Vertical compression bending machine

Information

  • Patent Grant
  • 6523388
  • Patent Number
    6,523,388
  • Date Filed
    Wednesday, September 6, 2000
    24 years ago
  • Date Issued
    Tuesday, February 25, 2003
    21 years ago
Abstract
A vertical compression bending machine that uses linear bearings to guide the ram and cushions assemblies. The inventive machine also employs an adjustment mechanism to align the wing dies relative to one another.
Description




BACKGROUND




1. Field of Invention




The present invention relates to a machine that bends tubing. The machine employs linear ball bearings to reduce friction in the system.




2. Description of Art




Manufacturers of industrial equipment have been building tube bending machines to bend tubing for decades. One such machine is a vertical compression bending machine. A vertical compression bender makes use of a ram die and two wing dies. During the bending process, the ram die, along with a supporting ram assembly, advances in a linear fashion toward the two wing dies. A tube, supported by the two wing dies, is initially contacted by the ram die during the advancement of the ram assembly. After the ram die makes initial contact with the tube, it continues to push through the tube while forcing the wing dies to rotate away and outward from the ram die. The ram die sees resistance from the tube along with the resistance from the wing dies. In order for the tube to stay up and inside the ram die during the bending process, the wing dies must provide a counter force (cushion) in a direction against the advancing ram die. The counter force from the wing dies will hold the tube in a firm position against the ram die. The ram die continues to advance while at the same time overcoming the resistance of the tube and wing dies. The ram die continues to advance until the tube reaches the required bend angle. At that point, the ram assembly reverses direction and returns to its home position. The wing dies also reverse direction and both wing dies rotate back to their home position.




Over the years manufacturers have relied on various types of wear pads to guide the ram assembly during the bending process. A typical wear pad is constructed from bronze and acts as a bearing surface guiding the ram die and thus the ram assembly during a bending stroke. Wear pads were designed into this application decades ago because they afforded the best load bearing capability at a reasonable cost.




A compression bender is depicted in U.S. Pat. No. 2,997,141 issued to Bower et al. The Bower et al. patent shows a bender that uses guide members


25


and


26


along with wing slides


29


and


30


to ensure that the ram die


36


is guided along a linear path during a bending operation. The guide members


25


and


26


act as wear plates. These wear plates, most often constructed from a bronze material, are the bearing surfaces that allow the ram die to lynamically thrust to and from the wing dies while at the same time providing a bearing surface guide the ram assembly along a linear path.




The Bower et al. patent also uses the same approach when guiding the motion of the piston rods


87


and


96


. Bower et al. relies on the bushings inside the cushion cylinders


77


and


78


to help support the forces on the piston rods


87


and


96


. Cylinders


77


and


78


provide a counter force (cushion) to the advancing ram die


36


. This counter force is transmitted to the ram die


36


through the wing dies


59


and


66


and the tube.




One disadvantage of the Bower et al. patent is the friction associated with the wear plates that guide the ram assembly. These bearing surfaces often require constant maintenance and eventually will need to be replaced due to the friction associated with the wear plates.




Another disadvantage of the Bower et al. patent is the side loads on the piston rods


87


and


96


. These side loads will in time require unnecessary maintenance and thus the bushings in the cylinders


77


and


78


will have to be replaced. In general, these bushings should never take side loading.




SUMMARY OF THE INVENTION




Accordingly, several objects and advantages of my invention are:




(a) to reduce the friction associated with the ram assembly during a bending operation;




(b) to reduce the cost of maintenance associated the ram and cushion assemblies;




(c) to reduce the friction of the bearing assembly used to guide the cushion assembly; and




(d) to prevent a side load from imparting on the cushion cylinder's piston rod.




Still further objects and advantages will become apparent from a consideration of the ensuing description and drawings.




The foregoing objects and advantages can be achieved by providing a vertical compression bending machine comprising a first wind die which supports a second part of the tube, a frame supporting a first linear rail, a first linear bearing which slidably moves along the first linear rail, a ram block mounted to the first linear bearing, and a ram die, mounted to the ram block, which vertically moves to form a bend in the tube, wherein the ram block and first linear bearing move in conjunction with the ram die so that the first linear bearing slides along the first linear rail, and the first and second wing dies provide movable support to the tube as the ram die bends the tube.











