CN110029284A - A kind of molybdenum toughening cast iron and its manufacture and heat treatment method - Google Patents
A kind of molybdenum toughening cast iron and its manufacture and heat treatment method Download PDFInfo
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- CN110029284A CN110029284A CN201910431573.2A CN201910431573A CN110029284A CN 110029284 A CN110029284 A CN 110029284A CN 201910431573 A CN201910431573 A CN 201910431573A CN 110029284 A CN110029284 A CN 110029284A
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- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D1/00—General methods or devices for heat treatment, e.g. annealing, hardening, quenching or tempering
- C21D1/18—Hardening; Quenching with or without subsequent tempering
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- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
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- C22C33/00—Making ferrous alloys
- C22C33/04—Making ferrous alloys by melting
- C22C33/06—Making ferrous alloys by melting using master alloys
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- 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
- C22C38/02—Ferrous alloys, e.g. steel alloys containing silicon
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- 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
- C22C38/04—Ferrous alloys, e.g. steel alloys containing manganese
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- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
- C22C38/22—Ferrous alloys, e.g. steel alloys containing chromium with molybdenum or tungsten
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- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
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- C22C38/00—Ferrous alloys, e.g. steel alloys
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- C22C38/24—Ferrous alloys, e.g. steel alloys containing chromium with vanadium
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- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
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- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
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- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
- C22C38/32—Ferrous alloys, e.g. steel alloys containing chromium with boron
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Abstract
A kind of molybdenum toughening cast iron and its casting and heat treatment method method, the mass content of alloy each element is Cr:9.0~13.0, B:2.6~2.9, C:0.7~0.9, Mo:1.8~3.0%, Nb:0.4~0.8, V:0.4~0.8, content of the content of Mn less than 0.3, Si is less than 0.07, surplus Fe；Wherein C and B:3.3~3.6；C/Cr content ratio: 0.06~0.08；Nb and V:0.5~1.0.Raw material is melted at 1500~1550 DEG C, then is down to 1280~1350 DEG C, with fine aluminium deoxidation；Heat preservation 5~10 minutes, in 1230~1280 DEG C of cast alloys.Ingot casting hardness of the present invention HRC67.0~70.8,12.6~18.0J/cm2 of impact flexibility, 1280~1600MPa of bending strength.
Description
Technical field
The invention belongs to high-hardness and wear-resistant cast-iron field, it is related to a kind of refractory metal molybdenum element toughening hard phase and supersaturation
Solid solution, martensitic matrix phase wear and corrosion resistant cast iron alloy and its casting, heat treatment method, can be widely used for electric power, smelting
Mechanical wearing piece manufacture in the industries such as gold, machinery, chemical industry.
Technical background
Fe-Cr-B-C abrasion resistant casting alloy is with Fe2B or M2B hard phase is hard phase, has good toughness and height hard
Degree, high corrosion-resistant, melting-casting manufacturability is good, has very wide application prospect.
Patent document 1: 105695884 B of Authorization Notice No. CN, the antifriction alloy hardness of preparation are HRC66~70, punching
Hit 4~9J/cm of toughness2.The hardness of such alloy is higher, but impact flexibility is insufficient, and intensity index is lower, and bending strength is lower,
In 346~477MPa range, therefore limit the field that the Alloyapplication is big in some external loads, impact resistance is needed to act on
It closes.
Also, when preparing large scale specification (thickness is greater than 30mm) and complex-shaped casting, it may appear that crack due to thermal stress,
And there is the phenomenon that hardness is unevenly distributed.It is ground used in the equipment such as large-scale Raymond mill bed, ore crusher, Pulp pump
The wearing pieces such as ball, liner plate, tup, tooth plate, flow passage part, impeller, it is bulky, it is complex-shaped, therefore used by patent document 1
Process limits the application of the alloy.
Document 2: the rapid cooling microstructure and property of eutectic Fe-Cr-B-C alloy, casting, 2017,66 (10): 1053~1056.
The rapid cooling tissue of as cast condition Fe-Cr-B-C alloy by martensite+retained austenite matrix and along the continuous net-shaped distribution of crystal boundary (Fe,
Cr)2(B,C)+(Fe,Cr)23(B,C)6Hard phase composition.The microhardness of rapid cooling tissue matrix phase is 800~880HV, hard
Phase microhardness is 1150~1400HV, macrohardness HRC68, and impact flexibility reaches 13.6J/cm2；And through 960 DEG C × 2h
After annealing, matrix is changed into ferrite and nodular cementite, hard phase (Fe, Cr)2(B, C) and (Fe, Cr)23(B,C)6It is few
There is suspension, cenotype (Fe, Cr) occur in amount dissolution, regional area3(B, C), after annealing matrix phase microhardness be 330~
400HV, hard phase are 850~1250HV, and macrohardness is reduced to HRC46, and impact flexibility is reduced to 3.4J/cm2。
2 acquired results of document reflect that the hardness of matrix phase plays significant role to the hardness and impact flexibility of such material；
Patent document 1 is compared, there are also the possibility promoted in aspect of performance such as impact flexibility for such alloy.
Summary of the invention
A kind of molybdenum toughening cast iron and its manufacture and heat treatment method, the alloy is with Fe2B or M2B is hard phase, addition Mo member
Element, segregation forms SS phase in hard phase, it is suppressed that hard phase crystal grain is grown up, and hard phase is hindered to form continuous net-shaped structure；
By heat treatment, forming the non-equilibrium phases such as multielement supersaturated solid solution, martensite is matrix.So that alloy is keeping high
While hardness, toughness and intensity are greatly improved, to have broader practice prospect.
High-wearing feature that the present invention selects, high corrosion-resistant Fe-Cr-B-C alloy are basic alloy, then add 1.0~
2.0wt.%Mo element.The multi-element eutectic alloy containing elements such as Fe, Cr, B, C, Nb, V, Mo is formed, the quality percentage of each element contains
Amount is Cr:9.0~13.0, B:2.6~2.9, C:0.7~0.9, Mo:1.0~2.0, Nb:0.4~0.8, V:0.4~0.8, Mn
Content of the content less than 0.3, Si less than 0.07, S, P :≤0.01, surplus Fe.Wherein C, B summation: 3.3~3.6；C/Cr
Content ratio: 0.06~0.08；The summation of Nb, V are 0.5~1.0.
Mo is that the affinity of carbide, i.e. Mo and C is larger.With SS phase shape in Ti (C, N) based ceramic metal
Similar at mechanism, Mo element can be with Fe2Among hard phase based on B or neighbouring segregation, formation chemical formula are similar to (Mo, Fe)x
(B, C), the transition tissue of x=2~3 prevent hard phase from forming continuous net-shaped structure or partial partition to refine hard phase
Hard phase is directly connected to matrix phase, to improve the toughness and intensity of alloy.
Since Mo element specific gravity is larger, it is easy to produce gross segregation in melting, in the tough alloy of introducing Mo element,
The content of Mo is unsuitable excessively high, and Mo content of the present invention should control within the scope of 1.0~2.0wt.%.
Referring to patent document 1, specifically prepare alloy when, can be used ferrochrome (high-carbon, middle carbon, micro- carbon), ferro-boron, ferro-niobium,
Vanadium iron, molybdenum-iron and pure iron etc. are according to component requirements ingredient.Raw material and its composition are listed in table 1.
Table 1 can be applied to the raw material and composition of preparation invention alloy
The material composition of table 1 is not unique optional material composition, and specific ingredient raw material obtained by reality are Lai really
It is fixed.Wherein ferrochrome, crome metal, ferro-boron, molybdenum-iron, ferro-niobium and vanadium iron provide the content of Cr, B, Mo, Nb and V of invention alloy, high
Carbon ferrochrome is used to balance C content.Pure iron includes electrical pure iron, electromagnetic pure iron or ingot iron, even low-carbon carbon steel and its
Leftover pieces.
Specific melting, casting and heat treatment process are as follows:
(1) melting and casting process
After weighing good corresponding raw material according to component requirements proportion, induction furnace, vaccum sensitive stove etc. can be used and carry out melting system
Standby alloy.Ferrochrome, crome metal, ferro-boron, ferro-niobium, vanadium iron, molybdenum-iron and pure iron are melted first, fusion temperature is higher than 1540~1660
DEG C, so that pure iron, molybdenum-iron and crome metal sufficiently melt；Then furnace power is reduced, melt temperature is down to 1300~1350 DEG C
Afterwards, with the fine aluminium deoxidation of ingredient total amount 0.1~0.15%；Continue heat preservation about 5~10 minutes, rapid cast alloys, cast temperature
Range is 1250~1300 DEG C.
Invention alloy is eutectic composition, and melt has good mobility fine, can be cast as by various methods
Type, such as normal sands Mold casting or model casting, lost foam casting, permanent mold casting, ceramic mold casting, die casting, centrifugal casting
The special casting method such as make.
(2) rapid cooling or slow cooling and heat treatment after casting
For small-sized and simple shape casting, rapid cooling is taken after casting, obtains the non-equilibrium microstructure with high rigidity, it is subsequent
Heat treatment is not taken.Its technique are as follows:
Cooling velocity from setting temperature to 600 DEG C should be not less than 60 DEG C/min, and solve between 600~800 DEG C
Except the constraint of mold.Rapid cooling is realized by placing the means such as chill in water cooling, swage, mold.
The subsequent stress relief annealing technique that can be used lower than 600 DEG C and necessary shape, dimensional accuracy and finish need
The mechanical process wanted.
The Fe-Cr-Mo-B-C alloy cast ingot hardness of preparation reaches HRC67.0~70.8, and impact flexibility reaches 12.6~
18.0J/cm2, bending strength reaches 1280~1600MPa.
Invention alloy is deep eutectic ingredient, non-equilibrium matrix can be formed under the conditions of common sand casting, such as
Supersaturated solid solution, amorphous, nanocrystalline or martensitic structure.But it will cause volume change, ingot casting since non-equilibrium transformation occurs
Each section causes stress to be concentrated since cooling velocity is inconsistent, causes cracking phenomena, therefore casting is needed at 600~800 DEG C
Between release mold constraint.
For large-scale and complex-shaped casting, need to take slow cooling and heat treatment after casting.Its technique are as follows:
Using slower coolings such as normal sands Mold casting, model casting, lost foam casting, ceramic mold casting, centrifugal castings
Forging type casting.Cooling with mold after having cast, die sinking temperature will be lower than 200 DEG C, subsequent natural cooling, to avoid generation
Thermal stress-cracking.
It needs to reheat when heat treatment, casting is put into box stove heating, is heated up with furnace, heating rate is according to heating
Furnace regulation, heat temperature raising speed are no more than 10 DEG C/min.Heating temperature is 950~1050 DEG C, and soaking time is 1~4h.
After heat preservation, casting is quickly entered to 5~15% salt water or buck quenching cooling.It should constantly be stirred in cooling procedure
It mixes, quenches cooling time >=30min.
Then in 200~250 DEG C of 2~4h of tempering, natural cooling.
