CN209394103U - A kind of tapping cutting code holes all-in-one machine - Google Patents

A kind of tapping cutting code holes all-in-one machine Download PDF

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Publication number
CN209394103U
CN209394103U CN201920014787.5U CN201920014787U CN209394103U CN 209394103 U CN209394103 U CN 209394103U CN 201920014787 U CN201920014787 U CN 201920014787U CN 209394103 U CN209394103 U CN 209394103U
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CN
China
Prior art keywords
backboard
screwed
center
machine
code holes
Prior art date
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.)
Expired - Fee Related
Application number
CN201920014787.5U
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Chinese (zh)
Inventor
黎艳
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Dongguan Yan Feng Cnc Equipment Co Ltd
Original Assignee
Dongguan Yan Feng Cnc Equipment Co Ltd
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Dongguan Yan Feng Cnc Equipment Co Ltd filed Critical Dongguan Yan Feng Cnc Equipment Co Ltd
Priority to CN201920014787.5U priority Critical patent/CN209394103U/en
Application granted granted Critical
Publication of CN209394103U publication Critical patent/CN209394103U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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Abstract

The utility model discloses a kind of tappings to cut code holes all-in-one machine, including fuselage, table top, crossbeam portion, axis chain-drive section, high-power tool changing main shaft, cylinder, automatic tapping device, control box, sliding axle, fixed block, support frame, bottom plate and backboard, the centrally located two sides of fuselage roof have been screwed support frame, crossbeam portion has been screwed at the top of support frame as described above, two sides have been screwed fixed block at crossbeam portion one end center, sliding axle is socketed at the fixed block center, motor casing is provided at the fixed block top center, the motor casing bottom has been screwed backboard, and backboard is located at sliding axle side, described backboard one end is provided with cylinder, the backboard bottom end is provided with automatic tapping device, it is simple that code holes all-in-one machine structure is cut in the tapping, it is easy to operate, both may be used Code holes, and it can be not necessarily to secondary operation with tapping, cost is substantially reduced, time and manpower are saved.