DESCRIPTION OF THE DRAWINGS





FIG. 1

shows an isometric view of the first embodiment depicting the linear rail and linear bearing supporting the ram assembly;





FIG. 2

shows an isometric view of the first embodiment depicting a tube being bent;





FIG. 3

shows an isometric view of the wing die assemblies, the cushion assembly, a linear rail supporting the cushion assembly, and a mechanism to adjust the wing dies relative to one another.





FIG. 4

shows an isometric view of the first linear rail and its internal lubrication passage.





FIG. 5

shows an isometric view of the second linear rail and its internal lubrication passage.





FIG. 6

shows the mechanism to adjust the position of the wing dies.











DESCRIPTION OF THE PREFERRED EMBODIMENTS




With initial reference to

FIG. 1

, the first embodiment


10


is shown. A ram die


11


is mechanically fastened to a ram block


12


. Ram block


12


is mechanically fastened to a linear bearing


13


. Linear bearing


13


may be of the type described by Teramachi in U.S. Pat. No. 4,040,679 and by Teramachi in U.S. Pat. No. 4,252,709.




In both U.S. Pat. No. 4,040,679 and U.S. Pat. No. 4,252,709, Teramachi teaches about a linear bearing that employs recirculating ball bearings. The ball bearings recirculate in a track while the bearing block advances in a linear fashion along a linear rail. The grooves in the linear rail help captivate the ball bearings as the ball bearings recirculate within the bearing block. This technique results in rolling friction as the linear bearing moves relative to the linear rail.




Linear bearing


13


is coupled to a linear rail


14


. A lube passage


63


is formed into linear rail


14


, see FIG.


4


.




Linear rail


14


is fastened to frame


15


. Ram block


12


is fastened to a coupling


17


. Coupling


17


is fastened to a piston rod


18


and piston rod


18


is joined to a ram cylinder


19


. Ram cylinder


19


is fastened to frame


15


.




A wing die


20


is supported by a wear strip


22


, a wear strip


24


, and a wear strip


26


. Wear strips


22


,


24


, and


26


are supported by a support housing


55


. Support housing


55


is fastened to a support block


28


. Support block


28


is fastened to a cushion shaft


30


. Wear strips


22


,


24


, and


26


, support housing


55


, and cushion shaft


30


are considered the first cushion shaft assembly


65


.




A wing die


21


is supported by a wear strip


23


, a wear strip


25


, and a wear strip


27


, see also FIG.


3


. Wear strips


23


,


25


, and


27


are supported by a support housing


56


. Support housing


56


is fastened to a support block


29


. Support block


29


is fastened to a cushion shaft


31


, see also FIG.


3


. Wear strips


23


,


25


, and


27


, support housing


56


, and cushion shaft


31


are considered the second cushion shaft assembly


66


.




Cushion shaft


30


is supported by a bearing block


32


and a bearing block


34


. Bearing blocks


32


and


34


are fastened to frame


15


.




Cushion shaft


31


is supported by a bearing block


33


and a bearing block


35


, see also FIG.


2


. Bearing blocks


33


and


35


are fastened to frame


15


.




From

FIG. 2

, located in wing dies


20


and


21


is a tube


57


.




From

FIG. 1

, an encoder bracket


58


is fastened to bearing block


35


. Fastened to encoder bracket


58


is an encoder


59


. Encoder


59


is coupled to cushion shaft


31


.




From

FIGS. 3 and 6

, a rocker arm


36


and a rocker arm


37


are fastened to cushion shafts


30


and


31


respectively. A rocker bearing


60


is supported by a pin


43


. Pin


43


is fastened to rocker arm


36


. A rocker bearing


61


is supported by a pin


44


. Pin


44


is fastened to rocker arm


37


.




Rocker arm


36


, rocker bearing


38


, and pin


43


are considered the rocker arm assembly


68


. Rocker arm


37


, rocker bearing


39


, and pin


44


are considered the rocker arm assembly


69


.




From

FIG. 6

, rocker bearings


60


and


61


roll inside a tilt block


40


on surface


40




a


and


40




b


, respectively. A cap block


41


, fastened to tilt block


40


, captivates rocker bearings


60


and


61


against tilt block


40


, see

FIG. 6. A

pin


45


supports tilt block


40


. Pin


45


is fastened to housing


42


. A bolt


70


and a bolt


71


are threaded into housing


42


and both bolts


70


and


71


butt up against tilt block


40


. Housing


42


is fastened to a piston rod


49


. Piston rod


49


is connected to a cushion cylinder


50


. Cushion cylinder


50


is fastened to frame


15


. Housing


42


is fastened to a linear bearing


47


. Linear bearing


47


is coupled to a linear rail


48


. Linear rail


48


is fastened to frame


15


.




Linear bearing


47


may be of the type described by Teramachi in U.S. Pat. No. 4,040,679 and by Teramachi in U.S. Pat. No. 4,252,709.




In both U.S. Pat. No. 4,040,679 and U.S. Pat. No. 4,252,709, Teramachi teaches about a linear bearing that employs recirculating ball bearings. The ball bearings recirculate in a track while the bearing block advances in a linear fashion along a linear rail. The grooves in the linear rail help captivate the ball bearings as the ball bearings recirculate within the bearing block. This technique results in rolling friction as the linear bearing moves relative to the linear rail.




Linear bearing


47


is coupled to linear rail


48


. Linear rail


48


is of the type described by Teramachi in U.S. Pat. Nos. 4,040,679 and 4,253,709. A lube passage


64


(see

FIG. 5

) is formed into linear rail


48


.




Tilt block


40


, cap block


41


, pin


45


, bolt


70


, bolt


71


, and housing


42


make up the cushion assembly


67


.




In operation, pressure is applied to one side of cylinder


19


causing piston rod


18


, initially extended in its home position, to retract toward cylinder


19


. The retraction of piston rod


18


causes coupling


17


, ram block


12


, ram die


11


, and linear bearing


13


to advance toward cylinder


19


.




Prior to ram die


11


making initial contact with tube


57


, sufficient pressure is present in cushion cylinder


50


to cause piston rod


49


to be fully extended in the home position. At this point, wing dies


20


and


21


are adjacent to one another at a right angle as shown in FIG.


1


.




From

FIG. 2

, the ram die


11


continues to advance toward ram cylinder


19


and thus starts to bend tube


57


. As the bending process continues, a pressure is maintained in cushion cylinder


50


. This pressure creates a counter force (cushion) against the advancing ram die


11


.




The counter force is realized by ram die


11


when wing dies


20


and


21


are forced to rotate about cushion shafts assemblies


65


and


66


. The pressure in cushion cylinder


50


tends to prevent cushion shaft assemblies


65


and


66


from rotating. With a pressure in cushion cylinder


50


, piston rod


49


tends to force cushion assembly


67


away from cushion cylinder


50


. This causes rocker arm assemblies


68


and


69


to keep a counter torque on cushion shaft assemblies


65


and


66


. This counter torque is in opposition to the advancing ram die


11


. As ram die


11


advances, it not only bends tube


57


, but it also forces piston rod


49


to retract into cushion cylinder


50


. Linear bearing


47


and linear rail


48


support cushion assembly


67


and piston rod


49


as piston rod


49


travels in a direction parallel to linear rail


48


. Any side loading caused by rocker arm assemblies


68


and


69


on cushion assembly


67


will be carried by linear bearing


47


and linear rail


48


.




When encoder


59


realizes the preset bend angle, the pressure in ram cylinder


19


causes ram die


11


to return to its home position. This in turn causes cushion cylinder


50


to extend piston rod


49


and thus returns both wing dies


20


and


21


to their home position.




