CN210211271U - Extruder with conveniently replaced die - Google Patents
Extruder with conveniently replaced die Download PDFInfo
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- CN210211271U CN210211271U CN201920904008.9U CN201920904008U CN210211271U CN 210211271 U CN210211271 U CN 210211271U CN 201920904008 U CN201920904008 U CN 201920904008U CN 210211271 U CN210211271 U CN 210211271U
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- Extrusion Moulding Of Plastics Or The Like (AREA)
Abstract
The utility model relates to a conveniently change extruder of mould relates to the technical field of extrusion equipment, has solved when the mould needs to be changed, needs the cooperation of many people, holds up the aircraft nose alone at least, dismantles the bolt alone to make the aircraft nose difficult directly drop because of tearing the bolt down, troublesome poeration when changing the mould, the problem that wastes time and energy, it includes: organism, aircraft nose, set up in the pole setting of the one side that the organism is close to the aircraft nose, swing joint in the pole setting keep away from one side of organism with the supporting component of support aircraft nose and set up in the organism and be close to one side of aircraft nose in order to lock the aircraft nose in the locking component on the organism. The utility model discloses have and just can accomplish alone the dismouting to the aircraft nose, easy operation has improved the effect of the efficiency when the mould is changed to the extruder.
Description
Technical Field
The utility model belongs to the technical field of extrusion equipment's technique and specifically relates to a conveniently change extruder of mould is related to.
Background
The extruder is a device for continuously mixing and extruding rubber and plastic, the head of the extruder is a main part of the extruder, the head converts the material which moves spirally in the extruder into linear motion, and a certain molding pressure is established by the head to extrude and compact the material to prepare a compact molded product.
The existing extruder comprises an extruder body and an extruder head, wherein an extrusion die is arranged on one side of the extruder body close to the extruder head, and the extruder head is made of steel, so that the extruder head is heavy mostly, and the extruder head is fixed on the extruder body through a plurality of bolts.
The above prior art solutions have the following drawbacks: when the mould needs to be changed, a plurality of persons are needed to be matched, the machine head is supported at least by one person, the bolt is detached by one person, so that the machine head is not easy to directly drop due to the detachment of the bolt, the operation is troublesome during the change of the mould, time and labor are wasted, and an improved space is provided.
SUMMERY OF THE UTILITY MODEL
The utility model aims at providing a conveniently change extruder of mould just can accomplish alone the dismouting to the aircraft nose, and easy operation has improved the efficiency when the mould is changed to the extruder.
The above utility model discloses an above-mentioned utility model purpose can realize through following technical scheme:
the utility model provides an extruder of convenient change mould, includes organism and aircraft nose, still including set up in the pole setting of one side that the organism is close to the aircraft nose, swing joint in the pole setting keep away from one side of organism with the supporting component of support aircraft nose with the locking component of setting up in one side that the organism is close to the aircraft nose in order to lock the aircraft nose on the organism.
Through adopting above-mentioned technical scheme, need not to hold up the aircraft nose, and can directly dismantle the aircraft nose, just can accomplish the dismouting to the aircraft nose alone, and need not a plurality of people and cooperate, easy operation has improved the efficiency when the mould is changed to the extruder.
The utility model discloses further set up to: the support assembly includes:
the first connecting plate is hinged to one side of the vertical rod, which is far away from the machine body;
the second connecting plate is hinged to one end, far away from the vertical rod, of the first connecting plate;
the support column is inserted into one end, far away from the first connecting plate, of the second connecting plate and is used for supporting the machine head.
Through adopting above-mentioned technical scheme, make the aircraft nose support through the support column to through first connecting plate and second connecting plate swing joint in the pole setting, during the dismouting aircraft nose, need not to hold up the aircraft nose, can directly dismantle the aircraft nose, easy operation has improved the dismouting efficiency of aircraft nose, has improved the efficiency that the mould was changed to the extruder.
The utility model discloses further set up to: the locking component is arranged on the upright rod to lock the support column;
the deadlocking assembly includes:
the base plate is fixed on the support column, and a locking hole is formed in the base plate;
the locking plate is hinged to the upright post and meshed with the base plate to lock the base plate, and a locking block inserted into the locking hole is integrally arranged on one side of the locking plate, which is far away from the upright post.
Through adopting above-mentioned technical scheme, when the aircraft nose was installed on the organism, the dead piece of lock dead plate was pegged graft in the dead hole of lock of base plate to lock the support column, make support column and aircraft nose be difficult for taking place to rock, improved the stability of aircraft nose and support column.
The utility model discloses further set up to: the base plate is close to one side of support column and is seted up the caulking groove that supplies the support column to inlay to establish, one side that the base plate is close to the support column is fixed with the piece of hugging closely on being fixed in the support column with the base plate.
