US2862449A - Positive action flow divider - Google Patents

Positive action flow divider Download PDF

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US2862449A
US2862449A US62112656A US2862449A US 2862449 A US2862449 A US 2862449A US 62112656 A US62112656 A US 62112656A US 2862449 A US2862449 A US 2862449A
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cylinders
rotor
fluid
valve
pistons
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Richard R Wyland
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Boeing Co
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Boeing Co
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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
    • F15B11/00Servomotor systems without provision for follow-up action; Circuits therefor
    • F15B11/16Servomotor systems without provision for follow-up action; Circuits therefor with two or more servomotors
    • F15B11/22Synchronisation of the movement of two or more servomotors
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T137/00Fluid handling
    • Y10T137/2496Self-proportioning or correlating systems
    • Y10T137/2514Self-proportioning flow systems
    • Y10T137/2516Interconnected flow displacement elements

Definitions

  • Identical valve rings 40 and 41 are. slidably seated in internal complemcntal annular seats formed in the rechamfered internally asat 38, and externally as at 39 spective heads 12 and 13.
  • the details of construction 7 are shown in Fig. 9. ,On their respective inner surface the rings are provided 'with arcuate superficial exhaust ports 42 and 43 (Figs. 4, 7 and 8), and with intake ports 44 and 45, each set of ports being arranged concentrically with respect to the open outer ends of each bank of cylinders, and adapted to register therewith as the rotor revolves.
  • Exhaust ports 42, 43 communicate respectively with fluid delivery ports 46, 47 and the valve rings are oriented so that delivery ports 46, 47 are in continuous registry with outlet openings 48, 49 in the respective heads 12 and 13.

Description

Dec. 2, 1958 R. R. WY LAND 2,862,449
POSITIVE ACTION FLOW DIVIDER Filed Nov. 8, 1956 3 Sheets-Sheet 1 iiii'dlmW 4 Ar ffiI/l Ad \M h I r A n I Q 4 m NN Mm um w Dec. 2, 1958 R. R. WYLAND POSITIVE ACTION FLOW DIVIDER 5 Sheets-Sheet 2 Filed Nov. 8, 1956 D Q m k MW M Q w m M NM W T T fi W\ W A on 6 an m H m W v Q w m x w 8 Dec. 2, 1958 R. R. WYLAND POSITIVE ACTION mow DIVIDER 3 Sheets-Sheet 3 Filed Nov. 8, 1956 INVENTOR'. Haw/420 2 WKM/VD A TIDE/V5) 2,862,449 POSITIVE ACTION FLOW :])IVIDER Richard R. Wyland, Wichita, Kans assignor to Boeing Airplane Company,"Wi'chita, Kans.,- a corporation of Delaware Application N overnber 8, 1956, l Se rialNo.-621,126
9 Claims. (CL 1113-49) This invention relates to an improved .hydraulic fluid dividing and metering device capable .ofreceiving fluid under pressure through a single conduit, dividing the fluid into two equal or unequal parts, and delivering the divided parts continuously linto twoseparate conduits without causing any-appreciable pressure drop between the fluid pressure source and the .two separate conduits.
By compounding several of the units the pressure fluid may be divided and delivered continuously in predetermined proportions into four, six, eight or more separate conduits, as desired.
A ,primary object of the invention is to solve the recognized industrial problem of precisely coordinating the distance travel of the pistons of two or more hydraulic cylinders whether thecylinders have equal or unequal displacement, and regardless of the loads imposed on the respective ,pistons' during their movement in either direction. Dependingon the piston performance desired, this :invention is capable of meteringfluid to two or more hydraulic working cylinders to produce simultaneous and "equalpiston 'travelin either the same or in opposite direc- "tion's, or to produce a predetermined travel of one or more working pistons while simultaneously -producing fa proportionatelygreater or less travel'by the other piston or"pistons,regardless of-load variations on the individual workingpistons.
Another object is to provide a unit of the type mentioned which requires noa'uxiliary power for its operation. Instead the single vro'tor of"the device is driven "'by' the pressure fluid which it receives from the supply source and subsequently meters and delivers.
