CN218575527U - Machine head structure of vertical machining center - Google Patents
Machine head structure of vertical machining center Download PDFInfo
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- CN218575527U CN218575527U CN202223232604.8U CN202223232604U CN218575527U CN 218575527 U CN218575527 U CN 218575527U CN 202223232604 U CN202223232604 U CN 202223232604U CN 218575527 U CN218575527 U CN 218575527U
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- slide plate
- plate seat
- main shaft
- machining center
- headstock
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Abstract
The utility model provides a vertical machining center's aircraft nose structure, including the slide plate seat that is located the workstation top and through horizontal slide rail set spare axial displacement, the top of slide plate seat is connected with the stand through first lead screw guide rail set spare, the front end of stand is connected with the headstock through second lead screw guide rail set spare, one side corresponds the headstock and has the tool magazine dish through tool magazine leg joint, the upper end of headstock is connected with driving motor, the main shaft is worn to be equipped with at the middle part, the upper end and the motor shaft of driving motor of this main shaft are connected, the tool bit has been dismantled to the bottom of main shaft, the utility model discloses have very strong support rigidity, set up vertical crisscross strengthening rib through slide plate seat and stand, make it to guarantee that the aircraft nose has very high resonant frequency, avoid producing resonance with the aircraft nose when the high-speed rotation of main shaft, cause the bad effect that lathe processing produced, can make the contact surface increase of slide plate seat and stand simultaneously, effectively give off the heat.
Description
Technical Field
The utility model relates to a machining center part field, more specifically say, especially relate to a vertical machining center's aircraft nose structure.
Background
The machining center is one of numerical control machines with highest yield and most extensive application in the world at present, and is key equipment for machining machinery equipment such as a casting machine and the like. The comprehensive processing capacity is strong, a lot of processing contents can be finished after the workpiece is clamped once, the processing precision is high, the batch of workpieces with medium processing difficulty can be processed, the efficiency is 5-10 times of that of common equipment, and great economic and social benefits can be brought to enterprises and society.
The aircraft nose is the main casting part in the machining center major structure, and wherein motor and the main shaft on the machining center are connected through the lift slip table on aircraft nose and the machining center, and the main shaft can produce certain heat at the high-speed in-process of moving on the aircraft nose, can influence the precision and the stability of aircraft nose like this.
SUMMERY OF THE UTILITY MODEL
The utility model discloses improve prior art to above-mentioned shortcoming, provide a vertical machining center's aircraft nose structure, technical scheme as follows:
the utility model provides a vertical machining center's aircraft nose structure, is including the slide bar seat that is located the workstation top and through transverse sliding rail subassembly axial displacement, the top of slide bar seat is connected with the stand through first lead screw guide rail set spare, the front end of stand is connected with the headstock through second lead screw guide rail set spare, and one side corresponds the headstock and has the tool magazine dish through tool magazine leg joint, the upper end of headstock is connected with driving motor, and the main shaft is worn to be equipped with in the middle part, the upper end of this main shaft with driving motor's motor shaft is connected, the tool bit has been installed to the bottom of main shaft can be dismantled.
And the outer wall of the sliding plate seat is provided with reinforcing ribs which are longitudinally staggered.
The upright post is of a hollow structure, and the inner wall of the upright post is provided with longitudinally staggered reinforcing ribs.
The front end of the sliding plate seat is connected with a front baffle, the rear end of the sliding plate seat is connected with a motor shield, and the left end and the right end of the sliding plate seat are connected with side shield plates.
The outer side of the handpiece seat is sleeved with a handpiece shield.
Compared with the prior art, the beneficial effects of the utility model are that: the utility model discloses have very strong support rigidity, set up vertical crisscross strengthening rib through slide plate seat and stand, make it can guarantee that the aircraft nose has very high resonant frequency, avoid producing resonance with the aircraft nose when the main shaft is high-speed rotatory, cause the harmful effects that lathe processing produced, can make the contact surface increase of slide plate seat and stand simultaneously, effectively give off the heat.
Drawings
In order to more clearly illustrate the technical solution of the embodiments of the present invention, the drawings needed to be used in the description of the embodiments will be briefly described as follows:
fig. 1 is a schematic view of the internal structure of the present invention;
fig. 2 is a perspective view of the present invention;
the method comprises the following steps: 1. a slide plate seat; 2. a first lead screw guide rail assembly; 3. a column; 4. a second lead screw guide rail assembly; 5. a headstock; 6. a tool magazine support; 7. a tool magazine disc; 8. a drive motor; 9. a main shaft; 10. a cutter head; 11. reinforcing ribs; 12. a front baffle; 13. a motor shield; 14. a side cover plate; 15. a handpiece shield.
