WO2003014577A1

WO2003014577A1 - Rotary servovalve and control system

Info

Publication number: WO2003014577A1
Application number: PCT/US2001/024856
Authority: WO
Inventors: Raymond D. Woodworth; James E. Bobrow
Original assignee: Woodworth Raymond D; Bobrow James E
Priority date: 2001-08-05
Filing date: 2001-08-05
Publication date: 2003-02-20

Abstract

An improved rotary servovalve system employs a rotary magnetic solenoid (33) having an armature that includes at least one permanent magnet. The armature is coupled to carry a movable valve element (7) in angular rotation therewith so that flow through the servovalve of the system can occur in alternative directions. Also, the valve element is biased toward a position in which all the valve ports (3, 5, 45, 47) are closed when power is removed from the rotary solenoid. The control circuit employed in the rotary servovalve system expands the bandwidth of response of the solenoid actuator by compensation for frequency variations in the input command signal and in the feedback signal. This compensation is achieved utilizing a combined proportional, integral, and differential amplification circuit. Also, imbalance of fluid forces within the servovalve mechanism can be avoided by utilizing a pair of inlet orifices, a pair of outlet orifices, a pair of first fluid control orifices, and a pair of second fluid control orifices. The orifices within each pair are located on opposite sides of the valve housing from each other.

Description

ROTARY SERVOVALVE AND CONTROL SYSTEM

Technical Field

The present invention relates to servovalves that are used to transfer quantities of fluid. The rotary servovalve and control system of the invention is particularly useful in situations requiring rapid response and precision control of fluid flow.

Background Art

Many different mechanical and electrical servovalve systems have been employed for controlling fluid flow in industrial and manufacturing environments, as well as in other applications. Fluid servovalve control systems which require precise and highly responsive control are employed in a multitude of widely varying applications, including the control of robots, the operations of presses for manufacturing rubber and plastic parts, the control of tensioning devices in the paper industry, automotive vehicle and parts manufacturing, petroleum refining operations, and numerous other applications.

In many of the applications in which servo control valve systems are utilized, pressurized fluid is typically provided from a high pressure source and transmitted through a load from which the fluid is then exhausted to a low pressure reservoir. The load may, for example, take the form of a double-acting piston operating within a cylinder. The transfer of fluid from one side of the piston to the other within the cylinder causes the piston to move some mechanism to which it is connected.

Servovalves are widely utilized to control the flow of both pneumatic and hydraulic fluids. Conventional servovalves are often linear motion devices. That is, they typically consist of a spool element operated manually or electrically. Typically the spool element is shuttled back and forth within a chamber defined within a valve housing. By its movement the spool element covers and uncovers different fluid orifices or ports.

The function of a servovalve is to control the velocity and quantity of fluid flow and the direction of movement of a piston within a cylinder. Conventional servovalves typically contain a high torque motor connected to a flapper assembly. Such servovalve systems are expensive and require high manufacturing tolerances. They are also sensitive to contamination and clogging. Furthermore, they typically require continuous flow from a pump in order to operate. Efforts have been made to develop rotary servovalves for use in servovalve systems. One such rotary servovalve is described in U.S. Patent No. 4,794,845 which describes the application of a torque motor to a servovalve system. The torque motor controls flow by rotating a spool element within a complex sleeve assembly containing appropriate fluid passageways. In the event of a power failure a rather intricate arrangement of mechanical elements, including torque rods and springs, is required to center the servo valve in order to halt fluid flow. Also, when power is available, energy is required to center the valve for a zero command, no flow condition. This is necessary because torque motors are directional devices, but have no detent or zero position when power is removed. Consequently, the torque motor must always be energized or actuated throughout operation of a conventional rotary servovalve system.

U.S. Patent No. 5,597,014 is directed to a high flow, direct drive rotary servovalve. This patent describes improvements in passageway designs, the function of which is to eliminate tangential Bernoulli reaction forces acting on the spool member. These forces tend to close the valve, thus requiring the torque motor to expend more energy in order to keep the valve open.

Prior rotary servovalve and control systems lack the requisite torque to be of commercial utility in many applications. This is because of the Bernoulli forces that are created with fluid flow and which tend to close the valve. Prior rotary servovalve and control systems provide elaborate means to combat the influence of these Bernoulli forces. For example, the rotary servovalve of U.S. Patent No. 4,794,845 employs a very complex arrangement to overcome the Bernoulli forces.

Disclosure of Invention

The present invention is a rotary servovalve system that does not require a servomotor for actuation at all, but instead is able to utilize a rotary magnetic solenoid as the valve actuator. One type of suitable rotary solenoid actuator is a rotary magnetic solenoid having an armature that includes at least one permanent magnet and which is rotatable relative to a stator that is formed as an electromagnet. The stator is energizable by electrical current flow in alternative directions to alternatively and selectively create electromagnetic fields of opposite polarity from each other. Moreover, when the stator is deenergized, the permanent magnet or magnets of the armature return the armature to a neutral, null position from positions of rotation in opposite angular directions. The armature is coupled to carry a movable servovalve element in angular rotation therewith.

The rotary magnetic solenoid employed is a rotary bidirectional, high torque solenoid device. One line of suitable rotary magnetic solenoids for use according to the invention is manufactured by Lucas Control Systems Products located in Vandalia, Ohio and is sold as the Ultamag® series of rotary actuators. The armature of this type of rotary magnetic solenoid is centered through the use of permanent magnets and can be driven bidirectionally to either side of a zero or null position. This device is described in U.S. Patent No. 5,337,030.

The armature of the rotary magnetic solenoid utilized in the invention rotates through arcs of twenty-two and one-half degrees to either side of the null position. The angular displacement from the null position and the direction of displacement therefrom is controlled by the amplitude and direction, respectively, of signals to the solenoid stator. When no driving signal to the stator is present, the force of the permanent magnet in the armature centers the armature relative to the stator at the zero or null position.

In a conventional rotary servovalve for the control of fluid flow, the fluid enters the valve housing at a single inlet port and exits the valve housing from a single outlet port. Flow through the valve is controlled by the position of the movable valve element which directs flow from the inlet port to alternative outlet ports. The flow to the outlet port of the valve housing is to a fluid reservoir, which is maintained at a reduced pressure from the pressure of the fluid source. Consequently, the pressure within the flow passage through the valve leading from the high pressure fluid source is greater than pressure within the fluid valve leading to the fluid reservoir. Since the fluid flow passageway within the valve which conducts fluid from the high pressure fluid source is typically located on the opposite side of the valve from the fluid passageway that conducts fluid to the fluid reservoir, there is an imbalance in internal pressure within the valve. The high pressure imbalance within the valve produces a load on the valve element that must be overcome in order to rotate the valve element. As the requirement for torque increases, so does the mass of the components of the driving motor or rotary solenoid.

In a preferred embodiment of the present invention the force imbalance within the valve is virtually eliminated. This is achieved by providing the valve housing with a pair of inlet ports and a pair of outlet ports. The inlet ports are located on diametrically opposite sides of the valve housing from each other. Similarly, the outlet ports are located on diametrically opposite sides of the valve housing from each other. By necessity, the valve ports in each pair must be longitudinally offset from each other so as not to interfere with the other ports in the valve. Corresponding pairs of fluid control ports are likewise provided in the valve housing. The fluid control ports within each pair are similarly diametrically opposed and longitudinally offset from each other in the valve housing. The rotary element of the valve is likewise provided with pairs of flow channels. The flow channels in each pair of flow channels are likewise diametrically opposed from each other and longitudinally offset on the movable valve element.

As a consequence, pairs of flow channels are defined in which the flow channels in each pair conduct fluid through the valve in opposite directions from each other. Therefore, the forces within the valve are balanced, regardless of the direction of fluid flow, the extent to which the ports are open, and even under no flow conditions. As a result, less torque and, therefore, less massive components in the rotary solenoid are required in order to operate the rotary valve. By reducing the mass of the rotary solenoid components, the inertia of the rotary solenoid is also reduced. Reduction in valve inertia results in an increase in the frequency bandwidth of responsiveness of the rotary solenoid to electrical input signals. An increase in frequency bandwidth produces a much faster response time of the rotary solenoid, and hence the servovalve, to electrical input signals that operate the solenoid.

In one broad aspect the present invention may be considered to be a rotary servovalve system comprising a pressurized fluid supply source, a fluid reservoir, a fluid transfer valve housing, a movable valve member located within the valve housing, a rotary magnetic solenoid having an armature and a stator that returns the armature to a null position in the absence of actuating signals, a Hall-effect sensor located proximate to the rotary magnetic solenoid, and a control circuit responsive to the Hall-effect sensor and which provides a feedback electrical signal.

The fluid reservoir has a fluid pressure lower than that of the fluid supply source. The fluid transfer valve housing has a wall of annular cross section and defines therein at least one fluid inlet port coupled to the fluid supply source. At least one fluid outlet port is also defined in the valve housing and is coupled to the fluid reservoir. The fluid outlet port is located diametrically opposite the fluid inlet port. The valve housing also defines at least one first fluid control port and at least one second fluid control port. The first and second fluid control ports are located diametrically opposite each other and equidistant from the inlet and outlet ports.

The movable valve member is located within the valve housing and is alternatively rotatable in opposite angular directions. The movable valve element is rotatable from a closed position in which flow through all of the ports is blocked to positions in which each of the first and second fluid control ports alternatively permits flow therethrough from the fluid inlet port while the other of the first and second fluid control ports concurrently permits flow therethrough to the reservoir. The stator of the rotary magnetic solenoid is electronically activated. The armature of the rotary magnetic solenoid has at least one permanent magnet thereon. The armature is alternatively rotatable relative to the stator in opposing angular directions from a null position. The permanent magnet returns the armature to the null position when the stator is deactuated. The armature drives the movable valve member so that the movable valve member is in its closed position when the armature is in its null position. The Hall-effect sensor is located proximate to the rotary magnetic solenoid to provide a feedback signal indicative of the position and direction of rotation of the armature relative to the null position. The control circuit, which is responsive to the Hall-effect sensor, provides a feedback electrical signal to the stator. This feedback electrical signal drives the movable valve member to a target angular orientation relative to the valve housing. This target orientation is determined by an externally generated command signal.

