CN209288413U - A kind of section steel cutting equipment - Google Patents
A kind of section steel cutting equipment Download PDFInfo
- Publication number
- CN209288413U CN209288413U CN201821810712.XU CN201821810712U CN209288413U CN 209288413 U CN209288413 U CN 209288413U CN 201821810712 U CN201821810712 U CN 201821810712U CN 209288413 U CN209288413 U CN 209288413U
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- CN
- China
- Prior art keywords
- motor
- fuselage
- transverse
- section steel
- cutting equipment
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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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Abstract
The utility model relates to a kind of section steel cutting equipment, including fuselage, cutting mechanism, transverse-moving mechanism, the fuselage interior is cavity, the transverse-moving mechanism is arranged in fuselage, the cutting mechanism is arranged on transverse-moving mechanism, the cutting mechanism includes first motor, second motor and diagonal brace, first motor and the second motor all pass through diagonal brace and are fixedly mounted on transverse-moving mechanism with being staggered front to back, the output shaft of the first motor and the second motor is all equipped with saw blade, the saw blade of the saw blade of the first motor and second motor is in 45 °~135 ° of angle, the fuselage top surface is equipped with operating platform, the operating platform is equipped with the opening of blades machining, hold-down mechanism is additionally provided on the operating platform.The utility model installs two motors in fuselage and multiple locating slots can cut more different profiles simultaneously, and time processing goes out respective one end of two profiles, saves manpower.
Description
Technical field
The utility model relates to a kind of section steel cutting equipment, belong to cutting equipment field.
Background technique
Shape product has obtained hair at full speed in China in recent years due to huge market demand and vast potential for future development
Exhibition, profile are had using more: window frame, balustrade, cabling channel, washboard, shape tube, furniture, the accessories such as building materials.
Profile needs to use cutting equipment during processing, in process, is generally cut into profiled ends
Oblique angle is in order to splice, and existing cutting machine can only once cut single sectional, and whole process needs manual operation, not only
It is time-consuming, and inefficiency.It is therefore necessary to research and develop the new cutting equipment of one kind to avoid these problems.
Summary of the invention
(1) technical problems to be solved
In order to solve the above problem of the prior art, the utility model provides a kind of cleavable more profiles of time processing
Cutting equipment.
(2) technical solution
In order to achieve the above object, the main technical schemes that the utility model uses include: a kind of section steel cutting equipment, packet
Fuselage, cutting mechanism, transverse-moving mechanism are included, the fuselage interior is cavity, and the transverse-moving mechanism is arranged in fuselage, the cutting
Mechanism is arranged on transverse-moving mechanism, and the cutting mechanism includes first motor, the second motor and diagonal brace, first motor and the second electricity
Machine all passes through diagonal brace and is fixedly mounted on transverse-moving mechanism with being staggered front to back, and the output shaft of the first motor and the second motor is all set
There is a saw blade, the saw blade of the saw blade of the first motor and second motor is in 45 °~135 ° of angle, and the fuselage top surface is set
There is operating platform, the operating platform is equipped with the opening of blades machining, is additionally provided with hold-down mechanism on the operating platform.
Further, the transverse-moving mechanism includes two guide rails, support plate and transverse cylinder, and two guide rail is separately positioned on
The left and right sides of fuselage interior, the support plate are arranged on the sliding block on two guide rails, the transverse cylinder cylinder head and support plate
Lower section is connected.
Further, the saw blade of the saw blade of the first motor and second motor is in 90 ° of angles, the first motor
Horizontal by 135 ° of angles, second motor is horizontal by 45 ° of angles.
Further, its two sides that are open of the operating platform are equipped with multiple positioning mechanisms.
Further, the positioning mechanism includes multiple locating pieces, is formed between two neighboring locating piece for processing
The locating slot of part positioning.
Further, the hold-down mechanism includes bracket, and the cradle top surface two sides are respectively provided with compression cylinder, the compression
The piston rod of cylinder runs through cradle top surface, and piston-rod lower end is equipped with lower platen, multiple briquettings are equipped with below lower platen.
Further, the bracket is surrounded by baffle.
Further, the fuselage two sides are respectively equipped with cradle.
Further, a locator is additionally provided on the cradle on the left of the fuselage.
It further, further include a recovering mechanism, the recovering mechanism is accumulator tank, and the accumulator tank is arranged in fuselage
The internal and underface between two saw blades.
(3) beneficial effect
The beneficial effects of the utility model are:
1, the utility model two motors are installed in fuselage and multiple locating slots can cut simultaneously more it is different
Profile, and time processing goes out respective one end of two profiles, saves manpower.
2, the cradle of fuselage two sides setting holds and conveys profile convenient for staff.
3, the cradle in left side is equipped with locator and graduated scale, and staff is facilitated to be cut into required length.
4, the underface setting recyclable device between two saw blades can recycle waste material in time.
5, the surrounding of bracket is additionally provided with baffle, can prevent powder from splashing.
Detailed description of the invention
Fig. 1 faces angled arrangement schematic diagram for the utility model；
Fig. 2 is the upper right view stereo figure of the utility model；
Fig. 3 is the upper left view stereo figure of the utility model；
Fig. 4 is the fuselage interior structural schematic diagram of the utility model；
Fig. 5 is the structural schematic diagram of the utility model another kind embodiment.
[description of symbols]
1: fuselage；
101: operating platform；
2: cutting mechanism
201: first motor；
202: the second motors；
203: diagonal brace；
3: transverse-moving mechanism；
301: guide rail；
302: support plate；
303: transverse cylinder；
4: positioning mechanism；
401: locating piece；
5: hold-down mechanism；
501: compression cylinder；
502: lower platen；
503: briquetting；
504: bracket；
505: baffle；
6: cradle；
7: locator；
8: accumulator tank.
Specific embodiment
It is with reference to the accompanying drawing, right by specific embodiment in order to understand in order to preferably explain the utility model
The utility model is described in detail.
The direction being previously mentioned of the utility model is only to facilitate illustrate, and be not limited to a position or a kind of sky
Between move towards.
Complete equipment is controlled by power control cabinet.Cutting equipment main structure includes fuselage 1, is cavity, fuselage 1 inside fuselage 1
The interior transverse-moving mechanism 3 that the back-and-forth motion of cutting mechanism 2 is driven equipped with cutting mechanism 2 and one.Transverse-moving mechanism 3 by two guide rails 301,
Support plate 302 and transverse cylinder 303 are constituted, and two guide rails 301 are respectively and fixedly installed to the left and right sides inside fuselage 1, support plate
302 are fixed on the sliding block on guide rail 301, and 303 cylinder head of transverse cylinder and the lower section of support plate 302 are connected to a fixed, as whole
The power resources of a device.
Cutting mechanism 2 includes two motors, and two motors are one in front and one in back alternately mounted on support plate by diagonal brace 203
On 302, saw blade is equipped on the output shaft of each motor.In actual production process, some profile ends will be cut into oblique angle, thus
The saw blade of motor will be arranged by certain angle tilt for we, and shape is in 45~135 ° of angles between two saw blades.Preferably, we
The setting of 90 ° of angles is selected, its saw blade of first motor 201 being located behind is arranged horizontal by 135 °, positioned at the of front
Two its saw blade of motor 202 are arranged horizontal by 45 °.The purpose for being fixed motor using diagonal brace 203 herein is just to be able to
Saw blade and horizontal plane is allowed to form required angle.
The surrounding of fuselage 1 offers door, and top surface is operating platform 101, and operating platform 101 is equipped with a rectangular aperture,
It is contacted convenient for stretching out opening at the top of saw blade with profile.The opening left and right sides is equipped with multiple locating pieces 401, two adjacent positioning
The locating slot for workpiece positioning is formed between block 401.The width between locating piece 401 can be adjusted according to required size
Degree, while cutting the profile of more different sizes.
Hold-down mechanism 5 is also equipped on operating platform 101,5 main structure of hold-down mechanism includes bracket 504, bracket 504
Right end is feed end, and the left end of bracket 504 is discharge end.Compression cylinder 501 is all housed at left and right sides of 504 top surface of bracket, is compressed
The piston rod of cylinder 501 runs through 504 top surface of bracket, and piston-rod lower end is equipped with lower platen 502, the lower section installation of lower platen 502
There are multiple briquettings 503,503 width of briquetting is less than positioning groove width, so that locating slot can accommodate briquetting 502.
For the ease of holding and conveying profile, the left and right sides of fuselage 1 is all connected with cradle 6.In actual mechanical process,
It needs to cut profile by specific length, for this purpose, being additionally provided with a locator 7, cradle 6 on the cradle 6 in left side
Whippletree on be additionally provided with graduated scale to cooperate locator 7, the position of locator 7 is preset by required length, will be to be cut
Profile one end is withstood, then is cut.
During cutting, a bit of waste material can be generated between two saw blades, in order to collect this waste material, fuselage interior is also
Equipped with an accumulator tank 8.The following location directly between two saw blades of accumulator tank 8, the waste material for cutting generation, which can take advantage of a situation, to be fallen into back
It receives slot 8 to be directly collected, avoiding the waste material generated from blocking saw blade influences the operation of whole equipment.
As shown in figure 5, the quantity of the compression cylinder 501 of hold-down mechanism 5 can also be two or more, reinforce the same of lower pressure
When be also possible to prevent to one end tilt., can be with many powders in cutting process, these powders are not easy to be collected, in order to keep away
Exempt from powder splashing, baffle 505 can be added in the surrounding of bracket.
The course of work of cutting equipment: firstly, preset locator 7 by required length, then by many types of material to be cut
It is individually placed in each locating slot, and the left end of profile is resisted into locator 7 and is fixed, then the switch of starting device.
