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US2463552A - High-pressure hydraulic system - Google Patents

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US2463552A
US2463552A US732043A US73204347A US2463552A US 2463552 A US2463552 A US 2463552A US 732043 A US732043 A US 732043A US 73204347 A US73204347 A US 73204347A US 2463552 A US2463552 A US 2463552A
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pressure
ram
cylinder
chamber
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US732043A
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Donald H Newhall
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F15FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
    • F15BSYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
    • F15B3/00Intensifiers or fluid-pressure converters, e.g. pressure exchangers; Conveying pressure from one fluid system to another, without contact between the fluids

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  • This invention relates to a high-pressure hydraulic system and more particularly to one adapted for developing a continuous flow of liquids-or gases at a steady high pressure.
  • Fig. 1 shows a schematic arrangement for a series of single-acting hydraulic-intensifier units connected in functional parallelism.
  • Fig. 2 shows a schematic arrangement for a series of double-acting hydraulic intensifier units connected in functional parallelism.
  • Fig. 1 there is shown-a plurality of intensifier units each consisting of an outer structure having a t p and bottom circular plate 2 and 2a bolted as shown at 3 in cylindrical relationship by tie rods 4.
  • a cylinder 5 is' irigidly mounted tobottom plate 2a and apiston member 6 is rigidly secured to-top. plate 2 in axial alignment with cylinder 5.
  • a cylindricalram member I having an axial cylindricalreces-s 8 is mounted for reciprocating mnovement within cylinder 5.
  • Piston 5 and ram 1 cooperate in a piston-cylinder relationshipand ram 1 and cylinder 5 also cooperate in a piston-cylinderrelationship.
  • ram 1 functions as a piston in its relation to cylinder 5 and as a cylinder in its relation topiston 6.
  • Cylindrical recess 8 thus defines a high-pressure'chamber for the pressure fluidv of the system while the interior of cylinder 5 act as amedium-pressure chamber 9 for the operating fluid ofv the system.
  • a pump J0 provides a constant supply of fluid under medium pressure for operation of the intensifiertunits.
  • Such. fluid is obtained from a reservoir ll connected to pump) by a feed line l2.
  • a relief linel3 also communicates with reservoir l l for the. passageof operating fluid when the intensifier unit is in the down stroke.
  • the fluid ispumpedthrough a supply line H and then through aconventional solenoid-operated valve 15 to a-lead-in line. 16 whichextendsinto medium-pressure chamber 9.
  • Relief line. l 3 communicates withlead-in line. l6 and includes a secondsolenoid-operated valve l1 which when open returns fluidto reservoir II.
  • an auxiliary pump. I8 is provided for furnishing fluid at low pressure through asupply line f9, such fluid being eventually delivered from the intensifier units at the high pressure for which the system is designed.
  • This fluid is originally obtained from a reservoir .20, connectedtopump. l8 by a feed line 2
  • a.safety line 22 having a safety valve 23 therein, by-passes. pump l8, and prevents any dangerous build-up of pressure.
  • .fiupply line I9 is provided with check..valve-s 24, one for each unit and arranged to permit the flow of fluid through piston li intov chamber 8 but designed to prevent back flow into pump it.
  • a manifold supplyline 25 having check valves 26 therein, one for eachintensifier unit to prevent back-flow, of v.fluid through piston 6, provides a passage forthe highpr'essure fluid from chamber -1 Ma o d-lin l endsu ply line s bot co municate with a lead-in line 21' which extends through piston 6 into chamber 8 of each intensifier unit.
  • a pressure gage 28 is included in manifold supply line 25 for recording the pressure available for the work to be done.
  • a pair of motor driven multiple-point rotary switches 29 of conventional design are provided to operate valves and I! in proper sequence in such manner that at no time will all the intensifier units be in a pump-down phase or pumpup phase. Rather the units should operate in a progressive overlapping sequence. It should be understood that there are a variety of means adapted for the proper synchronization of the units, and this invention is not intended to cover any particular one of such means.
  • each intensifier unit begins with valve 55 opening and valve ll closing.
