CN2035702U - Angle square type hydraulic injection moulding machine - Google Patents
Angle square type hydraulic injection moulding machine Download PDFInfo
- Publication number
- CN2035702U CN2035702U CN 88214119 CN88214119U CN2035702U CN 2035702 U CN2035702 U CN 2035702U CN 88214119 CN88214119 CN 88214119 CN 88214119 U CN88214119 U CN 88214119U CN 2035702 U CN2035702 U CN 2035702U
- Authority
- CN
- China
- Prior art keywords
- connecting rod
- rod
- tailstock
- fuselage
- head
- 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.)
- Withdrawn
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- Moulds For Moulding Plastics Or The Like (AREA)
Abstract
Disclosed is an angle square type hydraulic injection moulding machine, comprising a body, a hand piece, a tailstock and a tiger head. An oil and an oil pump tank are positioned under the body, and an oil cylinders and a piston which are positioned on the body individually controls a swaging mechanism in vertical direction and a press mould mechanism lateral in lateral direction. A mode locker positioned on the press mould mechanism is strengthened. The angle square type hydraulic injection moulding machine is suitable for producing various shapes of complicated pressed articles and has the characteristics of simple structure, convenient operation, small noise and safety.
Description
The utility model is a kind of injection machine, belongs to device of plastic processing.
Existing injection machine has vertical, horizontal and the angle square formula.Can be divided into manual, electronic and hydraulic pressure again by the active force difference.Angle square formula injection machine is applicable to the plastic products of different shape complexity, and discharging is convenient, handling safety.Existing angle square formula injection machine is a hand plate type and two electronic.But the labour intensity of hand plate type is big, and production efficiency is low; And two electronic process gears engaged are come rotating screw bolt, have that noise is big, operation inconvenience, and precision is difficult for shortcomings such as assurance.
The purpose of this utility model is that a kind of little hydraulic pressure of noise of using of design is power, angle square formula hydraulic injection molding machine simple in structure, that adaptability is strong, easy to use, safe.
The solution of the utility model design is made up of institutes such as fuselage, head, tiger head, tailstocks.Its fuselage is fuel tank, oil pump, banked direction control valves down, and oil pump is by driven by motor.Head vertically is installed on the fuselage, and the rigging position of head and fuselage can be regulated according to varying in size of mould.Oil cylinder is installed in the upper end of head, and in-oil cylinder piston rod heads on compressing rod, and the center of compressing rod is facing to feed hopper, and feed hopper is fixed on the head, taps into barrel under the feed hopper.Two templates are arranged on the fuselage, the template I is attached on the fuselage, and the template II is installed in Hu Toushang, and the tiger head is the critical piece that is used for fixing mould, tiger head slides on the guide rail of fuselage, and the mechanism that the tiger head can be slided be oil cylinder on the tailstock and tailstock with tiger between transmission mechanism.So-called transmission mechanism is: the big connecting rod that connects the tiger head, big connecting rod links to each other with the connecting lever of recessed pin connecting rod, one of recessed pin connecting rod is installed on the tailstock, the other end of recessed pin connecting rod joins with small rod, small rod and connecting rod base join, the connecting rod base stopper rod of taking over a job connects piston oil-feed cylinder, and oil cylinder is installed on the tailstock.After piston rod promoted connecting rod base, connecting rod base promoted small rod, and small rod makes recessed pin connecting rod connecting lever abduction, promoted big connecting rod, and big connecting rod promotes brave head, tiger head locking mould.When the piston adverse effect, mould is separately annotated part and is come out from discharge bucket automatically.Tailstock should slide on the guide rail of fuselage, locate according to varying in size of mould, but guarantee the tight locked mode tool of tiger head and at all can not the back sliding when injection moulding again, this will solve the fixation problem after tailstock is adjusted the position, i.e. the fixture of tailstock.The fixture of so-called tailstock is the locked mode seat, one end of locked mode seat is fixed on the fuselage, and the other end of locked mode seat is installed on the tailstock by the locked mode bar, and one of the locked mode bar screws in tailstock, the locked mode seat is passed in the other end, and is by two nuts that the locked mode seat is fixing with the locked mode bar.
