CN210791985U - Integrated composite extruder - Google Patents
Integrated composite extruder Download PDFInfo
- Publication number
- CN210791985U CN210791985U CN201921780738.9U CN201921780738U CN210791985U CN 210791985 U CN210791985 U CN 210791985U CN 201921780738 U CN201921780738 U CN 201921780738U CN 210791985 U CN210791985 U CN 210791985U
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- speed reducer
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- 239000002131 composite material Substances 0.000 title claims description 13
- 239000003638 chemical reducing agent Substances 0.000 claims abstract description 26
- 239000000463 material Substances 0.000 claims abstract description 23
- 150000001875 compounds Chemical class 0.000 claims abstract description 16
- 230000005540 biological transmission Effects 0.000 claims abstract description 14
- 238000013329 compounding Methods 0.000 claims abstract description 5
- 238000007599 discharging Methods 0.000 claims abstract description 4
- 238000001125 extrusion Methods 0.000 claims description 18
- 230000007246 mechanism Effects 0.000 claims description 5
- 230000000694 effects Effects 0.000 abstract description 6
- 239000002994 raw material Substances 0.000 description 8
- 238000000034 method Methods 0.000 description 4
- 230000009471 action Effects 0.000 description 3
- 230000008569 process Effects 0.000 description 2
- 230000004075 alteration Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
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- Extrusion Moulding Of Plastics Or The Like (AREA)
Abstract
The utility model discloses an integrated compound extruder, which comprises a frame, wherein a host motor is installed at the lower end in the frame through screws, a host material cylinder shaft, a host speed reducer and a compound machine head are installed at the upper end of the frame through screws, the host motor is in transmission connection with the host speed reducer through a belt, the host material cylinder shaft is in transmission connection with the host speed reducer through a connecting shaft, and the feeding end of the compound machine head is connected with the discharging end of the host material cylinder shaft; and one side of the main machine charging barrel shaft is provided with an auxiliary machine charging barrel shaft, an auxiliary machine speed reducer and an auxiliary machine motor through a support. This compound extruder of integral type extrudes through main engine feed cylinder axle and auxiliary engine feed cylinder axle to decorate the effect of realizing double-colored and different materials in compounding the aircraft nose, thereby make the colour and the material of the product of extruding no longer single.
Description
Technical Field
The utility model relates to an extruder technical field, concrete formula composite extrusion machine as an organic whole.
Background
The original extruder can only finally extrude a product with one color or one raw material, the color is single and dull, excessive color mixing is avoided, and the product is too single.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide a compound extruder of integral type extrudes the product through host computer feed cylinder axle and vice feed cylinder axle to decorate the effect that realizes two-colour in the compound aircraft nose of integral type, therefore can effectively solve the prior art problem, make the product colour of extruding no longer single.
In order to achieve the above object, the utility model provides a following technical scheme: the integrated compound extruder comprises a frame, wherein a main machine motor is mounted at the lower end in the frame through screws, a main machine cylinder shaft, a main machine speed reducer and a compound machine head are mounted at the upper end of the frame through screws, the main machine motor is in transmission connection with the main machine speed reducer through a belt, the main machine cylinder shaft is in transmission connection with the main machine speed reducer through a connecting shaft, and the feeding end of the compound machine head is connected with the discharging end of the main machine cylinder shaft; one side of the main machine charging barrel shaft is also provided with an auxiliary machine charging barrel shaft, an auxiliary machine speed reducer and an auxiliary machine motor through a support, the auxiliary machine charging barrel shaft is in transmission connection with the auxiliary machine speed reducer through a connecting shaft, and the auxiliary machine speed reducer is in transmission connection with the auxiliary machine motor through a screw; the feeding end of the main machine charging barrel shaft is provided with a main machine hopper through a screw, and the feeding end of the auxiliary machine charging barrel shaft is provided with an auxiliary machine hopper through a screw.
Preferably, the auxiliary machine cylinder shaft is connected with a pipe hole in the composite machine head through a conveying pipe.
