US2220084A - Alloy - Google Patents
Alloy Download PDFInfo
- Publication number
- US2220084A US2220084A US255242A US25524239A US2220084A US 2220084 A US2220084 A US 2220084A US 255242 A US255242 A US 255242A US 25524239 A US25524239 A US 25524239A US 2220084 A US2220084 A US 2220084A
- Authority
- US
- United States
- Prior art keywords
- alloy
- boron
- found
- present
- cobalt
- 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
Links
- 229910045601 alloy Inorganic materials 0.000 title description 32
- 239000000956 alloy Substances 0.000 title description 32
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 22
- ZOXJGFHDIHLPTG-UHFFFAOYSA-N Boron Chemical compound [B] ZOXJGFHDIHLPTG-UHFFFAOYSA-N 0.000 description 18
- 229910052796 boron Inorganic materials 0.000 description 18
- 229910017052 cobalt Inorganic materials 0.000 description 11
- 239000010941 cobalt Substances 0.000 description 11
- GUTLYIVDDKVIGB-UHFFFAOYSA-N cobalt atom Chemical compound [Co] GUTLYIVDDKVIGB-UHFFFAOYSA-N 0.000 description 11
- 229910052742 iron Inorganic materials 0.000 description 11
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 10
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 description 10
- 229910052799 carbon Inorganic materials 0.000 description 10
- 229910052804 chromium Inorganic materials 0.000 description 10
- 239000011651 chromium Substances 0.000 description 10
- WFKWXMTUELFFGS-UHFFFAOYSA-N tungsten Chemical compound [W] WFKWXMTUELFFGS-UHFFFAOYSA-N 0.000 description 10
- 229910052721 tungsten Inorganic materials 0.000 description 10
- 239000010937 tungsten Substances 0.000 description 10
- 238000007669 thermal treatment Methods 0.000 description 9
- 229910052720 vanadium Inorganic materials 0.000 description 9
- LEONUFNNVUYDNQ-UHFFFAOYSA-N vanadium atom Chemical compound [V] LEONUFNNVUYDNQ-UHFFFAOYSA-N 0.000 description 9
- 239000012535 impurity Substances 0.000 description 8
- ZOKXTWBITQBERF-UHFFFAOYSA-N Molybdenum Chemical compound [Mo] ZOKXTWBITQBERF-UHFFFAOYSA-N 0.000 description 7
- 238000004519 manufacturing process Methods 0.000 description 7
- 229910052751 metal Inorganic materials 0.000 description 7
- 239000002184 metal Substances 0.000 description 7
- 239000000203 mixture Substances 0.000 description 7
- 229910052750 molybdenum Inorganic materials 0.000 description 7
- 239000011733 molybdenum Substances 0.000 description 7
- 238000005266 casting Methods 0.000 description 6
- 238000009750 centrifugal casting Methods 0.000 description 5
- 230000000704 physical effect Effects 0.000 description 5
- 229910052770 Uranium Inorganic materials 0.000 description 4
- 239000000470 constituent Substances 0.000 description 4
- 238000005520 cutting process Methods 0.000 description 4
- 238000000034 method Methods 0.000 description 4
- JFALSRSLKYAFGM-UHFFFAOYSA-N uranium(0) Chemical compound [U] JFALSRSLKYAFGM-UHFFFAOYSA-N 0.000 description 4
- 230000005484 gravity Effects 0.000 description 3
- 239000011159 matrix material Substances 0.000 description 2
- 230000002411 adverse Effects 0.000 description 1
- 238000005275 alloying Methods 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 150000001639 boron compounds Chemical class 0.000 description 1
- 238000012777 commercial manufacturing Methods 0.000 description 1
- 230000006835 compression Effects 0.000 description 1
- 238000007906 compression Methods 0.000 description 1
- 230000001419 dependent effect Effects 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 238000002474 experimental method Methods 0.000 description 1
- 238000005242 forging Methods 0.000 description 1
- 229910000765 intermetallic Inorganic materials 0.000 description 1
- 238000011835 investigation Methods 0.000 description 1
- 230000001788 irregular Effects 0.000 description 1
- WPBNNNQJVZRUHP-UHFFFAOYSA-L manganese(2+);methyl n-[[2-(methoxycarbonylcarbamothioylamino)phenyl]carbamothioyl]carbamate;n-[2-(sulfidocarbothioylamino)ethyl]carbamodithioate Chemical compound [Mn+2].[S-]C(=S)NCCNC([S-])=S.COC(=O)NC(=S)NC1=CC=CC=C1NC(=S)NC(=O)OC WPBNNNQJVZRUHP-UHFFFAOYSA-L 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 238000002844 melting Methods 0.000 description 1
- 230000008018 melting Effects 0.000 description 1
