CN218874453U - Novel gantry cutting machine - Google Patents
Novel gantry cutting machine Download PDFInfo
- Publication number
- CN218874453U CN218874453U CN202223237264.8U CN202223237264U CN218874453U CN 218874453 U CN218874453 U CN 218874453U CN 202223237264 U CN202223237264 U CN 202223237264U CN 218874453 U CN218874453 U CN 218874453U
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- China
- Prior art keywords
- speed reducer
- aircraft nose
- portal frame
- rack
- gear
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02P—CLIMATE CHANGE MITIGATION TECHNOLOGIES IN THE PRODUCTION OR PROCESSING OF GOODS
- Y02P70/00—Climate change mitigation technologies in the production process for final industrial or consumer products
- Y02P70/10—Greenhouse gas [GHG] capture, material saving, heat recovery or other energy efficient measures, e.g. motor control, characterised by manufacturing processes, e.g. for rolling metal or metal working
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Abstract
The utility model relates to a novel longmen cutting machine, including the main frame, a workbench, the portal frame, the aircraft nose is decided to the hydro-cylinder, aircraft nose driving motor, a speed reducer, remove the seat, gear and rack, install the workstation in the main frame, the portal frame is located the workstation top, the aircraft nose is decided to portal frame below installation hydro-cylinder, aircraft nose driving motor installs in the speed reducer front side, aircraft nose driving motor drives the speed reducer start, the speed reducer is installed in removing the seat top, remove seat fixed connection hydro-cylinder and decide the aircraft nose, speed reducer output shaft installation gear, the gear engagement rack, rack transverse installation is in the portal frame, aircraft nose driving motor drives the speed reducer start, speed reducer driving gear rotates, because the gear engagement rack, rack transverse installation is in the portal frame, can drive during gear rotation and remove seat left and right sides transverse movement, traditional chain mode has been replaced, remove the in-process noise low, and can not split like the chain easy, firm, it is reliable, can realize accurate removal to the stop position of settlement.
Description
Technical Field
The utility model relates to a cutting machine field, concretely relates to novel longmen cutting machine.
Background
The traditional gantry cutting machine drives the machine head to move left and right by using a chain transmission mode, and the noise of the chain transmission mode is relatively high in the using process, and the chain is easy to break and unreliable, so that the gantry cutting machine with a brand-new movable machine head structure is needed to be developed.
SUMMERY OF THE UTILITY MODEL
There is above-mentioned defect to prior art, the utility model provides a novel longmen cutting machine that aircraft nose mobile structure is more reasonable, concrete technical scheme as follows:
the utility model provides a novel longmen cutting machine, including the main frame, a workbench, the aircraft nose is decided to portal frame and hydro-cylinder, install the workstation in the main frame, the portal frame is located the workstation top, the aircraft nose is decided to portal frame below installation hydro-cylinder, still include aircraft nose driving motor, the speed reducer, remove the seat, gear and rack, aircraft nose driving motor installs in the speed reducer front side, aircraft nose driving motor drives the speed reducer and starts, the speed reducer is installed and is being removed the seat top, it decides the aircraft nose to remove seat fixed connection hydro-cylinder, speed reducer output shaft installation gear, the gear engagement rack, the rack is transversely installed in the portal frame.
As a preferred scheme of the utility model, remove seat rear sliding connection guide rail, the guide rail transverse installation is in the portal frame.
As a preferred embodiment of the present invention, the guide rail is lower than the rack.
As a preferred scheme of the utility model, still include the hydraulic oil hose, the aircraft nose is decided to the hydro-cylinder is connected to hydraulic oil hose one end and the other end extends and is connected to fixed connection block, and fixed connection block installs at main frame top intermediate position, and main frame bottom installation hydraulic pressure is stood, and hydraulic pressure is stood and is passed through hydraulic oil hard tube connection fixed connection block.
Has the advantages that: the machine head driving motor drives the speed reducer to start, the speed reducer drives the gear to rotate, and the gear is transversely arranged on the portal frame and can drive the moving seat to transversely move left and right during rotation, so that the traditional chain mode is replaced, the noise in the moving process is low, the moving seat cannot be easily broken like a chain, and the moving seat is firm and reliable and can realize accurate movement to a set stop position.
Drawings
Fig. 1 is a perspective view of the present invention;
fig. 2 is a front view of the present invention;
fig. 3 is a rear view of the present invention;
FIG. 4 isbase:Sub>A cross-sectional view taken along line A-A of FIG. 3;
fig. 5 is an enlarged view at B in fig. 4.