After above-mentioned quenching-tempering, the Fe-Cr-Mo-B-C alloy rigidity of preparation is 66.2~68HRC, impact
14.6~17.5J/cm of toughness2, 1496~1600MPa of bending strength.
It is cooling with mold after casting described in step (2) is complete, from setting temperature to cast(ing) surface cooling velocity 600 DEG C
Lower than 3 DEG C/min.
Of the invention is mainly characterized by using Mo element and the strong feature of C element binding force, thus boron, carbon in high rigidity
Compound be precipitated during, among these compounds between occur forming the segregation of Mo element so that continuous net-shaped structure
It is interrupted, crystal grain refinement；Cr, B, C, Mo, Nb, V that matrix mutually remains as high rigidity simultaneously strengthen non-equilibrium microstructure.So that
While keeping high rigidity, impact flexibility and bending strength are promoted casting alloy.
Detailed description of the invention
1 low power cast sturcture of Fig. 1 present example figure；
2 high power cast sturcture of Fig. 2 present example figure；
The EDS analysis chart of segregation phase in the 4 casting metallographic structure of Fig. 3 present example；
9 low power cast sturcture of Fig. 4 present example figure；
10 high power cast sturcture of Fig. 5 present example figure；
Specific embodiment
Various method of smelting of the invention, casting method are not limited by following examples, any to want in right of the invention
The improvements and changes in range for asking book claimed are all within protection scope of the present invention.
Selecting high carbon ferro-chrome, chromic carbide iron, crome metal, ferro-boron, molybdenum-iron, ferro-niobium, vanadium iron, ingot iron etc. is raw material,
It invents in desired composition range and is configured to alloy.
It is raw material that embodiment 1., which selects high carbon ferro-chrome, chromic carbide iron, ferro-boron, ferro-niobium, vanadium iron, molybdenum-iron and ingot iron, at
Divide range as follows: Cr:10.0wt.%；B:2.9wt.%；C:0.7wt.%；Nb:0.4wt.%；V:0.2wt.%；Mo:
1.8wt.%；Impurity element control is shown in Table 2.After weighing good corresponding raw material according to component requirements proportion, using induction melting and
Sand mold die cast.Specific steps are as follows:
First by high carbon ferro-chrome, chromic carbide iron, ferro-boron, ferro-niobium, vanadium iron, molybdenum-iron and ingot iron, fusion temperature 1500
℃；Then furnace power is reduced, after melt temperature is down to 1280 DEG C, with the fine aluminium deoxidation of ingredient total amount 0.15%；After continuation of insurance
Temperature about 5 minutes, rapid cast alloys, cast temperature range are 1230 DEG C.About 6 minutes after having cast, sand mould is opened, is cast at this time
Ingot temperature be lower than 800 DEG C, from setting temperature to 800 DEG C cooling rate be about 70 DEG C/min.It is air-cooled to room temperature.Gained
Ingot casting average hardness reaches HRC67.8, and impact flexibility reaches 15.6J/cm2, bending strength reaches 1468MPa.
1 ingot casting fractograph of embodiment is shown in Fig. 1, is made of torulose α-Fe primary crystal and eutectic structure, wherein eutectic group
It is woven to α-Fe and hard phase line and staff control, continuous network structure does not occur in hard phase.In terms of performance, hardness HRC67.8 is said
The bright not simple ferrite of the primary crystal largely occurred, the martensite containing Cr, W, B, C solution strengthening or amorphous/nanometer
The non-equilibrium microstructures such as crystalline substance, because ferrite can not reach corresponding hardness.As it can be seen that the addition of W changes the group of casting alloy
Constituent is knitted, the hardness and toughness of matrix are improved, to greatly improve the toughness and intensity of material.
It is raw material that embodiment 2., which selects high carbon ferro-chrome, crome metal, ferro-boron, ferro-niobium, molybdenum-iron and ingot iron, and composition range is such as
Under: Cr:10.0wt.%；B:2.7wt.%；C:0.7wt.%；Nb:0.5wt.%；Mo:3.0wt.%；Impurity element control is shown in
Table 2.After weighing good corresponding raw material according to component requirements proportion, vacuum induction melting and water cooling iron mould casting can be used.Tool
Body step are as follows:
First by high carbon ferro-chrome, crome metal, ferro-boron, ferro-niobium, molybdenum-iron and ingot iron, fusion temperature is 1550 DEG C；Then
Furnace power is reduced, after melt temperature is down to 1350 DEG C, with the fine aluminium deoxidation of ingredient total amount 0.1%；Continue about 10 points of heat preservation
Clock, rapid cast alloys, cast temperature are 1280 DEG C.About 10 minutes after having cast, water cooling swage is opened, ingot casting temperature is low at this time
In 600 DEG C, from setting temperature to 600 DEG C cooling rate be about 70 DEG C/min.It is air-cooled to room temperature.Gained ingot casting hardness
Reach HRC70.8, impact flexibility reaches 12.6J/cm2, bending strength reaches 1280MPa.
2 high power cast sturcture of Fig. 2 example figure, figure it is seen that hard phase is mutually interspersed with matrix, without even
Continuous reticular structure.And it is inconsistent a large amount of obvious contrasts occur in the upper surface of these phases, but without obvious crystal boundary
Patch, these patches are exactly the product of Mo segregation, their appearance thinning microstructure, and further prevent forming continuous net-shaped knot
Structure, to improve the performance indicators such as toughness and the bending strength of material.