Angle square formula hydraulic injection molding machine of the present utility model, unlikely swing when making piston rod promote connecting rod base, at a upper and lower horizontal support and the guide rod longitudinally respectively installed of tailstock,, the groove of connecting rod base is slidingly matched along guide rod in each recessing of the upper and lower central authorities of connecting rod base.
Angle square formula hydraulic injection molding machine of the present utility model, in order to guarantee the moulding automatic demoulding, in the tiger head, the automatic demoulding plate is arranged, two ejector beams are arranged on the stripper plate, ejector beam is facing to two ejector beam holes on the template II, and demoulding push rod is installed on big connecting rod, when the tiger head retreated, demoulding push rod just in time headed on stripper plate.Demoulding push rod and ejector beam can be according to the adjustings of can both advancing and retreat of different situations such as mould.
Angle square formula hydraulic injection molding machine of the present utility model, its locked mode seat can be installed in respectively on the fuselage by two that separate, also can be by an integral body middle recessed being installed on the fuselage.
Angle square formula hydraulic injection molding machine of the present utility model, have wide adaptability, simple in structure, noise is little, easy to operate, safe in utilization, characteristics such as labour intensity is low.
Fig. 1, be structural representation of the present utility model;
Fig. 2, Fig. 3 are the utility model connecting rod base schematic diagram;
Fig. 4, Fig. 5 are the utility model small rod schematic diagram;
Fig. 6, Fig. 7 are recessed pin connecting rod schematic diagram of the present utility model;
Fig. 8, Fig. 9 are the utility model big connecting rod schematic diagram;
Figure 10, be stripper plate schematic diagram of the present utility model;
Figure 11, be the schematic diagram of whole locked mode seat of the present utility model;
Figure 12, be the utility model locked mode seat side schematic diagram;
Figure 13, be the utility model monomer locked mode seat schematic diagram.
Describe embodiment of the present utility model in detail below in conjunction with Fig. 1 to Figure 13.
1, oil cylinder; 2, head; 3, piston rod; 4, compressing rod; 5, feed hopper; 6, regulate screw mandrel; 7, feeding cylinder; 8, template I; 9, fuselage; 10, Pressure gauge; 11, action bars; 12, fuel tank; 13, discharging opening; 14, oil pipe; 15, locked mode seat; 16, screw; 17, screw; 18, locked mode bar; 19, mode transfer bar; 20, oil cylinder; 21, tailstock; 22, guide rod; 23, support; 24, brave head; 25, template II; 26, piston rod; 27, connecting rod base; 28, small rod; 29, recessed pin connecting rod; 30, big connecting rod; 31, groove; 32, connect the tailstock hole; 33, connect the big connecting rod hole; 34, connect the small rod hole; 35, demoulding push rod; 36, stripper plate; 37, ejector beam; 38, locked mode bar hole; 39, screw hole.