- 150000002739 metals Chemical class 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 239000002245 particle Substances 0.000 description 1
- 238000004881 precipitation hardening Methods 0.000 description 1
- 230000001105 regulatory effect Effects 0.000 description 1
- 238000011160 research Methods 0.000 description 1
- 230000000717 retained effect Effects 0.000 description 1
- 229910052710 silicon Inorganic materials 0.000 description 1
- 239000010703 silicon Substances 0.000 description 1
- 239000006104 solid solution 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
- C22C38/00—Ferrous alloys, e.g. steel alloys
Definitions
- the present invention relates to a new andof the alloy produced by ordinary casting methods useful alloy and relates particularly to an alloy containing as essential components metal from the group tungsten, molybdenum and uranium,
- An object of the present invention is to provide an alloy having certain physical properties and characteristics which can be developed and controlled by means of thermal treatment, and, further, to provide an alloy having certain characteristics which render it particularly suitable for manufacture in finished or semi-finished forms by means of centrifugal casting.
- the alloy of the present invention in the form 15 of articles produced by means of centrifugal casting, has a combination of physical properties and. characteristics which render it especially valuable for metal cutting tools and many other industrial purposes.
- the presence of boron in the present composition has a marked and beneficial effect upon certain physical and mechanical properties.
- the cutting efficiency 40 of tools composed of the alloy is, in a large measure, directly dependent upon the percentage of boron in the alloy.
- the maximum degree of hardness which can be developed in the alloy can be regulated over a comparatively wide range by 45 varying the boron content.
- Ingots or other forms of the alloy disclosed herein cannot be economically forged or rolled. This characteristic is apparently due in part to the inherent resistance to deformation possessed 55 by the alloy, and also to the fact that ingots, etc.,
- Cast bodies of the alloy produced by centrifugal 40 casting may be utilized in the as cast condition. However, I usually prefer to subject the castings to a suitable thermal treatment before using them for metal cutting tools.
- an aggregate of the present composition comprises at least two principal constituents: (a) a relatively hard, intermetallic compound of boron with one or more of the other essential components; and (b) a solid solution of two or more of the essential components, which has a lower degree of hardness and functions as a matrix.
- an appreciable percentage of the intermetallic boron compound should be in the form of more or less finely 5 divided particles dispersed throughout the matrix.
- An aggregate having the preferred physical structure possesses a combination of essential physical properties superior to the properties of a cast aggregate which has not been subjected to ther mal treatment.
- the present alloy is amenable to thermal treatment for the development of precipitation hardening.
- a distinctive characteristic of a body of the alloy which has been subjected to a suitable thermal treatment is the combination of relatively high hardness, e. g., 63 to Rockwell C, and high resistance to impact. Another important property is that virtually all of the values of hardness and resistance to impact developed by thermal treatment are retained when the alloy is subjected to temperatures up to approximately 600 C.
- tungsten can be supplanted, in whole or in part, by molybdenum, uranium or both.
- compositions within the scope of the present invention which I have found to be valuable for various industrial purposes, are the following: Boron 0.60%, tungsten 14%, chromium 3.80%, vanadium 1.00%, cobalt 16%, iron substantially the balance; boron 0.85%, molybdenum 12%, chormium 4%, vanadium 2%, cobalt 25%, iron substantially the balance; boron 0.95%, molybdenum 8%, tungsten 6%, chromium 3.50%, vanadium 1.60%, cobalt 30%, iron substantially the balance.
- the alloys of the present invention as reasonably free from carbon as commercial manufacturing conditions permit.
- certain of the metals and alloys used in producing the present compositions generally contain. varying amounts of carbon as an impurity and, consequently, the alloys of the present invention will usually contain small amounts of carbon in the nature of an impurity incidental to manufacture. It is essential to restrict the percentage of carbon so present to an amount which will not be adversely effective on the important physical properties. I have found that carbon may be present in amounts as high as approximately 0.70% without seriously affecting the value of the alloy for various uses.
- the alloy of this invention may contain small amounts of elements other than carbon in the nature of incidental impurities.
- composition of the present invention comprises the following essential components; boron 0.25% to 5%, metal selected from the group tungsten, molybdenum and uranium. 5% to 30%, chromium 1% to 25%, vanadium 0.50% to 5%, cobalt 15% to 40%, and the balance substantially iron except for minor amounts of incidental impurities in which carbon when present, will not exceed approximately 0.70%.
- a centrifugally cast form of an alloy comprising as essential elements boron 0.25% to 5%, metal selected from the group tungsten, molybdenum and uranium 5% to 30%, chromium 1% to 25%, vanadium 0.50% to 5%, cobalt.l5% to 40%, the balance substantially all iron, except for minor amounts of incidental impurities in which carbon does not exceed approximately 0.70%; said cast form being characterized by a relatively fine and uniform grain structure, and being'further characterized by being responsive to thermal treatment for the regulation of hardness.
- a centrifugally cast form of an alloy comprising as essential elements boron 0.25% to5 tungsten 5% to 30%, chromium 1% to 25%, vanadium. 0.50% to 5%, cobalt 15% to 40%, the balance substantially all iron, except for minor amounts of incidental impurities in which carbon does not exceed approximately 0.70%; said cast form. being characterized by a relatively fine and uniform grain structure, and being further characterized by being responsive to thermal treatment for the regulation of hardness.
- a centrifugally cast form of an alloy comprising as essential elements boron 0.25% to 5%, molybdenum 5% to 30%, chromium 1% to-25%,vanadium0.50-% to 5%, cobalt 15% to 40%, the balance substantially all iron, except for minor amounts of incidental impurities in which carbon does not exceed approximately 0.70%; said cast form, being characterized by a relatively fine and uniform grain structure, and being further characterized by being responsive to thermal treatment for the regulation of hardness.
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Manufacture, Treatment Of Glass Fibers (AREA)
Description
Patented Nov. 5, 1940 UNETED STATES PATENT No Drawing. Application February 8, 1939, Serial No. 255,242
3 Claims.
The present invention relates to a new andof the alloy produced by ordinary casting methods useful alloy and relates particularly to an alloy containing as essential components metal from the group tungsten, molybdenum and uranium,
5 boron, chromium, cobalt and iron.
An object of the present invention is to provide an alloy having certain physical properties and characteristics which can be developed and controlled by means of thermal treatment, and, further, to provide an alloy having certain characteristics which render it particularly suitable for manufacture in finished or semi-finished forms by means of centrifugal casting.
The alloy of the present invention, in the form 15 of articles produced by means of centrifugal casting, has a combination of physical properties and. characteristics which render it especially valuable for metal cutting tools and many other industrial purposes.
20 I have found through experiment that by alloying or otherwise intimately combining boron, tungsten, chromium, vanadium, cobalt and iron within the range of boron 0.25% to 5%, tungsten 5% to 30%, chromium 1% to 25%, vanadium 25 0.50% to 5%, cobalt 5% to 40% and iron substantially the balance, that I obtain metallic compositions which possess a combination of valuable physical properties and characteristics. An important essential characteristic of the present in- 30 vention is that the alloy is adapted for the production of forms by means of centrifugal casting. Another advantage is that such cast forms are readily amenable to thermal treatment for the modification and control of important physical 35 properties.
I have found that the presence of boron in the present composition has a marked and beneficial effect upon certain physical and mechanical properties. For example, the cutting efficiency 40 of tools composed of the alloy is, in a large measure, directly dependent upon the percentage of boron in the alloy. The maximum degree of hardness which can be developed in the alloy can be regulated over a comparatively wide range by 45 varying the boron content.
I have found that one of the most important and valuable efiects of boron is that it renders the alloy highly resistant to deformation from impact or compression at both normal and ele- 50 vated temperatures.
Ingots or other forms of the alloy disclosed herein cannot be economically forged or rolled. This characteristic is apparently due in part to the inherent resistance to deformation possessed 55 by the alloy, and also to the fact that ingots, etc.,
have a relatively coarse structure which includes irregular shaped masses of a hard and brittle segregate. Investigation indicates that this segregate contains a relatively high percentage of boron, and that it is not amenable to reduction in size by forging or other mechanical means.
I have found that it is virtually impossible to dissolve all or an appreciable percentage of such boron containing segregates in the other constituent or constituents of the aggregate at a temperature lower than the approximate melting point of the hard segregate.
I have also found that it is virtually impossible to produce commercially satisfactory shapes or forms of the alloy by means of gravity casting. Such castings do not have the requisite density, nor do they have a uniform grain structure. In general the physical structure of castings produced by gravity methods is such that the alloys are not suitable for use as metal cutting tools.
I have discovered that by applying suitable pressure to the molten alloy while it is in the mold, that I can produce cast forms having a relatively high density and requisite physical structure. I have found that while various methods may be used for developing the necessary degree of pressure, that centrifugal casting ofiers an entirely satisfactory and economical means of manufacturing cast forms of the present composition. I have found that by means of centrifugal casting I can increase the density of cast forms of this alloy from 15% to 25% over the density values of forms cast by gravity methods. Another important advantage is that centrifugally cast forms have, in general, an unusually uniform physical structure and are quite free from massive segregates of hard and brittle constituents.
Cast bodies of the alloy produced by centrifugal 40 casting may be utilized in the as cast condition. However, I usually prefer to subject the castings to a suitable thermal treatment before using them for metal cutting tools.
I have found by research that the preferred structure of an aggregate of the present composition comprises at least two principal constituents: (a) a relatively hard, intermetallic compound of boron with one or more of the other essential components; and (b) a solid solution of two or more of the essential components, which has a lower degree of hardness and functions as a matrix. For certain uses, an appreciable percentage of the intermetallic boron compound should be in the form of more or less finely 5 divided particles dispersed throughout the matrix. An aggregate having the preferred physical structure possesses a combination of essential physical properties superior to the properties of a cast aggregate which has not been subjected to ther mal treatment. The present alloy is amenable to thermal treatment for the development of precipitation hardening.
A distinctive characteristic of a body of the alloy which has been subjected to a suitable thermal treatment is the combination of relatively high hardness, e. g., 63 to Rockwell C, and high resistance to impact. Another important property is that virtually all of the values of hardness and resistance to impact developed by thermal treatment are retained when the alloy is subjected to temperatures up to approximately 600 C.
Although I usually prefer to have the alloy composed substantially of boron, tungsten, chromium, vanadium, cobalt and iron within the percentages specified herein, I have found that tungsten can be supplanted, in whole or in part, by molybdenum, uranium or both.
Specific examples of the compositions within the scope of the present invention, which I have found to be valuable for various industrial purposes, are the following: Boron 0.60%, tungsten 14%, chromium 3.80%, vanadium 1.00%, cobalt 16%, iron substantially the balance; boron 0.85%, molybdenum 12%, chormium 4%, vanadium 2%, cobalt 25%, iron substantially the balance; boron 0.95%, molybdenum 8%, tungsten 6%, chromium 3.50%, vanadium 1.60%, cobalt 30%, iron substantially the balance.
I prefer to have the alloys of the present invention as reasonably free from carbon as commercial manufacturing conditions permit. I have found that certain of the metals and alloys used in producing the present compositions generally contain. varying amounts of carbon as an impurity and, consequently, the alloys of the present invention will usually contain small amounts of carbon in the nature of an impurity incidental to manufacture. It is essential to restrict the percentage of carbon so present to an amount which will not be adversely effective on the important physical properties. I have found that carbon may be present in amounts as high as approximately 0.70% without seriously affecting the value of the alloy for various uses.
Furthermore, various materials used in producing this alloy frequently contain other elements such, for example, as manganese, silicon,
etc., more or less in the nature of impurities. Therefore the alloy of this invention may contain small amounts of elements other than carbon in the nature of incidental impurities.
t will be understood therefore that the composition of the present invention comprises the following essential components; boron 0.25% to 5%, metal selected from the group tungsten, molybdenum and uranium. 5% to 30%, chromium 1% to 25%, vanadium 0.50% to 5%, cobalt 15% to 40%, and the balance substantially iron except for minor amounts of incidental impurities in which carbon when present, will not exceed approximately 0.70%.
I claim:
1. As a new article of manufacture, a centrifugally cast form of an alloy comprising as essential elements boron 0.25% to 5%, metal selected from the group tungsten, molybdenum and uranium 5% to 30%, chromium 1% to 25%, vanadium 0.50% to 5%, cobalt.l5% to 40%, the balance substantially all iron, except for minor amounts of incidental impurities in which carbon does not exceed approximately 0.70%; said cast form being characterized by a relatively fine and uniform grain structure, and being'further characterized by being responsive to thermal treatment for the regulation of hardness.
2. As a new article of manufacture, a centrifugally cast form of an alloy comprising as essential elements boron 0.25% to5 tungsten 5% to 30%, chromium 1% to 25%, vanadium. 0.50% to 5%, cobalt 15% to 40%, the balance substantially all iron, except for minor amounts of incidental impurities in which carbon does not exceed approximately 0.70%; said cast form. being characterized by a relatively fine and uniform grain structure, and being further characterized by being responsive to thermal treatment for the regulation of hardness.
3. As a new article of manufacture, a centrifugally cast form of an alloy comprising as essential elements boron 0.25% to 5%, molybdenum 5% to 30%, chromium 1% to-25%,vanadium0.50-% to 5%, cobalt 15% to 40%, the balance substantially all iron, except for minor amounts of incidental impurities in which carbon does not exceed approximately 0.70%; said cast form, being characterized by a relatively fine and uniform grain structure, and being further characterized by being responsive to thermal treatment for the regulation of hardness.
ANTHONY G. DE GOLYER.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US255242A US2220084A (en) | 1939-02-08 | 1939-02-08 | Alloy |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US255242A US2220084A (en) | 1939-02-08 | 1939-02-08 | Alloy |
Publications (1)
Publication Number | Publication Date |
---|---|
US2220084A true US2220084A (en) | 1940-11-05 |
Family
ID=22967458
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US255242A Expired - Lifetime US2220084A (en) | 1939-02-08 | 1939-02-08 | Alloy |
Country Status (1)
Country | Link |
---|---|
US (1) | US2220084A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2756489A (en) * | 1946-05-03 | 1956-07-31 | Howard E Morris | Metal alloy |
US3012880A (en) * | 1960-11-28 | 1961-12-12 | Union Carbide Corp | Iron-base alloy |
US3035934A (en) * | 1957-05-13 | 1962-05-22 | Coast Metals Inc | Application of cobalt-base alloys to metal parts |
-
1939
- 1939-02-08 US US255242A patent/US2220084A/en not_active Expired - Lifetime
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2756489A (en) * | 1946-05-03 | 1956-07-31 | Howard E Morris | Metal alloy |
US3035934A (en) * | 1957-05-13 | 1962-05-22 | Coast Metals Inc | Application of cobalt-base alloys to metal parts |
US3012880A (en) * | 1960-11-28 | 1961-12-12 | Union Carbide Corp | Iron-base alloy |
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