It is raw material, composition range that embodiment 3., which selects high carbon ferro-chrome, chromic carbide iron, ferro-boron, ferro-niobium, molybdenum-iron and ingot iron,
It is as follows: Cr:10.0wt.%；B:2.7wt.%；C:0.8wt.%；Nb:0.6wt.%；Mo:2.8wt.%；Impurity element control
It is shown in Table 2.After weighing good corresponding raw material according to component requirements proportion, using induction melting and model casting, specific steps are as follows:
High carbon ferro-chrome, chromic carbide iron, ferro-boron, ferro-niobium, molybdenum-iron and ingot iron are melted first, fusion temperature 1560
℃；Then furnace power is reduced, after melt temperature is down to 1320 DEG C, with the fine aluminium deoxidation of ingredient total amount 0.12%；After continuation of insurance
Temperature about 8 minutes, rapid cast alloys, cast temperature range are 1260 DEG C.About 10 minutes after having cast, sand mold fusible pattern is opened, this
When ingot casting temperature be lower than 700 DEG C, from setting temperature to 700 DEG C cooling rate be about 60 DEG C/min.It is air-cooled to room temperature.
Gained ingot casting hardness reaches HRC69.0, and impact flexibility reaches 13.9J/cm2, bending strength reaches 1600MPa.
It is raw material, ingredient that embodiment 4., which selects high carbon ferro-chrome, crome metal, ferro-boron, ferro-niobium, vanadium iron, molybdenum-iron and ingot iron,
Range is as follows: Cr:11.0wt.%；B:2.7wt.%；C:0.7wt.%；Nb:0.2wt.%；V:0.4wt.%； Mo:
2.0wt.%；Impurity element control is shown in Table 2.After weighing good corresponding raw material according to component requirements proportion, using induction melting and
Sand casting, specific steps are as follows:
High carbon ferro-chrome, crome metal, ferro-boron, ferro-niobium, vanadium iron, molybdenum-iron and ingot iron are melted first, fusion temperature is
1520℃；Then furnace power is reduced, after melt temperature is down to 1330 DEG C, with the fine aluminium deoxidation of ingredient total amount 0.14%；After
Continuation of insurance temperature about 7 minutes, rapid cast alloys, cast temperature range are 1250 DEG C.About 7 minutes after having cast, sand mould is opened, this
When ingot casting temperature be lower than 800 DEG C, from setting temperature to 800 DEG C cooling rate be about 60 DEG C/min.It is air-cooled to room temperature.
Gained ingot casting average hardness reaches HRC70, and impact flexibility reaches 14.2J/cm2, bending strength reaches 1420MPa.
Fig. 3 is segregation phase EDS map and analysis in casting alloy as a result, as a result EDS can only be shown in the qualitative analysis of ingredient
Show in alloy there are Mo element, illustrates that Mo element forms segregation, block continuous net-shaped structure, improve the toughness of alloy.
It is raw material that embodiment 5., which selects high carbon ferro-chrome, chromic carbide iron, ferro-boron, ferro-niobium, vanadium iron, molybdenum-iron and ingot iron, at
Divide range as follows: Cr:10.0wt.%；B:2.6wt.%；C:0.6wt.%；Nb:0.3wt.%；V:0.1wt.%；Mo:
2.3wt.%；Impurity element control is shown in Table 2.After weighing good corresponding raw material according to component requirements proportion, using induction melting and
Lost foam casting, the specific steps are as follows:
High carbon ferro-chrome, chromic carbide iron, ferro-boron, ferro-niobium, vanadium iron, molybdenum-iron, ingot iron are melted first, fusion temperature is
1540℃；Then furnace power is reduced, after melt temperature is down to 1320 DEG C, with the fine aluminium deoxidation of ingredient total amount 0.12%；After
Continuation of insurance temperature about 9 minutes, rapid cast alloys, cast temperature range are 1250 DEG C.About 8 minutes after having cast, disappearance sand is opened
Type, at this time ingot casting temperature be lower than 700 DEG C, from setting temperature to 700 DEG C cooling rate be about 70 DEG C/min.It is air-cooled to
Room temperature.Gained ingot casting hardness reaches HRC67.0, and impact flexibility reaches 16.7J/cm2, bending strength reaches 1390MPa.
It is raw material, composition range that embodiment 6., which selects high carbon ferro-chrome, chromic carbide iron, ferro-boron, ferro-niobium, molybdenum-iron and ingot iron,
It is as follows: Cr:10.0wt.%；B:2.6wt.%；C:0.8wt.%；Nb:0.8wt.%；Mo:2.1wt.%；Impurity element control
It is shown in Table 2.After weighing good corresponding raw material according to component requirements proportion, using vacuum induction melting and iron mould casting, specific steps
It is as follows:
First by high carbon ferro-chrome, chromic carbide iron, ferro-boron, ferro-niobium, molybdenum-iron and ingot iron, fusion temperature is 1530 DEG C；So
After reduce furnace power, after melt temperature is down to 1300 DEG C, with the fine aluminium deoxidation of ingredient total amount 0.15%；Continue heat preservation about 10
Minute, rapid cast alloys, cast temperature range is 1250 DEG C.About 10 minutes after having cast, sand mould is opened, at this time ingot casting temperature
Degree be lower than 600 DEG C, from setting temperature to 600 DEG C cooling rate be about 70 DEG C/min.It is air-cooled to room temperature.Gained ingot casting
Hardness reaches HRC68.0, and impact flexibility reaches 14.3J/cm2, bending strength reaches 1460MPa.
