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Publication numberUS2800143 A
Publication typeGrant
Publication dateJul 23, 1957
Filing dateJul 21, 1952
Priority dateJul 21, 1952
Publication numberUS 2800143 A, US 2800143A, US-A-2800143, US2800143 A, US2800143A
InventorsKeller George R
Original AssigneeNorth American Aviation Inc
Export CitationBiBTeX, EndNote, RefMan
External Links: USPTO, USPTO Assignment, Espacenet
Hydraulic regulating valve
US 2800143 A
Abstract  available in
Images(1)
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Claims  available in
Description  (OCR text may contain errors)

July 23, 1957 G. R. KELLER HYDRAULIC REGULATING VALVE Filed July 21, 1952 PRESSURE SOURCE 7| AGTUATING CHAMBER VALVE ACTUATOR 59 REGULATING CHAMBER 1o AGTUATING 1 FIG.2

INVENTOR.

GEORGE R. KELLER ATTORNEY United States Patent HYDRAULIC REGULATING VALVE George R. Keller, Whittier, Calif., assignor to North American Aviation, Inc.

Application July 21, 1952, Serial No. 300,094

2 Claims. (Cl. 137-623) This invention relates to hydraulic regulating valves, and particularly to an improved pilot valve useful in controlling the actuation of a large control valve.

When the use of a large control valve is necessary in order to obtain a sufficiently high power output, the inertia of the valve piston has been found to be toohigh to permit actuation with high sensitivity and good linearity by ordinary means. It has been found necessary to slave the main control valve to a much smaller. pilot valve. The pilot valve has a light piston which has little inertia, and hence can be actuated with very good sensitivity by various electronic and mechanical means. The small pilot valve is used to control the pressure differential between two actuating chambers which, in turn, causes movement of the main control valve piston. It' has further been found desirable to permit the operator to override the pilot valve temporarily and move the control valve manually without aflecting the setting of the pilot valve.

It is an object of this invention to produce a pilot valve which actuates a control valve with improved sensitivity. It is another object of this invention to produce a pilot valve which actuates a control valve with better linearity.

It is another object of this invention to produce a hydraulic valve useful in maintaining a constant pressure,

differential between two actuating chambers.

It is another object of this invention to produce a hydraulic valve which utilizes the hydraulic pressure drop across the valve opening to regulate the opening of the valve.

It is another object. of this invention to provide a valve slaved to a pilot valve but which permits optional manual operation of the valve without affecting the sensitivity of the control by the pilot valve.

Other objects of invention will become apparent from the following description taken in connection with the accompanying drawings, in which Fig. 1 is a sectioned view of the preferred embodiment of the improved pilot valve contemplated by this invention;

And Fig. 2 is a schematic drawing utilizing the hydraulic valve contemplated by this invention,

Referring to Fig. 1, a hydraulic control system is shown consisting of control valve block 1 and pilot valve block 2. Control valve block 1 has inlet port 3 to which is connected 2. source (not shown) of hydraulic pressure and outlet port 4. Control valve piston 5 is fitted to slide freely in cylindrical chamber 6. Piston 5 has four lobes 7, 8, 9, and 1t) dividing cylindrical chamber 6 into sealed subchambers 12, 13, and 14, and piston actuating chambers 11 and 15.. Lobes 7, 8, 9, and .10 of piston 5 are spaced by reduced connecting rods 16, 17, and 18. Extension rods 19 and 20 of piston 5 are provided to permit manual operation of the control valve piston. Piston return springs 21 and 22 are positioned in actuating chambers 11 and 15, respectively, to normally maintain piston 5 in the neutral position.

Sealed chamber 13 is connected to inlet port 3 by means of duct 23. Sealed chamber 12 is connected to outlet port 4 by means of ducts 24 and 25. Sealed chamber 14 is connected to outlet port 4 by means of duct26. Actuating chamber 15 is connected to outlet port 4 by means of duct 27. Duct 27 has a fixed restrictive orifice 28 which materially retards the flow of fluid between chamber 15 and outlet port 4. Actuating chamber 11 is connected to outlet port 4 'by means of ducts 29 and 25. Duct 29 has a fixed restrictive orifice 30 which materially retards the flow of fluid between chamber 11 and port 4. Actuating ports 31 and 32 are connected to openings 33 and 34 of cylindrical chamber 6 by means of ducts 35 and 36, respectively.

