US2104980A - Steel alloy - Google Patents
Steel alloy Download PDFInfo
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- US2104980A US2104980A US67069A US6706936A US2104980A US 2104980 A US2104980 A US 2104980A US 67069 A US67069 A US 67069A US 6706936 A US6706936 A US 6706936A US 2104980 A US2104980 A US 2104980A
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- molybdenum
- alloy
- nickel
- steel
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- 229910000851 Alloy steel Inorganic materials 0.000 title description 15
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 46
- 229910000831 Steel Inorganic materials 0.000 description 29
- 235000019589 hardness Nutrition 0.000 description 29
- 239000010959 steel Substances 0.000 description 29
- 229910045601 alloy Inorganic materials 0.000 description 25
- 239000000956 alloy Substances 0.000 description 25
- 229910052750 molybdenum Inorganic materials 0.000 description 24
- 239000011733 molybdenum Substances 0.000 description 24
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 23
- ZOKXTWBITQBERF-UHFFFAOYSA-N Molybdenum Chemical compound [Mo] ZOKXTWBITQBERF-UHFFFAOYSA-N 0.000 description 23
- 229910052802 copper Inorganic materials 0.000 description 23
- 239000010949 copper Substances 0.000 description 23
- 229910052759 nickel Inorganic materials 0.000 description 23
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 22
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 20
- 229910052799 carbon Inorganic materials 0.000 description 20
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 description 19
- 229910052804 chromium Inorganic materials 0.000 description 19
- 239000011651 chromium Substances 0.000 description 19
- 238000005242 forging Methods 0.000 description 14
- 229910052742 iron Inorganic materials 0.000 description 11
- 238000010438 heat treatment Methods 0.000 description 10
- 238000004519 manufacturing process Methods 0.000 description 9
- 238000000034 method Methods 0.000 description 9
- 238000001816 cooling Methods 0.000 description 8
- 238000005275 alloying Methods 0.000 description 5
- 229910052751 metal Inorganic materials 0.000 description 5
- 239000002184 metal Substances 0.000 description 5
- 230000007547 defect Effects 0.000 description 4
- 230000008569 process Effects 0.000 description 4
- PWHULOQIROXLJO-UHFFFAOYSA-N Manganese Chemical compound [Mn] PWHULOQIROXLJO-UHFFFAOYSA-N 0.000 description 3
- 238000005336 cracking Methods 0.000 description 3
- 229910052748 manganese Inorganic materials 0.000 description 3
- 239000011572 manganese Substances 0.000 description 3
- 238000005406 washing Methods 0.000 description 3
- 238000005096 rolling process Methods 0.000 description 2
- 238000005204 segregation Methods 0.000 description 2
- 230000035939 shock Effects 0.000 description 2
- 229910052710 silicon Inorganic materials 0.000 description 2
- 239000010703 silicon Substances 0.000 description 2
- 229910000846 In alloy Inorganic materials 0.000 description 1
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 1
- 238000005299 abrasion Methods 0.000 description 1
- 230000009471 action Effects 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- OGSYQYXYGXIQFH-UHFFFAOYSA-N chromium molybdenum nickel Chemical compound [Cr].[Ni].[Mo] OGSYQYXYGXIQFH-UHFFFAOYSA-N 0.000 description 1
- 229910017052 cobalt Inorganic materials 0.000 description 1
- 239000010941 cobalt Substances 0.000 description 1
- GUTLYIVDDKVIGB-UHFFFAOYSA-N cobalt atom Chemical compound [Co] GUTLYIVDDKVIGB-UHFFFAOYSA-N 0.000 description 1
- 238000005520 cutting process Methods 0.000 description 1
- 238000001514 detection method Methods 0.000 description 1
- 230000006866 deterioration Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 239000000835 fiber Substances 0.000 description 1
- -1 however Substances 0.000 description 1
- 230000006872 improvement Effects 0.000 description 1
- 239000007788 liquid Substances 0.000 description 1
- 238000003754 machining Methods 0.000 description 1
- 239000000155 melt Substances 0.000 description 1
- 150000002739 metals Chemical class 0.000 description 1
- 238000010791 quenching Methods 0.000 description 1