One very important aspect of the invention resides in the control circuit. The control circuit provides a correction signal to the stator that is proportional to the feedback signal overa broad frequency range. A conventional rotary actuator, such as that described in U.S. Patent No. 5,338,030, has a uniform frequency response over a bandwidth of only about sixty hertz. By employing the control circuitry of the invention, the bandwidth at which the correction signal to the stator is proportional to the feedback signal is increased to a range of at least about one hundred twenty hertz. This increase in frequency responsive bandwidth means that the action of the valve in directing fluid flow is much quicker than in conventional servovalve systems. To a large extent the improved bandwidth of responsiveness of the servovalve system is attributable to the components of the control circuit. Specifically, the control circuit includes a comparator circuit and an error signal processing circuit that includes a proportional amplifier circuit, a differential amplifier circuit, and an integral amplifier circuit, each of which provides a separate output. The comparator circuit receives the feedback signal from the Hall-effect sensor and also an externally generated command signal. The comparator provides an error signal representing the difference between the feedback signal and the command signal. The error signal processing circuit provides separate outputs from the proportional amplifier circuit, the differential amplifier circuit, and the integral amplifier circuit. The combining circuit receives these outputs to produce a frequency-compensated error signal proportional to the difference between the feedback signal and the command signal over a frequency range of at least about one hundred twenty hertz.

Preferably, the control circuit is comprised of an absolute value amplifier circuit and a polarity-indicating amplifier circuit. The absolute value amplifier circuit is coupled to the combining circuit and has an absolute value error output signal proportional to the amplitude of the frequency-compensated error signal irrespective of the polarity thereof. The polarity- indicating amplifier circuit is also coupled to the combining circuit and produces an output indicative of the polarity of the frequency-compensated error signal. A current flow regulation circuit drives the stator of the rotary magnetic solenoid to cause the armature to rotate in an angular direction which is determined by the polarity-indicating amplifier circuit to an angle of displacement from the null position which is determined by the absolute value amplifier circuit.

As previously indicated, the valve housing is preferably comprised of a pair of inlet ports and a pair of outlet ports, as well as a pair of first fluid control ports and a pair of second fluid control ports. The ports within each pair of ports are located one hundred eighty degrees apart, diametrically opposite, and longitudinally offset from each other in the housing. The use of duplicate ports arranged to exert opposing force virtually eliminates pressure imbalances within the valve, thus allowing lighter weight, less massive components to be utilized in the rotary solenoid actuator. By employing a frequency-compensating conditioning circuit in the electrical control for the rotary solenoid, the bandwidth of operation of the servovalve system is improved significantly. The response time of the actuator is thereby improved.

Preferably also, a coupling member is employed to join the solenoid armature to the movable valve member. The rotary magnetic solenoid and the movable valve member are axially aligned with and longitudinally displaced from each other. The coupling member joins the rotary drive shaft of the rotary solenoid armature to the valve stem of the movable valve member. It has been found that by utilizing a coupling member, rather than joining the armature shaft directly to the rotary valve stem, the movable valve element is less likely to bind within the valve housing. When binding occurs the precision of control of the rotation of the movable valve member is adversely effected.

In another aspect the invention may be considered to be a rotary servovalve system comprising a pressurized fluid supply, a fluid reservoir, a valve housing, a bidirectional valve closure element, and a rotary solenoid having a stator and an armature rotatable within the stator between two extreme positions and biased toward a null position midway between the two extreme positions by the force of a permanent magnet on the armature. The pressurized fluid supply has a pressure supply line leading therefrom while the fluid reservoir has a fluid relief line leading thereto. The valve housing has a valve cavity of circular cross section defined therewithin. The valve housing defines at least one rectangular inlet port to the valve cavity that is coupled to the pressure supply line, and at least one rectangular outlet port from the valve cavity coupled to the relief line and located diametrically opposite to the inlet port. The valve housing further defines at least one first rectangular fluid control port and at least one second rectangular fluid control port in communication with the valve cavity and located diametrically opposite each other and equidistant from the inlet and outlet ports. The bidirectional valve closure element has a gate portion with at least one pair of mutually parallel, longitudinally oriented and longitudinally aligned, flow-directing faces of rectangular shape. The valve closure element is located within the valve cavity and is coaxially aligned and rotatable therewithin. The valve closure element is rotatable to create concurrent flow paths between the first fluid control port and the inlet port and between the second fluid control port and the outlet port. The bidirectional valve closure element is rotatable alternatively to block all of the ports. Alternatively still, the valve closure element can be rotated to create concurrent flow paths between the second fluid control port and the inlet port and between the first fluid control port and the outlet port. The rotary solenoid has a stator and an armature with a permanent magnet rotatable within the stator. The armature is rotatable between two extreme positions and is biased toward a null position midway between the two extreme positions by the magnetic force from the permanent magnet. The armature is joined to the valve closure element so that when the armature is at the null position the valve closure element blocks all of the ports, namely the inlet port, the outlet port and the first and second fluid control ports.

The invention may also be considered to be an improvement in a rotary servovalve system in which fluid is directed through at least one inlet port, at least one outlet port, at least one first fluid control port, and at least one second fluid control port in a valve housing. The flow of fluid is directed by a movable valve gate element that is rotatable within the housing in opposite directions of angular rotation from a position prohibiting fluid flow through any of the ports. The valve gate element is rotatable to alternative positions permitting fluid flow in alternative, opposite directions through each of the first and second fluid control ports.

The improvement of the invention is comprised of a rotary magnetic solenoid having an armature that includes at least one permanent magnet. The armature is rotatable relative to a stator formed as an electromagnet that is energizable to alternatively create electromagnetic fields having opposite polarities from each other. The stator, when deenergized, allows the armature to return to a neutral, null position from positions of orientation in opposite angular directions. The armature is coupled to carry the movable valve gate element in angular rotation therewith. A Hall-effect sensor is located proximate to the rotary magnetic solenoid. The Hall- effect sensor senses the position of the solenoid armature relative to the stator and provides a feedback signal responsive thereto. A control circuit is coupled between the Hall-effect sensor and the rotary magnetic solenoid to provide control inputs to the stator of the rotary magnetic solenoid. The electrical control circuitry employed in the rotary servovalve system of the invention is simple and inexpensive to implement and employs conventional, commercially available components. These components are arranged in a unique, yet simple and straight forward manner.

The rotary servovalve system of the invention may be utilized with either pneumatic or hydraulic fluids. In either case, the system precisely controls position, velocity, and acceleration of a mechanical load, such as movement of a piston within a cylinder.

The fluid control valve employed in the servovalve system of the invention has large orifices that are controlled by a small electromagnetic rotary solenoid. Valves constructed according to the invention are quite capable of providing pneumatic flow rates in excess of thirty standard cubic feet per minute and are designed to withstand high stress loads. The system features high torque operation and is capable of operating for millions of cycles.

The servovalve system of the invention has a system bandwidth that is operational over one hundred twenty hertz due to the unique closed loop rotary servovalve and control system design. The rotary servovalve system of the invention is useful in a wide variety of applications. For example, many applications for the system of the invention exist in the automotive industry, as well as the aerospace industry. The system is useful in electronics for medical equipment and with home appliances. It can be used for controlling manufacturing equipment and machines and is also useful in the marine industry. The servovalve system of the invention also has significant utility in the computer industry. Its small size and rapid response to signals over a broad bandwidth make the system particularly useful for flight simulators, both for FAA and PC games applications. The servovalve system of the invention also has significant applications for use in entertainment and theme parks.

The invention may be described with greater clarity and particularity by reference to the accompanying drawings.

Brief Description of Drawings

Fig. 1 is an exploded perspective view illustrating the mechanical components of a first embodiment of a rotary servovalve system according to the invention. Fig. 2 is a perspective view showing the mechanical components of Fig. 1 assembled together.

Fig. 3 is a sectional elevational view taken along the lines 3-3 of Fig. 2. Fig. 4 is a sectional elevational view of the valve housing of Fig. 1 shown in isolation. Fig. 5 is a sectional elevational view of the movable valve gate element of Fig. 1 , shown in isolation. Fig. 6 is a sectional plan view of the valve housing cap taken along the lines 6-6 of Fig. 1.

Fig. 7 is a sectional view taken along the lines 7-7 of Fig. 6.

Fig. 8 is a perspective diagram, partially broken away, showing the internal operating components of the rotary solenoid shown in Fig. 1.

Fig. 9 is a transverse sectional detail taken along the lines 9-9 of Fig. 3 showing the valve of the invention in a position to conduct fluid from a pressure supply line through a first fluid control port and to concurrently conduct fluid from a second fluid control port to a fluid relief line. Fig. 10 is diagrammatic view illustrating the mechanical components of the rotary servovalve system of the invention with a partial section taken along the lines 9-9 of Fig. 3 showing all valve ports closed.

Fig. 11 is a electrical block diagram illustrating an electrical control circuit coupled to the mechanical components of the rotary servovalve system illustrated in Fig. 10. Fig. 12 is a schematic diagram illustrating the electrical control system of Fig. 11 in greater detail.

Fig. 13 is an exploded perspective detail illustrating the valve and valve housing employed in the embodiment of the invention illustrated in Figs. 1-10.

Fig. 14 is an exploded perspective detail illustrating a preferred alternative valve and valve housing which may be employed in the rotary servovalve system of Fig. 10 in place of the embodiment of the valve and valve housing shown in Fig. 13.

Fig. 15 is a diagrammatic view illustrating the fluid passageway interconnections of the valve of Fig. 14 with all ports blocked.

Fig. 16 is a diagrammatic view illustrating the fluid passageway interconnections of the valve of Fig. 14 responsive to actuation of the rotary magnetic solenoid shown in Fig. 1 in one direction of operation.

Fig. 17 is a diagrammatic view illustrating the fluid passageway interconnections of the valve of Fig. 14 responsive to actuation of the rotary magnetic solenoid shown in Fig. 1 in a direction opposite to that shown in Fig. 16. Fig. 18 is a diagrammatic perspective view of a fluid flow control system employing a further preferred embodiment of the rotary servovalve of the invention having certain advantages over the embodiment depicted in Figs. 13-17 and shown actuated to permit fluid flows as illustrated by directional arrows.

Fig. 19 is an exploded perspective view that illustrates the component valve elements of the valve shown in the system of Fig. 18

Fig. 20 is a plan sectional view of the assembled valve of Fig. 19 taken along the lines 20-20 in Fig. 19.

