Piston-cylinder device with piston rod locking means

Information

  • Patent Grant
  • 6612221
  • Patent Number
    6,612,221
  • Date Filed
    Wednesday, January 30, 2002
    22 years ago
  • Date Issued
    Tuesday, September 2, 2003
    20 years ago
Abstract
A pressure medium activated piston-cylinder device comprises a cylinder with two end walls both having pressure medium communication ports, a piston movably guided in the cylinder and connected to a piston rod which extends out of the cylinder through a sealed-off passageway in a first one of the end walls, and a piston rod locking device located in the passageway and including a clamping element axially locked to the first end wall, and an activating member which is continuously spring biased toward a clamping element activating position and shiftable by pressure medium toward a release position, against the spring bias force, wherein a manually operable release mechanism comprises a tubular thrust element movable in the first end wall between a rest position and an activating member releasing position, and a maneuver spindle having a cam surface for co-operation with a cam surface on the thrust element for moving the thrust element between its rest position and the activating member releasing position as the maneuver spindle is rotated.
Description




The invention relates toga pressure medium activated piston-cylinder device including a cylinder with two end walls having pressure medium communication ports, a piston movably guided in the cylinder and connected to a piston rod which extends out of the cylinder through a sealed-off passageway in a first one of the end walls, a piston rod locking device located in the passageway and including at least one piston rod engaging clamping element which is axially locked relative to the first end wall, and an activating member continuously spring biassed toward a clamping element activating position and shiftable by pressure medium toward a release position against said spring bias as pressure medium is supplied to the cylinder via either one of the communication ports.




Piston-cylinder devices of this type are previously well known for various applications, See for instance U.S. Pat. No. 5,761,984, GB 997,815 and EP 103 555. They all suffer from a drawback relating to their pressure medium released piston rod locking mechanisms which lock automatically the piston rod and the object connected thereto in the very position occupied at the moment the medium pressure is interrupted. The drawback resides in the fact that there is no possibility to move manually the piston rod and the connected object without pressure medium being available. This may be particularly serious in some emergency cases where the connected object has to be moved immediately.




The primary object of the invention is to provide a piston-cylinder device of the above described type, wherein the piston rod locking device is releasable by means of a manually operable release mechanism.




Another object of the invention is to provide a piston-cylinder device of the above related type with a manually operable release mechanism which is simple and compact in design and which does not add considerably to the outer dimensions of the device.




A further object of the invention is to provide a piston-cylinder device of the above type wherein a manually operable release mechanism is designed so as to be easily operable by a low manual force.











Further objects and advantages of the invention will appear from the following specification in which is described in further detail and with reference to the accompanying drawings a preferred embodiment of the invention.




ON THE DRAWINGS





FIG. 1

shows a longitudinal section through a piston-cylinder device according to the invention.





FIG. 2

shows, on a larger scale, a longitudinal section through one of the cylinder end walls including the piston rod locking device.





FIG. 3

shows a side view of the thrust element of the manually operable release mechanism.





FIG. 4

shows a perspective view of the thrust element in FIG.


3


.





FIG. 5

shows a perspective view of the maneuver spindle in FIG.


1


.





FIG. 6

shows a torsion spring for the manuever spindle.











The piston-cylinder device illustrated in the drawings comprises basically a cylinder


10


with two end walls


11


,


12


, and a piston


13


movably guided in the cylinder


10


and connected to a piston rod


14


. Both of the cylinder end walls


11


,


12


are provided with.pressure medium communication ports


16


,


17


which are connected to a pressure medium control circuit (not shown) for supplying and draining pressure medium to and from the cylinder, respectively, thereby accomplishing movement of the piston


13


in the cylinder


10


.




One of the end walls


12


is formed with an axially extending passageway


18


through which the piston rod


14


extends out of the cylinder


10


. At its outer end the piston rod


14


is provided with a connection means


19


for connection to an object to be operated by the device.




In the passageway


18


, there is arranged a piston rod


14


locking device


21


comprising a tubular conical clamping element


22


which is axially locked relative to the end wall


12


and arranged to frictionally engage the piston rod


14


. An activating member


23


in the shape of an annular piston surrounds the clamping element


22


and is axially displaceable relative to the end wall


12


between a clamping element


22


activating position and a clamping element


22


releasing position. The activating member


23


is continuously biassed in the direction of the clamping element


22


activating position by a number of springs


24


one of which is illustrated in

FIGS. 1 and 2

.




The end wall


12


is formed with an internal cylinder portion


26


in which the activating member


23


is sealingly guided. The activating member


23


is formed with a tubular neck portion


27


which is sealingly guided in a narrowed part


28


of the passageway


18


. Pressure medium can reach the cylinder portion


26


via a control port


29


in order to pressurize and displace the activating member


23


in the direction of its release position. The control port


29


communicates with the non-illustrated control circuit, and is arranged to be supplied with pressure medium as soon as either one of the two communication ports


16


,


17


is pressurized. Alternatively, the pressure medium supply to the control port


29


may be controlled separately for obtaining piston rod braking and/or locking functions.




For reducing the frictional resistance between the activating member


23


and the clamping element


22


, there is provided a rectilinear ball bearing


31


therebetween.




Since the piston rod locking device


21


is continuously maintained in its locking position by the bias springs


24


, i.e. as long as no pressure medium is supplied via the control port


29


to lift off the spring bias force from the activating member


23


, it is not possible to move the piston rod


14


and the connected object manually or otherwise if so required.




This is not only an annoying but sometimes a serious problem, because if for some reason the medium pressure fails the object, for instance a door, can not be moved manually, which might be hazardous to people and equipment.




According to the invention, this problem is avoided by providing a manually operable release mechanism including tubular thrust element


32


which is movable in the end wall


12


between a rest position and an activating member


23


releasing position, and a maneuver spindle


33


rotatively supported in the end wall


12


about an axis Y perpendicular to the passageway


18


and the piston rod


14


. The thrust element


32


is located around a piston rod bushing


34


and has a larger diameter so as to be pivotal in the axial direction of the piston rod


14


. The thrust element


32


consists of a piece of tubing which has an inclined rear, end surface


35


, a right angle front surface


36


and a bevelled forward part


37


, and at the meeting of the bevelled part


37


and the right angle front surface


36


there are formed two diametrically opposite contact or abutment points


39


,


40


which are intended to engage the activating. member


23


. The abutment points


39


,


40


are located at about half the diameter of the thrust element


32


. See FIG.


4


.




Diametrically opposite the bevelled part


37


, the thrust element


32


is formed with a lateral opening


41


defining a cam surface for exerting a maneuvering force on the element


32


as the latter is to be pivoted about a support point


42


located on the rear end surface


35


, diametrically opposite the opening


41


. This support point


42


is axially supported against an adjustable set screw


43


mounted in an axially extending threaded bore


44


in the end wall


12


. By adjusting the set screw


43


, it is possible to compensate for the inevitable spreading of the manufacturing tolerances and set a correct rest position clearance between the thrust element abutment points


39


,


40


and the activating member


23


.




The maneuver spindle


33


is rotatively supported in a bore


45


defined by a sleeve


38


mounted in the end wall


12


. At its inner end, the maneuver spindle


33


is formed with an excentrically disposed cam pin


46


for co-operation with the cam opening


41


in the thrust element


32


, and at its outer end the spindle


33


is provided with a grip means


48


for engagement of a tool or other implement for accomplishing a manual rotation of the spindle


33


. The spindle


33


is also formed with a part-circumferential groove


47


which is intended to co-operate with a stop screw (not shown) to limit the rotational movement of the spindle


33


to a desired angle. See FIG.


5


.




Moreover, the manuever spindle


32


is formed at its inner end with a diametrically extending slot


49


for engagement with a clock type torsion spring


51


. See FIG.


6


. This spring


51


is arranged to exert a rotational bias force on the maneuver spindle


33


in a direction where the thrust element


32


occupies its rest position. For engagement with the slot


49


in the maneuver spindle


33


, the spring


51


is formed with a diametrically extending inner end portion


52


. At its outer end, the spring


51


is formed with a radially directed end portion


53


to be locked relative to the end wall


12


.




As described above, the piston


13


and piston rod


14


are locked by the clamping element


22


as the activating member


23


is biassed into engagement therewith by the springs


24


. This condition will prevail as long as pressure medium is not supplied via the control port


29


to accomplish a retraction of the activating member


23


against the force of the springs


24


. However, if pressure medium for some reason is not available and the object connected to the piston rod


14


has to be moved, the maneuver spindle


33


is operable by a tool or implement to accomplish a movement of the thrust element


32


and the activating member


23


.




In particular, at rotation of the maneuver spindle


33


the cam pin


46


co-operates with the cam surface defined by the opening


41


to make the thrust element


32


pivot in relation to its support point


42


and the projection


43


in the passageway


18


. During this movement, the thrust element


32


engages via its abutment points


39


,


40


the activating member


23


and urges the latter axially against the load of the springs


24


, whereby the engagement between the activating member


23


and the clamping element


22


is interrupted as is the locking engagement between the clamping element


22


and the piston rod


14


.




