CN106863898A - A kind of fly press material jacking mechanism - Google Patents

A kind of fly press material jacking mechanism Download PDF

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Publication number
CN106863898A
CN106863898A CN201710252000.4A CN201710252000A CN106863898A CN 106863898 A CN106863898 A CN 106863898A CN 201710252000 A CN201710252000 A CN 201710252000A CN 106863898 A CN106863898 A CN 106863898A
Authority
CN
China
Prior art keywords
fuselage
leading screw
jacking
fly press
sliding block
Prior art date
Application number
CN201710252000.4A
Other languages
Chinese (zh)
Inventor
孙生强
Original Assignee
苏州蓝王机床工具科技有限公司
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 苏州蓝王机床工具科技有限公司 filed Critical 苏州蓝王机床工具科技有限公司
Priority to CN201710252000.4A priority Critical patent/CN106863898A/en
Publication of CN106863898A publication Critical patent/CN106863898A/en

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Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B30PRESSES
    • B30BPRESSES IN GENERAL
    • B30B1/00Presses, using a press ram, characterised by the features of the drive therefor, pressure being transmitted directly, or through simple thrust or tension members only, to the press ram or platen
    • B30B1/18Presses, using a press ram, characterised by the features of the drive therefor, pressure being transmitted directly, or through simple thrust or tension members only, to the press ram or platen by screw means
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B30PRESSES
    • B30BPRESSES IN GENERAL
    • B30B15/00Details of, or accessories for, presses; Auxiliary measures in connection with pressing
    • B30B15/28Arrangements for preventing distortion of, or damage to, presses or parts thereof
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B30PRESSES
    • B30BPRESSES IN GENERAL
    • B30B15/00Details of, or accessories for, presses; Auxiliary measures in connection with pressing
    • B30B15/32Discharging presses

Abstract

A kind of fly press material jacking mechanism,Including fuselage table base and guide rail,Sliding block is set on guide rail,Leading screw insertion fuselage side,And through the feed screw nut in the middle of two sliding blocks,It is the opposite screw thread of the hand of spiral in the middle of leading screw,Leading screw is arranged on fuselage by bearing,A fairlead is fixedly installed in the centre bore of fuselage workbench,Push rod is provided with described fairlead,The lower end of push rod is actively hinged with two one end of toggle link simultaneously together with,Together with two other ends of push rod are actively hinged with one of sliding block respectively,Electricity is installed with the side of fuselage,Motor drives leading screw rotating by corresponding transmission mechanism,Realize the purpose of liftout,The present invention has the advantages that simple structure,The process of liftout does not rely on the backhaul action and strength of fly press sliding block,It is easy to do corresponding control according to specific technique and operating mode situation,And it is not susceptible to mistake.

Description

A kind of fly press material jacking mechanism

Technical field

The present invention relates to fly press, and in particular to fly press material jacking mechanism, belong to fly press technology neck Domain.

Background technology

At present, the material jacking mechanism of existing fly press, usually the sliding block backhaul strength of utilization fly press, general Workpiece or waste material from mold ejection, although this material jacking mechanism have the advantages that it is certain, due to described liftout machine Structure needs to keep stricter rhythm with sliding block backhaul, some unexpected situations easily cause liftout unsuccessfully set cause mould or Forcing press is damaged, additionally, fly press is under backhaul situation, universal weight machine is weaker, for some large-scale, special-shaped workpiece or Waste material can not be ejected timely sometimes, and this situation not only has influence on the efficiency of production, be solution while being also susceptible to security incident Certainly above mentioned problem, in existing technology, also there is the solution of the material jacking mechanism mode for setting independent under the workbench of fly press Certainly method, but, this kind of material jacking mechanism is typically mainly made up of hydraulic cylinder, because hydraulic cylinder needs corresponding hydraulic system, is made The investment in space and equipment that forming apparatus take all than larger, meanwhile, the place of fly press work typically has environment Temperature is higher, and the more severe situation of environment, hydraulic system is also easily damaged.