Fig. 21 is a plan sectional view of the assembled valve of Fig. 19 taken along the lines 21-21 in Fig. 19.

Fig 22 is a plan sectional view of the assembled valve of Fig. 19 taken along the lines 22-22 in Fig. 19.

Fig. 23 shows a perspective drawing an alternate rotary servovalve system fully assembled.

Fig. 24 is an exploded view of the alternate rotary servovalve system illustrated in Fig. 23. Fig. 25 is a partial exploded view of the alternate servovalve illustrated in Fig 24.

Fig 26A is an assembly view of the parts shown in Fig. 25.

Fig.26B shows an x-Ray view of the assembly shown in Fig. 26A.

Fig.27 shows a cross-section of the alternate rotary servovalve shown in Figs.24 and 25.

Best Mode for Carrying Out Invention

Figs. 10 and 11 provide an overview of a rotary servovalve system according to the invention. This system includes a mechanical section 50, illustrated generally in Fig. 10, and an electrical control circuit 52, illustrated in block diagram form in Fig. 11.

The mechanical section 50 of the rotary servovalve system of the invention has a valve and solenoid assembly 54 operated through signals from the control circuit 52 that are connected by appropriate wires to a terminal strip TS, illustrated in Figs. 1-3. The rotary servovalve and solenoid assembly 54 includes an Ultramag® rotary actuator 33 that is seated in a hollow, cup-shaped end cap 34. The end cap 34 has a cylindrical, annular wall open at its upper end to receive the rotary magnetic solenoid 33 and is closed at its lower end. The terminal strip TS is located externally on the lower, closed end of the hollow cap 34.

The rotary magnetic solenoid actuator 33 is of the type that includes an armature with at least one permanent magnet thereon, described in U.S. Patent No. 5,337,030, which is incorporated herein in its entirety by reference. Different sizes of rotary magnetic solenoid actuators 33 are commercially available as the Ultramag® Series Rotary Actuators, sold by Lucas Control System Products, Lodex Actuation Products, 800 Scholz Drive, Vandalia, OH 45377-0427. While the embodiments of the invention described herein envision use of the size model 4EM/4EMM, larger systems might employ size models 5EM/5EMM or 6EM/6EMM. The valve portion of the rotary servovalve system of the invention is located opposite the end cap 34 at the upper end of the servovalve and rotary magnetic solenoid assembly 54. Specifically, the valve portion of the assembly 54 includes an upper fluid transfer valve housing cap 56. The valve housing cap 56 defines a fluid inlet port 17 coupled to a fluid supply source which may be a pump 65 that supplies fluid under pressure through a supply line 67 connected to the inlet port 17 from a fluid reservoir 49, as shown in Fig. 10. The fluid reservoir 49 is at a fluid pressure lower than that of the output of the fluid pump 65. The fluid reservoir 49 is also connected directly to a relief port 15 in the valve housing cap 56 by a fluid return line 62. The fluid transfer valve housing cap 56 also has a first fluid control port 13 and a second fluid control port 21. The first fluid control port 13 is connected by a conduit 16 to the blind end 51 of a hydraulic actuator cylinder 55. The opposite end 59 of the hydraulic actuator cylinder 55 has a central, axial opening therein through which a piston rod 57 extends. A conventional sliding seal (not shown) about the piston rod 57 maintains pressure within the actuator cylinder end 59. The piston rod 57 is connected to a piston 53 which moves reciprocally within the actuator cylinder 55 in sliding, sealed engagement with the interior cylindrical wall thereof in a conventional manner.

The valve housing cap 56 has a cylindrical inner wall 58. The upper end 60 of the valve housing cap 56 is closed so that the central, cylindrical interior wall 58 defined within the cap 56 forms a blind well or bore closed at the top and open at the bottom. A pair of diametrically opposed, longitudinally extending cylindrical bores 72 are defined in the closed, upper end 60 of the valve housing cap 56 at locations located radially outwardly from the central inner cylindrical wall 58 in diametric opposition from each other. A pair of larger diameter cylindrical bores 74 are defined in the downwardly facing, annular surface of the cap 56 in coaxial alignment with the bores 72.

The valve housing portion of the assembly 54 also includes an annular, intermediate housing ring 64 having a central, cylindrical inner wall 66. Radially outwardly from the cylindrical inner wall 66 there are a pair of diametrically opposed cylindrical bores 68 that extend down into the intermediate ring 64 from the upper surface thereof. The bores 68 are of the same diameter as the bores 74 in the valve housing cap 56 and are coaxially aligned therewith. A pair of narrower cylindrical bores 70 are defined in the lower surface of the intermediate ring 64 and extend upwardly in coaxial alignment to intersect the larger diameter bores 68.

The valve and solenoid assembly 54 further includes a pair of cylindrical, annular, elongated metal bushings 80 which have smooth outer surfaces and which are internally tapped. The outer diameter of the bushings 80 is such that they fit snugly into both the bores 74 in the under surface of the valve housing cap 56 and into the bores 68 in the upper surface of the intermediate housing ring 64.

The rotary servovalve system of the invention also includes a valve housing sleeve 1 of cylindrical annular configuration. The outer diameter of the housing sleeve 1 is such that it can be press fitted into the cylindrical wall 58 of the central axial blind bore in the valve housing cap 56. The valve housing sleeve 1 is formed of hardened steel and contains four longitudinally elongated, precision, rectangular-shaped fluid passageways or openings 3, 5, 45, and 47. An EDM (electrical discharge machine) process forms the four rectangular fluid orifices 3, 5, 45, and 47 radially through the cylindrical annular walls of the sleeve 1. The inlet orifice 47 and outlet orifice 5 are located diametrically opposite to each other in the sleeve 1. Likewise, the first fluid control orifice 45 and the second fluid control orifice 3 are likewise located diametrically opposite each other. The first and second control orifices 45 and 3 are both located equidistant from the inlet orifice 47 and from the outlet orifice 5. All of the rectangular orifices 3, 5, 45, and 47 have the same rectangular dimensions and are all longitudinally aligned with each other and angularly located at ninety-degree intervals about the sleeve 1. The elongated, rectangular valve openings 3, 5, 45, and 47 in the interior valve housing sleeve 1 are respectively longitudinally and radially aligned with the valve ports 21 , 15, 13, and 17 in the valve housing cap 56.

The servovalve of the invention also includes a bidirectional, rotatable valve gate element 7 that is located radially within the valve housing sleeve 1. The rotatable valve gate element 7 has a generally cylindrical configuration, the lower end 86 of which is formed as a cylindrical valve stem and the upper end 88 of which forms a gate portion of the valve gate element 7. The gate portion 88 of the movable valve gate element 7 is formed with a set of mutually parallel, longitudinally oriented, rectangular-shaped, flow-directing faces 9 and 9'. The flow-directing faces 9 and 9' are oriented in mutually parallel alignment with each other and parallel to and equidistant from the axis of rotation of the movable valve gate element 7, which is indicated at 90 in Fig. 5.

The flow-directing faces 9 and 9' are formed by milling out notches or slots from diametrically opposites sides of the upper end of the movable valve gate element 7 so that the transverse ledge surfaces 92 above and beneath the flow-directing faces 9 and 9' all reside in planes perpendicular to the axis of rotation 90. All of the circular segment-shaped ledges 92 are equal to each other in surface area and in distance from the axis of rotation 90.

The structure of the movable valve gate element 7 remaining between the flow- directing faces 9 and 9' may be considered to be a web 94. The diametrically opposing, outwardly facing, curved surfaces of the web 94 are of a slightly greater width than the width of the elongated, rectangular openings 3, 5, 45, and 47 in the valve housing sleeve 1 in order to minimize valve overlap.

The upper, gate portion 88 of the rotatable valve member is inserted up into the central, cylindrical opening in the housing sleeve 1 until the web 94 resides in longitudinal alignment with the port openings 3, 5, 45, and 47. The lower, valve stem end 86 of the rotatable valve gate element 7 extends downwardly beneath the housing sleeve 1. The valve stem end 86 is received within a central, axial opening in a spool-shaped intermediate coupler 43 and is immobilized from rotation relative thereto by a radial set screw 43A in the upper portion of the coupler 43. The coupler 43 is preferably a Schmidt Control Flex Coupling, part no. C008P, manufactured by Zero-Max. The coupler 43 has sufficient flexibility to prevent any binding of the movable valve elements within the valve housing sleeve 1 , yet ensures that the moveable valve gate element 7 is locked in rotational movement to the rotary solenoid armature shaft 29. The internal construction and operation of the rotary solenoid 33 is shown in Fig. 8.

The rotary solenoid 33 operates on the principle of attraction and repulsion of opposite and like magnetic poles. The permanent magnetic armature A has permanent magnets PM that together have twice as many poles as the solenoid stator S. In the deenergized state, the armature poles each share half a stator pole, causing the shaft to seek midstroke. When power is applied, the stator poles are polarized. This attracts half and repels the other half of the armature poles, causing the shaft to rotate. When the voltage is reversed, the stator poles are polarized with the opposite magnetic pole. Consequently the opposite poles of the armature A are attracted and repelled, thus causing rotation in the opposite direction. Fig. 8 illustrates rotation of the armature in a counterclockwise direction relative to the stator S, as viewed from the top.

The solenoid armature A of the rotary solenoid 33 has a central, axial drive shaft 29 including an upper portion that extends upwardly out of the casing 30 of the rotary solenoid 33, and a lower portion that extends downwardly therefrom. The diameter of the rotary solenoid drive shaft 29 is the same as that of the valve stem 86, so that the upper portion of the drive shaft 29 of the rotary solenoid 33 fits snugly into the central axial opening in the coupler 43. A lower set screw 43B immobilizes the coupler 43 relative to the solenoid drive shaft 29. The intermediate coupler 43 thereby joins the armature drive shaft 29 to the movable valve gate element 7. The rotary magnetic solenoid 33 and the movable valve gate element 7 are thereby axially aligned with and longitudinally displaced from each other. The rotary magnetic solenoid 33 has a pair of upwardly projecting, externally threaded mounting studs 27 and a pair of downwardly projecting, externally threaded mounting studs 31 that are rigidly attached to and extend longitudinally from the solenoid case 30. To assemble the valve and solenoid assembly 54 the upper mounting studs 27 of the rotary solenoid 33 are inserted up into the openings 70 in the intermediate housing ring 64. This brings the coupler 43 into the opening 66 in the intermediate housing ring 64 with the movable valve gate element 7 projecting upwardly above the intermediate housing ring 64. The internally threaded bushings 80 are then rotated and threaded onto the upwardly projecting rotary solenoid mounting studs 27 and tightened down into the bores 68 of the intermediate housing ring 64. The bores 68 thereby serve as seating sockets for the lower ends of the bushings 80. The intermediate housing ring 64 is then moved upwardly, thereby seating the upper ends of the elongated bushings 80 into the bores 74 that also serve as seating sockets and which are defined in the underside of the housing cap 56. When the underside of the housing cap 56 makes contact with the upper surface of the intermediate housing ring 64, the gate portion 88 of the rotatable valve gate element 7 resides in longitudinal alignment with the rectangular openings 3, 5, 45, and 47 in the housing sleeve 1.

The assembly 54 further includes a pair of valve cap connecting bolts 82, each of which has a washer 84. The bolts 82 are inserted through the washers 84 and down into the openings 72 defined in the upper end 60 of the valve housing cap 56. The bolts 82 are advanced into engagement with the upper ends of the elongated bushings 80. The threaded shanks of the cap-connecting bolts 82 extend downwardly through the bores 72. The cap bolts 82 are tightened down into the elongated bushings 80, which are seated in the bores 74, thereby securing the valve housing cap 56 tightly in fluid-tight sealing relationship with the intermediate housing ring 64.

The casing 30 of the rotary solenoid 33, the intermediate housing ring 64, and the housing cap 56 are thereby securely fastened to each other. The fit of the movable valve gate element 7 against the internal cylindrical wall of the housing sleeve 1 is sufficiently close so that a fluid-tight seal is established therebetween. Fluid flow through the valve can therefore occur only if the flow directing faces 9 and 9' of the valve gate portion 88 are rotated in such a way as to permit flow to or from the rectangular openings 3, 5, 45, and 47 in the housing sleeve 1. The movable valve gate element 7 and the upper end of the drive shaft 29 from the armature A of the rotary solenoid 33 are coaxially aligned with each other and are longitudinally offset from each other. The annular coupling member 43 is secured to both the valve gate element 7 and to the upper end of the armature shaft 29.

The lower end of the armature shaft 29 projects downwardly from the bottom of the rotary solenoid housing 30 and into an annular Hall-effect position transducer 39 that is located proximate to the rotary solenoid 33. The position transducer 39 detects the direction and extent of angular rotation of the shaft 29 of the solenoid armature A from a null position, indicated at 0° in Figs. 1 and 9. The Hall-effect position transducer 39 is a magnetic sensor which provides a feedback signal 101 , as indicated in Figs. 11 and 12. The feedback signal 101 is indicative of the position and direction of rotation of the armature A and armature shaft 29 relative to the null position of 0°.

The Hall-effect position transducer 39 is attached to a flat, transverse bar 96 which has openings at its ends through which the lower rotary solenoid mounting studs 31 project. The mounting bracket 96 resides in contact with the underside of the rotary solenoid casing 30, and the lower mounting studs 31 project downwardly therethrough and through openings in the cup-shaped rotary solenoid housing end cap 34. Fastening nuts 98 are threaded onto the exposed ends of the lower mounting studs 31 that project downwardly through the bottom of the rotary solenoid end cap 34. The nuts 98 are tightened so that the upper, annular edge of the end cap 34 bears against the periphery of the underside of the rotary solenoid casing 30, as illustrated in Fig. 3. With all of the component parts of the servomotor and rotary valve assembly 54 assembled and tightened together as illustrated in Figs. 2 and 3, the assembly 54 is connected in the rotary servovalve system 50 as shown in Fig. 10. Fluid flow from the pump 65 is controlled by the rotatable valve gate element 7 to allow or block fluid flow as illustrated, for example, in Figs. 9 and 10. Specifically, the armature shaft 29 is rigidly coupled to the rotatable valve gate element 7 by means of the coupler 43, so that the rotatable valve gate element 7 rotates through the same angle as the armature shaft 29 in response to driving inputs to the rotary solenoid 33. As is evident from Figs. 8 and 9, the armature A of the rotary magnetic solenoid 33 is alternatively rotatable relative to the stator S of the rotary magnetic solenoid 33 in opposing angular directions from a null position of 0°.

As illustrated, the armature A of the rotary solenoid 33 drives the movable valve gate element 7 so that the movable valve gate element 7 is in the closed position depicted in Fig. 10 when the armature A is in the null position of 0° indicated in Fig. 10. The armature A and its shaft 29 are rotatable within the stator S of the rotary magnetic solenoid 33 between two extreme positions indicated at +α and -α in Figs. 1 and 9. The armature A is biased toward the null position, 0°, midway between the two extreme positions +α and -α by the forces of the permanent magnets PM on the armature A. The permanent magnets PM in the armature A of the rotary solenoid 33 return the armature A to the null position as described in U.S. Patent No. 5,337,030. The armature shaft 29 is joined to the valve gate element 7 so that when the armature A is at the null position of 0°, the valve gate element 7 is also at the null position of 0° indicated in Fig. 9. The valve web 94 then blocks flow into or out of all of the ports 13, 15, 17, and 21 , as illustrated in Fig. 10, when the feedback signal 101 is zero.

With reference to Fig. 10, the servovalve and rotary solenoid assembly 54 is connected in the mechanical section 50 of the rotary servovalve system of the invention in the same manner as a conventional four-way servovalve or proportional valve. That is, fluid flow from the pump 65 is controlled by the movable valve gate element 7. When the valve gate element 7 is rotated clockwise, as shown in Fig. 9, the rotary servovalve and solenoid assembly 54 allows flow from the supply line 67 to the first fluid control port 13 and on through line 16 to the blind end 51 of the hydraulic actuator cylinder 55. The valve gate element 7 concurrently allows flow from the cylinder cavity 59 through line 61 , through the second fluid control port 21 to the fluid return line 62 leading to the fluid reservoir 49. This fluid flow occurs when and to the extent that the web 94 of the rotary valve gate element 7 is rotated clockwise by the rotary solenoid armature shaft 29 from the null position, 0°, toward a maximum, extreme clockwise position of rotation indicated by +α in Fig. 9.

Conversely, if the web 94 is rotated in a counterclockwise direction by counterclockwise rotation of the rotary magnetic solenoid 33 is illustrated in Fig. 8 from the null position, 0°, as viewed in Figs. 9 and 10, toward an extreme counterclockwise position of rotation indicated at -α in Figs. 1 and 9, flow is from the inlet port 17 through the second fluid control port 21 to the cylinder cavity 59, with concurrent flow from the cylinder cavity 51 through the first fluid transfer port 13 to the outlet port 15, return line 62, and reservoir 49. The maximum angle α in both direction is twenty-two and a half degrees, as shown in Fig. 9. Since the valve openings 3, 5, 45, and 47 are rectangular, and since the extent to which the web 94 blocks or unblocks these openings is throughout their entire lengths, the window through which flow passes to or from the valve openings 3, 5, 45, and 47 past the flow-directing faces 9 and 9' is always of a rectangular shape. Consequently, the volume of flow through both sides of the rotary servovalve varies linearly with the angle of rotation of the armature shaft 29.

Rotation of the valve gate element 7 is controlled through an angle of between +α and -α degrees from a zero null position of 0° by electronic control circuitry as shown in Figs. 11 and 12. The armature shaft 29 is precisely rotated in either of two alternative directions by the application of an electrical power control signal 35, indicated in Fig. 11.

The rotation of the rotatable valve gate element 7 is controlled precisely and at a high bandwidth with a proportional, integral, and derivative (PID) electronic control system in the rotary transducer and conditioning electronics indicated generally at 81 in Fig. 11. The angle of the shaft 29 is sensed with the Hall-effect sensor 39 that transforms the magnetic field created by permanent magnets PM of the armature A attached to the shaft 29 into a voltage feedback signal 101. A command voltage 69 that is applied to the input of the PID control system 71 is compared to the conditioned feedback voltage signal 102 from the rotary transducer and conditioning electronics 81 and converted into a current in the rotary solenoid 33. The feedback control system of the PID controller 71 quickly drives the difference between the input command signal 69 and the conditioned feedback signal 102 to zero by the application of electrical current to the rotary solenoid 33 through the wires 110 and 111 , shown in Fig 2. 1 and 12. When electrical control power signals 35 are removed or when a zero command signal 69 is applied to the electronic control system 52, the armature shaft 29, shown in Fig. 1 , returns to the null position through the actions of the permanent magnetic restoring forces internal to the rotary solenoid 33.

As illustrated in Fig. 10, the fluid conduit 67 conducts high-pressure fluid flow produced by the pump 65 to the fluid supply inlet port 17 and orifice 47. Fig. 10 depicts the movable valve gate element 7 positioned in a null or fluid flow blocking position, thus preventing fluid entry into the cavities created within the housing sleeve 1 by the flow directing faces 9 and 9'. At the same time, fluid flow through the orifice 5 is also blocked, thus preventing fluid from returning to the reservoir 49 through the outlet port 15. Fluid flow to or from the first fluid transfer port 13 and the second fluid transfer port 21 is also blocked, as there is no path of flow through either of these ports by way of the orifices 45 and 3, respectfully. The substantially rectangular shape of the web 94 of the gate portion 88 of the movable valve element 7 inherently produces large tangential Bernoulli reaction forces when fluid flows past the flow directing faces 9 and 9'. These Bernoulli forces tend to drive the web 94 of the movable valve element 7 toward the closed or null position, as illustrated in Fig. 10. This null position is indicated at 0° in Fig. 9. Fig. 12 is a schematic electrical diagram of the control circuit 52 of the invention. The control circuit 52 is responsive to the Hall-effect sensor 39, which includes an operative electronic component indicted at Q4 in Fig. 12. The sensor element Q4 of the sensor 39 may be a UGN3516 Hall-effect transducer manufactured by Allegro. The Hall-effect sensor 39 is located proximate to the rotary magnetic solenoid 33 and senses the position of the solenoid armature A relative to the stator S as indicated by the position of the armature shaft 29, and provides a feedback electrical signal 101 responsive thereto. The electrical position feedback signal 101 is indicative of the orientation of the armature shaft 29 within the angular range of +α and -α. The signal 101 moves the movable valve gate element 7 to a target angular orientation within the range +α and -α with respect to the null point, 0°, relative to the valve housing sleeve 1.

