CN218341640U - Line rail vertical machining center head structure - Google Patents
Line rail vertical machining center head structure Download PDFInfo
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- CN218341640U CN218341640U CN202222744813.4U CN202222744813U CN218341640U CN 218341640 U CN218341640 U CN 218341640U CN 202222744813 U CN202222744813 U CN 202222744813U CN 218341640 U CN218341640 U CN 218341640U
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- aircraft nose
- machining center
- vertical machining
- machine head
- head structure
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Abstract
The utility model discloses a linear rail vertical machining center machine head structure, use in vertical machining center technical field, through setting up the aircraft nose, the posting, the carriage, lubricating mechanism, the removal subassembly, locating component and flowing back subassembly, through setting up the posting, can arrange the inside of posting in the aircraft nose, then through setting up lubricating mechanism and flowing back subassembly, can make the inside lubricating oil of lubricating mechanism emit to the inside aircraft nose of posting on the surface, thereby make and establish the oil film between two glide planes, the oil film that has enough thickness separates relative slip's partial surface, make the aircraft nose excessively wear when preventing the aircraft nose processing part, thereby reach the mesh that reduces wear, through setting up the removal subassembly, can make the aircraft nose remove, be convenient for lubricating oil distribution is on the surface of aircraft nose, through setting up locating component, can make the aircraft nose fixed in the inside of removal subassembly, prevent that the aircraft nose from breaking away from the removal subassembly.
Description
Technical Field
The utility model belongs to the technical field of vertical machining center, in particular to line rail vertical machining center machine head structure.
Background
A processing center: the numerical control machine tool is a highly automated multifunctional numerical control machine tool with a tool magazine and an automatic tool changer, and is mainly suitable for processing complex parts such as plates, discs, dies and small shells.
The current announcements are: CN 209953814U's chinese utility model patent discloses a line rail vertical machining center machine head structure, the on-line screen storage device comprises a base, vertical direction slide rail, bear the weight of the box, the headstock, driving motor, the main shaft, tray and line type track, it is connected with the base to bear the weight of the box rear end face, at least two vertical direction slide rails are established to the base rear end face, the operation groove is established to the terminal surface under the bearing the box, line type track is at least two, be located the bearing the box, the tray passes through slider and line type track sliding connection each other, headstock output and main shaft interconnect, driving motor installs at the headstock surface and with the input end interconnect of headstock, this novel one side can effectively satisfy the needs of the quick erection joint operation between with the lathe equipment, on the other hand can effectually satisfy the needs of carrying out high-efficient erection site operation to equipment such as main shaft gear case, thereby very big improvement lathe equipment stability and reliability and operation precision.
When the existing vertical machining center operates for a long time, the machine head and parts generate large friction, the machine head is excessively abraded due to the long-time friction, and economic loss is possibly generated while the stability of equipment is influenced.
SUMMERY OF THE UTILITY MODEL
The utility model aims at providing a vertical machining center of linear rail machine head structure, its advantage has the oil film of establishment, prevents the excessive effect of aircraft nose wearing and tearing.
The above technical scheme of the utility model can be realized through following technical scheme, a line rail vertical machining center machine head structure, which comprises a head, the outside of aircraft nose is provided with the posting, the outer lateral wall welding of posting has the carriage, the top of carriage is provided with lubricated mechanism, the inside of posting is provided with removes the subassembly, the inside of removing the subassembly is provided with locating component, the inside of lubricated mechanism is provided with the flowing back subassembly, lubricated mechanism uses with the flowing back subassembly cooperation.
Adopt above-mentioned technical scheme, through setting up the aircraft nose, the locating frame, the carriage, lubricating mechanism, the removal subassembly, locating component and flowing back subassembly, through setting up the locating frame, can arrange the aircraft nose in the inside of locating frame, then through setting up lubricating mechanism and flowing back subassembly, can make the inside lubricating oil of lubricating mechanism arrange into to the aircraft nose of locating frame on the surface, thereby make and establish the oil film between two glide planes, the oil film that has enough thickness separates the partial surface of relative slip, make the aircraft nose excessive wear when preventing aircraft nose processing part, thereby reach the purpose that reduces wearing and tearing, through setting up the removal subassembly, can make the aircraft nose remove, be convenient for lubricating oil distribution on the surface of aircraft nose, through setting up the locating component, can make the aircraft nose fixed in the inside of removing the subassembly, prevent that the aircraft nose from breaking away from the removal subassembly.