The content of the invention

It is an object of the invention to:For the drawbacks described above existing for existing fly press material jacking mechanism, the present invention is carried For a kind of new fly press material jacking mechanism.

A kind of fly press material jacking mechanism of the present invention, it includes fuselage(1), it is characterized in that:It also includes leading To set(2), push rod(3), toggle link(4), sliding block(5), left bearing(6), left axle pressure cap(7), feed screw nut(8), base(9)、 Guide rail(10), right bearing(11), right axle pressure cap(12), negative pulley wheel(13), belt(14), motor support frame(15), it is main Dynamic belt pulley(16), motor(17), leading screw(18), in described fuselage(1)Workbench lower space bottom is installed with Base(9), described base(9)On be provided with guide rail(10), in described guide rail(10)On be provided with two identical sliding blocks (5), described two sliding blocks(5)Left and right is relative to fuselage(1)Symmetrical, the described sliding block in table core hole(5)Upper setting There is feed screw nut(8), further:Feed screw nut(8)Can also be directly in sliding block(5)On make, i.e.,:Sliding block(5)With leading screw Nut(8)The structure type being integrated, leading screw(18)Insertion fuselage(1)The end side surface of left and right two, respectively with screw thread coordinate side Formula passes through two sliding blocks(5)Middle feed screw nut(8), further:Described leading screw (18) is spiral side at middle two ends To opposite screw thread, two sliding blocks(5)In leading screw(18)On remain left and right relative to fuselage(1)Table core hole pair Claim, leading screw(18)Left end pass through left bearing(6)With left axle pressure cap(7)Installed in fuselage(1)On, leading screw(18)Right-hand member lead to Cross right bearing(11)With right axle pressure cap(12)Installed in fuselage(1)On, in fuselage(1)It is fixedly installed in the centre bore of workbench One fairlead(2), push rod is provided with described fairlead(3), in a free state, push rod(3)With in fairlead (2)The free degree for inside sliding up and down, described push rod(3)Lower end and two toggle links(4)One end simultaneously be actively hinged Together, two push rods(4)Other end respectively with one of sliding block(5)Actively it is hinged together, in fuselage (1)Side be installed with motor support frame(15), in motor support frame(15)On be installed with motor(17), it is described Motor(17)Drive pulley is installed with axle(16), drive pulley(16)By belt(14)With installed in leading screw (18)Negative pulley wheel on one end(13)It is connected.

Beneficial effect:Operation principle of the invention is that motor drives the different direction of rotation of leading screw, and leading screw will drive two Sliding block mutually leaves or approaches, so as to drive two toggle links support or folding and unfolding downwards upwards, by operation principle of the invention and Structure principle chart can be seen that the present invention has the advantages that simple structure, meanwhile, the process of liftout does not rely on fly press The backhaul action and strength of sliding block, are easy to do corresponding control according to specific technique and operating mode situation, and be not susceptible to mistake By mistake.

Brief description of the drawings

Fig. 1 is structure principle chart of the invention.

Shown in figure:1 it is fuselage, 2 be fairlead, 3 be push rod, 4 be toggle link, 5 be sliding block, 6 be left bearing, 7 is left axle Pressure cap, 8 be feed screw nut, 9 be base, 10 be guide rail, 11 be right bearing, 12 be right axle pressure cap, 13 be negative pulley wheel, 14 it is belt, 15 be motor support frame, 16 be drive pulley, 17 be motor, 18 is leading screw.

