US3554528A - Energy dissipating hydraulic systems - Google Patents

Energy dissipating hydraulic systems Download PDF

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US3554528A
US3554528A US669515A US3554528DA US3554528A US 3554528 A US3554528 A US 3554528A US 669515 A US669515 A US 669515A US 3554528D A US3554528D A US 3554528DA US 3554528 A US3554528 A US 3554528A
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hydraulic
ram
reservoir
orifices
chamber
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Joseph R Kring
Josef F Schraner
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16FSPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
    • F16F9/00Springs, vibration-dampers, shock-absorbers, or similarly-constructed movement-dampers using a fluid or the equivalent as damping medium
    • F16F9/32Details
    • F16F9/44Means on or in the damper for manual or non-automatic adjustment; such means combined with temperature correction

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  • Means interconnecting the ram chamber and the reservoir are provided so that a transfer of hydraulic liquid occurs in opposition to said yieldable means from said ram chamber to said reservoir under relatively free flow conditions for a first part of said power stroke and under flow restriction conditions for the remainder thereof.
  • Said ram chamber provided with axially spaced orifices all but the last of which are closed off progressively by said hydraulic ram in its movement to its retracted position in said ram chamber during said power stroke.
  • the first of said orifices being free flow orifices through which hydraulic liquid flows from said ram chamber to said reservoir under free flow conditions for a first part of said power stroke and the remainder of said orifices being flow restriction orifices through which hydraulic liquid flows from said ram chamber to said reservoir under flow restriction conditions for the remainder of said power stroke.
  • Said hydraulic ram being fully retracted without closing off the last of said flow restriction orifices.
  • the reservoir piston effects a return of hydraulic liquid from the reservoir to the ram chamber to return the ram in the opposite direction in a single return stroke thereof.
  • Said interconnecting means includes unidirectional valve means closed during said power stroke and open to the ram chamber during said return stroke.
  • the principal object of our invention is the provision of an industrial-type hydraulic shock absorber which has such improved features of construction that it is self-contained, selfcooling, self-indicating as to fullness when being filled, truly adjustable in respect to its cushioning effect and rugged in respect to its size and weight so as to be capable of withstanding impacting forces of high order and particularly if such impacting forces are of a repetitive nature.
  • FIGS. 1, 3 and 4 are, respectively, opposite side and front elevational views of an industrial-type hydraulic shock absorber embodying our invention
  • FIG. 2 is a plan view of said embodiment with parts in section showing the same rear mounted;
  • FIGS. 5 and 6 are fragmentary views showing alternate mounts for said embodiment
  • FIG. 7 is a longitudinal sectional view of said embodiment taken on the line 7-7 of FIG. 2;
  • FIG. 8 is a transverse sectional view of said embodiment taken on the line 8-8 of FIG. 1;
  • FIGS. 9-24 are fragmentary views of parts of said embodiment.
  • 30 designates said embodiment generally and 31 the center section thereof which is fastened at its opposite ends to front and rear end plates 32 and 33, respectively, via fasteners 110.
  • Spring washers 111 are used in conjunction with said fasteners 110 to insure their security.
  • Steel liners 209. surround the fasteners 110 and extend into counterbores 144 formed in the center section 31 for alignment of the end plates 32 and 33 with the center section 31.
  • Gaskets 112 which comprise layers 137 of an asbestos material having a steel band 138 sandwiched therebetween are used to form liquidtight seals between the 138 embraces each aligned aperture-between the center section 31 and the end plates 32 and 33- and embeds itself into the asbestos layers 137 which in turn force themselves into irregularities in the mating machined surfaces creating a tight sealing condition.
  • the center section 31 is an investment casting which is provided with fins 145 for better cooling the hydraulic liquid in the embodiment 30 via ambientair.
  • the center section 31 has mounting apertures 146'thr'ough its flange portions on its opposite ends which are aligned with apertures 148 and 149 in the end plates 32 and 33, respectively, by which the embodiment 30 may be rear or front mounted as desired.
  • FIGS. 2 and 8 show the embodiment 30 rear mounted on suitable structure 147 via socket head fasteners 152 which are engaged by locknuts 153 held against rotation by the walls of section 31.
  • FIG. 5 shows the embodiment 30 rear mounted on structure 151 by fasteners 150.
  • FIG. 6 shows the embodiment 30 front mounted on structure 154 by fasteners 155.
  • An inner pressure cylinder 34 defining a pressure chamber 35 is provided centrally of the center section 31 and held therein by retainer inserts 44 and 45 which are disposed in end plates 32 and 33, respectively. A portion of the insert 45 projects into an end of the cylinder 34 and is liquid-tight sealed in respect thereto by a bronze piston ring 113.
  • a spring washer 46 of the three-wave type is provided between the cylinder 34 and the insert 44 to force the cylinder 34 against the insert 45 for positioning and to eliminate close tolerance machining.
  • the cylinder 34 rotatably supports an outer cylinder 41 the purpose of which will appear hereinafter.
  • the cylinder 34 slidably carries an hydraulic ram, generally designated 185, comprising a hard aluminum bronze sleeve 56 which is staked, as at 57, over the inner end of a piston rod 53 and liquid-tight sealed in respect to the cylinder 34 by a pair of piston rings 54 which are held in predetermined circumferential relationship with each other (i.e. so that the space at the ends of each, as at 180 in FIG. 21, are spaced apart from each other diametrically) by rivets 55, the heads of which are disposed in an annular groove 58.
  • the inside diameter of the cylinder 34 is honed.
  • a check valve 130 disposed in a bore 156 in the insert 45 and held therein by a'bowed retainer ring 134.
  • the check valve 130 is liquid-tight sealed in the bore 156 by an O-ring 132 and backup rings 132 therefor.
  • the cylinder 34 is provided with a groove 51 and four equally circumferentially spaced radial apertures 52 which (together with three such spaced radial apertures 50 in the cylinder 41) provide free travel of the piston 185 for aninitial portion (about one-third) of its travel.
  • the piston 185 is relieved, as at 157, for accommodating displaced hydraulic liquid via equally circumferentially spaced radial apertures 114 in the cylinder 34.
  • the cylinder 34 is also provided with six longitudinally spaced flats 38 machined in its outer surface which define a like number of cavities between itself and the cylinder 41. In each such flat 38 are formed a pair of spaced radial apertures 37.
  • the flats 38 and apertures 37 together with other cooperating structure including that on the cylinder 47 affect travel of the piston 185 for the remaining portion (about two-thirds) of its travel. At the end of such travel the piston 185 assumes'the extreme retracted position shown for it in dotted outline in P16. ,7.
  • Such cooperating structure includes honed finishes on the mating surfaces of the cylinder 34 (its 0D.) and of the cylinder 41 (its ID.) and six longitudinally spaced through-slots 40 formed through the wall of the cylinder 41 in annular grooves 49 therein.
  • the slots 40 constitute metering orifices and are longitudinally centrally aligned in respect to the cavities defined by the flats 38 and form therewith variable area metering orifices 39 which are adjustable in area by virtue of the rotatable disposition of the cylinder 41.
  • the maximum area position of the metering orifices 39 occurs when the slots 40 are fully open in respect to the cavities defined by the flats 38 as shown in FIG. 8.
  • FIG; 16 shows such minimum area position from which it can be noted that such variable area meteringorifices 39 are never fully closed to protect against breakage of parts of the embodiment 30 as well as of the impacting structure intended to be d ecelerated.
  • Flow of hydraulic liquid out of the variable area metering orifices 39 is into an intermediate relief chamber 42 formed in the center section 31 concentrically about the cylinderv 34 and also therebeneath as shown in FIGS. 7 and -8.
  • Rotation of the cylinder 41 is accomplished by a transversely disposed driftless gear train including a worm 87 fast (via pin 90 and shoulder 89) on a shaft 86 rotatably supported in a bore 102 in the center section 21 and in a retainer insert 91.
  • the bore 102 is liquid-tight sealed in respect to theoutside by an O-ring 94 and a pair of backup rings 95 on opposite sides thereof.
