CN109130108A

CN109130108A - A kind of integrated injection mold

Info

Publication number: CN109130108A
Application number: CN201810420468.4A
Authority: CN
Inventors: 张焕根; 张波
Original assignee: Individual
Current assignee: Individual
Priority date: 2018-05-04
Filing date: 2018-05-04
Publication date: 2019-01-04

Abstract

The invention discloses a kind of integrated injection molds, including fuselage and the first cavity of the fuselage inner opening to the left is set, it can slide up and down down in first cavity and divide mould, divide mould bilateral symmetry under described and front and back is symmetrically arranged with first through hole up and down, be slidably installed the first sliding bar extended up and down in the first through hole, first sliding bar upper and lower ends end wall above and below first cavity is fixedly connected, divide under described and is equipped with the first sliding cavity in mould, it can slide up and down in first sliding cavity and be provided with the first sliding shoe；The configuration of the present invention is simple, equipment depanning difficult problem is solved by ejecting mechanism, the automatic modulus of equipment is realized using clamping device, it cooperates and does not influence between each process, the safety of equipment is improved while reducing human cost, equipment whole-course automation of the invention reduces operation error, injection efficiency and quality are not only increased, and improves device practical performance.

Description

A kind of integrated injection mold

Technical field

The present invention relates to modeling product manufacturing field, specifically a kind of integrated injection molds.

Background technique

It is seen everywhere plastic products in life, plastic products were manufacturing the effect ever more important of the mankind, plastic products There is some problems, such as common injection machine device cannot achieve automation there are depanning difficulty there are also part machine and take in journey Mould leads to inefficiency, and there is some potential safety problemss in the course of work, and depanning effect is also bad, this device effectively solves It has determined this problem.

Summary of the invention

Technical problem to be solved by the invention is to provide a kind of integrated injection molds, are able to solve above-mentioned present skill The problems in art.

The present invention is achieved through the following technical solutions: a kind of integrated injection mold of the invention, including fuselage And the first cavity of the fuselage inner opening to the left is set, and it can slide up and down down in first cavity and divide mould, institute State down and divide mould bilateral symmetry and front and back is symmetrically arranged with first through hole up and down, in the first through hole in be slidably matched peace Equipped with the first sliding bar extended up and down, the first sliding bar upper and lower ends end wall above and below first cavity is fixed Connection divides under described and is equipped with the first sliding cavity in mould, and can slide up and down in first sliding cavity, it is sliding to be provided with first Motion block, the second through-hole being symmetrically set in first sliding shoe are fixedly installed in second through-hole downward The second sliding bar stretched, through first sliding cavity, end wall protrudes into first cavity second sliding bar up and down, institute State and be fixedly installed with a point mould in the first cavity roof, it is described on divide bilateral symmetry in mould to be equipped with third through-hole up and down, It can slide up and down in the third through-hole and be provided with the second sliding shoe, the second sliding shoe extends downwardly bottom and is fixedly connected Divide mould under described, it is described on divide and be equipped with symmetrical second sliding cavity above mould, can horizontally slip in second sliding cavity Be provided with third sliding shoe, the first drive cavity is provided with below first cavity, the connection of first drive cavity bottom is set It is equipped with the second cavity of opening upwards, the axle sleeve extended up and down, the axle sleeve are rotatably provided in first drive cavity Interior to be equipped with upper and lower perforative thread cavity, the thread cavity screw-internal thread fit has the first threaded rod extended up and down, first spiral shell Upwardly extend at the top of rasp bar and protrude into first cavity through the first drive cavity upper end wall, first threaded rod bottom to Under extend into second cavity, the first threaded rod top end in first cavity be fixedly connected it is described under divide mould Lower end surface, the sleeve outer surface are fixedly installed with first gear, are rotatably provided on the left of the axle sleeve and to extend up and down Shaft, the shaft top end are rotationally connected in the first drive cavity upper end wall, the shaft bottom end and fixation The first motor being set in the first drive cavity lower end wall is connected by power, the shaft outer surface be fixedly installed with it is described The second gear of first gear engagement, the fuselage right side are equipped with the second drive cavity, and second drive cavity bottom is equipped with therewith Connection and the third sliding cavity of opening to the right, the second drive cavity left side are equipped with the 4th sliding cavity, and the 4th sliding cavity can What is horizontally slipped is provided with the 4th sliding shoe, and it is symmetrical that front and back is provided with and communicated between the 4th sliding cavity and first cavity Fourth hole, the mandril that left and right extends slidably is provided in the fourth hole, the mandril in first cavity is left Side end is fixedly connected with clamping device, and it is sliding that the mandril right end in the 4th sliding cavity is fixedly connected with the described 4th Motion block, is equipped with the perforative threaded hole in left and right in the 4th sliding shoe, the threaded hole screw-internal thread fit have that left and right extends the Two threaded rods, second threaded rod left and right ends are rotatably assorted respectively to be connected in the 4th sliding cavity left hand end wall, institute It states the second threaded rod and extends through the 4th sliding cavity right end wall to the right and protrude into second drive cavity, second threaded rod On be fixedly installed with the first bevel gear in second drive cavity, second drive cavity bottom is provided with and communicated with opening Third sliding cavity to the right, what can be horizontally slipped in the third sliding cavity is provided with the 5th sliding shoe, the 5th sliding shoe It is fixedly installed the second motor in right side, the second motor right side power is connected with to be matched with the first bevel gear Second bevel gear, third sliding cavity and first cavity are provided with and communicated with fifth hole, can control cunning in the fifth hole Dynamic is provided with the 6th sliding shoe for controlling and extending, and the 6th sliding shoe right end in the third sliding cavity is fixed to be connected The 5th sliding shoe left side is connect, stabilizing mechanism is provided in the fuselage, the stabilizing mechanism includes support column and adjusting Seat.