Description

A kind of tapping cutting code holes all-in-one machine
Technical field
The utility model relates to tapping code holes machine technical field, code holes all-in-one machine is cut in specially a kind of tapping.
Background technique
People to the application range of aluminium sheet cutting machine than wide, code holes machine currently on the market can only code holes cannot Tapping considerably increases cost, waste of resource and manpower, and cannot freely adjust material orientation, no to cause secondary operation Conducive to material processing, the process velocity of material is greatly reduced, working efficiency is low, is unfavorable for processing and production, for these Defect, it is necessary for designing a kind of tapping cutting code holes all-in-one machine.
Utility model content
The purpose of this utility model is to provide a kind of tappings to cut code holes all-in-one machine, to solve to mention in above-mentioned background technique Out the problem of.
In order to solve the above-mentioned technical problem, the utility model provides the following technical solutions: a kind of tapping cutting code holes one Machine, including fuselage, table top, crossbeam portion, axis chain-drive section, high-power tool changing main shaft, cylinder, automatic tapping device, control box, sliding Axis, fixed block, support frame, baffle, sliding seat, sliding rail, motor casing, three-phase motor, bottom plate and backboard, the fuselage roof are located at Two sides have been screwed support frame at center, have been screwed crossbeam portion, the crossbeam at the top of support frame as described above Two sides have been screwed fixed block at portion, center, one end, and sliding axle, the fixation are socketed at the fixed block center Motor casing is provided at block top center, the motor casing bottom has been screwed backboard, and backboard is located at sliding axle one Side, described backboard one end are provided with cylinder, and the backboard bottom end is provided with automatic tapping device, and automatic tapping device position In cylinder bottom, the backboard bottom center is provided with high-power tool changing main shaft, and high-power tool changing main shaft is located at and attacks automatically Volume of tooth device is provided with sliding seat at the fuselage roof center, and centrally located two sides are all provided at the top of the sliding seat It is equipped with sliding rail, table top is provided at the sliding seat top center, and connect at the top of table top bottom and sliding rail, the mesa top It has been screwed several baffles.
Further, fixing sleeve is welded at backboard other end center, and fixing sleeve is socketed on the outside of sliding axle.
Further, the crossbeam portion other end has been screwed control box, and is socketed on the outside of control box dust-proof Film.
Further, the fuselage and sliding seat bottom are welded with bottom plate, and bottom plate heights are 2cm.
Further, described motor casing one end is welded with U-board, and connect at the top of U-board bottom and crossbeam portion.
Compared with prior art, the utility model beneficial effect achieved is: code holes all-in-one machine structure is cut in the tapping Simply, easy to operate, using manual operation control box, make automatic tapping device rapidoprint, then freely slidable by sliding rail Table top, not only can code holes, but also can be not necessarily to secondary operation with tapping, substantially reduce cost, save time and manpower, and adjustable Material orientation increases material working (finishing) area, is conducive to material processing, while accelerating the process velocity of material, processes more steady It is fixed, working efficiency is greatly increased, processing and production are conducive to.
Detailed description of the invention
Attached drawing is used to provide a further understanding of the present invention, and constitutes part of specification, practical with this Novel embodiment is used to explain the utility model together, does not constitute limitations of the present invention.In the accompanying drawings:
Fig. 1 is the overall structure diagram of the utility model;
Fig. 2 is the part enlarged drawing of the automatic tapping device of the utility model;
Fig. 3 is the overall structure front view of the utility model;
In figure: 1, fuselage;2, table top;3, crossbeam portion;4, axis chain-drive section;5, high-power tool changing main shaft;6, cylinder;7, automatic Tapping device;8, control box;9, sliding axle;10, fixed block;11, support frame;12, baffle;13, sliding seat;14, sliding rail;15, Motor casing;16, three-phase motor;17, bottom plate;18, backboard.
Specific embodiment
The following will be combined with the drawings in the embodiments of the present invention, carries out the technical scheme in the embodiment of the utility model Clearly and completely describe, it is clear that the described embodiments are only a part of the embodiments of the utility model, rather than whole Embodiment.Based on the embodiments of the present invention, those of ordinary skill in the art are without making creative work Every other embodiment obtained, fall within the protection scope of the utility model.
Fig. 1-3 is please referred to, the utility model provides a kind of technical solution: a kind of tapping cutting code holes all-in-one machine, including machine Body 1, table top 2, crossbeam portion 3, axis chain-drive section 4, high-power tool changing main shaft 5, cylinder 6, automatic tapping device 7, control box 8, sliding Axis 9, fixed block 10, support frame 11, baffle 12, sliding seat 13, sliding rail 14, motor casing 15, three-phase motor 16, bottom plate 17 and backboard 18, the 1 centrally located two sides in top of fuselage have been screwed support frame 11, have been screwed at the top of support frame 11 Crossbeam portion 3,3 other end of crossbeam portion has been screwed control box 8, and is socketed with dustproof film on the outside of control box 8, is conducive to The machine operates, and two sides have been screwed fixed block 10 at 3 one end center of crossbeam portion, and fixed block is socketed at 10 center Sliding axle 9 is provided with motor casing 15 at 10 top center of fixed block, and 15 one end of motor casing is welded with U-board, and U-board bottom It is connected at the top of crossbeam portion 3, is conducive to motor casing 15 and fixes, 15 bottom of motor casing has been screwed backboard 18, and backboard 18 are located at 9 side of sliding axle, fixing sleeve are welded at 18 other end center of backboard, and fixing sleeve is socketed in 9 outside of sliding axle, has Fixed conducive to backboard 18,18 one end of backboard is provided with cylinder 6, and 18 bottom end of backboard is provided with automatic tapping device 7, and automatic Tapping device 7 is located at 6 bottom of cylinder, and 18 bottom center of backboard is provided with high-power tool changing main shaft 5, and high-power tool changing main shaft 5 are located at 7 volumes of automatic tapping device, and sliding seat 13 is provided at 1 top center of fuselage, and 13 top of sliding seat is centrally located Two sides are provided with sliding rail 14, table top 2 are provided at 13 top center of sliding seat, and connect at the top of 2 bottom of table top and sliding rail 14, Several baffles 12 are screwed at the top of table top 2, fuselage 1 and 13 bottom of sliding seat are welded with bottom plate 17, and bottom plate 17 Height is 2cm, is conducive to fuselage 1 and sliding seat 13 is fixed;The tapping cuts code holes all-in-one machine in use, the tapping of needs is cut The material for cutting code holes is placed on 2 top of table top, and when needing tapping, manual operation control box 8, control box 8 controls cylinder 6 and pushes certainly Dynamic tapping device 7 moves downward, automatic tapping device 7 can tapping and cutting code holes, high-power tool changing main shaft 5 can freely change Knife, when needing certain positions of materials, table top 2 can be slid back and forth by sliding rail 14, while table top 2 can be freely in fuselage 1 top horizontally slips, can tapping and cutting code holes material.
It should be noted that, in this document, relational terms such as first and second and the like are used merely to a reality Body or operation are distinguished with another entity or operation, are deposited without necessarily requiring or implying between these entities or operation In any actual relationship or order or sequence.Moreover, the terms "include", "comprise" or its any other variant are intended to Non-exclusive inclusion, so that the process, method, article or equipment including a series of elements is not only wanted including those Element, but also including other elements that are not explicitly listed, or further include for this process, method, article or equipment Intrinsic element.
Finally, it should be noted that the above descriptions are merely preferred embodiments of the present invention, it is not limited to this Utility model, although the utility model is described in detail with reference to the foregoing embodiments, for those skilled in the art For, it is still possible to modify the technical solutions described in the foregoing embodiments, or to part of technical characteristic It is equivalently replaced.Within the spirit and principle of the utility model, any modification, equivalent replacement, improvement and so on, It should be included within the scope of protection of this utility model.