Due to the limited rotational movement of the spindle


33


, the cam pin


46


will occupy an end position as the lock device is fully released which means that the engagement point between the cam surfaces on pin


46


and in opening


41


is located on a straight line with the rotation axis of the spindle


33


which is parallel with the load direction of the springs


24


. This means that the spring load does not result in a rotational force on the spindle


33


and that the spindle


33


will remain in its locking device release position as long as the spring force prevails.




However, as soon as pressure medium is supplied via the control port


29


, the radial force on the cam pin


46


will cease and the spindle


33


will be returned to its inactive position by the torsion spring


51


. It is of course possible to turn the spindle


33


back to its inactive position by applying a tool or other implement to the grip means


48


.




By the difference in distance between the support point


42


and the cam surface opening


41


on one hand, and the distance between the abutment points


39


,


40


and the cam surface opening


41


on the other hand, there is obtained an amplification of the force transferred via the cam surfaces


46


,


41


and the force exerted by the abutment points


39


,


40


on the activating member


23


. This in combination with a small distance between the rotation axis of the maneuver spindle


33


and the cam surface on the cam pin


46


results in a relatively low operating force needed to release the locking device


21


.



Claims
  • 1. Pressure medium activated piston-cylinder device, comprising a cylinder (10) with two opposite end walls (11,12) provided with pressure medium communication ports (16,17), a piston (13) movably guided in said cylinder (10) and connected to a piston rod (14) which extends out of said cylinder (10) through a sealed-off passageway (18) in a first one (12) of said end walls (11,12), a piston rod locking device (21) located in said passageway (18) and including at least one clamping element (22) axially locked relative to said first end wall (12) and arranged to frictionally engage said piston rod (14), and an activating member (23) continuously spring biassed toward a clamping element (22) activating position and shiftable by pressure medium toward a release position against said spring bias force,characterized in that said piston rod locking device (21) comprises a manually operable release mechanism which includes a thrust element (32) movably supported in said first end wall (12) between a rest position and an activating member (23) releasing position, a maneuver spindle (33) rotatably supported in said first end wall (12) and having a maneuverable end portion (48) extending outside said first end wall (12), a first cam surface (41) provided on said thrust element (32) and a second cam surface (46) provided on said maneuver spindle (33), said first cam surface (41) being engaged by said second cam surface (46) for accomplishing movement of said thrust element (32) between said rest position and said activating member (23) releasing position as said maneuver spindle (33) is rotated.
  • 2. Piston-cylinder device according to claim 1, wherein said thrust element (32) is tubular in shape and located substantially coaxially with said piston rod (14), said thrust element (32) being pivotal in the axial direction of said passageway (18) about a support point (42) located on the outer circumference of said thrust element (32) and said first cam surface (41) is located diametrically opposite said support point (42), wherein rotation of said maneuver spindle (33) causes said thrust element (32) to pivot about said support point (42) between said rest position and said activating member (23) releasing position.
  • 3. Piston-cylinder device according to claim 2, wherein said thrust element (32) has two each other diametrically opposite and axially directed abutment points (39,40) for engagement with said activating member (23), said abutment points (39,40) are both disposed at an angular distance of about 90 degree from said support point (42) as well as from said first cam surface (41).
  • 4. Piston-cylinder device according to anyone of claims 1-3, wherein said maneuver spindle (33) is rotative about an axis extending perpendicularly to said passageway (18).
  • 5. Piston-cylinder device according to claim 4, wherein in said activating member (23) releasing position of said thrust element (32) said first and second cam surfaces (41,46) are arranged to engage each other in a point axially in line with the rotation axis (Y) of said maneuver spindle (33), whereby said spring bias force acting on said activating member (23) is unable to exert a rotational force on said maneuver spindle (33), and a torsion spring (51) is connected between said maneuver spindle (33) and said first end wall (12) so as to exert a rotational force on said maneuver spindle (33) in the direction of said thrust element (32) rest position.
  • 6. Piston-cylinder device according to claim 5, wherein said torsion spring (51) comprises a spiral type clock spring.
Priority Claims (1)
Number Date Country Kind
9901108 Mar 1999 SE
PCT Information
Filing Document Filing Date Country Kind
PCT/SE00/00579 WO 00
Publishing Document Publishing Date Country Kind
WO00/58632 10/5/2000 WO A
US Referenced Citations (7)
Number Name Date Kind
3918346 Ziegler Nov 1975 A
4214795 Kakuminato Jul 1980 A
5553690 Takahashi Sep 1996 A
5761984 Goellner et al. Jun 1998 A
6044934 Nemeth Apr 2000 A
6178870 Takahashi Jan 2001 B1
6343538 Skinner Feb 2002 B1
Foreign Referenced Citations (2)
Number Date Country
0103555 Mar 1984 EP
997815 Jul 1965 GB