Preferably technical solution is symmetrically arranged with the first limit of opening inwards in the first sliding cavity left hand end wall Position slot, is slidably fitted with the first limited block being fixedly connected with first sliding shoe in first limiting slot, and described first The first top pressure spring to offset with first limited block is fixedly installed on end wall on the upside of limiting slot.

Preferably technical solution is provided with the second limiting slot that Open Side Down, institute in the second sliding cavity roof The second limited block for being slidably fitted in the second limiting slot and being fixedly connected with the third sliding shoe is stated, outside second limiting slot The second top pressure spring to offset with second limited block is fixedly installed on the wall of side.

Preferably technical solution, the third sliding cavity are symmetrically arranged with the third limit for being open inside in end wall up and down Position slot, is slidably fitted with the third limited block being fixedly connected with the 5th sliding shoe, the third in the third limiting slot The third top pressure spring to offset with second limited block is fixedly installed on end wall on the left of limiting slot.

Preferably technical solution divides under described and is equipped with the first top bevel on the right side of mould, sets on the left of the 6th sliding shoe There is the first pushing tow face matched with first top bevel.

Preferably technical solution, the second sliding shoe top are equipped with the second top bevel, are equipped in the third sliding shoe The the second pushing tow face matched with second top bevel.

Preferably technical solution, the first cavity top end wall is interior equipped with the charging conduit extended up and down, described to fall The feed inlet being provided on the left of hopper outside connection, the fuselage roof are fixedly installed hydraulic cylinder, the hydraulic cylinder push rod to Under extend into the charging conduit, the push rod bottom in the charging conduit is fixedly connected with push plate, it is described on divide mould and One cavity is provided with and communicated with the 6th through-hole.

Preferably technical solution, the clamping device include holding frame and the 5th sliding in clamped frame Chamber, holding frame left side articulated connection are provided with the first clamping limb symmetrical above and below, can control cunning in the 5th sliding cavity Dynamic is provided with the 6th sliding shoe, is equipped with the perforative threaded hole in left and right in the 6th sliding shoe, the threaded hole internal screw thread is matched The third threaded rod for having left and right to extend is closed, the third threaded rod left pivot movement is connected in the wall of the 5th sliding cavity left end, It is connect with the third motor power in the 5th sliding cavity right end wall on the right side of the third threaded rod with being fixedly installed, described the The second clamping limb symmetrical above and below is hingedly connected on six sliding shoes, second clamping limb extends and first clamping to the left Arm articulated connection.

Preferably technical solution, the upper end of support column face are respectively fixedly connected with the angle of the fuselage lower end surface four, It is provided with the band internal thread thread cavity that Open Side Down in the support column, is provided with the spiral shell being threadedly engaged in the thread cavity Line column, the threaded post, which extends downwardly, stretches out outside the thread cavity, and bottom end is fixedly connected with the adjustment seat.

The beneficial effects of the present invention are: equipment of the invention is in the initial state, the first motor, the second motor and Third motor is in stationary state, divide under described mould with it is described on divide mould to separate, the cylinder is in contraction state.

When equipment pressing mold of the invention, start first motor rotation, the first motor rotation drives described the The rotation of two gears, the second gear rotation drive the first gear rotation, and the first gear rotation drives the axle sleeve It rotating, the axle sleeve rotation drives first threaded rod to rise, and divide mould to rise under the first threaded rod rising promotion is described, Divide under described mould and it is described on when mould being divided to mold, the second top bevel being arranged at the top of the second sliding shoe pushes described Second pushing tow face is set in third sliding shoe, and the third sliding shoe is to two Slideslips, and the cylinder pushes the push plate at this time It moves down, the push plate moves down extruding and moves down from the raw material that the feed inlet is fallen into the charging conduit, and the raw material passes through described 6th through-hole enter it is described under divide mould and it is described on divide between mould and form.

When equipment backform of the invention, product cooled and solidified after molding starts first motor reversion, and described the One motor reversal drives the second gear reversion, and the second gear reversion drives the first gear to invert, and described first Gear reversion drives the axle sleeve reversion, and the axle sleeve, which inverts, drives the first threaded rod decline, under first threaded rod Drop drive it is described under divide mould to decline, due to dividing mould to decline under described, second pushing tow face is separated with second top bevel, institute It states third sliding shoe and moves towards cutting raw material and closing the 6th through-hole under second top pressure spring effect, by institute It states down and mould is divided to move down, second sliding bar is contacted with first cavity, and second sliding bar, which moves up, produces the molding Product ejection.

When equipment modulus of the invention, due to dividing mould to move down under described, first top bevel and first pushing tow Face cooperation, the 6th sliding shoe moves to right, and the 6th sliding shoe, which moves to right, pushes the 5th sliding shoe to move to right, and described at this time the One bevel gear engages with the second bevel gear, starts the second motor rotation at this time, and the second motor rotation drives institute Second bevel gear rotation is stated, the second bevel gear rotation drives the first bevel gear rotation, the first bevel gear Rotation drives the second threaded rod rotation, and the second threaded rod rotation drives the 4th sliding shoe to move to left, and the described 4th Sliding shoe, which moves to left, pushes the mandril to move to left, and the mandril, which moves to left, pushes the clamping device to move to left, and moves to left when described to described On the right side of shaped article, start the third motor rotation, the third motor rotation drives the 6th sliding shoe to move to left, described 6th sliding shoe, which moves to left, pushes shaped article described in first gripping arm, starts second motor reversal, and described the Two motor reversals drive the second bevel gear reversion, and the second bevel gear reversion drives the first bevel gear reversion, institute It states the first bevel gear reversion and drives the second threaded rod reversion, the second threaded rod reversion drives the 4th sliding Block moves to right, and the 4th sliding shoe, which moves to right, pushes the mandril to move to right, and the mandril, which moves to right, pushes the clamping device to move to right, when The shaped article removes, and starts the third motor reversal, and the third motor reversal drives the 6th sliding shoe It moves to right, the 6th sliding shoe, which moves to right, pushes first clamping limb to put down the shaped article.

The configuration of the present invention is simple is solved equipment depanning difficult problem by ejecting mechanism, is realized and set using clamping device Standby automatic modulus cooperates between each process and does not influence, improves equipment while reducing human cost Safety, equipment whole-course automation of the invention, reduces operation error, not only increases injection efficiency and quality, Er Qieti High device practical performance.

Detailed description of the invention

The present invention is described in detail by following specific embodiments and drawings for ease of explanation,.

Fig. 1 is a kind of integrated injection mold overall structure diagram of the invention；

Fig. 2 is the structural schematic diagram of A in Fig. 1.

Specific embodiment

As Figure 1-Figure 2, a kind of integrated injection mold of the invention, including fuselage 100 and setting are in the machine The first cavity 110 of 100 inner opening of body to the left can slide up and down down in first cavity 110 and divide mould 125, under described 125 bilateral symmetry of point mould and front and back are symmetrically arranged with first through hole up and down, in the first through hole in be slidably matched peace Equipped with the first sliding bar 124 extended up and down, 124 upper and lower ends of the first sliding bar are respectively on first cavity 110 Lower end wall is fixedly connected, and is divided under described and is equipped with the first sliding cavity 126 in mould 125, can be upper and lower in first sliding cavity 126 Sliding is provided with the first sliding shoe 130, the second through-hole being symmetrically set in first sliding shoe 130, and described the The second sliding bar 132 extended up and down is fixedly installed in two through-holes, second sliding bar 132 runs through first sliding cavity About 126 end walls protrude into first cavity 110, are fixedly installed with point mould 123, institute in 110 roof of the first cavity The third through-hole 113 being symmetrically equipped in point mould 123 up and down is stated, can slide up and down in the third through-hole 113 Be provided with the second sliding shoe 111, the second sliding shoe 111 extend downwardly bottom be fixedly connected it is described under divide mould 125, it is described on Divide and be equipped with symmetrical second sliding cavity 119 above mould 123, what can be horizontally slipped in second sliding cavity 119 is provided with Third sliding shoe 115, the first drive cavity 101 is provided with below first cavity 110, and 101 bottom of the first drive cavity connects Lead to the second cavity 109 for being provided with opening upwards, is rotatably provided with the axle sleeve extended up and down in first drive cavity 101 105, it is equipped with upper and lower perforative thread cavity 106 in the axle sleeve 105,106 screw-internal thread fit of thread cavity has to be extended up and down First threaded rod 108 upwardly extends at the top of first threaded rod 108 and protrudes into institute through 101 upper end wall of the first drive cavity The first cavity 110 is stated, 108 bottom of the first threaded rod extends down into second cavity 109, first cavity 110 Interior 108 top end of the first threaded rod be fixedly connected it is described under divide mould 125 lower end surface, 105 outer surface of axle sleeve is solid Dingan County is equipped with first gear 104, and 105 left side of axle sleeve is rotatably provided with the shaft 102 extended up and down, the shaft 102 top ends are rotationally connected in 101 upper end wall of the first drive cavity, 102 bottom end of shaft and fixed setting It is connected by power in the first motor 107 in 101 lower end wall of the first drive cavity, 102 outer surface of shaft is fixedly installed with The second gear 103 engaged with the first gear 104, is equipped with the second drive cavity 141 on the right side of the fuselage 100, and described second 141 bottom of drive cavity is equipped with the in communication and third sliding cavity 137 of opening to the right, is equipped on the left of second drive cavity 141 4th sliding cavity 139, what the 4th sliding cavity 139 can horizontally slip is provided with the 4th sliding shoe 142, the 4th sliding cavity It is provided with and communicated with the symmetrical fourth hole in front and back between 139 and first cavity 110, is slidably set in the fourth hole It is equipped with the mandril 149 that left and right extends, 149 left distal end of mandril in first cavity 110 is fixedly connected with clamping device, institute It states 149 right end of mandril in the 4th sliding cavity 139 and is fixedly connected with the 4th sliding shoe 142, the 4th sliding The perforative threaded hole in left and right, the second threaded rod 138 that the threaded hole screw-internal thread fit has left and right to extend, institute are equipped in block 142 It states 138 left and right ends of the second threaded rod and is rotatably assorted respectively and be connected in 139 left hand end wall of the 4th sliding cavity, described second Threaded rod 138 extends through to the right the 139 right end wall of the 4th sliding cavity and protrudes into second drive cavity 141, second spiral shell The first bevel gear 140 being fixedly installed on rasp bar 138 in second drive cavity 141,141 bottom of the second drive cavity Portion is provided with and communicated with the third sliding cavity 137 of opening to the right, and what can be horizontally slipped in the third sliding cavity 137 is provided with the 5th Sliding shoe 153 is fixedly installed the second motor 152,152 right side of the second motor in 153 right side of the 5th sliding shoe It is connected by power the second bevel gear 136 matched with the first bevel gear 140, third sliding cavity 137 and first sky Chamber 110 is provided with and communicated with fifth hole 157, the 6th for being provided with left and right and extending that can be horizontally slipped in the fifth hole 157 Sliding shoe 156,156 right end of the 6th sliding shoe in the third sliding cavity 137 are fixedly connected with the 5th sliding 153 left side of block is provided with stabilizing mechanism in the fuselage 100, and the stabilizing mechanism includes support column 171 and adjustment seat 172.

Valuably, the first limiting slot 127 of opening inwards is symmetrically arranged in 126 left hand end wall of the first sliding cavity, The first limited block 129 being fixedly connected with first sliding shoe 130 is slidably fitted in first limiting slot 127, it is described The first top pressure spring 128 to offset with first limited block 129 is fixedly installed on first limiting slot, 127 upside end wall.

Valuably, it is provided with the second limiting slot 122 that Open Side Down in 119 roof of the second sliding cavity, described second The second limited block 138 being fixedly connected with the third sliding shoe 115, second limit are slidably fitted in limiting slot 122 The second top pressure spring 121 to offset with second limited block 104 is fixedly installed in 122 outer end wall of slot.

Valuably, the inside third limiting slot 133 that is open is symmetrically arranged in about 137 end wall of third sliding cavity, The third limited block 135 being fixedly connected with the 5th sliding shoe 153 is slidably fitted in the third limiting slot 133, it is described The third top pressure spring 134 to offset with second limited block 104 is fixedly installed on 133 left side end wall of third limiting slot.

Valuably, divide under described and be equipped with the first top bevel 154 on the right side of mould 125, be equipped on the left of the 6th sliding shoe 156 with The first pushing tow face 155 that first top bevel 154 matches.

Valuably, the second top bevel is equipped at the top of the second sliding shoe 111, be equipped in the third sliding shoe 115 with it is described The second pushing tow face 114 that second top bevel matches.

Valuably, the charging conduit 118 extended up and down, the charging conduit 118 are equipped in 110 top end wall of the first cavity Left side is provided with the feed inlet 151 outside connection, is fixedly installed hydraulic cylinder 117, the hydraulic cylinder at the top of the fuselage 100 117 push rods extend down into the charging conduit 118, and the push rod bottom in the charging conduit 118 is fixedly connected with push plate 116, it is described on divide mould 123 and the first cavity 110 to be provided with and communicated with the 6th through-hole 112.

Valuably, the clamping device includes holding frame 151 and the 5th sliding cavity 143 in clamped frame 151, Articulated connection is provided with the first clamping limb 146 symmetrical above and below on the left of the holding frame 151, can in the 5th sliding cavity 143 What is horizontally slipped is provided with the 6th sliding shoe 144, is equipped with the perforative threaded hole in left and right, the spiral shell in the 6th sliding shoe 144 The third threaded rod 147 that pit screw-internal thread fit has left and right to extend, 147 left pivot movement of third threaded rod are connected to described the In five sliding cavities, 143 left end wall, 147 right side of third threaded rod and fixed setting and the 143 right end wall of the 5th sliding cavity Interior third motor 148 is connected by power, and the second clamping limb 145 symmetrical above and below is hingedly connected on the 6th sliding shoe 144, Second clamping limb 145 extends to the left to be articulated and connected with first clamping limb 146.

Valuably, 171 upper surface of support column is respectively fixedly connected with fuselage 100 lower end surface four angle, the branch It is provided with the band internal thread thread cavity 174 that Open Side Down in dagger 171, is provided with and is threadedly engaged in the thread cavity 174 Threaded post 173, the threaded post 173, which extends downwardly, stretches out outside the thread cavity 174, and bottom end is fixedly connected with the tune Seat 172 is saved, by screwing the adjustment seat 172, the stationarity when fuselage 100 support can be improved.

In the initial state, the first motor 107, the second motor 152 and third motor 148 are equal for equipment of the invention Remain static, divide under described mould 125 with it is described on divide mould 123 to separate, the cylinder 117 is in contraction state.

When equipment pressing mold of the invention, start the first motor 107 and rotate, the rotation of first motor 107 drives The second gear 103 rotates, and the rotation of second gear 103 drives the first gear 104 to rotate, the first gear 104 rotations drive the axle sleeve 105 to rotate, and the rotation of axle sleeve 105 drives first threaded rod 108 to rise, and described first Threaded rod 108 rise push it is described under divide mould 125 to rise, divide under described mould 125 and it is described on when mould 123 being divided to mold, it is described The second top bevel being arranged at the top of the second sliding shoe 111, which pushes in the third sliding shoe 115, is arranged the second pushing tow face 114, the third sliding shoe 115 is to two Slideslips, and the cylinder 117 pushes the push plate 116 to move down at this time, the push plate 116 move down extruding moves down from the raw material that the feed inlet 151 is fallen into the charging conduit 118, and the raw material passes through the described 6th Through-hole 112 enter it is described under divide mould 125 and it is described on divide between mould 123 and form.

When equipment backform of the invention, product cooled and solidified after molding starts the first motor 107 and inverts, institute Stating the reversion of first motor 107 drives the second gear 103 to invert, and the reversion of second gear 103 drives the first gear 104 reversions, the reversion of first gear 104 drive the axle sleeve 105 to invert, and the reversion of axle sleeve 105 drives first spiral shell Rasp bar 108 declines, first threaded rod 108 decline drive it is described under divide mould 125 to decline, due to dividing mould 125 to decline under described, Second pushing tow face 114 is separated with second top bevel, and the third sliding shoe 115 is in second top pressure spring 121 Cutting raw material and closing the 6th through-hole 112 are moved towards under effect, due to dividing mould 125 to move down under described, described second is sliding Lever 132 is contacted with first cavity 110, and second sliding bar 132, which moves up, ejects the shaped article.

When equipment modulus of the invention, due to dividing mould 125 to move down under described, first top bevel 154 and described the The cooperation of one pushing tow face 155, the 6th sliding shoe 156 move to right, and the 6th sliding shoe 156, which moves to right, pushes the 5th sliding shoe 153 move to right, and the first bevel gear 140 is engaged with the second bevel gear 136 at this time, start second motor 152 at this time Rotation, the rotation of the second motor 152 drive the second bevel gear 136 to rotate, and the rotation of second bevel gear 136 drives institute The rotation of first bevel gear 140 is stated, the first bevel gear 140 rotation drives second threaded rod 138 to rotate, and described the The rotation of two threaded rods 138 drives the 4th sliding shoe 142 to move to left, and the 4th sliding shoe 142, which moves to left, pushes the mandril 149 It moves to left, the mandril 149, which moves to left, pushes the clamping device to move to left, and moves to left when described on the right side of the shaped article, starts institute The rotation of third motor 148 is stated, the rotation of third motor 148 drives the 6th sliding shoe 144 to move to left, the 6th sliding shoe 144, which move to left promotion first clamping limb 146, clamps the shaped article, starts second motor 152 and inverts, and described second The reversion of motor 152 drives the second bevel gear 136 to invert, and the reversion of second bevel gear 136 drives the first bevel gear 140 reversions, the reversion of first bevel gear 140 drive second threaded rod 138 to invert, second threaded rod 138 Reversion drives the 4th sliding shoe 142 to move to right, and the 4th sliding shoe 142, which moves to right, pushes the mandril 149 to move to right, the top Bar 149, which moves to right, pushes the clamping device to move to right, and when shaped article removal, starts the third motor 148 and inverts, The third motor 148 reversion drives the 6th sliding shoe 144 to move to right, and the 6th sliding shoe 144, which moves to right, pushes described the One clamping limb 146 puts down the shaped article.