The utility model is by fuselage (9), fuel tank (12) and oil pump etc. are arranged under the fuselage, head (2) vertically is installed on fuselage, oil cylinder (1) is installed on the head, connect compressing rod (4) under the piston rod in the oil cylinder (3), compressing rod is facing to feed hopper (5), and feed hopper is fixed on the head (2), repeatedly kicks into barrel (7) under the feed hopper.Pasting template I (8) on the fuselage (9).Fuselage (9) is gone up horizontal mounted tailstock (21), oil cylinder (20) is arranged on the tailstock, piston rod in the oil cylinder (26) connects connecting rod base (27), connecting rod base (27) drives small rod (28), small rod connects (34) of recessed pin connecting rod (29), and the other end of recessed pin connecting rod (32) are installed on the tailstock (21), and the connecting lever of recessed pin connecting rod (33) connects big connecting rod (30), big connecting rod links to each other with tiger head (24), is pasting template II (25) on the tiger head.After mixing up the position of tailstock and fuselage according to the difference of mould by mode transfer bar (19), fix by locked mode seat (15), locked mode seat (15) is by screw (16,17) be installed on the fuselage (9), the upper end of locked mode seat (15) is installed on the tailstock (21) by locked mode bar (18), one of locked mode bar (18) screws in the tailstock (21), locked mode hole (38) is passed in the other end of locked mode bar (18), and fix with two nuts, on tailstock (21), a horizontal support (23) and guide rod (22) longitudinally respectively are installed down, on connecting rod base (27), each recessing (31) of following central authorities makes the groove (31) of connecting rod base (27) slide along guide rod (22).In tiger head (24), stripper plate (36) is arranged, ejector beam (37) is arranged on the stripper plate (36), and demoulding push rod (35) is installed in big connecting rod (30) side.Locked mode seat (15) can also can be recessed into (15A) in the centre by an integral body by two (15B) separating.
Claims (4)
1, angle square formula hydraulic injection molding machine, fuel tank (12) is arranged under the fuselage (9), oil pump, head (2) vertically is installed on the fuselage, oil cylinder (1) is installed on the head, is connect compressing rod (4) under the piston rod in the oil cylinder (3), compressing rod is facing to feed hopper (5), tap into barrel (7) under the feed hopper, template I (8) is arranged on the fuselage.Horizontal mounted tailstock (21) on the fuselage, tailstock links to each other with tiger head (24) by transmission mechanism, on the tiger head template II (25) is arranged, it is characterized in that upward installation oil cylinder (20) of tailstock (21), piston rod in the oil cylinder (26) connects connecting rod base (27), connecting rod base drives small rod (28), small rod connects (34) of recessed pin connecting rod (29), the other end of recessed pin connecting rod (32) is installed on the tailstock (21), the connecting lever of recessed pin connecting rod (33) connects big connecting rod (30), and big connecting rod links to each other with tiger head (24), and mode transfer bar (19) is arranged between tailstock and fuselage, locked mode seat (15) is installed on fuselage, and the upper end of locked mode seat is installed on the tailstock (21) by locked mode bar (18).
2, injection machine as claimed in claim 1 is characterized in that support (23) and guide rod (22) on the tailstock (21), goes up fluted (31) at connecting rod base (27), and guide rod (22) is slidingly matched with groove (31).
3, injection machine as claimed in claim 1 or 2, it is characterized in that in the tiger head (24) stripper plate (36) being arranged, ejector beam (37) is arranged on the stripper plate, on template II (25), the ejector beam hole is arranged, demoulding push rod (35) is arranged on the big connecting rod (30), and ejector beam (37) and demoulding push rod (35) advance and retreat can be regulated.
4, injection machine as claimed in claim 3 is characterized in that locked mode seat (15) can be two (15B) separately, also can be one whole and middle recessed (15A).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 88214119 CN2035702U (en) | 1988-09-17 | 1988-09-17 | Angle square type hydraulic injection moulding machine |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 88214119 CN2035702U (en) | 1988-09-17 | 1988-09-17 | Angle square type hydraulic injection moulding machine |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN2035702U true CN2035702U (en) | 1989-04-12 |
Family
ID=4847111
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 88214119 Withdrawn CN2035702U (en) | 1988-09-17 | 1988-09-17 | Angle square type hydraulic injection moulding machine |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN2035702U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN1034157C (en) * | 1994-01-15 | 1997-03-05 | 山东工程学院 | Double-side oblique-wedge high-efficiency injection forming machine |
-
1988
- 1988-09-17 CN CN 88214119 patent/CN2035702U/en not_active Withdrawn
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN1034157C (en) * | 1994-01-15 | 1997-03-05 | 山东工程学院 | Double-side oblique-wedge high-efficiency injection forming machine |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| C19 | Lapse of patent right due to non-payment of the annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |