CN217369926U - Adjustable pipe bender head structure - Google Patents
Adjustable pipe bender head structure Download PDFInfo
- Publication number
- CN217369926U CN217369926U CN202220535219.1U CN202220535219U CN217369926U CN 217369926 U CN217369926 U CN 217369926U CN 202220535219 U CN202220535219 U CN 202220535219U CN 217369926 U CN217369926 U CN 217369926U
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- China
- Prior art keywords
- lift
- seat
- hand member
- aircraft nose
- lathe
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- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
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- Bending Of Plates, Rods, And Pipes (AREA)
Abstract
The utility model discloses a bending machine aircraft nose structure with adjustable, which comprises a lathe, lift guide and screw rod seat are installed to the right-hand member of lathe, it has the lift seat to peg graft on the lift guide, be connected with lift adjusting screw between the screw rod seat, lift adjusting screw runs through via lift seat middle part, the right-hand member of lift seat is connected with the mounting panel, the aircraft nose is installed through the mounting bracket to the right-hand member of mounting panel, the right-hand member of mounting bracket lower extreme left side is fixed in the mounting panel through the triangle reinforcing plate. The utility model discloses a to the rotation of lift adjusting screw, but the height that the lift seat drove the aircraft nose freely adjusts, run into the pipe fitting that has the interference then with the mode that the mould center increases, the aircraft nose descends and avoid the interference when the pipe fitting installation, then insert the left end of pipe fitting smoothly to the clamping section of thick bamboo in can carry out subsequent return bend operation.
Description
Technical Field
The utility model relates to a bending machine technical field specifically is a bending machine aircraft nose structure with adjustable.
Background
The traditional machine head is directly fixed on a lathe bed, the center height of a die is invariable, and the machine head cannot be bent when the die is interfered by a complex pipe fitting.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide a bending machine aircraft nose structure with adjustable to solve the problem that proposes among the above-mentioned background art.
In order to achieve the above purpose, the utility model provides a following technical scheme: the utility model provides a bending machine aircraft nose structure with adjustable, includes the lathe, lift guide and screw rod seat are installed to the right-hand member of lathe, it has the lift seat to slide on the lift guide, be connected with the lift adjusting screw between the screw rod seat, the lift adjusting screw runs through via lift seat middle part, the right-hand member of lift seat is connected with the mounting panel, the aircraft nose is installed through the mounting bracket to the right-hand member of mounting panel, the right-hand member of mounting panel is fixed in through the triangle reinforcing plate in mounting bracket lower extreme left side.
As the further optimization of this technical scheme, a plurality of groups of guard plates are installed in the front of lathe, be equipped with the ventilative grid of a plurality of groups on the guard plate, the landing leg is installed to the lathe bottom.
As the further optimization of this technical scheme, it has the removal seat to slide on the horizontal guide rail of lathe upper end, the right-hand member of removing the seat is connected with a clamping section of thick bamboo, remove the upper end of seat and install servo motor, servo motor's output passes through the drive shaft drive clamping section of thick bamboo in the gearbox.
Compared with the prior art, the beneficial effects of the utility model are that: the utility model discloses a to the rotation of lift adjusting screw, but the height that the lift seat drove the aircraft nose freely adjusts, run into the pipe fitting that has the interference then with the mode that the mould center increases, the aircraft nose descends and avoid the interference when the pipe fitting installation, then insert the left end of pipe fitting smoothly to the clamping section of thick bamboo in can carry out subsequent return bend operation.
Drawings
Fig. 1 is a schematic structural diagram of the present invention.
In the figure: the device comprises a screw seat 1, a lifting adjusting screw 2, a lifting guide rail 3, a lifting seat 4, a mounting plate 5, a mounting frame 6, a machine head 7, a triangular reinforcing plate 8, supporting legs 9, a machine tool 10, a protection plate 11, a ventilating grating 12, a clamping cylinder 13, a servo motor 14, a moving seat 15, a gearbox 16 and a horizontal guide rail 17.
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 present invention provides a technical solution: the utility model provides a bending machine aircraft nose structure with adjustable, includes lathe 10, lift guide 3 and screw rod seat 1 are installed to the right-hand member of lathe 10, it has lift seat 4 to slide to connect on the lift guide 3, be connected with lift adjusting screw 2 between the screw rod seat 1, lift adjusting screw 2 runs through 4 middle parts of lift seat, the right-hand member of lift seat 4 is connected with mounting panel 5, aircraft nose 7 is installed through mounting bracket 6 to the right-hand member of mounting panel 5, 6 lower extreme left sides of mounting bracket are fixed in the right-hand member of mounting panel 5 through triangle reinforcing plate 8.
A plurality of groups of protection plates 11 are installed on the front surface of the machine tool 10, a plurality of groups of air-permeable grids 12 are arranged on the protection plates 11, and supporting legs 9 are installed at the bottom of the machine tool 10.
Specifically, when the lifting device is used, the lifting guide rail 3 is slidably connected with the lifting seat 4, the lifting adjusting screw 2 penetrates through the middle of the lifting seat 4, and the lifting seat 4 can move up and down on the lifting guide rail 3 by rotating the lifting adjusting screw 2;
through the rotation to lift adjusting screw 2, but the height that lift seat 4 drove aircraft nose 7 is adjusted freely, touches the pipe fitting that has the interference and then increases with the mould center, the interference when the aircraft nose 7 descends avoids the pipe fitting installation, then inserts the left end of pipe fitting smoothly to the clamping section of thick bamboo 13 in can carrying out subsequent return bend operation.
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 (3)
1. An adjustable pipe bender head structure, includes lathe (10), its characterized in that: lifting guide (3) and screw rod seat (1) are installed to the right-hand member of lathe (10), it has lift seat (4) to slide to connect on lifting guide (3), be connected with lift adjusting screw (2) between screw rod seat (1), lift adjusting screw (2) run through via lift seat (4) middle part, the right-hand member of lift seat (4) is connected with mounting panel (5), aircraft nose (7) are installed through mounting bracket (6) to the right-hand member of mounting panel (5), the right-hand member in mounting bracket (5) is fixed in through triangle reinforcing plate (8) in mounting bracket (6) lower extreme left side.
2. The adjustable bender head structure according to claim 1, wherein: a plurality of groups of protection plates (11) are installed on the front surface of the machine tool (10), a plurality of groups of breathable grids (12) are arranged on the protection plates (11), and the bottom of the machine tool (10) is provided with supporting legs (9).
3. The adjustable bender head structure according to claim 1, wherein: horizontal guide rail (17) of lathe (10) upper end have slided and have moved seat (15), the right-hand member that moves seat (15) is connected with clamping barrel (13), servo motor (14) are installed to the upper end that moves seat (15), drive shaft drive clamping barrel (13) in gearbox (16) are passed through to servo motor's (14) output.
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202121503134 | 2021-07-05 | ||
| CN2021215031347 | 2021-07-05 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN217369926U true CN217369926U (en) | 2022-09-06 |
Family
ID=83102077
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202220535219.1U Active CN217369926U (en) | 2021-07-05 | 2022-03-14 | Adjustable pipe bender head structure |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN217369926U (en) |
-
2022
- 2022-03-14 CN CN202220535219.1U patent/CN217369926U/en active Active
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| GR01 | Patent grant | ||
| GR01 | Patent grant |