The feedback signal 101 is fed to a conditioning operational amplifier Q2C, which is configured as an inverting amplifier. A variable resistor R22 biases the signals from the Hall- effect transducer Q4 to a zero output to subtract out the direct current component of the feedback signal 101. The conditioned feedback signal is transmitted from the operational amplifier Q2C as a signal 102 to the negative side of an error-sensing circuit including an error-sensing operational amplifier QB1.

A position command signal 69 is provided from a command signal source and appears at pin3 of the terminal strip TS, shown in Fig. 12. The externally generated command signal 69 from terminal strip TS is directed to the positive side of a buffer amplifier Q1 A. The output signal 103 from the buffer amplifier Q1 A is connected to the positive side of the error-sensing amplifier QB1. The error-sensing amplifier QB1 is the operative component of a comparator that receives the position feedback signal 102 and the position command signal 103. The comparator circuit with amplifier QB1 compares the conditioned feedback signal 102 with the buffered command signal 103 to provide an error signal 104 in accordance with the different therebetween. The error signal 104 represents the difference between the feedback signal 102 and the unbuffered command signal 103.

The error signal 104 is directed to an error signal processing circuit which is the PID controller circuit 71 , indicated in Fig. 11. An HR Textron model EC250GP General Purpose PID Control Card provides all of the components necessary for the PID controller 71. The error signal processing circuit 71 includes a proportional amplifier circuit including, as an operative component, the linearly proportional amplifier Q1C; a differential amplifier circuit including, as an operative component, the differential amplifier Q2D; an integral amplifier circuit including, as an operative component, the integral amplifier Q3A; and a feed forward signal biasing amplifier Q3B. Each of the amplifiers, Q1C, Q2D, Q3B, and Q3A provides a separate output. These outputs appear, respectively, at 105, 106, 112, and 107 in Fig. 12. The error signal processing circuit 71 is formed of frequency-sensitive circuitry coupled to the comparator amplifier QB1 to condition the position error signal 104 and provide a conditioned output error signal from amplifier Q1 D that is proportionally responsive to the position feedback signal 101 over a frequency range of at least 120 hertz. The differential amplifier Q2D, the proportional amplifier Q1 C, and the integral amplifier Q3A, are connected in parallel to receive the position error signal 104.

The amplifier Q1 D is the operative component of a combining circuit that receives all of the differential, proportional, integral and feed amplifier circuit outputs from the PID controller circuit 71 to produce a frequency-compensated and conditioned output error signal 107. The signal 107 is proportional to the difference between the feedback signal 101 and the buffered command signal 103 over a frequency range of at least about 120 hertz. The output signal 107 from the combining amplifier Q1 D can be either positive or negative. The signal 107 is coupled to amplifiers Q2B and Q2A which produce an output signal 108 that will always be positive. The absolute value error output signal 108 is proportional to the amplitude of the frequency-compensated error signal 107 irrespective of the polarity of that signal. Together the amplifiers Q2B and Q2A form a full-wave rectifier circuit that is coupled to receive the conditioned output error signal 107 and provide an absolute value error output signal 108 of a predetermined polarity and having an amplitude proportional to the conditioned output error signal 107.

The amplifier Q3C is the operative component of a polarity indicating amplifier circuit that is coupled to receive the conditioned output error signal 107 and to provide a polarity- indicating output signal 109. The signal 109 is governed by the polarity of the conditioned output error signal 107 from the combining circuit amplifier Q1 D. Both the polarity-indicating signal 109 and the absolute value error signal 108 are directed as inputs to a current flow regulation circuit Q8. The current flow regulation circuit Q8 is coupled to receive the conditioned output error signal 108 and the polarity-indicating signal 109 and provide control outputs on lines 110 and 111 to operate the rotary solenoid 33.

The current flow regulation circuit Q8 is a model LMD18245 full bridge power amplifier circuit manufactured by National Semiconductor Corporation. The current flow regulation circuit Q8 is a very important element in the control circuit 52 because it allows closed-loop operation.

The current flow regulation circuit Q8 provides no current to the rotary solenoid 33 when the conditioned position feedback signal 102 is equal to the buffered position command signal 103 in Fig. 12. The feedback loop formed by the current flow regulation circuit Q8 is coupled to receive the buffered command signal 103 and the error signal 104 and to provide outputs to the rotary solenoid armature on lines 110 and 111 that rotate the rotary solenoid armature and its shaft 29 in a direction and to an extent so as to minimize the error signal on line 104. The control circuit 52 is thereby coupled between the Hall-effect sensor 39 and the rotary magnetic solenoid 33 to provide control inputs on lines 110 and 111 to the stator S of the rotary magnetic solenoid 33. The current flow regulation circuit Q8 serves as a full-bridge motor driver power amplifier circuit 75 connected between the frequency compensation circuitry of the PID controller 71 and the rotary magnetic solenoid 33 for providing actuating signals on lines 110 and 111 to the stator S of the rotary magnetic solenoid 33, as illustrated in Figs. 11 and 12. The current flow regulation circuit Q8 receives the absolute value error output signal 108 at its pin14 and the polarity-indicating output signal 109 at pin11 and drives the stator S of the rotary solenoid 33 in accordance therewith. These signals on lines 110 and 111 cause the armature A of the rotary solenoid 33 to rotate in an angular direction which is determined by the polarity-indicating amplifier Q3C to an angle of displacement from the null position, 0°, which is determined by the absolute value output 108 of amplifiers Q2B and Q2A.

The response of the rotary solenoid 33 as manufactured drops off at frequencies above about 60 hertz. The armature A of the rotary solenoid 33 therefore has a response that is frequency dependent. However, the signal-conditioning PID controller circuitry 71 receives the error signal 102 and compensates for frequency variations in the command signal 69 so that the outputs to the rotary solenoid stator S produce uniform responses by the armature A over an enhanced frequency range by the command signal 69 of at least about 120 hertz. The conditioned outputs 108 and 109 to the current flow regulation circuit

Q8 are therefore not dependent upon frequency for over a range of at least about 120 hertz.

The values of the components of the schematic circuit of Fig. 12 are listed in Table I.

It is important for these values to be selected so as to maximize the bandwidth of frequency response of the rotary solenoid armature to the stator inputs on lines 110 and 111. The proper selection of the components of Table I serves to extend the response bandwidth of the rotary solenoid 33. While the components of Table I have been optimized for the Ultamag rotary actuator size 4EM/4EMM previously described, the values of the components of Table I may have to be adjusted for different models of rotary solenoids. The resistor values are in ohms and the capacitor values are in farads, except as otherwise indicated in Table I.

TABLE I Resistors 1/8 watt 1% Metal Film Semiconductors

Quantity Quantity 19 (R1-R5), (R7-R15, R19, R29, 3 Q1-Q3 = LM324N quad op-

(R31-R33) = 10K amp with 14 pin DIP sockets

1 R6 = 1.8K 1 Q4 = UGN 3516 Hall-effect transducer (Allegro) 1 R16 = 6.8K 1 Q5 = LM317T 3-term adj. reg.

1 R17 = 56K 1 Q6 = ICL7660A CMOS volt, conv. (Harris)

2 R18, R20 = 4.7K 1 Q7 = 78L05+ 5v volt reg. 1 R21 - 33K 1 Q8 = LMD18245 DMOS full- bridge motor driver (National

Semiconductor) 1 R22 = 5K (18 turn trim pot)) 1 D1 = Zenior diod 5.1 volt

1 R23 = 220 2 (D2-D3 = 1 N914

1 R24 = 1200 1 R25 = 5K Misc. Hardware

1 R26 = 22K Quantity 1 R27 = 10K 2 Heatsinks (T-220) for Q5 &

Q8

1 R28 = 1 meg TS terminal strip 5 terminal

(AUGAT- .250 spacing)

1 R30 = 1 K 3 14 pin DIP sockets 1 18 pin DIP sockets

Capacitors

Quantity 3 C1 , C2, C10 = 0.1 UF @ 50v mono.

2 C4, C5 = 10UF @ 16v.

Tantilum

3 C3, C6, C11 = 1.0UF @ 50v tantilum

1 C7 = 100UF @ 50v electrolic 1 C8 = 2.2NF ceramic

1 C9 = 0.45NF ceramic

Fig. 13 is a diagrammatic illustration of the mechanical components of a rotary servovalve 100 which may be utilized in a rotary solenoid actuated system as illustrated and described above. Fig. 14 is a diagrammatic illustration of the mechanical components of an alternate embodiment of a servovalve which may be used in place of the valve shown in Fig. 13.

Fig. 13 illustrates the movable valve gate element 7 and the valve housing sleeve 1 (partially broken away) of a conventional rotary servovalve 100, heretofore described, in enlarged detail. The valve housing sleeve 1 is formed of hardened steel and contains four longitudinally elongated, precision, rectangular shaped fluid passageways or openings 3, 5, 45, and 47. The valve housing sleeve 1 of the rotary valve 100 has a single inlet orifice 47, a single outlet orifice 5, a single first fluid transfer orifice 45, and a single second fluid transfer orifice 3.

The servovalve 100 also includes a bidirectional, rotatable valve gate element 7 that is located radially within the valve housing sleeve 1. The rotatable valve gate element 7 has a generally cylindrical configuration. The lower end 86 of the rotatable valve element 7 is formed as a cylindrical valve stem. The upper end 88 forms a gate portion of the valve gate element 7. The gate portion 88 of the movable valve gate element 7 is formed with a set of planar, mutually parallel, longitudinally oriented, rectangular-shaped, flow- directing faces 9 and 9'. The flow-directing faces 9 and 9' are oriented in mutually parallel alignment with each other and parallel to and equidistant from the axis of rotation 90 of the movable valve gate element 7.