It is raw material that embodiment 7., which selects high carbon ferro-chrome, chromic carbide iron, ferro-boron, ferro-niobium, vanadium iron, molybdenum-iron and ingot iron, at
Divide range as follows: Cr:11.0wt.%；B:2.6wt.%；C:0.9wt.%；Nb:0.2wt.%；V:0.2wt.%；Mo:
2.5wt.%；Impurity element control is shown in Table 2.After weighing good corresponding raw material according to component requirements proportion, induction melting can be used
And lost foam casting.Specific step is as follows:
High carbon ferro-chrome, chromic carbide iron, ferro-boron, ferro-niobium, vanadium iron, molybdenum-iron and ingot iron are melted first, fusion temperature is
1550℃；Then furnace power is reduced, after melt temperature is down to 1280 DEG C, with the fine aluminium deoxidation of ingredient total amount 0.10%；After
Continuation of insurance temperature about 5 minutes, rapid cast alloys, cast temperature range are 1250 DEG C.About 9 minutes after having cast, disappearance sand is opened
Type, at this time ingot casting temperature be lower than 600 DEG C, from setting temperature to 600 DEG C cooling rate be about 70 DEG C/min.It is air-cooled to
Room temperature.Gained ingot casting hardness reaches HRC67.5, and impact flexibility reaches 18.0J/cm2, bending strength reaches 1520MPa.
It is raw material that embodiment 8., which selects high carbon ferro-chrome, chromic carbide iron, ferro-boron, ferro-niobium, molybdenum-iron, vanadium iron and ingot iron, at
Divide range as follows: Cr:13.0wt.%；B:2.6wt.%；C:0.8wt.%；Nb:0.6wt.%；V:0.4wt.%；Mo:
2.2wt.%；Impurity element control is shown in Table 2.After weighing good corresponding raw material according to component requirements proportion, using induction melting and
Lost foam casting, the specific steps are as follows:
High carbon ferro-chrome, chromic carbide iron, ferro-boron, ferro-niobium, vanadium iron, molybdenum-iron and ingot iron are melted first, fusion temperature is
1540℃；Then furnace power is reduced, after melt temperature is down to 1320 DEG C, with the fine aluminium deoxidation of ingredient total amount 0.13%；After
Continuation of insurance temperature about 7 minutes, rapid cast alloys, cast temperature range are 1260 DEG C.About 9 minutes after having cast, disappearance sand is opened
Type, at this time ingot casting temperature be lower than 700 DEG C, from setting temperature to 700 DEG C cooling rate be about 60 DEG C/min.It is air-cooled to
Room temperature.Gained ingot casting hardness reaches HRC69, and impact flexibility reaches 17.6J/cm2, bending strength reaches 1426MPa.
It is raw material that embodiment 9., which selects high carbon ferro-chrome, chromic carbide iron, ferro-boron, ferro-niobium, vanadium iron, molybdenum-iron and ingot iron, at
Divide range as follows: Cr:10.0wt.%；B:2.9wt.%；C:0.7wt.%；Mo:1.0wt.%；Nb:0.4wt.%；V:
0.2wt.%；Impurity element control is shown in Table 2.After weighing good corresponding raw material according to component requirements proportion, using induction melting and
Sand mold die cast.Specific steps are as follows:
First by high carbon ferro-chrome, chromic carbide iron, ferro-boron, ferro-niobium, vanadium iron, molybdenum-iron and ingot iron, fusion temperature 1540
℃；Then furnace power is reduced, after melt temperature is down to 1300 DEG C, with the fine aluminium deoxidation of ingredient total amount 0.15%；After continuation of insurance
Temperature about 5 minutes, rapid cast alloys, cast temperature range are 1250 DEG C.Die sinking temperature is lower than 200 DEG C after having cast.Naturally cold
But.
Then casting is put into box stove heating, heating temperature is 1050 DEG C, soaking time 4h.Heat temperature raising speed
No more than 10 DEG C/min.After heat preservation, the brine hardening that casting is quickly entered 5% is cooling.It should be stirred continuously in cooling procedure,
Quench cooling time >=30min.Then in 250 DEG C of tempering 1h, natural cooling.After above-mentioned quenching-tempering, institute
Obtaining alloy rigidity is 66.8HRC, impact flexibility 17.2J/cm2, bending strength 1520MPa.
1 ingot casting fractograph of embodiment is shown in Fig. 1, is made of torulose α-Fe primary crystal and eutectic structure, wherein eutectic group
It is woven to α-Fe and hard phase line and staff control, continuous network structure does not occur in hard phase.In terms of performance, hardness HRC66.8 is said
The bright not simple ferrite of the primary crystal largely occurred, martensite or amorphous containing Cr, Mo, B, C solution strengthening/receive
The non-equilibrium microstructures such as rice crystalline substance, because ferrite can not reach corresponding hardness.As it can be seen that the addition of Mo changes casting alloy
Constituent is organized, the hardness and toughness of matrix are improved, to greatly improve the toughness and intensity of material.
It is raw material, composition range that embodiment 10., which selects high carbon ferro-chrome, crome metal, ferro-boron, ferro-niobium, molybdenum-iron and ingot iron,
It is as follows: Cr:10.0wt.%；B:2.7wt.%Mo:2.0wt.%；；C:0.7wt.%；Nb:0.5wt.%；Impurity element control
It is shown in Table 2.After weighing good corresponding raw material according to component requirements proportion, vacuum induction melting and water cooling iron mould casting can be used.
Specific steps are as follows:
First by high carbon ferro-chrome, crome metal, ferro-boron, ferro-niobium, molybdenum-iron and ingot iron, fusion temperature is 1660 DEG C；Then
Furnace power is reduced, after melt temperature is down to 1350 DEG C, with the fine aluminium deoxidation of ingredient total amount 0.1%；Continue about 10 points of heat preservation
Clock, rapid cast alloys, cast temperature range are 1300 DEG C.Die sinking temperature is lower than 200 DEG C after having cast.Natural cooling.