Specific embodiment

With reference to Fig. 1, specific embodiment of the invention is:

A kind of fly press material jacking mechanism, it includes fuselage(1), it is characterized in that:It also includes fairlead(2), push rod(3)、 Toggle link(4), sliding block(5), left bearing(6), left axle pressure cap(7), feed screw nut(8), base(9), guide rail(10), right bearing (11), right axle pressure cap(12), negative pulley wheel(13), belt(14), motor support frame(15), drive pulley(16), electricity Motivation(17), leading screw(18), in described fuselage(1)Workbench lower space bottom is installed with base(9), described bottom Seat(9)On be provided with guide rail(10), in described guide rail(10)On be provided with two identical sliding blocks(5), described two cunnings Block(5)Left and right is relative to fuselage(1)Symmetrical, the described sliding block in table core hole(5)On be provided with feed screw nut(8), enter One step:Feed screw nut(8)Can also be directly in sliding block(5)On make, i.e.,:Sliding block(5)With feed screw nut(8)The knot being integrated Configuration formula, leading screw(18)Insertion fuselage(1)The end side surface of left and right two, respectively by screw thread coordinate in the way of pass through two sliding blocks(5) Middle feed screw nut(8), further:Described leading screw (18) is the opposite screw thread of the hand of spiral, two at middle two ends Sliding block(5)In leading screw(18)On remain left and right relative to fuselage(1)Table core hole it is symmetrical, leading screw(18)Left end By left bearing(6)With left axle pressure cap(7)Installed in fuselage(1)On, leading screw(18)Right-hand member pass through right bearing(11)With the right side Bearing gland(12)Installed in fuselage(1)On, in fuselage(1)A fairlead is fixedly installed in the centre bore of workbench(2), Push rod is provided with described fairlead(3), in a free state, push rod(3)With in fairlead(2)Inside slide up and down from By spending, described push rod(3)Lower end and two toggle links(4)One end simultaneously be actively hinged together, two push rods(4) Other end respectively with one of sliding block(5)Actively it is hinged together, in fuselage(1)Side be installed with Motor support frame(15), in motor support frame(15)On be installed with motor(17), described motor(17)It is fixed on axle Drive pulley is installed(16), drive pulley(16)By belt(14)With installed in leading screw(18)Passive skin on one end Belt wheel(13)It is connected.

Claims (7)

1. a kind of fly press material jacking mechanism, it includes fuselage(1), it is characterized in that:It also includes fairlead(2), push rod (3), toggle link(4), sliding block(5), left bearing(6), left axle pressure cap(7), feed screw nut(8), base(9), guide rail(10), right axle Hold(11), right axle pressure cap(12), negative pulley wheel(13), belt(14), motor support frame(15), drive pulley(16)、 Motor(17), leading screw(18).
2. according to claim 1, a kind of described fly press material jacking mechanism, it is characterised in that:In described fuselage(1)Work Make platform lower space bottom and be installed with base(9), base(9)On be provided with guide rail(10), in described guide rail(10)On It is provided with two identical sliding blocks(5), two sliding blocks(5)Left and right is relative to fuselage(1)Table core hole it is symmetrical, sliding block (5)On be provided with feed screw nut(8).
3. according to claim 1 or 2, a kind of described fly press material jacking mechanism, its spy is:Sliding block(5)With leading screw spiral shell It is female(8)The structure type being integrated.
4. according to claim 1, a kind of described fly press material jacking mechanism, it is characterised in that:Leading screw(18)Insertion fuselage (1)The end side surface of left and right two, respectively by screw thread coordinate in the way of pass through two sliding blocks(5)Middle feed screw nut(8), leading screw (18) it is the opposite screw thread of the hand of spiral, two sliding blocks at middle two ends(5)In leading screw(18)On remain left and right relative to Fuselage(1)Table core hole it is symmetrical.
5. according to claim 1, a kind of described fly press material jacking mechanism, it is characterised in that:Leading screw(18)Left end lead to Cross left bearing(6)With left axle pressure cap(7)Installed in fuselage(1)On, leading screw(18)Right-hand member pass through right bearing(11)With right axle Pressure cap(12)Installed in fuselage(1)On.
6. according to claim 1, a kind of described fly press material jacking mechanism, it is characterised in that:In fuselage(1)Workbench A fairlead is fixedly installed in centre bore(2), push rod is provided with described fairlead(3), push rod(3)Lower end and two Individual toggle link(4)One end simultaneously be actively hinged together, two push rods(4)Other end respectively with it is one of sliding Block(5)Actively it is hinged together.
7. according to claim 1, a kind of described fly press material jacking mechanism, it is characterised in that:In fuselage(1)Side consolidate Dingan County is equipped with motor support frame(15), in motor support frame(15)On be installed with motor(17), described motor(17) Drive pulley is installed with axle(16), drive pulley(16)By belt(14)With installed in leading screw(18)On one end Negative pulley wheel(13)It is connected.
CN201710252000.4A 2017-04-18 2017-04-18 A kind of fly press material jacking mechanism CN106863898A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201710252000.4A CN106863898A (en) 2017-04-18 2017-04-18 A kind of fly press material jacking mechanism