Another object is to provide a"unitwhich may be used for metering identical quantities offifue'l to 'two' or more jet engines to obtain substantially balanced thrust'on 1 opposite sides of the longitudinal centerline of an 'aircraftlor' missile.
Another object isto1provide' a flow divider which can "beinterposedibetween a source of 'fluidgpressure and two fhydraulicmot'ors of any type, and-which is capable of precisely dividing and metering the fluid'tothe motors so that they .will operate .in synchrohism. p
Another object is'toprovide a-pressure fluid divider which includes a plurality of metering cylinders and apistons, and in which half the work done byeachpiston is accomplished when thepistontravels" in one-direction and t-he?other-half of its work'is-donewhen the; piston travels rin' the-opposite direction, tandwin whicht'he dis- :'charge from the various cylinders is substantially Without pulsation. v i
Another object is to' provide a 'flow- 'divider 'havingle ak- -age miriimizingand-wear compensating features.
Still another object is to provide aiiowldivider in' which the 'moving parts are hydraulically balance'd' thus s'ubstantialiy' eliminating vibration and're'ducingbearing loads "andfriction.
The inven'tion,- together with other objects attending its United States Paten 2,862,449 Patented Dec. 2, 1958 cornpanying drawin'gs in which:
Fig. 1 is alongitudinal sectional view through a'flo divider-embodying my-invention,--and is taken in the :plane indicated by the line'1--1 of Fig. -3.
The view schematically shows the divider interposed in a hydraulic system which includes a pump,-a flow control valve, and two hydraulic working cylinders;
Fig. 2 is a similar longitudinal sectional view through the unit taken in the-plane indicated by'the line 2--2 of Fig. 3;
Fig. 3 is a transversesectional view taken along the line 3-3 of Fig. 2;
Fig. 4 is a hypothetical fiat pattern view of the rotor and its pistons, cylinders, and valves, and is primarily to simplify'explanation of the operation of the unit;
Fig. 5 is a fragmentary sectional view of one end of the unit, and is taken along the line 55 of Fig. 3;
Fig. 6 is a schematic 'view illustrating three flow dividers embodying my invention compounded and interposed in a hydraulic system .for metering equal volumes of fluid to four working cylinders;
Figs. 7-and 8 are schematic views showing-the arrange- -ment of intake and exhaust valve ports at the opposite ends of the'unit, and their relation to the respective cylinders at opposite adjacent ends of the rotor, the rotor being in the same position in both views; and
Fig. 9 is a perspective view of one of two identical valve. rings constituting .parts of the unit, and. particularly illustrates the configuration of the fluid intake port.
Referringparticularly'to'Figs. 1 and 2 that embodi- :ment of the invention illustrated includes a generally eiO production, will belmore clearly understood when the cylindrical-casihgltl :provided :with apressure fluid inlet ifltting 111, and sandwiched between a pair of heads 12 and '13 secured 'to the casing by means of studs 14 and 15. Conventional O-rings 16- and 17'-seal between the casing and the respective heads. A cam shaft 18 is positioned concentrically in the-casing and has its opposite ends seated in aligned central bores inthe opposed At-leastone of these bores has a longitudinally end of each'bore is threaded to receive plugs 19and 20 which serve to adjust the longitudinal position of'the shaft with respect to; the casing). -Near its opposite .ends the cam shaft is provided with annular grooves which seat O-rings 21and'22 which prevent leakage of the pressure fluid around'the shaft 18.
Interiorly casing 10 journals the opposite ends of a rotor on spaced bearings23 and 24, the rotor being designated as a whole by the numeral 25. Thecavity or chamber .in which the .rotor operates is designated as a whole by the numeral 26.
The rotor design illustratedincludes two banks of seven cylinders each, one bank at each end of the rotor,
,the cylinders being equally spaced and arranged con- :centrically with respect to the camshaft .18, and the cylinders .in one bank being longitudinally aligned with the respective cylinders'in .the other bank. It will be understood that a. greater or lesser "number of cylinders may be. provided, and that-the cylinders' injboth banks .maylhave equal orproportionately unequal displacement depending .on the. proportionate division of fluid desired. In this case an cylinders have equal displacement.
Seven piston rods (Figs. 7 and S) arepro'vided, one foreach opposed and alignedpairof cylinders, 'and each .rodcarriesa pair of integral tandem-pistons,-one at each end of the .rod. Since each rod and its twopistons Tare irite gral a:s ingle numeral is used to identify eachass embly and the word piston used toindicate-each-assembly.
The-pistons are identical but are identified by separate numerals 27 to 33 inclusive to facilitate subsequent explanation of the operation of the unit. (Also see Fig. 4.) Intermediate its ends each piston is provided with an annular V-section groove 34 which is operably engaged by an inclined V-section cam 35 which is carried centrally motion of the two cylinder banks and their pistons around the cam shaft as a unitary rotor.
In the rotor design illustrated the two banks of cylinders are formed in separate annular blocks 36 and 37.
At their respective, outer ends blocks 36 and 37 are to provide a reduced area end face to thus reduce frictional drag as the entire rotor rotates.
Identical valve rings 40 and 41 are. slidably seated in internal complemcntal annular seats formed in the rechamfered internally asat 38, and externally as at 39 spective heads 12 and 13. The details of construction 7 are shown in Fig. 9. ,On their respective inner surface the rings are provided 'with arcuate superficial exhaust ports 42 and 43 (Figs. 4, 7 and 8), and with intake ports 44 and 45, each set of ports being arranged concentrically with respect to the open outer ends of each bank of cylinders, and adapted to register therewith as the rotor revolves. Exhaust ports 42, 43 communicate respectively with fluid delivery ports 46, 47 and the valve rings are oriented so that delivery ports 46, 47 are in continuous registry with outlet openings 48, 49 in the respective heads 12 and 13. While the valve rings are slidable in their seats toward and away from the respective adjacent ends of the cylinder blocks, they are prevented from rotating by pins 50, 51 seated in bored holes in the heads 12 and 13. It should be noted that intake ports 44 and 45 are each provided with a series of transverse inclined ports 52, 53 (Figs. 1 and 9) which afford open communication between the intake ports and the casing chamber 26 even when the outer end of the cylinder block is seated flat against the inner surface of the adjacent valve ring. This is clearly shown in Fig. 1, in which the arrows indicate the flow of fluid from chamber 26 through ports 52, 53 into arcuate intake port 44.
It will be understood that the outer end faces of the cylinder blocks and the adjacent inner faces of the respective valve rings should preferably be surface ground for good sealing contact. As a means of urging the valve ring faces'into sealing contact the bottom of each annular valve ring seating groove is provided with an annular pressure fluid duct. These ducts are designated by the numerals 54, 55 and they communicate respectively with the outlet openings 48 and 49. The outer or back face of each valve ring is thus subjected to outlet fiuid pressure which urges the ring into sealing contact with the end face of the cylinder block.
It will be noted that each valve ring carries outer and inner O- ring seals 56, 57 which seal against the walls of the grooves in'which the valve rings are slidably seated. While it is entirely feasible to rigidly connect the cylinder blocks 36 and 37 one to the other, the preferredembodiment illustrated makes no such provision. Instead the inner end of each block is provided with a peripheral groove and these grooves seat and support, cooperating spring pressure rings 58 and 59 which house and are urged outwardly by a plurality of circumferentially spaced 1 compression springs 60. The combined axial length of these two pressure rings 58 and 59 is such as to permit a slight inward movement of the two cylinder blocks toward each other before the adjacent surfaces of the pressure rings make solid contact with each other. This described flexible connection between the two cylinder blocks eliminates a considerable amount of close tolerance machine work in the forming of the cylinder blocks. During operation the force applied by the fluid pressure against the outer surfaces of valve rings 40, 41 is suflicient to maintain the adjacent inner surfaces of pressure rings 58, 59 in firm and continuous contact.
Referring again to Fig. 1, the described flowdivider is shown connected into a hydraulic system which includes a three-position open-center four-way valve 61, a hydraulic pump 62 as a source of fluid pressure, two double acting working cylinders 63, 64, conduits 65 and 66 respectively connecting the working cylinders with the fluid outlet openings 48, 49 of the divider, a T-fitting 67 connecting the cylinders, and a conduit 68 connecting the T-fitting with valve 61.
Operation Assuming that this system is primed with fluid and that chamber 26 and all the cylinders, valve ports, etc., in the divider are filled, when the valve 61 is operated to connect fitting 11 with pump 62 and to simultaneously connect conduit 68 with return line 69, fluid under pressure enters chamber 26 in the divider. Assuming also that the pistons are in the relative longitudinal positions shown in Fig. 4, and in the positions shown in Figs. 7 and 8 with respect to the valve exhaust and intake ports, the differential pressure causes fluid to enter the cylinders at the left ends of pistons 27, 28, 29 through intake port 44, and to enter the cylinders at the right end of the pistons 30, 31, and 32 through intake port 45. The differential pressure causes pistons 27, 28, 29 to move to the right in Fig. 4, and causes pistons 30, 31, 32 to move to the left. The cylinders in which piston 33 operates are for the instant blocked off from both intake and both exhaust ports. The described longitudinal movement of the pistons is converted by the cam 35 into rotational movement of the entire rotor and its banks of cylinders and pistons.
Simultaneous with the described movement of the pistons fluid is forced out of the cylinders at the right ends of pistons 27, 28, 29 through exhaust port 43, delivery port 47,outlet 49, line 66 and into the lower end of cylinder 64, also fluid is forced out of the cylinders at the left ends of pistons 30, 31, 32 through valve exhaust port 42, delivery port 46 and line 65 into the lower end of cylinder 63.
Since in the illustrated example all 14 cylinders in ,th divider have the same displacement, the volume of fluid delivered to each Working cylinder 63, 64 will be the same as the rotor revolves and the cylinders in both banks come into and out of registration with the valve intake and exhaust ports in numerical order. Also it will .be understood that flow through both conduits 65 and 66 to the working cylinders will be continuous. The reciprocation of all seven pistons, as' coordinated by their continuous revolving contact with cam 35 is simulated by the sinuous line 70 in Fig. 4. I
It will be understood that the volume of fluid delivered by the flow divider into each of the conduits 65, 66 willbe proportionate to the displacement of the cylinders in each bank of the rotor. If the cylinders in block 37 have twice the displacement as the cylinders in block 36, then conduit 66 and working cylinder 64 will receive twice the volume of fluid received by cylinder 63. By varying the cylinder displacement during fabrication any desired ratio can be obtained in order to meet the requirements of a specific job.
After the desired equal travel of the pistons in working cylinders 63, 64 has been obtained, valve 61 is adjusted to cut ofl fluid flow to the divider. in cylinders 63, 64 in the opposite direction valve 61 is adjusted to connect fitting 11 with return line 69, and to connect line 68 with the pressure line from pump 62. Fluidfpressure then'causes the pistons in cylinders 63, 64, to start downward. Fluid beneath the pistons is respectively delivered into valve exhaust ports 42 and 43. Fluid pressure is now delivered to the rotor pistons in the opposite direction, and the cam forces the rotor to rotate in the opposite direction. The cylinders in both banks sequentially meter and deliver fluid through intake ports 44 and 45 into chamber 26, through inlet 11 to return line 69. The positive metering of the fluid by the cyline To move the pistons three of the'described'flow dividers compounded,- identified by numerals 71, 72," 73. Divider"71 receives pressure fluidfrom pump 62 andd'elivers equalvolumes of continuous flow to'dividers '72, 73. Each of the latter dividers divides and meters theilfiuid it receives, and
delivers equal volumes continuously to working cylinders 74 to 77 .It is evident then, based on'the above described operation of the divider of this -iI1VIltion, each cylinder will receive an identical volume 'of fluidin a given period of time, and assuming' thatithe four cylinders are identical in size, the respective, pistons in these cylinders will travel identicakdistances.during such time. Other methods of compounding will be apparent to those familiar withLthis art.