Then casting is put into box stove heating, heating temperature is 950 DEG C, soaking time 4h.Heat temperature raising speed
No more than 10 DEG C/min.After heat preservation, the brine hardening that casting is quickly entered 15% is cooling.It should constantly be stirred in cooling procedure
It mixes, quenches cooling time >=30min.Then in 200 DEG C of tempering 4h, natural cooling.By above-mentioned quenching-tempering
Afterwards, gained alloy rigidity is 67.2HRC, impact flexibility 17.5J/cm2, bending strength 1560MPa.
2 high power cast sturcture of Fig. 2 example figure, figure it is seen that hard phase is mutually interspersed with matrix, without even
Continuous reticular structure.And it is inconsistent a large amount of obvious contrasts occur in the upper surface of these phases, but without obvious crystal boundary
Patch, these patches are exactly the product of Mo segregation, their appearance thinning microstructure, and further prevent forming continuous net-shaped knot
Structure, to improve the performance indicators such as toughness and the bending strength of material.
It is raw material, ingredient model that embodiment 11., which selects high carbon ferro-chrome, chromic carbide iron, ferro-boron, ferro-niobium, molybdenum-iron and ingot iron,
It encloses as follows: Cr:10.0wt.%；B:2.7wt.%；；Mo:1.8wt.%；C:0.8wt.%；Nb:0.6wt.%；Impurity element control
System is shown in Table 2.After weighing good corresponding raw material according to component requirements proportion, using induction melting and model casting, specific steps are as follows:
High carbon ferro-chrome, chromic carbide iron, ferro-boron, ferro-niobium, molybdenum-iron and ingot iron are melted first, fusion temperature 1620
℃；Then furnace power is reduced, after melt temperature is down to 1320 DEG C, with the fine aluminium deoxidation of ingredient total amount 0.12%；After continuation of insurance
Temperature about 8 minutes, rapid cast alloys, cast temperature range are 1280 DEG C.Die sinking temperature is lower than 200 DEG C after having cast.Naturally cold
But.
Then casting is put into box stove heating, heating temperature is 1000 DEG C, soaking time 2h.Heat temperature raising speed
No more than 10 DEG C/min.After heat preservation, the brine hardening that casting is quickly entered 10% is cooling.It should constantly be stirred in cooling procedure
It mixes, quenches cooling time >=30min.Then in 220 DEG C of tempering 3h, natural cooling.By above-mentioned quenching-tempering
Afterwards, gained alloy rigidity is 66.7HRC, impact flexibility 16.9J/cm2, bending strength 1498MPa.
It is raw material, ingredient that embodiment 12., which selects high carbon ferro-chrome, crome metal, ferro-boron, ferro-niobium, vanadium iron, molybdenum-iron and ingot iron,
Range is as follows: Cr:11.0wt.%；B:2.7wt.%；Mo:1.5wt.%；C:0.7wt.%；Nb:0.2wt.%； V:
0.4wt.%；Impurity element control is shown in Table 2.After weighing good corresponding raw material according to component requirements proportion, using induction melting and
Sand casting, specific steps are as follows:
High carbon ferro-chrome, crome metal, ferro-boron, ferro-niobium, vanadium iron, molybdenum-iron and ingot iron are melted first, fusion temperature is
1580℃；Then furnace power is reduced, after melt temperature is down to 1320 DEG C, with the fine aluminium deoxidation of ingredient total amount 0.14%；After
Continuation of insurance temperature about 7 minutes, rapid cast alloys, cast temperature range are 1260 DEG C.Die sinking temperature is lower than 200 DEG C after having cast.From
It is so cooling.
Then casting is put into box stove heating, heating temperature is 1020 DEG C, soaking time 2h.Heat temperature raising speed
No more than 10 DEG C/min.After heat preservation, casting is quickly entered to 5% buck quenching cooling.It should be stirred continuously in cooling procedure,
Quench cooling time >=30min.Then in 220 DEG C of tempering 2h, natural cooling.After above-mentioned quenching-tempering, institute
Obtaining alloy rigidity is 68HRC, impact flexibility 14.6J/cm2, bending strength 1500MPa.
It is raw material that embodiment 13., which selects high carbon ferro-chrome, chromic carbide iron, ferro-boron, ferro-niobium, vanadium iron, molybdenum-iron and ingot iron, at
Divide range as follows: Cr:10.0wt.%；B:2.6wt.%；C:0.6wt.%；Mo:1.6wt.%；Nb:0.3wt.%；V:
0.1wt.%；Impurity element control is shown in Table 2.After weighing good corresponding raw material according to component requirements proportion, using induction melting and
Lost foam casting, the specific steps are as follows:
High carbon ferro-chrome, chromic carbide iron, ferro-boron, ferro-niobium, vanadium iron, molybdenum-iron, ingot iron are melted first, fusion temperature is
1580℃；Then furnace power is reduced, after melt temperature is down to 1320 DEG C, with the fine aluminium deoxidation of ingredient total amount 0.12%；After
Continuation of insurance temperature about 9 minutes, rapid cast alloys, cast temperature range are 1250 DEG C.Die sinking temperature will be lower than 200 DEG C after having cast.
Natural cooling.
