CN116275050B - Preparation method of high-strength molybdenum - Google Patents

Preparation method of high-strength molybdenum Download PDF

Info

Publication number
CN116275050B
CN116275050B CN202310581104.5A CN202310581104A CN116275050B CN 116275050 B CN116275050 B CN 116275050B CN 202310581104 A CN202310581104 A CN 202310581104A CN 116275050 B CN116275050 B CN 116275050B
Authority
CN
China
Prior art keywords
sintering
molybdenum
temperature
strength
purity
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.)
Active
Application number
CN202310581104.5A
Other languages
Chinese (zh)
Other versions
CN116275050A (en
Inventor
陈占洋
陈兴友
张慧霞
朱宇
罗志斌
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Xi'an Gemei Metal Material Co ltd
Original Assignee
Xi'an Gemei Metal Material Co ltd
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Xi'an Gemei Metal Material Co ltd filed Critical Xi'an Gemei Metal Material Co ltd
Priority to CN202310581104.5A priority Critical patent/CN116275050B/en
Publication of CN116275050A publication Critical patent/CN116275050A/en
Application granted granted Critical
Publication of CN116275050B publication Critical patent/CN116275050B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F5/00Manufacture of workpieces or articles from metallic powder characterised by the special shape of the product
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F3/00Manufacture of workpieces or articles from metallic powder characterised by the manner of compacting or sintering; Apparatus specially adapted therefor ; Presses and furnaces
    • B22F3/02Compacting only
    • B22F3/04Compacting only by applying fluid pressure, e.g. by cold isostatic pressing [CIP]
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F3/00Manufacture of workpieces or articles from metallic powder characterised by the manner of compacting or sintering; Apparatus specially adapted therefor ; Presses and furnaces
    • B22F3/10Sintering only
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F3/00Manufacture of workpieces or articles from metallic powder characterised by the manner of compacting or sintering; Apparatus specially adapted therefor ; Presses and furnaces
    • B22F3/18Manufacture of workpieces or articles from metallic powder characterised by the manner of compacting or sintering; Apparatus specially adapted therefor ; Presses and furnaces by using pressure rollers
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F3/00Manufacture of workpieces or articles from metallic powder characterised by the manner of compacting or sintering; Apparatus specially adapted therefor ; Presses and furnaces
    • B22F3/24After-treatment of workpieces or articles
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22BPRODUCTION AND REFINING OF METALS; PRETREATMENT OF RAW MATERIALS
    • C22B34/00Obtaining refractory metals
    • C22B34/30Obtaining chromium, molybdenum or tungsten
    • C22B34/34Obtaining molybdenum
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F3/00Manufacture of workpieces or articles from metallic powder characterised by the manner of compacting or sintering; Apparatus specially adapted therefor ; Presses and furnaces
    • B22F3/18Manufacture of workpieces or articles from metallic powder characterised by the manner of compacting or sintering; Apparatus specially adapted therefor ; Presses and furnaces by using pressure rollers
    • B22F2003/185Manufacture of workpieces or articles from metallic powder characterised by the manner of compacting or sintering; Apparatus specially adapted therefor ; Presses and furnaces by using pressure rollers by hot rolling, below sintering temperature
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F3/00Manufacture of workpieces or articles from metallic powder characterised by the manner of compacting or sintering; Apparatus specially adapted therefor ; Presses and furnaces
    • B22F3/24After-treatment of workpieces or articles
    • B22F2003/247Removing material: carving, cleaning, grinding, hobbing, honing, lapping, polishing, milling, shaving, skiving, turning the surface
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02PCLIMATE CHANGE MITIGATION TECHNOLOGIES IN THE PRODUCTION OR PROCESSING OF GOODS
    • Y02P10/00Technologies related to metal processing
    • Y02P10/20Recycling

Abstract

The invention belongs to the technical field of molybdenum preparation, and relates to a preparation method of high-strength molybdenum, which comprises the steps of raw material selection, mixing, isostatic pressing, sintering, hot rolling, warm rolling, heat treatment, machining, low-temperature shaping and the like. And a high-energy mixer is adopted, so that high-purity molybdenum powder particles are smashed, and agglomeration is avoided. The high-purity molybdenum powder is adopted and further purified in the sintering process, and the impurity gas content of C, H, O is controlled below 10 ppm. Meanwhile, the vacuum furnace and the hydrogen furnace are adopted for multiple sintering modes, and different from the conventional sintering modes, the sintering time is prolonged, the material is compact, and holes are less. The high-strength product is formed by adopting a high-temperature and low-temperature mixing treatment mode, the plate shape of the material is ensured not to be deformed, and the impurity content of the grain boundary is low. Compared with the traditional common molybdenum and molybdenum lanthanum alloy, the alloy has obviously better strength and creep resistance, and has obvious advantages as ceramic sintering supporting pieces, high-temperature furnace components, high-temperature deformation resistance bearing pieces, aviation aerospace high Wen Jian and the like.