  • the insert 91 in turn is held fast in a bore 99 in the center section 37 via fasteners 92 which bore 99 is similarly sealed by an O- ring 97 and a pair of backup rings 98.
  • the portion of the shaft 86 carried in the insert 91 is liquid-tight sealed in respect to the outside via an O-ring 96.
  • a knurled knob 85 is carried fast on an end of the shaft 86 (such end being square in cross section over the portion 100 thereof and having a tapped aperture for engaging the flat head screw 101) and a pinion gear 93 is carried fast on its opposite end.
  • the pinion gear 93 meshes with a gear 103 which is rotatably supported on the center section 21 via a shoulder screw 104.
  • the gears 93 and 103 are sealed against entrance of foreign matter by a seal 105 which is preferably of oil'resistant material such as nitrile rubber.
  • the gear 103 is graduated on its outside face (FIG. 1) and a reference mark 106 is provided on the outside wall of the center section 31 to serve as a reference in respect to the rotated position of the gear 103.
  • the worm 87 meshes with a gear segment 88 which is carried fast on a member 107 fastened to the cylinder 41 via drive studs 108 and welds as shown.
  • the member 107 has a forked portion 259 which projects outwardly of the gear segment 88 and embraces the worm 87 to position the outer cylinder 41 axially in respect to the pressure cylinder 34 during assembly.
  • the forked portion 159 centers the gear segment 88 in respect to the worm 87.
  • a full 360 revolution of the knob 85 rotates the cylinder 41 6 circular degrees and the graduated face gear 103 50 circular degrees.
  • Maximum rotation of the cylinder 41 is 30 circular degrees corresponding to five full revolutions of the knob 85 and 250 circular degrees of revolution of the gear 203 (corresponding to movement of the gear between its zero setting and its maximum setting as at 115).
  • Limitation of rotation of the cylinder 41 to its maximum of 30 circular degrees is accomplished by an opensided slot 126 in an end of the cylinder 41 and a pin 48 projecting from the cylinder 34 so as to operate in the slot 1 16.
  • the cylinder 34 must be circumferentially located during assembly in respect to the cylinder 41 which is accomplished by a locating pin 47 which is disposed in a slot 160 in the cylinder 34 and projects through the insert 45 into the end plate 33.
  • Flow of hydraulic liquid from the intermediate chamber 42 occurs into a reservoir 36 via passageways 162, 43 and 163 formed in the end plate 33.
  • a portion of the insert 45 projects into the passageway 43 and is provided with a throughout 229. for passing hydraulic liquid through the interruption in the passageway 43 occasioned by the presence of such projecting portion of the insert 45.
  • the open end of the passageway 43 is closed by a plug 139.
  • the reservoir 36 is formed by a honed liner 64 disposed in a bore 65 in the center section 31 above the chamber 42 and a piston, generally designated 166, slidably carried in the liner 64.
  • The-liner 64 is held in place in the bore 65 by an annular retainer insert 72 and between the two of them is a spring washer 78 of the three-wave type employed to position the liner against end plate 33 and to eliminate close tolerance machining.
  • An O-ring 79 and backup ring 80 therefor form aliquid tight seal for the liner 64 in respect to the bore 65.
  • the insert 72 extends through the end plate 32 via a bore 167 therein concentric with the bore 65 and in turn holds another insert 73 which has intersecting longitudinal 168 and transverse 169 passageways therein for purposes which will appear.
  • the insert 73 has an annular shoulder 74 against which one end of a compression spring 59 operates, the other end of which operates against another insert 66 which is a part of the piston 166.
  • the latter is made in separable component assemblies one of which comprises an outer piston sleeve 60 which is liquid-tight sealed in respect to the liner 64 by a U-cup sealed 62 and backup ring 63 therefor.
  • An advance located piston ring 61 takes up shock and protects the U-cup seal 62 from high shock pressures exerted against the piston 166. 1t also compensatesfor heat andpressure expansions of the liner 64.
  • the other component assembly of the piston 166 comprises a stainless .steel valve stem; 70. held against the insert 66 by a compression spring 69v which operates against a retainer ring 71 on an end of the valve stem 70 and against an end of the insert 66.
  • the opposite ends of the insert 66 and the stem 70 are liquid-tight sealed in respect to each other and in respect to the piston sleeve 60 by means 67 in the form of a square-cut seal ring.
  • the chamber in the liner 64 behind the piston 166 is designated 68 and is vented to atmosphere exterior of the embodiment 30 via four equally circumferentially space radial apertures 75 and an annular groove 76 in the liner 64 and by three 90 circumferentially spaced radial apertures 77 in the center section 31.
  • the passageways 168 and 169 in the insert 73 also vent the chamber 68.
  • the piston rod 53 is chrome plated and operates in a bronze bearing 117 press-fitted into a bore 158 in a protrusion170 formed on the front of the end plate 32 and beyond the hearing 117 is liquid-tight sealed in respect to displaced hydraulic liquid by mechanism disposed in a bore 169 in said protrusion 170 which includes a Utype packing seal 121 about the piston rod 53 and backup ring 122 therefor and an O-ring 119 about the bore 169 and backup rings therefor which are held in place by a retainer insert 118. Said mechanism also includes a wiper 123 for the piston rod which is held in place by a retainer insert 124. A bowed retainer ring 125 locks said mechanism in place inthe bore 169. An enlarged.
  • bore 171 is formed in the protrusion 170 outwardly of the bore 169 to receive a cap 126 carried on the freeend of the piston rod 53 and made fast thereto by a prong ring,1 27.
  • the end cap 126 is slotted, as at 178, to provide access to the prong ring 127 to squeeze the same for purposes of removing or replacing the end cap on said free end of the piston rod53'.
  • an impact plate 140 is provided for affixation by suitable fasteners 177 to moveable structure, as at 172, which is intended to impact against the piston rod 53.
  • the engaging face of the impact plate 140 is arcuately contoured, as at 173, to minimize side thrust on the piston rod 53 and its bearing 117.
  • the embodiment 30 is filled with hydraulic oil via an oil fitting 143 threadably engaged in an aperture 84 in the end plate 32. (If the embodiment 30 is front mounted the oil fitting 184 in the end plate 33 may beused.)
  • the ram 185 preferably is forcefully held in its extreme retracted position. Hydraulic oil is forced into the embodiment 30 with the ram 185 so held until the intermediate relief chamber 42 and the reservoir 36 are completely filled as well as the space behind the ram 185 which occurrence is signaled by flow of hydraulic oil out of the chamber68 via the aperture 77 and/or the passageways 168.
  • flow of hydraulic oil occurs from the reservoir 36 into the chamber 68 as shown in FIG.
  • the insert 66 has an axial bore 82 and diametrically disposed radial apertures 83 to provide for such flow of hydraulic oil during filling of the embodiment 30.
  • a relief passageway 81 behind the seal ring 67 communicates with the bore 72 to insure that the seal 67 will remain seated in the event of sudden opening of the valve stem 70. Filling of the embodiment 30 is terminated as soon as hydraulic oil is noted to flow out of the apertures 77 and/or the passageway 168.
  • vent screws and 136 are provided to accommodate the multiple positions in which the embodiment 30 may be disposed in use.
  • vent screws 18] are provided to accommodate the multiple positions in which the embodiment 30 may be disposed in use.
  • These multiplely located vent apertures permit proper bleeding of the embodiment 30 at any angle at which it may be mounted.
  • the reservoir piston 166 moves to the left to the position shown for it in FIG. 7 and in doing so moves the ram 185 to its extreme extended position shown for it in FIG. 7.
  • the initial portion of the travel of the piston 185 is under substantially free flow conditions as hydraulic oil is forced out of the pressure chamber 35 without restriction via the apertures 52 and the annular groove 51 in the cylinder 34 and the apertures 50 in the cylinder 41.
  • the remaining portion of the travel of the piston 185 (after the same closes off the apertures 52) is restricted from the flow restriction presented by the variable area metering orifices 39 to the flow of hydraulic liquid from the pressure chamber 35 into the intermediate relief chamber 42.
  • the stiffness with which the piston 185 absorbs the shock of the impacting force can be varied to suit the particular application by rotating the knob 75 to adjust the area opening presented by the variable area metering orifices 39.
  • a user can tell to what degree of cushioning the embodiment 30 is set for simply from glancing at the setting on the graduated face of the gear 103.
  • hydraulic liquid flows from the reservoir 36 under the force of the piston 166 into the pressure chamber 35 without restriction via the check valve 130 to return the piston 185 rapidly to its rest position shown in full lines in FIG. 7.
  • the system is unaffected by hydraulic losses due to the hydraulic liquid stored in the reservoir 36 and the continual pressure maintained by the piston 166 on the hydraulic liquid in the chamber 42 and in the pressure chamber 35.
  • the piston 166 continually maintains a nearly steady oil pressure in the system which increases the useful life of the seals.
  • Means in energy dissipating hydraulic systems for dissipating the energy of impacting forces comprising:
  • c. means interconnecting said ram chamber and said reservoir so that a transfer of hydraulic liquid occurs in opposition to said yieldable means from said ram chamber to said reservoir under relatively free flow conditions for a first part of said power stroke and under flow restriction conditions for the remainder thereof;
  • said ram chamber provided with axially spaced orifices all but the last of which are closed off progressively by said hydraulic ram in its movement to its retracted position in said ram chamber during said power stroke; the first of said orifices being free flow orifices through which hydraulic liquid flows from said ram chamber to said reservoir under free flow conditions for a first part of said power stroke and the remainder. of said orifices being flow restriction orifices through which hydraulic liquid flows from said ram chamber to said reservoir under flow restriction conditions for the remainder of said power stroke; said hydraulic ram being fully retracted without closing off the last of said flow restriction orifices;
  • said reservoir piston operative at the end of said power stroke to effect return of hydraulic liquid from the reservoir to the ram chamber to return the ram in the opposite direction in a single rapid return stroke thereof;
  • said interconnecting means including unidirectional valve means at the end of said ram chamber opposite that from which said ram operates which is closed during said power stroke and open to the ram chamber during said return stroke.
  • Means according to claim 1 further comprising means for varying the area of said flow restriction orifices comprising concentric cylinders which have communicating flow restriction orifices and means for rotating said cylinders relative to each other to vary the effective flow area of said flow restriction orifices to alter the cushioning efiect of said power stroke in accordance with the magnitude of the impacting force.
  • Means according to claim 1 further comprising housing means for the reservoir and said chamber having cooling fins on the exterior thereof for transfering heat from said hydraulic liquid to ambient air. during both said power and return strokes for cooling purposes.
  • An hydraulic shock absorber according to claim 1 having housing means with fins on its exterior for cooling hydraulic liquid therein via ambient air.
  • An hydraulic shock absorber according to claim 1 in which said ram includes a hard aluminum bronze piston sleeve and a pair of piston rings therefor and held thereon in diametrically opposed circumferential relationship to each other.
  • An hydraulic shock absorber according to claim 1 further comprising an end cap for the free end of said ram and resilient releasable holding means for said end cap.
  • An hydraulic shock absorber according to claim 8 further comprising an arcuately contoured impact plate for use in conjunction with said end cap for reducing side thrust on said ram.
  • An hydraulic shock absorber in which the wall of said reservoir is provided by a honed liner and in which said yieldable means comprises compression spring means operating on the reservoir piston to maintain the hydraulic liquid in the reservoir under a yieldable pressure.
  • An hydraulic shock absorber in which the reservoir piston is provided with liquid-tight seal means in respect to said liner and a piston ring in advance of said seal means to absorb surge hydraulic pressures on the reservoir piston.
  • An hydraulic shock absorber according to claim 3 in which said means for rotating said outer cylinder comprises a driftless gear train including a worm'and a manually rotated knurled knob.
  • An hydraulic shock absorber according to claim 12 in which graduated readout means are provided on the gear train for determining the setting of said metering orifice.
  • An hydraulic shock absorber in which said gear train includes a gear segment meshing with said worm and a bifurcated mechanism centering said gear segment in respect to said worm.
  • valve means including an axially moveable valve stem and liquid-tight seal means therefor and means to open said valve means when the reservoir piston reaches a predetermined position in its travel during filling of the shock absorber to prevent overfilling thereof.
  • An hydraulic shock absorber according to claim 1 which is so constructed as to be operative in any position in which it may be mounted, and manually openable normally closed vent means at different locations on the body of said shock absorber so that the hydraulic liquid therein can be air-bled in every such mounted position of said shock absorber.
  • said transferring of hydraulic liquid being accomplished by movement of an hydraulic ram to its retracted position in said rarn chamber during said power stroke by said ram progressively closing off all but the last of axially spaced orifices in said ram chamber; the first of said orifices being free flow orifices through which hydraulic liquid flows from said ram chamber to said reservoir under free flow conditions for a first part of said power stroke and the remainder of said orifices being flow restriction orifices through which hydraulic liquid flows from said ram chamber to said reservoir under flow restriction conditions for the remainder of said power stroke; said hydraulic ram being fully retracted without closing off the last of said flow restriction orifices; and
  • Process according to claim 20 further comprising transfering heat from said hydraulic liquid to ambient air during both said power and return strokes for cooling purposes.
  • An industrial type hydraulic shock absorber having a center section and end plates bolted to said center section at opposite ends thereof, an hydraulic ram chamber defined by a cylinder fast in said center section between said end plates, an hydraulic ram operative in said ram chamber and out of one of said end plates, said ram having a single energy dissipating power stroke in respect to an impacting force acting in one direction thereon, an hydraulic reservoir defined by a chamber in said center section, a piston slidable insaid reservoir and yieldable means operative upon said piston, means interconnecting said ram chamber and said reservoir so that a transfer of hydraulic liquid occurs in opposition to said yieldable means from said ram chamber to'said reservoir under free flow conditions for a first part of said power stroke and under flow restriction conditions for the remainder thereof, said ram chamber provided with axially spaced orifices all but the last of which are closed off progressively by said hydraulic ram in its movement to its retracted position in said ram chamber during said power stroke.
  • the first of said orifices being free flow orifices through which hydraulic liquid flows from said ram chamber to said reservoir under free flow conditions for a first part of said power stroke and the remainder of said orifices being flow restriction orifices through which hydraulic liquid flows from said ram chamber to said reservoir under flow restriction conditions for the remainder of said power stroke.
  • Said hydraulic ram being fully retracted without closing off the last of said flow restriction orifices, said reservoir piston operative at the end of said power stroke to effect return of hydraulic liquid from the reservoir to the ram chamber to return the ram in the opposite direction in a single return stroke thereof, said interconnecting means including unidirectional valve means closed during said power stroke and open to the ram chamber during said return stroke.
  • An hydraulic shock absorber according to cla1m 25 m which said ram chamber is defined by a first cylinder fast in said center section between said end plates, and further comprising an intermediate relief chamber defined by a cavity in said center section and a second cylinder concentric about and supported for rotation on said first cylinder, flow restriction means in said second cylinder providing a variable area metering orifice for flow of hydraulic liquid between said ram chamber and said intermediate relief chamber, and means for rotating said second cylinder to vary the effective area of said metering orifice.
  • each end plate is provided with mounting means by which the shock absorber can be front or rear mounted in respect to stationary structure.

Abstract

Improvements in energy dissipating hydraulic systems are disclosed for dissipating the energy of impacting forces comprising an industrial-type hydraulic shock absorber having an hydraulic ram chamber and an hydraulic ram operative therein which has a single energy dissipating power stroke in respect to an impacting force acting in one direction thereon. A selfcontained hydraulic reservoir, a piston therein and yieldable means operative upon said piston are provided. Means interconnecting the ram chamber and the reservoir are provided so that a transfer of hydraulic liquid occurs in opposition to said yieldable means from said ram chamber to said reservoir under relatively free flow conditions for a first part of said power stroke and under flow restriction conditions for the remainder thereof. Said ram chamber provided with axially spaced orifices all but the last of which are closed off progressively by said hydraulic ram in its movement to its retracted position in said ram chamber during said power stroke. The first of said orifices being free flow orifices through which hydraulic liquid flows from said ram chamber to said reservoir under free flow conditions for a first part of said power stroke and the remainder of said orifices being flow restriction orifices through which hydraulic liquid flows from said ram chamber to said reservoir under flow restriction conditions for the remainder of said power stroke. Said hydraulic ram being fully retracted without closing off the last of said flow restriction orifices. At the end of the power stroke the reservoir piston effects a return of hydraulic liquid from the reservoir to the ram chamber to return the ram in the opposite direction in a single return stroke thereof. Said interconnecting means includes unidirectional valve means closed during said power stroke and open to the ram chamber during said return stroke.

Description

United States Patent [72] Inventors Joseph R. Kring 676 Kennedy Drive, Mansfield, Ohio 44904; Josef F. Schraner, 35914 VY eidernan, Mount Clemens, Mich. 48043 [21] Appl. No. 669,515
[22] Filed Sept. 21, 1967 [45] Patented Jan. 12, 1971 [54] ENERGY DISSIPATING HYDRAULIC SYSTEMS Pn'mary Examiner lames B. Marbert Attorney-William L. Fisher ABSTRACT: Improvements in energy dissipating hydraulic systems are disclosed for dissipating the energy of impacting forces comprising an industrial-type hydraulic shock absorber having an hydraulic ram chamber and an hydraulic ram operative therein which has a single energy dissipating power stroke in respect to an impacting force acting in one direction thereon. A self-contained hydraulic reservoir, a piston therein and yieldable means operative upon said piston are provided. Means interconnecting the ram chamber and the reservoir are provided so that a transfer of hydraulic liquid occurs in opposition to said yieldable means from said ram chamber to said reservoir under relatively free flow conditions for a first part of said power stroke and under flow restriction conditions for the remainder thereof. Said ram chamber provided with axially spaced orifices all but the last of which are closed off progressively by said hydraulic ram in its movement to its retracted position in said ram chamber during said power stroke. The first of said orifices being free flow orifices through which hydraulic liquid flows from said ram chamber to said reservoir under free flow conditions for a first part of said power stroke and the remainder of said orifices being flow restriction orifices through which hydraulic liquid flows from said ram chamber to said reservoir under flow restriction conditions for the remainder of said power stroke. Said hydraulic ram being fully retracted without closing off the last of said flow restriction orifices. At the end of the power stroke the reservoir piston effects a return of hydraulic liquid from the reservoir to the ram chamber to return the ram in the opposite direction in a single return stroke thereof. Said interconnecting means includes unidirectional valve means closed during said power stroke and open to the ram chamber during said return stroke.
PATENIED JAN 1 21971 3,554,52
sum 3 0F 4 JOSEPH R. KRING J JOSEF F. SCHRANER INVENTORS PATENTEU JAN 1 21971 7 3554,5253
saw a UF 4 JOSEPH R. KRlNG JOSEF E SCHRANER INVENTORS BY @wwszmmazo THEIR ATTORNEY ENERGY DISSIPATING HYDRAULIC SYSTEMS Our invention relates to energy dissipating hydraulic systems and more particularly to industrial-type hydraulic shock absorbers.
The principal object of our invention is the provision of an industrial-type hydraulic shock absorber which has such improved features of construction that it is self-contained, selfcooling, self-indicating as to fullness when being filled, truly adjustable in respect to its cushioning effect and rugged in respect to its size and weight so as to be capable of withstanding impacting forces of high order and particularly if such impacting forces are of a repetitive nature.
The foregoing object of our invention and its advantages will become apparent during the course of the following description, taken in conjunction with the accompanying drawings, in which:
FIGS. 1, 3 and 4 are, respectively, opposite side and front elevational views of an industrial-type hydraulic shock absorber embodying our invention;
FIG. 2 is a plan view of said embodiment with parts in section showing the same rear mounted;
FIGS. 5 and 6 are fragmentary views showing alternate mounts for said embodiment;
FIG. 7 is a longitudinal sectional view of said embodiment taken on the line 7-7 of FIG. 2;
FIG. 8 is a transverse sectional view of said embodiment taken on the line 8-8 of FIG. 1; and
FIGS. 9-24 are fragmentary views of parts of said embodiment.
Referring to the drawings in greater detail, 30 designates said embodiment generally and 31 the center section thereof which is fastened at its opposite ends to front and rear end plates 32 and 33, respectively, via fasteners 110. Spring washers 111 are used in conjunction with said fasteners 110 to insure their security. Steel liners 209. surround the fasteners 110 and extend into counterbores 144 formed in the center section 31 for alignment of the end plates 32 and 33 with the center section 31. Gaskets 112 which comprise layers 137 of an asbestos material having a steel band 138 sandwiched therebetween are used to form liquidtight seals between the 138 embraces each aligned aperture-between the center section 31 and the end plates 32 and 33- and embeds itself into the asbestos layers 137 which in turn force themselves into irregularities in the mating machined surfaces creating a tight sealing condition. The center section 31 :is an investment casting which is provided with fins 145 for better cooling the hydraulic liquid in the embodiment 30 via ambientair. The center section 31 has mounting apertures 146'thr'ough its flange portions on its opposite ends which are aligned with apertures 148 and 149 in the end plates 32 and 33, respectively, by which the embodiment 30 may be rear or front mounted as desired. FIGS. 2 and 8 show the embodiment 30 rear mounted on suitable structure 147 via socket head fasteners 152 which are engaged by locknuts 153 held against rotation by the walls of section 31. FIG. 5 shows the embodiment 30 rear mounted on structure 151 by fasteners 150. FIG. 6 shows the embodiment 30 front mounted on structure 154 by fasteners 155.
An inner pressure cylinder 34 defining a pressure chamber 35 is provided centrally of the center section 31 and held therein by retainer inserts 44 and 45 which are disposed in end plates 32 and 33, respectively. A portion of the insert 45 projects into an end of the cylinder 34 and is liquid-tight sealed in respect thereto by a bronze piston ring 113. A spring washer 46 of the three-wave type is provided between the cylinder 34 and the insert 44 to force the cylinder 34 against the insert 45 for positioning and to eliminate close tolerance machining. The cylinder 34 rotatably supports an outer cylinder 41 the purpose of which will appear hereinafter. The cylinder 34 slidably carries an hydraulic ram, generally designated 185, comprising a hard aluminum bronze sleeve 56 which is staked, as at 57, over the inner end of a piston rod 53 and liquid-tight sealed in respect to the cylinder 34 by a pair of piston rings 54 which are held in predetermined circumferential relationship with each other (i.e. so that the space at the ends of each, as at 180 in FIG. 21, are spaced apart from each other diametrically) by rivets 55, the heads of which are disposed in an annular groove 58. The inside diameter of the cylinder 34 is honed. Opposite its end in which the piston rod 53 operates the cylinder 34 is closed against flow of hydraulic liquid therefrom but not thereinto by a check valve 130 disposed in a bore 156 in the insert 45 and held therein by a'bowed retainer ring 134. The check valve 130 is liquid-tight sealed in the bore 156 by an O-ring 132 and backup rings 132 therefor. The cylinder 34 is provided with a groove 51 and four equally circumferentially spaced radial apertures 52 which (together with three such spaced radial apertures 50 in the cylinder 41) provide free travel of the piston 185 for aninitial portion (about one-third) of its travel. Behind its piston rings 54 the piston 185 is relieved, as at 157, for accommodating displaced hydraulic liquid via equally circumferentially spaced radial apertures 114 in the cylinder 34. The cylinder 34 is also provided with six longitudinally spaced flats 38 machined in its outer surface which define a like number of cavities between itself and the cylinder 41. In each such flat 38 are formed a pair of spaced radial apertures 37. The flats 38 and apertures 37 together with other cooperating structure including that on the cylinder 47 affect travel of the piston 185 for the remaining portion (about two-thirds) of its travel. At the end of such travel the piston 185 assumes'the extreme retracted position shown for it in dotted outline in P16. ,7. Such cooperating structure includes honed finishes on the