CN102618739B - Aluminum molybdenum vanadium chromium iron intermediate alloy and preparation method thereof - Google Patents

Aluminum molybdenum vanadium chromium iron intermediate alloy and preparation method thereof Download PDF

Info

Publication number
CN102618739B
CN102618739B CN2012101137290A CN201210113729A CN102618739B CN 102618739 B CN102618739 B CN 102618739B CN 2012101137290 A CN2012101137290 A CN 2012101137290A CN 201210113729 A CN201210113729 A CN 201210113729A CN 102618739 B CN102618739 B CN 102618739B
Authority
CN
China
Prior art keywords
percent
parts
starting material
smelting
carry out
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
CN2012101137290A
Other languages
Chinese (zh)
Other versions
CN102618739A (en
Inventor
陆树兴
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.)
SHANGHAI KANGCHEN SPECIAL METAL MATERIALS CO Ltd
Original Assignee
SHANGHAI KANGCHEN SPECIAL METAL MATERIALS 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 SHANGHAI KANGCHEN SPECIAL METAL MATERIALS CO Ltd filed Critical SHANGHAI KANGCHEN SPECIAL METAL MATERIALS CO Ltd
Priority to CN2012101137290A priority Critical patent/CN102618739B/en
Publication of CN102618739A publication Critical patent/CN102618739A/en
Application granted granted Critical
Publication of CN102618739B publication Critical patent/CN102618739B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Abstract

The invention discloses an aluminum molybdenum vanadium chromium iron intermediate alloy, which comprises the following components in percentage by weight: 25-40 percent of Mo, 25-40 percent of V, 3-9 percent of Cr, 3-9 percent of Fe, less than or equal to 0.35 percent of Si, less than or equal to 0.2 percent of O, less than or equal to 0.05 percent of C, less than or equal to 0.05 percent of N, less than or equal to 0.2 percent of Cu, less than or equal to 0.1 percent of Mn and the balance Al. The invention also provides a preparation method of the aluminum molybdenum vanadium chromium iron intermediate alloy. According to the invention, smelting is performed by using a two-step method; compared with the conventional smelting method outside a furnace, the obtained ingredients are more uniform, particularly Al, Fe and Cr are added in the two steps at twice respectively, so that the uniformity of the ingredients is better than that in the case of one addition process; in addition, a unique smelting method that a carbon crucible coated with a yttrium oxide layer is used in a vacuum furnace as a smelting container is adopted; and thus, compared with the conventional copper crucible needing to be water-cooled, the manufacturing cost is greatly reduced, and the introduction of impurities can also be excellently controlled.