Detailed Description
The technical solutions in the embodiments of the present invention are clearly and completely described below with reference to the 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 embodiment of 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.
Embodiments of the present invention will be described in further detail below with reference to the following drawings, in which:
the utility model provides a vertical machining center's aircraft nose structure, slide plate seat 1 including being located the workstation top and through horizontal slide rail set spare axial displacement, the top of slide plate seat 1 is connected with stand 3 through first lead screw guide rail set spare 2, the front end of stand 3 is connected with headstock 5 through second lead screw guide rail set spare 4, one side corresponds headstock 5 and is connected with tool magazine dish 7 through tool magazine support 6, the upper end of headstock 5 is connected with driving motor 8, main shaft 9 is worn to be equipped with at the middle part, the upper end of this main shaft 9 is connected with driving motor 8's motor shaft, tool bit 10 has been dismantled to the bottom of main shaft 9.
The outer wall of the sliding plate seat 1 is provided with longitudinal staggered reinforcing ribs 11, the upright post 3 is of a hollow structure, the inner wall of the upright post is provided with the longitudinal staggered reinforcing ribs 11, the machine head can be guaranteed to have high resonance frequency, and the phenomenon that the machine tool machining generates bad effect due to resonance with the machine head when the main shaft 9 rotates at high speed is avoided.
The front end of the slide plate seat 1 is connected with a front baffle 12, the rear end of the slide plate seat is connected with a motor shield 13, the left end and the right end of the slide plate seat are connected with side shield plates 14, and the outer side of the headstock 5 is sleeved with a machine head shield 15, so that the transmission parts can be effectively prevented from being blocked and damaged by scraps and cooling liquid generated in the high-speed running process of a machining center.
The utility model discloses have very strong support rigidity, set up vertical crisscross strengthening rib 11 through slide plate seat 1 and stand 3, make it can guarantee that the aircraft nose has very high resonant frequency, avoid producing resonance with the aircraft nose when 9 high-speed rotations of main shaft, cause the bad effect that machine tooling produced, can make the contact surface increase of slide plate seat 1 and stand 3 simultaneously, effectively give off the heat.
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 (5)
1. The utility model provides a vertical machining center's aircraft nose structure, its characterized in that, including slide plate seat (1) that is located the workstation top and passes through horizontal slide rail assembly axial displacement, the top of slide plate seat (1) is connected with stand (3) through first lead screw guide rail assembly (2), the front end of stand (3) is connected with headstock (5) through second lead screw guide rail assembly (4), and one side corresponds headstock (5) and is connected with tool magazine dish (7) through tool magazine support (6), the upper end of headstock (5) is connected with driving motor (8), and main shaft (9) are worn to be equipped with in the middle part, the upper end of this main shaft (9) with the motor shaft of driving motor (8) is connected, tool bit (10) have been installed to the bottom of main shaft (9) can be dismantled.
2. The machine head structure of the vertical machining center according to claim 1, characterized in that the outer wall of the slide plate seat (1) is provided with reinforcing ribs (11) which are longitudinally staggered.
3. The machine head structure of a vertical machining center according to claim 1, characterized in that the upright (3) is a hollow structure, and the inner wall of the upright is provided with longitudinally staggered reinforcing ribs (11).
4. The machine head structure of the vertical machining center according to claim 1, wherein the front end of the slide plate seat (1) is connected with a front baffle (12), the rear end is connected with a motor shield (13), and the left end and the right end are connected with side shield plates (14).
5. The machine head structure of the vertical machining center according to claim 1, wherein a machine head shield (15) is sleeved on the outer side of the machine head seat (5).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202223232604.8U CN218575527U (en) | 2022-11-30 | 2022-11-30 | Machine head structure of vertical machining center |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202223232604.8U CN218575527U (en) | 2022-11-30 | 2022-11-30 | Machine head structure of vertical machining center |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN218575527U true CN218575527U (en) | 2023-03-07 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202223232604.8U Active CN218575527U (en) | 2022-11-30 | 2022-11-30 | Machine head structure of vertical machining center |
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| Country | Link |
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| CN (1) | CN218575527U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN117620755A (en) * | 2024-01-26 | 2024-03-01 | 山东豪迈机械制造有限公司 | Water ripple line processing device for container pipe box |
-
2022
- 2022-11-30 CN CN202223232604.8U patent/CN218575527U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN117620755A (en) * | 2024-01-26 | 2024-03-01 | 山东豪迈机械制造有限公司 | Water ripple line processing device for container pipe box |
| CN117620755B (en) * | 2024-01-26 | 2024-04-26 | 山东豪迈机械制造有限公司 | Water ripple line processing device for container pipe box |
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