Preferably, the main engine motor and the auxiliary engine motor are both connected with a 380V power supply through lines.
Preferably, the main machine material cylinder shaft and the auxiliary machine material cylinder shaft are both screw extrusion mechanisms.
Compared with the prior art, the beneficial effects of the utility model are as follows:
this compound extruder through main engine feed cylinder axle and the vice quick-witted feed cylinder axle that sets up two the same screw extrusion mechanism for the extrusion raw materials of main engine feed cylinder axle and the extrusion raw materials of vice quick-witted feed cylinder axle decorate main engine feed cylinder axle extrusion material at compound aircraft nose front end through vice quick-witted feed cylinder axle extrusion material, realize double-colored effect, therefore can effectively solve prior art problem, make the product colour of extruding no longer single.
Drawings
Fig. 1 is an overall structure diagram of the present invention.
In the figure: 1. a frame; 2. a host motor; 3. a main machine barrel shaft; 4. a main machine speed reducer; 5. compounding machine heads; 6. a support; 7. a secondary machine charging barrel shaft; 8. an auxiliary machine speed reducer; 9. an auxiliary machine motor; 10. a host hopper; 11. auxiliary machinery hopper.
Detailed Description
The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.
Referring to fig. 1, the integrated composite extruder comprises a frame 1, wherein a main machine motor 2 is mounted at the lower end in the frame 1 through screws, and a main machine material cylinder shaft 3, a main machine speed reducer 4 and a composite machine head 5 are mounted at the upper end of the frame 1 through screws, wherein the main machine motor 2 is in transmission connection with the main machine speed reducer 4 through a belt, the main machine material cylinder shaft 3 is in transmission connection with the main machine speed reducer 4 through a connecting shaft, and the feeding end of the composite machine head 5 is connected with the discharging end of the main machine material cylinder shaft 3; when the host motor 2 is connected with a 380V power supply through a circuit, the host motor 2 starts the host material cylinder shaft 3 to drive the host material cylinder shaft to run, and the host speed reducer 4 controls the condition that the speed of the host motor 2 is too high after starting; an auxiliary machine charging barrel shaft 7, an auxiliary machine speed reducer 8 and an auxiliary machine motor 9 are further mounted on one side of the main machine charging barrel shaft 3 through a support 6, wherein the auxiliary machine charging barrel shaft 7 is in transmission connection with the auxiliary machine speed reducer 8 through a connecting shaft, the auxiliary machine charging barrel shaft 7 is connected with a pipe hole in the composite machine head 5 through a material conveying pipe, and the auxiliary machine speed reducer 8 is in transmission connection with the auxiliary machine motor 9 through a screw; when the auxiliary engine motor 9 is connected with a 380V power supply through a circuit, the auxiliary engine motor 9 is started to drive the auxiliary engine charging barrel shaft 7 to run, and the auxiliary engine speed reducer 8 controls the condition that the speed of the auxiliary engine motor 9 is too high after the auxiliary engine motor 9 is started; the feeding end of the main machine charging barrel shaft 3 is also provided with a main machine hopper 10 through a screw, and the feeding end of the auxiliary machine charging barrel shaft 7 is also provided with an auxiliary machine hopper 11 through a screw; because the main machine charging barrel shaft 3 and the auxiliary machine charging barrel shaft 7 are both screw extrusion mechanisms, after raw materials are respectively input into the main machine charging barrel shaft 3 and the auxiliary machine charging barrel shaft 7 through the main machine hopper 10 and the auxiliary machine hopper 11, the extrusion raw materials of the main machine charging barrel shaft 3 and the auxiliary machine charging barrel shaft 7 are dotted with the extrusion materials of the main machine charging barrel shaft 3 at the front end of the composite machine head 5 through the extrusion materials of the auxiliary machine charging barrel shaft 7, so that a double-color effect is realized, and the extrusion is carried out from the composite machine head 5.
