US2471630A - Pressed and sintered oxidation resistant nickel alloys - Google Patents
Pressed and sintered oxidation resistant nickel alloys Download PDFInfo
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- US2471630A US2471630A US624095A US62409545A US2471630A US 2471630 A US2471630 A US 2471630A US 624095 A US624095 A US 624095A US 62409545 A US62409545 A US 62409545A US 2471630 A US2471630 A US 2471630A
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- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C1/00—Making non-ferrous alloys
- C22C1/04—Making non-ferrous alloys by powder metallurgy
- C22C1/0433—Nickel- or cobalt-based alloys
Definitions
- the present invention relates to alloys having a high resistanc to oxidation and to the action of strong alkaline solvents such as fused alkaline nitrates.
- the alloy of the invention has particular advantages for use in making mounts for diamond dies.
- Die mounts for hot drawing of wires must have a high resistance to oxidation.
- the drawing temperatures are frequently high enough to cause oxidation of the mounts at present in general use, to such a de gree that the die will be loosened in the mount.
- Such a condition greatly impairs or even totally destroys the usefulness of the die, since the bearing in the die is no longer concentric in relation to the mount, nor is it any longer truly at right angles to the faces thereof.
- the axes of the bearings of the diamond nib and of the mount must coincide exactly. A high degree of accuracy in this respect is necessary and even a slight deviation from axial symmetry will greatly impair the usefulness and efficiency of the die.
- the alloy of the invention consists of nickel, copper, chromium and silver combined in the proportions and according to the method hereinafter described. It must first be noted, however, that chromium, when heat treated either by fusion methods or by methods of powder metallurgy, has a marked tendency to oxidize and, in such case, not to alloy in a true sense with the other constituents noted. On the contrary, the chromium oxide forms nodes and these nodes are distributed through the mass of alloy of the other constituents in a porphyritic structure. Such a result is highly undesirable.
- the chromium is first alloyed with nickel to form a nickel chromium. alloy. This is effected by adding 90% nickel powder to 10% chromium powder, both of about 200 mesh or finer. The metal powders are thoroughly mixed as by ball milling until they are thoroughly commingled. The mixed nickel and chromium powders are then placed in a mold and compressed under hydraulic pressure of about 10 to 20 tons per square inch. The ingot so formed is then sintered in a hydrogen atmosphere at a temperature of about BOW-400 C.
- the hydrogen may be dried by bubbling it through sulphuric acid or by passing it over phosphorus pentoxide.
- the nickel and chromium may, however, be heat treated in any suitable non-oxidizing atmosphere other than hydrogen or the heating may be carried out in a vacuum as in a high frequency vacuum furnace.
- the nickel and chromium are sintered into a porous rod and are thoroughly diffused so as to form an alloy having a high resistance to oxidation.
- This rod is then broken down to powder form by mechanical means such as crushing or hammering. I call this alloy metal A.
- a second batch of metal powders consisting of nickel powder and copper powder 30% and also about 200 mesh or finer is thoroughly ball milled for several hours or until thorough distribution of the constituent powders is obtained. I call this metal, metal B.
- a third batch of metal is then formed by mixing A and B metals in about the following proportions:
- metal B I refer to this metal as metal C.
- the final alloy is then formed by mixing from 75%-96% of powdered metal C with from 25%- 4% of silver powder.
- the pressed compact is rem e ed from the press and given a presintering treatment in a furnace in a dry hydrogen atmosphere at a temperature of from 300 to 400 C. for about one-half hour.
- a further and final sintering is then effected also in a dry hydrogen atmosphere at a temperature of from about 800900 C. for about a half hour. and alloying of the constituents takes place without any trace of porphyritic characteristics and the metal shrinks to about 92% to 80% of the volume of the compacted mass.
- chromium zirconium, beryllium, or aluminum may be substituted in the same proportion as the chromium without substantial change either in the method or in the characteristics of the final alloy.
- Chromium, zirconium, beryllium and aluminum have the same properties in adding resistance to oxidation when combined with the other constituents of the alloy and should be alloyed separately with nickel in the same proportions as hereinabove stated for chromium alone to form the preliminary alloy. Thorough difiusion Under this treatment thorough diffusion and alloying of nickel with these metals should be efiected before adding to the other constituents if a true final alloy is to be obtained and a porphyritic structure is to be prevented. In any case, however, the proportions given above for the constituents are to be observed, viz: 75% to 96% of metal 0 powder with from 25% to 4% of silver powder.
- the proportions of the constituents of the final alloy will then be within the ranges of from 70.2% to 74% nickel, 0.1% to 2.0% of one or more of the group consisting of chromium, zirconium, beryllium or aluminum, and from 29.7% to 24% copper alloyed with silver in the proportions of 75% to 96% of the combined metals and 25% to 4% silver; or from 52.65% to 71.04% nickel, 0.075% to 1.92% chromium, zirconium, beryllium or aluminum, 22.275% to 23.04% copper and 25% to 4% silver.
- a pressed and sintered oxidation resistant alloy consisting of 75% to 96% of nickel, chromium and copper in the proportions of 70.2% 74% nickel; 0.1%-2.0% chromium; and 29.7%- 24% copper; and silver in the proportions of %-4%; the constituents being thoroughly diffused free from chromium oxide inclusions.
- a pressed and sintered oxidation resistant alloy consisting of 64.8% nickel, 24.3% copper, 0.2% chromium and 10% silver, the constituents being thoroughly diffused and free from chromium oxide inclusions.
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Description
Patented May 31, 1949 UNITED STATES OFFICE PRESSED AND SINTERED OXIDATION RESISTANT NICKEL ALLOYS Jacob Kurtz, Teaneck, N. J., assignor to Oallite Tungsten Corporation, Union City, N. J a corporation of Delaware 2 Claims.
The present invention relates to alloys having a high resistanc to oxidation and to the action of strong alkaline solvents such as fused alkaline nitrates. The alloy of the invention has particular advantages for use in making mounts for diamond dies.
Die mounts for hot drawing of wires must have a high resistance to oxidation. In drawing refractory metals, the drawing temperatures are frequently high enough to cause oxidation of the mounts at present in general use, to such a de gree that the die will be loosened in the mount. Such a condition greatly impairs or even totally destroys the usefulness of the die, since the bearing in the die is no longer concentric in relation to the mount, nor is it any longer truly at right angles to the faces thereof. The axes of the bearings of the diamond nib and of the mount must coincide exactly. A high degree of accuracy in this respect is necessary and even a slight deviation from axial symmetry will greatly impair the usefulness and efficiency of the die. Again, in the drawing of tungsten or molybdenum, it frequently happens that a piece of wire breaks in the die and must be dissolved out. For this purpose, a fused alkaline nitrate is generally used. Such powerful reactants, however, also tend to cause oxidation and even to dissolve the mount metals generally employed and consequently to loosen the die nib in the mount with the deleterious effects hereinbefore described.
It is an object of the present invention to provide an alloy suitable for forming die mounts that will resist the oxidizing effects of temperatures encountered in hot drawing of refractory metal wires, such as tungsten of molybdenum wires and wires of other high melting point metals.
It is a further object to provide an alloy that will be suitable for use wherever it is necessary to prevent oxidation effects of high temperatures and of strong alkaline reactants.
Briefly described, the alloy of the invention consists of nickel, copper, chromium and silver combined in the proportions and according to the method hereinafter described. It must first be noted, however, that chromium, when heat treated either by fusion methods or by methods of powder metallurgy, has a marked tendency to oxidize and, in such case, not to alloy in a true sense with the other constituents noted. On the contrary, the chromium oxide forms nodes and these nodes are distributed through the mass of alloy of the other constituents in a porphyritic structure. Such a result is highly undesirable.
l or. d522) Accordingtojhe method of the present invention, the chromium is first alloyed with nickel to form a nickel chromium. alloy. This is effected by adding 90% nickel powder to 10% chromium powder, both of about 200 mesh or finer. The metal powders are thoroughly mixed as by ball milling until they are thoroughly commingled. The mixed nickel and chromium powders are then placed in a mold and compressed under hydraulic pressure of about 10 to 20 tons per square inch. The ingot so formed is then sintered in a hydrogen atmosphere at a temperature of about BOW-400 C. Great care must be taken to dry the hydrogen, as water vapor, which is present in nearly all commercially produced hydrogen, is a very active oxidizing agent and will cause the chromium to oxidize rapidly and to form the undesirable porphyritic structure above described instead of alloying with the nickel. The hydrogen may be dried by bubbling it through sulphuric acid or by passing it over phosphorus pentoxide.
The nickel and chromium may, however, be heat treated in any suitable non-oxidizing atmosphere other than hydrogen or the heating may be carried out in a vacuum as in a high frequency vacuum furnace.
At the temperatures and under the nonoxidizing conditions mentioned, the nickel and chromium are sintered into a porous rod and are thoroughly diffused so as to form an alloy having a high resistance to oxidation. This rod is then broken down to powder form by mechanical means such as crushing or hammering. I call this alloy metal A.
A second batch of metal powders consisting of nickel powder and copper powder 30% and also about 200 mesh or finer is thoroughly ball milled for several hours or until thorough distribution of the constituent powders is obtained. I call this metal, metal B.
A third batch of metal is then formed by mixing A and B metals in about the following proportions:
1%, 20% metal A; 99%, metal B I refer to this metal as metal C.
The final alloy is then formed by mixing from 75%-96% of powdered metal C with from 25%- 4% of silver powder.
Assuming that the proportions of metal C consist of 10% of metal A and of metal B, and assuming also that the final metal alloy is to consist of 90% of metal 0 and 10% silver, the
3 resulting very satisfactory alloy will consist of the following:
The proportions given are by Weight.
In my Patent No. 2,374,942 issued May 1, 1945, application for which was filed January 13, 1944 contemporaneously with application Ser. No. 518,100, now Patent No. 2,441,126, issued May 11, 1948, and of which latter application this appli cation is a division, I have described the use of this metal for forming mounts for dies. The further treatment of the powdered metal above described, whether used for making die mounts or for other purposes, will be the same. The powdered metal is first poured into a mold of the desired shape and compressed in a hydraulic press under a pressure of 5-20 tons pressure to the square inch.
The pressed compact is rem e ed from the press and given a presintering treatment in a furnace in a dry hydrogen atmosphere at a temperature of from 300 to 400 C. for about one-half hour. A further and final sintering is then effected also in a dry hydrogen atmosphere at a temperature of from about 800900 C. for about a half hour. and alloying of the constituents takes place without any trace of porphyritic characteristics and the metal shrinks to about 92% to 80% of the volume of the compacted mass.
Instead of chromium, zirconium, beryllium, or aluminum may be substituted in the same proportion as the chromium without substantial change either in the method or in the characteristics of the final alloy.
Chromium, zirconium, beryllium and aluminum have the same properties in adding resistance to oxidation when combined with the other constituents of the alloy and should be alloyed separately with nickel in the same proportions as hereinabove stated for chromium alone to form the preliminary alloy. Thorough difiusion Under this treatment thorough diffusion and alloying of nickel with these metals should be efiected before adding to the other constituents if a true final alloy is to be obtained and a porphyritic structure is to be prevented. In any case, however, the proportions given above for the constituents are to be observed, viz: 75% to 96% of metal 0 powder with from 25% to 4% of silver powder. The proportions of the constituents of the final alloy will then be within the ranges of from 70.2% to 74% nickel, 0.1% to 2.0% of one or more of the group consisting of chromium, zirconium, beryllium or aluminum, and from 29.7% to 24% copper alloyed with silver in the proportions of 75% to 96% of the combined metals and 25% to 4% silver; or from 52.65% to 71.04% nickel, 0.075% to 1.92% chromium, zirconium, beryllium or aluminum, 22.275% to 23.04% copper and 25% to 4% silver.
Having thus described my invention, what I claim is:
1. A pressed and sintered oxidation resistant alloy consisting of 75% to 96% of nickel, chromium and copper in the proportions of 70.2% 74% nickel; 0.1%-2.0% chromium; and 29.7%- 24% copper; and silver in the proportions of %-4%; the constituents being thoroughly diffused free from chromium oxide inclusions.