Pilot valve block 2 has a cylindrical chamber 37 in which pilot valve piston 38 is fitted to slide freely longitudinally. Piston 38 has two lobes 39 and 40 separated by reduced connecting rod 41. Lobes 39 and 40 of pilot valve piston 38 are spaced to form sealed subchamber 42 and end chambers 43 and 44. Armature buttons 45 and 46 in end chambers 43 and 44, respectively, are secured to. the ends of piston 38. Solenoids 47 and 48 are positioned in end chambers43 and 44 to attract armature buttons 45 and 46, respectively.

Sealed chamber 42 is connected to center chamber 13 by means of ducts 49 and 50. Variable orifice 51 is connected to actuating chamber 11 by means of ducts 52 and 53. Variable orifice 54 is connected to actuating chamber 15 by means of ducts 55 and 56. End chamber 43 is-connected to duct 52 by means of duct 57. End chamber 44 is connected to duct 55 by means of duct 58.-

In operation, the hydraulic pilot valve of Fig. 1 is used to actuate control valve piston'S which regulates the direction and rate of flow of hydraulic fluid to a double-acting cylinder (not shown) connected to actuating ports 31 and 32. Since openings 33 and 34 are completely covered by lobes 8 and 9 when control valve piston 5 is in the neutral position, as shown in Fig. 1, no fluid is initially allowed to flow to the double-acting cylinder. There is, however, a continuous circulation of hydraulic fluid through the pilot valve circuit. Variable orifices 51 and 54 are maintained partly opened at all times by the spacing of lobes 39 and 40. Hydraulic fluid enters port 3 and passes through duct 23, chamber;13, and ducts 49 and 50 into chamber 42. 'In chamber 42, the flow of the fluid divides into two parallel paths. One of these paths comprises variable orifice 51, ducts 52 and 53, actuating chamber 11, duct 29, restrictive orifice 30, duct 25, and outlet port 4. The other path comprises variable orifice 54, ducts 55 and 56, actuating chamber 15, duct 27, restrictive orifice 28,.and outlet port 4. By continuously circulating fluid through both pathsiof pilot valve circuit, the formation of air bubbles in the circuit is eliminated. Any formation of air bubbles in the pilot valve circuit has a detrimental effect on damping, resulting in poorer sensitivity.

The position of pilot valve piston 38 is determined by the relative magnitude of the tractive forces caused by the currents in solenoids 47 and 48. Initially a bias D.-C. voltage is applied to each of solenoids ,47 and 48, causing them to exert equal and opposite tractive forces on piston 38. Superimposed on the DC. bias voltage is a low amplitude high frequency A.-C. voltage of from 200 to 400 cycles per second which is applied to each of solenoids 47 and 43. This high frequency voltage is applied to solenoid 47, out of phase to that applied to solenoid 48. This low amplitude high frequency voltage causes a small longitudinal oscillation of pilot valve piston 38 to preclude the adverse eifects of static The valve of this inventionfriction on the valve piston.

longitudinal oscillation of the piston. Since the mass of the control valve piston is much greater than that of the light pilot valve, the control valve will not follow the high frequency oscillation of the pilot valve.

For purposes of illustrating the excellent linearity obtained by the pilot valve contemplated by this; invention, assume the D..C. bias voltage applied to left solenoid 47 is increased while the D.-C. bias voltage applied to right solenoid 48 is decreased. The change in the relative magnitude of the tractive forces to which piston 38 is subjected, causes pilot valve piston 38 to be displaced longitudinally to the left. The movement of lobe 39 of piston 38 to the left increases the size of variable orifice 51. This causes a reduction in the pressure drop across orifice 51 with a corresponding increase in the pressure drop across orifice 30. The resistance to flow of the other elements in the fluid path is negligible. The movement of lobe 40 of piston 38 to the left decreases the size of variable orifice 54. This results in increasing the pressure drop across orifice 54, While the pressure drop across orifice 28 decreases. The resistance to flow of the other elements in this fluid path is negligible.

The redistribution of the pressure drops in the two fluid paths results in an increase of the pressure in duct 52 and actuating chamber 11, while there is a decrease of the pressure in duct 55 and actuating chamber 15. The increased pressure in actuating chamber 11 coupled with the decreased pressure in actuating chamber 15 causes control valve piston 5 to move to the right. Movement to the right of lobes 8 and 9 results in the uncovering of openings 33 and 34. Actuating port 32 is now connected to inlet port 3 through chamber 13. Actuating port 31 is connected to outlet port 4 through chamber 12.

The rate of flow of the fluid through actuating ports 31 and 32 is determined by the distance piston 5 moves to the right. This distance is determined by the point atwhich the force on piston 5 due to the pressure differential between chambers 11 and is exactly balanced by the force on piston 5 exerted by piston return spring 22.

Due to connecting duct 57, chamber 43 is continuously subjected to the same pressure as that in duct 52 and chamber 11. Similarly, due to duct 58, chamber 44 is continuously subjected to the same pressure as that in duct and chamber 15. Therefore, the hydrauhc pressure in end chamber 43 and actuating chamber 11 is always the same. Correspondingly, the hydraulic pressure in end chamber 44 is always the same as the hydraulic pressure in actuating chamber 15.

Since the pressure in chamber 43 is increased while the pressure in chamber 44 is decreased when piston 38 is moved to the left, a restraining force is imposed on piston 38 tending to return the piston to the neutral position. of the pressure differential and the cross-section area of lobe 39. At some predetermined value of pressure differential the restraining force acting on piston 38 is equal and opposite to the resultant of the tractive forces of solenoids 47 and 48. Piston 38, thereafter, assumes a new position around which it continues the minute longitudinal oscillations. The pressure differential between actuating chambers 11 and 15 is therefore determined solely by the magnitude of the resultant of the tractive forces of solenoids 47 and 48. It is therefore to be noted that any variation'in the source pressure applied between inlet port 3 and outlet port 4 merely causes a compensating movement of control valve piston 38 sufficient to maintain the hydraulic pressure differential between chambers 43 and 44 at a constant predetermined value. This is clear when the forces acting on piston 38 are analyzed. The tractive forces acting on piston 38 are proportional tothe magnitude of the D.-C. applied voltages. The resultant of the tractive forces is constant for a given value of D.-C. applied voltages This restraining force is equal to the product over the small range of movement of pilot valve piston 38. Opposing this constant resultant force is the force due to the pressure differential between chambers 43 and 44. Since piston 38 always moves a direction and distance necessary to maintain a balance between these forces, the pressure differential is made solely dependent on the relative voltages applied to solenoids 47 and 48.

Extension rods 19 and 20 .of piston 5 permit manual control over the control valve overriding the pilot valve control. The manual manipulation of piston 5 does not affect the setting of the pilot valve which continues to maintain the desired pressure differential between chambers 11 and 15. Upon removal of the manual override, control valve piston 5 again is positioned in accordance with the setting of the pilot valve.

It is contemplated that the tractive forces exerted on piston 38 by solenoids 47 and 48 can be provided by permanent magnets. Variations in the relative tractive forces are then provided by electromagnets wound around the permanent magnets. It is further contemplated by this invention that other means may be used to actuate pilot valve piston 38. The means used may be either electronic or mechanical. It is only desirable that the means used be capable of maintaining a constant force over the range of movement of piston 38.

In the schematic drawing of Fig. 2, a regulating valve 59 is used to regulate the pressure differential between actuating chambers 60 and 61. Two parallel hydraulic paths 63 and 64 are connected across a pressure source 62. Path 63 comprises a variable orifice 65, actuating chamber 60, and fixed orifice 66. Hydraulic path 64 comprises variable orifice 67, actuating chamber 61, and restrictive orifice 68. Variable orifices 65 and 67 are always maintained in a slightly open position in order to insure continuous circulation of hydraulic fluid. Variable orifice 65 is varied inversely to variable orifice 67 by regulating valve 59. vAn actuator 69 exerts a displacement force of a predetermined magnitude on a piston of regulating valve 59. This displacement force is opposed by the pressure differential between actuating chambers 60 and 61. The pressure differential between actuating chambers 60 and 61 is conveyed to opposite sides of the piston in regulating valve 59 by means of ducts 70 and 71.

In operation, a constant pressure differential is obtained between actuating chambers 60 and 61 despite small fluctuations in the pressure supplied by pressure source 62. This pressure differential is determined by the amount'of force exerted on the piston of regulating valve 59 by actuator 69. If there is a decrease in pressure from the pressure source the pressure differential between actuating chambers 60 and 61 tends to decrease. This decrease in the pressure difierential results in a decrease in the restraining force acting against the piston' of regulating valve 59. The piston therefore moves in a manner necessary to readjust variable orifices 65 and 67 to increase the pressure differential between chambers 60 and 61. When the pressure differential has reached its previous value the movement of the piston of regulating valve 59 will cease since the restraining force caused by the pressure differential will again exactly equal the force exerted by actuator 69. Variable orifices 65 and 67, regulating valve 59, actuator 69, and ducts 70 and 71 are preferably made similar to the solenoid pilot valve of Fig. 1. It is, however, contemplated that a different type of actuator could be used. The only requirement being that the actuator exerts a constant force of a predetermined value against the piston of regulating valve 59.

Although the invention has been described and illustrated in detail, it is to be clearly understood that the same is by way of illustration and example only and is not to be taken by way of limitation, the spirit and 5 scope of this invention being limited only by the terms of the appended claims.

I claim:

1. Regulating means comprising a pair of fluid channels arranged in parallel, a single fluid channel, means causing flow of fluid to said pair of channels from said single channel, means for restricting flow of fluid in said pair of channels; a pilot valve including a cylindrical chamber connected near one end to one of said pair of channels, near the other end to the other of said pair of channels, and at its central portion to said single channel; said pilot valve further including a pilot valve stem having a central portion of reduced diameter and two end lobes filling said chamber, said end lobes being separated by a distance slightly greater than the distance between the intersections of said pair of channels with said chamber, a first pressure balancing chamber opening into one end of said cylindrical chamber, a second pressure balancing chamber opening into the other end of said cylindrical chamber, conduit means connecting each of said pair of channels to the said balancing chamber adjacent thereto and means for actuating said pilot valve stem longitudinally in said cylindrical chamber 6 to thereby control the diflerential pressure between said pair of channels.

2. A device as recited in claim 1 and further comprising a hydraulic regulating valve actuable in response to said differential pressure.

References Cited in the file of this patent UNITED STATES PATENTS 335,855 Toole -L Feb. 9, 1886 1,518,894 Bliss Dec. 9, 1924 1,756,824 Hasemann Apr. 29, 1930 2,102,400 Wunsche Dec. 14, 1937 2,200,578 Mahon May 14, 1940 2,391,930 Stone Jan. 1, 1946 2,436,992 Ernst Mar. 2, 1948 2,655,940 Jackson Oct. 20, 1953 FOREIGN PATENTS 574,387 France of 1924 792,774 France of 1936 801,509 France of 1936

Patent Citations
Cited PatentFiling datePublication dateApplicantTitle
US335855 *Feb 9, 1886 Steam-actuated valve
US1518894 *Feb 8, 1918Dec 9, 1924Vapor Car Heating Co IncSteam-regulating means
US1756824 *Oct 30, 1929Apr 29, 1930Friedrich HasemannDevice for regulating flow of fluids
US2102400 *Jan 9, 1935Dec 14, 1937Gen ElectricController apparatus
US2200578 *Nov 7, 1938May 14, 1940Mahon Thomas CPressure equalizing valve
US2391930 *Dec 1, 1942Jan 1, 1946Stone Albert RPower transmission system
US2436992 *Jun 16, 1944Mar 2, 1948Hpm Dev CorpSolenoid with plunger
US2655940 *Jan 9, 1950Oct 20, 1953North American Aviation IncTime-modulated two-stage hydraulic valve
FR574387A * Title not available
FR792774A * Title not available
FR801509A * Title not available
Referenced by
Citing PatentFiling datePublication dateApplicantTitle
US2941515 *Feb 13, 1956Jun 21, 1960Moog Servocontrols IncDual input servo valve
US2970575 *Dec 30, 1954Feb 7, 1961Gen ElectricMultiple input hydraulic amplifier
US2985141 *Nov 14, 1958May 23, 1961Gustafson Robert DHigh performance hydraulic servo valve
US2988056 *Dec 20, 1956Jun 13, 1961Houdaille Industries IncLinear type shimmy and steer damper
US2993477 *Dec 17, 1958Jul 25, 1961IbmRegenerative hydraulic control valve
US3004447 *Oct 16, 1956Oct 17, 1961Gen Motors CorpTransmission control device
US3006376 *Apr 28, 1958Oct 31, 1961Culligan IncAutomatic control valve for water softeners or conditioners
US3008486 *Dec 17, 1956Nov 14, 1961Culligan IncDirectional valve for automatic water softeners or conditioners
US3023781 *May 9, 1958Mar 6, 1962Raytheon CoHydraulic servo valves
US3086553 *Jun 24, 1960Apr 23, 1963Levine Gerald ATwo-stage, two-fluid, uni-directional control valve
US3117585 *Sep 12, 1955Jan 14, 1964Weston Hydraulics LtdElectro-hydraulic control valve
US3152612 *Sep 28, 1956Oct 13, 1964Gen ElectricPiezoelectric crystal transducer for controlling fluid flow
US3185167 *May 18, 1961May 25, 1965Sanders Associates IncElectro-hydraulic servo valve unit
US3199536 *Sep 1, 1960Aug 10, 1965Union Tank Car CoThree-position electromagnetic valve
US3485255 *May 2, 1966Dec 23, 1969Ltv Electrosystems IncFixed jet servo valve
US3862643 *Feb 26, 1973Jan 28, 1975Caterpillar Tractor CoPilot pump bleed control for earthmoving scrapers
US4066102 *Apr 14, 1976Jan 3, 1978Danfoss A/SHydraulic regulator
US4066103 *Mar 24, 1977Jan 3, 1978Danfoss A/SHydraulic regulator
US4114650 *Oct 6, 1976Sep 19, 1978Gordon Carroll GValve structure
US4126293 *Jul 16, 1976Nov 21, 1978Control Concepts, Inc.Feathering valve assembly
US4489757 *Dec 3, 1979Dec 25, 1984Conoco Inc.Electrically actuated servocontrol system for a static pressure operated load
US9360132 *Jul 9, 2012Jun 7, 2016Bifold Fluidpower LimitedDirectional fluid control valve
US20140367599 *Jul 9, 2012Dec 18, 2014Bifold Fluidpower LimitedValve
DE1204901B *Aug 27, 1959Nov 11, 1965Sperry Rand CorpEinrichtung zum Steuern des Zu- und Abflusses von oder zu einem hydraulischen Verbraucher
DE1270906B *Jun 20, 1968Flick Reedy CorpSteuerschieber
DE1284774B *Jun 12, 1964Dec 5, 1968Licentia GmbhEinrichtung zur elektromagnetischen Betaetigung eines Steuerschiebers, vorzugsweise fuer eine hydraulische Druckfluessigkeit
DE1301931B *Jul 3, 1963Aug 28, 1969Rolls RoyceBrennstoffregelventil fuer Gasturbinentriebwerke
DE1500185B1 *Jul 2, 1965Dec 18, 1969Philco Ford CorpElektromagnetisch betaetigtes Ventil
DE2621272A1 *May 13, 1976Nov 18, 1976RenaultElektromagnetische betaetigungsvorrichtung, insbesondere fuer hydraulische servo-steuerschuetze
EP0010116A1 *Oct 25, 1978Apr 30, 1980Sperry CorporationImprovements in or relating to hydraulic actuator controls
WO1999055142A1 *Apr 22, 1999Nov 4, 1999D'antonio Consultants International, Inc.System for controlling fluid flow
Classifications
U.S. Classification137/625.63, 91/52, 122/240.1, 251/31, 251/30.1, 251/282
International ClassificationF15B13/043, F15B13/00
Cooperative ClassificationF15B13/0435
European ClassificationF15B13/043E