This compound extruder through the host computer feed cylinder axle 3 and the vice machine feed cylinder axle 7 that set up two the same screw extrusion mechanism for the extrusion raw materials of host computer feed cylinder axle 3 and the extrusion raw materials of vice machine feed cylinder axle 7 decorate host computer feed cylinder axle 3 extrusions through vice machine feed cylinder axle 7 extrusions at 5 front ends of compound aircraft nose, realize double-colored effect, therefore can effectively solve prior art problem, make the product colour of extruding no longer single.
In summary, the following steps: this compound extruder extrudes the raw materials through main engine feed cylinder axle 3 and auxiliary engine feed cylinder axle 7 to decorate in compound aircraft nose 5 and realize double-colored effect, therefore can effectively solve prior art problem, make the product colour of extruding no longer single.
It is noted that, in this document, relational terms such as host and slave, and the like are used solely to distinguish one entity or action from another entity or action without necessarily requiring or implying any actual such relationship or order between such entities or actions. Also, the terms "comprises," "comprising," or any other variation thereof, are intended to cover a non-exclusive inclusion, such that a process, method, article, or apparatus that comprises a list of elements does not include only those elements but may include other elements not expressly listed or inherent to such process, method, article, or apparatus.
Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.
Claims (4)
1. Compound extruder of integral type, including frame (1), its characterized in that: the lower end in the frame (1) is provided with a main machine motor (2) through a screw, the upper end of the frame (1) is provided with a main machine material cylinder shaft (3), a main machine speed reducer (4) and a composite machine head (5) through screws, the main machine motor (2) is in transmission connection with the main machine speed reducer (4) through a belt, the main machine material cylinder shaft (3) is in transmission connection with the main machine speed reducer (4) through a connecting shaft, and the feeding end of the composite machine head (5) is connected with the discharging end of the main machine material cylinder shaft (3); one side of the main machine charging barrel shaft (3) is also provided with an auxiliary machine charging barrel shaft (7), an auxiliary machine speed reducer (8) and an auxiliary machine motor (9) through a support (6), the auxiliary machine charging barrel shaft (7) is in transmission connection with the auxiliary machine speed reducer (8) through a connecting shaft, and the auxiliary machine speed reducer (8) is in transmission connection with the auxiliary machine motor (9) through a screw; the feeding end of the main machine charging barrel shaft (3) is provided with a main machine hopper (10) through a screw, and the feeding end of the auxiliary machine charging barrel shaft (7) is provided with an auxiliary machine hopper (11) through a screw.
2. The integrated compounding extruder of claim 1, wherein: and the auxiliary machine cylinder shaft (7) is connected with a pipe hole on the composite machine head (5) through a material conveying pipe.
3. The integrated compounding extruder of claim 1, wherein: the main engine motor (2) and the auxiliary engine motor (9) are connected with a 380V power supply through lines.
4. The integrated compounding extruder of claim 1, wherein: the main machine material cylinder shaft (3) and the auxiliary machine material cylinder shaft (7) are both screw extrusion mechanisms.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201921780738.9U CN210791985U (en) | 2019-10-22 | 2019-10-22 | Integrated composite extruder |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201921780738.9U CN210791985U (en) | 2019-10-22 | 2019-10-22 | Integrated composite extruder |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN210791985U true CN210791985U (en) | 2020-06-19 |
Family
ID=71246800
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201921780738.9U Active CN210791985U (en) | 2019-10-22 | 2019-10-22 | Integrated composite extruder |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN210791985U (en) |
-
2019
- 2019-10-22 CN CN201921780738.9U patent/CN210791985U/en active Active
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20240823 Address after: No. 32 Xingyuantun Village, Liyuantun Town, Weixian County, Xingtai City, Hebei Province, China 054700 Patentee after: Jiang Junyan Country or region after: China Address before: 054700 xingyuantun village, Liyuantun Town, Wei County, Xingtai City, Hebei Province Patentee before: Hebei Shuangda rubber and Plastic Machinery Co.,Ltd. Country or region before: China |