Description

Preparation method of high-strength molybdenum
Technical Field
The invention belongs to the technical field of molybdenum preparation, and relates to a preparation method of high-strength molybdenum.
Background
Under the high temperature condition, the grain boundary sliding and the grain boundary diffusion are main microcosmic mechanisms of the deformation (creep) of the molybdenum material. The common pure molybdenum is easy to recrystallize at the temperature of more than 900 ℃ and is in a coarse structure, and oxygen is easy to react with molybdenum to form oxide at the high temperature of 1600 ℃. Oxide and impurities gather in the grain boundary, so that the strength of the grain boundary is reduced, and phenomena such as thermal fatigue, thermal creep and the like can occur when the alloy is used at high temperature, thereby generating defects such as deformation, cracks and the like.
Disclosure of Invention
The invention aims to provide a preparation method of high-strength molybdenum, which can prepare a molybdenum product with higher purity and less impurity content, and has obviously higher strength and creep resistance compared with the traditional common molybdenum and molybdenum lanthanum alloy.
The technical scheme adopted by the invention is a preparation method of high-strength molybdenum, which is implemented according to the following steps:
s1, selecting raw materials: selecting high-purity molybdenum powder, wherein the purity of the high-purity molybdenum powder is ensured to be more than 99.99%, and the impurity content of the high-purity molybdenum powder is ensured to be less than 0.01%;
s2, mixing: fully crushing and mixing high-purity molybdenum powder;
s3, isostatic pressing: isostatic pressing is carried out on the crushed high-purity molybdenum powder;
s4, sintering: high-temperature sintering is carried out on the high-purity molybdenum powder subjected to isostatic pressing treatment, and the sintering time is 4-10 h when the temperature is 800-1000 ℃; sintering time is 8-16 h at 1700-2100 ℃; sintering for 8-16 h at 2100-2300 ℃ to finally obtain a plate blank;
s5, hot rolling: carrying out hot rolling treatment on the plate blank, wherein the cogging temperature is 1000-1300 ℃;
s6, warm rolling: preserving heat at the temperature of 350-450 ℃ for 20-40 min, and rolling the plate blank after hot rolling treatment into a plate;
s7, heat treatment: carrying out heat treatment on the plate subjected to warm rolling treatment at 1900-2100 ℃ for 9-10 hours to obtain a molybdenum product;
s8, machining: grinding the molybdenum product, wherein the thickness dimension of the molybdenum product is controlled to be +/-0.05 mm, the length and width dimensions of the molybdenum product are controlled to be +/-0.2 mm, and the flatness of the molybdenum product is controlled to be less than 0.1 mm;
s9, low-temperature shaping: and (3) carrying out low-temperature treatment on the molybdenum product subjected to grinding treatment at 600-800 ℃ for 2-4 hours to finally obtain high-strength molybdenum.
The invention is also characterized in that:
the impurities of the high-purity molybdenum powder in S1 comprise Ca, fe and K.
The specific process of S2 is as follows: and crushing and fully mixing large-particle agglomerated molybdenum powder particles in the high-purity molybdenum powder by adopting a high-energy mixer, wherein the rotating speed of the high-energy mixer is 3500r/min-4500r/min, and the mixing time is 2h-4h.
The high-energy mixer is a 1000L high-energy mixer.
S4 is divided into three stages for sintering, wherein the first stage is carried out by adopting a mode comprising presintering and vacuum sintering, and the vacuum degree of the furnace is required to be 1.0x10 -3 Pa, pre-sintering temperature is 800-1000 ℃, and sintering time is 4-10 h; the second stage is vacuum furnace sintering, gradient slow heating is adopted, and sintering time is 8-16 h when sintering temperature is 1700-2100 ℃; in the third stage, sintering is carried out by adopting a hydrogen furnace, wherein the hydrogen flow is 0.2m 3 /h-0.4m 3 And/h, sintering at 2100-2300 ℃ for 8-16 h to obtain a sintered plate blank.
The thickness of the slab in S5 is 35mm.
The thickness of the sheet rolled in S6 was 2mm.
And S7, separating the plates subjected to heat treatment by adopting zircon sand.
And S8, controlling the frequency of the grinding treatment below 17Hz, controlling the feed rate of the grinding treatment below 0.02mm, and performing multiple turn-over grinding.
And S9, performing low-temperature treatment in a vacuum furnace.
According to the scheme, a mixing treatment procedure is increased, and a high-energy mixer is adopted, so that high-purity molybdenum powder particles are smashed, and agglomeration is avoided. In the powder selection, high-purity molybdenum powder is adopted, and further purification is carried out in the sintering process, so that the impurity gas content of C, H, O is controlled below 10 ppm. Meanwhile, the vacuum furnace and the hydrogen furnace are adopted for multiple sintering modes, and different from the conventional sintering modes, the sintering time is prolonged, the material is compact, and holes are less. In addition, a high-temperature and low-temperature mixed treatment mode is adopted for the rolled plate, so that a molybdenum product is formed, the impurity content at the grain boundary is low, the plate shape of the material is ensured, the deformation and coarsening are avoided. Compared with the traditional common molybdenum and molybdenum lanthanum alloy, the alloy has obviously better strength and creep resistance, and has obvious advantages as ceramic sintering supporting pieces, high-temperature furnace components, high-temperature deformation resistance bearing pieces, aviation aerospace high Wen Jian and the like.
Drawings
FIG. 1 is a schematic flow chart of a method of preparing high strength molybdenum according to the present invention;
FIG. 2 is a gold phase diagram of the molybdenum prepared according to the present invention at 500 x under a metallographic microscope;
FIG. 3 is a 500 times gold phase diagram of a prior molybdenum product under a metallographic microscope;
FIG. 4 is a schematic illustration of a designed anti-sagging protocol;
FIG. 5 is a schematic representation of a designed anti-deformation protocol.
Detailed Description
The invention will be described in detail below with reference to the drawings and the detailed description.
As shown in fig. 1, the preparation method of the high-strength molybdenum sequentially comprises the steps of raw material selection, mixing, isostatic pressing, sintering, hot rolling, warm rolling, heat treatment, machining and low-temperature shaping treatment. The method comprises the following steps:
s1, selecting raw materials:
the raw material powder is high-purity molybdenum powder with purity of more than 99.99 percent, and the content of Ca, fe, K and other impurities is controlled below 0.01 percent.
S2, mixing:
before pressing, the high-purity molybdenum powder is fully mixed and smashed by a 1000L high-energy mixer, the rotating speed is 3500-4500, the mixing time is 2-4 h, and the original large-particle agglomerated molybdenum powder particles are kept smashed. The purpose is to ensure that the high-purity molybdenum powder has certain fluidity in the subsequent sintering process, and the sintered slab structure is more uniform and compact.
S3, isostatic pressing:
the isostatic pressing technology can lead the molybdenum powder to form microscopic particles under the action of pressure, improves the specific surface area and the activity of the molybdenum powder, and further leads the density of the high-purity molybdenum powder to be higher and uniform, thereby providing a good foundation for the subsequent sintering and hot rolling treatment;
s4, sintering:
in the prior art, electron beam furnace equipment is generally adopted for purification, and the invention is prepared by a powder metallurgy method. Compared with an electron beam furnace, the powder metallurgy method has potential advantages; firstly, the equipment cost is lower than that of an electron beam furnace by 10 times; meanwhile, the powder metallurgy method has simple process, and can further purify and remove impurities in the sintering process, thereby improving the purity of the powder metallurgy method.
In the powder metallurgy sintering process, the invention adopts three stages to sinter.
The first stage is performed by adopting a plurality of modes such as presintering, vacuum sintering and the like, and the vacuum degree of the furnace is required to be 1.0x10 -3 Pa, the presintering temperature is 800-1000 ℃, the presintering temperature is kept for 4-10 h, the gas and the moisture of the sintered slab are removed and volatilized, and the residual stress during pressing is eliminated.
The second stage is vacuum furnace sintering, the sintering temperature is 1700-2100 ℃, and the sintering time is kept for 8-16 h. In the heating process of the vacuum furnace, a gradient slow heating process is adopted, so that the high-purity molybdenum powder is ensured to be completely diffused at high temperature, gas impurities such as C, O, H are further volatilized, the content of the gas impurities is ensured to be reduced to below 10ppm, and the sintering density can be increased. In the working procedure, the sintering temperature is not lower than 1700 ℃, and the heat preservation time is not lower than 8 hours; the temperature is too low, the driving energy in the sintering process is insufficient, the shrinkage of the pores of the material is not obvious, the heat preservation time is too short, powder particles cannot be completely diffused, the sintering neck cannot be completely grown, and the density of the material cannot be improved; the sintering temperature is not more than 2100 ℃, the temperature is not more than 16 hours, and the cost of the sintering furnace is 250 yuan/hour mainly from the production cost. With the increase of time, the manufacturing cost is increased, and the method is uneconomical, so that the sintering temperature and the heat preservation time are in a proper range.
In the third stage, sintering is carried out by adopting a hydrogen furnace, wherein the hydrogen flow is set to be 0.2m 3 /h-0.4m 3 And/h, setting the sintering temperature between 2100-2300 ℃ and maintaining for 8-16 h, during which the reduction of pore size and pore number is ensured, and the sintering density is further increased. The temperature is too high, the molybdenum powder is recrystallized in the crystallization process, so that the structure grows up, the subsequent rolling performance is influenced, and the material is reducedToughness and elongation of (3); at the same time, the temperature is not too low and the time is not too low. This is because at this stage the number of sintered pores and the size will decrease further and the density will reach the highest value; if the temperature is too low, insufficient sintering and more pores are caused, and the material is not compact. By adopting the method, the density of the prepared sintered plate blank is more than 9.5g/cm < 3 >.
S5, hot rolling:
and (3) carrying out hot rolling procedure treatment on the sintered plate blank, wherein the sintering thickness is 35mm, and the cogging temperature is 1000-1300 ℃. In the process, if the cogging temperature is lower than 1000 ℃, the deformation of the material is difficult, and the rolling is easy to crack; above 1300 ℃, the structure coarsens, which has an adverse effect on the subsequent properties.
In this step, the total working ratio is ensured to be more than 90%, and a hot-rolled slab with a thickness of 3.5mm is finally obtained, the density of which is close to the theoretical density of 10.2g/cm 3 . In the actual production process, the invention has the advantage that reversing rolling is needed when the pass processing rate is 30 percent so as to ensure that the grains in the length direction and the width direction are basically consistent.
S6, warm rolling:
preserving heat for 20-40 min at the temperature of 350-450 ℃, and the thickness of the rolled plate is 2.0mm.
S7, heat treatment:
the rolled plate is subjected to high-temperature heat treatment in a sintering furnace, the process is a key process of the whole product, a plurality of plates can be treated each time, the middle is separated by zirconium sand, the treatment temperature is 1900-2100 ℃, and the heat preservation time is kept for 9-10 h.
This step is critical and determines whether molybdenum is capable of being formed without deformation at high temperatures, so that the temperature and time must be controlled strictly to obtain a molybdenum product.
S8, machining:
and (3) carrying out grinding process treatment on the molybdenum product, wherein the thickness dimension is controlled to be +/-0.05 mm, the length and width dimensions are controlled to be +/-0.2 mm, and the flatness is controlled to be less than 0.1 mm. Because the zirconium sand adhered on the surface after molybdenum is treated at high temperature can bring away grains in the length direction under the action of shearing force when a large surface is ground, and macroscopic phenomenon is shown as slag falling phenomenon, the zirconium sand at the edge needs to be polished away firstly when grinding is carried out, so that slag falling is prevented. In addition, the grinding speed is not too high, otherwise deformation is caused, so the grinding frequency is controlled below 17Hz, the grinding feed is controlled below 0.02mm, and the grinding is performed by turning over for multiple times.
S9, low-temperature shaping:
and (3) carrying out low-temperature treatment on the polished plate in a vacuum furnace at 600-800 ℃ for 2-4 hours to eliminate the stress after grinding and ensure the flatness of the material, and finally obtaining the high-strength molybdenum.
In order to further illustrate the technical scheme of the invention, the following specific examples are provided for the purpose of illustration.
Example 1
S1, selecting raw materials:
the raw material powder is high-purity molybdenum powder with purity of more than 99.99 percent, and the content of Ca, fe, K and other impurities is controlled below 0.01 percent.
S2, mixing:
before pressing, the high-purity molybdenum powder is fully mixed by a 1000L high-energy mixer, smashed, and mixed for 2 hours at the rotating speed of 3500 r/min.
S3, isostatic pressing:
and carrying out an isostatic pressing treatment procedure to ensure that the density of the high-purity molybdenum powder is higher and uniform.
S4, sintering:
in the powder metallurgy sintering process, the invention adopts three stages to sinter.
The first stage is performed by adopting a plurality of modes such as presintering, vacuum sintering and the like, and the vacuum degree of the furnace is required to be 1.0x10 -3 Pa, the pre-sintering temperature is 800 ℃, and the pre-sintering time is kept for 4 hours.
The second stage is vacuum furnace sintering, the sintering temperature is 1700 ℃, and the sintering time is kept for 8 hours. In the heating process of the vacuum furnace, a gradient slow heating process is adopted, gas impurities such as C, O, H are further volatilized, and the content of the gas impurities is guaranteed to be reduced to below 10 ppm.
In the third stage, sintering is carried out by adopting a hydrogen furnace, wherein the hydrogen flow is set to be 0.2m 3 And/h, the sintering temperature was set between 2100℃and maintained for 8h. By adopting the method, the density of the prepared sintered plate blank is more than 9.5g/cm < 3 >.
S5, hot rolling:
the sintered slab was subjected to a hot rolling process at a sintered thickness of 35mm and a cogging temperature of 1000 ℃. In this step, the total working ratio is ensured to be more than 90%, and a hot-rolled slab with a thickness of 3.5mm is finally obtained, the density of which is close to the theoretical density of 10.1g/cm 3
S6, warm rolling:
preserving heat for 20min at the temperature of 350 ℃, wherein the thickness of the rolled plate is 2.0mm.
S7, heat treatment:
and (3) carrying out high-temperature heat treatment on the rolled plate in a sintering furnace, wherein a plurality of plates can be treated each time, the middle is separated by zirconium sand, the treatment temperature is 1900 ℃, and the heat preservation time is kept for 9 hours.
S8, machining:
and (3) carrying out grinding process treatment on the molybdenum product, wherein the thickness dimension is controlled to be +/-0.05 mm, the length and width dimensions are controlled to be +/-0.2 mm, and the flatness is controlled to be less than 0.1 mm. During grinding, zirconium sand at the edge is firstly ground away to prevent slag from falling. In addition, the grinding speed is not too fast, the grinding frequency is controlled below 17Hz, the grinding feed is controlled below 0.02mm, and the grinding is performed by turning over for multiple times.
S9, low-temperature shaping:
and (3) carrying out low-temperature treatment on the polished plate in a vacuum furnace at 600 ℃, and preserving heat for 2 hours to finally obtain the high-strength molybdenum.