- 230000000171 quenching effect Effects 0.000 description 1
- 230000009467 reduction Effects 0.000 description 1
- 239000010936 titanium Substances 0.000 description 1
- 229910052719 titanium Inorganic materials 0.000 description 1
- 238000011282 treatment Methods 0.000 description 1
- WFKWXMTUELFFGS-UHFFFAOYSA-N tungsten Chemical compound [W] WFKWXMTUELFFGS-UHFFFAOYSA-N 0.000 description 1
- 229910052721 tungsten Inorganic materials 0.000 description 1
- 239000010937 tungsten Substances 0.000 description 1
- 229910052720 vanadium Inorganic materials 0.000 description 1
- LEONUFNNVUYDNQ-UHFFFAOYSA-N vanadium atom Chemical compound [V] LEONUFNNVUYDNQ-UHFFFAOYSA-N 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
- C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
- C22C38/40—Ferrous alloys, e.g. steel alloys containing chromium with nickel
- C22C38/44—Ferrous alloys, e.g. steel alloys containing chromium with nickel with molybdenum or tungsten
Definitions
- This invention relates to steel alloys which are particularly adapted for use in pieces of relatively large or heavy sections such as die blocks used for hot work forging processes, and other steel lo the tendency to develop internal thermal ruptures or cracks is practically eliminated, and the resulting piece is capable of being hardened to a substantially uniform hardness throughout its mass by proper heat treatment.
- the present invention is an improvement over my prior United States Letters Patent No. 1,464,174 issued August 7, 1923, in which the principal alloying elements are chromium, nickel and molybdenum. Alloy steels made in accordance with this patent have demonstrated their superiority for hot work dies and similar forging work. At present, approximately ninety per cent of the dies used in the drop forging industry are made from chromium-nickel-molybdenum steel 35 alloy in one or another of its various forms.
- the method in general consists of heating the metal (usually steel) to a plastic condition and forming it in dies which contain the desired shape in negative.
- the dies are operated by powerful hammers in the case of drop forging, and by forging machines in the case of upsetting.
- the dies In order that the drop forger may do his job well and profitably, his dies must produce thousands of duplicate parts without any great wear or deterioration. This'calls for a die steel having great strength and durability. since the dies are subjected to extremely heavy shocks and high temperatures.
- the dies are usually furnished to the drop forger in the form of blocks in either the annealed or tempered condition. If annealed, the dies must be hardened and tempered after being, machined. If tempered, the dies are used in the hammer immediately after machining without further heat treatment.
- the block is heattreated in the rough condition by the die block 5 manufacturer, then machined by the die maker, and then put to use by the forger without further heat-treatment. After the initial die impression is worn out from use, it is machined off the die block, and a new impression remachined in the fresh metal surface of the block, and the block is used again without further heat-treatment. This remachining operation may be repeated several times, often as many as seven times, until the blockbecomes too thin for economical use.
- Thermal rupture also known as flaking
- center porosity which occurs in a wide variety of metals, in the form of small voids and segregations.
- Thermal rupture consists in the formation of minute cracks which develop on the interior of the heavy mass of metal, when it is cooled from its originalsolidification temperatures. Asthese cracks or flakes are entirely confined to the interior of the block, their presence is practically impossible of detection without cutting into the body of theblock, and even then they sometimes cannot be visually detected unless the exposed surface is etched to show its grain.
- Such alloys may also have nickel in amounts up to 3.00%, manganese in amounts up to 1.00%, and silicon in-amounts up to 1.00%.
- nickel in amounts up to 3.00%
- manganese in amounts up to 1.00%
- silicon in-amounts up to 1.00%.