2. A pressed and sintered oxidation resistant alloy consisting of 64.8% nickel, 24.3% copper, 0.2% chromium and 10% silver, the constituents being thoroughly diffused and free from chromium oxide inclusions.
JACOB KURTZ.
REFERENCES CITED The following references are of record in the file of this patent:
UNITED STATES PATENTS Number Name Date 1,757,507 Barker M May 6, 1930 2,263,246 Wise et a1. May 19, 1942 2,323,169 Nagenhals June 29, 1943 2,404,248 Parker July 16, 1946 2,428,205 Dannohl et al Sept. 30, 1947 2,441,126 Kurtz May 11, 1948
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US624095A US2471630A (en) | 1944-01-13 | 1945-10-23 | Pressed and sintered oxidation resistant nickel alloys |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US518100A US2441126A (en) | 1944-01-13 | 1944-01-13 | Oxidation resistant alloys |
US624095A US2471630A (en) | 1944-01-13 | 1945-10-23 | Pressed and sintered oxidation resistant nickel alloys |
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US2471630A true US2471630A (en) | 1949-05-31 |
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US624095A Expired - Lifetime US2471630A (en) | 1944-01-13 | 1945-10-23 | Pressed and sintered oxidation resistant nickel alloys |
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Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2851354A (en) * | 1954-01-13 | 1958-09-09 | Schwarzkopf Dev Co | Process of forming sintered sheets having copper infiltrated portions |
US2928733A (en) * | 1957-06-21 | 1960-03-15 | Purolator Products Inc | Sintering of metal elements |
US3039000A (en) * | 1956-07-14 | 1962-06-12 | Schwarzkopf Dev Co | Radiation shield structures and their production |
US3078157A (en) * | 1960-07-08 | 1963-02-19 | Mannesmann Ag | Metallurgical product and process |
US3357826A (en) * | 1966-11-14 | 1967-12-12 | Int Nickel Co | Powder metallurgical production of chromium-containing alloys |
Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1757507A (en) * | 1928-09-05 | 1930-05-06 | Harry H Semmes | Alloy |
US2283246A (en) * | 1940-03-29 | 1942-05-19 | Int Nickel Co | Cast valve |
US2323169A (en) * | 1940-02-08 | 1943-06-29 | Rca Corp | Process of plating metal bodies |
US2404248A (en) * | 1940-09-18 | 1946-07-16 | Gen Electric | Heat-resistant alloy |
US2428205A (en) * | 1937-09-27 | 1947-09-30 | Dannohl Walter | Permanent magnet alloy |
US2441126A (en) * | 1944-01-13 | 1948-05-11 | Callite Tungsten Corp | Oxidation resistant alloys |
-
1945
- 1945-10-23 US US624095A patent/US2471630A/en not_active Expired - Lifetime
Patent Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1757507A (en) * | 1928-09-05 | 1930-05-06 | Harry H Semmes | Alloy |
US2428205A (en) * | 1937-09-27 | 1947-09-30 | Dannohl Walter | Permanent magnet alloy |
US2323169A (en) * | 1940-02-08 | 1943-06-29 | Rca Corp | Process of plating metal bodies |
US2283246A (en) * | 1940-03-29 | 1942-05-19 | Int Nickel Co | Cast valve |
US2404248A (en) * | 1940-09-18 | 1946-07-16 | Gen Electric | Heat-resistant alloy |
US2441126A (en) * | 1944-01-13 | 1948-05-11 | Callite Tungsten Corp | Oxidation resistant alloys |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2851354A (en) * | 1954-01-13 | 1958-09-09 | Schwarzkopf Dev Co | Process of forming sintered sheets having copper infiltrated portions |
US3039000A (en) * | 1956-07-14 | 1962-06-12 | Schwarzkopf Dev Co | Radiation shield structures and their production |
US2928733A (en) * | 1957-06-21 | 1960-03-15 | Purolator Products Inc | Sintering of metal elements |
US3078157A (en) * | 1960-07-08 | 1963-02-19 | Mannesmann Ag | Metallurgical product and process |
US3357826A (en) * | 1966-11-14 | 1967-12-12 | Int Nickel Co | Powder metallurgical production of chromium-containing alloys |
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