  • fluid from reservoir H is admitted under medium pressure into chamber 9.
  • ram 1 moves upward compressing the fluid present in chamber 8 to build up a pressure directly proportional to the ratio of the pressure areas of ram 1 and piston 6.
  • This highpressure fluid is thus forced out of chamber 8 through lead-in line 21 and past check valve 25 and into manifold supply line 25.
  • Check valve 24 prevents any of this fluid from being forced into supply line 19 and therefore into pump Hi.
  • rotary switches 29 open valve I! and close valve l5.
  • check valve 24 opens and check valve 26 closes due to the absence of high pressure fluid in lead-in line 21.
  • the fluid in chamber 9 is permitted to drain back to reservoir l I and ram 1 consequently moves downwardly.
  • the fluid being pumped from reservoir 20 under low pressure through piston 6 into chamber 8 in preparation for the next stroke of the intensifier unit helps return ram 1 to the starting position for the next cycle of operation.
  • a double-pole safety switch 30 mounted in each intensifier unit prevents any further action of that particular unit in the event of a breakdown.
  • a contact 46 projects from ram 1 and operates switch 30 in the event ram 1 is forced beyond its normal length of stroke in either direction.
  • each unit consists of a cylinder 3i having oppositely disposed pistons 32 and 32a each rigidly secured within the interior of cylinder 3
  • a cylindrical ram member 33 having axial cylindrical recesses 3:3 and 34a in each end is mounted for reciprocating movement in cylinder 3
  • medium-pressure chambers 35 and 35a and high-pressure chambers 34 and 34a are defined as ram 33 reciprocates.
  • a low-pressure pump 36 supplies fluid to chambers 34 and 34a and a medium pressure pump 31 supplies fluid to chambers 35 and 35a in a manner similar to that explained in Fig. 1.
  • and Ma also operate in the manner described for Fig. 1.
  • valves 49 and Mia are open and valves 4
  • the fluid in chamber 35a is thus compressed and forced out at a high pressure thereby closing check valve 39a and opening check valve 38a when the pressure developed is in excess of that already existing in a manifold line d2.
  • a safety valve 43 for pump 36 and safety switches 4% for each intensifier unit operate in a manner similar to that shown in Fig. 1.
  • additional emergency solenoid operated valves are provided for immediate relief flow of fluid from each intensifier unit in the event safety switches M do not reverse valves 40, Ma, it and 43a quickly enough, thereby preventing damage to such intensifier unit which fails to operate normally.
  • Each intensifier unit is grounded to permit such emergency relief action.
  • the normal closing and opening of the regular solenoid-operated valves is controlled by a motor d en multiple-point rotary switch Ll! of conventional design.
  • a hydraulic system for delivering a continuous and steady flow of fluid at high pressure comprising in combination, a series of hydraulic intensifier units having a compression stroke and a relief stroke, each of said intensifier units having a medium pressure chamber and a high pressure chamber, said medium pressure chamber having a supply valve adapted to supply medium pressure fluid thereto during said compression stroke and a relief valve adapted to permit escape of said medium pressure fluid therefrom during said relief stroke, a first check valve for said high pressure chamber adapted to permit entry of low pressure fluid thereto during said relief stroke, a second check valve for said high pressure chamber adapted to permit delivery of fluid therefrom during said compression stroke, and means for successively adjusting said supply valves and said relief valves whereby said hydraulic intensifier units are operated in progressive overlapping sequence with a plurality of said intensifier units in compression stroke at all times.