Through adopting above-mentioned technical scheme, the base plate can be dismantled through holding tightly the piece and connect on the support column, and when the base plate takes place to damage or length dimension is not fit for the time, the convenience is changed the base plate, has improved the change efficiency of base plate.
The utility model discloses further set up to: the deadlocking assembly further comprises:
the fixing plate is fixed on one side of the vertical rod;
the regulating plate is integrally arranged on one side, far away from the machine body, of the fixing plate and hinged to the dead locking plate so as to regulate the position of the dead locking plate according to the size of the substrate.
Through adopting above-mentioned technical scheme, the position that makes the dead board of lock can be adjusted through the angle of buckling of fixed plate and regulating plate to suit with the size of base plate, the cooperation base plate locks the support column, reasonable in design, the practicality is strong.
The utility model discloses further set up to: a first outer convex ring is integrally arranged on one side of the machine head, which is close to the machine body, and a second outer convex ring is integrally arranged on one side of the machine body, which is close to the machine head;
the locking assembly includes:
one end of the first connecting rod is hinged on the machine body;
one end of the second connecting rod is hinged on the machine body;
one end of the first hoop is hinged with the other end of the first connecting rod;
one end of the second hoop is hinged with the other end of the second connecting rod and is matched with the first hoop to tightly hold the first convex ring and the second convex ring, and a through hole is formed in one end, far away from the second connecting rod, of the second hoop;
one end of the locking column is hinged to one side of the first hoop, which is far away from the first connecting rod, and penetrates through the through hole;
and the locking nut is connected with one side of the locking column, which is far away from the first hoop, in a threaded manner and compresses the second hoop.
Through adopting above-mentioned technical scheme, the through-hole is worn out to the locking post, and lock nut and locking post threaded connection compress tightly the second staple bolt to order about first staple bolt and second staple bolt and lock the aircraft nose, and need not to lock through the bolt, make the aircraft nose dismouting more convenient, improved the efficiency that the mould was changed to the extruder.
The utility model discloses further set up to: and the second hoop is also provided with a sliding groove which is mutually communicated with the through hole and is used for the locking column to slide in.
Through adopting above-mentioned technical scheme, make when removing the locking of aircraft nose, the locking post need not through wearing to establish the hole installation or dismantlement of sliding, and can directly slide through the groove of sliding and install to wearing to establish the hole or shift out the wearing to establish the hole, conveniently locks or removes the locking to the aircraft nose, has improved the locking efficiency of locking subassembly.
To sum up, the utility model discloses a beneficial technological effect does:
1. the machine head can be disassembled and assembled by one person, the operation is simple, and the efficiency of the extruder in replacing the die is improved;
2. the machine head is supported by the support column and is movably connected to the upright rod through the first connecting plate and the second connecting plate, so that the machine head can be directly disassembled, the operation is simple, and the die replacing efficiency of the extruder is improved;
3. the aircraft nose is fixed in the organism through first staple bolt and second staple bolt on, and need not to lock through the bolt, makes the aircraft nose dismouting more convenient, has improved the efficiency that the mould was changed to the extruder.
Drawings
Fig. 1 is a schematic structural diagram of the extruder with a die convenient to replace according to the present invention.
Fig. 2 is a partial structural schematic view after the extruder head is disassembled.
Fig. 3 is a schematic diagram of a partial explosion of the substrate, the supporting pillars and the hugging block.
In the figure, 1, a machine body; 11. erecting a rod; 12. a second male ring; 2. a machine head; 21. a first outer convex ring; 3. a support assembly; 31. a first connecting plate; 32. a second connecting plate; 33. a support pillar; 4. a locking assembly; 41. a first link; 42. a second link; 43. a first hoop; 44. a second hoop; 441. perforating holes; 442. sliding into the groove; 45. a locking post; 46. a locking nut; 5. locking the assembly; 51. a substrate; 511. locking the hole; 52. locking the plate; 521. locking the block; 512. caulking grooves; 53. a hugging block; 54. a fixing plate; 55. an adjusting plate.
Detailed Description
The present invention will be described in further detail with reference to the accompanying fig. 1-3.
Referring to fig. 1, for the utility model discloses a conveniently change extruder of mould, including organism 1, aircraft nose 2, pole setting 11, supporting component 3 and locking Assembly 4.
Referring to fig. 1 and 2, a machine head 2 is arranged at the end of an extrusion material channel of a machine body 1, a vertical rod 11 is integrally arranged at one side of the machine body 1 close to the machine head 2, and the vertical rod 11 is used for supporting the extrusion material channel; the supporting component 3 is movably connected to one side of the upright rod 11, which is far away from the machine body 1, the supporting component 3 is used for supporting the machine head 2, and the supporting component 3 comprises a first connecting plate 31, a second connecting plate 32 and a supporting column 33; one end of the first connecting plate 31 is hinged to the upright column, the second connecting plate 32 is hinged to one end, far away from the upright rod 11, of the first connecting plate 31, the lower end of the supporting column 33 is inserted into one end, far away from the first connecting plate 31, of the second connecting plate 32, and the upper end of the supporting column 33 is fixed with the machine head 2, so that the machine head 2 is movably connected to the upright rod 11.
The outer peripheral wall that aircraft nose 2 is close to organism 1 is gone up an organic whole and is equipped with first outer bulge loop 21, and one side that organism 1 is close to aircraft nose 2 is an organic whole and is equipped with second outer bulge loop 12, and first outer bulge loop 21 corresponds with second outer bulge loop 12.
The locking assembly 4 is arranged on the machine body 1 and is positioned on one side of the machine body 1 close to the machine head 2, the locking assembly 4 is used for locking the machine head 2 on the machine body 1, and the locking assembly 4 comprises a first connecting rod 41, a second connecting rod 42, a first hoop 43, a second hoop 44, a locking column 45 and a locking nut 46; the upper end of the first link rod 41 is hinged to the machine body 1, the lower end of the first link rod 41 is hinged to the upper end of the first hoop 43, the locking column 45 is hinged to the lower end of the first hoop 43, the upper end of the second link rod 42 is hinged to the machine body 1, the lower end of the second link rod 42 is hinged to the upper end of the second hoop 44, the first hoop 43 and the second hoop 44 are matched to tightly hold the first outer convex ring 21 and the second outer convex ring 12, the lower end of the second hoop 44 is provided with a through hole 441, the through hole 441 is used for the locking column 45 to penetrate, the locking column 45 penetrates through the through hole 441, the locking nut 46 is in threaded connection with the locking column 45, and the locking nut 46 compresses one side of the second hoop 44, which is far away from the first hoop 43, so as to drive the first hoop 43 and the second hoop 44 to tightly hold the first outer convex ring 21 and the second outer convex ring 12; the lower extreme of second staple bolt 44 has still seted up the groove of slipping 442, slips into groove 442 and wears to establish hole 441 intercommunication and cut apart the lower lateral wall of second staple bolt 44, slips into groove 442 and supplies locking post 45 to slide out and wears to establish hole 441 or slide and install to wearing to establish in the hole 441, conveniently carries out the dismouting to locking post 45.
Still including locking subassembly 5, locking subassembly 5 is located on the lateral wall of pole setting 11, and locking subassembly 5 is used for locking support column 33.
Referring to fig. 2 and 3, in one embodiment, the deadlocking assembly 5 includes a base plate 51 and a deadlocking plate 52; the substrate 51 can be welded on the support and can also be detachably connected with the support column 33, one side of the substrate 51 close to the support column 33 is provided with an embedding groove 512, the embedding groove 512 is used for embedding the support column 33, the side wall of the substrate 51 close to the support column 33 is divided into two parts by the embedding groove 512, the substrate 51 is also fixed with a holding block 53 through a screw, and the holding block 53 is matched with the substrate 51 to clamp the substrate 51 on the support column 33; one side of the base plate 51, which is far away from the supporting column 33, is provided with a locking hole 511, the locking plate 52 is hinged to one side wall of the vertical rod 11 through a screw, one end, which is far away from the vertical rod 11, of the locking plate 52 is integrally provided with a locking block 521, and the locking block 521 is inserted into the locking hole 511 so as to engage the locking plate 52 with the base plate 51 to lock the supporting column 33.
In one embodiment, the deadlocking assembly 5 further comprises a fixed plate 54 and an adjustment plate 55; the fixing plate 54 is fixed on one side wall of the vertical rod 11, the adjusting plate 55 is integrally arranged on one side of the fixing plate 54 close to the base plate 51, the locking plate 52 is hinged on the adjusting plate 55, and the hinge position of the locking plate 52 can be adjusted through the bending angles of the adjusting plate 55 and the fixing plate 54 so as to match the base plate 51 to lock the supporting column 33.
The implementation principle of the embodiment is as follows:
the first connecting plate 31 is hinged to the upright rod 11, the second connecting plate 32 is hinged to one end, far away from the upright rod 11, of the first connecting plate 31, the upper end of the supporting column 33 is fixed with the machine head 2, and the lower end of the supporting column 33 is inserted into one end, far away from the first connecting plate 31, of the second connecting plate 32, so that the machine head 2 is supported through the supporting column 33 and is movably connected with the upright rod 11, the machine head 2 does not need to be lifted when the machine head 2 is detached, and the machine head 2 can be directly detached; the machine head 2 is fixed on the machine body 1 through the first hoop 43 and the second hoop 44 without using a plurality of screws, so that the machine head 2 is more convenient to assemble and disassemble; when aircraft nose 2 was fixed in on the organism 1, the dead subassembly 5 of lock is dead to the lock of support column 33, and aircraft nose 2 is more stable when making extruder work.