During the initial setup of the machine, it may be necessary to adjust the relative position of wing die


20


with respect to wing die


21


. When in the correct home position, both wing dies


20


and


21


should be adjacent and at a right angle to one another in the home position. Therefore, both die


20


and die


21


should be inline to one another when cylinder


19


is in the extended position. Wing dies


20


and


21


can be adjusted to ensure that both wing dies


20


and


21


are inline to one another (coplanar). By adjusting bolts


70


and


71


, the angle between housing


42


and tilt plate


40


will change. Adjusting bolts


70


and


71


will rotate tilt plate


40


about pin


45


. By advancing bolt


70


and retracting bolt


71


, wing die


20


will rotate up and away from ram cylinder


19


. At the same time, wing die


21


will rotate down and toward ram cylinder


19


. By retracting bolt


70


and advancing bolt


71


toward tilt plate


40


, wing die


20


will rotate down and toward cylinder


19


and wing die


21


will rotate up and away from cylinder


19


. This adjustment feature provides for ease of assembly to ensure that both wing dies are inline (parallel and coplanar) to one another in the home position. When wing die


20


and wing die


21


are inline, the relative angle formed between both dies


20


and


21


is zero. The relative angle is measured in the plane at which tube


57


is being bent.




During operation of the inventive machine, lubrication can be supplied to the rolling elements located inside linear bearings


13


and


47


through lube passage


63


and


64


, respectively. As lubrication is supplied to lube passages


63


and


64


, the rolling elements inside linear bearings


13


and


47


respectively will come in contact with the lubricant being transported through lube passages


63


and


64


.




Linear bearings


13


and


47


make use of ball bearings as a rolling element. It should be noted that the ball bearings could be replaced with roller bearings or needle bearings. Both the roller bearings and needle bearings would take the form of a right circular cylinder. This approach would improve the load bearing capability of the linear bearing.




Cylinders


19


and


50


operate on hydraulic pressure. However, any number of mechanical power devices could replace one or both of cylinders


19


and


50


. For example, an all electric actuator could replace either cylinder


19


and/or cylinder


50


.




Accordingly, the scope of the invention should be determined not by the embodiments illustrated, but by the appended claims and their legal equivalents.



