CN105855527A - Continuous casting machine - Google Patents

Continuous casting machine Download PDF

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Publication number
CN105855527A
CN105855527A CN201610319814.0A CN201610319814A CN105855527A CN 105855527 A CN105855527 A CN 105855527A CN 201610319814 A CN201610319814 A CN 201610319814A CN 105855527 A CN105855527 A CN 105855527A
Authority
CN
China
Prior art keywords
tail
drive sprocket
head
mould
nozzle
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.)
Pending
Application number
CN201610319814.0A
Other languages
Chinese (zh)
Inventor
孟要谦
孟洋
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.)
Ningxia Zhuyuan Machinery Repair Co Ltd
Original Assignee
Ningxia Zhuyuan Machinery Repair 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 Ningxia Zhuyuan Machinery Repair Co Ltd filed Critical Ningxia Zhuyuan Machinery Repair Co Ltd
Priority to CN201610319814.0A priority Critical patent/CN105855527A/en
Publication of CN105855527A publication Critical patent/CN105855527A/en
Pending legal-status Critical Current

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Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22DCASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
    • B22D35/00Equipment for conveying molten metal into beds or moulds
    • B22D35/04Equipment for conveying molten metal into beds or moulds into moulds, e.g. base plates, runners
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22DCASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
    • B22D29/00Removing castings from moulds, not restricted to casting processes covered by a single main group; Removing cores; Handling ingots
    • B22D29/04Handling or stripping castings or ingots
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22DCASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
    • B22D30/00Cooling castings, not restricted to casting processes covered by a single main group

Abstract

The invention provides a continuous casting machine, and belongs to metallurgical equipment. The continuous casting machine comprises a machine head frame, a machine body frame, a machine tail frame, a die, machine head transmission chain wheels, a machine head transmission main shaft, a machine tail transmission chain wheel, a machine tail transmission shaft, a motor, a speed reducer, a transmission chain, cooling devices, a die releasing agent spraying device, a die releasing device and a casting port, wherein the machine head frame, the machine body frame and the machine tail frame are all of rectangular steel frame structures and are sequentially integrally fixedly connected; bearing blocks which are assembled to the machine head transmission main shaft are mounted at two sides of the machine head frame; the machine head transmission chain wheels are mounted at two ends of the machine head transmission main shaft. The continuous casting machine is simple in structure; all components can be independently dismounted and replaced, so that the convenience of maintenance is ensued, a plurality of problems caused by manual breaking can be completely solved, and as a result, huge economic benefits can be brought to metallurgical enterprises.