The flow-directing faces 9 and 9' are formed by milling out notches or slots from diametrically opposites sides of the upper end 88 of the movable valve gate element 7 so that the transverse ledge surfaces 92 above and beneath the flow-directing faces 9 and 9" all reside in planes perpendicular to the axis of rotation 90. All of the circular segment- shaped ledges 92 are equal to each other in surface area and are the same distance from the axis of rotation 90. The structure of the movable valve gate element 7 remaining between the flow- directing faces 9 and 9' may be considered to be a web 94. The diametrically opposing, outwardly facing, curved surfaces of the web 94 are of a slightly greater width than the width of the elongated, rectangular openings 3, 5, 45, and 47 in the valve housing sleeve 1 in order to minimize valve overlap. Depending upon the pressure in the pressurized fluid supply line coupled to the single inlet orifice 47, a significant imbalance of forces on the flow directing faces 9 and 9' of the rotatable valve element 7 may exist. When there is a significant pressure imbalance within the servovalve 100, the forces required to return the web 94 of the servovalve to a null or 0° position are markedly increased. As a consequence, this would require the use of a rotary solenoid 33 of greater size to provide the torque necessary to drive the solenoid armature away from the 0° position. However, the larger the torque required, the greater will be the mass and size of the rotary solenoid 33 that must be used. As the mass of the parts of the rotary solenoid 33 that drives the valve element 7 in rotation increase, inertia also increases and the time responsiveness of the valve 100 to changing inputs on the electrical control lines coupled to it 110 and 111 decreases.

Therefore, a unique system has been devised for obviating and virtually eliminating any lateral force imbalance on the valve components in the rotary servovalve system of the invention. Specifically, and as illustrated in Fig. 14, an improved rotary valve 200 may be used in place of the valve 100. A valve housing sleeve 201 and a movable valve gate element 207 may be substituted in the valve 200 for the valve housing sleeve 1 and movable valve gate element 7 depicted in the valve 100 shown Fig. 13. As shown in Figs.14-17, the valve housing sleeve 201 includes an upper and lower set of each of the orifices and each of the gating sections previously described. That is, the valve housing sleeve 201 includes a pair of inlet orifices 247U and 247L (upper and lower), a pair of outlet orifices 205U and 205L, a pair of first fluid transfer control orifices 245U and 245L, and a pair of second fluid transfer control orifices 203U and 203L. The orifices within each pair of orifices are located one hundred eighty degrees opposite each other and are longitudinally offset from each other in the housing sleeve 201.

That is, the lower inlet orifice 247L is located below the level of the upper inlet orifice 247U and on the opposite side of the valve housing sleeve 201 , angularly displaced one hundred eighty degrees away from longitudinal or verticalalignment with the upper inlet orifice 247U. Likewise, the lower outlet orifice 205L is located on the opposite side of the housing sleeve 201 from the upper outlet orifice 205U and beneath the level of the upper outlet orifice 205U. The angular displacement of the upper and lower outlet orifices 205U and 205L from each other is likewise one hundred eighty degrees. As a consequence, the lower outlet orifice 205L is located directly beneath and in longitudinal alignment with the upper inlet orifice 247U. Conversely, the lower inlet orifice 247L is located directly beneath and in longitudinal alignment with the upper outlet orifice 205U, as shown in Fig. 14.

In a like manner the upper, first fluid transfer orifice 245U is located on the opposite side of the housing sleeve 201 angularly displaced one hundred eighty degrees from the lower, first fluid transfer orifice 245L. The upper, second fluid transfer orifice 203U is located on the opposite side of the housing sleeve 201 from the lower, second fluid transfer orifice 203L angularly displaced one hundred eighty degrees therefrom. As a consequence, the upper, first fluid transfer orifice 245U is located directly above the lower, second fluid transfer orifice 203L. The upper, second fluid transfer orifice 203U is located directly above the lower first fluid transfer orifice 245L, as illustrated in Fig. 2.

Similarly, the movable valve member 207 has an upper gate section 288U and a lower gate section 288L. The upper gate section 288U is longitudinally aligned with the upper orifices 247U, 205U, 203U, and 245U. Similarly, the lower gate section 288L is longitudinally aligned with the lower orifices 247L, 205L, 203L, and 245L. The upper gate section 288U has a pair of mutually parallel faces 209U and 209'U located equidistant from the axis of rotation 290 of the movable valve member 207. Similarly, the lower gating section 288L has a pair of flow directing faces 209L and 209'L, mutually parallel to each other and located the same distance from the valve axis of rotation 290 as the upper fluid flow directing faces 209U and 209'U. The flow directing faces 209U and 209'L therefore reside in the same vertically oriented plane while the flow directing faces 209'U and 209L reside in the same vertically oriented plane

As illustrated in Fig. 14, the flow directing faces 209U and 209'L are longitudinally offset from each other and the flow directing faces 209L and 290'U are longitudinally offset from each other. The faces 209U and 209'U are longitudinally aligned with the upper orifices 203U, 205U, 245U, and 247U in the valve housing sleeve 201. The faces 209L and 209'L are longitudinally aligned with the orifices 203L, 205L, 245L, and 247L in the valve housing sleeve 201.

As illustrated diagrammatically in Figs. 3, 4, and 5, the orifices in each pair of orifices are interconnected to provide alternative flow paths into and out of the valve housing sleeve 201 from opposite sides thereof. This prevents a lateral imbalance from existing in the valve housing sleeve 201.

More specifically, when a pressure is applied to one flow-directing valve face in the upper gating section 288 through the high-pressure inlet orifice 247U, an equal and diametrically opposite force is applied against one of the flow-directing faces in the lower section 288L of the movable valve gate element 207. As a consequence, equal and opposite radial forces act at all times in a lateral direction upon the movable valve gate element 207. Therefore, the movable valve element 207 is in a state of lateral equilibrium from the equal and opposite dynamic fluid forces acting upon it. This reduces the torque necessary to rotate the movable valve element 207. As a consequence, the mass-of the rotary solenoid components employed in the rotary solenoid 33 that operates the valve 200 can be reduced, thereby improving the response time of the rotary solenoid 33. Figs. 15, 16, and 17 illustrate the interconnection of the orifices in each set of orifices. In a system employing the valve 200 shown in Fig. 14 the two inlet orifices 247U and 247L are each connected to separate inlet orifice lines 217U and 217L, both of which are connected to the same high-pressure fluid supply line 67 by means of a channel, duct, or connecting line 267. Likewise, the outlet orifices 205U and 205L are both connected to the return line 62 by means of an interconnecting passage 262.

In a like manner, the pair of first fluid transfer orifices 245U and 245L are connected together by an interconnecting duct or line 216 so that both of the first fluid transfer orifices 245U and 245L are connected to the line 16 leading to the cylinder fluid cavity section 51 of the actuator cylinder 55. Likewise, both of the second fluid transfer orifices 203U and 203L are connected together by a connection line 261 , so that both of the second fluid transfer orifices 203U and 203L are connected to the fluid transfer line 61 that leads to the cylinder fluid cavity section 59 of the actuator cylinder 55. Fig. 15 illustrates the condition of the valve passageways of the valve gate element

7 relative to the orifices of the valve housing sleeve 201 when the center of the web 94 of the valve gate element 7 is rotated by the solenoid armature shaft 29 is at the null or 0° position. In that position all of the inlet and outlet valve orifices are blocked by the upper web 294U and the lower web 294L of the movable valve gate element 207. Fig. 16 illustrates the interconnection and direction of fluid flow when the movable valve gate element 207 has been rotated in a clockwise direction from the position depicted in Fig. 15. As is evident in Fig. 16, fluid flows from line 67, through connecting line 267, to fluid inlet ports 247U and 247L. Fluid then flows through the upper and lower passageways of rotatable valve element 207 to the two first fluid transfer orifices 245U and 245L, which are coupled to line 16 by connecting line 216. The fluid flow to the first cylinder fluid cavity 51 is from line 16 and the flow from the second fluid cylinder cavity 59 in the fluid actuator cylinder 55 is to the line 61. From line 61 fluid flows to second fluid transfer orifices 203U and 203L, through the valve passageways, and out of the two outlet orifices 205U and 205L, through connecting line 262, and to the reservoir through line 62. However, unlike the situation that exists when using the valve 100 in the embodiment of Figs.14-17, there is no lateral pressure imbalance within the valve 200, since equal and opposing laterally acting radial forces act upon the movable valve gate element 207 regardless of the pressure in the system.

The same is true in Fig. 17 which illustrates the direction of fluid flow when the armature shaft 29 turns the rotatable valve element 207 in a counterclockwise direction from the null or 0° position. With the valve element 207 turned in the counterclockwise direction from the position of Fig. 15, as shown in Fig. 17, fluid flow is from the high- pressure supply line 67, into the inlet orifices 247U and 247L that are connected together by line 267, through the second fluid transfer valve orifices 203U and 203L, that are connected together by line 261 , and to the actuator cylinder cavity 59 through line 61. Concurrently, fluid flows from the first cylinder fluid cavity 51 through line 16 to both of the first fluid transfer orifices 245L and 245U, which are interconnected by the line 216. The fluid flows out of the valve housing sleeve 201 through the outlet orifices 205U and 205L, through the connecting line 262 and on to the return line 62 leading to the reservoir 49. By employing the innovative servovalve structure of the type depicted in Figs. 14- 17, the system is relieved of lateral pressure imbalances within the valve housing 201 , since equal and opposite lateral force components always act on the sides of the movable valve gate element 207 from opposite radial directions. As a consequence, smaller, lighter-weight components can be utilized in the rotary solenoid actuator for the valve gate element 207, thus improving the responsiveness of the valve to changing electrical signals to the solenoid actuator.

While the laterally acting force components are balanced in the valve 200, there are still unbalanced forces acting in vertical planes that pass through and contain the axis of rotation 290 of the rotatable valve member 207. These unbalanced forces still produce a rotational bending moment on the valve member 207 in vertical planes. That is, even though the lateral components of force in the valve 200, as viewed in a direction parallel to the axis 290, are balanced, these forces act in an unbalanced manner at different locations along the longitudinal length of the valve gate member 207, as viewed perpendicular to the axis 290.

Fig. 19 illustrates a force balanced rotary valve 300 in which the forces are balanced both laterally and vertically. The valve 300 employees a hollow, cylindrical, annular valve housing 301 and a rotatable valve closure or gating element 307 located coaxially within the confines of the valve housing 301. The valve housing 301 has a longitudinal axis 390 and first and second opposite ends 371 and 372, respectively. The valve housing 301 defines a central, radial inlet port 347 therein, which is visible in Fig 9. A central radial outlet port 305 is also defined in the wall of the valve housing 301 diametrically opposite the central inlet port 347. The central inlet port 347 and the central outlet port 305 both have a rectangular shape and are equal in area to each other.