- Another desirable characteristic heretofore I unattained in steel alloys of the types generally used for die blocks is that of maintaining substantially the same hardness throughout the entire mass of a die block so as to permit several successive "sinkings of dies therein, without requiring re-heat treatments, and without reducing the effectiveness of each such successive die sinking.
- steel die blocks heretofore employed there is usuallya substantial reduction in hardness toward the center of the block, with a resulting loss in production from such softer die faces, and a greater tendency to cracking or breakage of the die due to the variation in hardness from the outside edge to the middle of such center sinkings.
- nickebchromium-molybdenum die steels heretofore used possess the property numbered above 5 to 9, both' inclusive, to'a high degree.
- Other types of steels have been developed having one or'more of these characteristics. I have demonstrated, however, that the alloy of,my present invention combines all of the qualities to an unusual degree never found in any other steels. This is particularly so with the propertiesof resistance to internal thermal ruptures, and complete or uniform hardness at relatively high working hardnesses.
- Manganese in fractions to 1.00% and silicon in fractions to 1.00% may also be present, the remainder being substantially all iron.
- the block was cut through the middle, and hardness readings taken on the cut surface at intervals from the center to all sides thereof. It was found that the hardness was uniform throughout the surface within a total range of .05 mm. Brinell ball diameter at 350 Brinell hardness number. This substantial uniformity is remarkable; greater uniformity than this could hardly be expected, even over the outside surface of the block.
- Nickel-chromium-mo lybdenum alloys The presence of copper seems to be largely responsible for the important properties of resistance to thermal rupture and complete hardenability, as well as increasing the air hardening efiect heretofore noted in nickel-chromium-mo lybdenum alloys and raising their tensile properties. Nickel of 50% or more is necessary to contribute the required toughness. Nickel also helps to overcome the tendency for copper-bearing steels to roughen at the surface or to become hot short during forging or rolling, but I find that the addition of molybdenum in small quantities seems to intensify this action of nickel to a marked degree, thereby reducing the amount of nickel necessary in alloys of this character,
- My alloy can be annealed by heating to above the critical range and cooling slowly in the furnace. Hardening is accomplished by heating to above the critical range and cooling in still air, in an air blast, or'by quenching in a liquid medium. The more rapid the cooling method, the
- the steel may be tem-- pared to the desired point after hardening by the critical range. ing ranges, the hardness will be substantially uniform throughout the mass of the piece.
- a die block for hot forging characterized by its resistance to thermal rupture and substantial uniformity of hardness at working hardnesses, which comprises as its principal alloying elements carbon ranging from .30 to 1.00%, chromium from .25 to 1.25%, molybdenum from .05 to 2.00%, nickel from .50 to 2.50%, and copper from .25 to 4.00%, the remainder being substantially all iron.
- a die block for hot forging characterized by its resistance to thermal rupture and heat checking, and its substantial uniformity of hardness at working hardnesses, which comprises as its principal alloying elements carbon ranging from .30 to 170%, nickel from .50 to 2.50%, chromium from'.25 to 1.25 molybdenum from .05 to 2.00%.
- a steel alloy characterized by itsresistance to thermal rupture, and by substantial uniformity of depth hardening, and containing carbon ranging from .30 to 1.00%, nickel from .50 to 2.50%, chromium from .25 to 1.25%, molybdenum from .05 to 2.00%, copper from .25 to 4.00%, and the balance substantially all iron.
- a steel alloy characterized by its resistance to thermal rupture, and by substantial uniformity of depth hardening, and containingcarbon from .30 to 170%, nickel from .50 to2.50%, molybdenum from .05 to 2.00%, chromium from .25 75 1.25%, copper from .50 to 3.50%, and the balance substantially all iron. 4
- a steel alloy characterized by its resistance to thermal rupture, and by substantial unlform- I for hot forging made of steel alloy characterized by'substantial uniformity of depth hardening and its practical freedom from thermal rupture, said steel alloy containing carbon ranging from .25 to 1.10%, nickel ranging from .50 to 3.00%, chro-, mium ranging from .25 to 1.50%, molybdenum ranging'from .05 to 2.00%, copper ranging from .25 to 6.50%, and thebalance substantially all iron.