The above description is merely a specific embodiment, but scope of protection of the present invention is not limited thereto, any The change or replacement expected without creative work, should be covered by the protection scope of the present invention.Therefore, of the invention Protection scope should be determined by the scope of protection defined in the claims.

Claims

1. including fuselage and the first sky of the fuselage inner opening to the left is arranged in a kind of integrated injection mold of the invention Chamber can slide up and down down in first cavity and divide mould, and mould bilateral symmetry is divided under described and front and back is symmetrically arranged with up and down The first through hole of perforation, in the first through hole in be slidably installed the first sliding bar extended up and down, described first is sliding Lever upper and lower ends end wall above and below first cavity is fixedly connected, and is divided in mould under described and is equipped with the first sliding Chamber can slide up and down in first sliding cavity and be provided with the first sliding shoe, is symmetrical set in first sliding shoe The second through-hole having is fixedly installed with the second sliding bar extended up and down in second through-hole, and second sliding bar runs through End wall protrudes into first cavity first sliding cavity up and down, is fixedly installed with a point mould in the first cavity roof, Divide bilateral symmetry in mould to be equipped with third through-hole up and down on described, can slide up and down in the third through-hole and be provided with the Two sliding shoes, the second sliding shoe extend downwardly bottom be fixedly connected it is described under divide mould, it is described on divide and be equipped with left and right above mould Symmetrical second sliding cavity, what can be horizontally slipped in second sliding cavity is provided with third sliding shoe, under first cavity Side is provided with the first drive cavity, and first drive cavity bottom is provided with and communicated with the second cavity of opening upwards, and described first passes Move it is intracavitary be rotatably provided with the axle sleeve extended up and down, upper and lower perforative thread cavity, the thread cavity are equipped in the axle sleeve Screw-internal thread fit has the first threaded rod extended up and down, upwardly extends at the top of first threaded rod through first drive cavity Upper end wall protrudes into first cavity, and first threaded rod bottom extends down into second cavity, first cavity Interior the first threaded rod top end be fixedly connected it is described under divide mould lower end surface, the sleeve outer surface is fixedly installed with One gear, the axle sleeve left side are rotatably provided with the shaft extended up and down, and the shaft top end is rotationally connected with institute State in the first drive cavity upper end wall, the shaft bottom end be fixedly installed in the first drive cavity lower end wall first Motor power connection, the shaft outer surface are fixedly installed with the second gear engaged with the first gear, and the fuselage is right Side is equipped with the second drive cavity, and second drive cavity bottom is equipped in communication and opening third sliding cavity to the right, and described the The 4th sliding cavity is equipped on the left of two drive cavities, what the 4th sliding cavity can horizontally slip be provided with the 4th sliding shoe, described the It is provided with and communicated with the symmetrical fourth hole in front and back between four sliding cavities and first cavity, it is slidable in the fourth hole It is provided with the mandril that left and right extends, the mandril left distal end in first cavity is fixedly connected with clamping device, and the described 4th Mandril right end in sliding cavity is fixedly connected with the 4th sliding shoe, is equipped with left and right in the 4th sliding shoe and runs through Threaded hole, the second threaded rod that the threaded hole screw-internal thread fit has left and right to extend, second threaded rod left and right ends point It is not rotatably assorted and is connected in the 4th sliding cavity left hand end wall, it is sliding that second threaded rod extends through to the right the described 4th Dynamic chamber right end wall protrudes into second drive cavity, is fixedly installed in second drive cavity on second threaded rod First bevel gear, second drive cavity bottom are provided with and communicated with opening third sliding cavity to the right, in the third sliding cavity What can be horizontally slipped is provided with the 5th sliding shoe, is fixedly installed the second motor in the 5th sliding shoe right side, and described Two motor right side powers are connected with the second bevel gear matched with the first bevel gear, third sliding cavity and first sky Chamber is provided with and communicated with fifth hole, the 6th sliding shoe for being provided with left and right and extending that can be horizontally slipped in the fifth hole, institute It states the 6th sliding shoe right end in third sliding cavity and is fixedly connected with the 5th sliding shoe left side, in the fuselage It is provided with stabilizing mechanism, the stabilizing mechanism includes support column and adjustment seat.