mating surfaces of the cylinder 34 (its 0D.) and of the cylinder 41 (its ID.) and six longitudinally spaced through-slots 40 formed through the wall of the cylinder 41 in annular grooves 49 therein. The slots 40 constitute metering orifices and are longitudinally centrally aligned in respect to the cavities defined by the flats 38 and form therewith variable area metering orifices 39 which are adjustable in area by virtue of the rotatable disposition of the cylinder 41. The maximum area position of the metering orifices 39 occurs when the slots 40 are fully open in respect to the cavities defined by the flats 38 as shown in FIG. 8. The minimum area position of such metering orifices 39 occurs when the slots 40 are maximumly closed in respect t o the cavities defined by the flats 38. FIG; 16 shows such minimum area position from which it can be noted that such variable area meteringorifices 39 are never fully closed to protect against breakage of parts of the embodiment 30 as well as of the impacting structure intended to be d ecelerated. Flow of hydraulic liquid out of the variable area metering orifices 39 is into an intermediate relief chamber 42 formed in the center section 31 concentrically about the cylinderv 34 and also therebeneath as shown in FIGS. 7 and -8. Rotation of the cylinder 41 is accomplished by a transversely disposed driftless gear train including a worm 87 fast (via pin 90 and shoulder 89) on a shaft 86 rotatably supported in a bore 102 in the center section 21 and in a retainer insert 91. The bore 102 is liquid-tight sealed in respect to theoutside by an O-ring 94 and a pair of backup rings 95 on opposite sides thereof. The insert 91 in turn is held fast in a bore 99 in the center section 37 via fasteners 92 which bore 99 is similarly sealed by an O- ring 97 and a pair of backup rings 98. The portion of the shaft 86 carried in the insert 91 is liquid-tight sealed in respect to the outside via an O-ring 96. A knurled knob 85 is carried fast on an end of the shaft 86 (such end being square in cross section over the portion 100 thereof and having a tapped aperture for engaging the flat head screw 101) and a pinion gear 93 is carried fast on its opposite end. The pinion gear 93 meshes with a gear 103 which is rotatably supported on the center section 21 via a shoulder screw 104. The gears 93 and 103 are sealed against entrance of foreign matter by a seal 105 which is preferably of oil'resistant material such as nitrile rubber. The gear 103 is graduated on its outside face (FIG. 1) and a reference mark 106 is provided on the outside wall of the center section 31 to serve as a reference in respect to the rotated position of the gear 103. Zero and designate,
respectively, the maximum and minimum restriction positions for the variable metering orifice 39. The worm 87 meshes with a gear segment 88 which is carried fast on a member 107 fastened to the cylinder 41 via drive studs 108 and welds as shown. The member 107 has a forked portion 259 which projects outwardly of the gear segment 88 and embraces the worm 87 to position the outer cylinder 41 axially in respect to the pressure cylinder 34 during assembly. The forked portion 159 centers the gear segment 88 in respect to the worm 87. A full 360 revolution of the knob 85 rotates the cylinder 41 6 circular degrees and the graduated face gear 103 50 circular degrees. Maximum rotation of the cylinder 41 is 30 circular degrees corresponding to five full revolutions of the knob 85 and 250 circular degrees of revolution of the gear 203 (corresponding to movement of the gear between its zero setting and its maximum setting as at 115). Limitation of rotation of the cylinder 41 to its maximum of 30 circular degrees is accomplished by an opensided slot 126 in an end of the cylinder 41 and a pin 48 projecting from the cylinder 34 so as to operate in the slot 1 16. For this reason the cylinder 34 must be circumferentially located during assembly in respect to the cylinder 41 which is accomplished by a locating pin 47 which is disposed in a slot 160 in the cylinder 34 and projects through the insert 45 into the end plate 33.
Flow of hydraulic liquid from the intermediate chamber 42 occurs into a reservoir 36 via passageways 162, 43 and 163 formed in the end plate 33. A portion of the insert 45 projects into the passageway 43 and is provided with a throughout 229. for passing hydraulic liquid through the interruption in the passageway 43 occasioned by the presence of such projecting portion of the insert 45. The open end of the passageway 43 is closed by a plug 139. The reservoir 36 is formed by a honed liner 64 disposed in a bore 65 in the center section 31 above the chamber 42 and a piston, generally designated 166, slidably carried in the liner 64. The-liner 64 is held in place in the bore 65 by an annular retainer insert 72 and between the two of them is a spring washer 78 of the three-wave type employed to position the liner against end plate 33 and to eliminate close tolerance machining. An O-ring 79 and backup ring 80 therefor form aliquid tight seal for the liner 64 in respect to the bore 65. The insert 72 extends through the end plate 32 via a bore 167 therein concentric with the bore 65 and in turn holds another insert 73 which has intersecting longitudinal 168 and transverse 169 passageways therein for purposes which will appear. The insert 73 has an annular shoulder 74 against which one end of a compression spring 59 operates, the other end of which operates against another insert 66 which is a part of the piston 166. The latter is made in separable component assemblies one of which comprises an outer piston sleeve 60 which is liquid-tight sealed in respect to the liner 64 by a U-cup sealed 62 and backup ring 63 therefor. An advance located piston ring 61 takes up shock and protects the U-cup seal 62 from high shock pressures exerted against the piston 166. 1t also compensatesfor heat andpressure expansions of the liner 64. The other component assembly of the piston 166 comprises a stainless .steel valve stem; 70. held against the insert 66 by a compression spring 69v which operates against a retainer ring 71 on an end of the valve stem 70 and against an end of the insert 66. The opposite ends of the insert 66 and the stem 70 are liquid-tight sealed in respect to each other and in respect to the piston sleeve 60 by means 67 in the form of a square-cut seal ring. The chamber in the liner 64 behind the piston 166 is designated 68 and is vented to atmosphere exterior of the embodiment 30 via four equally circumferentially space radial apertures 75 and an annular groove 76 in the liner 64 and by three 90 circumferentially spaced radial apertures 77 in the center section 31. The passageways 168 and 169 in the insert 73 also vent the chamber 68.
The piston rod 53 is chrome plated and operates in a bronze bearing 117 press-fitted into a bore 158 in a protrusion170 formed on the front of the end plate 32 and beyond the hearing 117 is liquid-tight sealed in respect to displaced hydraulic liquid by mechanism disposed in a bore 169 in said protrusion 170 which includes a Utype packing seal 121 about the piston rod 53 and backup ring 122 therefor and an O-ring 119 about the bore 169 and backup rings therefor which are held in place by a retainer insert 118. Said mechanism also includes a wiper 123 for the piston rod which is held in place by a retainer insert 124. A bowed retainer ring 125 locks said mechanism in place inthe bore 169. An enlarged. bore 171 is formed in the protrusion 170 outwardly of the bore 169 to receive a cap 126 carried on the freeend of the piston rod 53 and made fast thereto by a prong ring,1 27. The end cap 126 is slotted, as at 178, to provide access to the prong ring 127 to squeeze the same for purposes of removing or replacing the end cap on said free end of the piston rod53'. For cooperation with the end cap 126 an impact plate 140 is provided for affixation by suitable fasteners 177 to moveable structure, as at 172, which is intended to impact against the piston rod 53. The engaging face of the impact plate 140 is arcuately contoured, as at 173, to minimize side thrust on the piston rod 53 and its bearing 117.