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201710252000.4A CN106863898A (en) 2017-04-18 2017-04-18 A kind of fly press material jacking mechanism

Publications (1)

Publication Number Publication Date
CN106863898A true CN106863898A (en) 2017-06-20

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Family Applications (1)

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CN201710252000.4A CN106863898A (en) 2017-04-18 2017-04-18 A kind of fly press material jacking mechanism

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CN (1) CN106863898A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107127260A (en) * 2017-07-13 2017-09-05 邹小辉 A kind of hardware stamping panel piece stretch process die assembly
CN107824692A (en) * 2017-12-07 2018-03-23 安徽吉思特智能装备有限公司 A kind of diel of harvester pick-up machine pawl
CN108787861A (en) * 2018-06-12 2018-11-13 盐城市顺天铸造有限公司 A kind of cast-aluminum end cover heat emission hole hole punched device

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2006255790A (en) * 2006-05-17 2006-09-28 Janome Sewing Mach Co Ltd Portable motor-operated press
CN201711489U (en) * 2010-06-30 2011-01-19 青岛聚鑫锻压机械有限公司 Hydraulic ejector
CN202418452U (en) * 2012-01-17 2012-09-05 中国矿业大学 Synchronous belt tension mechanism of press machine
CN103742019A (en) * 2014-01-02 2014-04-23 十堰华恒机电科技有限公司 Method and device for lifting door/window glass of car
CN104897391A (en) * 2015-06-19 2015-09-09 中国航空工业集团公司西安飞机设计研究所 Mechanism test platform
CN205472511U (en) * 2016-01-28 2016-08-17 大唐呼图壁能源开发有限公司水力发电厂 Stable elevating platform that overhauls
CN106314506A (en) * 2016-08-23 2017-01-11 郭强 Hospital flower pot handling device

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2006255790A (en) * 2006-05-17 2006-09-28 Janome Sewing Mach Co Ltd Portable motor-operated press
CN201711489U (en) * 2010-06-30 2011-01-19 青岛聚鑫锻压机械有限公司 Hydraulic ejector
CN202418452U (en) * 2012-01-17 2012-09-05 中国矿业大学 Synchronous belt tension mechanism of press machine
CN103742019A (en) * 2014-01-02 2014-04-23 十堰华恒机电科技有限公司 Method and device for lifting door/window glass of car
CN104897391A (en) * 2015-06-19 2015-09-09 中国航空工业集团公司西安飞机设计研究所 Mechanism test platform
CN205472511U (en) * 2016-01-28 2016-08-17 大唐呼图壁能源开发有限公司水力发电厂 Stable elevating platform that overhauls
CN106314506A (en) * 2016-08-23 2017-01-11 郭强 Hospital flower pot handling device

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107127260A (en) * 2017-07-13 2017-09-05 邹小辉 A kind of hardware stamping panel piece stretch process die assembly
CN107824692A (en) * 2017-12-07 2018-03-23 安徽吉思特智能装备有限公司 A kind of diel of harvester pick-up machine pawl
CN108787861A (en) * 2018-06-12 2018-11-13 盐城市顺天铸造有限公司 A kind of cast-aluminum end cover heat emission hole hole punched device

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Application publication date: 20170620