Claims (5)

1. code holes all-in-one machine is cut in a kind of tapping, including fuselage (1), table top (2), crossbeam portion (3), axis chain-drive section (4), high-power Tool changing main shaft (5), cylinder (6), automatic tapping device (7), control box (8), sliding axle (9), fixed block (10), support frame (11), baffle (12), sliding seat (13), sliding rail (14), motor casing (15), three-phase motor (16), bottom plate (17) and backboard (18), It is characterized by: centrally located two sides have been screwed support frame (11), support frame as described above at the top of the fuselage (1) (11) top has been screwed crossbeam portion (3), and two sides have been screwed solid at crossbeam portion (3) one end center Determine block (10), be socketed with sliding axle (9) at fixed block (10) center, is provided with electricity at fixed block (10) top center Casing (15), motor casing (15) bottom has been screwed backboard (18), and backboard (18) is located at sliding axle (9) one Side, described backboard (18) one end are provided with cylinder (6), and backboard (18) bottom end is provided with automatic tapping device (7), and Automatic tapping device (7) is located at cylinder (6) bottom, and backboard (18) bottom center is provided with high-power tool changing main shaft (5), And high-power tool changing main shaft (5) is located at (7) volumes of automatic tapping device, is provided with sliding at fuselage (1) top center Seat (13), the centrally located two sides in sliding seat (13) top are provided with sliding rail (14), in sliding seat (13) top It is provided at the heart table top (2), and is connect at the top of table top (2) bottom and sliding rail (14), is screwed at the top of the table top (2) There are several baffles (12).
2. code holes all-in-one machine is cut in a kind of tapping according to claim 1, it is characterised in that: backboard (18) other end Fixing sleeve is welded at center, and fixing sleeve is socketed on the outside of sliding axle (9).
3. code holes all-in-one machine is cut in a kind of tapping according to claim 1, it is characterised in that: the crossbeam portion (3) is another End has been screwed control box (8), and is socketed with dustproof film on the outside of control box (8).
4. code holes all-in-one machine is cut in a kind of tapping according to claim 1, it is characterised in that: the fuselage (1) and sliding Seat (13) bottom is welded with bottom plate (17), and bottom plate (17) is highly 2cm.
5. code holes all-in-one machine is cut in a kind of tapping according to claim 1, it is characterised in that: described motor casing (15) one end It is welded with U-board, and is connect at the top of U-board bottom and crossbeam portion (3).
CN201920014787.5U 2019-01-05 2019-01-05 A kind of tapping cutting code holes all-in-one machine Expired - Fee Related CN209394103U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201920014787.5U CN209394103U (en) 2019-01-05 2019-01-05 A kind of tapping cutting code holes all-in-one machine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201920014787.5U CN209394103U (en) 2019-01-05 2019-01-05 A kind of tapping cutting code holes all-in-one machine

Publications (1)

Publication Number Publication Date
CN209394103U true CN209394103U (en) 2019-09-17

Family

ID=67897793

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201920014787.5U Expired - Fee Related CN209394103U (en) 2019-01-05 2019-01-05 A kind of tapping cutting code holes all-in-one machine

Country Status (1)

Country Link
CN (1) CN209394103U (en)

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GR01 Patent grant
GR01 Patent grant
CF01 Termination of patent right due to non-payment of annual fee
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20190917

Termination date: 20220105