2. a kind of integrated injection mold according to claim 1, it is characterised in that: the first sliding cavity left hand end wall In be symmetrically arranged with opening the first limiting slot inwards, be slidably fitted in first limiting slot solid with first sliding shoe Surely the first limited block connected is fixedly installed with the to offset with first limited block on the upside of first limiting slot on end wall One top pressure spring.

3. a kind of integrated injection mold according to claim 1, it is characterised in that: set in the second sliding cavity roof It is equipped with the second limiting slot that Open Side Down, is slidably fitted in second limiting slot and is fixedly connected with the third sliding shoe Second limited block is fixedly installed with the second press bullet to offset with second limited block in the second limiting slot outer end wall Spring.

4. a kind of integrated injection mold according to claim 1, it is characterised in that: end wall above and below the third sliding cavity In be symmetrically arranged with the inside third limiting slot of being open, be slidably fitted in the third limiting slot solid with the 5th sliding shoe Surely the third limited block connected is fixedly installed with the to offset with second limited block on the left of the third limiting slot on end wall Three top pressure springs.

5. a kind of integrated injection mold according to claim 1, it is characterised in that: divide under described and be equipped with first on the right side of mould Top bevel, the 6th sliding shoe left side are equipped with the first pushing tow face matched with first top bevel.

6. a kind of integrated injection mold according to claim 1, it is characterised in that: be equipped with second at the top of the second sliding shoe Top bevel, the third sliding shoe is interior to be equipped with the second pushing tow face matched with second top bevel.

7. a kind of integrated injection mold according to claim 1, it is characterised in that: in the first cavity top end wall Equipped with the charging conduit extended up and down, the feed inlet being provided with outside connection on the left of the charging conduit, the fuselage roof fixation is set It is equipped with hydraulic cylinder, the hydraulic cylinder push rod extends down into the charging conduit, and the push rod bottom in the charging conduit is solid Surely be connected with push plate, it is described on divide mould and the first cavity to be provided with and communicated with the 6th through-hole.

8. a kind of integrated injection mold according to claim 1, it is characterised in that: the clamping device includes holding frame And the 5th sliding cavity in clamped frame, holding frame left side articulated connection are provided with the first clamping symmetrical above and below Arm, what can be horizontally slipped in the 5th sliding cavity is provided with the 6th sliding shoe, is equipped with left and right in the 6th sliding shoe and runs through Threaded hole, the third threaded rod that the threaded hole screw-internal thread fit has left and right to extend, the third threaded rod left pivot movement connects It is connected in the wall of the 5th sliding cavity left end, on the right side of the third threaded rod and is fixedly installed and the 5th sliding cavity right end wall Interior third motor power connection, is hingedly connected with the second clamping limb symmetrical above and below on the 6th sliding shoe, and described second Clamping limb extends to the left to be articulated and connected with first clamping limb.

9. a kind of integrated injection mold according to claim 1, it is characterised in that:, the upper end of support column face difference It is fixedly connected with the angle of the fuselage lower end surface four, the band internal thread thread cavity that Open Side Down is provided in the support column, The threaded post being threadedly engaged is provided in the thread cavity, the threaded post, which extends downwardly, stretches out outside the thread cavity, and bottom End is fixedly connected with the adjustment seat.