Description

Continuous casting machine
Technical field:
The invention belongs to a kind of metallurgical equipment, invention entitled continuous casting machine.
Background technology:
In metal smelt industry, after the metal cools of molten condition is solidified, how according to client Demand go to make fragment, become the biggest problem, past majority is all molten by smelted Melt metal to pour in a cooling bay the biggest, after waiting its solidification, then by manpower by bulk Alloy breaks down is opened, the most original mode, has shortcomings, uses artificial, and cost is very big, In shattering process, the chip sputtered easily is hurted sb.'s feelings, danger close, in broken product out Having the broken foam of at least 20%, when these broken foams are sold, price just can not show a candle to qualified products, makes Become loss.
The ferroalloy casting machine proposed in documents (Application No. 200810230825.7), Lack releasing agent spraying process, make the alloy of cast into molds be difficult to from mould depart from, underlying Cooling water spray equipment can leak, hit the demoulding thick stick demoulding during die flip, because lacking de- Mould agent, its demoulding efficiency is inevitable low, and mould overturns for a long time, causes described locating shaft Heavy wear, mould taps demoulding thick stick for a long time, the most as easy as rolling off a log causes mould to damage, and lacks and subtracts Speed device and the buffering of shaft coupling, the most easily cause burn-down of electric motor, and repair and replacement are all wasted time and energy, In sum, there is significant drawback in ferroalloy casting machine disclosed in documents.
Summary of the invention:
Therefore, it is necessary to a kind of simple in construction is provided, and can quantity-produced casting machine.
Continuous casting machine, including headstock, fuselage cradle, aircraft tail shelf, mould, head driving-chain Wheel, head transmission main shaft, tail drive sprocket, tail power transmission shaft, motor, decelerator, biography Dynamic chain, chiller, mold releasing agent spraying device, stripper apparatus and casting gate;Headstock, Fuselage cradle and aircraft tail shelf are rectangular bar of steel shelf structure, and headstock, fuselage cradle and aircraft tail shelf are solid successively Surely link together;Bearing block, head transmission main shaft and headstock two are installed in the both sides of headstock The bearing block of side is equipped with, and head drive sprocket is installed at the two ends of head transmission main shaft;Aircraft tail shelf Bearing block is installed in both sides, and the bearing block of tail power transmission shaft and aircraft tail shelf both sides is equipped with, tail transmission Tail drive sprocket is installed at the two ends of axle;Head drive sprocket and the installation position of tail drive sprocket Put corresponding;Motor and decelerator are arranged on headstock with the side at headstock, motor and Decelerator is in transmission connection, and the clutch end of decelerator and one end of shaft coupling connect, shaft coupling The other end and head transmission main shaft one end connect;Driving chain is arranged on head transmission main shaft Between the head drive sprocket of both sides and the tail drive sprocket of tail power transmission shaft both sides, become parallel right Claim around head drive sprocket and tail drive sprocket Synchronous Transmission;Motor passes through decelerator band motivation Head transmission main shaft rotates, and head transmission main shaft rotational band motivation head drive sprocket rotates, and head passes Movable sprocket can drive tail drive sprocket by driving chain;The two ends of mould are respectively and transmission Chain becomes vertical being arranged between two driving chains;Casting gate is arranged on aircraft tail shelf top die Above tool, the running channel alignment mould of casting gate can make molten steel flow into mould uniformly;Releasing agent Spray equipment is parallel is fixedly mounted on aircraft tail shelf rearward end, the shower nozzle direction of mold releasing agent spraying device Just releasing agent is uniformly sprayed on mould by mould;Stripper apparatus be installed on driving chain it Between, inside head drive sprocket and be fixedly mounted on fuselage cradle;Chiller is fixedly mounted on On fuselage cradle, coolant is just uniformly sprayed at mould by the shower nozzle direction of chiller by mould On.
Preferably, stripper apparatus uses the vibration demoulding, by the vibration of certain frequency, taps mould Tool, coordinates effect and the cooling effect of cooling water of releasing agent, makes alloy pig all from mould Depart from.
Preferably, described chiller includes coolant hose, shower nozzle and axial flow blower;Coolant The outlet of pipe and shower nozzle fixed installation, the outlet of shower nozzle and the outlet of axial flow blower are equidirectional parallel Fixed installation.What coolant was the most frequently used cools down water exactly, and the effect of chiller is to cool down Water atomization is sprayed on mould, reduces mold temperature, makes alloy pig and mould be rapidly separated, contracting Short cooling cycle and mold use life-span and use cycle can be extended.
Preferably, described mold releasing agent spraying device include nozzle, regulation short tube, clamp nut, Pipe joint, nozzle holder, main support and pipeline;Suit regulation short tube, nozzle tail in the middle part of nozzle One end of end and pipe joint is equipped with, and the other end of pipe joint and pipeline are equipped with, and nozzle holder is straight Corner structure, nozzle holder two ends are shaped with hole, and nozzle is fixedly mounted on nozzle holder by clamp nut In the hole at two ends, two nozzles are at a right angle to be mounted opposite, and nozzle holder is arranged on above main support. Nozzle is for being arranged in pairs, and every pair of nozzle is divided into release agent nozzle and gas nozzle, and releasing agent flows out Coordinate gas injection to be atomized completely by releasing agent, uniformly spray on mould, according to mould The width in tool face, optional multipair nozzle is mounted side by side use at equal intervals.
The present invention possesses advantages below: thoroughly break away from original hand breaking, reduces cost of labor, Working environment also can be substantially improved, and occurs the accident hurted sb.'s feelings of splashing never again;Owing to connecting Continuous metaplasia is produced, and its efficiency also is able to rise to conventional several times even decades of times, and work efficiency surpasses Amount improves;The broken foam amount of the generation of hand breaking is very big, and broken foam amount can be reduced by the present invention To zero, the final alloy ingot of output all can reach the granularity of customer demand, and economic benefit is big Big lifting.
Compared to documents, mould is fixed on driving chain by the present invention, will not overturn, Use the built-in vibration stripper apparatus demoulding, mould will not be made to tap, do not cause abrasion and damage, Protect mould and drive system, it is ensured that safety in production, be substantially reduced maintenance cost, cooling Device is arranged on above mould, and cooling water all can spray on mould and alloy pig, will not Water clock, and can rapidly mould and alloy pig be cooled down, releasing agent is sprayed on die surface, both protects Having protected mould can make again the use of alloy pig quicker de-mold, decelerator and shaft coupling well protect Motor, makes the operating that motor can be the most stable, it is achieved safe and continuous produces.
Accompanying drawing illustrates:
Fig. 1 is the structural representation of casting machine.
Fig. 2 is the structural representation of chiller.
Fig. 3 is mold releasing agent spraying device structural representation.
In figure: headstock 1, fuselage cradle 2, aircraft tail shelf 3, mould 4, head drive sprocket 5, machine Tail drive sprocket 6, motor 7, decelerator 8, chiller 9, mold releasing agent spraying device 10, Stripper apparatus 11, casting gate 12, head transmission main shaft 13, tail power transmission shaft 14, driving-chain Bar 15, coolant hose 91, shower nozzle 92, axial flow blower 93, nozzle 101, regulation short tube 102, Clamp nut 103, pipe joint 104, nozzle holder 105, main support 106 and pipeline 107.
Detailed description of the invention:
Refer to continuous casting machine as shown in Figure 1, including headstock 1, fuselage cradle 2, machine Tailstock 3, mould 4, head drive sprocket 5, head transmission main shaft 13, tail drive sprocket 6, tail power transmission shaft 14, motor 7, decelerator 8, driving chain 15, chiller 9, Mold releasing agent spraying device 10, stripper apparatus 11 and casting gate 12;Headstock 1, fuselage cradle 2 Being rectangular bar of steel shelf structure with aircraft tail shelf 3, headstock 1, fuselage cradle 2 and aircraft tail shelf 3 are successively It is fixed together;Bearing block, head transmission main shaft 13 and machine are installed in the both sides of headstock 1 The bearing block of the headstock 1 both sides is equipped with, and head driving-chain is installed at the two ends of head transmission main shaft 13 Wheel 5;Bearing block, tail power transmission shaft 14 and aircraft tail shelf 3 both sides are installed in the both sides of aircraft tail shelf 3 Bearing block is equipped with, and tail drive sprocket 6 is installed at the two ends of tail power transmission shaft 14;Head driving-chain Wheel 5 is corresponding with the installation site of tail drive sprocket 6;Motor 7 and decelerator 8 are with at machine The side of the headstock 1 is arranged on headstock 1, and motor 7 and decelerator 8 are in transmission connection, and slows down The clutch end of device 8 and one end of shaft coupling connect, the other end of shaft coupling and head transmission One end of main shaft 13 connects;Driving chain 15 is arranged on the head of head transmission main shaft 13 both sides Between the tail drive sprocket 6 of drive sprocket 5 and tail power transmission shaft 14 both sides, become Parallel Symmetric Around head drive sprocket 5 and tail drive sprocket 6 Synchronous Transmission;Motor 7 is by decelerator 8 Head transmission main shaft 13 is driven to rotate, head transmission main shaft 13 rotational band motivation head drive sprocket 5 rotate, and head drive sprocket 5 can drive tail drive sprocket 6 by driving chain 15; The two ends of mould 4 become with driving chain 15 respectively vertical be arranged on two driving chains 15 it Between;Casting gate 12 is arranged on above aircraft tail shelf 3 top mold 4, the running channel pair of casting gate 12 Quasi-mode tool 4 can make molten steel flow into mould 4 uniformly;Mold releasing agent spraying device 10 is parallel solid Dingan County is contained in aircraft tail shelf 3 rearward end, and the shower nozzle direction of mold releasing agent spraying device 10 is just to mould Releasing agent is uniformly sprayed on mould 4 by 4;Stripper apparatus 11 is installed on driving chain 15 Between, inside head drive sprocket 5 and be fixedly mounted on fuselage cradle 2;Chiller 9 is solid Dingan County is contained on fuselage cradle 2, and the shower nozzle direction of chiller 9 is just equal by coolant to mould 4 Even is sprayed on mould 4.
Refer to chiller 9 as shown in Figure 2, it is preferred that shown chiller 9 wraps Include coolant hose 91, shower nozzle 92 and axial flow blower 93;The outlet of coolant hose 91 and shower nozzle 92 fixed installations, the outlet of shower nozzle 92 and the outlet of axial flow blower 93 are equidirectional parallel fixing Install.What coolant was the most frequently used cools down water exactly, and the effect of chiller is to cool down water smoke Change and be sprayed on mould, reduce mold temperature, make alloy pig and mould be rapidly separated, shorten cold But cycle and mold use life-span and use cycle can be extended.
Refer to mold releasing agent spraying device 10 as shown in Figure 3, it is preferred that the shown demoulding Agent spray equipment 10 includes nozzle 101, regulation short tube 102, clamp nut 103, pipe joint 104, nozzle holder 105, main support 106 and pipeline 107;Suit regulation in the middle part of nozzle 101 Short tube 102, one end of nozzle 101 tail end and pipe joint 104 is equipped with, pipe joint 104 another One end and pipeline 107 are equipped with, and nozzle holder 105 is right-angle structure, nozzle holder 105 two ends Being shaped with hole, nozzle 101 is fixedly mounted on the hole at nozzle holder 105 two ends by clamp nut 103 In, two nozzles 101 are at a right angle to be mounted opposite, and nozzle holder 105 is arranged on main support 106 Top.Nozzle is for being arranged in pairs, and every pair of nozzle is divided into release agent nozzle and gas nozzle, the demoulding Agent is flowed out and is coordinated gas injection to be atomized completely by releasing agent, uniformly sprays on mould, According to the width of die face, optional multipair nozzle is mounted side by side use at equal intervals.
Preferably, stripper apparatus uses the vibration demoulding, by the vibration of certain frequency, taps mould Tool, coordinates effect and the cooling effect of cooling water of releasing agent, makes alloy pig all from mould Depart from.
Embodiment:
After start, electric machine rotation, drive to decelerator, decelerator drives head by shaft coupling Transmission main shaft, head transmission main shaft drives head drive sprocket, and head drive sprocket passes through transmission Chain-driving tail drive sprocket, forms the drive mechanism of Guan Bi, fixing peace on driving chain The mould of dress operates the most therewith, and mould is first through the mold releasing agent spraying device at aircraft tail shelf rear portion, at mould Tool one layer of releasing agent of surface spraying, then goes to below casting gate, and the molten steel in ladle is through watering The buffering of casting nozzle, in the uniform mould flowing into the most spray coated releasing agent, the most slowly to machine Headstock direction is run, and period passes through axle through twice chiller, the cooling water in chiller The gas effect of flow fan blowout, is sprayed on the alloy pig in mould and mould uniformly, it is achieved Rapidly mould and alloy pig are cooled down under the double effects of cooling water and blow gas, when running extremely During head drive sprocket, complete cooling, through head drive sprocket rotate and under, major part close Ingot is under the effect of releasing agent and mould separating, and residue minority fails to depart from once, then continue Operating, after the stripper apparatus vibration beating inside head drive sprocket, all de-from mould From, the casting operation of complete set completes, and empty mould remains in operation to mold releasing agent spraying device, Continue next one circulation, it is achieved work continuously, uninterruptedly produce.
Efficiency is that conventional outmoded technique cannot be mentioned in the same breath completely, and safety coefficient carries the most significantly Height, reduces artificial simultaneously, reduces employment cost, moreover it is possible to improve working environment.
The present invention have passed through test of many times and improvement, utilizes simple and effective frame for movement, Complete the most nerve-wracking subpackage work in metal smelt, be worth of widely use.

