Track for drawing assembly and method to remove the relative gripping elements

Information

  • Patent Grant
  • 6644467
  • Patent Number
    6,644,467
  • Date Filed
    Friday, February 22, 2002
    23 years ago
  • Date Issued
    Tuesday, November 11, 2003
    21 years ago
Abstract
Track for drawing assembly and method to replace the gripping elements associated with said tracks, wherein the track comprises a plurality of links able to support at least part of at least one gripping element of a product to be drawn, each of the gripping elements being able to be selectively clamped in a housing seating by means of rapid attachment/detachment means, said rapid attachment/detachment means comprising at least a clamping element axially movable along an axis substantially orthogonal to the plane on which said gripping element lies, and an activation element axially movable and able to displace said clamping element from a first clamping position to a second position wherein said gripping element is released.
Description




FIELD OF THE INVENTION




This invention concerns a track for drawing assemblies, used preferentially on drawing machines for metal products, such as bars or tubes, the drawing machines comprising two opposite and counter-rotating tracks suitable to achieve the axial drawing of said metal products.




The invention also concerns the connected method to remove and to replace the gripping elements associated with said tracks.




In the following description, to simplify the explanation, the metal products will be referred to under the general term of “bars”, irrespective of the section thereof (round, square, polygonal, etc.) and of the fact that they are hollow or solid.




BACKGROUND OF THE INVENTION




The state of the art includes drawing machines for metal bars in which the drawing assembly comprises two tracks counter-rotating and opposite each other with respect to the drawing axis, each one consisting of a plurality of links on which pads are mounted to grip the bar to be drawn.




Each gripping pad has a hollow shaped to mate with the section of the bar in its already drawn segment. The two tracks are made to rotate continuously and, in co-operation with relative rigid guides, are suitable to clamp and draw the bar to achieve the drawing process.




The gripping pads can be removed from the respective links, so that they can be removed in the event of wear or if the section of the bar is changed.




The state of the art includes gripping pads which have two faces, a front and a rear face, inclined and suitable to cooperate with the walls of mating “dove-tailed” seatings made on the links of the track. The gripping pads are mounted by inserting them inside the relative “dove-tailed” seatings and they are subsequently clamped by means of rapid attachment/detachment means provided for this purpose and associated with the links of the track.




Generally speaking, the rapid attachment/detachment means consist of a pair of lateral clamps, associated with relative elastic means, suitable to clamp the sides of the gripping pads and prevent them from coming off.




In a condition of association with the links of the track, the gripping pads are therefore stably constrained inside the relative seating; they cannot be removed sideways due to the lateral clamps, nor lengthways because their faces and the inclined surfaces of the “dove-tailed” seating are coupled together through interference.




The gripping pads are released from the relative links by compressing the elastic means of the lateral clamps which in this way are released from the sides of the pads, and thus allow them to be extracted.




The arrangement of the lateral clamps and the reduced space available in proximity thereof means that the release operation is carried out manually, for the most part, possibly with the aid of appropriate tools.




This is necessary also to mount and clamp new gripping pads, making it practically impossible to automate the operations to replace the pads which are therefore very long and laborious, and entail a prolonged interruption of the production cycle and an increase in the overall costs of drawing.




The present Applicant has devised and embodied this invention to overcome these shortcomings and to obtain further advantages.




SUMMARY OF THE INVENTION




The invention is set forth and characterized in the respective main claims, while the dependent claims describe other characteristics of the invention.




The purpose of the invention is to achieve a track for the drawing assembly in drawing machines including rapid attachment/detachment means suitable to allow the operations to replace the gripping pads to be carried out quickly and easily, at the same time ensuring that the pads are stably and safely clamped to the relative links.




Another purpose of the invention is to allow the operations to replace the gripping pads of the tracks to be automated, so as to reduce to a minimum both the time taken to carry out these operations and also the manpower required.




In the track according to the invention each link comprises rapid attachment/detachment means suitable to selectively clamp the relative gripping pad in correspondence with a specific housing seating.




According to the invention, the rapid attachment/detachment means comprise a clamping element, arranged substantially orthogonal to the plane on which the track and the relative pad lie, and an activation element, or thruster element, arranged substantially transverse to said clamping element, and therefore substantially parallel to the plane on which the track lies, and cooperating therewith in constraining the pad.