Claims
  • 1. A compression bending machine to bend a tube, comprising:a first wing die which supports a first part of the tube; a second wing die which supports a second part of the tube; a frame; a first linear rail supported by the frame; a first linear bearing which slidably moves along the first linear rail; a ram block mounted to the first linear bearing; and a ram die, mounted to the ram block, which moves to form a bend in the tube, wherein the ram block and first linear bearing move in conjunction with the ram die so that the first linear bearing slides along the first linear rail, and the first and second wing dies provide movable support to the tube as the ram die bends the tube; wherein the first linear bearing comprises ball bearings which roll along the first linear rail as the first linear bearing moves along the first linear rail.
  • 2. The compression bending machine according to claim 1, wherein the first linear rail comprises a lube passage formed therein, the lube passage having lubricant to lubricate the first linear bearing.
  • 3. The compression bending machine according to claim 1, further comprising:a coupling fastened to the ram block; a first driving device, attached to the coupling, which moves the coupling, ram block, ram die and first linear bearing, enabling the ram die to form the bend in the tube.
  • 4. The compression bending machine according to claim 3, further comprising:a first cushion shaft assembly which supports the first wing die; a second cushion shaft assembly which supports the second wing die; a first rocker arm assembly fastened to the first cushion shaft assembly; a second rocker arm assembly fastened to the second cushion shaft assembly; a cushion assembly coupled to the first and second rocker arm assemblies; and a second driving device, attached to the cushion assembly, which movably supports the first and second wing dies from an initial position to a completed bend position as the ram die bends the tube, and moves the first and second wing dies back from the completed bend position to the initial position subsequent to completion of the bend.
  • 5. The compression bending machine according to claim 4, further comprising:a second linear rail mounted on the frame; and a second linear bearing, mounted to the cushion assembly, which slidably moves along the second linear rail as the second driving device moves the cushion assembly so as to guide the cushion assembly.
  • 6. The compression bending machine according to claim 3, wherein the first driving device comprises:a piston rod coupled to the coupling; and a ram cylinder which receives the piston rod.
  • 7. The compression bending machine according to claim 4, wherein: the first driving device comprises:a first piston rod coupled to the coupling, and a ram cylinder which receives the first piston rod; and the second driving device comprises: a second piston rod coupled to the cushion assembly, and a cushion cylinder which receives the second piston rod.
  • 8. The compression bending machine according to claim 5, wherein the second linear bearing comprises ball bearings which roll along the second linear rail as the second linear bearing moves along the second linear rail.
  • 9. The compression bending machine according to claim 5, wherein the second linear bearing comprises roller bearings which roll along the second linear rail as the second linear bearing moves along the second linear rail.
  • 10. The compression bending machine according to claim 5, wherein the second linear rail comprises a lube passage formed therein, the lube passage having lubricant to lubricate the second linear bearing.
  • 11. The compression bending machine according to claim 1, further comprising:a tilt plate which causes the first and second wing dies to rotate; first and second bolts which adjust the tilt plate so as to rotate the first and second wing dies.
  • 12. The compression bending machine according to claim 4, further comprising:a tilt plate which causes the first and second wing dies to rotate; wherein the cushion assembly comprises first and second bolts which adjust the tilt plate so as to rotate the first and second wing dies about the first and second cushion shaft assemblies, respectively.
  • 13. A compression bending machine to bend a tube, comprising:a first wing die which supports a first part of the tube; a second wing die which supports a second part of the tube; a frame; a first linear rail supported by the frame; a first linear bearing which slidably moves along the first linear rail; a ram block mounted to the first linear bearing; and a ram die, mounted to the ram block, which moves to form a bend in the tube, wherein the ram block and first linear bearing move in conjunction with the ram die so that the first linear bearing slides along the first linear rail, and the first and second wing dies provide movable support to the tube as the ram die bends the tube; wherein the first linear bearing comprises roller bearings which roll along the first linear rail as the first linear bearing moves along the first linear rail.
  • 14. A compression bending machine to bend a tube, comprising:a first wing die which supports a first part of the tube; a second wing die which supports a second part of the tube; a ram block; and a ram die, mounted to the ram block, which moves to form a bend in the tube, wherein the first and second wing dies provide movable support to the tube as the ram die bends the tube; a tilt plate which causes the first and second wing dies to rotate; at least one bolt which adjusts the tilt plate so as to rotate the first and second wing dies.
  • 15. The compression bending machine according to claim 14, wherein the at least one bolt comprises first and second bolts which adjust the tilt plate so as to rotate the first and second wing dies.
  • 16. A compression bending machine to bend a tube, comprising:a first wing die which supports a first part of the tube; a second wing die which supports a second part of the tube; a frame; a ram block; a ram die, mounted to the ram block, which moves to form a bend in the tube, wherein the first and second wing dies provide movable support to the tube as the ram die bends the tube; a first cushion shaft assembly which supports the first wing die; a second cushion shaft assembly which supports the second wing die; a first rocker arm assembly fastened to the first cushion shaft assembly; a second rocker arm assembly fastened to the second cushion shaft assembly; a cushion assembly coupled to the first and second rocker arm assemblies; and a driving device, attached to the cushion assembly, which movably supports the first and second wing dies from an initial position to a completed bend position as the ram die bends the tube, and moves the first and second wing dies back from the completed bend position to the initial position subsequent to completion of the bend; a linear rail mounted on the frame; and a linear bearing, mounted to the cushion assembly, which slidably moves along the linear rail as the driving device moves the cushion assembly so as to guide the cushion assembly.
  • 17. The compression bending machine according to claim 16, wherein the linear bearing comprises ball bearings which roll along the linear rail as the linear bearing moves along the linear rail.
  • 18. The compression bending machine according to claim 16, wherein the linear rail comprises a lube passage formed therein, the lube passage having lubricant to lubricate the linear bearing.
  • 19. The compression bending machine according to claim 16, further comprising:a tilt plate which causes the first and second wing dies to rotate; wherein the cushion assembly comprises first and second bolts which adjust the tilt plate so as to rotate the first and second wing dies about the first and second cushion shaft assemblies, respectively.
US Referenced Citations (8)
Number Name Date Kind
3279236 Lance Oct 1966 A
3306093 Sassak Feb 1967 A
3429157 Huth Feb 1969 A
3756058 Hamkins Sep 1973 A
4040679 Teramachi Aug 1977 A
4253709 Teramachi Mar 1981 A
4833907 Grimaldo May 1989 A
4967585 Grimaldo Nov 1990 A