  • a hydraulic system for delivering a continuoils and steady flow of fluid at high pressure comrising combination, a series of hydraulic cylinders having oppositely disposed cylinder heads, each of said cylinders being provided with oppositely disposed fixed pistons extending inwardly toward one another in axial alignment from said cylinder heads, a ram reciprocally engaged in each of said cylinders in a piston-cylinder relation,
  • each of said hydraulic cylinders thereby comprising a pair of oppositely acting said compression units arranged whereby the compression phase for one of said compression units corresponds to the relief phase of the other end oppositely acting said compression unit, a supply valve for each medium pressure chamber adapted to supply medium pressure fluid thereto, thereby instituting movement of said ram whereby each of said recesses therein cooperates with said corresponding oppositely disposed fixed piston in compression phase, a relief valve for each of said medium pressure chambers adapted to permit escape of said medium pressure fluid therefrom during said relief phase, a first check valve for each of said high pressure chambers adapted to permit entry of low pressure fluid there

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  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Fluid-Pressure Circuits (AREA)

Description

March 8, 1949. Q NEWHALL 2,463,552
HIGH-PRES SURE HYDRAULIC SYSTEM Filed March 5, 1947 I 2 Sheets-Sheet 1 1:1 :nnld 1-1.. Newhull' j ffioz iwmmmu S March 8, 1949. n. H. NEWHALL 2,463,552
HIGH-PRESSURE HYDRAULIC SYSTEM 2 Sheets-Shea} 2 Filed March 3, 1947 I II N ii' im' Patented Mar. 8, 1949 -=UNlTED STATES PATENT "OFFICE (Granted under the act of. March 3, .1883, as amended April 30, 1928; 370 O. G. 757) 2 Claims.
The invention described in the following specification and claims may be manufactured and used by or for the Government for governmental purposes without the payment to me of any royalty thereon.
This invention relates to a high-pressure hydraulic system and more particularly to one adapted for developing a continuous flow of liquids-or gases at a steady high pressure.
In many applications where excessively high hydraulic pressures are required, steadiness of pressure in the flow of liquids or gases is of reat importance but is diflicult to attain.
The fixation of nitrogeniorthe manufacture of explosives is but one of the many applications in which a continuous pressure is particularly invaluable. Without a steady and continuous flow of fluid or gas at high pressure to areactor vessel, the reactionsdesired would necessitate the handling of the chemicals involved in batch lots, a procedure which is obviously expensive and time-consuming. Another important application where a constant flow of fluids or gasesat extremelyhigh pressures is essential lies. in-the art of prestressing the bore of cannon barrels by cold working to effect an increased yield strength of the steel constituting such barrels.
It is therefore an object of this invention to provide a system whereby very high hydraulic pressures can be generated and whereby such pressures will yield a steady flow of fluid.
It is a particular object of this invention to provide a system comprising a series of hydraulic intensifier units arranged in functional parallelism and operated in a progressive overlapping se quence to obtain a steady flow of fluid-at high pressures.
The specific nature of the invention-as well as other objects and advantages thereof-will clearly appear from a description of a preferredembodiment as shown in the accompanying drawings in which:
Fig. 1 shows a schematic arrangement for a series of single-acting hydraulic-intensifier units connected in functional parallelism.
Fig. 2 shows a schematic arrangement for a series of double-acting hydraulic intensifier units connected in functional parallelism.
In the preferred embodiment of Fig. 1 there is shown-a plurality of intensifier units each consisting of an outer structure having a t p and bottom circular plate 2 and 2a bolted as shown at 3 in cylindrical relationship by tie rods 4.
Within this structure, a cylinder 5 is' irigidly mounted tobottom plate 2a and apiston member 6 is rigidly secured to-top. plate 2 in axial alignment with cylinder 5. A cylindricalram member I having an axial cylindricalreces-s 8 is mounted for reciprocating mnovement within cylinder 5. Piston 5 and ram 1 cooperate in a piston-cylinder relationshipand ram 1 and cylinder 5 also cooperate in a piston-cylinderrelationship. It i apparent therefore that ram 1 functions as a piston in its relation to cylinder 5 and as a cylinder in its relation topiston 6. Cylindrical recess 8 thus defines a high-pressure'chamber for the pressure fluidv of the system while the interior of cylinder 5 act as amedium-pressure chamber 9 for the operating fluid ofv the system.
A pump J0 provides a constant supply of fluid under medium pressure for operation of the intensifiertunits. Such. fluid is obtained from a reservoir ll connected to pump) by a feed line l2.- A relief linel3 also communicates with reservoir l l for the. passageof operating fluid when the intensifier unit is in the down stroke. The fluid ispumpedthrough a supply line H and then through aconventional solenoid-operated valve 15 to a-lead-in line. 16 whichextendsinto medium-pressure chamber 9. Relief line. l 3 communicates withlead-in line. l6 and includes a secondsolenoid-operated valve l1 which when open returns fluidto reservoir II.
.In the preferred embodiment, an auxiliary pump. I8 is provided for furnishing fluid at low pressure through asupply line f9, such fluid being eventually delivered from the intensifier units at the high pressure for which the system is designed. This fluid is originally obtained from a reservoir .20, connectedtopump. l8 by a feed line 2|. In the event of aternporary failure of one or more intensifier units, a.safety line 22 having a safety valve 23 therein, by-passes. pump l8, and prevents any dangerous build-up of pressure. It is to bedistinctly understoomhowever, that this invention contemplates in addition, the case where the fluidprovided by pump 10 for operation of the intensifier units is also to be admitted to chamber 8 .for delivery at high pressure, thus requiring the use of but one pump.
.fiupply line I9 is provided with check..valve-s 24, one for each unit and arranged to permit the flow of fluid through piston li intov chamber 8 but designed to prevent back flow into pump it. A manifold supplyline 25 having check valves 26 therein, one for eachintensifier unit to prevent back-flow, of v.fluid through piston 6, provides a passage forthe highpr'essure fluid from chamber -1 Ma o d-lin l endsu ply line s bot co municate with a lead-in line 21' which extends through piston 6 into chamber 8 of each intensifier unit. A pressure gage 28 is included in manifold supply line 25 for recording the pressure available for the work to be done.
A pair of motor driven multiple-point rotary switches 29 of conventional design are provided to operate valves and I! in proper sequence in such manner that at no time will all the intensifier units be in a pump-down phase or pumpup phase. Rather the units should operate in a progressive overlapping sequence. It should be understood that there are a variety of means adapted for the proper synchronization of the units, and this invention is not intended to cover any particular one of such means.
Assuming ram 1 to be in the starting position at the bottom of cylinder 5, the operating cycle of each intensifier unit begins with valve 55 opening and valve ll closing. As a result, fluid from reservoir H is admitted under medium pressure into chamber 9. Under the force of this medium pressure, ram 1 moves upward compressing the fluid present in chamber 8 to build up a pressure directly proportional to the ratio of the pressure areas of ram 1 and piston 6. This highpressure fluid is thus forced out of chamber 8 through lead-in line 21 and past check valve 25 and into manifold supply line 25. Check valve 24 prevents any of this fluid from being forced into supply line 19 and therefore into pump Hi. When ram 7 has reached the end of its normal stroke, rotary switches 29 open valve I! and close valve l5. Thereupon check valve 24 opens and check valve 26 closes due to the absence of high pressure fluid in lead-in line 21. Thus the fluid in chamber 9 is permitted to drain back to reservoir l I and ram 1 consequently moves downwardly. The fluid being pumped from reservoir 20 under low pressure through piston 6 into chamber 8 in preparation for the next stroke of the intensifier unit helps return ram 1 to the starting position for the next cycle of operation. A double-pole safety switch 30 mounted in each intensifier unit prevents any further action of that particular unit in the event of a breakdown. A contact 46 projects from ram 1 and operates switch 30 in the event ram 1 is forced beyond its normal length of stroke in either direction. As a result valves I5 and I! immediately reverse themselves thereby avoiding the damage which such high pressures would most certainly cause to the cylinders of the unit.
The intensifiers illustrated in Fig. 2 differ from those in Fig. 1 in that power strokes are made in each direction. To this end each unit consists of a cylinder 3i having oppositely disposed pistons 32 and 32a each rigidly secured within the interior of cylinder 3|. Pistons 32 and 32a are concentric with cylinder 3| and in axial alignment with one another. A cylindrical ram member 33 having axial cylindrical recesses 3:3 and 34a in each end is mounted for reciprocating movement in cylinder 3|. Recesses 34 and 34a align with and engage pistons 32 and 32a respectively in a cylinder-piston relation. whereas cylinder 3| and ram 33 also cooperate in a cylinder-piston relation. Thus medium-pressure chambers 35 and 35a and high-pressure chambers 34 and 34a are defined as ram 33 reciprocates.