The clamping element is constrained to the relative link so as to be able to move only in an axial direction.




In one embodiment of the invention, the clamping element has at least a segment comprising a cam profile, cooperating with a mating cam profile made on at least a segment of the thruster element.




In a first embodiment, the cam profiles consist respectively of a spherical or semi-spherical element solid with the clamping element and by a mating curved or semi-spherical portion of the surface made on the thruster element. According to another embodiment, the cam profiles consist of mating inclined planes.




The thruster element is arranged in a lateral position on the relative link, accessible laterally with respect thereto and is also axially movable, transversely to the axis of the clamping element, at least from a first retracted position to a second advanced position.




The axial movement of the thruster element, in a direction substantially parallel to the plane on which the track and pad lie, causes its cam profile to slide on the corresponding cam profile of the clamping element, in such a manner as to define the clamped/unclamped conditions of the gripping pad to/from the relative track.




To be more exact, with the thruster element in a first position, the clamping element partially emerges from the relative link, and inserts itself into a mating positioning and constraining seating made on the gripping pad, and causes the latter to be clamped.




The movement of the thruster element into a second position, on the contrary, causes the clamping element to be axially displaced and therefore released from said positioning and constraining seating, and then to be retracted to a position of non-interference with the gripping pad; in this condition, the gripping pad is released and therefore can be removed from the relative track.




By the axial movement alone of the thruster element, the invention therefore allows to clamp/unclamp each gripping pad, allowing the operations to replace the pads to be carried out easily and rapidly.




The arrangement and lateral accessibility of the thruster element on the relative link also allows to install, in a position of non-interference with the drawing assembly and with the two relative tracks opposite each other, an automatic drive device for the thruster element, and possibly automatic pick-up and positioning means for the assembly/dis-assembly of the gripping pads onto/from the tracks of the drawing assembly. This allows to accelerate the operations to replace the gripping pads and therefore to reduce the time that the production cycle of the drawing machine is interrupted.











BRIEF DESCRIPTION OF THE DRAWINGS




These and other characteristics of the invention will become clear from the following description of some preferential forms of embodiment, given as non-restrictive examples, with reference to the attached drawings wherein:





FIG. 1

is a part side view of a drawing assembly provided with tracks according to the invention;





FIG. 2



a


shows the transverse section from A to A of

FIG. 1

of a track in one embodiment of the invention with the gripping pad in the clamped condition;





FIG. 2



b


is a partly sectioned view from above of a detail from

FIG. 2



a;







FIG. 3



a


shows the track from

FIG. 2



a


with the gripping pad in the released condition;





FIG. 3



b


is a partly sectioned view from above of a detail from

FIG. 3



a;







FIGS. 4



a


and


4




b


show another embodiment of the invention respectively in the clamped and unclamped position.











DETAILED DESCRIPTION OF PREFERRED EMBODIMENTS




With reference to the attached Figures, two tracks


10


according to the invention are part of a drawing assembly


11


of a conventional drawing machine for bars


12


, which is not shown in the drawings in any greater detail. The two tracks


10


, shown partly in

FIG. 1

, are symmetrical and opposite each other with respect to the drawing axis “x”; they are in counter-rotation with respect to each other, respectively above and below the drawing axis “x”.




Each track


10


comprises a plurality of links


13


attached to each other by means of suitable articulated joints; on each link


13


a relative gripping pad


14


is mounted, and is selectively removable.




Every gripping pad


14


is provided at the upper part with longitudinal hollows


18


inside which the bars


12


are retained in correspondence with one segment thereof, to be drawn by the tracks


10


during the drawing process.




The two tracks


10


are mounted in a conventional manner on respective rigid supporting plates


16


, they are made to rotate continuously by toothed wheels


15


on which they engage and exert a pressure on the bar


12


in cooperation with intermediate chains


17


of the roller type, imparting to the bar


12


a drawing action along the axis “x”.




The two front faces


14




a


, respectively front and rear, of the pads


14


are inclined and convergent towards the outside and are arranged inside “dovetail-shaped” housing seatings


19


made transverse on the outer face of the respective links


13


and extending from one side to the other thereof.




The couplings between the front faces


14




a


and the mating inclined walls of the housing seating


19


cause each link


13


and the relative pad


14


to be constrained; this prevents both the accidental fall and the longitudinal extraction of the latter from the housing seating


19


.