Example 2
S1, selecting raw materials:
the raw material powder is high-purity molybdenum powder with purity of more than 99.99 percent, and the content of Ca, fe, K and other impurities is controlled below 0.01 percent.
S2, mixing:
before pressing, the high-purity molybdenum powder is fully mixed by a 1000L high-energy mixer, smashed, and mixed for 3 hours at 4000 r/min.
S3, isostatic pressing:
and carrying out an isostatic pressing treatment procedure to ensure that the density of the high-purity molybdenum powder is higher and uniform.
S4, sintering:
in the powder metallurgy sintering process, the invention adopts three stages to sinter.
The first stage is performed by adopting a plurality of modes such as presintering, vacuum sintering and the like, and the vacuum degree of the furnace is required to be 1.0x10 -3 Pa, the pre-sintering temperature is 900 ℃, and the pre-sintering temperature is kept for 7h.
The second stage is vacuum furnace sintering, the sintering temperature is 1900 ℃, and the sintering time is 12 hours. In the heating process of the vacuum furnace, a gradient slow heating process is adopted, gas impurities such as C, O, H are further volatilized, and the content of the gas impurities is guaranteed to be reduced to below 10 ppm.
In the third stage, sintering is carried out by adopting a hydrogen furnace, wherein the hydrogen flow is set to be 0.3m 3 And/h, the sintering temperature is set between 2200 ℃ and maintained for 12h. By adopting the method, the density of the prepared sintered plate blank is more than 9.5g/cm < 3 >.
S5, hot rolling:
the sintered slab was subjected to a hot rolling process at a firing temperature of 1200 ℃ at a firing thickness of 35mm. In this step, the total working ratio is ensured to be more than 90%, and a hot-rolled slab with a thickness of 3.5mm is finally obtained, the density of which is close to the theoretical density of 10.2g/cm 3
S6, warm rolling:
preserving the temperature for 30min at the temperature of 400 ℃, wherein the thickness of the rolled plate is 2.0mm.
S7, heat treatment:
and (3) carrying out high-temperature heat treatment on the rolled plate in a sintering furnace, wherein a plurality of plates can be treated each time, the middle is separated by zirconium sand, the treatment temperature is 2000 ℃, and the heat preservation is carried out for 9.5 hours.
S8, machining:
and (3) carrying out grinding process treatment on the molybdenum product, wherein the thickness dimension is controlled to be +/-0.05 mm, the length and width dimensions are controlled to be +/-0.2 mm, and the flatness is controlled to be less than 0.1 mm. During grinding, zirconium sand at the edge is firstly ground away to prevent slag from falling. In addition, the grinding speed is not too fast, the grinding frequency is controlled below 17Hz, the grinding feed is controlled below 0.02mm, and the grinding is performed by turning over for multiple times.
S9, low-temperature shaping:
and (3) carrying out low-temperature treatment on the polished plate in a vacuum furnace at 700 ℃, and preserving heat for 3 hours to finally obtain the high-strength molybdenum.
Example 3
S1, selecting raw materials:
the raw material powder is high-purity molybdenum powder with purity of more than 99.99 percent, and the content of Ca, fe, K and other impurities is controlled below 0.01 percent.
S2, mixing:
before pressing, the high-purity molybdenum powder is fully mixed by a 1000L high-energy mixer, smashed, and mixed for 4 hours at the rotating speed of 4500 r/min.
S3, isostatic pressing:
and carrying out an isostatic pressing treatment procedure to ensure that the density of the high-purity molybdenum powder is higher and uniform.
S4, sintering:
in the powder metallurgy sintering process, the invention adopts three stages to sinter.
The first stage is carried out by adopting a plurality of modes such as presintering, vacuum sintering and the like, wherein the vacuum degree of a furnace is 1.0x10 < -3 > Pa, the presintering temperature is 1000 ℃, and the presintering is kept for 10 hours.
And sintering in a vacuum furnace at 2100 ℃ for 16h in the second stage. In the heating process of the vacuum furnace, a gradient slow heating process is adopted, gas impurities such as C, O, H are further volatilized, and the content of the gas impurities is guaranteed to be reduced to below 10 ppm.
In the third stage, sintering is carried out by adopting a hydrogen furnace, wherein the hydrogen flow is set to be 0.4m 3 And/h, the sintering temperature is set between 2300 ℃ and maintained for 16h. By adopting the method, the density of the prepared sintered plate blank is more than 9.5g/cm < 3 >.
S5, hot rolling:
the sintered slab was subjected to a hot rolling process at a sintering thickness of 35mm and a cogging temperature of 1300 ℃. In this step, the total working ratio is ensured to be more than 90%, and a hot-rolled slab with a thickness of 3.5mm is finally obtained, the density of which is close to the theoretical density of 10.2g/cm 3
S6, warm rolling:
preserving heat for 40min at the temperature of 450 ℃, wherein the thickness of the rolled plate is 2.0mm.
S7, heat treatment:
and (3) carrying out high-temperature heat treatment on the rolled plate in a sintering furnace, wherein a plurality of plates can be treated each time, the middle of the plates are separated by zirconium sand, the treatment temperature is 2100 ℃, and the plates are kept for 10 hours.
S8, machining:
and (3) carrying out grinding process treatment on the molybdenum product, wherein the thickness dimension is controlled to be +/-0.05 mm, the length and width dimensions are controlled to be +/-0.2 mm, and the flatness is controlled to be less than 0.1 mm. During grinding, zirconium sand at the edge is firstly ground away to prevent slag from falling. In addition, the grinding speed is not too fast, the grinding frequency is controlled below 17Hz, the grinding feed is controlled below 0.02mm, and the grinding is performed by turning over for multiple times.
S9, low-temperature shaping:
and (3) carrying out low-temperature treatment on the polished plate in a vacuum furnace at 800 ℃, and preserving the heat for 4 hours to finally obtain the high-strength molybdenum.
The preparation method adopts high-purity molybdenum powder as raw material, ensures that the purity of the molybdenum material reaches more than 99.99 percent, thereby improving the oxidation resistance, corrosion resistance and heat resistance of molybdenum; through high-temperature sintering and hot rolling treatment, molybdenum crystals can be grown to obtain high-strength molybdenum, and the requirements of high strength and high stability of continuous use of the molybdenum are met; through low-temperature shaping treatment, the grain boundary structure of molybdenum can be optimized, so that the high-temperature characteristic of the molybdenum is improved.
As shown in table 1, the content of impurities such as Al, ca, fe, mg, ni, si, C, N, P, O in the molybdenum of the present invention is far lower than that in pure molybdenum.
TABLE 1 comparison of high strength molybdenum and ordinary pure molybdenum compositions
As shown in FIG. 2, the molybdenum prepared by the invention has smooth surface and no grain boundary as can be seen from a gold phase diagram. As shown in fig. 3, the gold phase diagram of the conventional molybdenum product is equiaxed, has grain boundaries, conventional molybdenum and impurities are easy to segregate at the grain boundaries, and when the product is used at a high temperature exceeding 1600 ℃, the structure grows up, coarsens, the grain boundaries are wider, and the grain boundaries become weak areas of the whole material, so that deformation and even cracking are easy to occur to fracture.
As such, compared with the traditional common molybdenum and molybdenum lanthanum alloy, the molybdenum prepared by the method has obviously better strength and creep resistance, and has obvious advantages as ceramic sintering supporting pieces, high-temperature furnace components, high-temperature deformation-resistant supporting pieces, high Wen Jian on aviation and aerospace and the like.
The main performance parameters of high strength molybdenum are as follows:
(1) The purity of the material is more than 99.99 percent, and the content of C, O, N in impurities is less than or equal to 10ppm;
(2) The density of molybdenum is close to the theoretical density rho and is more than or equal to 10.2g/cm < 3 >;
(3) The grain boundary of the structure is narrow under the high-temperature treatment of molybdenum, and the impurity segregation is less;
(4) After high temperature treatment at 1800 ℃, the deformation resistance is strong and is improved by more than 10 times compared with pure molybdenum.
In order to further verify the properties of the molybdenum prepared by the method of the invention, sag resistance experiments and deformation experiments were specially designed.
The anti-sagging protocol was as follows:
test sample: pure molybdenum sample No. 1, pure molybdenum sample No. 2, molybdenum lanthanum sample No. 3, molybdenum lanthanum sample No. 4, high-strength molybdenum sample No. 5 and high-strength molybdenum sample No. 6;
test sample size: a sheet material with a length of 100mm and a width of 10mm and 2 mm;
test time: 10. hours;
test temperature: 1800 ℃;
the test method comprises the following steps: an anti-deformation experiment was performed using the dead weight of the work, as shown in fig. 4, where l is the deformation amount.
Experimental results: as shown in Table 2, the deformation amount of the high-strength molybdenum prepared by the method is only 0.2. 0.2mm, and the sagging resistance of the high-strength molybdenum is improved by 10 times compared with that of pure molybdenum.
TABLE 2 high strength molybdenum to pure molybdenum, molybdenum lanthanum alloy high temperature deformation resistance comparison (sag resistance experiment)
The anti-deformation protocol was as follows:
test sample: pure molybdenum sample No. 1, pure molybdenum sample No. 2, high-strength molybdenum sample No. 3 and high-strength molybdenum sample No. 4;
test sample: thickness 2mm width 130mm height 260 mm;
test time: 3 hours;
test temperature: 1600 ℃.
Load: 98g;
the test method comprises the following steps: the test panels were supported at four corners with 4 columns of 10mm height and after 3 hours of incubation at 1600℃the flatness was measured as shown in FIG. 5.
Experimental results: as shown in table 3, the flatness of the high-strength molybdenum sample No. 3 and the high-strength molybdenum sample No. 4 were less different before and after deformation, only 0.02; the flatness of the pure molybdenum sample No. 1 and the pure molybdenum sample No. 2 change greatly before and after deformation, and reach 0.13-0.14; therefore, the high-strength molybdenum prepared by the method has better deformation resistance.
TABLE 3 results of anti-deformation test of crystalline molybdenum and pure molybdenum
In conclusion, the molybdenum prepared by the method has good sagging resistance and deformation resistance, excellent high-temperature performance and oxidation resistance, and can stably operate for a long time in a high-temperature environment. Therefore, the method can be widely used for manufacturing the working environments under high-temperature, static pressure and corrosion environments such as ceramic supporting pieces, high-temperature furnaces, vacuum furnaces, nuclear reactors and the like.

Claims (10)

1. The preparation method of the high-strength molybdenum is characterized by comprising the following steps of:
s1, selecting raw materials: selecting high-purity molybdenum powder, wherein the purity of the high-purity molybdenum powder is ensured to be more than 99.99%, and the impurity content of the high-purity molybdenum powder is ensured to be less than 0.01%;
s2, mixing: fully crushing and mixing high-purity molybdenum powder;
s3, isostatic pressing: isostatic pressing is carried out on the crushed high-purity molybdenum powder;
s4, sintering: high-temperature sintering is carried out on the high-purity molybdenum powder subjected to isostatic pressing treatment, and the sintering time is 4-10 h when the temperature is 800-1000 ℃; sintering time is 8-16 h at 1700-2100 ℃; sintering for 8-16 h at 2100-2300 ℃ to finally obtain a plate blank;
s5, hot rolling: carrying out hot rolling treatment on the plate blank, wherein the cogging temperature is 1000-1300 ℃;
s6, warm rolling: preserving heat at the temperature of 350-450 ℃ for 20-40 min, and rolling the plate blank after hot rolling treatment into a plate;
s7, heat treatment: carrying out heat treatment on the plate subjected to warm rolling treatment at 1900-2100 ℃ for 9-10 hours to obtain a high-strength product;
s8, machining: grinding the molybdenum product, wherein the thickness dimension of the molybdenum product is controlled to be +/-0.05 mm, the length and width dimensions of the molybdenum product are controlled to be +/-0.2 mm, and the flatness of the molybdenum product is controlled to be less than 0.1 mm;
s9, low-temperature shaping: the molybdenum product after grinding treatment is stored for 3 hours at 600-800 ℃ for low-temperature treatment, and finally high-strength molybdenum is obtained;
in the powder metallurgy sintering process, three stages are adopted for sintering:
the first stage is carried out by adopting a plurality of modes of pre-sintering and vacuum sintering, and the vacuum degree of the furnace is required to be 1.0x10 -3 Pa, and the presintering temperature is 800-1000 ℃;
the second stage is vacuum furnace sintering, the sintering temperature is 1700-2100 ℃, and a gradient slow heating process is adopted in the heating process of the vacuum furnace, so that the high-purity molybdenum powder is ensured to be completely diffused at high temperature, gas impurities such as C, O, H are further volatilized, the content of the gas impurities is ensured to be reduced to below 10ppm, and the sintering density can be increased;
in the third stage, sintering is carried out by adopting a hydrogen furnace, wherein the hydrogen flow is set to be 0.2m 3 /h-0.4m 3 /h。
2. The method for preparing high-strength molybdenum according to claim 1, wherein the impurities of the high-purity molybdenum powder in S1 include Ca, fe, and K.
3. The method for preparing high-strength molybdenum according to claim 1, wherein the specific process of S2 is: and crushing and fully mixing large-particle agglomerated molybdenum powder particles in the high-purity molybdenum powder by adopting a high-energy mixer, wherein the rotating speed of the high-energy mixer is 3500r/min-4500r/min, and the mixing time is 2h-4h.
4. A method of producing high strength molybdenum as defined in claim 3, wherein the high energy blender is a 1000L high energy blender.
5. The method for preparing high-strength molybdenum according to claim 1, wherein the step S4 is divided into three stages for sintering;
the first stage is carried out by adopting a mode comprising presintering and vacuum sintering, wherein the vacuum degree of the furnace is required to be 1.0x10 -3 Pa, pre-sintering temperature is 800-1000 ℃, and sintering time is 4-10 h;
the second stage is vacuum furnace sintering, gradient slow heating is adopted, and sintering time is 8-16 h when sintering temperature is 1700-2100 ℃;
and in the third stage, sintering is carried out by adopting a hydrogen furnace, wherein the hydrogen flow is 0.3m < 3 >/h, and the sintering time is 8-16 h when the sintering temperature is 2100-2300 ℃ to obtain a sintered plate blank.
6. The method for preparing high-strength molybdenum according to claim 1, wherein the thickness of the slab in S5 is 35mm.
7. The method for preparing high-strength molybdenum according to claim 1, wherein the thickness of the sheet rolled in S6 is 2mm.
8. The method for preparing high-strength molybdenum according to claim 1, wherein the heat-treated plates in S7 are separated by zircon sand.
9. The method for preparing high-strength molybdenum according to claim 1, wherein the frequency of the grinding treatment in S8 is controlled below 17Hz, the feed rate of the grinding treatment is controlled below 0.02mm, and the high-strength molybdenum is subjected to multiple turn-over grinding.
10. The method for preparing high-strength molybdenum according to claim 1, wherein the low-temperature treatment is performed in a vacuum furnace in S9.
CN202310581104.5A 2023-05-23 2023-05-23 Preparation method of high-strength molybdenum Active CN116275050B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202310581104.5A CN116275050B (en) 2023-05-23 2023-05-23 Preparation method of high-strength molybdenum