Claims (3)

1. continuous casting machine, it is characterised in that: include headstock, fuselage cradle, aircraft tail shelf, mould, Head drive sprocket, head transmission main shaft, tail drive sprocket, tail power transmission shaft, motor, Decelerator, driving chain, chiller, mold releasing agent spraying device, stripper apparatus and casting gate; Headstock, fuselage cradle and aircraft tail shelf are rectangular bar of steel shelf structure, headstock, fuselage cradle and tail Frame is fixedly connected sequentially together;Bearing block is installed in the both sides of headstock, head transmission main shaft and The bearing block of headstock both sides is equipped with, and head drive sprocket is installed at the two ends of head transmission main shaft; Bearing block is installed in the both sides of aircraft tail shelf, and the bearing block of tail power transmission shaft and aircraft tail shelf both sides is equipped with, Tail drive sprocket is installed at the two ends of tail power transmission shaft;Head drive sprocket and tail drive sprocket Installation site corresponding;Motor and decelerator are arranged on headstock with the side at headstock, Motor and decelerator are in transmission connection, and the clutch end of decelerator and one end of shaft coupling connect, The other end of shaft coupling and one end of head transmission main shaft connect;Driving chain is arranged on head and passes Between the dynamic head drive sprocket of main shaft both sides and the tail drive sprocket of tail power transmission shaft both sides, become Parallel Symmetric is around head drive sprocket and tail drive sprocket Synchronous Transmission;Motor passes through decelerator Driving head transmission main shaft to rotate, head transmission main shaft rotational band motivation head drive sprocket rotates, Head drive sprocket can drive tail drive sprocket by driving chain;The two ends of mould are respectively With driving chain becomes vertical being arranged between two driving chains;Casting gate is arranged on aircraft tail shelf Above top mold, the running channel alignment mould of casting gate can make molten steel flow into mould uniformly; Mold releasing agent spraying device is parallel is fixedly mounted on aircraft tail shelf rearward end, the spray of mold releasing agent spraying device Releasing agent is just uniformly sprayed on mould by head direction by mould;Stripper apparatus is installed on transmission Between chain, inside head drive sprocket and be fixedly mounted on fuselage cradle;Chiller is fixed Being arranged on fuselage cradle, coolant is just uniformly sprayed by the shower nozzle direction of chiller by mould On mould.
2. continuous casting machine as claimed in claim 1, it is characterised in that: described chiller includes Coolant hose, shower nozzle and axial flow blower;The outlet of coolant hose and shower nozzle fixed installation, shower nozzle Outlet and the equidirectional parallel fixed installation of outlet of axial flow blower.
3. continuous casting machine as claimed in claim 1, it is characterised in that: described releasing agent spraying dress Put and include nozzle, regulation short tube, clamp nut, pipe joint, nozzle holder, main support and pipe Road;Suit regulation short tube in the middle part of nozzle, one end of nozzle tail end and pipe joint is equipped with, pipe joint The other end and pipeline be equipped with, nozzle holder is right-angle structure, and nozzle holder two ends are shaped with hole, Nozzle is fixedly mounted in the hole at nozzle holder two ends by clamp nut, two nozzle phases at a right angle To installation, nozzle holder is arranged on above main support.
CN201610319814.0A 2016-05-12 2016-05-12 Continuous casting machine Pending CN105855527A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201610319814.0A CN105855527A (en) 2016-05-12 2016-05-12 Continuous casting machine

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Application Number Priority Date Filing Date Title
CN201610319814.0A CN105855527A (en) 2016-05-12 2016-05-12 Continuous casting machine

Publications (1)

Publication Number Publication Date
CN105855527A true CN105855527A (en) 2016-08-17

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Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106623826A (en) * 2016-11-15 2017-05-10 宁夏铸源机械制造有限公司 Self-vibration type continuous casting system
CN109909461A (en) * 2019-04-10 2019-06-21 东北大学 A kind of easily broken manganese block running gate system device and method

Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1394716A (en) * 1971-09-22 1975-05-21 Union Carbide Corp Casting apparatus
US3976120A (en) * 1972-08-25 1976-08-24 Demag Aktiengesellschaft Casting arrangement for forming plate-shaped metal parts
JPH03254335A (en) * 1990-03-01 1991-11-13 Sumitomo Metal Mining Co Ltd Continuous casting apparatus
JPH04305337A (en) * 1991-04-03 1992-10-28 Keiyo Burankingu Kogyo Kk Method and device for continuous casting annular steel products
JPH10263749A (en) * 1997-03-27 1998-10-06 Kawasaki Steel Corp Production of molded pig iron and apparatus therefor
CN203900414U (en) * 2014-06-10 2014-10-29 上海中捷有色金属有限公司 Automatic continuous casting block making machine for composite ferro-silicon-aluminum deoxidizing agents
CN203900456U (en) * 2014-06-10 2014-10-29 上海中捷有色金属有限公司 Tabletop aluminum plate deoxidizing agent automated continuous pouring and continuous casting granulator
CN204182893U (en) * 2014-09-17 2015-03-04 交城义望铁合金有限责任公司 Casting machine demoulding bobbing machine
CN205732939U (en) * 2016-05-12 2016-11-30 宁夏铸源机械修配有限公司 Continuous casting machine

Patent Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1394716A (en) * 1971-09-22 1975-05-21 Union Carbide Corp Casting apparatus
US3976120A (en) * 1972-08-25 1976-08-24 Demag Aktiengesellschaft Casting arrangement for forming plate-shaped metal parts
JPH03254335A (en) * 1990-03-01 1991-11-13 Sumitomo Metal Mining Co Ltd Continuous casting apparatus
JPH04305337A (en) * 1991-04-03 1992-10-28 Keiyo Burankingu Kogyo Kk Method and device for continuous casting annular steel products
JPH10263749A (en) * 1997-03-27 1998-10-06 Kawasaki Steel Corp Production of molded pig iron and apparatus therefor
CN203900414U (en) * 2014-06-10 2014-10-29 上海中捷有色金属有限公司 Automatic continuous casting block making machine for composite ferro-silicon-aluminum deoxidizing agents
CN203900456U (en) * 2014-06-10 2014-10-29 上海中捷有色金属有限公司 Tabletop aluminum plate deoxidizing agent automated continuous pouring and continuous casting granulator
CN204182893U (en) * 2014-09-17 2015-03-04 交城义望铁合金有限责任公司 Casting machine demoulding bobbing machine
CN205732939U (en) * 2016-05-12 2016-11-30 宁夏铸源机械修配有限公司 Continuous casting machine

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106623826A (en) * 2016-11-15 2017-05-10 宁夏铸源机械制造有限公司 Self-vibration type continuous casting system
CN106623826B (en) * 2016-11-15 2018-09-18 宁夏铸源机械制造有限公司 Auto-oscillation type direct casting system
CN109909461A (en) * 2019-04-10 2019-06-21 东北大学 A kind of easily broken manganese block running gate system device and method

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Application publication date: 20160817

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