The valve housing 301 also has first and second end radial inlet ports 373 and 374, respectively. The ports 373 and 374 are respectively located in the first end 371 and in the second end 372 of the valve housing 301. The end radial inlet ports 373 and 374 are in angular alignment with each other and with the central outlet port 305. The end inlet ports 373 and 374 are longitudinally displaced equidistantly from the central outlet port 305 in a direction parallel to the valve axis 390.

The valve housing 301 also has first end and second end radial outlet ports 375 and 376, located, respectively, in the first end 371 and in the second end 372 of the valve housing 301. The end outlet ports 375 and 376 are in angular alignment with each other and with the central inlet port 347. The end outlet ports 375 and 376 are longitudinally displaced equidistantly from the central inlet port 347 in a direction parallel to the valve axis 390. Each of the first and second end inlet and outlet ports 373,374,375, and 376 has an area one half the area of each of the central ports 305 and 347. The valve closure element 307 also differs from the valve closure element 207.

The valve closure or gating element 307 defines a pair of central passages 377 and 378 therethrough, a pair of first end transverse passageways 379 and 380 therethrough, and a pair of second end transverse passageways 381 and 382 therethrough. The central transverse passageways 377 and 378 are longitudinally aligned with the central ports 347 and 305 in the valve housing 301. The first end transverse passageways 379 and 380 are longitudinally aligned with the first end ports 373 and 375 in the valve housing 301. The second end transverse passageways 381 and 382 are longitudinally aligned with the second end ports 374 and 376 in the valve housing 301.

The first end passageways 379 and 380 and the second end passageways 381 and 382 are each of a cross-sectional area one half that of each of the central passageways 377 and 378. All of the passageways 377, 378, 379, 380, 381 , and 382 are parallel to each other. They also extend in a transverse direction so that, as the valve closure element 307 rotates within the valve housing 301 , it concurrently brings the central passageways 377 and 378 into alignment with both of the central ports 347 and 305, the first end passageways 379 and 380 into alignment with both of the first end ports 373 and 375, and the second end passageways 381 and 382 into alignment with both of the second end ports 374 and 376.

Because the areas of the end ports and end passageways are each one half of the area of the central ports and central passageways, the forces acting upon the rotatable valve element 307 are always in balance in planes passing through and containing the valve axis 390. The end ports 373, 374, 375, and 376 in the valve housing 301 are all located equidistant from the central ports 305 and 307 therein. The end passageways 379, 380, 381 , and 382 in the rotatable valve element 307 are also equidistant from the central passageways 377 and 378. Therefore, there is no bending moment applied to the rotatable valve element 307 along its length even though there may be very large pressure differentials between the fluid inlet and fluid outlet sides of the valve 300.

From Fig. 19 it can be seen that the inlet force (M) that is applied at the central inlet port 347 from the pump 65 acting through lines 67 and 367, as shown in Fig. 18, is in a direction opposite both the force (U) which is acting through the second, upper end inlet port 374 and the force (L) acting through the lower, first end inlet port 373. The forces (U) and (L) are generated by pressure from a pump 65 acting through lines 67 and 341 and through lines 347U and 347L, respectively. The pressure in each of the lines 367, 347U, and 347L is, of course, the same, because those lines are all in direct fluid communication with each other. Since the area of the central inlet port 347 is twice the area of each of the end inlet ports 373 and 374, the force (M) is equal and opposite to the combined forces (U) and (L). Moreover, since the end inlet ports 373 and 374 are located equidistant from the central inlet port 347 parallel to the axis 390, the bending moment created by the force (U) is in a direction equal and opposite to the bending moment created by the force (L). Therefore, the valve 300 is in balanced force equilibrium not only in a lateral direction, but also in planes passing through and containing the longitudinal axis of rotation 390 of the rotatable valve element 307.

Fluid flow through the valve 300 is illustrated in the system diagram shown in Fig. 18. When the rotatable valve element 307 is rotated by the solenoid in one direction, fluid under pressure flows from the primary high pressure inlet line 67, through the branch inlet lines 341 and 367 and from inlet lines 367, 347U, and 347L to the inlet ports 347,374, and 373, respectively. The force SM which acts at inlet port 347 is in a direction equal and opposite to the sum of the forces SU and SL which act at ports 374 and 373, respectively. From these inlet ports, fluid flows into the transverse valve passageways.

If the rotatable valve element 307 is turned from the null position in a clockwise direction, as illustrated in Figs 20, 21 , and 22, flow will be from the inlet ports 347, 374 and 373 into passageways 377, 380 and 382, respectively. From these passageways fluid flow is to the first fluid transfer ports 345C, 345U, and 345L, respectively. From these fluid transfer control ports fluid respectively flows into control lines C2M, C2U, and C2L, respectively, and then into control line 16 leading to port C2 at the blind end 51 of the hydraulically actuated cylinder 55. Concurrently, fluid flows from the cylinder actuator end 59 through port C1 thereof to line 61. From control line 61 fluid flows through lines C1 M, C1 U, and C1 L to control ports 303C, 303U, and 303L, respectively. Fluid then flows from control port 303C through passageway 378 to relief port 305, and on to relief lines 362C and 62 to the reservoir 49. At the same, time fluid flows from control port 303U through passageway 381 to relief port 376 and on to relief lines 362U and 62 to the reservoir 49, and from control port 303L through passageway 379 to relief port 375 and on to relief lines 362L and 62 to the reservoir 49. The force RM that exists at port 305 is equal and opposite to the sum of the forces RU and RL that exist at ports 376 and 375, respectively.

If the valve element 307 is rotated in the opposite, counterclockwise direction from the null point, flow through the control ports 303U, 345U, 303C, 345C, 303L, and 345L and through control lines 16 and 61 will be in the opposite directions from those shown in Figs. 18-22.

In addition to the rotary servovalve configuration previously implemented and described as shown in Fig's 1 through 17, an additional alternate servovalve design 400 is shown in Fig.'s 23 through 27. This alternate servovalve 400 provides certain additional advantages: lower construction cost due to component elimination, such as spacer 64; enhanced bandwidth or faster response due in part to a reduced inertial load by removing the coupler 43 previously attached to rotor shaft 29; and permanent attachment of valve shaft 86 to rotor shaft 29 to form a single shaft 432 integral to the rotary solenoid actuator 33 resulting in smaller size and reduced overall weight. Fig. 23 shows a perspective drawing of this alternate rotary servovalve system

400, fully assembled. Fig. 24 is an exploded view of the alternate rotary servovalve system 400. Shown is the rotary solenoid actuator 33 attached to the fluid four port manifold 56, which connects to a cover 408 and cover lid 402 assembly which contains a closed loop electronic PID controller 71 internally fixed to the cover 408. The cover lid 402 is attached to the cover 408 with screws 414. The PID controller 71 is secured to cover 408 by screws 416 and contains a Hall effect position sensor 39, which is used to electronically sense the rotary solenoid valve's 33 shaft 432 position through the use of the shaft sensing magnet SSM. External drive command signals and power supply connections are provided through electrical connector 412 shown mounted in the cover lid 402 assembly. The mating connector (not shown) is connected through use of the stand offs 410. The cover 408 and lid 402 assembly are shown secured to the fluid manifold 56 through the use of screws 406. Loosening the cover securing screws 406 allows the cover to be rotated via the screw slots 407. This adjustment capability permits the calibration of electrical null between the shaft sensing magnet SSM and Hall Effect position sensor 39. The original rotary servovalve, as defined in Fig.'s 1 through 17, used a coupler 43 to prevent binding of the valve shaft 86 in the sleeve 1 and manifold assembly 56. The coupler 43 is now unnecessary. The knurling 434 shown on rotor shaft 432 is used to hold the rotary actuator's 33 permanent magnet PM in place via a simple press fit.

Fig. 25 is a partial exploded view of the alternate servovalve 400. Fig 26A is an assembly view of the parts shown in Fig. 25. Fig.26B shows an x-Ray detail view of the assembled components of Fig. 25. Fig's 25, 26A, 26B illustrate in better detail how this alternate valve design 400 uses a "floating" integrated rotor 432 in place of the separate rotor shaft 29, coupler 43 and rotatable valve shaft 7. The new common shaft 432, is supported on both ends by two self aligning "floating" ball bearings: top bearing 422 and bottom bearing 426. The bearings 422 and 426 rest on ball bearing seats machined into the rotor shaft 432 end points 424 and 428, top and bottom respectively. This implementation allows the new common shaft 432 to rotate smoothly and minimize binding in sleeve 1. Sleeve 1 is press fitted into the manifold assembly 56. The top ball bearings 422 self aligns on the inner surface of the top hat 418. The bottom ball bearing 426 self aligns on set screw 427. The top hat 418 is made out of non-magnetic material and it overlays the shaft sensing magnet which is attached to shaft 432. The Hall effect sensor 39 is placed near the top hat 418.

Fig. 27 shows a cross-section of the alternate rotary servovalve 400 and how Sleeve 1 is press fitted into fluid manifold 56. Also shown is the positional relationship of the stator S and the actuator magnet PM, with specific functionality depicted in Fig. 8. Also shown is how electronic driver Q8 431 attaches to cover 408 via heat sink 430. Top hat 418 and set screw 427 are used to set proper tension for the shaft 432. Sleeve 1 is held in place by locknut 420. Bolts 82 are used to secure manifold 56 to rotary solenoid 33, inserted through holes 72 in the manifold. Sleeve 1 has been redesigned to have two precision rectangular slots 5, 47 and two circular openings 3, 45. Rectangular slots 5, 47 are retained from the original sleeve 1 design. Slot 47 is dedicated to fluid supply and slot 5 is used for fluid return. Control orifice 45 is associated with fluid port C2 and control orifice 3, diametrically opposite, is associated with fluid port C1. These ports C1 and C2, previously rectangular, are now circular allowing for greater ease in the manufacturing process resulting in reduced costs. Undoubtedly, numerous variations and modifications of the invention will become readily apparent to those familiar with servovalve system. For example, while particular, preferred operating mechanical and electrical components have been described, alternative components may be utilized in place of those suggested. Accordingly, the scope of the invention should not be construed as limited to the specific embodiments depicted and described.