Then casting is put into box stove heating, heating temperature is 990 DEG C, soaking time 3h.Heat temperature raising speed
No more than 10 DEG C/min.After heat preservation, casting is quickly entered to 15% buck quenching cooling.It should constantly be stirred in cooling procedure
It mixes, quenches cooling time >=30min.Then in 220 DEG C of tempering 3h, natural cooling.By above-mentioned quenching-tempering
Afterwards, gained alloy rigidity is 66.8HRC, impact flexibility 16.6J/cm2, bending strength 1582MPa.
It is raw material, ingredient model that embodiment 14., which selects high carbon ferro-chrome, chromic carbide iron, ferro-boron, ferro-niobium, molybdenum-iron and ingot iron,
It encloses as follows: Cr:10.0wt.%；B:2.6wt.%；Mo:1.5wt.%；C:0.8wt.%；Nb:0.8wt.%；Impurity element control
System is shown in Table 2.It is specific to walk using vacuum induction melting and iron mould casting after weighing good corresponding raw material according to component requirements proportion
It is rapid as follows:
First by high carbon ferro-chrome, chromic carbide iron, ferro-boron, ferro-niobium, molybdenum-iron and ingot iron, fusion temperature is 1650 DEG C；So
After reduce furnace power, after melt temperature is down to 1320 DEG C, with the fine aluminium deoxidation of ingredient total amount 0.15%；Continue heat preservation about 10
Minute, rapid cast alloys, cast temperature range is 1300 DEG C.Die sinking temperature is lower than 200 DEG C after having cast.Natural cooling.
Then casting is put into box stove heating, heating temperature is 1020 DEG C, soaking time 2h.Heat temperature raising speed
No more than 10 DEG C/min.After heat preservation, casting is quickly entered to 10% buck quenching cooling.It should constantly be stirred in cooling procedure
It mixes, quenches cooling time >=30min.Then in 220 DEG C of tempering 3h, natural cooling.By above-mentioned quenching-tempering
Afterwards, gained alloy rigidity is 67.0HRC, impact flexibility 16.8J/cm2, bending strength 1559MPa.
It is raw material that embodiment 15., which selects high carbon ferro-chrome, chromic carbide iron, ferro-boron, ferro-niobium, vanadium iron, molybdenum-iron and ingot iron, at
Divide range as follows: Cr:11.0wt.%；B:2.6wt.%；Mo:1.6wt.%；C:0.9wt.%；Nb:0.2wt.%；V:
0.2wt.%；Impurity element control is shown in Table 2.After weighing good corresponding raw material according to component requirements proportion, induction melting can be used
And lost foam casting.Specific step is as follows:
High carbon ferro-chrome, chromic carbide iron, ferro-boron, ferro-niobium, vanadium iron, molybdenum-iron and ingot iron are melted first, fusion temperature is
1580℃；Then furnace power is reduced, after melt temperature is down to 1300 DEG C, with the fine aluminium deoxidation of ingredient total amount 0.10%；After
Continuation of insurance temperature about 5 minutes, rapid cast alloys, cast temperature range are 1250 DEG C.Die sinking temperature is lower than 200 DEG C after having cast.From
It is so cooling.
Then casting is put into box stove heating, 980 DEG C of heating temperature, soaking time 1h.Heat temperature raising speed is not
More than 10 DEG C/min.After heat preservation, casting is quickly entered to 15% buck quenching cooling.It should be stirred continuously in cooling procedure,
Quench cooling time >=30min.Then in 220 DEG C of tempering 4h, natural cooling.After above-mentioned quenching-tempering, institute
Obtaining alloy rigidity is 66.9HRC, impact flexibility 16.5J/cm2, bending strength 1496MPa.
It is raw material that embodiment 16., which selects high carbon ferro-chrome, chromic carbide iron, ferro-boron, ferro-niobium, molybdenum-iron, vanadium iron and ingot iron, at
Divide range as follows: Cr:13.0wt.%；B:2.6wt.%；Mo:1.2wt.%；C:0.8wt.%；Nb:0.6wt.%；V:
0.4wt.%；Impurity element control is shown in Table 2.After weighing good corresponding raw material according to component requirements proportion, using induction melting and
Lost foam casting, the specific steps are as follows:
High carbon ferro-chrome, chromic carbide iron, ferro-boron, ferro-niobium, vanadium iron, molybdenum-iron and ingot iron are melted first, fusion temperature is
1590℃；Then furnace power is reduced, after melt temperature is down to 1320 DEG C, with the fine aluminium deoxidation of ingredient total amount 0.13%；After
Continuation of insurance temperature about 7 minutes, rapid cast alloys, cast temperature range are 1280 DEG C.Die sinking temperature is lower than 200 DEG C after having cast.From
It is so cooling.
Then casting is put into box stove heating, heating temperature is 1000 DEG C, soaking time 2h.Heat temperature raising speed
No more than 10 DEG C/min.After heat preservation, casting is quickly entered to 10% buck quenching cooling.It should constantly be stirred in cooling procedure
It mixes, quenches cooling time >=30min.Then in 220 DEG C of tempering 2h, natural cooling.By above-mentioned quenching-tempering
Afterwards, gained alloy rigidity is 67.2HRC, impact flexibility 16.9J/cm2, bending strength 1600MPa.
Casting alloy performance detection prepared by each embodiment is as described below:
1. pair example casting metal carries out hardness test using HR-150A Rockwell hardness machine, load 150Kg makes a call to five
It is averaged after point, is listed in table 2.
2. pair example casting metal carries out impact flexibility test using JBS-300B shock machine, range 150J is beaten
It is averaged after five samples, is listed in table 2.
3. pair example casting metal material electronics universal testing machine carries out three-point bending resistance experiment, sample having a size of 2 × 5 ×
The rectangular specimen of 50mm, span 30mm take the bending strength average value of three same treatment samples to be listed in table 2.
