CN206764319U - Machining center and its saddle - Google Patents
Machining center and its saddle Download PDFInfo
- Publication number
- CN206764319U CN206764319U CN201720588297.7U CN201720588297U CN206764319U CN 206764319 U CN206764319 U CN 206764319U CN 201720588297 U CN201720588297 U CN 201720588297U CN 206764319 U CN206764319 U CN 206764319U
- Authority
- CN
- China
- Prior art keywords
- fuselage
- slide rail
- machining center
- saddle
- supporting table
- 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.)
- Active
Links
Landscapes
- Machine Tool Units (AREA)
Abstract
The utility model discloses a kind of saddle of machining center, including fuselage, slide rail and transition supporting table for supporting extreme, wherein, slide rail is two, two slide rails are arranged in parallel on fuselage, the end of slide rail extends to fuselage outer side, and transition supporting table upper surface is connected with slide rail bottom, and transition supporting table is fixedly connected with fuselage.By being provided with transition supporting table in the end of slide rail, and then strengthen the support strength of extreme, reduce slide rail deflection in use, and then improve the machining accuracy of machining center.The invention also discloses a kind of machining center for including above-mentioned saddle.
Description
Technical field
Part machining technique field is the utility model is related to, more particularly to a kind of saddle of machining center.This practicality is new
Type further relates to a kind of machining center for including above-mentioned saddle.
Background technology
In the minds of work in-process, it is connected with base below saddle, is connected above saddle with workbench, is existed for support works platform
Slided on base, for realizing the functions such as Y-axis movement.
Saddle is one of machining center important feature part, and its architectural characteristic is very big to its performance impact, is mainly reflected in
Machining accuracy, vibration resistance, stock-removing efficiency, service life etc., for saddle as feed drive system, it is to ensure knife rest straight line
The key of motion.Traditional saddle includes fuselage and is arranged on two slide rails being parallel to each other on fuselage, wherein, slide rail both ends are prolonged
Extend fuselage outer side, during work, saddle can move as feed drive system, workbench along slide rail.
However, because slide rail both ends extend to fuselage outer side, it is easily deformed in the slide rail course of work, if slide rail deforms
Afterwards, because workbench is arranged on slide rail so that the machining accuracy of machining center reduces.
Therefore, the machining accuracy of machining center how is improved, is those skilled in the art's technical problem urgently to be resolved hurrily.
Utility model content
The purpose of this utility model is to provide a kind of saddle of machining center, to improve the machining accuracy of machining center.This
The another object of utility model is to provide a kind of machining center for including above-mentioned saddle.
To achieve the above object, the utility model provides a kind of machining center saddle, including fuselage and is arranged on fuselage
Two slide rails being parallel to each other, the end of the slide rail extend to the fuselage outer side, in addition to for supporting the slide rail end
The transition supporting table in portion, the transition supporting table upper surface are connected with the slide rail bottom, the transition supporting table and the machine
Body is fixedly connected.
Preferably, the transition supporting table and the slide rail are formed in one structure.
Preferably, the transition supporting table is transition sloping platform, and the bottom of the transition supporting table offers transition loss of weight
Groove.
Preferably, in addition to the deep floor that is arranged on the inside of the slide rail, it is equipped with reinforcement on the inside of each slide rail
Floor, the deep floor side are connected with the slide rail medial surface, the bottom of the deep floor and the fuselage upper surface
Connection.
Preferably, each slide rail is provided with multiple deep floors, and multiple on each slide rail described add
Strong floor is along the slide rail length direction successively equidistantly distributed, and the deep floor on two slide rails is along the machine
Body center line is symmetrical.
Preferably, the deep floor bottom is provided with floor lightening grooves, and the upper surface of the deep floor is to close to institute
State the inclined-plane that fuselage center direction tilts down.
Preferably, the fuselage is provided with X-axis motor base assembly platform, tail end bearing holder (housing, cover) assembly platform and nut seat and is bearing on
Block platform.
Preferably, the fuselage is n-type hollow structure, is provided with and strengthens between the fuselage roof and the side-of-body
Muscle, and the reinforcement is symmetrically arranged in the fuselage opposite sides.
Preferably, the fuselage roof center is provided with multiple loss of weight circular holes, and the side-of-body is provided with multiple losss of weight
Square hole, multiple loss of weight circular holes and multiple loss of weight square holes are along the slide rail length direction successively equidistantly distributed.
A kind of machining center, including saddle and the workbench on the saddle, the saddle are any of the above-described
Described saddle.
In the above-mentioned technical solutions, machining center saddle provided by the utility model includes fuselage, slide rail and for supporting
The transition supporting table of extreme, wherein, slide rail is two, and two slide rails are arranged in parallel on fuselage, the end of slide rail
Fuselage outer side is extended to, transition supporting table upper surface is connected with slide rail bottom, and transition supporting table is fixedly connected with fuselage.
By foregoing description, in the machining center saddle that the application provides, it was provided with by the end in slide rail
Supporting table is crossed, and then strengthens the support strength of extreme, reduces slide rail deflection in use, and then improve in processing
The machining accuracy of the heart.
Brief description of the drawings
, below will be to embodiment in order to illustrate more clearly of the utility model embodiment or technical scheme of the prior art
Or the required accompanying drawing used is briefly described in description of the prior art, it should be apparent that, drawings in the following description are only
It is embodiment of the present utility model, for those of ordinary skill in the art, on the premise of not paying creative work, also
Other accompanying drawings can be obtained according to the accompanying drawing of offer.
The tomograph for the machining center saddle that Fig. 1 is provided by the utility model embodiment；
The tomograph at another visual angle for the machining center saddle that Fig. 2 is provided by the utility model embodiment；
The upward view for the machining center saddle that Fig. 3 is provided by the utility model embodiment；
Fig. 4 is structural representation of the machining center saddle along A-A directions shown in Fig. 3；
The side view for the machining center saddle that Fig. 5 is provided by the utility model embodiment；
The top view for the machining center saddle that Fig. 6 is provided by the utility model embodiment；
Fig. 7 is the structural representation along B-B directions of machining center saddle shown in Fig. 6；
The end top view for the machining center saddle that Fig. 8 is provided by the utility model embodiment.
In wherein Fig. 1-8：1- transition supporting table, 2-X axle motor bases assembly platform, 3- losss of weight circular hole, 4- slide rails, 5- strengthen
Floor, 6- tail end bearing holder (housing, cover)s assembly platform, 7- losss of weight square hole, 8- reinforcements, 9- lifting hole(eyelet)s platform, 10- floors lightening grooves, 11- spiral shells
Cap seat is bearing on block platform, 12- fuselages.
Embodiment
Core of the present utility model is to provide a kind of saddle of machining center, to improve the machining accuracy of machining center.This
Another core of utility model is to provide a kind of machining center for including above-mentioned saddle.
In order that those skilled in the art more fully understands the technical solution of the utility model, it is below in conjunction with the accompanying drawings and real
Applying mode, the utility model is described in further detail.
Fig. 1 to Fig. 8 is refer to, in a kind of embodiment, in the processing that the utility model specific embodiment provides
Heart saddle includes fuselage 12, slide rail 4 and the transition supporting table 1 for supporting the end of slide rail 4, wherein, slide rail 4 is two, two
Slide rail 4 is arranged in parallel on fuselage 12, and the end of slide rail 4 extends to the outside of fuselage 12, the upper surface of transition supporting table 1 and cunning
The bottom of rail 4 connects, and transition supporting table 1 is fixedly connected with fuselage 12, specifically, it is preferable that as shown in Fig. 2 in transition supporting table 1 and
The side of its upper surface linking is connected with the side that its its upper surface on fuselage 12 is connected.In order to reduce adding for machining center saddle
Work difficulty, it is preferable that transition supporting table 1 and slide rail 4 are formed in one structure.Wherein, it can be rectangle knot that transition supporting table 1 is overall
Structure.It is preferred that each end of slide rail 4 is equipped with transition supporting table 1.In order to improve the performance of machining center saddle, it is preferable that
Fuselage 12 is provided with X-axis motor base assembly platform 2, tail end bearing holder (housing, cover) assembly platform 6 and nut seat and is bearing on block platform 11.Specifically
, there are two X-axis motor base assembly platforms 2 termination of fuselage 12, while the termination of fuselage 12 is provided with two lifting hole(eyelet) platforms 9, certainly, machine
Body 12 can also set a tail end bearing holder (housing, cover) assembly platform 6, and the middle part of fuselage 12 has two nut seats to be bearing on block platform 11.
By foregoing description, in the machining center saddle that the application specific embodiment is provided, by slide rail 4
End be provided with transition supporting table 1, and then strengthen the support strength of the end of slide rail 4, reduce slide rail 4 and deform in use
Amount, and then improve the machining accuracy of machining center.To reduce its elastic deformation amount, machine stress deflection reduces by 20%
Preferably, transition supporting table 1 is transition sloping platform, and the bottom of transition supporting table 1 offers transition lightening grooves.More
Preferably, the thickness of transition sloping platform is equal.By setting transition lightening grooves, while support strength is ensured, mitigate total weight
Amount, reduce materials.
