GB2266929A

GB2266929A - A method of applying intensified force to a workpiece

Info

Publication number: GB2266929A
Application number: GB9315551A
Authority: GB
Inventors: Michael H Wolfbauer
Original assignee: Savair Inc
Current assignee: Savair Inc
Priority date: 1989-09-18
Filing date: 1993-07-27
Publication date: 1993-11-17
Anticipated expiration: 2013-07-27
Also published as: GB9315551D0; GB2266929B

Abstract

A method for applying an intensified force to a workpiece comprises the following steps: a) a fluid pressure is applied to one side of a reservoir piston (132) located in a master cylinder (12) to move the reservoir piston (132) along the master cylinder (12) from a first predetermined position in a first predetermined direction; this effects movement of a piston (154) and its associated piston rod (46) located in an actuator cylinder (14) from a first predetermined position in a direction towards the workpiece, so that a first predetermined force is applied to said workpiece; b) a fluid pressure is applied to one side of an intensifier piston (104) to positively constrain the intensifier piston (104) in a first predetermined position from movement concurrently with the aforementioned step of applying a fluid pressure and simultaneously moving said piston (154); c) concurrently i) a fluid pressure is applied to the other side of the intensifier piston (104) and ii) said fluid pressure is relieved which was applied to said one side of said intensifier piston (104) to move said intensifier piston (104) and its associated piston rod (110) in said first predetermined direction to intensify said first predetermined force applied to said workpiece; and d) said fluid pressure which was applied to said one side of said reservoir piston (132) is relieved and simultaneously a fluid pressure is applied to a side of said piston (184) most distal from said master cylinder (12) and said one side of said intensifier piston (104) to return said intensifier piston (104), said reservoir piston (132) and said piston (154) in said actuating cylinder (14) to its first predetermined position. <IMAGE>

Description

A METHOD OF APPLYING INTENSIFIED FORCE TO A WORKPIECE This invention relates to a method of applying an intensified force to a workpiece.

This patent application is divided out from our co-pending parent patent application No. 9020351. 4 (Serial No. 2,238,079) entitled "OLEOPNEUMATIC INTENSIFIER" which has claims to an apparatus for intensifying a force that is applied to a tool to move the tool into and out of engagement with a workpiece.

The invention which is the subject of that parent patent application relates to a fluid powered

apparatus that has application for clamping, punching, welding and other functions that are necessary in the manufacture and assembly of machines and vehicles such as automobiles. More particularly, the invention is related to a dual action fluid powered apparatus designed to implement a rapid movement in approaching a workpiece until contact Is is effected. The movement of the apparatus upon contact with the workpiece is then transformed to a slow, more powerful working mode.

The prior art reveals a wide variety of fluid powered devices that employ a plurality of cylinder and piston combinations to control the speed and force of the device as an element thereof advances toward a workpiece.

In general, most of the prior art devices utilize a tandem arrangement tor the various pistons that are all contained within a single cylindrical housing.

By way of example, the

the oleopneumatic Dack that is shown and described in U.S. Patent N0.3,426,530 entitled "Oleopneumatic Jack with Singed Structure" Issued February 11, 1969, to Alexander Georgelin. The jack has a cylindrical tubular

body structure with end caps attached thereto. A first piston is positioned at one end within the cylindrical body. The piston has attached thereto an elongated hollow plunger that is adapted to move with the piston.

A floating piston is positioned so that is slides freely along the previously mentioned hollow plunger. A third piston is positioned near the other end of the cylindrical body. The third piston has coupled thereto, as an intergral part,a thrust member that protrudes from the other end of the cylindrical body. The third piston contains a hollow central chamber into which extends a portion of a thurst member. Air pressure is applied to one end of the floating piston thus causing it to urge oil against the third piston which in turn causes the thurst member attached to the third piston to extend from the cylindrical body. After the initial rapid advancement of the third piston and the thurst member, air pressure is introduced behind the first piston.As the first piston moves axially along the interior of the cylindrical body, its attached hollow plunger enters the oil filled hollow central chamber of the third piston thus causing it to move slowly while entering a large force.

In U. S. Patent No. 4. 099. 436 entitled "Apparatus for Piercing Sheet Material" Issued July 11, 1978, to Donald Beneteau, there is described a force Intensifier that employs an oil reservoir that is external of a cylindrical structure that contains a pair of pistons in axial alignment. The oil in the reservoir is forced into the cylinder by pressurized air that is in direct contact with the oil. The oil that is introduced into the cylinder moves one of the pistons, causing a tool carrying plunger to advance toward a workpiece. In order to intensify the force delivered by the tool carrying plunger, air is introduced behind the other piston, causing it to move an attached plunger into a constricted cavity where the oil pressure 19 greatly Increased, thereby exerting an even greater force on the tool carrying plunger.

One of the disadvantages of the above described apparatus is that its position cannot be readily changed because of the air-oil interface in the reservoir.

An additional load producing cylinder shown in Figure 3 of U.S. Patent No. 4,395,027 entitled "Pressure Intensifying Device" issued July 26, 1983, to Robert Nordmeyer. Figure 3 of the above referenced patent depicts a cross-sectional view of a pressure intensifying device that has an essentially cylindrical configuration. There is a first piston and plunger combination that moves in the direction towards a second piston plunger, combination. The first piston moves under the influence of air pressure and returns to its original position by the biasing action of a compression spring. The second piston 15 essentially hollow and is filled with oil that supplies the force that causes the second piston and plunger to move linearly.After the second piston has accomplished its initial movement, the first piston plunger is advanced into the oil filled chamber of the second piston. The force on the second piston is thus intensified. The cylinder contains an internally positioned oil reservoir through which the first piston plunger passes. The just mentioned device utilizes, in tandem, pistons that move in the same direction during the initial or advancement movement.

One of the inherent drawbacks of the just described device is its is overall length. Then. too, the spring that is biased against the first piston subtracts from the overall load that is applied by air pressure.

r)99rocea;cTi since the oil is self-contained completely withi e confinement of the apparatus. Also, the sent invention utilizes a reverse direc n floating piston concept to reduce the over length of the apparatus.

In addition, che pre tinve ntion has a plunger unit that is srom the load enhancement plunger.

< prooollt ln:on~ion dooo not utlllio opelngo to and sn

The present invention provides a method of applying an intensified force to a workpiece as claimed in claim 1, to which reference is directed.

There follows a description, eventually referring to drawings, of a preferred form of apparatus for carrying out the method of the present invention.

This preferred apparatus

4b

original position by the biasing action of a compr Sion spring. The second piston is essentially holly and is filled with oil that supplies the force tha causes the second piston and plunger to move linea y. After the second piston has accomplished its i tial movement, the first piston plunger is advanced to the oil filled chamber of the second piston. / he force on the second piston is thus intensified. The cylinder contains an internally positioned 0 reservoir through which the first piston plunger asses. The just mentioned device utilizes, in tan m, pistons that move in the same direction dur g the initial or advancement movement.

One of the inherent drawbacks of the just described devicits is overall length. Then. too, the spring that is biased against the first piston subtracts from go o orall Load 'hat 1C applloa bi alr prooouro

does not have an air-oil interface since the oil is self-contained completely within the confinement of the apparatus. Also, the

a yp a r atLtr L4- 6s ulilizes a reverse direction floating piston concept to reduce the overall length of the apparatus.

In addition, the

peFerreLi aFparatLss procvno-n:oniiow has a plunger unit that is separate from the load enhancement plunger.

The

p 'e Frred JpgaratuS prooflt n-on=1on does not utilize springs to aid in

the movement of the pistons. Also, the,

not arranged in a continuous linear array as is the device described In U.S.Patent 4,395,027.

xho prozont 1n-ontlon ifi a rirst acpoaw pro ldGc an/ apparatus for intensifying a force that is applie to a tool to move said tool into and out of engageme i with a workpiece, said apparatus comprising: a master cylinder divided into a first avity and a second cavity with a first bore situated ss erebetween; an actuating cylinder comprising a third cavity; an intensifier piston slidably slated. in said first cavity and dividing the first cavity into first and second chambers; a reservoir piston having second bore and slidably situated in said se H nd cavity and dividing the second cavity into third a fourth chambers; an intensifier rod ttached to said intensifier piston and passing through said first bore into said second cavity and through said second bore;; a rear pisto slidably situated in said third cavity and divi ng the third cavity into fifth and sixth chamber passag means connecting said fourth and sixth chambers nd capable of passing hydraulic fluid therebe ween;;

solno for lfitroduolng 1 prcogurleea f'ui lnto satd third chamber for moving said reservoir piston so at when the fourth chamber contains hydraulic fl /, at least some is forced into the sixth chamb via said passage means, thereby to move said ar piston and actuating rod, for bringing a to < into contact with a workpiece;; means for introdu ng a pressurised fluid into said first chamber to m e said intensifier piston, for causing said tensifier rod to act on any hydraulic fluid in + e fourth chamber and/or the passage means, to intfying the force which any tool associated with zo aotuatlng rod brlngo to boAr on a szorkploso.

is a load intensifier apparatus for use in any application where a linear force of considerable magnitude is required such as in metal shaping, punching, clamping and welding.

includes a two part housing wherein the second portion of the housing can be arranged at any attitude with respect to the first portion of the housing. The first portion of the housing contains an enclosed oil reservoir that is in communication with the second housing. The first portion of the housing contains a floating piston that moves along the piston rod of an intensifier piston. The second portion of the

housing contains a piston and a piston rod that extends from the housing. In the first housing, air pressure is introduced to one side of the floating piston causing a volume of oil located on the other side of the floating piston to move into the second portion of the housing where its pressure causes the piston within the second portion of the housing to undergo rapid movement to advance the attached piston rod toward a workpiece.

After the rapid movement of the piston in the second portion of the housing has occurred, the pressure intensifier piston within the first portion of the housing is moved under the influence of air pressure.

The end of the piston rod of the intensifier piston then enters a constricted oil passageway causing a slow but intense movement of the piston in the second portion of the housing. The further movement of the piston in the second portion of the housing causes its piston rod to additionally bias itself against the workpiece.

is compact and can function with a variety of tools attached thereto.

utilizes two separable housings so that the apparatus can be employed in confined spaces.

the externally applied motivating force is pneumatic utilizing a retardant fluid.

contains a completely enclosed hydraulic circuit which will properly operate in any degree of orientation with reference to gravity.

distinct housing portions located at selectively spaced apart locations, each of which lends itself to rapid replacement and repair.

axial length of the overall

is hihlm;iecl device kand thereby conservetspace.

utilizes, initially, a fast stroke followed by a low impact stroke to contact the workpiece and rapid pressure build up to hold the workpiece.

electronic capability to detect if the hydraulic oil needs replenishing and allow refilling, if needed,

without removing the unit from the machine.

utilizes one valve to operate forward stroke, intensifier stroke and return stroke thereby keeping the cycle time to a minimum.

has a load cell to indicate the position of work and to display the pressure holding the workpiece while not experiencing any impact loads on the load cell.

rhe p re pre ferrecl 9fplrat6fS hag a 4il1 - C.rba-~ajLqF*4Jt 0' reduceL overall length o' the t by incorporating special structure into the end cap of the apparatus resulting in a more leak-proof, efficient communication between the master cylinder and the actuating cylinder, utilization of fewer parts, as well as permitting selective orientation of the actuating cylinder.

provides an intermediate retract position for reducing the cycle time during multiple weld operations.

Further objects and advantages of the present invention will become apparent from the following description and the appended claims, reference being made to the accompanying drawings forming a part of this specification, wherein like reference characters designate corresponding parts in several views.

Figure 1 is a perspective view that shows a preferred

present invention; Figure 2 is a top view of the preferred

of Figure 1; Figure 3 is a cross-sectional view taken along section lines 3-3 of Figure 2 showing the cylinders and pistons and their interrelationship to one another; Figure 4 is a part sectional view of the preferred

of Figure 1 as mounted to a mounting bracket; Figure 5 is a cross-sectional view showing the intensifier cap seal arrangement depicted in circle 5 of Figure 3; Figure 6 is a cross-sectional view showing the positions of the O-ring and backup ring arrangement of the actuating cylinder detailed in circle 6 of Figure 3; Figure 7 shows an

for nl o S apparalS - s alternativel6a-;;oSeene with the actuating cylinder in fluidic communication with the master cylinder by an external fluid connection to the end cap; Figure 8A is a cross-sectional view that shows the position of the pistons and piston rods in the fully retracted position; Figure 8B is a cross-sectional view that shows the position of the pistons and piston rods after pressure has been applied to the reservoir piston; Figure 8C is a cross-sectional view similar to that shown in Figures and 8B except that intensification has occurred; Figure 8D is a legend to the fluid pressures indicated in Figures 8A through 8C and Figures 13A and 13D;; Figure 9 is a part sectional view of an embodiment that employs a load cell near the end of the working piston rod; Figure 10 shows an alternate mounting arrangement with the actuating cylinder directly mounted to the master cylinder auxiliary port; Figure 11 is a schematic view that shows the valving system utilized with the present apparatus; Figure 12 is a cross-sectional view taken along section line 13-13 of Figure 12 showing the cylinders and pistons and their interrelationship to one another; Figure 13A is a cross-sectional view of the second embodiment that shows the position of the pistons and piston rods in the fully retracted position; Figure 13B is a cross-sectional view similar to that shown in Figure 13A showing the position of the pistons and piston rods after pressure has been applied to the retract piston;; Figure 13C is a cross-sectional view to that shown in Figure 13A and 13B showing the position of the pistons and piston rods after pressure has been applied to the reservoir piston; Figure 13D is a cross-sectional view similar to that shown in Figures 13A, 13B, 13C except that intensification has occurred; Figure 14 is a perspective view that shows another

Gor < oF apedratSs fr perFDr there LocI ombodimont 8H8; "C of to forgo inton=if'or of the present invention; Figure 15 is a cross-sectional side view of the intensifier shown in Figure 14, showing the pistons and their interrelationship to one another; Figure 16 is a cross-sectional view taken along section lines 3-3 of Figure 16 that shows the flat sections of the piston rod; Figure 17 is a part sectional view of an embodiment that employs a load cell near the end of the working piston rod; Figure 18 is a cross-sectional view of the embodiment shown in Figure 17 and which shows the position of the pistons and piston rods in the fully retracted position; Figure 19 is a cross-sectional view that shows the position of the pistons and piston rods after pressure has been applied to the reservoir piston;; Figure 20 is a cross-sectional view similar to that shown in Figures 21 and 22 except that intensification has occurred; and Figure 21 is a schematic view that shows the valving system utilized with the present apparatus.

Referring now to the drawings and more particularly to Figure 1, there is illustrated in perspective one configuration of the present load intensification apparatus. The overall apparatus is identified by the numeral 10. The overall apparatus 10 has two distinct subassemblies or housings which shall hereinafter be identified as the master cylinder 12 and the actuating cylinder 14. The master cylinder 12 is essentially a hollow structure with a front manifold 16, a center manifold 18, and an end cap 20 that are in spaced apart, axially aligned relationship to one another. A cylindrically shaped thin-walled front sleeve 22 is positioned between the front manifold 16 and the center manifold 18. A similar cylindrically shaped rear sleeve 24 is positioned between the center manifold 18 and the end cap 20.The master cylinder 12 is held together by studs 26 that pass through each one of the manifolds 16 and 18 and the end cap 20. The studs 26 are threaded on each end and tension thereon is maintained by threaded nuts 28.

The actuating cylinder 14 is cylindrical throughout its internal and external configuration. As shown in the preferred embodiment of Figure 1, the actuating cylinder 14 is directly mounted to the end cap 20 with threaded fasteners 40. While the actuating cylinder 14 is shown in a parallel attitude with respect to the master cylinder 12, it is readily understood that the orientation and positioning of the actuating cylinder 14 can be altered to fit any particular application by providing an auxiliary port 42 to the end cap 20. A fluidic connection 38 can then be used between the master cylinder 12 and the actuating cylinder 14, as shown as an alternative embodiment in Figure 7.

Further, if desired, the actuating cylinder 14 may be mounted directly to the end cap' s 20 auxiliary port 42 for a 90 direct mounting configuration as shown in Figure 10. Additionally, it is readily understood that this embodiment allows a single master cylinder 12 to control any desired number of actuating cylinders 14 in series or in parallel connection. Accordingly, the master cylinder 12 should be proportionally sized for the particular application.

Figure 3 is a cross-sectional view of the overall apparatus 10 that is depicted in Figure 1. Figure 3 shows the pistons and their interrelationship to one another in an at rest condition. The front sleeve 22 may, if desired, have the same overall dimensions as the rear sleeve 24. The front and rear sleeves 22 and 24 are preferably manufactured from steel. The leading end 48 of the front sleeve 22 fits over a machined boss 50 on the front manifold 16. Even though close tolerances are maintained between the inside diameter of the front sleeve 22 and the outside diameter of the boss 50, it is desirable to utilize an O-ring 52 for sealing purposes.

The trailing end 54 of the front sleeve 22 fits over a machined boss 56 on the center manifold 18. An O-ring 58 is utilized between the machined boss 56 and the interface with the front sleeve 22 to ensure a fluid tight joint. The leading end 60 of the rear sleeve 24 fits over a machined boss 62 on the center manifold 18.

An O-ring 64 is positioned so that it affects a fluid tight seal between the inside surface of the rear sleeve 24 and the machined boss 62. The trailing end 66 of the rear sleeve 24 fits over a machined boss 68 on an annular manifold member 72. An O-ring 70 is used to ensure a fluid tight seal between the inside surface of the rear sleeve 24 and the machined boss 68. The end cap 20 is attached to the trailing end of the annular manifold member 72. A first O-ring 74 ensures a fluid tight seal between the perimeter of the annular manifold member 72 and the end cap 20. A second O-ring 76 is utilized to maintain a fluid tight seal between a reduced portion of the annular manifold member 72 and the end cap 20. The annular manifold member 72 has a bore 78 that contains a groove 80 therein for an elastomeric seal 82 retained by a retainer cap 81, as best illustrated in Figure 5.The purpose of the reduced diameter bore 78 will be discussed in more detail below.

An intensifier piston 104 is positioned within a bore 106 in the front sleeve 22. The intensifier piston 104 is sealed against the bore 106 by means of an O-ring 108. An intensifier piston rod 110 is centrally attached to the intensifier piston 104 by a threaded fastener 118. The intensifier piston rod 110 passes through a bore 120 that is located in the center manifold 18. A groove 122 within the bore 120 carries an O-ring 124 provided as a seal between the center manifold 18 and the intensifier piston rod 110.

