[0001] This invention relates to new and improved, infinitely positionable locking and bearing
apparatus, and to new and improved fluid-operated actuating apparatus incorporating
the same; and the apparatus of this invention embody and provide novel and significant
structural and functional improvements and advantages over the similar apparatus of
United States Patent 3,150,571, commonly owned.
[0002] Although apparatus similar to those disclosed in this application are disclosed in
commonly owned United States Patent 3,150,571, which United States Patent represents
the most relevant prior art known to applicants, it has nonetheless been determined
in accordance with the teachings of this invention that certain structural and functional
aspects of those prior art apparatus are less than optimal, and that novel and significant
improvements can be made therein. More specifically, it has been determined in accordance
with the teachings of this invention that the cost of manufacture, operation, repair
and inventory of the prior art apparatus of United States Patent 3,150,571--wherein
a sleeve element acts directly upon a rod element to prevent relative movement therebeiwreen,
and wherein pressurized fluid is introduced between the respective sleeve and rod
elements to elastically deform the sleeve element and enable relative sleeve-rod element
movement--can each be significantly reduced, while the reliability of operation, the
operational life and the range of suitable applications for such prior art apparatus
can each be significantly increased.
[0003] It is accordingly, an object of this invention to provide new and improved, fluid-operated
infinitely positionable locking and bearing apparatus.
[0004] The invention will now be described by way of example with reference to the accompanying
drawing which is a side elevational view partially broken away and in cross section
of an embodiment of actuating locking and bearing apparatus constructed and operative
in accordance with the teachings of our invention,
[0005] A sleeve element is indicated generally at 242 and comprises a cylinder 244. which
also functions as the sleeve with regard to apparatus locking and unlocking as heretofore
described, and which extends as shown into and between suitable bores provided therefor
in a blind end cap 246 and a rod end cap 248. The relevant cylinder and bore surfaces
are complementally threaded as indicated at 250 and 252 to secure the cylinder in
the blind and rod end caps; and locknuts are provided as indicated at 254 and 256
to secure the cylinder-cap assembly. Cylinder seats are provided as respectively indicated
at 258 and 264 for obvious purpose.
[0006] A rod element is indicated generally at 266, and comprises a tubular rod 268 and
a tubular piston 270 which includes an enlarged piston head 271 and a tube-like portion
273 which functions as the rod with regard to apparatus locking and unlocking as heretofore
described.
[0007] The rod 268 and piston 270 are interconnected as shown at complementally threaded
areas 272 and 274 by a generally cylindrical connector 276 to form a functionally
integral piston-connector-rod assembly. Piston to connector and rod to connector seals
are provided for obvious purpose as shown at 278 and 280. A rod end is indicated at
282 and is secured as shown in the open end of rod 268 at complementally threaded
areas 28
4. A piston seal 286 is carried as shown from the piston 270 and cooperates with the
inner wall of cylinder 244 to prevent the leakage of pressurized fluid around the
piston; while rod wear ring, rod seal rod scraper 288. 290 and 292 are respectively
carried as shown from the rod end cap 252 to cooperate with the outer surface of rod
268 to prevent leakage of pressurized fluid from the apparatus 240.
[0008] An intermediate element is indicated generally at 294 and comprises a liner 296 which
is configured, dimensioned, disposed and operable relative to cylinder or sleeve 244
and piston portion 273 s heretofore described and which to those ends, comprises liner
segments as indicated at 84, 86, 88, 90 and 92, and a spacer as again indicated at
100. The spacer 100 will be seen to be carried from the piston portion 273 and to
be of somewhat lesser outer diameter than the inner diameter of the cylinder or sleeve
244. As a result, the annular space or volume 104 will, in this embodiment be seen
to be provided between the sleeve and the spacer.
[0009] As pressurized fluid passage 298. including orifice 300 and check valve 302. is provided
to extend as shown through connector 276 to communicate. and permit fluid flow only
in the direction between. the internal volume or space 304 of piston 270 and the generally
annular volumes or spaces 306 and 308 which are respectively formed between the connector
276 and rod 268. and the inner wall of the cylinder or sleeve 244. A pressurized fluid
relief passage 310, including relief valve 312. is provided to also extend as shown
through connector 276 and further communicate. and permit fluid flow only in the direction
between. volumes or spaces 308 and 306. and volume or space 304.
[0010] A rod extend port is indicated at 314 and extends as shown through blind end cap
246 into communication with internal piston volume 304. A flow control device is schematically
indicated at 315 and is operatively disposed as shown relative to extend port 314.
A rod retract port is indicated at 316 and extends as shown through rod end cap 248
into communication with annular volume 308. A pressure relief valve is schematically
indicated at 317 and is operatively disposed as shown relative to retract port 316.
The respective rod extend and retract ports are connected as indicated to a non-illustrated,
suitably vatved-as for venting--source of pressurized fluid which, in the apparatus
240, functions as both the actuating and operating fluid as described in detail hereinbelow.
A safety fuse or blowout plug is indicated at 318 and is operable to discharge pressurized
fluid outside apparatus 240 to prevent excessive pressure build-up in volume 308.
[0011] Of particular advantage with regard to the apparatus 240 is the fact that the same
are fully operable to perform both the actuating and unlocking functions through use
of only two fluid ports, namely the extend port 314 and the retract port 316. Significantly,
no additional port(s) are required for apparatus unlocking since, as described in
detail hereinbelow, apparatus 240 functions as a pump for the internal development
of unlock pressure attendant extension of rod 268. This is accomplished by providing
a high ratio between the piston end area of the apparatus, namely the combined areas
of connector face 320 and the annular end 321 of piston 271, and the rod end area
of the apparatus, namely the cross-sectional area of annular space 308. This ratio
may, for example, range between 5:1 to 10:1, The pumping action is achieved by closing
off the retract port 316 with relief valve 317 set at apparatus unlock pressure during
extension of rod 268. Upon extension of piston 270 and rod 268. Upon extension of
piston 270 and rod 268, the actuating-operating fluid in volume 308 is pressurized
to the apparatus unlock pressure, as determined by the setting of relief valve 317,
thus automatically unlocking the apparatus 240 and maintaining the same unlocked until
piston and rod extension cease. When this occurs. through external venting of the
operating-actuating fluid, the pressure in rod end volume 308 is also vented, thus
reapplying the appara. tus lock. Under these circumstances, it become clear that the
effective output of the apparatus 240 is equal to actuating-operating fluid pressure
as multiplied by the cross-sectional area of rod 268.
[0012] More specifically, and taking for example a situation wherein the unlock pressure
of the apparatus 240 is 3200 psi. and the piston-rod end are ratio is approximately
8:1, extension of rod 268 can occur with the application of actuating-operating fluid
at only approximately 1600 psi to extend port 31
4. This is made possible by the fact that the pressurized fluid passes freely from
piston volume 308 through check valve 302 in connector 276 to in turn pressurize annular
spaces 306, 308 and 104, and thus the liner 82; it being clear that as pressure in
the liner increases, the apparatus locking force decreases proportionally. Thus, as
soon as both the piston volume 304 and the liner 82 are pressurized to approximately
1600 psi, it may be understood that the resultant combination of extend and unlock
forces will cause momentary slippage of the sleeve-liner-piston lock with attendant
small initial movement of the piston 270 and rod 268 to the right As soon as this
small initial movement takes place, the pressure in annular spaces 306, 308 and 104,
and in the liner 82, will be rapidly increased to the 3200 psi setting of relief valve
317 by the above-described apparatus pumping action as provided by the high piston-rod
end area ratio. Thus, apparatus unlocking and extension of rod 268 will occur. If
rod 268 is being extended against no external load, the pressurization of the actuating-operating
fluid at extend port 314 may the be reduced to approximately 400 psi, with the 8:1
piston-rod end area ratio functioning nonetheless to maintain the 3200 psi unlock
pressure in the liner 82 and enable rod extension to continue. If rod 268 is being
extended against an external load, maintenance of the pressurization of the actuating-operating
fluid at extend port 314 at an appropriate level above 400 psi will be required.
[0013] Of course, as rod extension progresses, there will be a pressure build-up in space
308 as the enlarged piston head 271 and seal 286 move to the right and, when this
pressure build-up exceeds the setting of pressure relief valve 312 in connector passage
310, the former will open to permit the return of the pressurized fluid from space
308 into piston volume 304. Should relief valve 312 fail, safety fuse or blowout plug
318 would open with resultant de-pressurization of the apparatus 240 and immediate
return thereof to the locked condition.
[0014] Once the rod end 282 has reached the desired partially or fully extended position
thereof, as the case may be, it will be clear that simple de-pressurization of the
actuating-operating fluid through extend port 314 below the unlock level will result
in the immediate re-locking of the apparatus 240, in the said desired position.
[0015] For subsequent retraction of the rod end 282, and with all of the heretofore described
apparatus volumes or spaces remaining filled with the essentially de-pressurized actuating-operating
fluid, it will be understood that fluid pressurization through retract port 316 to
the appartus unlock level, with extend port 314 vatved open and flow control device
315 operable to meter fluid therethrough at a predetermined, controlled pressure,
will result in the unlocking of the apparatus, again by pressure communication through
spaces 308, 306 and 104 to and through the liner 296, and the immediately following
movement of the rod- connector-piston assembly to the left as seen attendant the action
of the pressurized fluid against the annular retract area provided by the enlarged
piston head 271 and the piston seal 286. As this movement occurs, the fluid in the
now decreasing volume between the separated piston 270 and face 322 of end cap 246
will simply be expelled by pumping through the extend port 314 and flow control device
315, with connector passage 298 acting as a pressure relief means in the event of
clogging of port 314, or failure of its associated valving, to prevent excessive pressure
build-up in that decreasing volume. Of course, the speed of retraction will be limited
by the setting of flow control device 315 which operates on a metering out principle
to maintain sufficient pressure within the apparatus 240 to in turn maintain the same
unlocked. In the given 8:1 area ratio and 3200 psi unlock pressure example, flow control
device 315 would be operable to maintain 400 psi in piston space 304. Again, fowout
fuse 318 will function to, in any event, prevent excessive pressure build-up in annular
volume 308 and its communicatd apparatus volumes. Thus, the apparatus 240 remains
fail-safe under all operational conditions.
[0016] Once the rod end 282 has reached the desired, relatively retracted position thereof,
it will be clear that simple de-pressurization of the operating-actuating fluid through
retract port 316, with virtually concomitant closure of extend port 314 to prevent
further fluid flow from the apparatus 240 and insure that the same remains essentially
fluid-filled, will result in the re-kxking of the appartus in that position by the
re-establishment of the sleeve-liner-rod interference tits as heretofore described.
[0017] Of additionally significant advantage with regard to the appartus 240 is that fact
that the liner 82 is disposed as described between the outside diameter of piston
270 and the inside diameter of the cylinder barrel or sleeve element 242. This configuration,
which may be termed a "piston lock," functions to provide the shortest possible length
for the apparatus locking section--or, as seen from a different perspective, the maximum
effective locking area per unit length of the apparatus 240--since the locking action
is applied to the largest diametral elements of the appartatus. As a result particularly
compact apparatus of the type described, with attendant particularly high resistance
to side loading, are provided without sacrifice in the locking capability of those
apparatus.
[0018] Manufacture of the hereindisclosed apparatus is effected in substantiate the same
manner as that illustrated and described in detail with reference to Figures 11 and
12 of United States Patent 3,150,571 and this need not be repeated in detail. In this
instance, however, it may be understood that the respective sleeve and liner elements
would be assembled as a unit, through sleeve element expansion and use of the assembly
mandrel, as described in United States Patent 3,150,571, around the rod element
[0019] The actuating, locking and bearing apparatus 240 are readily utilizable in conjunction
with outrigger jacks on a high capacity hydraulic crane through the affixation of
the sleeve element 242, as by use of mounting shaft 326, to the crane chassis and
the attachment of rod end 78 to the jack pads thereby enabling jacking and levelling
of the crane relative to its support structure throughout a virtually infinite range
of crane positions. In such use, an outer tube or cover, not shown, may be secured
around cylinder element 242 to provide an appropriate surface for the attachment of
mounting brackets or the like, and to further protect the apparatus 240 from the environment
The significant advantages provided by the best mode applications of the teachings
of applicants' invention as heretofore illustrated and described include the following:
(a) The interposition of the liner between the respective sleeve and rod elements
eliminates the need for grooving of the sleeve, with attendant formation of areas
of stress concentration therein, to enable the requisite operating fluid flow between
the rod and the sleeve. As a result, the strength and operational life of the sleeve
are materially increased, while the cost of manufacture thereof is materially decreased.
(b) The interposition of the liner between the respective sleeve and rod elements
enables the use of the apparatus as a readily and precisely controllable and programmable
braking or deceleration device without damage to the rod or sleeve through use of
readily expendable and replaceable liner materials which are less hard than either
of the sleeve or rod materials.
(c) The use of the liner as above completely eliminates sleeve-rod surface contact
whereby sleeve-rod wear is also eliminated with attendant material increase in operational
life.
(d) The use of the liner as above enables the shifting of all of the final machining
operations essentially to the sleeve, as opposed to both the rod and sleeve as heretofore
required, since the liner can accept and function with a rod which is slightly "out"
of tolerance. As a result, the overall cost of manufacture is further materially decreased.
(e) Machining of the operating fluid grooves is simplified and rendered materially
less costly since the "softer" material of the liner is significantly more readily
machinable than would be the "harder" material of the sleeve.
(f) Repair and/or overhaul of the apparatus are greatly simplified and rendered relatively
inexpensive in that, in most instances, replacement of the liner will function to
totally accomplish the same. In addition, repair and/or overhaul inventories, and
attendant carrying charges, are greatly reduced because the same can essentially be
limited to a supply of relatively standard, and readily shippable, liner segments.
Also, in those instances wherein repair and/or overhaul require more than simple liner
replacement, it will be clear that the same is no longer limited to the rod, but rather,
may be made to either or both of the rod and sleeve as, for example, by appropriate
plating of the relevant surfaces.
(g) The interposition as above of the liner between the sleeve and rod elements greatly
increases the range of materials which can be employed in the manufacture of those
elements and, as a result, greatly increases the range of operating fluids and operating
temperatures which can be employed therewith, thereby combining to greatly increase
the range of useful applications to which the apparatus can be put This range of materials
for the rod would include any appropriately strong metal such as steel, stainless
steel or aluminium, and a wide variety or appropriately strong plastic materials such
as molded or fibreglass wound compositions, or boron. The metals could be heat treated
or surface hardened or, alternatively, chrome electroless or nickel plated. The range
of materials for the sleeve would again include any appropriately strong metal having,
in addition, an appropriate modulus of elasticity, such as steel, stainless steel,
or aluminium; or similarly characterized plastics such as fibre would or fibreglass
reinforced tubing, glass wound and cross-hatched epoxies, or materials com- posities.
For apparatus use attendant controlled decellera- tion as described hereinabove wherein
high thermal conductivity and resistance to surface wear are likely to be required
of the liner material, appropriately heat treated steel or bronze would be particularly
qualified. High operational temperature applications of the apparatus could also dictate
the use of ceramic liner materials. Representative operating fluids would include
a wide range of petroleum, water of synthetic based hydraulic fluids, and gases such
as nitrogen or air. Although apparatus operating pressures can vary widely depending
upon the application to which the apparatus are put, the 3200 psi operating pressure
as set forth hereinabove by way of example with regard to the apparatus 240 is a representative
operating pressure.
[0020] The major advantages provided as described in detail hereinabove by the new and improved
basic structural configuration and manner of operation of the apparatus 240, in addition
to and independent to those provided as described by the incorporation of the liner
82 therein, can, in certain instances, warrant the fabrication of the apparatus 240
without the liner in further accordance with the teachings of our invention. In such
instances, the respective extemal diameter of the piston 270 and the internal diameter
of the sleeve element 244 would be carefully predetermined to create an interference
fit directly therebetween in the manner illustrated and described in detail in United
States Patent 3,150,571. Under these circumstances, appropriate operating fluid grooves
would be formed, for example, in the inner surface of the sleeve element 244 as illustrated
and described in United States Patent 3,150,57
1, and these grooves would, of course, communicate freely with annular spaces 308 and
306 to provide for the flow of the operating fluid to the sleeve element to expand
the same within the elastic limit thereof and release the sleeve element-piston interference
fit, and thus the apparatus lock, upon the pressurization of the operating fluid to
a sufficient level.
1. A locking and bearing apparatus comprising
(a) actuating cylinder means (244),
(b) a double acting actuating piston means (268-270) operatively disposed within said
actuating cylinder means (244) and dividing the same into first and second cylinder
spaces,
(c) an intermediate pressure responsive locking means (82) operatively associated
with said actuating cylinder and piston means and operable to lock the same together
and prevent relative movement therebetween,
(d) means (317) to pressurize said locking means to a level sufficient to release the locking eftect
characterised in that
(i) said actuating piston means comprise piston faces of different effective areas
with the larger of said piston faces (320-321) being operatively associated with said
first cylinder space and the smaller of said piston faces (308 cross-section) being
operatively associated with said second cylinder space,
(ii) said second cylinder space being in communication with said locking means,
(iii) said first cylinder space being in communication with said second cylinder space
through fluid transfer passage means (300-302) to permit fluid flow only from said
first to said sacond cylinder spaces whereby
(iv) the introduction to said first cylinder space of fluid pressurized to a level sufficient
to effect initial movement of said piston into said second cylinder space but not
sufficient to release said locking means,
(v) and the concomitant flow of said fluid from said first to said second cylinder
spaces through said fluid transfer passage means will be effective to further pressurize
said fluid in said second cylinder space to a level sufficient to release said locking
means for continued movement of said piston into said cylinder space.
2. Apparatus as in claim 1, wherein said locking means comprise an interference fit
between said actuating cylinder and piston means, and whereby said fluid, when pressurized
to said level, is effective to expand said actuating cylinder means within the elastic
limit thereof to an extent sufficent to release said interference fit and the lock
between said actuating cylinder and piston means.
3. Apparatus as claimed in Claim 1 or 2, characterised in that said locking means
comprises a plurality of generally longitudinally extending segments (84,86,90,92)
which are disposed in side-by- side relationship in said operating space.
4. Apparatus as claimed in Claim 3, characterised in that each of said segments comprises
a discontinuity (94) generally longitudinally and coextensively thereof, said discontinuities
being longitudinally alignable to form one of said fluid passeges.
5. Apparatus as claimed in Claim 1, characterised in that said fluid transfer passage
means comprise a fluid passage formed in said actuating piston and connecting said
first and second actuating cylinder spaces therethrough, and check valve means (303)
operatively associated with said passage and permitting fluid flow therethrough only
in the direction from said first to said second cylinder spaces.
6. Apparatus as claimed in Claim 5, further characterised by additional fluid transfer
passage means communicating said second and first actuating cylinder spaces and permitting
fluid flow from said second to said first cylinder spaces only when the fluid pressure
in said second cylinder space has reached a level sufficient to release the lock.
7. Apparatus as claimed in Claim 6, characterised in that said fluid additional fluid
transfer passage means comprise an additional fluid passage formed in said actuating
piston and connecting said second and first actuating cylinder spaces therethrough,
and relief valve means operatively associated with said additional fluid passage and
permitting fluid flow from said second to said first cylinder spaces only when the
fluid pressure in said second cylinder space has reached a level sufficient to release
the lock.
8. Apparatus as claimed in claim 1, further characterised by flow restrictor means
operatively associated with said first actuating cylinder space and operable to control
the flow rate of fluid therefrom to without said apparatus.
9. Apparatus as claimed in Claim 1, further characterised by pressure relief means
operatively associated with said second actuating cylinder space and operable to discharge
pressurized fluid therefrom to without said apparatus upon pressure build-up in said
second actuating cylinder space beyond a predetermined level.