The embodiment 30 is filled with hydraulic oil via an oil fitting 143 threadably engaged in an aperture 84 in the end plate 32. (If the embodiment 30 is front mounted the oil fitting 184 in the end plate 33 may beused.) During filling the ram 185 preferably is forcefully held in its extreme retracted position. Hydraulic oil is forced into the embodiment 30 with the ram 185 so held until the intermediate relief chamber 42 and the reservoir 36 are completely filled as well as the space behind the ram 185 which occurrence is signaled by flow of hydraulic oil out of the chamber68 via the aperture 77 and/or the passageways 168. During filling of the embodiment 30 flow of hydraulic oil occurs from the reservoir 36 into the chamber 68 as shown in FIG. 19 by the unseating of the valve stem 70from the square-cut seal 67 which occurs from continued travel of the piston sleeve 60 after the stem 70 bottoms against the insert 73. The insert 66 has an axial bore 82 and diametrically disposed radial apertures 83 to provide for such flow of hydraulic oil during filling of the embodiment 30. A relief passageway 81 behind the seal ring 67 communicates with the bore 72 to insure that the seal 67 will remain seated in the event of sudden opening of the valve stem 70. Filling of the embodiment 30 is terminated as soon as hydraulic oil is noted to flow out of the apertures 77 and/or the passageway 168. The system is vented by loosening self-sealing vent screws and 136, respectively, in passageways 275 (in end plate 33) and 176 (in end plate 33). Further vent screws 18] (in end plate32) and 182 and 183 (in opposite sides of center section 31) and 186 and 187 (in opposite sides of the end plate 33) are provided to accommodate the multiple positions in which the embodiment 30 may be disposed in use. These multiplely located vent apertures permit proper bleeding of the embodiment 30 at any angle at which it may be mounted. After filling, the reservoir piston 166 moves to the left to the position shown for it in FIG. 7 and in doing so moves the ram 185 to its extreme extended position shown for it in FIG. 7.
in operation of the embodiment 30 the impacting force which is sought to be absorbed in transmitted to the piston rod 53 preferably via the impact plate and such force causes the piston to move in its energy-dissipating power stroke. The initial portion of the travel of the piston 185 is under substantially free flow conditions as hydraulic oil is forced out of the pressure chamber 35 without restriction via the apertures 52 and the annular groove 51 in the cylinder 34 and the apertures 50 in the cylinder 41. The remaining portion of the travel of the piston 185 (after the same closes off the apertures 52) is restricted from the flow restriction presented by the variable area metering orifices 39 to the flow of hydraulic liquid from the pressure chamber 35 into the intermediate relief chamber 42. Such flow of hydraulic liquid into the chamber 42 displaces hydraulic liquid therein and in the reservoir 36 which causes the piston 166 to move against the urging of the spring 59. Some hydraulic liquid displaced from the chamber 32 is forced behind. the piston 185 via the apertures 114 in the cylinder 34 and lubricates the piston rod 43 in its bearing 107.
The stiffness with which the piston 185 absorbs the shock of the impacting force can be varied to suit the particular application by rotating the knob 75 to adjust the area opening presented by the variable area metering orifices 39. A user can tell to what degree of cushioning the embodiment 30 is set for simply from glancing at the setting on the graduated face of the gear 103. Upon removal of the impacting force from the piston 185 hydraulic liquid flows from the reservoir 36 under the force of the piston 166 into the pressure chamber 35 without restriction via the check valve 130 to return the piston 185 rapidly to its rest position shown in full lines in FIG. 7.
The system is unaffected by hydraulic losses due to the hydraulic liquid stored in the reservoir 36 and the continual pressure maintained by the piston 166 on the hydraulic liquid in the chamber 42 and in the pressure chamber 35. The piston 166 continually maintains a nearly steady oil pressure in the system which increases the useful life of the seals.
It will thus be seen that there has been provided by our invention an industrial-type hydraulic shock absorber in which the object hereinabove set forth together with many other thoroughly practical advantages has been successfully achieved. While preferred embodiments of the invention have been shown and described it is to be understood that variations and changes may be resorted to without departing from the spirit of the invention as defined by the appended claims.
We claim:
1. Means in energy dissipating hydraulic systems for dissipating the energy of impacting forces comprising:
a. an hydraulic ram chamber and an hydraulic ram operative out of one end thereof, said ram having a single energy dissipating power stroke in respect to an impacting force acting in one direction thereon;
b. an hydraulic reservoir, a piston operative therein, and
yieldable means operative upon said piston;
c. means interconnecting said ram chamber and said reservoir so that a transfer of hydraulic liquid occurs in opposition to said yieldable means from said ram chamber to said reservoir under relatively free flow conditions for a first part of said power stroke and under flow restriction conditions for the remainder thereof;
. said ram chamber provided with axially spaced orifices all but the last of which are closed off progressively by said hydraulic ram in its movement to its retracted position in said ram chamber during said power stroke; the first of said orifices being free flow orifices through which hydraulic liquid flows from said ram chamber to said reservoir under free flow conditions for a first part of said power stroke and the remainder. of said orifices being flow restriction orifices through which hydraulic liquid flows from said ram chamber to said reservoir under flow restriction conditions for the remainder of said power stroke; said hydraulic ram being fully retracted without closing off the last of said flow restriction orifices;
e. said reservoir piston operative at the end of said power stroke to effect return of hydraulic liquid from the reservoir to the ram chamber to return the ram in the opposite direction in a single rapid return stroke thereof; and
f. said interconnecting means including unidirectional valve means at the end of said ram chamber opposite that from which said ram operates which is closed during said power stroke and open to the ram chamber during said return stroke.
2. Means according to claim 1 further comprising means for varying the area of said flow restriction orifices comprising concentric cylinders which have communicating flow restriction orifices and means for rotating said cylinders relative to each other to vary the effective flow area of said flow restriction orifices to alter the cushioning efiect of said power stroke in accordance with the magnitude of the impacting force.
3. Means according to claim 2 in which the outer cylinder is provided with axially spaced slits and means for rotating said outer cylinder relative to the inner cylinder to vary said effective flow area.
4. Means according to claim 1 further comprising housing means for the reservoir and said chamber having cooling fins on the exterior thereof for transfering heat from said hydraulic liquid to ambient air. during both said power and return strokes for cooling purposes.
5. Means according to claim 1 in which the reservoir piston is provided with axially separable valve means permitting flow of hydraulic liquid through said piston during filling of said reservoir to prevent overfilling thereof.v
6. An hydraulic shock absorber according to claim 1 having housing means with fins on its exterior for cooling hydraulic liquid therein via ambient air.
7. An hydraulic shock absorber according to claim 1 in which said ram includes a hard aluminum bronze piston sleeve and a pair of piston rings therefor and held thereon in diametrically opposed circumferential relationship to each other.
8. An hydraulic shock absorber according to claim 1 further comprising an end cap for the free end of said ram and resilient releasable holding means for said end cap.
9. An hydraulic shock absorber according to claim 8 further comprising an arcuately contoured impact plate for use in conjunction with said end cap for reducing side thrust on said ram.
10. An hydraulic shock absorber according to claim 1 in which the wall of said reservoir is provided by a honed liner and in which said yieldable means comprises compression spring means operating on the reservoir piston to maintain the hydraulic liquid in the reservoir under a yieldable pressure.
11. An hydraulic shock absorber according to claim 9 in which the reservoir piston is provided with liquid-tight seal means in respect to said liner and a piston ring in advance of said seal means to absorb surge hydraulic pressures on the reservoir piston.
12. An hydraulic shock absorber according to claim 3 in which said means for rotating said outer cylinder comprises a driftless gear train including a worm'and a manually rotated knurled knob.
13. An hydraulic shock absorber according to claim 12 in which graduated readout means are provided on the gear train for determining the setting of said metering orifice.
14. An hydraulic shock absorber according to claim 13 in which said gear train includes a gear segment meshing with said worm and a bifurcated mechanism centering said gear segment in respect to said worm.
15. An hydraulic shock absorber according to claim 1 in which said reservoir piston comprises valve means including an axially moveable valve stem and liquid-tight seal means therefor and means to open said valve means when the reservoir piston reaches a predetermined position in its travel during filling of the shock absorber to prevent overfilling thereof.
16. An hydraulic shock absorber according to claim 3 in which said inner cylinder has a series of flats on its exterior circumferential surface and radial apertures through its wall intersection each such flat.
17. An hydraulic shock absorber according to claim 3 in which said flow restriction orifice on said outer cylinder comprises a series of annular grooves and a tangential flow restriction slot through its wall intersecting each such groove.
18. An hydraulic shock absorber according to claim 1 in which liquid-tight seal means are provided between said unidirectional valve means and said ram chamber comprising piston ring means operative against the wall of said ram chamber.
19. An hydraulic shock absorber according to claim 1 which is so constructed as to be operative in any position in which it may be mounted, and manually openable normally closed vent means at different locations on the body of said shock absorber so that the hydraulic liquid therein can be air-bled in every such mounted position of said shock absorber.