A low-pressure pump 36 supplies fluid to chambers 34 and 34a and a medium pressure pump 31 supplies fluid to chambers 35 and 35a in a manner similar to that explained in Fig. 1. Check valves 38, 38a, 39 and 39a and solenoid operated r valves ti) and Ma close.
valves 40, 40a, 4| and Ma also operate in the manner described for Fig. 1.
At the beginning of upstroke of ram 33, valves 49 and Mia are open and valves 4| and Ma are closed. This permits fluid to be pumped against the underside of ram 33 forcing it upward and permits the fluid in chamber 350, to drain back to the reservoir for pump 3'1. The fluid in chamber 35a is thus compressed and forced out at a high pressure thereby closing check valve 39a and opening check valve 38a when the pressure developed is in excess of that already existing in a manifold line d2. At the end of the upstroke solenoid-operated valves 4! and Ma open and Thus the direction of ram 33 is reversed and high pressure is consequently developed in chamber 34, the fluid passing into manifold line 432 as explained above until solenoid operated valves 58 and Mia open and valves ll and Ma close to initiate another cycle of operation. A safety valve 43 for pump 36 and safety switches 4% for each intensifier unit operate in a manner similar to that shown in Fig. 1. However, additional emergency solenoid operated valves are provided for immediate relief flow of fluid from each intensifier unit in the event safety switches M do not reverse valves 40, Ma, it and 43a quickly enough, thereby preventing damage to such intensifier unit which fails to operate normally. Each intensifier unit is grounded to permit such emergency relief action. The normal closing and opening of the regular solenoid-operated valves is controlled by a motor d en multiple-point rotary switch Ll! of conventional design.
It therefore apparent that by using a series of hydraulic intensifier units arranged in functional parallelism and operated in a progressive overlapping sequence whereby a plurality of the intensifier units are at all times in the compression phase, a steady flow of fluid or gases at high pressures can be easily obtained.
I claim:
1. A hydraulic system for delivering a continuous and steady flow of fluid at high pressure comprising in combination, a series of hydraulic intensifier units having a compression stroke and a relief stroke, each of said intensifier units having a medium pressure chamber and a high pressure chamber, said medium pressure chamber having a supply valve adapted to supply medium pressure fluid thereto during said compression stroke and a relief valve adapted to permit escape of said medium pressure fluid therefrom during said relief stroke, a first check valve for said high pressure chamber adapted to permit entry of low pressure fluid thereto during said relief stroke, a second check valve for said high pressure chamber adapted to permit delivery of fluid therefrom during said compression stroke, and means for successively adjusting said supply valves and said relief valves whereby said hydraulic intensifier units are operated in progressive overlapping sequence with a plurality of said intensifier units in compression stroke at all times.
2. A hydraulic system for delivering a continuoils and steady flow of fluid at high pressure comrising combination, a series of hydraulic cylinders having oppositely disposed cylinder heads, each of said cylinders being provided with oppositely disposed fixed pistons extending inwardly toward one another in axial alignment from said cylinder heads, a ram reciprocally engaged in each of said cylinders in a piston-cylinder relation,
said cylinder and said ram thereby defining a medium pressure chamber in each end of said cylinder, said ram having a recess in each end thereof adapted to slidably engage said corresponding fixed piston in a cylinder-piston relation thereby defining a high pressure chamber in each end of said ram, each said medium pressure chamber and each said high pressure chamber cooperating to form a compression unit, each of said hydraulic cylinders thereby comprising a pair of oppositely acting said compression units arranged whereby the compression phase for one of said compression units corresponds to the relief phase of the other end oppositely acting said compression unit, a supply valve for each medium pressure chamber adapted to supply medium pressure fluid thereto, thereby instituting movement of said ram whereby each of said recesses therein cooperates with said corresponding oppositely disposed fixed piston in compression phase, a relief valve for each of said medium pressure chambers adapted to permit escape of said medium pressure fluid therefrom during said relief phase, a first check valve for each of said high pressure chambers adapted to permit entry of low pressure fluid thereto during said relief phase, a sec- 0nd check valve for each of said high pressure chambers adapted to permit delivery of fluid therefrom during said compression phase, and means for successively adjusting said supply valves and said relief valves whereby said hydraulic intensifier units are operated with said compression units functioning in overlapping sequence, a plurality of said compression um'ts being in compression phase at all times.
DONALD H. NEWHALL.
REFERENCES CITED The following references are of record in the file of this patent:
UNITED STATES PATENTS Number Name Date 342,528 McGehee May 25, 1886 1,381,562 Jones June 14, 1921 1,451,303 Mitchell Apr. 10, 1923 2,053,543 Vincent Sept. 8, 1936 2,231,307 Wallace Feb. 11, 1941 2,258,493 Hull Oct. 7, 1941 2,336,446 Tucker et a1 Dec. '7, 1943 2,340,929 Caddbury Feb. 8, 1944
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Cited By (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2699218A (en) * 1949-06-24 1955-01-11 Chrysler Corp Control apparatus
US2819835A (en) * 1954-11-26 1958-01-14 Harwood Engineering Co System for delivering a continuous and steady flow of a compressible fluid at high pressure
DE1097275B (en) * 1953-06-12 1961-01-12 Electraulic Presses Ltd Device for regulating the piston speed of a hydraulic press
US3056384A (en) * 1957-05-07 1962-10-02 Mccorquodale Colour Display Apparatus for the deposition of liquid materials
US3114379A (en) * 1960-03-09 1963-12-17 Cordis Nat Automatic fluid supply actuated motor and piston additive device
US3609066A (en) * 1969-11-13 1971-09-28 Mcneil Corp Lubricant injection system
US4167373A (en) * 1973-05-11 1979-09-11 C.A.V. Limited Fuel injection pumping apparatus
US4470771A (en) * 1982-08-20 1984-09-11 Towler Hydraulics, Inc. Quadraplex fluid pump
US4527954A (en) * 1983-01-14 1985-07-09 Halliburton Company Pumping apparatus
US5088898A (en) * 1989-12-05 1992-02-18 Nippon Pillar Packing Co., Ltd. Reciprocating pump
US6558134B2 (en) * 2001-07-27 2003-05-06 Imation Corp. Fluid intensifier pump system
US6827479B1 (en) * 2001-10-11 2004-12-07 Amphastar Pharmaceuticals Inc. Uniform small particle homogenizer and homogenizing process
US20080203199A1 (en) * 2007-02-07 2008-08-28 Imation Corp. Processing of a guar dispersion for particle size reduction
US9003955B1 (en) 2014-01-24 2015-04-14 Omax Corporation Pump systems and associated methods for use with waterjet systems and other high pressure fluid systems
US9322397B2 (en) 2013-03-06 2016-04-26 Baker Hughes Incorporated Fracturing pump assembly and method thereof
US10295433B2 (en) * 2016-09-27 2019-05-21 Agency For Defense Development Device for testing performance of pyro device using high-pressure air
US10808688B1 (en) 2017-07-03 2020-10-20 Omax Corporation High pressure pumps having a check valve keeper and associated systems and methods
US11904494B2 (en) 2020-03-30 2024-02-20 Hypertherm, Inc. Cylinder for a liquid jet pump with multi-functional interfacing longitudinal ends
US12064893B2 (en) 2020-03-24 2024-08-20 Hypertherm, Inc. High-pressure seal for a liquid jet cutting system

Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US342528A (en) * 1886-05-25 Boiler-feeder
US1381562A (en) * 1919-08-26 1921-06-14 Jones Oceola Pump
US1451303A (en) * 1922-07-26 1923-04-10 Mitchell Edward Albert Gas-distributing system
US2053543A (en) * 1932-01-18 1936-09-08 Continental Motors Corp Fuel pumping system for engines
US2231307A (en) * 1940-05-10 1941-02-11 Cleveland Pneumatic Tool Co Air pump
US2258493A (en) * 1940-01-25 1941-10-07 Trabon Engineering Corp Hydraulic operator
US2336446A (en) * 1941-10-06 1943-12-07 Hydraulic Dev Corp Inc Fluid pressure intensifier
