CN209078260U - A kind of anti-Caton mechanism of horizontal gap-bed lathe guide rail - Google Patents

A kind of anti-Caton mechanism of horizontal gap-bed lathe guide rail Download PDF

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Publication number
CN209078260U
CN209078260U CN201821952763.6U CN201821952763U CN209078260U CN 209078260 U CN209078260 U CN 209078260U CN 201821952763 U CN201821952763 U CN 201821952763U CN 209078260 U CN209078260 U CN 209078260U
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CN
China
Prior art keywords
guide rail
fuselage
reservoir
layer
fixing groove
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Expired - Fee Related
Application number
CN201821952763.6U
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Chinese (zh)
Inventor
姜宇喆
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Guangzhou Yulan Automation Equipment Co Ltd
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Guangzhou Yulan Automation Equipment Co Ltd
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Priority to CN201821952763.6U priority Critical patent/CN209078260U/en
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Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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Abstract

The utility model provides a kind of anti-Caton mechanism of horizontal gap-bed lathe guide rail, this kind of horizontal anti-Caton mechanism of gap-bed lathe guide rail includes round guide, fuselage, reservoir, nesting level, flapper, clean layer, fixing groove, sealing ring, magnet layer;The outer wall of guide rail is nested fuselage, the top insertion of fuselage is provided with reservoir, opening is provided with nesting level at left and right sides of reservoir, insertion is provided with flapper in nesting level, clean layer is closely fitted in the middle part of fuselage, the left and right sides of fuselage is open and is provided with fixing groove, and the equal inner tight of fixing groove is fitted with sealing ring, and the inside of fixing groove is embedded in and is provided with magnet layer.The utility model design is more unreasonable, and knife rest in the process of moving, can effectively clean the dust or iron filings that are attached on guide rail, and knife rest can be lubricated guide rail in moving process by guide rail, enhance flexibility and the practicability of device.

Description

A kind of anti-Caton mechanism of horizontal gap-bed lathe guide rail
Technical field
The present invention relates to field of machining more particularly to a kind of feed devices.
Background technique
Horizontal gap-bed lathe generally by vehicle head part, change gear box part, feeding part, slide carriage part, tailstock portion and divides bed The composition such as body part, and the knife rest of part is fed, for clamping lathe tool and it being made to make longitudinally, laterally to do feeding fortune along guide rail It is dynamic, turnery processing is carried out with workpiece of the lathe tool above vehicle frame to rotation, and lathe tool is cut during processing to workpiece The workpiece debris cut out is splashed sometimes to be sticky on guide rail, and the mobile mechanism of knife rest is caused to generate card in mobile cutting process Or slight vibration, not only affect the working efficiency of lathe, it is also possible to influence the machining accuracy of device.
By patent retrieval, existing Patent No. CN201610956885.1 disclosure of the invention vehicle anti-sticking low and deep load pull Platform, including bracket, two rolling guides and bracket limiting locking device are respectively equipped with channel steel longitudinal direction in longitudinal two sides of bracket Frame.Rolling guide includes U-bar guide rail body and the multiple groups idler wheel that is arranged at intervals on U-bar guide rail body vertical edges lateral surface, slot Steel guide rail body is located at channel steel longitudinal edge outer frame side, and channel steel longitudinal direction frame, which is respectively embedded into, to be supported on corresponding multiple groups idler wheel.Bracket Limiting locking device includes night bolt mechanism and lock handle mechanism, and night bolt mechanism is separately positioned on bracket two sides rear portion And on two rolling guide rear portions, lock handle mechanism is separately positioned on the front end and the corresponding preceding limit of bracket of two rolling guides On the position of position.For the present invention using save trouble and labor and safe and reliable, structure is simple, manufacturing cost is low, can bear heavy duty and movement gently Just, bracket can be effectively prevented and occurs catching phenomenon in moving process, clamping stagnation will not occur.
Based on foregoing description, and equipment in the prior art is combined to find, existing knife rest when being moved by guide rail, Mobile mechanism's design of knife rest is simultaneously unreasonable, knife rest can not be made to pass through guide rail in the process of moving, to the dust on guide rail Perhaps iron filings, which are cleaned, causes knife rest that can generate Caton or shake in moving process, and knife rest is for a long time in guide rail Middle movement needs to smear some lubricating oil and is lubricated to guide rail surface, reduces the friction between knife rest and guide rail, otherwise vehicle frame Frictional force between guide rail can be excessive, to reduce the working efficiency of device, reduces the service life of vehicle frame, therefore the design It is directed to the above problem, a structurally reasonable, and functional good feed device is designed, to improve practicability.
Summary of the invention
The purpose of the present invention is to provide a kind of horizontal anti-Caton mechanisms of gap-bed lathe guide rail, are passing through guide rail to solve frame When mobile, mobile mechanism's design of knife rest is simultaneously unreasonable, and knife rest passes through guide rail in the process of moving, can not be to the ash on guide rail Dirt or iron filings are cleaned, and the problem of can not be lubricated to guide rail.
The purpose and effect of the horizontal anti-Caton mechanism of gap-bed lathe guide rail of the present invention, are reached by technological means in detail below At:
A kind of anti-Caton mechanism of horizontal gap-bed lathe guide rail, this kind of horizontal anti-Caton mechanism of gap-bed lathe guide rail include that circle is led Rail, fuselage, reservoir, nesting level, flapper, clean layer, fixing groove, sealing ring, magnet layer;The outer wall of the guide rail is nested It is provided with fuselage, the top insertion of the fuselage is provided with reservoir, and opening is provided with nesting at left and right sides of the reservoir Layer, insertion is provided with flapper in the nesting level, clean layer is closely fitted in the middle part of the fuselage, the fuselage The left and right sides is open and is provided with fixing groove, and the equal inner tight of the fixing groove is fitted with sealing ring, the fixing groove it is interior Portion is embedded in and is provided with magnet layer.
Further, the inner tight of the sealing ring has several small " protrusions ", and sealing ring is magnetic rubber Glue sealing ring.
Further, the magnet layer is hollow " cylinder " shape, and the magnet layer mutually agrees with fixing groove, and magnet layer Length it is longer than the length that clean layer extends fuselage right lateral surface, and magnet layer is detachably replaced.
Further, the inner wall of the clean layer is fitted closely with fuselage, between the outer wall and magnet layer of the clean layer It fits closely, the clean layer is superfine fibre cleaning cloth clean layer, and the inside of clean layer is in hollow " honeycomb " shape.
Further, the top opening of the reservoir is provided with oil filler point, the nesting level and active catch of the reservoir Mutually agree between plate, and reservoir is located at the center position on guide rail top.
Further, the bottom end opening of the reservoir is provided with the oil groove that of " circular arc " shape, and oil groove and guide rail phase out Agree with.
In comparison with existing structure, the invention has the following beneficial effects:
By being equipped with magnet layer and clean layer, magnet layer is hollow " cylinder " shape, and magnet layer mutually agrees with fixing groove, and The inner wall of clean layer is fitted closely with fuselage, is fitted closely between the outer wall and magnet layer of clean layer, so that fuselage is led by circle In the process of moving, magnet layer can in advance be adsorbed iron filings on round guide rail, and the clean layer on the inside of it can lead circle later Track surface wipes and cleans, and the clast of the appearance of round guide is removed, and is equipped with reservoir, and the top opening of reservoir is provided with Oil filler point, the bottom end opening of reservoir is provided with the oil groove that of " circular arc " shape, and reservoir is located at the center position on guide rail top It sets, so that lubricating oil can be previously stored in the left and right two for oil groove and round guide of " circular arc " shape due to gravity in reservoir End, lubricating oil can successively slide along round guide left and right ends later, so that lubricating oil is uniformly applied to round guide outer wall, simultaneously Parts of lubricating oil can also infiltrate into clean layer, so that clean layer is when moving, can be lubricated to round guide outer wall, so as to Reduce the friction between knife rest and guide rail.
Detailed description of the invention
Fig. 1 is the whole positive structure schematic of the present invention;
Fig. 2 is airframe structure partial schematic diagram of the present invention;
Fig. 3 is partial cutaway schematic on the right side of airframe structure of the present invention;
Fig. 4 is enlarged structure schematic diagram at Fig. 3 A of the present invention;
Fig. 5 is airframe structure right side schematic view of the present invention;
Fig. 6 is local overlooking schematic diagram on the right side of fixed slot configurations of the present invention;
In figure, the corresponding relationship of component names and accompanying drawing number are as follows:
1- round guide, 2- fuselage, 201- reservoir, 202- nesting level, 203- flapper, 204- clean layer, 205- are solid Determine slot, 206- sealing ring, 3- magnet layer.
Specific embodiment
In the description of the present invention, unless otherwise indicated, the meaning of " plurality " is two or more;Term " on ", The orientation or positional relationship of the instructions such as "lower", "left", "right", "inner", "outside", " front end ", " rear end ", " head ", " tail portion " is It is based on the orientation or positional relationship shown in the drawings, is merely for convenience of description of the present invention and simplification of the description, rather than instruction or dark Show that signified device or element must have a particular orientation, be constructed and operated in a specific orientation, therefore should not be understood as pair Limitation of the invention.In addition, term " first ", " second ", " third " etc. are used for description purposes only, and should not be understood as instruction or Imply relative importance.
In the description of the present invention, it should be noted that unless otherwise clearly defined and limited, term " connected " " connects Connect " it shall be understood in a broad sense, for example, it may be being fixedly connected, it may be a detachable connection, or be integrally connected;It can be machine Tool connection, is also possible to be electrically connected;It can be directly connected, it can also be indirectly connected through an intermediary.For this field For those of ordinary skill, the concrete meaning of above-mentioned term in the present invention can be understood with concrete condition.
Embodiment:
As shown in attached drawing 1 to attached drawing 6:
The present invention provides a kind of anti-Caton mechanism of horizontal gap-bed lathe guide rail: this kind of horizontal anti-Caton machine of gap-bed lathe guide rail Structure includes round guide 1, fuselage 2, reservoir 201, nesting level 202, flapper 203, clean layer 204, fixing groove 205, sealing Enclose 206, magnet layer 3;The outer wall of the guide rail 1 is nested fuselage 2, and the top insertion of the fuselage 2 is provided with reservoir 201,201 left and right sides of reservoir opening is provided with nesting level 202, and insertion is provided with work in the nesting level 202 Dynamic baffle 203, the middle part of the fuselage 2 are closely fitted with clean layer 204, and the left and right sides of the fuselage 2, which is open, to be provided with Fixing groove 205, the equal inner tight of the fixing groove 205 are fitted with sealing ring 206, and the inside of the fixing groove 205 is embedded in It is provided with magnet layer 3.
Wherein, the inner tight of the sealing ring 206 has several small " protrusions ", and sealing ring 206 is magnetic Rubber seal 206, when so that magnet layer 3 being embedded in fixing groove 205, magnet layer 3 is close in several small " protrusions " compression, Sealing ring 206 generates magnetic force and is close to magnet layer 3 simultaneously, increases the active force between magnet layer 3, prevents magnet layer 3 in machine It falls off in 2 moving process of body.
Wherein, the magnet layer 3 is hollow " cylinder " shape, and the magnet layer 3 agrees with 205 phase of fixing groove, and magnet The length of layer 3 is longer than the length that clean layer 204 extends 2 right lateral surface of fuselage, and magnet layer 3 is detachably replaced, so that machine In the process of moving by round guide 1, magnet layer 3 can generate magnetic force to body 2, in advance be adsorbed iron filings on round guide 1.
Wherein, the inner wall of the clean layer 204 is fitted closely with fuselage 2, the outer wall and magnet layer 3 of the clean layer 204 Between fit closely, the clean layer 204 is superfine fibre cleaning cloth clean layer 204, and the inside of clean layer 204 is in hollow " honeycomb " shape so that fuselage 2 by round guide 1 in the process of moving, clean layer 204 can wipe 1 surface of round guide It wipes, the clast of the appearance of round guide 1 is removed, while lubricating oil is from reservoir 201 when falling, during lubricating oil can penetrate into In the clean layer 204 of empty " honeycomb " shape, so that clean layer 204 is in the process of moving, lubricating oil can be uniformly applied to circle The outer wall of guide rail 1.
Wherein, the top opening of the reservoir 201 is provided with oil filler point, the nesting level 202 of the reservoir 201 and work Mutually agree between dynamic baffle 203, and reservoir 201 is located at the center position on 1 top of guide rail, so that moistening in reservoir 201 Lubricating oil can fall the top in round guide 1 due to gravity, lubricating oil meeting later again due to gravity, along 1 outer wall of round guide according to Secondary landing is lubricated 1 outer wall of round guide, so as to reduce the friction between knife rest and guide rail.
Wherein, the bottom end opening of reservoir 201 is provided with the oil groove out of " circular arc " shape, and oil groove mutually agrees with guide rail out, So that lubricating oil when being fallen from reservoir 201, can be previously stored in " circular arc " shape go out between oil groove and round guide 1 so that Lubricating oil can successively slide along 1 left and right ends of round guide, so that lubricating oil is uniformly applied to 1 outer wall of round guide, to round guide 1 Outer wall is lubricated, so as to reduce the friction between knife rest and round guide 1
The specifically used mode and effect of the present embodiment:
In the present invention, suitable lubricating oil is injected into reservoir 201 first, knife rest is when starting to work, by active catch Plate 203 is extracted from nesting level 202, and lubricating oil can fall the top in round guide 1, Zhi Hourun due to gravity in reservoir 201 Lubricating oil meeting successively slides again due to gravity along the left and right ends of round guide outer wall, and at this moment some lubricating oil can infiltrate into clearly In clean layer 204, when fuselage 2 moves in round guide 1, magnet layer 3 generates magnetic force, is in advance siphoned away iron filings on round guide 1, The clean layer 204 on the inside of it can wipe and clean 1 surface of round guide later, and the clast of the appearance of round guide 1 is removed, and Lubricating oil is uniformly applied to 1 surface of round guide simultaneously, 1 outer wall of round guide is lubricated, can be reduced between knife rest and guide rail 2 Friction.
In conclusion although the present invention is described in detail referring to the foregoing embodiments, for the technology of this field For personnel, it is still possible to modify the technical solutions described in the foregoing embodiments, or to part of technology Feature is equivalently replaced, all within the spirits and principles of the present invention, any modification, equivalent replacement, improvement and so on, and It should be included within protection scope of the present invention.

Claims (6)

1. a kind of anti-Caton mechanism of horizontal gap-bed lathe guide rail, it is characterised in that: this kind of horizontal anti-Caton machine of gap-bed lathe guide rail Structure includes round guide (1), fuselage (2), reservoir (201), nesting level (202), flapper (203), clean layer (204), consolidates Determine slot (205), sealing ring (206), magnet layer (3);The outer wall of the guide rail (1) is nested fuselage (2), the fuselage (2) top insertion is provided with reservoir (201), and opening is provided with nesting level at left and right sides of the reservoir (201) (202), insertion is provided with flapper (203) in the nesting level (202), is closely fitted in the middle part of the fuselage (2) Clean layer (204), the left and right sides of the fuselage (2), which is open, to be provided with fixing groove (205), the fixing groove (205) it is equal Inner tight is fitted with sealing ring (206), and the inside of the fixing groove (205), which is embedded in, is provided with magnet layer (3).
2. the anti-Caton mechanism of horizontal gap-bed lathe guide rail according to claim 1, it is characterised in that: the sealing ring (206) inner tight has several small " protrusions ", and sealing ring (206) is magnetic rubber seal (206).
3. the anti-Caton mechanism of horizontal gap-bed lathe guide rail according to claim 1, it is characterised in that: the magnet layer (3) For hollow " cylinder " shape, the magnet layer (3) is mutually agreed with fixing groove (205), and the length of magnet layer (3) compares clean layer (204) length for extending fuselage (2) right lateral surface will be grown, and magnet layer (3) is detachably replaced.
4. the anti-Caton mechanism of horizontal gap-bed lathe guide rail according to claim 1, it is characterised in that: the clean layer (204) inner wall is fitted closely with fuselage (2), is fitted closely between the outer wall and magnet layer (3) of the clean layer (204), institute Stating clean layer (204) is superfine fibre cleaning cloth clean layer (204), and the inside of clean layer (204) is in hollow " honeycomb " Shape.
5. the anti-Caton mechanism of horizontal gap-bed lathe guide rail according to claim 1, it is characterised in that: the reservoir (201) top opening is provided with oil filler point, phase between the nesting level (202) and flapper (203) of the reservoir (201) Agree with, and reservoir (201) is located at the center position on guide rail (1) top.
6. the anti-Caton mechanism of horizontal gap-bed lathe guide rail according to claim 1, it is characterised in that: the reservoir (201) bottom end opening is provided with the oil groove out of " circular arc " shape, and oil groove mutually agrees with guide rail out.
CN201821952763.6U 2018-11-26 2018-11-26 A kind of anti-Caton mechanism of horizontal gap-bed lathe guide rail Expired - Fee Related CN209078260U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201821952763.6U CN209078260U (en) 2018-11-26 2018-11-26 A kind of anti-Caton mechanism of horizontal gap-bed lathe guide rail

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201821952763.6U CN209078260U (en) 2018-11-26 2018-11-26 A kind of anti-Caton mechanism of horizontal gap-bed lathe guide rail

Publications (1)

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CN209078260U true CN209078260U (en) 2019-07-09

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109202470A (en) * 2018-11-26 2019-01-15 姜宇喆 A kind of anti-Caton mechanism of horizontal gap-bed lathe guide rail

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109202470A (en) * 2018-11-26 2019-01-15 姜宇喆 A kind of anti-Caton mechanism of horizontal gap-bed lathe guide rail
CN109202470B (en) * 2018-11-26 2024-02-06 杭州追猎科技有限公司 Anti-blocking mechanism for guide rail of horizontal saddle lathe

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Granted publication date: 20190709