The gripping pads


14


can be released from the relative links


13


, in order to be replaced, only by means of lateral extraction from the relative housing seatings


19


.




According to the invention, this extraction is obtained by activating a rapid attachment/detachment organ


20


, with which each link


13


is provided, comprising a central clamping element and a relative activation element; the organ


20


is suitable to clamp the relative gripping pad


14


, in a stable and removable manner, inside the housing seating


19


.




In the embodiment shown in

FIGS. 2



a


,


2




b


,


3




a


and


3




b


, the organ


20


comprises a clamping pin


21


, mounted to slide axially inside a cavity


23


made on the link


13


substantially orthogonally to the plane on which the pad


14


lies and communicating with the housing seating


19


, and a thruster element


24


mounted laterally on the link


13


and located substantially orthogonal to the central pin


21


.




On the face opposite that of the longitudinal hollow


18


, and in a substantially central position, the gripping pad


14


is provided with a blind hole


28


axially aligned with the cavity


23


and suitable to receive the outer end of the central pin


21


to define the reciprocal clamping of the pad


14


and the link


13


.




The central pin


21


is constrained at the lower part to a spring


22


which is also housed inside the cavity


23


and suitable to keep the pin


21


thrusting towards the outside and therefore in the direction of the blind hole


28


. In a lateral, diametrically opposed position, the central pin


21


, which in this embodiment consists of a little cylinder, has two inclined planes


21




a


facing towards the thruster element


24


.




The thruster element


24


is housed to slide axially inside a transverse cavity


25


, made through on the link


13


substantially parallel to the plane on which the pad


14


lies and orthogonally intersecting the cavity


23


, from one side of which it partly protrudes.




The thruster element


24


is shaped like a fork and comprises two inclined plane extensions


24




a


which rest on the inclined planes


21




a


of the central pin


21


, said inclined segments


24




a


and


21




a


defining respective cam profiles cooperating with each other.




The thruster element


24


is also provided with a through eyelet


24




b


communicating with a threaded hole


26




a


which intersects the transverse cavity


23


and is substantially parallel to the central pin


21


.




A screw element


27


is inserted into the threaded hole


26




a


and is suitable to constrain the thruster element


24


to the link


13


and to define the axial sliding travel thereof inside the transverse cavity


23


.




According to the invention, the thruster element


24


is movable from a first clamping position “I” (in this case retracted:

FIGS. 2



a


and


2




b


), defined by the abutment of the inner end of the through eyelet


24




b


with the screw element


27


, to a second release position “II” (in this case advanced:

FIGS. 3



a


and


3




b


), defined by the abutment of the outer end of the through eyelet


24




b


with the screw element


27


.




The first “I” and second “II” positions define respectively the conditions wherein the gripping pad


14


is clamped and released with respect to the relative link


13


.




To be more exact, when the thruster element


24


is in its clamping position “I”, the inclined plane extensions


24




a


rest on the lower part of the inclined planes


21




a


of the central pin


21


, allowing the latter to rise and insert itself with its outer end inside the blind hole


28


due to the effect of the thrust of the spring


22


. In this condition, the pin


21


stably clamps the gripping pad


14


with respect to the link


13


.




As they take the thruster element


24


into the release position “II”, the inclined plane extensions


24




a


slide on the inclined planes


21




a


of the central pin


21


and push it downwards, by compressing the spring


22


, and cause the relative end to protrude from the blind hole


28


. In this condition, the gripping pad


14


is released and can be removed by lateral extraction from the relative link


13


.




The spring


22


tends to return the central pin


21


to the clamping position, once the pad


14


has been replaced, if necessary, and once the manual or automatic means which axially drive the thruster element


24


have been released.




In the embodiment shown in

FIGS. 4



a


and


4




b


, in which the same reference numbers have been given to those elements which are similar to, or which have the same function as, those in the embodiment shown above, the clamping element consists of a ball


121


, while the activation element consists of a thruster element


124


associated at the rear with spring means


122


.




In correspondence with an upper segment cooperating with the ball


121


, the thruster element


124


has a cavity


29


, substantially semi-spherical in shape, which acts as a cam profile to position the ball


121


.