The ingredient and hardness, impact flexibility and bending strength * of 2 embodiment of table
* in table 2, Si < 0.07, S, P :≤0.01, it is impurity element.
Claims (3)
1. a kind of molybdenum toughening cast iron, it is characterised in that: the mass percentage of alloy each element is Cr:9.0~13.0, B:2.6
The content of~2.9, C:0.7~0.9, Mo:1.8~3.0%, Nb:0.4~0.8, V:0.4~0.8, Mn contain less than 0.3, Si's
Amount is less than 0.07, S, P :≤0.01, surplus Fe；Wherein C and B gross mass percentage composition are as follows: 3.3~3.6；C/Cr content ratio:
0.06~0.08；The gross mass percentage composition of Nb and V is 0.5~1.0.
2. manufacture and the heat treatment method of molybdenum toughening cast iron as described in claim 1, it is characterised in that the following steps are included:
(1) melting and casting process；
After weighing good corresponding raw material according to component requirements proportion, alloy is prepared using induction furnace melting, first by ferrochrome, metal
Chromium, ferro-boron, ferro-niobium, vanadium iron, molybdenum-iron and pure iron fusing, 1500~1550 DEG C of fusion temperature, so that pure iron and crome metal are sufficiently molten
Change；Then furnace power is reduced, it is de- with the fine aluminium of ingredient total amount 0.1~0.15% after melt temperature is down to 1280~1350 DEG C
Oxygen；Continue heat preservation 5~10 minutes, cast alloys, cast temperature range is 1230~1280 DEG C；
(2) rapid cooling or slow cooling and heat treatment after casting
For small-sized and simple shape casting, rapid cooling is taken after casting, obtains the non-equilibrium microstructure with high rigidity, it is subsequent not adopt
Take heat treatment, technique are as follows:
Cooling velocity from setting temperature to 600 DEG C is not less than 60 DEG C/min, and releases mold between 600 ~ 800 DEG C
Constraint, pass through in water cooling, swage, mold place chill realize be quickly cooled down；
The machine that subsequent stress relief annealing technique and necessary shape using lower than 600 DEG C, dimensional accuracy and finish need
Working process；
For large-scale and complex-shaped casting, need to take slow cooling and heat treatment, technique after casting are as follows:
Using the casting side of normal sands Mold casting, model casting, lost foam casting, ceramic mold casting or centrifugal casting slow cool down
Formula casting, cooling with mold after having cast, die sinking temperature will be lower than 200 DEG C, and subsequent natural cooling is opened to avoid thermal stress occurs
It splits；
It needs to reheat when heat treatment, casting is put into box stove heating, is heated up with furnace, heating rate is advised according to heating furnace
Journey, heat temperature raising speed are no more than 10 DEG C/min, heating temperature is 950~1050 DEG C, and soaking time is 1~4h；
After heat preservation, casting is quickly entered to 5~15% salt water or buck quenching cooling, should be stirred continuously, quench in cooling procedure
Fiery cooling time >=30min；
Then in 200~250 DEG C of 2~4 h of tempering, natural cooling.
3. manufacture and the heat treatment method of molybdenum toughening cast iron as claimed in claim 2, it is characterised in that: after the casting is complete
It is cooling with mold, it is lower than 3 DEG C/min from setting temperature to cast(ing) surface cooling velocity 600 DEG C.
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| CN201810588898.7A CN108570614A (en) | 2018-06-08 | 2018-06-08 | A kind of molybdenum element segregation toughening high hardness alloy and its casting method |
| CN2018105888987 | 2018-06-08 | ||
| CN201810589669.7A CN108531826A (en) | 2018-06-08 | 2018-06-08 | A kind of molybdenum element segregation toughening high hard alloy and its casting and heat treatment method |
| CN2018105896697 | 2018-06-08 |
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| CN1260841A (en) * | 1997-06-17 | 2000-07-19 | 赫加奈斯公司 | Stainless steel powder |
| CN1803339A (en) * | 2006-01-19 | 2006-07-19 | 郑州航空工业管理学院 | Low crack type high speed steel roll and its centrifugal casting method |
| JP2015196870A (en) * | 2014-03-31 | 2015-11-09 | 新日鐵住金ステンレス株式会社 | High strength dual-phase stainless steel wire rod excellent in spring fatigue characteristic and production method therefor, and high strength dual-phase stainless steel wire excellent in spring fatigue characteristic |
| CN105695884A (en) * | 2016-03-22 | 2016-06-22 | 湖南省冶金材料研究院 | High-hardness, wear-resistant and corrosion-resistant alloy of amorphous/nanocrystal matrix and preparation method of high-hardness, wear-resistant and corrosion-resistant alloy |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN1260841A (en) * | 1997-06-17 | 2000-07-19 | 赫加奈斯公司 | Stainless steel powder |
| CN1803339A (en) * | 2006-01-19 | 2006-07-19 | 郑州航空工业管理学院 | Low crack type high speed steel roll and its centrifugal casting method |
| JP2015196870A (en) * | 2014-03-31 | 2015-11-09 | 新日鐵住金ステンレス株式会社 | High strength dual-phase stainless steel wire rod excellent in spring fatigue characteristic and production method therefor, and high strength dual-phase stainless steel wire excellent in spring fatigue characteristic |
| CN105695884A (en) * | 2016-03-22 | 2016-06-22 | 湖南省冶金材料研究院 | High-hardness, wear-resistant and corrosion-resistant alloy of amorphous/nanocrystal matrix and preparation method of high-hardness, wear-resistant and corrosion-resistant alloy |
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