US2340929A (en) * 1940-08-21 1944-02-08 E M B Co Ltd Compressed air intensifier

Patent Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US342528A (en) * 1886-05-25 Boiler-feeder
US1381562A (en) * 1919-08-26 1921-06-14 Jones Oceola Pump
US1451303A (en) * 1922-07-26 1923-04-10 Mitchell Edward Albert Gas-distributing system
US2053543A (en) * 1932-01-18 1936-09-08 Continental Motors Corp Fuel pumping system for engines
US2258493A (en) * 1940-01-25 1941-10-07 Trabon Engineering Corp Hydraulic operator
US2231307A (en) * 1940-05-10 1941-02-11 Cleveland Pneumatic Tool Co Air pump
US2340929A (en) * 1940-08-21 1944-02-08 E M B Co Ltd Compressed air intensifier
US2336446A (en) * 1941-10-06 1943-12-07 Hydraulic Dev Corp Inc Fluid pressure intensifier

Cited By (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2699218A (en) * 1949-06-24 1955-01-11 Chrysler Corp Control apparatus
DE1097275B (en) * 1953-06-12 1961-01-12 Electraulic Presses Ltd Device for regulating the piston speed of a hydraulic press
US2819835A (en) * 1954-11-26 1958-01-14 Harwood Engineering Co System for delivering a continuous and steady flow of a compressible fluid at high pressure
US3056384A (en) * 1957-05-07 1962-10-02 Mccorquodale Colour Display Apparatus for the deposition of liquid materials
US3114379A (en) * 1960-03-09 1963-12-17 Cordis Nat Automatic fluid supply actuated motor and piston additive device
US3609066A (en) * 1969-11-13 1971-09-28 Mcneil Corp Lubricant injection system
US4167373A (en) * 1973-05-11 1979-09-11 C.A.V. Limited Fuel injection pumping apparatus
US4470771A (en) * 1982-08-20 1984-09-11 Towler Hydraulics, Inc. Quadraplex fluid pump
US4527954A (en) * 1983-01-14 1985-07-09 Halliburton Company Pumping apparatus
US5088898A (en) * 1989-12-05 1992-02-18 Nippon Pillar Packing Co., Ltd. Reciprocating pump
US6558134B2 (en) * 2001-07-27 2003-05-06 Imation Corp. Fluid intensifier pump system
US6827479B1 (en) * 2001-10-11 2004-12-07 Amphastar Pharmaceuticals Inc. Uniform small particle homogenizer and homogenizing process
US20080203199A1 (en) * 2007-02-07 2008-08-28 Imation Corp. Processing of a guar dispersion for particle size reduction
US9322397B2 (en) 2013-03-06 2016-04-26 Baker Hughes Incorporated Fracturing pump assembly and method thereof
US9003955B1 (en) 2014-01-24 2015-04-14 Omax Corporation Pump systems and associated methods for use with waterjet systems and other high pressure fluid systems
US9810205B2 (en) 2014-01-24 2017-11-07 Omax Corporation Pump systems and associated methods for use with waterjet systems and other high pressure fluid systems
US10295433B2 (en) * 2016-09-27 2019-05-21 Agency For Defense Development Device for testing performance of pyro device using high-pressure air
US10808688B1 (en) 2017-07-03 2020-10-20 Omax Corporation High pressure pumps having a check valve keeper and associated systems and methods
US12064893B2 (en) 2020-03-24 2024-08-20 Hypertherm, Inc. High-pressure seal for a liquid jet cutting system
US11904494B2 (en) 2020-03-30 2024-02-20 Hypertherm, Inc. Cylinder for a liquid jet pump with multi-functional interfacing longitudinal ends

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