When the thruster element


124


is in its clamping position “I” (

FIG. 4



a


), which in this case is its advanced position, the ball


121


cooperates with the upper edge of the cavity


29


; in this way the ball


121


, since it is contained laterally and unable to translate, is thrust towards the outside and is partly inserted inside the blind hole


28


made on the lower surface of the pad


14


, thus clamping the pad


14


with respect to the link


13


.




When the thruster element


124


is taken back to the release position “II” (

FIG. 4



b


), which in this case is the retracted position, by compression of the spring means


122


, the ball


121


is positioned inside the cavity


29


, suitably sized; it is lowered and freed from the blind hole


28


, and therefore releases the pad


14


which can be removed laterally with respect to the relative link


13


.




Once the pad


14


has been replaced and the means to drive the thruster element


124


have been released, the spring means


122


, like the spring means


22


in the embodiment shown in

FIGS. 2



a


-


3




b


, return the thruster element


124


automatically to the position “I” and thus to the position wherein the pad


14


is clamped.




In this case, the ball


121


is kept in position inside a conical housing seating


30


made on an insert


31


located in the outer part of the link


13


in direct cooperation with the blind hole


28


of the pad


14


. The conical seating


30


causes the ball


121


to be precisely centered and positioned with respect to the cavity


29


provided on the thruster element


124


and hence guarantees the accuracy of the operations to clamp/unclamp the pad


14


with respect to the relative link


13


.




Therefore, with this invention, we obtain that each pad


14


is clamped and unclamped simply by axially displacing the thruster element


24


in a direction substantially parallel to the plane on which the links


13


and pads


14


of the track


10


lie. This operation of axial displacement may be performed either manually, or automatically, by providing a suitable actuator device which can be arranged laterally to each track


10


and therefore in a position which does not interfere with the drawing assembly


11


with opposite tracks.




In this last case, the tracks


10


are made to rotate progressively so as to take all the links


13


, one at a time, to a position corresponding to the actuator devices which can unclamp all the gripping pads


14


in sequence.




It is possible to remove the gripping pads


14


from the same side of the track


10


on which the thruster element


24


is arranged, or from the opposite side; it is also possible to remove the pads


14


automatically by a suitable manipulator device, which may also be suitable to insert new pads


14


into the housing seatings


19


of the links


13


.




In this way the operations to replace the gripping pads


14


may be partly or completely automated according to the specific requirements connected to the production process. Once the pad


14


has been replaced, we have seen how the spring means


22


and


122


return the relative clamping means


21


,


121


to their clamping position to clamp the new pad


14


.




In the embodiment shown here, every link


13


also has, apart from the threaded hole


26




a


, a further threaded hole


26




b


, symmetrical to the first


26




a


, inside which the screw element


27


may, as an alternative, be screwed; this allows to associate the thruster element


24


on the opposite side of the link


13


should that be necessary or preferable for constructional and/or operative requirements.




In this case, the central pin


21


is mounted rotated by 180° to present its inclined planes


21




a


facing towards the thruster element


24


.




It is obvious, however, that modifications and/or additions may be made to the track


10


as described heretofore, but these shall remain within the field and scope of this invention.




For example, the end of the central pin


21


may be shaped like a sphere, or the ball


121


may be associated with spring-type positioning means. Moreover, more than one clamping element may be provided for each pad


14


, each one associated with a relative hole


28


made on the lower face of the pad


14


and suitable, for example, to be driven by the same drive element, or by different drive elements such as the thruster elements


24


and


124


.



Claims
  • 1. Track for drawing assembly, comprising a plurality of links able to support at least part of at least a gripping element, or pad of a product to be drawn, each of said gripping elements being able to be selectively clamped in a housing seating by means of rapid attachment/detachment means, wherein said rapid attachment/detachment means comprise at least a clamping element axially movable along an axis substantially orthogonal to the plane on which said gripping element lies, and an activation element axially movable and suitable to displace said clamping element from a first clamping position to a second position wherein said gripping element is released.
  • 2. Track as in claim 1, wherein said activation element is suitable to move axially on a plane substantially parallel to the plane on which said gripping element lies.
  • 3. Track as in claim 1, wherein in said first clamping position said clamping element cooperates with a seating made on the lower face of the relative gripping element.
  • 4. Track as in claim 1, wherein in said second release position said clamping element is released from said seating.
  • 5. Track as in claim 3, wherein said seating is a blind hole arranged axially with respect to said clamping element.
  • 6. Track as in claim 1, wherein said clamping element is associated with elastic means suitable to maintain it in said first clamping position.
  • 7. Track as in claim 1, wherein said activation element is associated with elastic means suitable to maintain it in a position wherein it maintains the clamping element in said first clamping position.
  • 8. Track as in claim 1, wherein said clamping element has at least a segment comprising a cam profile cooperating with a mating cam profile made on at least one segment of said activation element.
  • 9. Track as in claim 8, wherein said cam profile of said clamping element comprises a spherical or semi-spherical element suitable to be inserted at least partly inside said seating made on the lower face of the pad and said cam profile of the activation element comprises a cavity made on an upper segment cooperating with said spherical or semi-spherical element.
  • 10. Track as in claim 8, wherein said cam profile of said clamping element comprises at least an inclined plane and said cam profile of said activation element comprises at least an inclined plane suitable to cooperate by sliding with said inclined plane to define said clamping and release positions of said clamping element.
  • 11. Track as in claim 10, wherein said activation element has a fork-shaped segment comprising two inclined plane extensions cooperating with a pair of respective inclined planes of said clamping element.
  • 12. Track as in claim 1, wherein said clamping element is movable axially inside a mating cavity made on said link and substantially aligned with said seating made on the lower face of the pad.
  • 13. Track as in claim 1, wherein said activation element comprises a thruster element movable axially inside a seating made on said link and arranged substantially transverse to said cavity.
  • 14. Track as in claim 1, wherein said activation element is mounted in a laterally accessible position on said link.
  • 15. Track as in claim 1, wherein said link comprises constraining means and end-of-axial-travel means for said activation element.
  • 16. Track as in claim 15, wherein said constraining and end-of-travel means comprise at least a screw element arranged inside a longitudinal eyelet of said activation element and attached inside a threaded hole intersecting with said transverse seating.
  • 17. Track as in claim 1, wherein said activation element can be selectively associated in correspondence with both sides of said link.
  • 18. Track as in claim 1, wherein said activation element can be associated with an automatic movement actuator device to automate the operations to replace said gripping pads.
  • 19. Track as in claim 3, wherein in said second release position said clamping element is released from said seating.
  • 20. Track as in claim 4, wherein said seating is a blind hole arranged axially with respect to said clamping element.
  • 21. Track as in claim 12, wherein said activation element comprises a thruster element movable axially inside a seating made on said link and arranged substantially transverse to said cavity.
  • 22. Method to remove a gripping element of a product to be drawn in a drawing assembly with tracks, each of said tracks comprising links able to support in a clamped position at least part of at least one of said gripping elements in a relative seating, the method comprising thrusting on at least one activation element, arranged in a lateral position on a relative link and at least partly accessible from one side thereof, to determine an axial displacement thereof in a direction substantially parallel to the plane on which said gripping element lies, the displacement of said activation element causing an action to release a relative clamping element which allows said gripping element to be removed from the relative seating.
  • 23. Method as in claim 22, wherein said axial displacement of said activation element causes a mating axial displacement of the relative clamping element in a direction substantially orthogonal to the plane on which the relative gripping element lies, from a first outer clamping position to a second inner position wherein said gripping element is released.
  • 24. Method as in claim 22, wherein the axial displacement of said activation element is performed manually or automatically by acting from a lateral position with respect to said tracks and not interfering therewith.
  • 25. Method as in claim 23, wherein the axial displacement of said activation element is performed manually or automatically by acting from a lateral position with respect to said tracks and not interfering therewith.
Priority Claims (1)
Number Date Country Kind
UD99A0152 Aug 1999 IT
PCT Information
Filing Document Filing Date Country Kind
PCT/IB00/00668 WO 00
Publishing Document Publishing Date Country Kind
WO01/14076 3/1/2001 WO A
US Referenced Citations (5)
Number Name Date Kind
2251291 Reichelt Aug 1941 A
2679924 Powell Jun 1954 A
4798281 Egger Jan 1989 A
5094340 Avakov Mar 1992 A
5988364 Boyce et al. Nov 1999 A
Foreign Referenced Citations (1)
Number Date Country
645200 Mar 1995 EP