The utility model discloses further set up to: lubricating mechanism includes liquid reserve tank, feed liquor pipe, sealed lid, division board and air pump, the liquid reserve tank bolt is in the inside of carriage, feed liquor pipe intercommunication set up with the outer lateral wall of liquid reserve tank, sealed lid threaded connection is in the outer wall of feed liquor pipe, the division board welds on a lateral wall of carriage, the air pump bolt is in the top of division board, the output of air pump and the inside intercommunication of liquid reserve tank.
Adopt above-mentioned technical scheme, through setting up liquid reserve tank, feed liquor pipe, sealed lid, division board and air pump, when using, through starting the air pump, make the inside lubricating oil of liquid reserve tank be convenient for can passive discharge to the outside of liquid reserve tank, played the effect of lubricating the aircraft nose.
The utility model discloses further set up to: the movable assembly comprises a first screw rod, a sliding rod, a fixing plate, a motor and a supporting table, the first screw rod is connected to the inside of the positioning frame in a rotating mode, the sliding rod is welded to the inside of the positioning frame and located on one side of the positioning frame, the fixing plate is welded to the outer side wall of the positioning frame, the motor is bolted to the top of the fixing plate, the supporting table is connected to the outside of the first screw rod in a threaded mode, and one end of the supporting table is connected with the sliding rod in a sliding mode.
Adopt above-mentioned technical scheme, through setting up first screw rod, slide bar, fixed plate, motor and brace table, the motor drives first screw rod rotatory when using, and first screw rod is rotatory to be made the brace table remove along first screw rod and slide bar, has played the effect that removes the aircraft nose.
The utility model discloses further set up to: the locating component comprises a second screw rod, a rotating shaft and a clamping plate, the second screw rod is connected to the inside of the supporting table in a threaded mode, the rotating shaft is connected to one end of the second screw rod in a rotating mode, and the clamping plate is welded to one end of the rotating shaft.
Adopt above-mentioned technical scheme, through setting up second screw rod, pivot and splint, when using, through twisting the second screw rod, can make a lateral wall of splint closely laminate with a lateral wall of aircraft nose, played the effect of fixed aircraft nose.
The utility model discloses further set up to: the flowing back subassembly includes fluid-discharge tube and shower nozzle, the fluid-discharge tube intercommunication sets up in a lateral wall of liquid reserve tank, the shower nozzle intercommunication sets up in the one end of fluid-discharge tube.
Adopt above-mentioned technical scheme, through setting up fluid-discharge tube and shower nozzle, when the air pump function, can make the inside lubricating oil of liquid reserve tank pass through the fluid-discharge tube and discharge to the outside of liquid reserve tank, played the effect of direction lubricating oil.
The utility model discloses further set up to: the horizontal height of the bottom end of the spray head is higher than that of the top of the machine head.
By adopting the technical scheme, the sprayer with the horizontal height higher than the sprayer head is arranged, so that when the movable assembly drives the sprayer head to move, collision between the sprayer head and the sprayer head is prevented, and the sprayer head is protected.
The utility model discloses further set up to: the liquid discharge pipe is S-shaped, and the horizontal height of one end of the liquid discharge pipe is slightly higher than the inner bottom wall of the liquid storage tank.
Adopt above-mentioned technical scheme, be the fluid-discharge tube of S type through setting up the shape, when using, can make the outside of the outflow shower nozzle that the inside remaining lubricating oil of liquid reserve tank and fluid-discharge tube can not be initiative, played the effect of preventing leaking.