Further, the machining center saddle also includes the deep floor 5 for being arranged on the inner side of slide rail 4, and each inner side of slide rail 4 is
Provided with deep floor 5, specifically, deep floor 5 can be solid construction, the side of deep floor 5 is connected with the medial surface of slide rail 4,
The bottom of deep floor 5 is connected with the upper surface of fuselage 12.By setting deep floor 5, slide rail semi-finals degree is further improved, is reduced
Deformation during the use of slide rail 4, extend the service life of slide rail 4.
Preferably, as shown in figure 1, each slide rail 4 is provided with multiple deep floors 5, multiple ribs on each slide rail 4
Plate 5 is along the length direction of slide rail 4 successively equidistantly distributed, and the deep floor 5 on two slide rails 4 symmetrically divides along the center line of fuselage 12
Cloth, i.e. deep floor 5 on two slide rails 4 are arranged symmetrically.Specifically, the number of deep floor 5 is according to slide rail on each slide rail 4
Depending on 4 length and the size of deep floor 5, the application is not specifically limited.By being set as above, and then improve deep floor 5
Bulk strength, while cause 5 overall stress balance of deep floor.
It is more highly preferred to, the bottom of deep floor 5 is provided with floor lightening grooves 10, and the upper table of deep floor 5 is towards close to fuselage
The inclined-plane that 12 centerline directions tilt down.Specifically, it is preferable that the thickness of deep floor 5 is equal, i.e., floor lightening grooves 10 are oblique
Groove.By setting floor lightening grooves 10, while proof strength, raw material is saved, mitigates overall weight.
On the basis of above-mentioned each scheme, it is preferable that fuselage 12 is n-type hollow structure, the top of fuselage 12 and the sidepiece of fuselage 12
Between be provided with reinforcement 8, and reinforcement 8 is symmetrically arranged in the opposite sides of fuselage 12.By the way that fuselage 12 is arranged into hollow structure,
Further mitigate the overall weight of machining center saddle, and by setting reinforcement 8, ensure the overall support intensity of fuselage 12.
Further, the top center of fuselage 12 is provided with multiple loss of weight circular holes 3, and multiple loss of weight circular holes 3 are along the length side of slide rail 4
To equidistantly distributed successively.It is more highly preferred to, the sidepiece of fuselage 12 is provided with multiple loss of weight square holes 7, and multiple loss of weight square holes 7 are along slide rail 4
The equidistantly distributed of length direction successively, it is preferred that the arrangement square centreline of loss of weight circular hole 3 overlaps with the center line of fuselage 12.
By setting loss of weight circular hole 3, further mitigate the overall weight of machining center saddle, and loss of weight circular hole 3 is set, avoid loss of weight from justifying
The situation that the ambient stress of hole 3 is concentrated, effectively extend the service life of fuselage 12.Further, the side of fuselage 1 is provided with multiple subtract
Double recipe hole 7, for loss of weight square hole 7 along the length direction of slide rail 4 successively equidistantly distributed, fuselage 12 is provided with per side can be with four loss of weight square holes
7。
In order to further reduce the difficulty of processing of machining center saddle, fuselage 12 and reinforcement 8 are formed in one structure, and
Bonding strength is further increased, extends the service life of fuselage 12.Preferably, reinforcement 8 is arranged on floor lightening grooves 10
It is interior.
A kind of machining center that the application provides includes saddle and the workbench on saddle, wherein, saddle is upper
State any saddle.
Each embodiment is described by the way of progressive in this specification, what each embodiment stressed be and other
The difference of embodiment, between each embodiment identical similar portion mutually referring to.
The foregoing description of the disclosed embodiments, professional and technical personnel in the field are enable to realize or new using this practicality
Type.A variety of modifications to these embodiments will be apparent for those skilled in the art, determine herein
The General Principle of justice can be realized in other embodiments in the case where not departing from spirit or scope of the present utility model.Cause
This, the utility model is not intended to be limited to the embodiments shown herein, and is to fit to and principles disclosed herein
The most wide scope consistent with features of novelty.
Claims (10)
1. a kind of machining center saddle, including fuselage (12) and the slide rail (4) that upper two of fuselage (12) is parallel to each other is arranged on, institute
The end for stating slide rail (4) is extended on the outside of the fuselage (12), it is characterised in that also includes being used to support the slide rail (4) to hold
The transition supporting table (1) in portion, transition supporting table (1) upper surface are connected with the slide rail (4) bottom, the transition supporting table
(1) it is fixedly connected with the fuselage (12).
2. machining center saddle according to claim 1, it is characterised in that the transition supporting table (1) and the slide rail
(4) be formed in one structure.
3. machining center saddle according to claim 2, it is characterised in that the transition supporting table (1) is transition sloping platform,
And the bottom of the transition supporting table (1) offers transition lightening grooves.
4. machining center saddle according to claim 1, it is characterised in that also include being arranged on the inside of the slide rail (4)
Deep floor (5), be equipped with deep floor (5) on the inside of each slide rail (4), deep floor (5) side with it is described
Slide rail (4) medial surface is connected, and the bottom of the deep floor (5) is connected with the fuselage (12) upper surface.
5. machining center saddle according to claim 4, it is characterised in that each slide rail (4) is provided with multiple institutes
State deep floor (5), multiple deep floors (5) on each slide rail (4) along the slide rail (4) length direction successively
Equidistantly distributed, and the deep floor (5) on two slide rails (4) is symmetrical along the fuselage (12) center line.
6. machining center saddle according to claim 4, it is characterised in that deep floor (5) bottom is provided with floor
Lightening grooves (10), the upper surface of the deep floor (5) is oblique to being tilted down close to the fuselage (12) centerline direction
Face.
7. machining center saddle according to claim 1, it is characterised in that the fuselage (12) is provided with X-axis motor base
Assembly platform (2), tail end bearing holder (housing, cover) assembly platform (6) and nut seat are bearing on block platform (11).
8. the machining center saddle according to any one of claim 1-7, it is characterised in that the fuselage (12) is n-type
Hollow structure, reinforcement (8), and the reinforcement (8) are provided between fuselage (12) top and the fuselage (12) sidepiece
It is symmetrically arranged in the fuselage (12) opposite sides.
9. machining center saddle according to claim 8, it is characterised in that fuselage (12) top center is provided with
Multiple loss of weight circular holes (3), fuselage (12) sidepiece are provided with multiple loss of weight square holes (7), multiple loss of weight circular holes (3) and multiple
The loss of weight square hole (7) is along the slide rail (4) length direction successively equidistantly distributed.
10. a kind of machining center, including saddle and the workbench on the saddle, it is characterised in that the saddle is
Saddle any one of claim 1-9.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720588297.7U CN206764319U (en) | 2017-05-24 | 2017-05-24 | Machining center and its saddle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720588297.7U CN206764319U (en) | 2017-05-24 | 2017-05-24 | Machining center and its saddle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206764319U true CN206764319U (en) | 2017-12-19 |
Family
ID=60637996
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720588297.7U Active CN206764319U (en) | 2017-05-24 | 2017-05-24 | Machining center and its saddle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206764319U (en) |
-
2017
- 2017-05-24 CN CN201720588297.7U patent/CN206764319U/en active Active
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN100532198C (en) | Assembly for providing flexure to blade system | |
| AU2014234411A1 (en) | Lattice-mast element, lattice-mast jib having at least one such lattice-mast element, and crane having at least one such lattice-mast jib | |
| CN206764319U (en) | Machining center and its saddle | |
| CN207358578U (en) | The workbench of machining center | |
| CN206067405U (en) | A kind of fixing structure for transverse stabilizer bar and QS assembly | |
| CN102491200A (en) | Movable counter weight structure of crawler crane and crane comprising movable counter weight structure | |
| CN106476892A (en) | A kind of longitudinal beam of automobile frame structure | |
| JP2016031016A (en) | Telescopic ladder comprising ladder parts different in specific gravity | |
| CN207255262U (en) | The main tapping of machining center | |
| CN206738414U (en) | A kind of multipurpose outward flange disk | |
| CN206521904U (en) | A kind of wire casing net floor | |
| CN208005167U (en) | The low shake processing machine beam structure of high speed | |
| CN219639220U (en) | Check ring for high-speed drive motor shaft | |
| CN206032997U (en) | Novel girder construction on elevator counterweight frame frame | |
| CN211072589U (en) | Gantry milling machine ball cage cross-shaped stand column | |
| CN213298790U (en) | Novel piston pin of engine | |
| CN209888935U (en) | Stand column for passenger car | |
| CN216097498U (en) | Upright post structure and machining center | |
| CN217381441U (en) | Safety buffer device for construction elevator | |
| CN212613675U (en) | Attached lifting operation safety protection platform guide rail for building construction | |
| CN219009682U (en) | Multifunctional hanging bracket for engineering construction | |
| CN211621949U (en) | Novel assembly type building bottom connecting mechanism | |
| CN205243418U (en) | Structure of elevator pit cat ladder | |
| CN220811635U (en) | Stator hoisting and overturning tool | |
| CN213258893U (en) | Mounting bracket for 3D glass polishing machine |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant |