US2289641A - Alloy - Google Patents
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- Publication number
- US2289641A US2289641A US273502A US27350239A US2289641A US 2289641 A US2289641 A US 2289641A US 273502 A US273502 A US 273502A US 27350239 A US27350239 A US 27350239A US 2289641 A US2289641 A US 2289641A
- Authority
- US
- United States
- Prior art keywords
- boron
- ingots
- ingot
- alloy
- chromium
- 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
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- 229910045601 alloy Inorganic materials 0.000 title description 7
- 239000000956 alloy Substances 0.000 title description 7
- ZOXJGFHDIHLPTG-UHFFFAOYSA-N Boron Chemical compound [B] ZOXJGFHDIHLPTG-UHFFFAOYSA-N 0.000 description 19
- 229910052796 boron Inorganic materials 0.000 description 19
- 238000007792 addition Methods 0.000 description 11
- 239000000047 product Substances 0.000 description 9
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 7
- 239000000463 material Substances 0.000 description 7
- 229910052751 metal Inorganic materials 0.000 description 7
- 239000002184 metal Substances 0.000 description 7
- 241000237858 Gastropoda Species 0.000 description 6
- PALQHNLJJQMCIQ-UHFFFAOYSA-N boron;manganese Chemical compound [Mn]#B PALQHNLJJQMCIQ-UHFFFAOYSA-N 0.000 description 6
- 239000000470 constituent Substances 0.000 description 6
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 description 5
- 229910052804 chromium Inorganic materials 0.000 description 5
- 239000011651 chromium Substances 0.000 description 5
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 4
- 229910018487 Ni—Cr Inorganic materials 0.000 description 3
- VNNRSPGTAMTISX-UHFFFAOYSA-N chromium nickel Chemical compound [Cr].[Ni] VNNRSPGTAMTISX-UHFFFAOYSA-N 0.000 description 3
- 230000000694 effects Effects 0.000 description 3
- 238000002844 melting Methods 0.000 description 3
- 230000008018 melting Effects 0.000 description 3
- 229910052759 nickel Inorganic materials 0.000 description 3
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 description 2
- OYPRJOBELJOOCE-UHFFFAOYSA-N Calcium Chemical compound [Ca] OYPRJOBELJOOCE-UHFFFAOYSA-N 0.000 description 2
- 229910000640 Fe alloy Inorganic materials 0.000 description 2
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 description 2
- QCWXUUIWCKQGHC-UHFFFAOYSA-N Zirconium Chemical compound [Zr] QCWXUUIWCKQGHC-UHFFFAOYSA-N 0.000 description 2
- 229910052782 aluminium Inorganic materials 0.000 description 2
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 2
- 229910052791 calcium Inorganic materials 0.000 description 2
- 239000011575 calcium Substances 0.000 description 2
- BIJOYKCOMBZXAE-UHFFFAOYSA-N chromium iron nickel Chemical compound [Cr].[Fe].[Ni] BIJOYKCOMBZXAE-UHFFFAOYSA-N 0.000 description 2
- 239000012535 impurity Substances 0.000 description 2
- 229910052742 iron Inorganic materials 0.000 description 2
- 238000004519 manufacturing process Methods 0.000 description 2
- 239000000203 mixture Substances 0.000 description 2
- 238000005096 rolling process Methods 0.000 description 2
- 229910052710 silicon Inorganic materials 0.000 description 2
- 239000010703 silicon Substances 0.000 description 2
- 229910052726 zirconium Inorganic materials 0.000 description 2
- 229910000521 B alloy Inorganic materials 0.000 description 1
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 1
- 229910001018 Cast iron Inorganic materials 0.000 description 1
- FYYHWMGAXLPEAU-UHFFFAOYSA-N Magnesium Chemical compound [Mg] FYYHWMGAXLPEAU-UHFFFAOYSA-N 0.000 description 1
- 230000002411 adverse Effects 0.000 description 1
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 229910052790 beryllium Inorganic materials 0.000 description 1
- ATBAMAFKBVZNFJ-UHFFFAOYSA-N beryllium atom Chemical compound [Be] ATBAMAFKBVZNFJ-UHFFFAOYSA-N 0.000 description 1
- QDWJUBJKEHXSMT-UHFFFAOYSA-N boranylidynenickel Chemical compound [Ni]#B QDWJUBJKEHXSMT-UHFFFAOYSA-N 0.000 description 1
- 229910052799 carbon Inorganic materials 0.000 description 1
- 239000000919 ceramic Substances 0.000 description 1
- UPHIPHFJVNKLMR-UHFFFAOYSA-N chromium iron Chemical compound [Cr].[Fe] UPHIPHFJVNKLMR-UHFFFAOYSA-N 0.000 description 1
- 238000001816 cooling Methods 0.000 description 1
- 238000005336 cracking Methods 0.000 description 1
- 230000001419 dependent effect Effects 0.000 description 1
- 239000003599 detergent Substances 0.000 description 1
- 229910001338 liquidmetal Inorganic materials 0.000 description 1
- 229910052749 magnesium Inorganic materials 0.000 description 1
- 239000011777 magnesium Substances 0.000 description 1
- 150000001247 metal acetylides Chemical class 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 229910000623 nickel–chromium alloy Inorganic materials 0.000 description 1
- 150000004767 nitrides Chemical class 0.000 description 1
- 229910052757 nitrogen Inorganic materials 0.000 description 1
- 230000003647 oxidation Effects 0.000 description 1
- 238000007254 oxidation reaction Methods 0.000 description 1
- 229910052760 oxygen Inorganic materials 0.000 description 1
- 239000001301 oxygen Substances 0.000 description 1
- 230000002093 peripheral effect Effects 0.000 description 1
- 238000002360 preparation method Methods 0.000 description 1
- 238000007790 scraping Methods 0.000 description 1
- 238000007711 solidification Methods 0.000 description 1
- 230000008023 solidification Effects 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
- 239000002699 waste material Substances 0.000 description 1
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
Definitions
- the molten prod uct is considerably contaminated during its manufacture.
- the resulting oxides, nitrides, carbides, etc, accumulate at the grain boundaries upon solidification, thereby producing an alloy which lacks uniformity in its thermo-expansive characteristics. As a result, the material tends to further oxidize along the grain boundaries when subjected to elevated temperatures.
- test slug like the ingot, is formed in a cast-iron slug mold and is approximately 2 inches square on the base, 4 inches in height and 1% inches square on the top surface so as to form, in effect, a truncated pyramid.
- boron constituent serves additionally to materi-
- the yield of usable material is predicated upon the percentage or weight of good stock obtained, to theoriginal weight of the ingots as cast or produced in the foundry.
- the ingot is poured with a so-called hot-top," which refers to a ceramic, or metal form, inserted in the top of the ingot through which the hot metal is poured and which functions as a reservoir of hot metal to allow the production of a full ingot when shrinkage occurs during the solidifying action.
- the hot-top which is a necessary and unavoidable loss, is removed, and the surface of the ingot is machined to remove scale and impurities and to provide a clear surface free of cracks.
- the decapitated and machined ingot is then reheated and partially converted or formed into a billet which, in turn, is allowed to cool before imperfections, such as seams, cracks or imbedded material are either chipped or ground out of its surface.
- the billets are reheated and then fabricated into rods and the yields," above referred to, is the ratio of the weight of good stock in the rods to the original weight of all of the ingots in their first form as cast in the foundry.
- ingots of 100 pounds each were made under identical conditions and from the same nickelchromium base constituents.
- 40 grams of manganese-boron was added in the manner above described.
- 50 grams of manganese-boron was added, and to the third, 60 grams of manganese-boron.
- deoxidizers such as are described in some of their 2,289,641 aspects in the United States patent to Hunter,
- boron in the forms in which it is readily obtainable commercially; that is, as manganeseboron, nickel-boron, boron metal and other alloys of boron. Furthermore, the boron constituent representing the most reactive addition to the basic alloy is introduced only after the basic materials are in molten condition and just prior to pouring. It will be apparent likewise that this practice insures a residual quantity of boron in the finished product.
- An electrical resistance alloy containing approximately 60% of nickel, approximately 15% of chromium, an appreciable amount of boron, up to 2%, and the balance, iron.
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Forging (AREA)
- Manufacture And Refinement Of Metals (AREA)
Description
Patented July-1 4, 1942 UNITED STATES. PATENT omcg ALLOY Erich Feta, Newark, N. 1., assignor to Wilbur B. Driver 00., Newark, N. 1., a corporation of New Jersey No Drawing. Application May 13,1939,
Serial No. 273,502 g 1 Claim. (Cl. 75-171) nickel-chromium-iron, are conventionally em-v ployed where service conditions necessitate performance of the resistance material at elevated temperatures. These basic compositions of themselves are susceptible to mechanical failure in service which may be attributed to a large extent to the crystalline or grain structure of the material. v
Because of the high affinity of chromium towards oxygen, nitrogen and carbon, and due to the high melting temperatures necessarily employed in the melting operation, the molten prod uct is considerably contaminated during its manufacture. The resulting oxides, nitrides, carbides, etc, accumulate at the grain boundaries upon solidification, thereby producing an alloy which lacks uniformity in its thermo-expansive characteristics. As a result, the material tends to further oxidize along the grain boundaries when subjected to elevated temperatures.
By the addition of such elements as silicon, aluminum, calcium, magnesium, beryllium, zirconium,,etc., the susceptibility of the produce to oxidation at elevated temperatures is appreciably lowered and, furthermore, these latter constituents function as cleansing agents to remove the non-metallic impurities introduced either during melting or which result from the use of relatively impure commercial chromium.
Such alloysare disclosed in the United States patents to Hunter, No. 2,005,423, and Lohr, Nos. 2,019,687, 2,019,688, 2,005,431, 2,051,562, 2,047,916, 2,047,917, 2,047,918, 2,005,430, 2,005,433 and 2,020,686.
Although the addition of such substances as silicon, aluminum, calcium, zirconium, eta, prolong the life of the product under service conditions, theirpresence in sufiicient proportions to' insure this result measurably detracts from the hot workability ofthe product during the fabri eating operations.
I have found that the addition of a relatively small amount of boron to a nickel-chromium or to a nickel-chromium-iron alloy, of the above character greatly improves the malleable characteristics of the product without adversely affecting other desirable properties.
Both slugs and ingots containing varying proportions 'of boron were cast and tested exhaustively to provide a wide range of data and corresponding accuracy of results. Furthermore, with a view to obtaining slugs which were truly representative of the composition of the ingots, the metal from which the slugs were formed was taken from the stream of liquid metal when the corresponding ingot mold was about half filled.
The test slug, like the ingot, is formed in a cast-iron slug mold and is approximately 2 inches square on the base, 4 inches in height and 1% inches square on the top surface so as to form, in effect, a truncated pyramid.
Both the ingot and slug were raised to temperatures of approximately 2200 Fahrenheit and forged under a steam hammer. The slug was subjected to a few hard blows of the hammer, as a result of which its height was reduced from 4 inches to inch, the mass of the metal being caused to define a flat cylindrical section. It will be apparent to. those skilled in the art that the condition of the peripheral edge of this hammered cylindrical body will be dependent upon the hot workability or forgeability of the product. Thus, an alloy of poor forgeability will show cracks of varying depth and number in its circumferential edge, whereas an ideal product will be smooth and entirely free from cracks.
I have evaluated the results obtained in the above mentioned tests upon a number of nickelchromium slugs containing manganese-boron by ascribing the letter A to those samples which produced perfect results; B to those which resulted in fair products; -C for very poor products and D to indicate no forgeable characteristics. More particularly, onlyv those samples, the circumference of which wer completely smooth and free from cracks, were identified by ered with very deep vertical cracks which started to form with the first blow of the hammer, the
letter "D" is the index of the result.
Manganese- Forgeability, boron addition sample slug Grams No C- Now coming to the tests conducted upon the ingots: Whereas it is ordinary foundry practice to scrape or machine the surfaces of ingots whose corresponding sample slugs show forgeability corresponding with my C or D categories, all ingots of the boron-treated series herein described were not forged without resorting to scraping with a view to obtaining critical data concerning the eflect of the varying additions of boron to the ingots. V
After raising the temperature of the ingots to 220i)- Fahrenheit, they were placed under a steam hammer to billets of 1H xlH cross sectional area. Predicated upon the number, size and character of cracks appearing in the billets, the scale of forgeability indlces which were used to characterize the workability of the slugs were again applied.
:I'he result of these tests was as follows:
Manganese- Forgeability, boron addition ingot Grams No C 10 C 20 B 30 A 40 A 50 A 60 A 70 D v Forgeability Manganeseboron I addition Sample Ingot Gram:
No C- O C 20 A B 30 A A 40 A A 50 A A 60 B A 70 C- D 2,289,641 the mark "A" and only those having a few small 'In addition to its property of improving the hot working characteristics of the alloy, the
boron constituent serves additionally to materi-,
ally increase the yield of usable material. The yield of usable material is predicated upon the percentage or weight of good stock obtained, to theoriginal weight of the ingots as cast or produced in the foundry. In ordinary practice the ingot is poured with a so-called hot-top," which refers to a ceramic, or metal form, inserted in the top of the ingot through which the hot metal is poured and which functions as a reservoir of hot metal to allow the production of a full ingot when shrinkage occurs during the solidifying action. After cooling, the hot-top, which is a necessary and unavoidable loss, is removed, and the surface of the ingot is machined to remove scale and impurities and to provide a clear surface free of cracks. The decapitated and machined ingot is then reheated and partially converted or formed into a billet which, in turn, is allowed to cool before imperfections, such as seams, cracks or imbedded material are either chipped or ground out of its surface. After this second operation to remove waste material, the billets are reheated and then fabricated into rods and the yields," above referred to, is the ratio of the weight of good stock in the rods to the original weight of all of the ingots in their first form as cast in the foundry.