To sum up, the utility model discloses following beneficial effect has:
through setting up the aircraft nose, the locating frame, the carriage, lubricating mechanism, the removal subassembly, locating component and flowing back subassembly, through setting up the locating frame, can arrange the aircraft nose in the inside of locating frame, then through setting up lubricating mechanism and flowing back subassembly, can make the inside lubricating oil of lubricating mechanism arrange into to the aircraft nose of locating frame on the surface, thereby make and establish the oil film between two glide planes, the oil film that has enough thickness separates the partial surface of relative slip, make the aircraft nose excessive wearing and tearing when preventing the aircraft nose processing part, thereby reach the mesh of reducing wear, through setting up the removal subassembly, can make the aircraft nose remove, be convenient for lubricating oil distributes on the surface of aircraft nose, through setting up locating component, can make the aircraft nose fixed in the inside of removal subassembly, prevent that the aircraft nose from breaking away from the removal subassembly.
Drawings
FIG. 1 is a schematic view of the overall structure of the present invention;
fig. 2 is a left side view of the present invention;
FIG. 3 isbase:Sub>A perspective cross-sectional view taken at A-A of FIG. 2 according to the present invention;
fig. 4 is a schematic structural view of the liquid discharge assembly of the present invention;
fig. 5 is an enlarged view of a portion a in fig. 3 according to the present invention.
In the figure, 1, a machine head; 2. a positioning frame; 3. a support frame; 4. a lubrication mechanism; 5. a moving assembly; 6. a positioning assembly; 7. a liquid discharge assembly; 401. a liquid storage tank; 402. a liquid inlet pipe; 403. a sealing cover; 404. a separator plate; 405. an air pump; 501. a first screw; 502. a slide bar; 503. a fixing plate; 504. a motor; 505. a support table; 601. a second screw; 602. a rotating shaft; 603. a splint; 701. a liquid discharge pipe; 702. and (4) a spray head.
Detailed Description
The present invention will be described in further detail with reference to the accompanying drawings.
Example (b):
referring to fig. 1-5, the present invention provides a technical solution: the utility model provides a vertical machining center aircraft nose 1 structure of line rail, including aircraft nose 1, the outside of aircraft nose 1 is provided with locating frame 2, locating frame 2's outer lateral wall has welded carriage 3, carriage 3's top is provided with lubricating mechanism 4, carriage 2's inside is provided with removal subassembly 5, removal subassembly 5's inside is provided with locating component 6, lubricating mechanism 4's inside is provided with flowing back subassembly 7, lubricating mechanism 4 uses with flowing back subassembly 7 cooperation, through setting up aircraft nose 1, locating frame 2, carriage 3, lubricating mechanism 4, removal subassembly 5, locating component 6 and flowing back subassembly 7, through setting up locating frame 2, can arrange aircraft nose 1 in the inside of locating frame 2, then through setting up lubricating mechanism 4 and flowing back subassembly 7, can make the lubricating oil of lubricating mechanism 4 inside discharge into to aircraft nose 1 inside on the surface of locating frame 2, thereby make and establish between two glide planes, the partial surface that relative slip separates with having enough thickness, make aircraft nose 1 excessively abrade when preventing aircraft nose 1 processing part, thereby reach the mesh that reduces wearing and tearing, through setting up removal subassembly 5, be convenient for make aircraft nose 1 move, the lubricating oil film that distributes and is fixed at aircraft nose subassembly 1, prevent to be separated from moving by locating component 5, prevent aircraft nose subassembly 5.
Referring to fig. 3, the lubricating mechanism 4 includes a liquid storage tank 401, a liquid inlet pipe 402, a sealing cover 403, a partition plate 404 and an air pump 405, the liquid storage tank 401 is bolted to the inside of the supporting frame 3, the liquid inlet pipe 402 is communicated with an outer side wall of the liquid storage tank 401, the sealing cover 403 is in threaded connection with the outer wall of the liquid inlet pipe 402, the partition plate 404 is welded on one side wall of the supporting frame 3, the air pump 405 is bolted to the top of the partition plate 404, the output end of the air pump 405 is communicated with the inside of the liquid storage tank 401, by arranging the liquid storage tank 401, the liquid inlet pipe 402, the sealing cover 403, the partition plate 404 and the air pump 405, when in use, by starting the air pump 405, the lubricating oil inside the liquid storage tank 401 can be passively discharged to the outside of the liquid storage tank 401, and a function of lubricating the handpiece 1 is achieved.
Referring to fig. 3, the moving assembly 5 includes a first screw 501, a sliding rod 502, a fixing plate 503, a motor 504 and a support platform 505, the first screw 501 is rotatably connected to the inside of the positioning frame 2, the sliding rod 502 is welded to the inside of the positioning frame 2 and located at one side of the positioning frame 2, the fixing plate 503 is welded to an outer side wall of the positioning frame 2, the motor 504 is bolted to the top of the fixing plate 503, the support platform 505 is threadedly connected to the outside of the first screw 501, one end of the support platform 505 is slidably connected to the sliding rod 502, the first screw 501, the sliding rod 502, the fixing plate 503, the motor 504 and the support platform 505 are disposed, when in use, the motor 504 drives the first screw 501 to rotate, and the support platform 505 rotates along the first screw 501 and the sliding rod 502, thereby playing a role of moving the machine head 1.
Referring to fig. 3, the positioning assembly 6 includes a second screw 601, a rotating shaft 602, and a clamping plate 603, the second screw 601 is screwed into the supporting platform 505, the rotating shaft 602 is rotatably connected to one end of the second screw 601, and the clamping plate 603 is welded to one end of the rotating shaft 602, and by providing the second screw 601, the rotating shaft 602, and the clamping plate 603, when in use, by screwing the second screw 601, one side wall of the clamping plate 603 can be tightly attached to one side wall of the handpiece 1, thereby playing a role of fixing the handpiece 1.
Referring to fig. 5, the liquid discharge assembly 7 includes a liquid discharge pipe 701 and a spray head 702, the liquid discharge pipe 701 is communicated with and disposed in a side wall of the liquid storage tank 401, the spray head 702 is communicated with and disposed at one end of the liquid discharge pipe 701, and by providing the liquid discharge pipe 701 and the spray head 702, when the air pump 405 operates, the lubricating oil in the liquid storage tank 401 can be discharged to the outside of the liquid storage tank 401 through the liquid discharge pipe 701, so that a function of guiding the lubricating oil is performed.
Referring to fig. 3, the horizontal height of the bottom end of the spray head 702 is higher than the horizontal height of the top of the machine head 1, and by arranging the spray head 702 with the horizontal height higher than the machine head 1, when the moving assembly 5 drives the machine head 1 to move, collision between the machine head 1 and the spray head 702 is prevented, and the spray head 702 is protected.
Referring to fig. 3, the drain pipe 701 is S-shaped, the horizontal height of one end of the drain pipe 701 is slightly higher than the inner bottom wall of the liquid storage tank 401, and by providing the drain pipe 701 in the S-shaped shape, the lubricant remaining inside the liquid storage tank 401 and the drain pipe 701 can not actively flow out of the spray head 702 during use, thereby achieving a leakage-proof effect.
The using process is briefly described as follows: when the device is used, lubricating oil is poured into the liquid storage tank 401 through the liquid inlet pipe 402, the motor 504 and the air pump 405 are connected with an external power supply, the machine head 1 is placed on the top of the support platform 505, the second screw 601 is screwed, one side wall of the clamping plate 603 is tightly attached to one side wall of the machine head 1, the machine head 1 is fixed, the motor 504 is started, the motor 504 drives the first screw 501 to rotate, the support platform 505 can move along the first screw 501 and the sliding rod 502 due to the rotation of the first screw 501, the machine head 1 can move towards one side, when the machine head 1 moves to a proper position, the air pump 405 is started, the lubricating oil in the liquid storage tank 401 can be discharged onto the surface of the machine head 1 through the liquid discharge pipe 701 and the spray head 702 by the air pump 405, so that an oil film is established between the two sliding surfaces, the oil film with enough thickness separates partial surfaces sliding, the machine head 1 is prevented from being excessively worn when parts are machined by the machine head 1, and the purpose of preventing the machine head 1 from being excessively worn.
The present embodiment is only for explaining the present invention, and it is not limited to the present invention, and those skilled in the art can make modifications to the present embodiment without inventive contribution as required after reading the present specification, but all of them are protected by patent laws within the scope of the claims of the present invention.