20. Process in energy dissipating hydraulic systems for dissipating the energy of impacting forces comprising:
a. applying pressure in a single energy dissipating power stroke to hydraulic liquid in a hydraulic ram chamber via an impacting force acting in one direction upon an hydraulic ram operating out of one end of said ram chamber;
b. transferring hydraulic liquid from said ram chamber to hydraulic liquid in an hydraulic reservoir maintained under yieldable pressure;
c. said transferring of hydraulic liquid being accomplished by movement of an hydraulic ram to its retracted position in said rarn chamber during said power stroke by said ram progressively closing off all but the last of axially spaced orifices in said ram chamber; the first of said orifices being free flow orifices through which hydraulic liquid flows from said ram chamber to said reservoir under free flow conditions for a first part of said power stroke and the remainder of said orifices being flow restriction orifices through which hydraulic liquid flows from said ram chamber to said reservoir under flow restriction conditions for the remainder of said power stroke; said hydraulic ram being fully retracted without closing off the last of said flow restriction orifices; and
at the end of said power stroke applying pressure to said hydraulic liquid in said ram chamber by effecting return of hydraulic liquid thereto from said reservoir under said yieldable pressure and under free flow conditions to produce a return force acting in the opposite direction in a single return stroke.
21. Process according to claim in which said ram chamber and said reservoir are filled by transferring hydraulic liquid under pressure into said reservoir until it visibly flows out therefrom.
22. Process according to claim 20 in which a flow restricting orifice is moved relative to a cavity to alter the cushioning effect of said power stroke in accordance with the magnitude of the impacting force.
23. Process according to claim 22 in which said flow restricting orifice is rotated relative to said cavity between maximum and minimum area positions corresponding, respectively, to maximum and minimum flow of hydraulic liquid through said cavity and said flow restricting orifice.
24. Process according to claim 20 further comprising transfering heat from said hydraulic liquid to ambient air during both said power and return strokes for cooling purposes.
25. An industrial type hydraulic shock absorber having a center section and end plates bolted to said center section at opposite ends thereof, an hydraulic ram chamber defined by a cylinder fast in said center section between said end plates, an hydraulic ram operative in said ram chamber and out of one of said end plates, said ram having a single energy dissipating power stroke in respect to an impacting force acting in one direction thereon, an hydraulic reservoir defined by a chamber in said center section, a piston slidable insaid reservoir and yieldable means operative upon said piston, means interconnecting said ram chamber and said reservoir so that a transfer of hydraulic liquid occurs in opposition to said yieldable means from said ram chamber to'said reservoir under free flow conditions for a first part of said power stroke and under flow restriction conditions for the remainder thereof, said ram chamber provided with axially spaced orifices all but the last of which are closed off progressively by said hydraulic ram in its movement to its retracted position in said ram chamber during said power stroke. The first of said orifices being free flow orifices through which hydraulic liquid flows from said ram chamber to said reservoir under free flow conditions for a first part of said power stroke and the remainder of said orifices being flow restriction orifices through which hydraulic liquid flows from said ram chamber to said reservoir under flow restriction conditions for the remainder of said power stroke. Said hydraulic ram being fully retracted without closing off the last of said flow restriction orifices, said reservoir piston operative at the end of said power stroke to effect return of hydraulic liquid from the reservoir to the ram chamber to return the ram in the opposite direction in a single return stroke thereof, said interconnecting means including unidirectional valve means closed during said power stroke and open to the ram chamber during said return stroke.
26. An hydraulic shock absorber according to cla1m 25 m which said ram chamber is defined by a first cylinder fast in said center section between said end plates, and further comprising an intermediate relief chamber defined by a cavity in said center section and a second cylinder concentric about and supported for rotation on said first cylinder, flow restriction means in said second cylinder providing a variable area metering orifice for flow of hydraulic liquid between said ram chamber and said intermediate relief chamber, and means for rotating said second cylinder to vary the effective area of said metering orifice.
27. An hydraulic shock absorber according to claim 26 in which resilient thrust washer means are provided between said first cylinder and one of said end plates.
28. An hydraulic shock absorber according to claim 25 in which the center section and end plates are sealed in respect to each other by gasket means comprising a metal layer sandwiched between a pair of asbestos layers.
29. An hydraulic shock absorber according to claim 25 in which each end plate is provided with mounting means by which the shock absorber can be front or rear mounted in respect to stationary structure.

Claims (28)

1. Means in energy dissipating hydraulic systems for dissipating the energy of impacting forces comprising: a. an hydraulic ram chamber and an hydraulic ram operative out of one end thereof, said ram having a single energy dissipating power stroke in respect to an impacting force acting in one direction thereon; b. an hydraulic reservoir, a piston operative therein, and yieldable means operative upon said piston; c. means interconnecting said ram chamber and said reservoir so that a transfer of hydraulic liquid occurs in opposition to said yieldable means from said ram chamber to said reservoir under relatively free flow conditions for a first part of said power stroke and under flow restriction conditions for the remainder thereof; d. said ram chamber provided with axially spaced orifices all but the last of which are closed off progressively by said hydraulic ram in its movement to its retracted position in said ram chamber during said power stroke; the first of said orifices being free flow orifices through which hydraulic liquid flows from said ram chamber to said reservoir under free flow conditions for a first part of said power stroke and the remainder of said orifices being flow restriction orifices through which hydraulic liquid flows from said ram chamber to said reservoir under flow restriction conditions for the remainder of said power stroke; said hydraulic ram being fully retracted without closing off the last of said flow restriction orifices; e. said reservoir piston operative at the end of said power stroke to effect return of hydraulic liquid from the reservoir to the ram chamber to return the ram in the opposite direction in a single rapid return stroke thereof; and f. said interconnecting means including unidirectional valve means at the end of said ram chamber opposite that from which said ram operates which is closed during said power stroke and open to the ram chamber during said return stroke. . 2. Means according to claim 1 further comprising means for varying the area of said flow restriction orifices comprising concentric cylinders which have communicating flow restriction orifices and means for rotating said cylinders relative to each other to vary the effective flow area of said flow restriction orifices to alter the cushioning effect of said power stroke in accordance with the magnitude of the impacting force.
3. Means according to claim 2 in which the outer cylinder is provided with axially spaced slits and means for rotating said outer cylinder relative to the inner cylinder to vary said effective flow area.
4. Means according to claim 1 further comprising houSing means for the reservoir and said chamber having cooling fins on the exterior thereof for transfering heat from said hydraulic liquid to ambient air during both said power and return strokes for cooling purposes.
5. Means according to claim 1 in which the reservoir piston is provided with axially separable valve means permitting flow of hydraulic liquid through said piston during filling of said reservoir to prevent overfilling thereof.
6. An hydraulic shock absorber according to claim 1 having housing means with fins on its exterior for cooling hydraulic liquid therein via ambient air.
7. An hydraulic shock absorber according to claim 1 in which said ram includes a hard aluminum bronze piston sleeve and a pair of piston rings therefor and held thereon in diametrically opposed circumferential relationship to each other.
8. An hydraulic shock absorber according to claim 1 further comprising an end cap for the free end of said ram and resilient releasable holding means for said end cap.
9. An hydraulic shock absorber according to claim 8 further comprising an arcuately contoured impact plate for use in conjunction with said end cap for reducing side thrust on said ram.
10. An hydraulic shock absorber according to claim 1 in which the wall of said reservoir is provided by a honed liner and in which said yieldable means comprises compression spring means operating on the reservoir piston to maintain the hydraulic liquid in the reservoir under a yieldable pressure.
11. An hydraulic shock absorber according to claim 9 in which the reservoir piston is provided with liquid-tight seal means in respect to said liner and a piston ring in advance of said seal means to absorb surge hydraulic pressures on the reservoir piston.
12. An hydraulic shock absorber according to claim 3 in which said means for rotating said outer cylinder comprises a driftless gear train including a worm and a manually rotated knurled knob.
13. An hydraulic shock absorber according to claim 12 in which graduated readout means are provided on the gear train for determining the setting of said metering orifice.
14. An hydraulic shock absorber according to claim 13 in which said gear train includes a gear segment meshing with said worm and a bifurcated mechanism centering said gear segment in respect to said worm.