- a steel alloy characterized by its resistance to thermal rupture and by substantial uniformity of depth hardening, and containing carbon ranging from .30 to 1.00%, nickel from .50 to 2.50%, chromium from .25 to 1.25% molybdenum from .05 to 2.00%, copper from .25 to 4.00%, and the balance substantially all iron, the molybdenum content varying approximately in inverse proportions to the carbon content.
- a steel alloy characterized by its resistance to thermal rupture and by substantial uniformity of depth hardening, and containing carbon ranging from .30 to 370%, nickel from -.50 to 2.50%, chromium from .25 to 1.25%, molybdenum from .05 to 2.00%, copper from .50 to 3.50%, and the balance substantially all iron, the molybdenum content varying approximately in inverse proportionsto the carbon content.
- a steel alloy characterized by its resistance to thermal rupture and by substantial uniform ity of depth hardening, and containing carbon ranging 'from..25 to 1.10%, nickel from .50 to 3.00%, chromium from .25 to 1.50%, molybdenum from .05 to 2.00%, copper from .25 to 6.00%, and the balance substantially all iron, the molybdenumand chromium contents, respectively,
- '11 A steel alloy characterized by its resistance to thermal rupture and by substantial uniformity of depth hardening, and containing carbon ranging from .30 to 370%, nickel from .50 to 2.50%, chromium from .25 to 1.00%, molybdenum from .05 to 2.00%, copper from .50 to 3.50%, and the balance substantially all iron, the molyba denum and chromium contents, respectively, varying in approximately inverse proportions to the carbon content.
- a new article of manufacture, a tempered die block for hot forging made of steel alloy containing carbon ranging from .25 to 1.10%, nickel from .50 to 2.50%, chromium from .25 to 1.50%, molybdenum from .05 to 2.00%, copper from .25 to 6.50%, and the balance substantially all iron.
- a new article of manufacture, a'tempered die block for hot forging made of steel alloy containing carbon ranging from .30 to .70%, nickel from .50 to 2.50%, chromium from .25 to 1.25%,
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- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Forging (AREA)
Description
Patented Jan. '11, 1938 STEEL ALLOY William F. Finkl, Chicago, 11]., assignor to A.
Finkl & Sons Company, Chicago, 111., a corporation of Illinois No Drawing. Application March 4, 1936.
Serial No. 67,069
13 Claims.
This invention relates to steel alloys which are particularly adapted for use in pieces of relatively large or heavy sections such as die blocks used for hot work forging processes, and other steel lo the tendency to develop internal thermal ruptures or cracks is practically eliminated, and the resulting piece is capable of being hardened to a substantially uniform hardness throughout its mass by proper heat treatment.
The present invention is an improvement over my prior United States Letters Patent No. 1,464,174 issued August 7, 1923, in which the principal alloying elements are chromium, nickel and molybdenum. Alloy steels made in accordance with this patent have demonstrated their superiority for hot work dies and similar forging work. At present, approximately ninety per cent of the dies used in the drop forging industry are made from chromium-nickel-molybdenum steel 35 alloy in one or another of its various forms.
The present application is ,a continuation in part of my prior applications Serial No. 33,331 filed July'26, 1935, and Serial No. 35,104, filed August '7, 1935.
30 Among the many methods of mass production used in modern industry, there are none more important than that of drop forging and its near relation, upsetting. -By these two processes, which may both be referred to generally by the accurately metal parts of surprisingly, intricate design in large quantities with remarkable speed.
The method in general consists of heating the metal (usually steel) to a plastic condition and forming it in dies which contain the desired shape in negative. The dies are operated by powerful hammers in the case of drop forging, and by forging machines in the case of upsetting.