Description

A kind of aluminium Mo-V-Cr iron master alloy and preparation method thereof
Technical field
The present invention relates to a kind of master alloy and preparation method thereof, relate in particular to a kind of aluminium Mo-V-Cr iron master alloy of smelting use and preparation method thereof.
Background technology
, along with the development of titanium alloy, adopt master alloy to add in the smelting of titanium alloy more and more general.Master alloy for adding, require segregation-free, and without metal inclusion, foreign matter content is low as much as possible.
Present master alloy adopts single stage method to smelt more, and the alloy of smelting not only foreign matter content is higher, and homogeneity is not fine.
Summary of the invention
The object of the present invention is to provide a kind of aluminium Mo-V-Cr iron master alloy and preparation method thereof, the foreign matter content of aluminium Mo-V-Cr iron master alloy can reach titanium alloy and smelt the requirement of adding, and the preparation method of master alloy can more easily control.
A kind of aluminium Mo-V-Cr iron master alloy provided by the invention, comprise following component: Mo25~40%, V25~40%, Cr3~9%, Fe3~9%, Si≤0.35%, O≤0.2%, C≤0.05%, N≤0.05%, Cu≤0.2%, Mn≤0.1%, and surplus is Al; Wherein, described per-cent is weight percentage; Described aluminium Mo-V-Cr iron master alloy prepares as follows:
1) according to MoO 3100 parts, V 2O 598~139 parts, Al114~216 part, CaF 218~45 parts, 24~50 parts, slag, Fe5~21 part, Cr0~21 part take each starting material;
2), with the shove charge at normal temperatures of each starting material, adopt the outer aluminothermy smelting method of stove to carry out the first step and smelt;
3) measure in addition the Cr starting material of 0~1 part of Al, the Fe of 0~3 part and 1~13 part and smelt in the first step primary products that obtain and be placed in together vacuum melting furnace and carry out vacuum melting, the smelting temperature of vacuum melting is 1450~1600 ℃, vacuum tightness is less than 0.67Pa, the rear refining 6~15 minutes of seething with excitement in short-term under the high temperature of 1500 ℃ of furnace charge fusing, and carry out alloy casting under vacuum condition.
Preferably, comprise following component: Mo25~40%, V25~40%, Cr3~9%, Fe3~9%, Si≤0.15%, O≤0.1%, C≤0.05%, N≤0.05%, Cu≤0.1%, Mn≤0.05%, surplus is Al; Wherein, described per-cent is weight percentage.
Preferably, comprise following component: Mo25~40%, V25~40%, Cr3~9%, Fe3~9%, Si≤0.1%, O≤0.02%, C≤0.02%, N≤0.02%, Cu≤0.05%, Mn≤0.05%, surplus is Al; Wherein, described per-cent is weight percentage.
The present invention also provides a kind of preparation method of aluminium Mo-V-Cr iron master alloy, comprises the steps:
1) according to MoO 3100 parts, V 2O 598~139 parts, Al114~216 part, CaF 218~45 parts, 24~50 parts, slag, Fe5~21 part, Cr0~21 part take each starting material;
2), with the shove charge at normal temperatures of each starting material, adopt the outer aluminothermy smelting method of stove to carry out the first step and smelt;
3) measure in addition the Cr starting material of 0~1 part of Al, the Fe of 0~3 part and 1~13 part and smelt in the first step primary products that obtain and be placed in together vacuum melting furnace and carry out vacuum melting, the smelting temperature of vacuum melting is 1450~1600 ℃, vacuum tightness is less than 0.67Pa, the rear refining 6~15 minutes of seething with excitement in short-term under the high temperature of 1500 ℃ of furnace charge fusing, and carry out alloy casting under vacuum condition.
Preferably, when described vacuum melting furnace carries out melting, adopt carbon crucible filling furnace charge, and apply one deck yttrium oxide in described carbon crucible.
The present invention is by adopting two-step approach to smelt, the outer smelting method of the existing stove of comparing, the composition that obtains is more even, especially adopts in two steps and adds at twice respectively Al, Fe and Cr, make that the homogeneity of composition more once adds better; In addition, the present invention has also adopted in vacuum oven and has used and be coated with the unique smelting process of the carbon crucible of one deck yttrium oxide as smelting vessel, like this, with the water-cooled copper crucible that will adopt in the past, compares, manufacturing cost reduces greatly, and also can control preferably the introducing of impurity.
Embodiment
The present invention adopts two-step approach to smelt aluminium Mo-V-Cr iron master alloy, mainly comprises the steps:
1) according to MoO 3100 parts, V 2O 598~139 parts, Al114~216 part, CaF 218~45 parts, 24~50 parts, slag, Fe5~21 part, Cr0~21 part take each starting material;
2), with the shove charge at normal temperatures of each starting material, adopt the outer aluminothermy smelting method of stove to carry out the first step and smelt;
3) will measure in addition the Cr starting material of 0~1 part of Al, the Fe of 0~3 part and 1~13 part and smelt in the first step primary products that obtain and be placed in together vacuum melting furnace and carry out vacuum melting, the smelting temperature of vacuum melting is 1450~1600 ℃, vacuum tightness is less than 0.67Pa, after furnace charge is melted to 1/4 to 2/5, can be filled with argon gas, furnace pressure is remained in 50~80Pa, to prevent that in stove, solution too seethes with excitement.After furnace charge in stove melts fully, make in stove and carry out short time high temperature boiling refining, refining time is 6~15 minutes, temperature 〉=1500 ℃.Until the alloy liquid level is tranquil, overflow without bubble, then when being 1480~1550 ℃, the alloy solution temperature casts.
In step 3), what the present invention adopted in vacuum oven is the carbon crucible, and at the internal surface of crucible, is coated with one deck yttrium oxide.Owing to adopting such container to load the alloy of smelting, compared with adopt the water-cooled copper crucible in the past on the one hand, production cost reduces greatly, and, also can keep good stability due to yttrium oxide under the condition of 1450~1600 ℃, therefore can prevent from introducing other impurity in the process of smelting, the control of the homogeneity of the tissue of alloy and the content of impurity plays a good role.
In addition, the present invention adds starting material Al, Fe and Cr in two steps in step 3), can make more disposable the wanting better of adding in the first step of homogeneity of composition.In addition, in the present invention, the yttrium oxide of coating preferably adopts analytically pure yttrium oxide.
In addition, in step 2) in, employing be that the outer thermite reaction of stove is smelted method, low as much as possible in order to make N content, for example,, lower than 0.001%, adopt vacuum aluminum thermal response smelting process in stove, specific practice is:
The starting material of step 1) weighing are put in crucible, then crucible is placed in vacuum oven, and connect the portfire of igniting, vacuumize, and then be filled with helium, by portfire, light a fire, thereby carry out thermite reaction.
Below, come by specific embodiment that the present invention is further described, the concrete method that adopts is same as the above-mentioned method.
Embodiment 1
The batching weight take Kg as unit, MoO 3100Kg, V 2O 5117.8Kg, Al114.7Kg, CaF 238.1Kg, slag 44.4Kg, Fe9.09Kg take each starting material; Add 0.2KgAl, 2.4KgFe and the 11.6KgCr that measures in addition in step 3), smelt through two steps the alloy component that obtains as follows:
Mo is 34%, V is 33.5%, Fe is 6.6%, Cr is 6.38%, Si is 0.05%, O is 0.06%, C is 0.1%, B is 0.006%, N is 0.02%, P is 0.03%, Cu is 0.08%, Mn is 0.05%; Surplus is Al; Wherein, the per-cent here is weight percentage.
It is that stove is smelted outward that the two step smelting method the first steps of the present embodiment adopt.
Embodiment 2
The batching weight take Kg as unit, MoO 3100Kg, V 2O 5100Kg, Al113.3Kg, CaF 230.4Kg, slag 40.6Kg, Fe5.8Kg, Cr1.45Kg take each starting material; Add 3.9KgFe and the 9KgCr that measures in addition in step 3), smelt through two steps the alloy component that obtains as follows:
Mo is 35.64%, V is 34.95%, Fe is 6.91%, Cr is 6.99%, Si is 0.07%, O is 0.07%, C is 0.08%, B is 0.007%, N is 0.002%, P is 0.02%, Cu is 0.08%, Mn is 0.04%; Surplus is Al; Wherein, the per-cent here is weight percentage.
It is vacuum metling in stove that the two step smelting method the first steps of the present embodiment adopt.
Embodiment 3
The batching weight take Kg as unit, MoO 3100Kg, V 2O 5100Kg, Al128.2Kg, CaF 234.2Kg, slag 26.1Kg, Fe5.8Kg take each starting material; Add 1.2KgFe and the 6KgCr that measures in addition in step 3), smelt through two steps the alloy component that obtains as follows:
Mo is 34.1%, V is 33.7%, Fe is 3.71%, Cr is 3.89%, Si is 0.06%, O is 0.06%, C is 0.09%, B is 0.008%, N is 0.002%, P is 0.02%, Cu is 0.06%, Mn is 0.04%; Surplus is Al; Wherein, the per-cent here is weight percentage.
It is vacuum metling in stove that the two step smelting method the first steps of the present embodiment adopt.

Claims (5)

1. an aluminium Mo-V-Cr iron master alloy, is characterized in that, comprise following component: Mo25~40%, V25~40%, Cr3~9%, Fe3~9%, Si≤0.35%, O≤0.2%, C≤0.05%, N≤0.05%, Cu≤0.2%, Mn≤0.1%, surplus is Al; Wherein, described per-cent is weight percentage; Described aluminium Mo-V-Cr iron master alloy prepares as follows:
1) according to MoO 3100 parts, V 2O 598~139 parts, Al114~216 part, CaF 218~45 parts, 24~50 parts, slag, Fe5~21 part, Cr0~21 part take each starting material;
2), with the shove charge at normal temperatures of each starting material, adopt the outer aluminothermy smelting method of stove to carry out the first step and smelt;
3) measure in addition the Cr starting material of 0~1 part of Al, the Fe of 0~3 part and 1~13 part and smelt in the first step primary products that obtain and be placed in together vacuum melting furnace and carry out vacuum melting, the smelting temperature of vacuum melting is 1450~1600 ℃, vacuum tightness is less than 0.67Pa, the rear refining 6~15 minutes of seething with excitement in short-term under the high temperature of 1500 ℃ of furnace charge fusing, and carry out alloy casting under vacuum condition.
2. aluminium Mo-V-Cr iron master alloy as claimed in claim 1, it is characterized in that, comprise following component: Mo25~40%, V25~40%, Cr3~9%, Fe3~9%, Si≤0.15%, O≤0.1%, C≤0.05%, N≤0.05%, Cu≤0.1%, Mn≤0.05%, surplus is Al; Wherein, described per-cent is weight percentage.
3. aluminium Mo-V-Cr iron master alloy as claimed in claim 2, it is characterized in that, comprise following component: Mo25~40%, V25~40%, Cr3~9%, Fe3~9%, Si≤0.1%, O≤0.02%, C≤0.02%, N≤0.02%, Cu≤0.05%, Mn≤0.05%, surplus is Al; Wherein, described per-cent is weight percentage.
4. the preparation method of an aluminium Mo-V-Cr iron master alloy, is characterized in that, comprises the steps:
1) according to MoO 3100 parts, V 2O 598~139 parts, Al114~216 part, CaF 218~45 parts, 24~50 parts, slag, Fe5~21 part, Cr0~21 part take each starting material;
2), with the shove charge at normal temperatures of each starting material, adopt the outer aluminothermy smelting method of stove to carry out the first step and smelt;
3) measure in addition the Cr starting material of 0~1 part of Al, the Fe of 0~3 part and 1~13 part and smelt in the first step primary products that obtain and be placed in together vacuum melting furnace and carry out vacuum melting, the smelting temperature of vacuum melting is 1450~1600 ℃, vacuum tightness is less than 0.67Pa, the rear refining 6~15 minutes of seething with excitement in short-term under the high temperature of 1500 ℃ of furnace charge fusing, and carry out alloy casting under vacuum condition.
5. method as claimed in claim 4, is characterized in that, when described vacuum melting furnace carries out melting, adopts carbon crucible filling furnace charge, and apply one deck yttrium oxide in described carbon crucible.
CN2012101137290A 2012-04-18 2012-04-18 Aluminum molybdenum vanadium chromium iron intermediate alloy and preparation method thereof Active CN102618739B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN2012101137290A CN102618739B (en) 2012-04-18 2012-04-18 Aluminum molybdenum vanadium chromium iron intermediate alloy and preparation method thereof

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN2012101137290A CN102618739B (en) 2012-04-18 2012-04-18 Aluminum molybdenum vanadium chromium iron intermediate alloy and preparation method thereof

Publications (2)

Publication Number Publication Date
CN102618739A CN102618739A (en) 2012-08-01
CN102618739B true CN102618739B (en) 2013-11-13

Family

ID=46558939

Family Applications (1)

Application Number Title Priority Date Filing Date
CN2012101137290A Active CN102618739B (en) 2012-04-18 2012-04-18 Aluminum molybdenum vanadium chromium iron intermediate alloy and preparation method thereof

Country Status (1)

Country Link
CN (1) CN102618739B (en)

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103911537B (en) * 2014-03-31 2016-09-14 承德天大钒业有限责任公司 A kind of aluminum vanadium ferrochrome titanium intermediate alloy and preparation method thereof
CN106947904B (en) * 2016-01-06 2018-07-03 宝钢特钢有限公司 It is a kind of for aluminium vanadium molybdenum chromium zirconium intermediate alloy of TB9 titanium alloys and preparation method thereof
CN107312963B (en) * 2017-07-17 2018-11-30 攀钢集团研究院有限公司 A kind of molybdenum vanadium manganese iron intermediate alloy and preparation method thereof
CN107829006A (en) * 2017-10-24 2018-03-23 沈阳理工大学 A kind of molybdenum-iron aluminium silicon titanium intermediate alloy and preparation method thereof
CN110343929B (en) * 2019-08-22 2020-12-22 承德天大钒业有限责任公司 Aluminum-molybdenum-vanadium intermediate alloy and preparation method thereof
CN112126806B (en) * 2020-09-15 2021-07-09 承德天大钒业有限责任公司 Preparation method of aluminum molybdenum chromium iron silicon intermediate alloy
CN112680647A (en) * 2020-11-30 2021-04-20 攀钢集团钒钛资源股份有限公司 Production method of vanadium-molybdenum-chromium-iron aluminum alloy

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101451206A (en) * 2007-11-30 2009-06-10 中国科学院金属研究所 Superhigh intensity titanium alloy
CN101545061A (en) * 2009-04-30 2009-09-30 武汉泛洲中越合金有限公司 Multivariate interalloy and smelting method thereof

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101451206A (en) * 2007-11-30 2009-06-10 中国科学院金属研究所 Superhigh intensity titanium alloy
CN101545061A (en) * 2009-04-30 2009-09-30 武汉泛洲中越合金有限公司 Multivariate interalloy and smelting method thereof

Also Published As

Publication number Publication date
CN102618739A (en) 2012-08-01

Similar Documents

Publication Publication Date Title
CN102534315B (en) Al-Mo intermediate alloy and preparing method thereof
CN102618739B (en) Aluminum molybdenum vanadium chromium iron intermediate alloy and preparation method thereof
CN102534316B (en) Al-Mo-W-Ti intermediate alloy and preparing method thereof
CN102373350B (en) Preparation method for special aluminum-silicon-magnesium alloy for advanced car wheel hub
CN102719682B (en) Smelting method of GH901 alloy
CN110408806B (en) Aluminum niobium tantalum intermediate alloy and preparation method thereof
CN100480410C (en) Vacuum grade aluminum-molybdenum-silicon alloy
CN102628130B (en) Aluminum tin zirconium molybdenum chromium intermediate alloy and preparation method thereof
CN113444891B (en) Method for producing rare earth-containing high-temperature alloy by adopting rare earth oxide
CN102560213B (en) Aluminum-niobium interalloy and preparation method thereof
CN104152710B (en) The smelting process of esr refining slag and application thereof
CN110396605A (en) A kind of preparation method of wrought superalloy ingot casting
CN110453085A (en) The electroslag remelting heat resisting steel of 9Cr containing Type B slag system, preparation method and application method
WO2018228140A1 (en) Method for preparing ferrotitanium alloy based on aluminothermic self-propagating gradient reduction and slagging refining
CN103468864B (en) 1Cr21Ni5Ti steel smelting method
CN101418365B (en) Magnesia-alumina-ferroalloy preparation method
CN112126806B (en) Preparation method of aluminum molybdenum chromium iron silicon intermediate alloy
CN102618767B (en) Vanadium aluminum iron intermediate alloy and preparation method thereof
CN102634697A (en) Aluminum-manganese intermediate alloy and preparation method thereof
CN110230002B (en) Martensite steel and preparation method thereof
CN104404279A (en) Aluminum-magnesium-beryllium intermediate alloy and preparation method thereof
CN101619405A (en) Ti-Al series intermetallic compound alloy
CN103691913B (en) The manufacture method of 1Mn18Cr18N hollow steel ingot
CN113403492B (en) Preparation method of ultra-low-sulfur high-temperature alloy
CN104099487A (en) Preparation method for silicon-calcium alloy

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
C14 Grant of patent or utility model
GR01 Patent grant