An annular-shaped floating reservoir piston 132 is positioned over the intensifier piston rod 110. A portion of an inner surface 126 of the floating reservoir piston 132 is elongated and tapered to closely mate with a frustoconically shaped portion 128 of the annular manifold member 72. The reservoir piston 132 is positioned within a bore 134 within the rear sleeve 24.

The floating reservoir piston 132 is sealed against the surface of the bore 134 by means of a leading end O-ring 136 and a trailing end 0ring 138, located in grooves 140 and 142, respectively, in the floating reservoir piston 132. The floating reservoir piston 132 is also sealed against the intensifier piston rod 110 along which it slides by O-rings 144 and 146 which seal the floating reservoir piston 132 against the intensifier rod 110 on opposite sides of a relief passage 148 within the floating reservoir piston 132.The relief passage 148 places the area between the leading and trailing end O-rings 136 and 138 on the perimeter of the floating reservoir piston 132 and the area between the O-rings 144 and 146 adjacent the intensifier piston rod 110 in fluid communication, thus preventing the build up of residual pressure between the leading and trailing end O-rings on the floating reservoir piston 132. The arrangement of the floating reservoir piston 132 on the intensifier piston rod 110 within the rear sleeve creates two fluid chambers 152 and 154 within the area of the rear sleeve 24. The fluid chamber 152 lies between the annular manifold member 72 and the internal surface 126 of the floating reservoir piston 132. The fluid chamber 154 lies between the center manifold 18 and a recess in the leading face of the floating reservoir piston 132.

The front manifold 16 contains a fluid chamber 156 and a threaded bore 160. An additional fluid chamber 162 lies between the intensifier piston 104 and the center manifold 18. The center manifold 18 contains a first bore or port 86 that is in communication with the chamber 154. A second bore or port 164 is in communication with the additional fluid chamber 162.

The end cap 20 contains a bore 168 that is in communication with the chamber 152 through the reduced diameter bore 78 in the annular manifold chamber 72. In addition, the end cap 20 has a supply port 90 which is also in fluidic communication with the chamber 152 via a supply passage 92 in the annular manifold member 72. A reservoir 94, positioned in any convenient location, is fluidically connected to the supply port 90 for purposes of supplying the chamber 152 with hydraulic fluid. A one-way check valve 96 is positioned between the reservoir 94 and the supply port 90 to allow fluid to be supplied to the chamber 152 and also to prevent backflow from the chamber 152 to the reservoir 94.

The actuating cylinder 14 has an external cylindrical configuration over its axial extent. The rear portion of the actuating cylinder 14 has a bore 174 that is threaded (not shown) for communication with the bore 168 of the end cap 20. The interior of the actuating cylinder 14 is formed by an axial bore 176 that extends over approximately the rear one half of the actuating cylinder 14. The remaining or forward one half of the interior of the actuating cylinder 14 is formed by an axially extending bore 178 that is of greater diameter than the axial bore 176 of the rear half of the actuating cylinder. A radially extending shoulder 180 forms the intersection between the bores 176 and 178. A sleeve 182 is positioned within the bore 178 of the actuating cylinder 14. The shoulder 180 acts as a stop for the sleeve 182 thus defining its axial position within the actuating cylinder 14.

A rear piston 184 is positioned within the bore 176.

The rear piston 184 has a first O-ring seal and backup rings 185 positioned within a groove 187, and a second O-ring seal 186 positioned within a groove 188 located in the cylindrical exterior surface of the rear piston 184 as more clearly shown in Figure 6. A piston rod 46 has one end thereof attached to the rear piston 184.

The piston rod 46 has a reduced diameter end 192 with a threaded portion (not shown) that extends through an axially aligned bore 194 in the rear piston 184. The rear piston 184 is attached to the piston rod 46 by means of a threaded nut 196 that engages the threaded portion threads (not shown) on the end of the reduced diameter end 192 of the piston rod 46. The piston rod 46 extends from the rear piston 184 through the entire axial extent to the right, as viewed in Figure 3, where it exits the actuating cylinder 14 as an unencumbered cantilevered end 198.

Returning once again to the actuating cylinder 14, a forward piston 200 is press fit onto the piston rod 46.

The forward piston 200 is located generally toward the mid-portion of the axial extent of the piston rod 46.

The forward piston 200 has a peripheral groove 202 that contains an O-ring 204. The sleeve 182 accommodates the forward piston 200 within a bore 206 of the sleeve 182.

The O-ring 204 seats against the surface of the bore 206. The sleeve 182 contains a second bore 212 that permits the piston rod 46 to pass therethrough, forming a chamber 210 between the forward piston 200 and the shoulder formed between the bore 206 and the second bore 212. The second bore 212 contains a groove 214 in which an O-ring 216 is positioned for providing a seal between the sleeve 182 and the piston rod 46. The sleeve 182 contains a groove 218 positioned in its external surface so that an 0ring 220 can be placed therein to effect a seal between the sleeve 182 and the bore 178 of the actuating cylinder 14.

The section of the piston rod 46 located to the right of the forward piston 200, as viewed in Figure 3, has a diameter that is less than the bore 206 of the sleeve 182, thus forming a chamber 222. A chamber 222 is in communication with a central bore 226 through the rear portion of the piston rod 46 by way of a radial passage in the piston rod 46. In a similar manner, the rear piston 184 has a radial bore 228 extending between the O-ring seals 185 and 186 that is in communication with the central bore 226. A chamber 231, which is positioned to the right of the rear piston 184, is in communication with a passage 232 in the sleeve 182.A chamber 236, located to the left of the rear piston 184 as viewed in Figure 3, is in communication with the fluid chamber 152 of the master cylinder 12 via the bore 174 of the actuating cylinder 14, the passage 168 in the end cap 20, and the bore 78 in the annular manifold member 72.

A retaining bushing 44 is mounted to the forward portion of the actuating cylinder 14 and has an external part cylindrical section 240 that fits into the bore 178 to establish the chamber 222. The retaining bushing 44 is immobilized by means of a retaining ring 242 that coacts with a groove 244 in the wall of the bore 178 in the actuating cylinder 14 and with a groove 246 that is milled in the external surface of the external part cylindrical section 240.

As can be better seen in Figure 1, the piston rod 46 contains a milled planar area 248 on one side and a similar milled planar area 250 on the other side thereof which is optional. The purpose of the milled planar areas 248 and 250 is to provide orientation to the piston rod 46 so that it will not rotate and cause misalignment with a non-symmetrical tool that may be affixed to the cantilevered end 198 of the piston rod 46.

Figure 4 is a part sectional view of an embodiment that employs a trunnion 254 as an integral part of the actuating cylinder 14. Figure 4 shows the trunnion 254 engaged with mounting slots 256 within a mounting bracket 258. This arrangement allows the actuating cylinder 14 to be pivo-ted to the preferred attitude for a particular application.

Figure 9 is a part sectional view of an embodiment that employs a load cell device within the piston rod 46 of the actuating cylinder 14. Figure 9 shows the sleeve 182, the piston rod 46 and the retaining bushing 44 similar to like components shown in Figure 3. The piston rod 46 has a reduced diameter cylindrical section 30. The reduced diameter cylindrical section 30 telescopes within a piston rod adapter 32. The piston rod adapter 32 has an external cylindrical surface that fits within a bore 34 in the retaining bushing 44. The piston rod adapter 32 has an internal bore 36 into which the telescoping end of the piston rod 46 fits. A load cell 35 is positioned within the bore 36 and a compression spring 37 is aligned within the bore 36 between the end of the piston rod 46 and the load cell 35.In order to retain the piston rod adapter 32 on the end of the piston rod 46, a pin 33 is installed in a bore 31 that is diametrically aligned with respect to the piston rod 46. The pin 33 protrudes beyond the external surface of the reduced diameter cylindrical section 30. The ends of the pin 33 fit into slots 29 that are milled into the piston rod adapter 32. In this manner, the piston rod adapter 32 has a limited degree of axial movement with respect to the piston rod 46.

The piston rod adapter 32 has a radially aligned bore 39 that permits electrical lead wires 41 of the load cell 35 to exit the interior of the piston rod adapter 32.

During operation of the overall apparatus the piston rod 46 causes the compression spring 37 to exert a force on the load cell 35. After the load has been released from the load cell, the compression spring 37 will cause the piston rod adapter 32 to move axially subject to the constrains of the pin 33 and the slots 29.

During the assembly of the overall apparatus 10, great care must be taken to preserve the integrity of the seals, particularly the O-rings which are subject to the nicks caused by assembly. The master cylinder is assembled by installing the appropriate seals on the reservoir piston 132 and the intensifier piston 104.

The intensifier piston 104 is affixed to the end of the intensifier piston rod 110 by the threaded fastener 118. The intensifier piston rod 110 is then inserted through the bore 120 in the center manifold 18. The reservoir piston 132 is then slid over the free end of the intensifier piston rod 110. The front and rear sleeves 22 and 24 are then installed over the respective bosses 56 and 62 on the center manifold 18. The front manifold 16 and the annular manifold member 72 are then positioned so that their respective bosses 50 and 68 slide within the ends of the front and rear sleeves 22 and 24. The end cap 20 is then positioned against the annular manifold member 72, aligning the bore 168 with the reduced diameter bore 78 and the supply port 90 with the supply passage 92. The four studs 26 are then installed in the holes (not shown) within the front and center manifolds 16 and 18 and the end cap 20. The studs 26 are then tensioned by the installation of the nuts 28.

During the assembly of the actuating cylinder 14, the forward piston 200 is press fit onto the piston rod 46 as seen in Figure 3, the fit being an interference fit.

The sleeve 182 is then positioned over the left end (as viewed in Figure 3) of the piston rod 46. Next, the rear piston 184 is affixed to the end of the piston rod 46 by the nut 196. The rear piston 184, the piston rod 46 and the sleeve 182 are installed within the bores 176 and 178 of the actuating cylinder 14. The retaining bushing 44 is then slid over the cantilevered or free end 198 of the piston rod 46. The retaining bushing 44 is then moved into locking arrangement with the retaining ring 242. The actuating cylinder 14 is then mounted to the end cap 20 with the threaded fasteners 40 Figure 8A is a cross-sectional view that shows the position of the pistons and piston rods when the overall apparatus 10 is in the fully retracted position.At the commencement of a cycle of the overall apparatus 10, the intensifier piston 104 is held to the extreme right end of the chamber 162 by high air pressure, as shown, through the bore 120 and its external port.

Consequently, the end of the intensifier piston rod 110 is retracted to a position outside of the bore 78 permitting the fluid chamber 152 to communicate with the bore 78. The reservoir piston 132 is to the extreme right end of travel against the center manifold 18. In the actuating cylinder 14 portion of the overall apparatus 10, the rear piston 184 is positioned toward the extreme left toward the end cap 20 defining the greatest extent of the chamber 231, therefore, the extreme right free end of the piston rod 46 is almost entirely retracted within the confinement of the actuating cylinder 14. The forward piston 200, acting as an integral part of the piston rod 46, is positioned against the shoulder defined by.the bores 212 and 206.

Figure 8B is a cross-sectional view that shows the position of the pistons and piston rods after the overall apparatus 10 has been actuated to begin a work cycle. Air pressure is introduced to the fluid chamber 154 through the first bore 86 causing the reservoir piston 132 to move toward the left. The oil to the left of the reservoir piston 132 begins to exit the fluid chamber 152 and, being prevented from returning to the reservoir 94 by the check valve 96, travels via the reduced diameter bore 78 and the bore 168 into the chamber 236. The increase in volume of oil in the chamber 236 causes the rear piston 184 to move rapidly to the right. As the rear piston moves toward the right, air is exhausted from the chamber 231 through the passage 232.Since the forward piston 200 acts as a part of the piston rod 46, the forward piston 200 also moves toward the right thus causing an ingress of atmospheric air into the chamber 210 and an egress of atmospheric air from the chamber 222. After the initial introduction of air pressure to the fluid chamber 154 at the right of the reservoir piston 132 there is a rapid deployment of the piston rod 46 to the right where its travel is halted by an interception with, for example, a workpiece 47.

It has been determined through experimentation that performance characteristics may be diminished if the forward piston 200 is driven toward the right by introducing air pressure into the chamber 210 during the commencement of the cycle illustrated in Figure 8B. The cause for this loss in performance is believed to be the result of a "sucking action" created when the forward piston 200, as a result of air pressure introduced into the chamber 210, begins to travel before or travels at a faster rate than the reservoir piston 132, thereby forming a partial vacuum in the chamber 236. This in turn provides an additional force that compels the reservoir piston 132 to travel to the left faster than intended by the action of the air pressure in the fluid chamber 154.

Figure 8C is a cross-sectional view similar to that shown in Figures 8A and 8B that shows the final stage of the work cycle of the overall apparatus 10. Since rapid deployment of the piston rod 46 has brought a tool (not shown) carried by it into contact with the workpiece 47, the load must be increased beyond the capability of the air pressure normally found at an industrial site.

Consequently, air pressure is introduced into the chamber 156 which is positioned to the right of the intensifier piston 104. As the intensifier piston 104 moves to the left, the tip of the intensifier piston rod 110 enters the bore 78 in the annular manifold member 72, causing the oil trapped before it to act as a closed loop system between the intensifier rod 110, the bore 78, and the chamber 236. The continued travel of the intensifier piston rod 110 into the bore 78 acts on the oil in the chamber 236 urging the rear piston 184 to the right, delivering a greatly increased or intensified force to the piston rod 46. The actual movement of the piston rod 46 has been exaggerated in Figure 8C for purposes of illustrating the movement thereof.The increased movement of the forward piston 200 to the right will exhaust additional atmospheric air from the chamber 222 and cause an influx of additional atmospheric air into the chamber 21. Thus, there will be a combined hydraulic intensifying force introduced to the piston rod 46.

On the return stroke, both the intensifier piston 104 and the rear piston 184 are driven back to their original positions by introducing high pressure air into their respective chambers 162 and 231 through the bore 164 and the passage 232. The return stroke of the rear piston 184 acts to return the reservoir piston 132 to its original position to the right end of the fluid chamber 152 against the center manifold.

As an added feature to ensure adequate performance of the apparatus 10, there is provided a proximity sensor 252 for sensing the position of the reservoir piston 132 in relation to the extreme left end of the fluid chamber 152. As shown in Figure 3, the proximity sensor 252 is located adjacent the extreme left end of the fluid chamber 152 and can be instrumented through any conventional means to relay a warning signal when the reservoir piston 132 is approaching the end of its stroke capability within the fluid chamber 152. This condition would arise if, for example, the hydraulic fluid within the fluid chamber 152 has dropped to an unacceptable level. By way of a warning signal, an operator of the apparatus 10 is put on notice that replenishment of the hydraulic system is necessary.

Figure 11 is a schematic fluid diagram according to the present invention and the control that achieve the fluid motion. For purposes of the present invention the fluids have been described as air and oil. Figure 11 shows a simplified layout of the pistons and piston rods. Since the oil within the overall apparatus 10 is self-contained, the oil has been shown for clarity as shaded. In order to operate the overall apparatus through its entire work cycle, only external air pressure need be applied. For purposes of explanation, it is assumed the overall apparatus 10 is coupled to an air supply 272. Air under pressure is supplied to a three-way valve mechanism 274 which is a solenoid actuated spring return device. The air under pressure exists the air supply through a line 276 and travels through the three-way valve mechanism 274 to a line 278 and to the chamber 231.The air supply 272 also supplies air under pressure to a line 304 through a two-way valve mechanism 288 to the chamber 162. The pressure supplied to the chamber 231 causes the rear piston 184 to move to the left as viewed in Figure 8A forcing the oil from the chamber 236 into the fluid chamber 152 and urging the floating reservoir piston 132 to the right. As the floating reservoir piston 132 moves to the right, air is exhausted from the fluid chamber 154 through a line 282 to the valve mechanism 274 which permits the expelled air to enter a line 284 and travel to an exhaust port 286 which may, if desired, be a device such as a muffler to attenuate the noise level of the exhausting air.The air pressure delivered via a line 280 to the chamber 162 causes the intensifier piston 104 to remain to the right, ensuring that the tip of the intensifier piston rod 110 does not impede the flow of oil into the fluid chamber 152. The chamber 156 is connected to the two-way valve mechanism 288 by a line 290. In the unenergized position, the two-way valve mechanism 288 permits the exhaust air from the line 290 to enter a line 292 and pass to the exhaust port 286. At the start of the cycle, a solenoid 294 on the three-way valve mechanism 274 is energized by the movement of a workpiece into a work station or by other means that connects to an electrical source to the solenoid.The energizing of the solenoid 294 connects the air supply line 276 to the line 282 pressurizing the fluid chamber 154 which causes the floating reservoir piston 132 to move to the left, forcing oil from the fluid chamber 152 into the chamber 236. Oil entering the chamber 236 causes the rear piston 184 to move rapidly to the right, hence the piston rod 46 moves to the right along with the forward piston 200. The energizing of the solenoid 294 on the three-way valve mechanism 274 also causes the air supply line 278 to the chamber 231 to become connected to the exhaust line 284. As the forward piston 200 moves to the right, air is exhausted from the chamber 222 through a line 295 and air from the exhaust port 286 is drawn through a line 296 to the chamber 210.After the piston rod 46 has made its rapid advance toward and against a workpiece such as is identified by numeral 298, the pressure, or an electrical sensing switch such as 300, energizes a solenoid 302 on the two-way mechanism 288 causing the line 304 to be reversed and connected to the pressure line and the line 280 to the exhaust line 292. The air pressure delivered by the line 290 to the chamber 156 causes the intensifier piston 104 to move to the left thus permitting the tip of the intensifier rod 110 to enter the bore 78 and apply an intensified pressure on the oil in the chamber 236. The increased force supplied to the rear piston 184 is transferred to the piston rod 46 and to the workpiece 298.As the command of an operator or by automatic timing, the solenoids 294 and 302 are de-energized, permitting springs 306 and 308 to return the valve mechanism 274 and 288 to their original starting positions. It is to be noted that by utilizing air to hold the intensifier piston positively in place while the floating reservoir piston is subjected to air pressure avoids the need for using springs and results in a more positive control of the intensifier pistons. It is also to be noted that appropriate bleed passages are provided, as is customary in the art, between cooperating seals to prevent the buildup of residual pressures due to blow by.

By way of illustration, the intensifier piston rod 110 has a diameter of 0. 5 inches and the intensifier and rear pistons 104 and 184 each have a diameter of 1. 75 inches. The increase in the pressure delivered to the rear piston 184 varies as the square of the diameter, 1. 75 squared divided by 0. 5 squared yields a pressure increase of 12. 25. Thus, if typical shop air at 80 p. s. i. is delivered to the intensifier piston, there will be 980 p.s.i. delivered to the rear piston 184.

In a second embodiment of the present invention, Figure 12 illustrates a load intensification apparatus identified by numeral 410. The load intensification apparatus 410 of the second embodiment is distinguished from the load intensification apparatus 10 of the first embodiment by the provisicn of an intermediate retract position capability. As will be readily seen, the intermediate retract position facilitates multiple weld operations by reducing the cycle time between successive welds which do not require the full clearance provided by the full retract position of the overall apparatus 410.

In a manner similar to the first embodiment, Figure 12 shows the overall apparatus 410 of the second embodiment having a master cylinder 412 and an actuating cylinder 414 which together constitute two distinct subassemblies or housings of the overall apparatus 410. The overall apparatus 410 of the second embodiment is constructed nearly identically to the overall apparatus 10 of the first embodiment except for specific modifications to the master cylinder 412 which will be delineated below.

Similar to the first embodiment, the master cylinder 412 of the second embodiment has a front manifold 416, a center manifold 418, and an annular manifold member 472 which are in spaced-apart, axially-aligned relationship to one another. Cylindrically-shaped front and rear sleeve 422 and 424 are positioned between the front and center manifold 416 and 418, and the center manifold and annular manifold member 418 and 472, respectively. The front and rear sleeves 422 and 424 form a front bore 506 and a rear bore 534, respectively. Within the rear bore 534 there is provided a retaining ring 538 within an internal groove 540 which is positioned approximately midway between the annular manifold member 472 and the center manifold 418. The retaining ring 538 is of sufficient strength to act as a piston stop in a manner to be described later.

The annular manifold member 472 has an elongated annular portion 473 with an outer cylindrical surface 528 extending towards the center manifold 418. The interior surface of the elongated annular portion 473 provides a reduced diameter bore 478. An end cap 420 is mounted to the annular manifold member 472 on a side opposite the elongated annular portion 473. The end cap 420 has a bore 568 that is in communication with the reduced diameter bore 478 of the annular manifold member 472.

As with the first embodiment, the second embodiment has an intensifier piston 504 which is attached to an intensifier piston rod 510 and is positioned within the front bore 506. The intensifier piston 504 divides the front bore 506 into a first chamber 556 adjacent the front manifold 416, and a second chamber 562 adjacent the center manifold 418. The first chamber 556 is in fluidic communication with a port 560 in the front manifold 416. The second chamber 562 is in fluidic communication with a port 564 within the center manifold 418. The intensifier piston rod 510 passes through a bore 520 located in the center manifold 418 and extends short of the reduced diameter bore 478 of the annular manifold member 472.

Similar to the first embodiment, a floating reservoir piston 532 of the second embodiment is positioned over the intensifier piston rod 510 within the rear bore 534. The floating reservoir piston 532 divides the rear bore 534 into a third chamber 554 adjacent the center manifold 418, and a fourth chamber 552 adjacent the annular manifold 472. The third chamber 554 is in fluidic communication with a port 486 in the center manifold 418. The fourth chamber 552 is in fluidic communication with the reduced diameter bore 478 of the annular manifold member 472 and the bore 568 of the end cap 420. The end cap 420 also is provided with a supply port 490 which is in fluidic communication with the rear bore 534 through a supply passage 492 in the annular manifold 472.

In contrast to the first embodiment, the floating reservoir piston 532 is truncated and does not mate with the cylindrical surface 528 of the annular manifold member 472. Instead, the floating reservoir piston 532 is retained within the rear bore 534 between the center manifold 418 and the retaining ring 538.

In addition, in the second embodiment a retract piston 536 which is positioned over the outer cylindrical surface 528 of the annular manifold member 472 is provided. The retract piston 536 defines a retract chamber 553 within the rear bore 534 between the annular manifold member 472 and the retract piston 536. The retract piston 536 operates between the annular manifold member 472 and the retaining ring 538 such that the retract piston 536 always remains piloted upon the outer cylindrical surface 528 of the annular manifold member 472. Further, the retract piston 536 is constructed such that it cannot interrupt the fluidic path between the forth chamber 552 and the reduced diameter bore 478. The retract chamber 553 is in communication with the supply port 490 via the supply passage 492 for purposes of actuating the retract piston 536.

Similar to the first embodiment, a proximity sensor 652 is provided for sensing the position of the floating reservoir piston 532 in relation to the retaining ring 538. The proximity sensor 652 serves to warn an operator that the quantity of hydraulic fluid within the fourth chamber 552 is low and needs replenishing. The hydraulic fluid is introduced into the fourth chamber 552 through a fill port 542 positioned in proximity to the retaining ring 538.

The actuating cylinder 414 is constructed identically to the actuating cylinder 14 of the first embodiment. As shown, the actuating cylinder 414 is mounted to the end cap 420, but as noted with the first embodiment, the actuating cylinder 414 can be fluidically connected to the end cap 420 with a suitable fluidic connection. The rear portion of the actuating cylinder 414 has a bore 576 that is in fluidic communication with the bore 568 of the end cap 420. A rear piston 584 is positioned within the bore 576. The rear piston 584 is attached to a piston rod 446 which extends from the rear piston 584 through the entire axial extent to the right, where it exists the actuating cylinder 414 as an unencumbered cantilevered end 598.

The rear piston 584 divides the bore 576 into a fifth and sixth chamber 631 and 636, respectively. The sixth chamber 636 is in communication with the fourth chamber 552 of the master cylinder 412 via the passage 568 in the end cap 420 and the reduced diameter bore 478 in the annular manifold member 472.

Operation of the second embodiment is nearly identical to the first embodiment except for the ability of the force intensification apparatus 410 to reach an intermediate retract position from either the fully extended position. Figure 13A is a cross-sectional view that shows the position of the pistons and piston rods when the overall apparatus 410 is in the fully retracted position. At the commencement of a cycle, the intensifier piston 504 is held to the extreme right end of the front bore 506 by high pressure air in the second chamber 562, as shown. Consequently, the end of the intensifier piston rod 510 is retracted to a position outside of the reduced diameter bore 478 permitting the fourth chamber 552 to communicate with the reduced diameter bore 478. The floating reservoir piston 532 is to the extreme right end of its travel against the center manifold 418.The retract piston 536 is to the extreme left end of its travel against the annular manifold member 472.

In the actuating cyclinder 414, the rear piston 584 is held by high pressure air to the extreme left toward the end cap 420 defining the greatest extent of the fifth chamber 631. Therefore, the extreme right free end of the piston rod 446 is almost entirely retracted within the confinement of the actuating cylinder 414.

Figure 13B is a cross-sectional view that shows the position of the pistons and piston rods after the overall apparatus 10 has been actuated to the intermediate retract position at the start of a work cycle. Air pressure is introduced into the retract chamber 553 through the supply port 490, causing the retract piston 536 to move toward the center manifold 418 until it abuts against the retaining ring 538. A volume of oil corresponding to the volume displaced by the retract piston 536 exits the fourth chamber 552 and travels via the reduced diameter bore 478 and the bore 568 to the sixth chamber 636. The increase in volume of oil in the sixth chamber 636 causes the rear piston 584 to move rapidly to the right. Consequently, there is a rapid deployment of the piston rod 446 to the right where its travel is arrested a predetermined distance from a workpiece 447, serving as an intermediate retract position for the overall apparatus 410. The predetermined distance travelled by the piston rod 446 is determined directly by the volume of oil displaced by the retracted piston 536.

Figures 13C is a cross-sectional view that shows the position of the pistons and piston rods after the overall apparatus 410 has been actuated to engage the workpiece 447. Figures 13C corresponds to Figure 8B of the first embodiment, and the operation of the overall apparatus 410 corresponds accordingly. Air pressure is introduced to the third chamber 554 causing the floating reservoir piston 532 to move to the left toward the retract position 536. An additional volume of oil corresponding to the volume displaced by the floating reservoir piston 532 exists the fourth chamber 552 and travels via the reduced diameter bore 478 and the bore 568 into the sixth chamber 636, further causing the rear piston 584 to mover rapidly to the right. The piston rod 446 consequently moves rapidly to the right where its travel is halted by its interception with the workpiece 447.

Figure 13D is a cross-sectional view corresponding to Figure 8C of the first embodiment, showing the final stage of the work cycle of the overall-apparatus 410.

For achieving force intensification at the piston rod 446, air pressure is introduced into the first chamber 556 to the right of the intensifier piston 504. As the intensifier piston 504 moves to the left, the tip of the intensifier piston rod 510 enters the reduced diameter bore 478 in the annular manifold member 472, causing the oil trapped before it to act as a closed system between the intensifier rod 510, the bore reduced diameter 478, the bore 568 and the sixth chamber 636. The continued travel of the intensifier piston rod 510 into the reduced diameter bore 478 acts on the oil in the sixth chamber 636 urging the rear piston 584 to the right, delivering a greatly increased or intensified force to the piston rod 446.