In order that the drop forger may do his job well and profitably, his dies must produce thousands of duplicate parts without any great wear or deterioration. This'calls for a die steel having great strength and durability. since the dies are subjected to extremely heavy shocks and high temperatures. The dies are usually furnished to the drop forger in the form of blocks in either the annealed or tempered condition. If annealed, the dies must be hardened and tempered after being, machined. If tempered, the dies are used in the hammer immediately after machining without further heat treatment.
Over 60% of the dies used in the industry today are thus tempered. The block is heattreated in the rough condition by the die block 5 manufacturer, then machined by the die maker, and then put to use by the forger without further heat-treatment. After the initial die impression is worn out from use, it is machined off the die block, and a new impression remachined in the fresh metal surface of the block, and the block is used again without further heat-treatment. This remachining operation may be repeated several times, often as many as seven times, until the blockbecomes too thin for economical use.
One of the principal difliculties encountered by the manufacturers of alloy steels of the nickelchromium-molybdenum class is that of avoiding thermal ruptures when the alloy is first produced at the mill. Thermal rupture (also known as flaking) should not be confused with "center porosity" which occurs in a wide variety of metals, in the form of small voids and segregations. Thermal rupture consists in the formation of minute cracks which develop on the interior of the heavy mass of metal, when it is cooled from its originalsolidification temperatures. Asthese cracks or flakes are entirely confined to the interior of the block, their presence is practically impossible of detection without cutting into the body of theblock, and even then they sometimes cannot be visually detected unless the exposed surface is etched to show its grain. Hence such ruptures will not usually become apparent until after the block has been rough-machined, and perhaps given its final heat treatment, The defect may not even be discovered when the first impression or die is cut, but such defects soon show up when in the hammer, and the particular piece is rendered useless as a die-block. In instances where such alloys are used for heavy structural purposes, the defect usually does not become. evident until an unexpected failure or breakage occurs.
The exact cause of thermal ruptures or flaking does not seem to havebeen definitely ascertained, and heretofore the only practical method of control has been through great care in the manufacture of alloy steels of this general character 50 whereby cooling of the massive sections from their original rolling or forging temperatures is carefully retarded in cooling pits by various methods well known to those skilled in the art. But
'even such great care in cooling has provedin- 55 sufllcient to eliminate frequent recurrence: of
. Per cent Carbon .25 to 1.10 Chromium .25 to 1.50 Molybdenum .05 to 2.00 Copper .25 to 6.50
Such alloys may also have nickel in amounts up to 3.00%, manganese in amounts up to 1.00%, and silicon in-amounts up to 1.00%. In alloy steels coming within the above ranges having copper added in the amounts indicated, the tendency to thermal ruptures or flaking can be effectively controlled so as to greatly reduce the care in handling these steels during their manufacture, and thereby insin'ing practical freedom from such internal defects.
Another desirable characteristic heretofore I unattained in steel alloys of the types generally used for die blocks, is that of maintaining substantially the same hardness throughout the entire mass of a die block so as to permit several successive "sinkings of dies therein, without requiring re-heat treatments, and without reducing the effectiveness of each such successive die sinking. In steel die blocks heretofore employed, there is usuallya substantial reduction in hardness toward the center of the block, with a resulting loss in production from such softer die faces, and a greater tendency to cracking or breakage of the die due to the variation in hardness from the outside edge to the middle of such center sinkings.
I findthat the'addition of copper in certain proportions to alloy steels used in die blocks or similar heavy-sectioned masses gives "a substantially uniform depth of hardnesses at die-working values, which uniformity of hardness has hitherto been considered unattainable. further that the addition of copper appreciably increases resistance to checking or surface cracking from heat, which are also common faults of alloy die steels used in hot work.
Summarizing the ideal requirements for a hot work die steel, it must have the following properties to a marked degree:
l. Resistance to internal thermal crackingduring cooling from high temperatures.
2. Complete hardenability. in large sections (the ability to harden with complete pniformity -of hardness throughout the mass of the piece).
3. Resistance to heat cracking (surface crackingduetoheat).
4. Resistance to washing (localized wear). l 5. Ease and simplicity of manufacture in either the open hearth or electric furnace processes to produce sound'ingots and billets with practically the total absence of segregation, center porosity, and hot shortness.
6. Easy forgeability into the necessary size and shape.
7. Simple heat treatment to required 'hardness.
8. Great strength and density of fibre combined with high ductibility and high values.
9. Machinability at high (working) hardnesses.
The importance of properties Nos. 1 and 2 has already been set; forth. Alloy steels heretofore employed in heavy sections for die block purposes are especially subject to internal rupture cracks or flaking. Property No. 2 is most'important in a tempered die block, whereas successive recuts or sinkings are made, the center of the block is approached and used. In most impact die steels that have been hardened, the hardness w drops off toward the center of the block.
As to properties Nos. 3 and 4, these are opposing characteristics. When the die is too soft it will wash, when too hard it may heat-check. A compromise hardness where these opposite faults are at a minimum is usually necessary.-
Obviously a steel that will resist heat-checking at any and all hardnesses is the ideal, since washing may be overcome by simply raising the hardness sufliciently.
Property No. 5.-In the .large sizes in which the'modern die block is made, it is important that the total alloy content be low, since the higher this content goes the more diflicult it is to produce sound ingots in such large sizes.
Property No. 6.It is obvious that to produce die blocks commercially, the steel must be readil y forged. This is another reason for low alloy content. In general, the higher the alloy content, the greater are the difficulties in forging.
Property No. 7.-Heat treating processes are expensive in their simplest forms, and therefore complicated treatments are to be avoided.
Property No. 8.Die blocks must undergo ex- .treme. conditions of shock, heat and abrasion, a
combination of opposing conditions very difl'icult to meet.
Property No. 9.In the tempered die block it is necessary to leave the steel atthe relatively high hardness suitable for use as a die, 'yet it must be machinable at this high'hardness.
The nickebchromium-molybdenum die steels heretofore used possess the property numbered above 5 to 9, both' inclusive, to'a high degree. Other types of steels, of course, have been developed having one or'more of these characteristics. I have demonstrated, however, that the alloy of,my present invention combines all of the qualities to an unusual degree never found in any other steels. This is particularly so with the propertiesof resistance to internal thermal ruptures, and complete or uniform hardness at relatively high working hardnesses. X
Referring now' more' specifically to the analysis of die block steels in which substantial uniformity of hardness at high working hardnesses is desired, together with the other desirable properties of such steels hereinbefore listed, I find that theranges of the principal alloying elements should be restricted, substantially as follows:
v I Per cent Carbon .30 to 1.00 phromium nun .25 to 1.25 Molybdenum .05 to 2.00 Nickel .50 to 2.50 Copper .25 to 4.00
Manganese in fractions to 1.00% and silicon in fractions to 1.00% may also be present, the remainder being substantially all iron.
- I find that the addition of certain other e1ements commonly used in special alloys such as tungsten, cobalt, vanadium, or titanium seem to have no appreciable effect in improving the alloy Per cent Carbon .30 to .70 Nickel .50 to 2.50 Chromium. .25 to 1.25 Molybdenum .05 to 2.00 Copper .50 to 3.50
The ranges above specified are critical to the economical production of a hot work die steel having the nine necessary characteristics-mentioned above toan exceptional degree. Of particular importance is its remarkable resistance to thermal rupture, or flaking, its complete or uniform hardenability at working hardnesses, and its resistance to heat-checking.
I have yet to encounter thermal ruptures or flakes in the many melts of this improved alloy so far prepared, even though in some instances deliberate attempts have been made to produce them. This characteristic, therefore, permits less expensive methods of handling during fabrication from the ingot to the billet, and ultimately to the die block.- It also shortens the time required for cooling the steel, andthus saves in the Per cent Carbon .50 Manganese .75 Chromium .75 Copper 2.00 Nickel 1.00 Molybdenum .25
The block was cut through the middle, and hardness readings taken on the cut surface at intervals from the center to all sides thereof. It was found that the hardness was uniform throughout the surface within a total range of .05 mm. Brinell ball diameter at 350 Brinell hardness number. This substantial uniformity is remarkable; greater uniformity than this could hardly be expected, even over the outside surface of the block.
The improvedresistance to heat checking noted in the alloy makes it possible to employ a higher hardness than normal, thus improving resistance to washing. In those applications to dies in which this alloy has been used, heat checking has been practically unknown.
The presence of copper seems to be largely responsible for the important properties of resistance to thermal rupture and complete hardenability, as well as increasing the air hardening efiect heretofore noted in nickel-chromium-mo lybdenum alloys and raising their tensile properties. Nickel of 50% or more is necessary to contribute the required toughness. Nickel also helps to overcome the tendency for copper-bearing steels to roughen at the surface or to become hot short during forging or rolling, but I find that the addition of molybdenum in small quantities seems to intensify this action of nickel to a marked degree, thereby reducing the amount of nickel necessary in alloys of this character,
and also making it possible to use more copper with its attendant advantages. Over 2.50% nickel makes the steel difficult to fabricate and adds greatly to the expense of the alloy.
The air hardening qualities of my improved alloy appear to follow substantially the same laws disclosed in my prior Patent No. 1,464,174
in so far as variation in the principal alloying' elements is concerned. That is to say, superior air hardening qualities may be maintained by varying the carbon content inversely with the chromium or molybdenum content, and the amount of chromium and molybdenum may also be varied inversely with each other within the ranges indicated. In the present improved alloy, however, copper can be used to produce a more economical product by partially replacing both the nickel and molybdenum, and with the new and added results of resistance to thermal rupture, and greatly increased uniformity of hardening.
My alloy can be annealed by heating to above the critical range and cooling slowly in the furnace. Hardening is accomplished by heating to above the critical range and cooling in still air, in an air blast, or'by quenching in a liquid medium. The more rapid the cooling method, the
harder will be the steel. The steel may be tem-- pared to the desired point after hardening by the critical range. ing ranges, the hardness will be substantially uniform throughout the mass of the piece.
I claim as my invention:
1. A die block for hot forging characterized by its resistance to thermal rupture and substantial uniformity of hardness at working hardnesses, which comprises as its principal alloying elements carbon ranging from .30 to 1.00%, chromium from .25 to 1.25%, molybdenum from .05 to 2.00%, nickel from .50 to 2.50%, and copper from .25 to 4.00%, the remainder being substantially all iron.
2. A die block for hot forging characterized by its resistance to thermal rupture and heat checking, and its substantial uniformity of hardness at working hardnesses, which comprises as its principal alloying elements carbon ranging from .30 to 170%, nickel from .50 to 2.50%, chromium from'.25 to 1.25 molybdenum from .05 to 2.00%.
and copper from .50 to 3.50%, and the balance 5 to thermal rupture, and by substantial uniformity of depth hardening, and containing carbon ranging from .25 to 1.10%, nickel from .50 to 3.00%, chromium from .25 to 1.50%, molybdenum from .05 to 2.00%, copper from .25 to 6.50%, and the balance substantially all iron.
4. A steel alloy characterized by itsresistance to thermal rupture, and by substantial uniformity of depth hardening, and containing carbon ranging from .30 to 1.00%, nickel from .50 to 2.50%, chromium from .25 to 1.25%, molybdenum from .05 to 2.00%, copper from .25 to 4.00%, and the balance substantially all iron.
'5. A steel alloy characterized by its resistance to thermal rupture, and by substantial uniformity of depth hardening, and containingcarbon from .30 to 170%, nickel from .50 to2.50%, molybdenum from .05 to 2.00%, chromium from .25 75 1.25%, copper from .50 to 3.50%, and the balance substantially all iron. 4
6. A steel alloy characterized by its resistance to thermal rupture, and by substantial unlform- I for hot forging made of steel alloy characterized by'substantial uniformity of depth hardening and its practical freedom from thermal rupture, said steel alloy containing carbon ranging from .25 to 1.10%, nickel ranging from .50 to 3.00%, chro-, mium ranging from .25 to 1.50%, molybdenum ranging'from .05 to 2.00%, copper ranging from .25 to 6.50%, and thebalance substantially all iron.
8. A steel alloy characterized by its resistance to thermal rupture and by substantial uniformity of depth hardening, and containing carbon ranging from .30 to 1.00%, nickel from .50 to 2.50%, chromium from .25 to 1.25% molybdenum from .05 to 2.00%, copper from .25 to 4.00%, and the balance substantially all iron, the molybdenum content varying approximately in inverse proportions to the carbon content.
9. A steel alloy characterized by its resistance to thermal rupture and by substantial uniformity of depth hardening, and containing carbon ranging from .30 to 370%, nickel from -.50 to 2.50%, chromium from .25 to 1.25%, molybdenum from .05 to 2.00%, copper from .50 to 3.50%, and the balance substantially all iron, the molybdenum content varying approximately in inverse proportionsto the carbon content.
10. A steel alloy characterized by its resistance to thermal rupture and by substantial uniform ity of depth hardening, and containing carbon ranging 'from..25 to 1.10%, nickel from .50 to 3.00%, chromium from .25 to 1.50%, molybdenum from .05 to 2.00%, copper from .25 to 6.00%, and the balance substantially all iron, the molybdenumand chromium contents, respectively,
varying in approximately inverse proportions to the carbon content.
'11 A steel alloy characterized by its resistance to thermal rupture and by substantial uniformity of depth hardening, and containing carbon ranging from .30 to 370%, nickel from .50 to 2.50%, chromium from .25 to 1.00%, molybdenum from .05 to 2.00%, copper from .50 to 3.50%, and the balance substantially all iron, the molyba denum and chromium contents, respectively, varying in approximately inverse proportions to the carbon content.
12. A new article of manufacture, a tempered die block for hot forging made of steel alloy containing carbon ranging from .25 to 1.10%, nickel from .50 to 2.50%, chromium from .25 to 1.50%, molybdenum from .05 to 2.00%, copper from .25 to 6.50%, and the balance substantially all iron.
13. A new article of manufacture, a'tempered die block for hot forging made of steel alloy containing carbon ranging from .30 to .70%, nickel from .50 to 2.50%, chromium from .25 to 1.25%,
molybdenum from .05 to 2.00%, and copper from V
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US67069A US2104980A (en) | 1936-03-04 | 1936-03-04 | Steel alloy |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US67069A US2104980A (en) | 1936-03-04 | 1936-03-04 | Steel alloy |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US2104980A true US2104980A (en) | 1938-01-11 |
Family
ID=22073518
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US67069A Expired - Lifetime US2104980A (en) | 1936-03-04 | 1936-03-04 | Steel alloy |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US2104980A (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2676098A (en) * | 1951-04-06 | 1954-04-20 | Crucible Steel Co America | Drill rod steel and articles thereof |
| US2950968A (en) * | 1957-05-31 | 1960-08-30 | Carpenter Steel Co | Deep-hardened alloy steel having improved impact strength |
| US4253874A (en) * | 1976-11-05 | 1981-03-03 | British Steel Corporation | Alloys steel powders |
-
1936
- 1936-03-04 US US67069A patent/US2104980A/en not_active Expired - Lifetime
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2676098A (en) * | 1951-04-06 | 1954-04-20 | Crucible Steel Co America | Drill rod steel and articles thereof |
| US2950968A (en) * | 1957-05-31 | 1960-08-30 | Carpenter Steel Co | Deep-hardened alloy steel having improved impact strength |
| US4253874A (en) * | 1976-11-05 | 1981-03-03 | British Steel Corporation | Alloys steel powders |
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