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202310581104.5A CN116275050B (en) 2023-05-23 2023-05-23 Preparation method of high-strength molybdenum

Publications (2)

Publication Number Publication Date
CN116275050A CN116275050A (en) 2023-06-23
CN116275050B true CN116275050B (en) 2023-08-01

Family

ID=86836350

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202310581104.5A Active CN116275050B (en) 2023-05-23 2023-05-23 Preparation method of high-strength molybdenum

Country Status (1)

Country Link
CN (1) CN116275050B (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN116875838B (en) * 2023-09-08 2023-11-21 西安格美金属材料有限公司 Preparation method of potassium-doped molybdenum alloy plate

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110257784A (en) * 2019-07-24 2019-09-20 洛阳高新四丰电子材料有限公司 A kind of preparation process of high-compactness molybdenum niobium alloy sputtering target material

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102005003445B4 (en) * 2005-01-21 2009-06-04 H.C. Starck Hermsdorf Gmbh Metal substrate material for the anode plates of rotary anode X-ray tubes, method for producing such a material and method for producing an anode plate using such a material
CN101956159A (en) * 2010-09-30 2011-01-26 金堆城钼业股份有限公司 Method for preparing high-purity molybdenum titanium sputtering target
CN103302295B (en) * 2013-06-20 2015-09-02 安泰科技股份有限公司 A kind of method of rolling processing high-purity, high-density molybdenum alloy target
US9238852B2 (en) * 2013-09-13 2016-01-19 Ametek, Inc. Process for making molybdenum or molybdenum-containing strip
CN105483626B (en) * 2015-12-09 2018-01-16 西安瑞福莱钨钼有限公司 A kind of production method of fine grain planar molybdenum target material
CN106399787B (en) * 2016-08-31 2018-06-01 安泰天龙(天津)钨钼科技有限公司 A kind of high temperature and creep resistance molybdenum plate for adulterating K, Si element and preparation method thereof
CN113000844A (en) * 2019-12-21 2021-06-22 张玉琪 Preparation method of large-size molybdenum plate
CN112126822B (en) * 2020-08-31 2021-11-23 江苏大学 Rolling (FeCoNiCrR)n/Al) -2024Al composite board and preparation method thereof

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110257784A (en) * 2019-07-24 2019-09-20 洛阳高新四丰电子材料有限公司 A kind of preparation process of high-compactness molybdenum niobium alloy sputtering target material

Also Published As

Publication number Publication date
CN116275050A (en) 2023-06-23

Similar Documents

Publication Publication Date Title
CN116275050B (en) Preparation method of high-strength molybdenum
CN109796209B (en) (Ti, Zr, Hf, Ta, Nb) B2High-entropy ceramic powder and preparation method thereof
CN111370191A (en) Heavy rare earth element-free samarium-cobalt permanent magnet material with low coercive force temperature coefficient and high temperature and preparation method thereof
CN115198162B (en) Entropy alloy in high-toughness heterogeneous multi-phase core-shell organization structure and preparation method thereof
CN109898005B (en) High-strength WVTaZrHf refractory high-entropy alloy and preparation method thereof
CN111996397A (en) Method for regulating hydrogen embrittlement resistance and corrosion resistance of CoNiV medium-entropy alloy
CN101956112B (en) Mo-Ce alloy wire and preparation method thereof
CN113930696A (en) Preparation method of light titanium-rich Ti-Zr-Nb-Al series refractory high-entropy alloy-based composite material
KR101288592B1 (en) Method of manufacturing an oxide dispersion strengthened platinum-rhodium alloy
CN111621659A (en) Method for preparing Ti2AlNb alloy by powder metallurgy method
CN112853283A (en) Chromium-nickel alloy sputtering target material and preparation method and application thereof
KR101587837B1 (en) Molybdenum material
CN113862546B (en) High-strength high-toughness high-entropy alloy and preparation method thereof
KR101560455B1 (en) LCD Glass METHOD OF MANUFACTURING AN OXIDE DISPERSION STRENGTHENED PLATINUMRHODIUM ALLOYS MATERIALS USING SPARK PLASMA SINTERING FOR LIQUID CRYSTAL DISPLAY GLASS MANUFACTURING
JPH07233434A (en) Corrosion resistant material and its production
CN115011838A (en) Rare earth modified titanium alloy and preparation method and application thereof
CN117884617A (en) Preparation method of high-plasticity recrystallized molybdenum and molybdenum alloy
KR101279555B1 (en) Method of manufacturing an oxide dispersion strengthened Platinum materials using a Cross-roll
CN111590071B (en) Molybdenum-niobium alloy target material and preparation method thereof
CN115386759B (en) Ti (C) 7 ,N 3 )/TiB 2 WC micro-nano composite metal ceramic cutter material and preparation method thereof
CN114850473B (en) Sintering method and application of molybdenum and molybdenum alloy material
CN116037933A (en) Ti (titanium) 2 Preparation method of AlNb powder metallurgy material
CN115710667A (en) Refractory high-entropy alloy with high strength and toughness and high thermal stability at room temperature and preparation method thereof
CN114350997A (en) Uranium molybdenum niobium alloy fuel pellet and preparation method and application thereof
CN112863718A (en) Preparation method of UMoZr dispersed fuel

Legal Events

Date Code Title Description
PB01 Publication
PB01 Publication
SE01 Entry into force of request for substantive examination
SE01 Entry into force of request for substantive examination
GR01 Patent grant
GR01 Patent grant