According to the second embodiment of the present invention, the overall apparatus 410 does not automatically return to the fully retracted position shown in Figure 13A, but returns to the intermediate retract position shown in 13B for purposes of facilitating rapid successive weld operations. To return the overall apparatus 410 to the intermediate retract position from the intensified position, air pressure is released from the first chamber 556 and re-introduced in the second chamber 562 to drive the intensifier piston 504 back to its original position.

Consequently, the intensifier piston rod 510 is withdrawn from the reduced diameter bore 478, simultaneously reduced the pressure against the rear piston 584 in the sixth chamber 636. The floating reservoir piston 532 is driven back to its original position by the partial return stroke of the rear piston 584 in cooperation with the releasing of the high pressure air from the third chamber 554 which has originally moved and held the floating reservoir piston 532 in its actuated position. The rear piston 584 and, therefore, the piston rod 446, is retracted to the intermediate retract position upon the floating reservoir piston 532 being returned to its original position. The rear piston 584 and the piston rod 446 retract no further because of the volume of oil yet displaced by the retract piston 536.

At the end of a multiple weld operation, the operation of the overall apparatus 410 is again similar to the overall apparatus 10 of the first embodiment. From the intermediate retract position, air pressure is re-introduced into the fifth chamber 631, driving the rear piston 584 back to its original position. Upon release of the high pressure air in the retract chamber 553 which had originally moved and held the retract piston 536 in its actuated position, the retract piston 536 is returned to its original position adjacent the annular manifold 472 by the return stroke of rear piston 584.

From the above, it can be appreciated that rapid successive weld operations can be accomplished more quickly by eliminating the first embodiment' s requirement for a complete retraction of the piston rod 446 between weld operations. The overall apparatus 410 under the second embodiment can rapidly perform a successive number of weld operations by first extending to the intermediate retract position (Figure 13B), further extending to the weld position (Figure 13C), intensifying during the weld operation (Figure 13D), partially retracting to the intermediate retract position (Figure 13B) which is designed to sufficiently clear the workpiece 447, and then return to the weld position (Figure 13D) for an additional intensification and weld operation.When the desired series of weld operations is completed, the overall apparatus can then be cycled directly from the intermediate retract position (Figure 13B) to the full retract position (Figure 13A) for purposes of providing maximum clearace with the workpiece 447.

A fluid control system for the second embodiment of the present invention would be analogous to the schematic fluid diagram of the first embodiment illustrated in Figure 11. Those with ordinary skill in the art can readily recognize the minor modifications necessary to accommodate the operational requirements of the retract piston 536. By example, a solenoid-operated valve can be employed to operate the retract piston 536 between its "stowed" position when the piston rod 446 is fully retracted, and its "deployed" position when the piston rod 446 is at the intermediate retract, weld and intensified positions. In addition, the three-way valve mechanism 274 of the first embodiment can be modified to provide a valve position in which both lines 282 and 278 are exhausted to the exhaust port 286 when the overall apparatus is in the intermediate retract position.

In a third embodiment of the present invention, Figure 14, illustrates in perspective one configuration of the present load intensification apparatus. The overall apparatus is identified by the numeral 10'. The overall apparatus 10' has two distinct subassemblies or housings which shall hereinafter be identified as the master cylinder 12' and the actuating cylinder 14'. The master cylinder 12' is essentially a hollow structure with a front manifold 16', a center manifold 18' and a rear manifold 20' that are in spaced apart, axially aligned relationship to one another. A cylindrically shaped thin-walled front sleeve 22' is positioned between the front manifold 16' and the center manifold 18'. A similar cylindrically shaped rear sleeve 24' is positioned between the center manifold 18' and the rear manifold 20'. The master cylinder 12' is held together by studs 26' that pass through each one of the manifolds 16', 18' and 20'. The studs 26' are threaded on each end and tension thereon is maintained by threaded nuts 28'. A viewing tube 30' for the hydraulic fluid contained within the master cylinder 12' spans the distance between the center manifold 18' and the rear manifold 20'. A nipple 32' is positioned in axial alignment with the viewing tube 30' and a quick disconnect fitting 34 is coupled to the cantilevered end of the nipple 32'. The quick disconnect fitting 34' provides for easy access to the hydraulic system should the addition of hydraulic fluid becomes necessary.

A compression fitting 90' elbow 36' is attached to the rear manifold 20'. The elbow 36' is in turn coupled with an elastomeric tube 38' that is made of urethane or other suitable material that can withstand contact with hydraulic oil and reasonable pressures generated thereby. The elastomeric tube 38' is coupled to a straight compression fitting 40'.

The actuating cylinder 14 is essentially cylindrical throughout its internal and external configuration and at the back end is a tapped hole to accept the compression fitting 40'. The front end of the actuating cylinder is supported by a mounting plate 42'. The mounting plate 42' is cantilevered in a downward direction from its rigid support on the front manifold 16'. While the actuating cylinder 14 is shown in a parallel attitude with respect to the master cylinder 12', it is readily understandable that the flexible nature of the elastomeric tube 38', as well as its selectable varying length permits orientation or positioning of the actuating cylinder 14 to assume any location with respect to the master cylinder 12' A retaining bushing 44' is attached to the front end of the actuating cylinder 14'.The retaining bushing 44' permits the end of a piston rod 46' to protrude therefrom. By way of example, a tool 47' such as an electrode for welding purposes can be affixed to the cantilevered end of the piston rod 46.

Figure 15 is a cross-sectional view of the overall apparatus 10 that is depicted in Figure 47. Figure 14 shows the pistons and their inter-relationship to one another. The front sleeve 22' can, if desired, have the same overall dimensions as the rear sleeve 24'. The front and rear sleeves 22' and 24' are preferably manufactured from steel. The leading end 48 of the front sleeve 22' fits over a machined boss 50' on the front manifold 16'. Even though close tolerances are maintained between the inside diameter of the front sleeve 22' and the outside diameter of the boss 50', it is desirable to utilize an 0-ring seal 52'. The trailing end 54' of the front sleeve 22' fits over a machined boss 56' on the center manifold 18'. An 0-ring 58' is utilized between the boss 56' and the interface with the front sleeve 22' to ensure a fluid tight joint.The leading end 60' of the rear sleeve 24' fits over a machined boss 62' on the center manifold 18'. An 0-ring 64' is positioned so that it effects a fluid tight seal between the inside surface of the rear sleeve 24' and the boss 62'. The trailing end 66' of the rear sleeve 24' fits over a machined boss 68' on the rear manifold 20'. An 0-ring 70' is used to ensure a fluid tight seal between the inside surface of the rear sleeve 24' and the boss 68'.

An end cap 72' is attached to the trailing end of the rear manifold 20'. The end cap 72' has a threaded section that engages similar threads in an axially aligned bore 74' in the rear manifold 20'. An 0-ring 76' is utilized to maintain a fluid tight seal between the end cap 72' and the rear manifold 20'. The end cap 72' has a reduced diameter bore 78' that contains a groove 80' for an elastomeric seal 82'. The purpose of the reduced diameter bore 78' will be discussed in more detail below.

The center manifold 18' has a 90 elbow fitting 84' threadedly engaged in an upper threaded bore 86'. The elbow fitting 84' has its non-threaded end 88' directed toward the left or toward the rear manifold 20'. A tee fitting 90' has its stem end 92' threadedly engaged within a threaded lower bore 94' in the rear manifold 20'. The lower bore 948 is located on the top of the rear manifold 20'. The top of the tee fitting 90' is aligned so that its axis is parallel with the longitudinal axis of the master cylinder 12'. The viewing tube 30' is aligned between the tee fitting 901 and the end 88' of the elbow fitting 84'. 0-ring seals 96' and 98 effect seals at the leading and trailing ends 100' and 102' of the viewing tube 30' with the respective elbow fitting 84' and tee fitting 90'.The viewing tube 30' can be fabricated from tempered glass tubing or high strength plastic material. The nipple 32' is threadedly attached to the end of the tee fitting 90' and the quick disconnect fitting 34' is attached to the nipple 32'. Thus, the quick disconnect fitting 34t, the nipple 32', and the viewing tube 30' are in axial alignment with one another.

An intensifier piston 104' is positioned within a bore 106' in the front sleeve 22'. The intensifier piston 104 is sealed against the bore 106' by means of an 0-ring 108'. An intensifier rod 110' is centrally attached to the intensifier piston 104'. A reduced diameter end 112' of the intensifier rod 110' is positioned within a bore 114' in the intensifier piston 104'. The intensifier piston 104' abuts against a shoulder 116' on the intensifier rod 110'. The shoulder 116' is formed by the reduced diameter end 112'. The intensifier piston 104 is immobilized by the attachment of a nut 118' to a threaded portion of the reduced diameter end 112'. The intensifier rod 110' passes through a bore 120' that is located in the center manifold 18'.A groove 122' within the bore 120 carries an O-ring 124' providing for a seal between the center manifold 18' and the intensifier rod 110'. The intensifier rod 110' also passes through a bore 126' that is located within the rear manifold 20'. A seal is maintained between the rear manifold 20 and the intensifier rod 110' by means of an O-ring 128' that is positioned within a groove 130' in the wall of the bore 126' A floating reservoir piston 132' is trained over the intensifier rod 110'. The reservoir piston 132' is positioned within a bore 134' in the rear sleeve 24'.

The reservoir piston 132' is sealed against the surface of the bore 134' by means of an O-ring 136' and wiper seals 138' and 140' that are positioned on each side of the O-ring 136'. The O-ring 136' and accompanying wiper seals 138' and 140' are positioned within a groove 142' that is located in a peripheral surface of the reservoir piston 132'. The floating reservoir piston 132' is also sealed against the intensifier rod 110' along which it slides. A glide or wiper ring 144 and an adjacent O-ring 146' are positioned in grooves 148' and 150' respectively. The positioning of the floating reservoir piston 132' on the intensifier rod 110' creates two fluid chambers 152 and 154' within the area of the rear sleeve 24'. The first fluid chamber 152 lies between the rear manifold 20 and the floating reservoir piston 132'.The second fluid chamber 154' lies between the center manifold and the floating reservoir piston 132'.

The front manifold 16' contains a fluid chamber 156 and an elbow fitting 158' that is threaded into a threaded bore 160' or the front manifold. The bore 160' is in communication with the fluid chamber 156' and the elbow fitting 158'. An additional fluid chamber 162' lies between the intensifier piston 104' and the center manifold 18'. The center manifold 18' contains the upper bore 86' that is in communication with the second chamber 154' and the interior of the elbow 84'. A lower bore 164' is in communication with the chamber 162' and an elbow 166' that is threaded into the bottom of the center manifold 18'. The rear manifold 20' contains a bore 168' that is in communication with the first chamber 152' and the interior of an elbow fitting 170 that is anchored in the rear manifold 20'.

The actuating cylinder 14' has an external cylindrical configuration over its axial extent. The rear portion of the actuating cylinder 14' has a section 172' of reduced external diameter. The end of the section 172' contains a bore 174 that is threaded (not shown) for coupling with the compression fitting 40. The interior of the actuating cylinder 14' is formed by an axial bore 176' that extends over approximately the rear one half of the actuating cylinder 14'. The remaining or forward one half of the interior of the actuating cylinder 14' is formed by an axially extending bore 178' that is of greater diameter than the axial bore 176' of the rear half of the actuating cylinder. A radially extending shoulder 180' forms the intersection between the bores 176' and 178'.A sleeve 182' is positioned primarily within the bore 178' of the actuating cylinder 14'. A portion of the sleeve 182' is of reduced external diameter so that it fits within the bore 176' . The reduced external diameter portion of the sleeve 182' creates a reentrant notch that coacts with the shoulder 180' of the actuating cylinder 14'. The shoulder 180' acts as a stop for the sleeve 182' thus defining its axial position within the actuating cylinder 14'.

A rear piston 184' is positioned within the bore 176' The rear piston 184' has an O-ring seal 186' positioned within a groove 188' located in the cylindrical exterior surface of the rear piston 1848* The piston rod 46' has one end thereof attached to the rear piston 184'. The piston rod 46' has a reduced diameter end portion 192' that extends through. an axially aligned bore 194' in the rear piston 184'. The rear piston 184' is attached to the piston rod 46' by means of a threaded nut 196' that engages threads (not shown) on the end of the reduced diameter end portion 192' of the piston rod 46'. The piston rod 46' extends from the rear piston 184' through the entire axial extent to the right, as viewed in Figure 15, where it exits as an unencumbered cantilevered end 198'.

Returning once again to the sleeve 182', a forward piston 200' is machined into the piston rod 46' as an integral part thereof. The forward piston 200' is located generally toward the mid-portion of the axial extent of the piston rod 46'. The forward piston 200' has a peripheral groove 202' that contains an O-ring 204'. The sleeve 182' accommodates the forward piston 200' within a bore 206'. The O-ring seal 204' seats against the surface of the bore 206'. The sleeve 182' contains a second bore 208' that can be seen in Figure 15 to the left of the forward piston 200'. The second bore 208' forms a chamber 210' between the internal surface of the second bore 208' and the external surface of the piston rod 46'.The sleeve 182' contains a third bore 212 that permits the piston rod 46' to pass therethrough; The bore 212' contains a groove 214' in which an O-ring 216 is positioned for providing a seal between the sleeve 182' and the piston rod 46'. The sleeve 182' contains a groove 218' positioned in its external surface so that an O-ring 220' can be placed therein to effect a seal between the sleeve 182 and the bore 176' of the actuating cylinder 14'.

The section of the piston rod 46' located to the right of the forward piston 200' , as viewed in Figure 15, has a diameter that is less than the bore 206' of the sleeve 182', thus forming a chamber 222'. The chamber 222' has a bore 224' that is in communication with an elbow fitting 226'. In a similar manner, the chamber 210' has a bore 228' that is in communication with an elbow fitting 230'.A chamber 231', which is positioned to the right of the rear piston 184', has a bore 232' that is in communication with an elbow fitting 234, and, a chamber 236', located to the left of the rear piston 184', is in communication with the second chamber 154 of the master cylinder 12' via the bore 174', the elastomeric tube 38' , the elbow 36' , a bore 238' in the end cap 72', the bore 78', the bore 94' and the viewing tube 30' and its included elbow and tee fittings.

The retaining bushing 44' is supported by the mounting plate 42'. The mounting plate 42' is anchored to the front manifold 16 by the studs 26' and the nuts 28'.

The retaining bushing 44' has an external part cylindrical section 240' that fits into the bore 178'.

The retaining bushing 44' is immobilized by means of a retaining ring 242' that coacts with a groove 244' in the wall of the bore 178' in the actuating cylinder 14' and with a groove 246' that is milled in the external surface of the part cylindrical section 240'.

Figure 16 is a cross-sectional view taken along the section lines 3-3 of Figure 15. The piston rod 46' contains a milled planar area 248' on one side and a similar milled planar area 250' on the other side thereof. The milled planar areas 248' and 250' interact with a bifurcated support 252', the arms of which extends vertically along a portion of each of the milled planar areas 248' and 250'. The bifurcated support 252 is shown in phantom lines since it is not considered to be an essential component of the present invention. The purpose of the milled planar areas 248' and 250' is to provide a degree of rigidity to the piston rod 46' so that it will not rotate and cause misalignment with a non-symmetrical tool 47' that may be affixed to the end 198 of the piston rod 46'.

Figure 17 is a part sectional view of an embodiment that employs a load detection device within the piston rod 46 of the actuating cylinder 14'. Figure 17 shows the sleeve 182', the mounting plate 42' and the retaining bushing 44' similar to like components shown in Figure 15. The piston rod 46' has a reduced diameter cylinder section 254'. The cylindrical section 254' telescopes within a piston rod adapter 256'. The piston rod adapter 256' has an external cylindrical surface that fits within a bore 258' in the retaining bushing 44'.

The piston rod adapter 256' has an internal bore 260' into which the telescoping end of the piston rod 46' fits. A load cell 262' is positioned within the bore 260' and a compression spring 264' is aligned within the bore 260' between the end of the piston rod 46' and the load cell 262'. In order to retain the piston rod adapter 256' on the end of the piston rod 46', a pin 266' is installed in a bore 267' that is diametrically aligned with respect to the piston rod 46'. The pin 266' protrudes beyond the external surface of the cylindrical section 254'. The ends of the pin 266' fit into slots 268' that are milled into the piston rod adapter 256'. In this manner, the piston rod adapter 256' has a limited degree of axial movement with respect to the piston rod 46'.The piston rod adapter 256' has a radially aligned bore 270' that permits electrical lead wires 271' of the load cell 262' to exit the interior of the piston rod adapter 256'. During operation of the overall apparatus the piston rod 46' causes the compression spring 264' to exert a force on the load cell 262'. After the load has been released from the load cell, the compression spring 264' will cause the piston rod adapter 256' to move axially subject to the constraints of the pin 266' and the slots 268' During the assembly of the overall apparatus 10', great care must be taken to preserve the integrity of the seals, particularly the O-rings which are subject to the nicks caused by assembly. The master cylinder is assembled by installing the appropriate seals on the reservoir piston 132' and the intensifier piston 104'.

The intensifier piston 104' is affixed to the end of the intensifier rod 110' by the nut 118'. The intensifier rod 110' is then inserted through the bore 120' in the center manifold 18'. The reservoir piston 132' is then slid over the free end of the intensifier rod 110'. The front and rear sleeves 22' and 24' are then installed over the respective bosses 56' and 62' on the center manifold 18'. The front and rear manifolds 16' and 20' are then positioned so that their is respective bosses 50' and 68' slide within the ends of the front and rear sleeves 22' and 24' . The four studs 26' are then installed in the holes (not shown) within th front, center and rear manifolds 16', 18' and 20'. The studs 26 are then tensioned by the installation of the nuts 28'.The elbow fittings 158' and 170' along with the elbow 166' are then installed in their respective manifolds. The tee fitting 90' and the elbow 84' are installed in the rear and center manifolds 20' and 18' respectively. The viewing tube 30' is then installed along with the appropriate O-ring seals 96' and 98'.

The nipple 32' and its accompanying quick disconnect fitting 34' is then installed to the tee fitting 90' The end cap 72', the elbow 36' and the elastomeric tube 38' are then attached to the rear manifold 20'.

During the assembly of the actuating cylinder 14', the sleeve 182' is positioned over the left end (as viewed in Figure 15) of the piston rod 46'. Next, the rear piston 184' is affixed to the end of the piston rod 46' by the nut 196'. The rear piston 184', the piston rod 46' and the sleeve 182' are installed within the bores 176' and 178' of the actuating cylinder 14'. The retaining bushing 44', and its accompanying mounting plate 42', is then slid over the free end of the piston rod 46'. The lower two nuts 28' on the studs that protrude from the front manifold are removed to permit installation of the mounting plate 42'. The retaining bushing 44' is then moved into locking arrangement with the retaining ring 242'. The nuts 28 are reinstalled on the studs 26', anchoring the mounting plate 42' to the front manifold.The elbow fittings 226', 230' and 234' are then installed in the actuating cylinder 14'.

The compression fitting 40' is then attached to the end of the section 172' of the actuating cylinder 14'.

Figure 18 is a cross-sectional view that shows the position of the pistons and piston rods when the overall apparatus 10' is in the fully retracted position. At the commencement of a cycle of the overall apparatus 10', the intensifser piston 104' is to the extreme right end of the chamber 162', as viewed in Figure 18.

Consequently, the end of the intensifier rod 110' is retracted to a position clear of the bore 78'. The reservoir piston 132' is to the extreme left end of the second chamber 154'. In the actuating cylinder 14' portion of the overall apparatus 10', the rear piston 184' is positioned toward the left end of the chamber 231', therefore, the extreme right free end of the piston rod 46' is nearly retracted within the confinement of the actuating cylinder 14'. The forward piston 200', which is an integral part of the piston rod 46' , is positioned at the left end of the chamber 222'.

Figure 19 is a cross-sectional view that shows the position of the pistons and piston rods after the overall apparatus 10' has been actuated to begin a work cycle. Air pressure is introduced to the chamber 152 causing the reservoir piston 132' to move toward the right. The oil to the right of the reservoir piston 132' begins to exit the second chamber 154 and travel via the viewing tube 30' and the elastomeric tube 38' into the chamber 236'. The increase in volume of oil in the chamber 236' causes the rear piston 184' to move rapidly to the right. As the rear piston moves toward the right, air is exhausted from the chamber 231'.

Since the forward piston 200' is a part of the piston rod 46', the forward piston 200' also moves toward the right thus causing an ingress of air into the chamber 210' and an egress of air from the chamber 222'. After the initial introduction of air pressure to the chamber 152' at the left of the reservoir piston 132' there is a rapid deployment of the piston rod 46' to the right where its travel is halted by an interception with, for example, a workpiece.

Figure 20 is a cross-sectional view similar to that shown in Figures 18 and 19 that shows the final stage of the work cycle of the overall apparatus 10'. Since rapid deployment of the piston rod 46' has brought a tool (not shown) carried by it into contact with a workpiece, the load must be increased beyond the capability of the air pressure normally found at an industrial site. Consequently, air pressure is introduced into the chamber 156 which is positioned to the right of the intensifier piston 104'. As the intensifier piston 104 moves to the left, the tip of the intensifier rod 110' enters the bore 78' in the rear manifold thus causing the oil trapped before it to act as a closed loop system between the intensifier rod 104', bore 78 and the chamber 236. The continued travel of the intensifier piston rod 110' into the bore 78' acts on the oil in the chamber 236' urging the rear piston 184' to the right, delivering a greatly increased force to the piston rod 46'. The actual movement of the piston rod 46' has been exaggerated in Figure 20 for purposes of illustrating the movement thereof. The increased movement of the forward piston 200' to the right will exhaust additional air from the chamber 222' and cause an influx of additional air into the chamber 210'.If an additional force is desirable in the piston rod 46', air pressure above ambient can be introduced into the chamber 210'. Thus, there will be a combined hydraulic, as well as intensifying force introduced to the piston rod 46'.

Figure 21 is a schematic fluid diagram according to the present invention and the controls that achieve the fluid motion. For purposes of the present invention the fluids have been described as air and oil. Figure 21 shows a simplified layout of the pistons and piston rods. Since the oil within the overall apparatus 10' is self-contained, the oil has been shown for clarity as sectioned. In order to operate the overall apparatus through its entire work cycle, only external air pressure need be applied. For purposes of explanation, it is assumed the overall apparatus 10' is coupled to an air supply 272'. Air under pressure is supplied to a three-way valve mechanism 274' which is a solenoid actuated spring return device.The air under pressure exits the air supply through a line 276' and travels through the valve mechanism 2748 to a line 278' and to the chamber 231'. The line 278' also supplies air under pressure to a line 280' which is connected to the chamber 162'. The air pressure supplied to the chamber 231' causes the rear piston 184' to move to the left forcing the oil from the chamber 236' into the second chamber 154' and urging the reservoir piston 132' to the left. As the reservoir piston 132' moves to the left, air is exhausted from the chamber 152' through a line 282' to the valve mechanism 274' which permits the expelled air to enter a line 284' and travel to an exhaust port 286' which may, if desired, be a device such as a muffler to attenuate the noise level of the exhausting air.The air pressure delivered via the line 280' to the chamber 162' causes the intensifier piston 104' to remain to the right, ensuring that the tip of the intensifier rod 110' does not impede the flow of oil into the second chamber 154'. The chamber 156 is connected to a two-way valve mechanism 288' by a line 290'. In the unenergized position, the valve mechanism 288' permits the exhaust air from the line 290' to enter a line 292' and pass to the exhaust port 286'. At the start of the cycle, a solenoid 294' on the valve mechanism 274 is energized by the movement of a workpiece into a work station or by other means that connects an electrical source to the solenoid.The energizing of the solenoid 294' connects the air supply line 276' to line 282' pressurizing the chamber 152', which causes the reservoir piston 132' to move to the right, forcing oil from the second chamber 154' to the chamber 236two Oil entering the chamber 236' causes the rear piston 184' to move rapidly to the right, hence the piston rod 46' moves to the right along with the forward piston 200'. The energizing of the solenoid 294' on the valve mechanism 274' causes chambers 231' and 162' to become connected to the exhaust line 284'. As the forward piston 200' moves to the right, air is exhausted from the chamber 222' through a line 295' and air from the exhaust port 286' is drawn through a line 296' to the chamber 210'.After the piston rod 46' has made its rapid advance toward and against a workpiece such as is identified by numeral 298', the pressure, or an electrical switch such as 300', energizes a solenoid 302' on the valve mechanism 288' causing a blocked line 304' to be connected to the line 290'. The air pressure delivered by the line 290' to the chamber 156' causes the intensifier piston 104' to move to the left thus permitting the tip of the intensifier rod 110' to enter the bore 78 which causes an intensified oil pressure in the chamber 236'. The increased force supplied to the rear piston 184' is transferred to the piston rod 46' and to the workpiece 298'. At the command of an operator or by automatic timing the solenoids 294' and 302' are deenergized, permitting the springs 306' and 308' to return the valve mechanism 274' and 288' to their original starting positions.It is to be noted that by utilizing oil te push the reservoir piston backwards as well as forwards, any contaminated air in the closed loop system will collect harmlessly in the reservoir.

By way of illustration, the intensifier rod 110' has a diameter of 0. 5 inches and the intensifier and rear pistons 104' and 184' each have a diameter of 1. 75 inches. Since the increase in the pressure delivered to the rear piston 184' varies as the square of the diameter, 1. 75 squared divided by 0. 5 squared yields a pressure increase of 12. 25. Thus, if typical shop air at 80 psi is delivered to the intensifier piston, there will be 980 psi delivered to the rear piston 184'.

Depending, of course, on the area of the forward piston 200' the load resulting from the 980 psi delivered to the rear piston 184' can be increased by supplying 80 psi air to the forward piston 200' via an additional air supply line 310' and closing the exhaust line 296'.

Embodiments of the invention have been described in detail for illustrating practical operative structures whereby the invention may be put in to practice. However, it is to be understood that the particular apparatus described are intended to be illustrative only, and various novel characteristics of the invention may be incorporated in other structural forms without departing from the scope of the invention defined in the appended claims.

Claims

CLAIMS: -

1. A method for applying an intensified force to a workpiece , said method comprising the steps of: applying a fluid pressure to one side of a reservoir piston located in a master cylinder to move said reservoir piston along said master cylinder from a first predetermined position in a first predetermined direction to effect movement of a piston and its associated piston rod located in an actuator cylinder from a first predetermined position in a direction towards said workpiece whereby a first predetermined force is applied to said workpiece; applying a fluid pressure to one side of an intensifier piston to positively constrain said intensifier piston in a first predetermined position from movement concurrently with said step of applying a fluid pressure and simultaneously moving said piston; ; concurrently applying a fluid pressure to the other side of said intensifier piston and relieving said fluid pressure applied to said one side of said intensifier piston to move said intensifier piston and its associated piston rod in said first predetermined direction to intensify said first predetermined force applied to said workpiece; and relieving said fluid pressure applied to said one side of said reservoir piston and simultaneously applying a fluid pressure to a side of said piston most distal from said master cylinder and said one side of said intensifier piston to return said intensifier piston, said reservoir piston and said piston in said actuating cylinder to said first predetermined position.

2.A method for applying an intensified force to a workpiece, said method being substantially as hereinbefore described with reference to the accompanying drawings.