Having described the invention'with su'flicient clarity to enable those familiar with this art to construct and use it, 1' claim:
1. A positive action fluid flow'divider comprisingzla housing having a fluid outlet opening at'each of its opposite ends and one fluid inlet opening; a rotor, journaled within said housing and'having a central'longitudinal...
opening therethrough; a concentric -inclined cam within .the rotor and nonrotatably secured inthe housing; two "axially spaced banks of respectively axially aligned open ended cylinders in said rotor, one' bank arranged concentrically around each endthereof; a tandem piston assembly reciprocable in each pair of aligned cylinders in the two banks; an annular concentric cam track or groove intermediate the ends of each piston assembly receiving and cooperating with the peripheral edge portion of the inclined fixed cam to convert reciprocal movement of the pistons into rotational movement of the rotor; two valves non-rotatably secured in the housing, one in slidable sealing contact with each end face of the rotor; concentrically arranged exhaust and intake ports in each valve cooperating with the open ends of the cylinders in the respective adjacent banks, the respective intake ports openly communicating with the housing fluid inlet opening and the registering open ends of the adjacent cylinders, and the respective exhaust ports openly communicating with the adjacent housing fluid outlet opening and with the registering open ends of the adjacent cylinders.
2. The flow divider described in claim 1 in which the ports in the valves are arranged so that a plurality of cylinders in one bank are in registry with the adjacent exhaust port while the aligned cylinders in the other bank are in registry with the adjacent intake port.
3. A positive action fluid flow divider comprising; a housing having two fluid outlet openings one at each of its ends, and one fluid inlet opening; two valves having planar faces and fluid distributing ports therein, one nonrotatably secured within each end of the housing with their adjacent face parallel, one port in each valve being in open communication with a respective one of said fluid outlet openings; a rotor journaled in said housing, its opposite end faces being parallel and planar, each rotor end face being in slidable flat sealing contact with a respective inner face of one valve; two banks of open ended cylinders in said rotor, one bank in each end thereof, the axes of the cylinders in each bank being arranged concentrically about and parallel to the rotor axis or rotation, the respective axes of the cylinder in one bank being in alignment with the axis of the cylinders in the other bank, the open outer ends of the cylinders in each bank being located to move into and out of registry with the fluid distributing ports in a respective one of said valves as the rotor rotates; a tandem piston assembly reciprocable in each aligned pair of cylinders in the two banks; a fixed inclined cam in said housing located concentrically with respect to said rotor and its piston assemblies; and means carried centrally by each piston assembly for contacting said cam and. cooperating therewith to convert reciprocal piston movement into rotational'movement of the rotor.
'4. The How divider described in claim 3 and duct means for 'directingifluid under pressure against the respective outer faces of said valves torurge their respective inner faces into sealing. contact .with the respective adjacent end faces ofithe rotor.
5. A positive action fluidflow divider comprising; a housing defining atpressure sealed rotor chamber and having a fluid inlet and two fluid outlet openings, oneiat each .end. of the housing; an elongated cam shaft extending'through the'rotor chamber and secured against rotation in said housing, said shaft central'lycarrying an inclined cam all points on the periphery of which are equidistant radially from the longitudinal axis of the cam shaft; a generally tubular rotorsurrourlding "the cam shaft concentrically and journaled near each of its ends within said rotor chamber; two banks of open ended cylinders in said rotor, one bank is each end thereof, each bank having an identical number of cylinders and the cylinders in one bank being aligned axially with the respective cylinders in the other bank, the longitudinal axes of the respective aligned cylinders" being arranged concentrically about the longaxis' of the cam shaft; a tandem ,piston assembly reciprocable in each aligned pair of cylinders in the two banks, the opposite. ends of each piston assembly serving as pistons in the respective align-ed, pairs ofcylinders; an annular groove intermediate the ends of each piston assembly for receiving a peripheral portion of and for coacting with said inclined cam to cause rotation of the rotor as said pistons are reciprocated by differential fluid pressure on their opposite ends; a non-rotatable valve ring in said housing immediately adjacent and seating flat against the outer open ends of each bank of cylinders in said rotor; superficial intake and exhaust ports in the inner seated face of each valve ring arranged concentrically with respect to the respective adjacent banks of cylinders to register with the open ends of said cylinders as the rotor revolves; and a fluid delivery port in each valve ring aflording open communication between the exhaust port therein and one of the fluid outlet openings in said housing.