The piston rod of compression cylinder 501 moves down until briquetting 503 touches profile to be cut, and compression cylinder 501 is downwardly applied to
Pressure briquetting 503 resist profile to be fixed.Then, the transverse cylinder 303 on transverse-moving mechanism 3 starts to start,
Motor positioned at 1 interior forward end of fuselage gradually moves backward under the drive of transverse-moving mechanism 3, and first motor 201 takes the lead in touching
Profile and successively profile is cut, feed end of 201 cut place of first motor close to right side.Then again by the second motor
202 cut profile, the cut place of the second motor 202 close to left side discharge end, can time processing go out two profiles
Respective one end.After two motors are sequentially completed cutting, a bit of waste material can be generated between two saw blades, this bit of waste material
It can take advantage of a situation and fall into accumulator tank 8 by centralized collection.Finally, transverse-moving mechanism 3 is moved to 1 interior forward end of fuselage, work next time is waited
Make.One cutting process is completed.
Claims (10)
1. a kind of section steel cutting equipment, it is characterised in that: including fuselage (1), cutting mechanism (2), transverse-moving mechanism (3), the machine
It is cavity inside body (1), in fuselage (1), the cutting mechanism (2) is arranged in transverse-moving mechanism for transverse-moving mechanism (3) setting
(3) on, the cutting mechanism (2) includes first motor (201), the second motor (202) and diagonal brace (203), first motor (201)
It is all fixedly mounted on being staggered front to back on transverse-moving mechanism (3) by diagonal brace (203) with the second motor (202), the first motor
(201) and the output shaft of the second motor (202) is all equipped with saw blade, the saw blade and second motor of the first motor (201)
(202) saw blade is in 45 °~135 ° of angle, and fuselage (1) top surface is equipped with operating platform (101), the operating platform
(101) it is equipped with the opening of blades machining, is additionally provided with hold-down mechanism (5) on the operating platform (101).
2. a kind of section steel cutting equipment as described in claim 1, it is characterised in that: the transverse-moving mechanism (3) includes two guide rails
(301), support plate (302) and transverse cylinder (303), two guide rail (301) are separately positioned on the internal left and right two of fuselage (1)
Side, the support plate (302) are arranged on the sliding block on two guide rails (301), transverse cylinder (303) cylinder head and support plate
(302) lower section is connected.
3. a kind of section steel cutting equipment as described in claim 1, it is characterised in that: the saw blade of the first motor (201) with
The saw blade of second motor (202) is in 90 ° of angles, and the first motor (201) is horizontal by 135 ° of angles, and described second
Motor (202) is horizontal by 45 ° of angles.
4. a kind of section steel cutting equipment as described in claim 1, it is characterised in that: its opening two of the operating platform (101)
Side is equipped with multiple positioning mechanisms (4).
5. a kind of section steel cutting equipment as claimed in claim 4, it is characterised in that: the positioning mechanism (4) includes multiple fixed
Position block (401) forms the locating slot for workpiece positioning between two neighboring locating piece (401).
6. a kind of section steel cutting equipment as described in claim 1, it is characterised in that: the hold-down mechanism (5) includes bracket
(504), bracket (504) the top surface two sides are respectively provided with compression cylinder (501), and the piston rod of the compression cylinder (501) runs through
Bracket (504) top surface, piston-rod lower end are equipped with lower platen (502), and lower platen is equipped with multiple briquettings below (502)
(503)。
7. a kind of section steel cutting equipment as claimed in claim 6, it is characterised in that: the bracket (504) is surrounded by gear
Plate (505).
8. a kind of section steel cutting equipment as described in claim 1, it is characterised in that: fuselage (1) two sides, which are respectively equipped with, to be sent
Expect frame (6).
9. a kind of section steel cutting equipment as claimed in claim 8, it is characterised in that: the cradle (6) on the left of the fuselage (1)
On be additionally provided with a locator (7).
10. a kind of section steel cutting equipment as claim in any one of claims 1 to 9, it is characterised in that: further include one
Recovering mechanism (8), the recovering mechanism (8) are accumulator tank, accumulator tank setting it is internal in fuselage (1) and be located at two saw blades it
Between underface.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821810712.XU CN209288413U (en) | 2018-11-05 | 2018-11-05 | A kind of section steel cutting equipment |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821810712.XU CN209288413U (en) | 2018-11-05 | 2018-11-05 | A kind of section steel cutting equipment |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN209288413U true CN209288413U (en) | 2019-08-23 |
Family
ID=67647808
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201821810712.XU Expired - Fee Related CN209288413U (en) | 2018-11-05 | 2018-11-05 | A kind of section steel cutting equipment |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN209288413U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109262060A (en) * | 2018-11-05 | 2019-01-25 | 倪华亭 | A kind of section steel cutting equipment |
-
2018
- 2018-11-05 CN CN201821810712.XU patent/CN209288413U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109262060A (en) * | 2018-11-05 | 2019-01-25 | 倪华亭 | A kind of section steel cutting equipment |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20190823 Termination date: 20201105 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |