyllium to a rod and plunging it into the molten mass. Once the copper or nickel-beryllium is wet it alloys readily. While the beryllium addition alone very greatly increases the fluidity of the material at casting temperatures a small amount or silicon may be added if desired, but this addition should not exceed 1%. Just before the molten mass is poured I prefer to add about 0.05% of calcium as a de-oxidizer.
One of the outstanding characteristics which 5 distinguishes my alloy from a similar chromiumnickel-cobalt alloy without beryllium is its comparatively high yield point. For example, an alloy containing the following ingredients 10 Per cent Cr 27.3 Ni 35.0 C0 J 28.7 MO 6.0 15
' g 1.0 Ti 0.7 Mn 1.3
showed a tensile strength of 100,000 pounds per 20 marked improvement in the surface of the ma- 35 terial as cast. This feature combined with a substantial reduction in the melting point, a reduction in the specific gravity, and a reduction in the shrinkage of cast specimens makes the composition particularly desirable for cast den- 40 tures 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 5 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 50 most of the alloys to between 2300 F. and 2500 F.
Another desirable characteristic developed by the beryllium addition is a decided reduction in the specific gravity of the material. This is a a5 very important factor where the material is used for prosthetic articles.
The following series of melts using, for comparative purposes, substantially the same per- 5 centages of chromium, nickel, cobalt and molybdenum, show the effect of adding various percentages of beryllium either in the form of copper-beryllium or nickel-berylliumfrom this type of 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 From the foregoing table it will be observed, among other things, that small additions of 25 beryllium efiect a remarkable increase in the hardness of the material as measured on the Rockwell C-scale. For example, the base alloy without beryllium has a hardness of C13v whereas melt No. 43 with an addition of 4% of beryllium shows an increase in hardness to (3-42, while heats Nos. 45 and 46 show that the addition of 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 1. Reduces the melting point;
2. Increases the fluidity;
3. Reduces the gravity;
4. Improves the surface as cast;
5. Increases the resistance to high temperature oxidation;
6. Increases the yield point;
7. Increases the hardness;
8. Reduces the elongation;
9. Reduces the tendency of the material 'to react with the casting crucible; and
10. Reduces the coeificient of expansion.
All additions of beryllium within the limits disclosed above produce a substantial increase in thefluidity 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 castingis 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 affect this highly desirable characteristic of the base alloy yet it makes possible the casting of lactic acid-resisting articles composition in the form of an alloy with a heavier metal such, for example, as copper, and
the titanium, when employed, is preferably added as a manganese-titanium alloy, and silicon is a permissible addition within the limits stated, it will be apparent that in addition to the principal alloying elements, chromium, nickel, cobalt and molybdenum and minor but efiective quantitles of beryllium, my alloy may contain other elements in quantities somewhat exceeding those ordinarily encountered as impurities but which do not materially aifect 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, molybdenum and beryllium as essential 9.1-. loying ingredients, the chromium content being from 10% to 35%, the beryllium content being from 0.1% to the molybdenum content being from 0.1% to 8%, 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, molybdenum and beryllium as essential alloying ingredients, the chromium content being from 20% to 30%, the beryllium content being from 0.1% to 5%, the molybdenum content being from 0.1% to 8%, 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, molybdenum and beryllium as-essential alloying ingredients, the chromium content being from to 35%, the beryllium content being from more than 1.6% to 5%, the molybdenum content being from 0.1% to 8%, and the balance beingsubstantially 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.
4. An alloy comprising chromium, nickel, cobalt, molybdenum and beryllium as essential alloying ingredients, the chromium content being from 20% to 30%, the beryllium content being from more than 1.6% to 5%, the molybdenum content being from 0.1% to 8%, and the balance being substantially nickel and cobalt; the nickel content being from 35% to 40% and the cobalt 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, cobait, molybdenum and beryllium as essential alloying ingredients, the chromium content being from 25% to 32%, the beryllium content being from 0.1% to 5%, the molybdenum content being from 0.1% to 8%, 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, cobalt, molybdenum 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%, the molybdenum content being from 0.1% to 8%, and the balance being substantially nickel and cobalt; the nickel content being from 30% to and the cobalt content being from 25% to 35%; said alloy being 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.
ENRIQUE G. TOUCEDA.
US83078A 1935-05-17 1936-06-02 Alloy Expired - Lifetime US2072911A (en)

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Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2631095A (en) * 1950-02-21 1953-03-10 Cons Car Heating Co Inc Alloy adapted for prosthetic articles
US2695844A (en) * 1949-09-28 1954-11-30 Armco Steel Corp High-temperature cobalt base alloys
US2973291A (en) * 1957-06-07 1961-02-28 Straumann Inst Ag Manufacture of point bearings in instruments
US2981620A (en) * 1959-08-24 1961-04-25 Westinghouse Electric Corp Cobalt-nickel base alloy
US3177074A (en) * 1962-04-23 1965-04-06 Duriron Co Cobalt base alloys
US3464817A (en) * 1966-03-17 1969-09-02 Cmp Ind Inc Alloy composition and method of forming the same
US4592890A (en) * 1983-08-08 1986-06-03 Dentsply Research & Development Corp. Dental prostheses alloy

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2695844A (en) * 1949-09-28 1954-11-30 Armco Steel Corp High-temperature cobalt base alloys
US2631095A (en) * 1950-02-21 1953-03-10 Cons Car Heating Co Inc Alloy adapted for prosthetic articles
US2973291A (en) * 1957-06-07 1961-02-28 Straumann Inst Ag Manufacture of point bearings in instruments
US2981620A (en) * 1959-08-24 1961-04-25 Westinghouse Electric Corp Cobalt-nickel base alloy
US3177074A (en) * 1962-04-23 1965-04-06 Duriron Co Cobalt base alloys
US3464817A (en) * 1966-03-17 1969-09-02 Cmp Ind Inc Alloy composition and method of forming the same
US4592890A (en) * 1983-08-08 1986-06-03 Dentsply Research & Development Corp. Dental prostheses alloy

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