6. A liquid flow divider comprising; a housing; a rotor journaled in the housing, said rotor having parallel planar end faces; a like plurality of cylinders in each end of the rotor having their major axes parallel to the rotor axis and arranged concentrically thereabout, the axes of the cylinders in one end of the rotor being in alignment with the respective axes of the cylinders in the other end of the rotor and said cylinders being open at both ends; a pair of non-rotatable valves having planar inner faces in frictional sealing contact with the respective planar end faces of said rotor; open ports recessed into the planar inner face of each valve positioned to register with the open outer ends of the respective adjacent cylinders; a tandem piston assembly reciproca-ble in each pair of axially aligned cylinders; a fixed cam in the housing positioned concentrically and inclined with respect to the rotor axis and about which the rotor and its piston assemblies rotate; means carried intermediate its ends by each piston assembly for contacting said cam and cooperating therewith to convert reciprocal movement of the piston assemblies to rotary movement of the rotor; a fluid inlet opening in the housing in open communication through the housing interior with an inlet port in each valve; and two outlet ports in the housing, one in open communication with an outlet port in each valve, whereby fluid under pressure received through the housing inlet exerts a force against each piston whose cylinder is in registry with a respective valve inlet port, and piston movement causes the rotor ,to revolve, and as it revolves the cylinders come into nately with the respective outlet ports, through which the fluid under pressure is delivered. I
7. A device for dividing and metering liquid pressur comprising: a rotor housing; a rotor journaled within 7 the housing and having a central longitudinal opening throughout its length and having planar parallel annular end faces; two banks of longitudinally disposed cylinders in said rotor, one bank in each of its ends, each bank including the same number of cylinders, and the cylinders in one bank being axially aligned -with the respective cylinders in the other bank, all cylinders being open' at both ends; a tandem piston assembly reciprocable in the respectively aligned cylinders in each bank; a rotor actuating inclined cam extending coaxially through the longitudinal opening in said rotor and securedin said housing against rotation; cam cooperating means carried by each tandem piston assembly intermediate its ends and between said cylinder banks for contacting said inclined cam and causing the rotor to rotate as the piston assemblies reciprocate; a non-rotatable planar valve at each end of said rotor, each valve seated flat against a respective rotor end face and cooperating with the open ends of the cylinders therein as the rotor rotates; an intake port in each valve registerablewith the adjacent cylinder ends and in open communication with the interior of the rotor housing; a pressure fluid inlet in the rotor housing; an exhaust port in each valve also registerable with the adjacent open cylinder ends; and a fluid outlet opening adjacent each valve and in communication only with the exhaust port therein, whereby liquid under pressure entering the-housing through the inlet causes piston reciprocation and, through cam action, rotor rotation, and the liquid is metered consecutively to the cylinders in each bank during their registry with the respective intake ports, and is discharged by them during their reg istry with the respective exhaust ports, and the liquid delivered into the respective exhaust ports is directly proportional to the displacement of the aligned cylinders in each bank.
8. The device described in claim 7 in which the rotor includes two separate cylinder blocks having limited relative axial movement; and means resiliently urging said blocks apart axially and into seating contact with the respective valves.
9. The device described in claim 7 in' which said valves are mounted for limited axial movement with respect to the rotor; and ducts connected with the respective exhaust ports for directing liquid under pressure against the respective outer faces of the valves to urge them into firm seating contact with the respective end faces of the rotor.