Detailed Description
The following description of the embodiments of the present invention will be made with reference to the accompanying drawings:
in the description of the present invention, it should be noted that the terms "center", "upper", "lower", "left", "right", "vertical", "horizontal", "inner", "outer", and the like indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings, and are only for convenience of description and simplification of description, but do not indicate or imply that the indicated position or element must have a specific orientation, be constructed and operated in a specific orientation, and thus, should not be construed as limiting the present invention.
In the description of the present invention, it is to be noted that, unless otherwise explicitly specified or limited, the terms "mounted," "connected," and "connected" are to be construed broadly, and may be, for example, fixedly connected, detachably connected, or integrally connected; can be mechanically or electrically connected; they may be connected directly or indirectly through intervening media, or they may be interconnected between two elements. The specific meaning of the above terms in the present invention can be understood as appropriate by those of ordinary skill in the art.
As shown in fig. 1-5, a novel longmen cutting machine, including main frame 1, workstation 2, portal frame 3, aircraft nose 4 is decided to the hydro-cylinder, aircraft nose driving motor 5, speed reducer 6, remove seat 7, gear 8 and rack 9, install workstation 2 in the main frame 1, portal frame 3 is located workstation 2 top, aircraft nose 4 is decided to 3 below installation hydro-cylinders of portal frame, aircraft nose driving motor 5 installs in 6 front sides of speed reducer, aircraft nose driving motor 5 drives speed reducer 6 and starts, speed reducer 6 installs in removing seat 7 top, it decides aircraft nose 4 to remove seat 7 fixed connection hydro-cylinder, gear 8 is installed to 6 output shafts of speed reducer, gear 8 meshes rack 9, rack 9 transversely installs in portal frame 3.
For better guidance, a guide rail 10 is slidably connected behind the moving seat 7, the guide rail 10 is transversely installed on the portal frame 3, and the installation position of the guide rail 10 is lower than that of the rack 9.
Gantry cutting machine still includes hydraulic oil hose 11, and hydraulic oil hose 11 one end is connected the hydro-cylinder and is decided aircraft nose 4 and the other end extension is connected to fixed connection block 12, and fixed connection block 12 is installed at 1 top intermediate position of main frame, and 1 bottom installation hydraulic pressure station 13 of main frame, hydraulic pressure station 13 pass through hydraulic oil hard tube 14 and connect fixed connection block 12, and hydraulic pressure station 13 provides hydraulic power and decides the material for the hydro-cylinder cutting die of aircraft nose 4 below.
The above description is provided for the purpose of illustrating the present invention in more detail with reference to the preferred embodiments, and it should not be understood that the present invention is limited to the illustrated embodiments, and those skilled in the art can make various changes and substitutions without departing from the spirit and scope of the present invention.
Claims (4)
1. The utility model provides a novel longmen cutting machine, decides the aircraft nose including main frame, workstation, portal frame and hydro-cylinder, installs workstation, portal frame in the main frame, and the portal frame is located the workstation top, and the aircraft nose is decided to portal frame below installation hydro-cylinder, its characterized in that: the automatic cutting machine further comprises a machine head driving motor, a speed reducer, a moving seat, a gear and a rack, wherein the machine head driving motor is installed on the front side of the speed reducer, the machine head driving motor drives the speed reducer to start, the speed reducer is installed above the moving seat, the machine head is cut by a moving seat fixedly connected with an oil cylinder, the gear is installed on an output shaft of the speed reducer, the gear is meshed with the rack, and the rack is transversely installed on a portal frame.
2. The novel gantry cutting machine according to claim 1, characterized in that: the rear part of the moving seat is connected with a guide rail in a sliding way, and the guide rail is transversely arranged on the portal frame.
3. The novel gantry cutting machine according to claim 2, characterized in that: the guide rail is lower than the rack.
4. The novel gantry cutting machine according to claim 1, characterized in that: still include the hydraulic oil hose, the aircraft nose is decided to the hydro-cylinder is connected to hydraulic oil hose one end and the other end extends and is connected to fixed connection block, and fixed connection block installs at main frame top intermediate position, and main frame bottom installation hydraulic pressure station, hydraulic pressure station pass through hydraulic oil hard tube and connect fixed connection block.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202223237264.8U CN218874453U (en) | 2022-12-01 | 2022-12-01 | Novel gantry cutting machine |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202223237264.8U CN218874453U (en) | 2022-12-01 | 2022-12-01 | Novel gantry cutting machine |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN218874453U true CN218874453U (en) | 2023-04-18 |
Family
ID=85956273
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202223237264.8U Active CN218874453U (en) | 2022-12-01 | 2022-12-01 | Novel gantry cutting machine |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN218874453U (en) |
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2022
- 2022-12-01 CN CN202223237264.8U patent/CN218874453U/en active Active
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| GR01 | Patent grant |