15. An hydraulic shock absorber according to claim 1 in which said reservoir piston comprises valve means including an axially moveable valve stem and liquid-tight seal means therefor and means to open said valve means when the reservoir piston reaches a predetermined position in its travel during filling of the shock absorber to prevent overfilling thereof.
16. An hydraulic shock absorber according to claim 3 in which said inner cylinder has a series of flats on its exterior circumferential surface and radial apertures through its wall intersection each such flat.
17. An hydraulic shock absorber according to claim 3 in which said flow restriction orifice on said outer cylinder comprises a series of annular grooves and a tangential flow restriction slot through its wall intersecting each such groove.
18. An hydraulic shock absorber according to claim 1 in which liquid-tight seal means are provided between said unidirectional valve means and said ram chamber comprising piston ring means operative against the wall of said ram chamber.
19. An hydraulic shock absorber according to claim 1 which is so constructed as to be operative in any position in which it may be mounted, and manually openable normally closed vent means at different locations on the body of said shock absorber so that the hydraulic liquid therein can be air-bled in every such mounted position of said shock absorber.
20. Process in energy dissipating hydraulic systems for dissipating the energy of impacting forces comprising: a. applying pressure in a single energy dissipating power stroke to hydraulic liquid in a hydraulic ram chamber via an impacting force acting in one Direction upon an hydraulic ram operating out of one end of said ram chamber; b. transferring hydraulic liquid from said ram chamber to hydraulic liquid in an hydraulic reservoir maintained under yieldable pressure; c. said transferring of hydraulic liquid being accomplished by movement of an hydraulic ram to its retracted position in said ram chamber during said power stroke by said ram progressively closing off all but the last of axially spaced orifices in said ram chamber; the first of said orifices being free flow orifices through which hydraulic liquid flows from said ram chamber to said reservoir under free flow conditions for a first part of said power stroke and the remainder of said orifices being flow restriction orifices through which hydraulic liquid flows from said ram chamber to said reservoir under flow restriction conditions for the remainder of said power stroke; said hydraulic ram being fully retracted without closing off the last of said flow restriction orifices; and d. at the end of said power stroke applying pressure to said hydraulic liquid in said ram chamber by effecting return of hydraulic liquid thereto from said reservoir under said yieldable pressure and under free flow conditions to produce a return force acting in the opposite direction in a single return stroke.
21. Process according to claim 20 in which said ram chamber and said reservoir are filled by transferring hydraulic liquid under pressure into said reservoir until it visibly flows out therefrom.
22. Process according to claim 20 in which a flow restricting orifice is moved relative to a cavity to alter the cushioning effect of said power stroke in accordance with the magnitude of the impacting force.
23. Process according to claim 22 in which said flow restricting orifice is rotated relative to said cavity between maximum and minimum area positions corresponding, respectively, to maximum and minimum flow of hydraulic liquid through said cavity and said flow restricting orifice.
24. Process according to claim 20 further comprising transfering heat from said hydraulic liquid to ambient air during both said power and return strokes for cooling purposes.
25. An industrial type hydraulic shock absorber having a center section and end plates bolted to said center section at opposite ends thereof, an hydraulic ram chamber defined by a cylinder fast in said center section between said end plates, an hydraulic ram operative in said ram chamber and out of one of said end plates, said ram having a single energy dissipating power stroke in respect to an impacting force acting in one direction thereon, an hydraulic reservoir defined by a chamber in said center section, a piston slidable in said reservoir and yieldable means operative upon said piston, means interconnecting said ram chamber and said reservoir so that a transfer of hydraulic liquid occurs in opposition to said yieldable means from said ram chamber to said reservoir under free flow conditions for a first part of said power stroke and under flow restriction conditions for the remainder thereof, said ram chamber provided with axially spaced orifices all but the last of which are closed off progressively by said hydraulic ram in its movement to its retracted position in said ram chamber during said power stroke. The first of said orifices being free flow orifices through which hydraulic liquid flows from said ram chamber to said reservoir under free flow conditions for a first part of said power stroke and the remainder of said orifices being flow restriction orifices through which hydraulic liquid flows from said ram chamber to said reservoir under flow restriction conditions for the remainder of said power stroke. Said hydraulic ram being fully retracted without closing off the last of said flow restriction orifices, said reservoir piston operative at the end of said power stroke to effect return of hydraulic liquid from the reservoir to the ram chamber to return the ram in the opposite direction in a singlE return stroke thereof, said interconnecting means including unidirectional valve means closed during said power stroke and open to the ram chamber during said return stroke.
26. An hydraulic shock absorber according to claim 25 in which said ram chamber is defined by a first cylinder fast in said center section between said end plates, and further comprising an intermediate relief chamber defined by a cavity in said center section and a second cylinder concentric about and supported for rotation on said first cylinder, flow restriction means in said second cylinder providing a variable area metering orifice for flow of hydraulic liquid between said ram chamber and said intermediate relief chamber, and means for rotating said second cylinder to vary the effective area of said metering orifice.
27. An hydraulic shock absorber according to claim 26 in which resilient thrust washer means are provided between said first cylinder and one of said end plates.
28. An hydraulic shock absorber according to claim 25 in which the center section and end plates are sealed in respect to each other by gasket means comprising a metal layer sandwiched between a pair of asbestos layers.
29. An hydraulic shock absorber according to claim 25 in which each end plate is provided with mounting means by which the shock absorber can be front or rear mounted in respect to stationary structure.
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Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4059175A (en) * 1975-05-06 1977-11-22 Dressell Jr Richard G Linear force shock absorber
FR2353759A1 (en) * 1976-05-25 1977-12-30 Mecman Ab HYDRAULIC SHOCK ABSORBER
FR2409424A1 (en) * 1976-04-28 1979-06-15 Dressell Richard FLUID SHOCK ABSORBER
US4174098A (en) * 1978-07-03 1979-11-13 Ace Controls, Inc. Shock absorber and mounting means therefor
WO1990012967A1 (en) * 1989-04-25 1990-11-01 Enertrols, Inc. Improved shock absorber
US20150076753A1 (en) * 2013-09-19 2015-03-19 Dadco, Inc. Overtravel Pressure Relief For A Gas Spring
US20150137435A1 (en) * 2013-09-19 2015-05-21 Dadco, Inc. Overtravel Pressure Relief For A Gas Spring
US10822005B2 (en) * 2018-03-12 2020-11-03 Twinco Manufacturing Co., Inc. Submersible switch point machine

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1664486A (en) * 1927-04-21 1928-04-03 Marquette Tool & Mfg Co Hydraulic cushion for sheet-metal presses
US3171640A (en) * 1961-12-15 1965-03-02 James V Perrone Hydraulic cushion and return device for dies

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1664486A (en) * 1927-04-21 1928-04-03 Marquette Tool & Mfg Co Hydraulic cushion for sheet-metal presses
US3171640A (en) * 1961-12-15 1965-03-02 James V Perrone Hydraulic cushion and return device for dies

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4059175A (en) * 1975-05-06 1977-11-22 Dressell Jr Richard G Linear force shock absorber
FR2409424A1 (en) * 1976-04-28 1979-06-15 Dressell Richard FLUID SHOCK ABSORBER
FR2353759A1 (en) * 1976-05-25 1977-12-30 Mecman Ab HYDRAULIC SHOCK ABSORBER
US4174098A (en) * 1978-07-03 1979-11-13 Ace Controls, Inc. Shock absorber and mounting means therefor
WO1990012967A1 (en) * 1989-04-25 1990-11-01 Enertrols, Inc. Improved shock absorber
US20150076753A1 (en) * 2013-09-19 2015-03-19 Dadco, Inc. Overtravel Pressure Relief For A Gas Spring
US20150137435A1 (en) * 2013-09-19 2015-05-21 Dadco, Inc. Overtravel Pressure Relief For A Gas Spring
US9447834B2 (en) * 2013-09-19 2016-09-20 Dadco, Inc. Overtravel pressure relief for a gas spring
US10822005B2 (en) * 2018-03-12 2020-11-03 Twinco Manufacturing Co., Inc. Submersible switch point machine

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