Claims (7)
1. The utility model provides a line rail vertical machining center head structure, includes aircraft nose (1), its characterized in that: the outside of aircraft nose (1) is provided with posting (2), the outer lateral wall welded of posting (2) has carriage (3), the top of carriage (3) is provided with lubricated mechanism (4), the inside of posting (2) is provided with removes subassembly (5), the inside of removing subassembly (5) is provided with locating component (6), the inside of lubricated mechanism (4) is provided with flowing back subassembly (7), lubricated mechanism (4) and flowing back subassembly (7) cooperation are used.
2. The machine head structure of the linear rail vertical machining center of claim 1, characterized in that: lubricated mechanism (4) include liquid reserve tank (401), feed liquor pipe (402), sealed lid (403), division board (404) and air pump (405), liquid reserve tank (401) bolt is in the inside of carriage (3), feed liquor pipe (402) intercommunication sets up in the outer lateral wall of liquid reserve tank (401), sealed lid (403) threaded connection is in the outer wall of feed liquor pipe (402), division board (404) weld on the lateral wall of carriage (3), air pump (405) bolt is at the top of division board (404), the output of air pump (405) and the inside intercommunication of liquid reserve tank (401).
3. The machine head structure of the vertical machining center for wire rails as claimed in claim 1, wherein: the moving assembly (5) comprises a first screw (501), a sliding rod (502), a fixing plate (503), a motor (504) and a supporting table (505), the first screw (501) is rotatably connected to the inside of the positioning frame (2), the sliding rod (502) is welded to the inside of the positioning frame (2) and located on one side of the positioning frame (2), the fixing plate (503) is welded to the outer side wall of the positioning frame (2), the motor (504) is bolted to the top of the fixing plate (503), the supporting table (505) is in threaded connection with the outside of the first screw (501), and one end of the supporting table (505) is in sliding connection with the sliding rod (502).
4. The machine head structure of the vertical machining center for wire rails as claimed in claim 3, wherein: the positioning assembly (6) comprises a second screw rod (601), a rotating shaft (602) and a clamping plate (603), the second screw rod (601) is connected to the inside of the supporting table (505) in a threaded mode, the rotating shaft (602) is connected to one end of the second screw rod (601) in a rotating mode, and the clamping plate (603) is welded to one end of the rotating shaft (602).
5. The machine head structure of the vertical machining center of a linear rail as claimed in claim 2, wherein: the liquid discharge assembly (7) comprises a liquid discharge pipe (701) and a spray head (702), the liquid discharge pipe (701) is communicated with and arranged in one side wall of the liquid storage tank (401), and the spray head (702) is communicated with and arranged at one end of the liquid discharge pipe (701).
6. The machine head structure of the vertical machining center for wire rails as claimed in claim 5, wherein: the horizontal height of the bottom end of the spray head (702) is higher than that of the top of the machine head (1).
7. The machine head structure of the vertical machining center of a linear rail as claimed in claim 5, wherein: the liquid discharge pipe (701) is S-shaped, and the horizontal height of one end of the liquid discharge pipe (701) is slightly higher than the inner bottom wall of the liquid storage tank (401).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202222744813.4U CN218341640U (en) | 2022-10-18 | 2022-10-18 | Line rail vertical machining center head structure |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202222744813.4U CN218341640U (en) | 2022-10-18 | 2022-10-18 | Line rail vertical machining center head structure |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN218341640U true CN218341640U (en) | 2023-01-20 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202222744813.4U Active CN218341640U (en) | 2022-10-18 | 2022-10-18 | Line rail vertical machining center head structure |
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| Country | Link |
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| CN (1) | CN218341640U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN116394060A (en) * | 2023-03-07 | 2023-07-07 | 云一机(江苏)智能装备有限公司 | Automatic lubrication system of variable speed numerical control machine tool |
-
2022
- 2022-10-18 CN CN202222744813.4U patent/CN218341640U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN116394060A (en) * | 2023-03-07 | 2023-07-07 | 云一机(江苏)智能装备有限公司 | Automatic lubrication system of variable speed numerical control machine tool |
| CN116394060B (en) * | 2023-03-07 | 2023-10-20 | 云一机(江苏)智能装备有限公司 | Automatic lubrication system of variable speed numerical control machine tool |
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