The embodiment of this specific implementation mode is the preferred embodiment of the present invention, not limit according to this the utility model discloses a protection scope, so: all equivalent changes made according to the structure, shape and principle of the utility model are covered within the protection scope of the utility model.
Claims (7)
1. The utility model provides a conveniently change extruder of mould, includes organism (1) and aircraft nose (2), its characterized in that: the device is characterized by further comprising a vertical rod (11) arranged on one side, close to the machine head (2), of the machine body (1), a supporting component (3) movably connected to one side, far away from the machine body (1), of the vertical rod (11) and used for supporting the machine head (2), and a locking component (4) arranged on one side, close to the machine head (2), of the machine body (1) and used for locking the machine head (2) on the machine body (1).
2. The extruder convenient for die replacement according to claim 1, wherein: the support assembly (3) comprises:
the first connecting plate (31) is hinged to one side of the upright rod (11) far away from the machine body (1);
the second connecting plate (32) is hinged to one end, away from the vertical rod (11), of the first connecting plate (31);
and the supporting column (33) is inserted into one end, far away from the first connecting plate (31), of the second connecting plate (32) and is used for supporting the machine head (2).
3. The extruder convenient for die replacement according to claim 2, wherein: the device also comprises a locking component (5) which is arranged on the upright rod (11) and used for locking the support column (33);
the deadlocking assembly (5) comprises:
the base plate (51) is fixed on the supporting column (33), and a locking hole (511) is formed in the base plate (51);
the locking plate (52) is hinged to the upright column and meshed with the base plate (51) to lock the base plate (51), and a locking block (521) inserted into the locking hole (511) is integrally arranged on one side, far away from the upright column, of the locking plate (52).
4. The extruder convenient for die replacement according to claim 3, wherein: the clamping device is characterized in that one side, close to the supporting column (33), of the substrate (51) is provided with a caulking groove (512) for the supporting column (33) to be embedded, and one side, close to the supporting column (33), of the substrate (51) is fixed with a clamping block (53) for fixing the substrate (51) on the supporting column (33).
5. The extruder convenient for die replacement according to claim 3, wherein: the deadlocking assembly (5) further comprises:
a fixing plate (54) fixed to one side of the vertical rod (11);
and the adjusting plate (55) is integrally arranged on one side of the fixing plate (54) far away from the machine body (1) and is hinged with the locking plate (52) so as to adjust the position of the locking plate (52) according to the size of the base plate (51).
6. The extruder convenient for die replacement according to claim 1, wherein: a first outer convex ring (21) is integrally arranged on one side of the machine head (2) close to the machine body (1), and a second outer convex ring (12) is integrally arranged on one side of the machine body (1) close to the machine head (2);
the locking assembly (4) comprises:
one end of the first connecting rod (41) is hinged on the machine body (1);
one end of the second connecting rod (42) is hinged on the machine body (1);
one end of the first hoop (43) is hinged with the other end of the first connecting rod (41);
one end of the second hoop (44) is hinged with the other end of the second connecting rod (42) and is matched with the first hoop (43) to tightly hold the first convex ring (21) and the second convex ring (12), and a through hole (441) is formed in one end, far away from the second connecting rod (42), of the second hoop (44);
one end of the locking column (45) is hinged to one side, away from the first connecting rod (41), of the first hoop (43) and penetrates through the penetrating hole (441);
and the locking nut (46) is in threaded connection with one side of the locking column (45) far away from the first hoop (43) and compresses the second hoop (44).
7. The extruder convenient for die replacement according to claim 6, wherein: and the second hoop (44) is also provided with a sliding groove (442) which is mutually communicated with the through hole (441) and is used for the locking column (45) to slide in.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920904008.9U CN210211271U (en) | 2019-06-15 | 2019-06-15 | Extruder with conveniently replaced die |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920904008.9U CN210211271U (en) | 2019-06-15 | 2019-06-15 | Extruder with conveniently replaced die |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN210211271U true CN210211271U (en) | 2020-03-31 |
Family
ID=69932072
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201920904008.9U Active CN210211271U (en) | 2019-06-15 | 2019-06-15 | Extruder with conveniently replaced die |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN210211271U (en) |
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2019
- 2019-06-15 CN CN201920904008.9U patent/CN210211271U/en active Active
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