References Cited in the file of this patent UNITED STATES PATENTS 2,353,802 Zimmermann July 18, 1944 2,387,761 Kendrick Oct. 30, 1945 2,452,470 Johnson Oct. 26, 1948 2,454,418 Zimmerman Nov. 23, 1948
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Cited By (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3002760A (en) * 1959-06-01 1961-10-03 Russell W Lee Trailer lift
US3046898A (en) * 1959-06-10 1962-07-31 Vickers Inc Power transmission
US3046897A (en) * 1959-06-10 1962-07-31 Vickers Inc Power transmission
US3065602A (en) * 1960-12-02 1962-11-27 Gurries Mfg Co Flow dividing system
US3188963A (en) * 1962-06-04 1965-06-15 Bendix Corp Fluid intensifier
US3225760A (en) * 1962-11-14 1965-12-28 Orthopaedic Specialties Corp Apparatus for treatment of bone fracture
US3322069A (en) * 1965-09-07 1967-05-30 Kobe Inc Fluid operated well pumping apparatus
US3326136A (en) * 1965-09-30 1967-06-20 Houdaille Industries Inc Fluid flow control device
US3369491A (en) * 1966-01-11 1968-02-20 Parker Hannifin Corp Energy transfer mechanism
US3373691A (en) * 1965-06-03 1968-03-19 Escher Wyss Ag Gearwheel type distributor pump
US3405641A (en) * 1967-05-25 1968-10-15 Kobe Inc Rotary, fluid operated, axial plunger pump
DE1285321B (en) * 1964-09-30 1968-12-12 Rexroth Gmbh G L Device for evenly distributing a pressure medium
US9416871B1 (en) 2013-03-15 2016-08-16 Hydro-Gear Limited Partnership Flow divider assembly
US9506561B1 (en) 2013-03-15 2016-11-29 Hydro-Gear Limited Partnership Flow divider assembly

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2353802A (en) * 1940-12-12 1944-07-18 Vickers Inc Power transmission
US2387761A (en) * 1942-04-17 1945-10-30 Manly Corp Fluid pressure device
US2452470A (en) * 1946-01-17 1948-10-26 James P Johnson Distributing device
US2454418A (en) * 1944-01-15 1948-11-23 Zimmermann Lukas Hydraulic flow divider

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2353802A (en) * 1940-12-12 1944-07-18 Vickers Inc Power transmission
US2387761A (en) * 1942-04-17 1945-10-30 Manly Corp Fluid pressure device
US2454418A (en) * 1944-01-15 1948-11-23 Zimmermann Lukas Hydraulic flow divider
US2452470A (en) * 1946-01-17 1948-10-26 James P Johnson Distributing device

Cited By (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3002760A (en) * 1959-06-01 1961-10-03 Russell W Lee Trailer lift
US3046898A (en) * 1959-06-10 1962-07-31 Vickers Inc Power transmission
US3046897A (en) * 1959-06-10 1962-07-31 Vickers Inc Power transmission
US3065602A (en) * 1960-12-02 1962-11-27 Gurries Mfg Co Flow dividing system
US3188963A (en) * 1962-06-04 1965-06-15 Bendix Corp Fluid intensifier
US3225760A (en) * 1962-11-14 1965-12-28 Orthopaedic Specialties Corp Apparatus for treatment of bone fracture
DE1285321B (en) * 1964-09-30 1968-12-12 Rexroth Gmbh G L Device for evenly distributing a pressure medium
US3373691A (en) * 1965-06-03 1968-03-19 Escher Wyss Ag Gearwheel type distributor pump
US3322069A (en) * 1965-09-07 1967-05-30 Kobe Inc Fluid operated well pumping apparatus
US3326136A (en) * 1965-09-30 1967-06-20 Houdaille Industries Inc Fluid flow control device
US3369491A (en) * 1966-01-11 1968-02-20 Parker Hannifin Corp Energy transfer mechanism
US3405641A (en) * 1967-05-25 1968-10-15 Kobe Inc Rotary, fluid operated, axial plunger pump
US9416871B1 (en) 2013-03-15 2016-08-16 Hydro-Gear Limited Partnership Flow divider assembly
US9506561B1 (en) 2013-03-15 2016-11-29 Hydro-Gear Limited Partnership Flow divider assembly
US10385882B1 (en) 2013-03-15 2019-08-20 Hydro-Gear Limited Partnership Flow divider assembly
US10385881B1 (en) 2013-03-15 2019-08-20 Hydro-Gear Limited Partnership Flow divider assembly

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