While the losses entailed in the skimming of the ingot, removing of hot-tops and surfacing of billets are considered to be necessary and unavoidable in their nature, their relative amount is decidedly reduced by the addition of boron.
Furthermore, the minute temperature control formerly necessary to prevent cracking or fracturing in the surfaces of the. ingot or billet during, the rolling operation to effect change of shape, is eliminated by the presence of boron. Not only does the boron constituent permit of the employment of greater latitude of rolling temperatures, but a relatively higher yield of good stock is obtained at the same time.
To indicate the effect of boron upon yield," ingots of 100 pounds each were made under identical conditions and from the same nickelchromium base constituents. To one group of these ingots, 40 grams of manganese-boron was added in the manner above described. To another, 50 grams of manganese-boron was added, and to the third, 60 grams of manganese-boron.
All of the ingots were then carefully scraped or machined until crack and scale-free surfaces were reached and the ingots were then forged to billets, which, after surface preparation, were hot rolled to A, inch rod. Evaluating the per cent of yield of the finished A inch rod in terms of the total weight of the three groups of ingots, as identified by the 40, 50 and 60 gram additions of boron, the following results were obtained:
Mangancse- Percent yield] boron addition cast weight Grams Percent 40 71. 2 50 v 75.0 60 61. 8 I
deoxidizers, such as are described in some of their 2,289,641 aspects in the United States patent to Hunter,
No. 2,005,423, because it produces a cleaner metal, as is demonstrated by the reduction of wastage.
In carrying out the method of my invention, I utilize boron in the forms in which it is readily obtainable commercially; that is, as manganeseboron, nickel-boron, boron metal and other alloys of boron. Furthermore, the boron constituent representing the most reactive addition to the basic alloy is introduced only after the basic materials are in molten condition and just prior to pouring. It will be apparent likewise that this practice insures a residual quantity of boron in the finished product.
Although I have enumerated the constituents of a typical nickel-chromium alloy, experimentation has shown that boron is equally beneficial when added to a nickel-'chromium-iron alloy containing substantially 60 per cent of nickel, 15 per cent chromium, with the balance iron, or 30 per cent nickel, 20 per cent chromium and the balanceiron. 1
I claim as my invention:
An electrical resistance alloy containing approximately 60% of nickel, approximately 15% of chromium, an appreciable amount of boron, up to 2%, and the balance, iron.
ERICH FETZ.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US273502A US2289641A (en) | 1939-05-13 | 1939-05-13 | Alloy |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US273502A US2289641A (en) | 1939-05-13 | 1939-05-13 | Alloy |
Publications (1)
Publication Number | Publication Date |
---|---|
US2289641A true US2289641A (en) | 1942-07-14 |
Family
ID=23044200
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US273502A Expired - Lifetime US2289641A (en) | 1939-05-13 | 1939-05-13 | Alloy |
Country Status (1)
Country | Link |
---|---|
US (1) | US2289641A (en) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2456370A (en) * | 1945-02-19 | 1948-12-14 | Int Nickel Co | Process for producing electrodeposited nickel strip containing boron |
US2744009A (en) * | 1951-07-30 | 1956-05-01 | Crucible Steel Co America | Ni-cr hard facing alloys |
US2755183A (en) * | 1955-01-25 | 1956-07-17 | Coast Metals Inc | Nickel-silicon-boron alloys |
DE1068023B (en) * | 1959-10-29 |
-
1939
- 1939-05-13 US US273502A patent/US2289641A/en not_active Expired - Lifetime
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1068023B (en) * | 1959-10-29 | |||
US2456370A (en) * | 1945-02-19 | 1948-12-14 | Int Nickel Co | Process for producing electrodeposited nickel strip containing boron |
US2744009A (en) * | 1951-07-30 | 1956-05-01 | Crucible Steel Co America | Ni-cr hard facing alloys |
US2755183A (en) * | 1955-01-25 | 1956-07-17 | Coast Metals Inc | Nickel-silicon-boron alloys |
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