Claims

1. A rotary servovalve system comprising: a pressurized fluid supply source, a fluid reservoir having a fluid pressure lower than that of said fluid supply source, a fluid transfer valve housing having a wall of annular cross section and at least one fluid inlet port coupled to said fluid supply source, at least one fluid outlet port coupled to said fluid reservoir and located diametrically opposite said fluid inlet port and at least one first fluid control port and at least one second fluid control port located diametrically opposite each other and equidistant from said inlet and outlet ports, a movable valve member located within said valve housing and alternatively rotatable in opposite angular directions from a closed position in which flow through all of said ports is blocked to positions in which each of said first and second fluid control ports alternatively permits flow therethrough from said fluid inlet port while the other of said first and second fluid control ports concurrently permits flow therethrough to said reservoir, a rotary magnetic solenoid having an electrically activated stator and an armature with at least one permanent magnet thereon alternatively rotatable relative to said stator in opposing angular directions from a null position and said at least one permanent magnet returns said armature to said null position when said stator is deactuated, and said armature drives said movable valve member so that said movable valve member is in said closed position when said armature is in said null position, a position sensor located proximate to said rotary magnetic solenoid to provide a feedback signal indicative of the position and direction of rotation of said armature relative to said null position, and a control circuit responsive to said position sensor to provide a feedback electrical signal having an electrical frequency response bandwidth of at least about sixty hertz to said stator to move said movable valve member to a target angular orientation relative to said valve housing.

2. A rotary servovalve according to Claim 1 wherein said control circuit provides a correction signal to said stator that is proportional to said feedback signal over a frequency range of at least about sixty hertz.

3. A rotary servovalve system according to Claim 1 wherein said control circuit includes: a comparator circuit for receiving said feedback signal and an externally generated command signal and for providing an error signal representing the difference between said feedback signal and said command signal, an error signal processing circuit including a proportional amplifier circuit, a differential amplifier circuit, and an integral amplifier circuit, each of which provides a separate output, and a combining circuit that receives all of said outputs from said processing circuit to produce a frequency compensated error signal proportional to the difference between said feedback signal and said command signal over a frequency range of at least about sixty hertz.

4. A rotary servovalve system according to Claim 3 further comprising an absolute value amplifier circuit coupled to said combining circuit and providing an absolute value error output signal proportional to the amplitude of said frequency compensated error signal irrespective of the polarity thereof, a polarity indicating amplifier circuit coupled to said combining circuit to produce an output indicative of the polarity of said frequency compensated error signal, and a current flow regulation circuit that drives said stator of said rotary magnetic solenoid to cause said armature to rotate in an angular direction which is determined by said polarity indicating amplifier circuit to an angle of displacement from said null position which is determined by said absolute value amplifier circuit.

5. A rotary servovalve system according to Claim 1 further comprising a pair of inlet ports as aforesaid, a pair of outlet ports as aforesaid, a pair of first fluid control ports as aforesaid, and a pair of second fluid control ports as aforesaid, and said ports within each pair of ports are located diametrically opposite and longitudinally offset from each other in said housing.

6. A rotary servovalve system according to Claim 1 wherein said rotary magnetic solenoid and said movable valve member are axially aligned with and longitudinally displaced from each other, and further comprising a coupling member joining said solenoid armature to said movable valve member.

7. A rotary servovalve system comprising a pressurized fluid supply having a pressure supply line leading therefrom, a fluid reservoir having a fluid relief line leading thereto, a valve housing having a valve cavity of circular cross section defined therewithin and defining at least one rectangular input port to said valve cavity coupled to said pressure supply line, at least one rectangular outlet port from said valve cavity coupled to said relief line and located diametrically opposite said inlet port, and at least one first rectangular fluid control port and at least one second rectangular fluid control port in communication with said valve cavity and said first and second control ports are located diametrically opposite each other and equidistant from said inlet and outlet ports, a bidirectional valve closure element having a gate portion with at least one pair of mutually parallel, longitudinally oriented and longitudinally aligned flow directing faces of rectangular shape and said valve closure element is located within said valve cavity and is coaxially aligned and rotatable therewithin to, in the alternative: (1 ) create concurrent flow paths between said first fluid control port and said inlet port and between said second fluid control port and said outlet port, (2) block all of said ports, and (3) create concurrent flow paths between said second fluid control port and said inlet port and between said first fluid control port and said outlet port, and a rotary solenoid having a stator and an armature with at least one permanent magnet rotatable within said stator between two extreme positions and biased toward a null position midway between said two extreme positions by magnetic force from said permanent magnet, and said armature is joined to said valve closure element so that when said armature is at said null position said valve closure element blocks all of said ports as aforesaid, a position sensor located proximate to said rotary solenoid to provide a feedback signal indicative of the position and direction of rotation of said armature relative to said null position, and a control circuit responsive to said position sensor to provide a feedback electrical signal having an electrical frequency response bandwidth of at least about sixty hertz to said stator to move said valve closure element to a target orientation relative to said valve housing.

8. A rotary servovalve system according to Claim 7 further characterized in that said position sensor is comprised of a Hall-effect magnetic sensor located proximate to said rotary solenoid and which detects the direction and extent of angular rotation of said solenoid armature from said null position and which provides an electrical position feedback signal indicative thereof, and said control circuit is responsive to rotation of said armature and includes: a position command signal source that provides an electrical position command signal, a comparator that receives said position feedback signal and said position command signal and which produces a position error signal, frequency sensitive circuitry coupled to said comparator to condition said position error signal and provide a conditioned output error signal having an amplitude that is proportionally responsive to said position feedback signal over a frequency range of at least about sixty hertz, and a current flow regulation circuit coupled to receive said conditioned output error signal and provide control outputs to operate said rotary solenoid and which provides no current to said rotary solenoid when said position feedback signal is equal to said position command signal.

9. A rotary servovalve system according to Claim 8 wherein said frequency sensitive circuitry includes a differential amplifier circuit, a proportional amplifier circuit and an integral amplifier circuit which are connected in parallel to each receive said position error signal, and a combining circuit which receives the outputs from said differential, proportional, and integral amplifier circuits and which provides said conditioned output error signal.

10. A rotary servovalve system according to Claim 9 further comprising a rectifier circuit coupled to receive said conditioned output error signal and to provide an absolute value error output signal of a predetermined polarity and having an amplitude proportional to said conditioned output error signal, and a polarity indicating amplifier circuit coupled to receive said conditioned output error signal and to provide a polarity indicating output governed by the polarity of said conditioned output error signal, and a full bridge power amplifier motor driver circuit that receives said absolute value error output signal and said polarity indicating output and which drives said stator of said rotary solenoid in accordance therewith.

11. A rotary servovalve system according to Claim 7 wherein said valve housing has a cylindrical annular shape and further comprising at least one pair of inlet ports, one pair of outlet ports, one pair of first fluid control ports, and one pair of second fluid control ports as aforesaid, and said ports in each of said pairs of ports are longitudinally offset on said valve housing from each other and are located on diametrically opposite sides of said valve housing from each other, and said gate portion of said valve closure element is comprised of at least one pair of said sets of mutually parallel, longitudinally oriented flow directing faces, and said pairs of flow directing faces are longitudinally offset from each other and are longitudinally aligned with said pairs of ports, whereby parallel flow paths are established through said valve housing and through said gate portion of said valve closure element as aforesaid.

12. A rotary servovalve system according to Claim 7 wherein said valve closure element and said armature are coaxially aligned with each other and longitudinally offset from each other, and further comprising an annular coupling member secured to both said valve closure element and to said armature.

13. A rotary servovalve system according to Claim 7 further characterized in that said position sensor is a Hall-effect magnetic sensor located proximate to said armature to detect rotation of said armature relative to said stator and which provides an electrical feedback signal indicative of direction and extent of angular rotation of said armature relative to said stator, and said control circuit receives said feedback signal and an externally generated command signal and generates an error signal indicative of the difference between said feedback signal and said error signal, and said control circuit is further comprised of a feedback loop coupled to receive said command and error signals and to provide outputs to said rotary solenoid armature to rotate it in a direction and to an extent so as to minimize said error signal.

14. A rotary servovalve system according to Claim 13 wherein said armature has a response that is frequency dependent and further comprising signal conditioning circuitry for receiving said error signal and for compensating forfrequency variations in said command signal so that said outputs to said rotary solenoid armature produce uniform responses by said armature over a frequency range by said command signal of at least about sixty hertz.

15. In a rotary servovalve system in which fluid is directed through at least one inlet port, at least one outlet port, at least one first fluid control port, and at least one second fluid control port in a valve housing as directed by a movable valve gate element rotatable within said housing in opposite directions of angular rotation from a position prohibiting fluid flow through any of said ports to alternative positions permitting fluid flow in alternative opposite directions through each of said first and second fluid control ports, the improvement comprising: a rotary magnetic solenoid having an armature that includes at least one permanent magnet and which is rotatable relative to a stator formed as an electromagnet that is energizeable to alternatively create electromagnetic fields having opposite polarities from each other and which, when deenergized, allows said armature to return to a neutral null position from positions of orientation in opposite angular directions, and said armature is coupled to carry said movable valve gate element in angular rotation therewith, a position sensor located proximate to said rotary magnetic solenoid and which senses the position of said solenoid armature relative to said stator and provides a feedback signal responsive thereto, and a control circuit coupled between said position sensor and said rotary magnetic solenoid to provide control inputs having an electrical frequency response bandwidth of at least about sixty hertz to said stator of said rotary magnetic solenoid.

16. A rotary servovalve system according to Claim 15 wherein said control circuit receives an externally generated command signal and said control circuitry includes a comparator circuit to compare said feedback signal with said command signal and to provide an error signal in accordance with the difference therebetween, and a frequency compensation circuitry coupled to receive said error signal and provide conditioned outputs that are not dependent upon frequency over a range of at least about sixty hertz.

17. A rotary servovalve system according to Claim 16 further comprising a full bridge motor driver amplifier circuit connected between said frequency compensation circuitry and said rotary magnetic solenoid for providing actuating signals to said stator.

18. A rotary servovalve system according to Claim 15 further comprising an intermediate coupler that joins said armature to said movable valve gate element.

19. A rotary servovalve system according to Claim 15 further comprising a pair of each of said ports as aforesaid, and said ports in each pair are located on opposite sides of said valve housing from each other so as to exert offsetting longitudinal bending forces on said movable valve element.

20. In a rotory valve including a hollow, cylindrical housing defining a longitudinal axis and having inlet and outlet ports defined therethrough and a valve core of a cylindrical configuration having transverse passageways defined therethrough and rotatably mounted within said valve housing, the improvement wherein said ports are aligned on said valve housing and said passageways are alignable with said ports by rotation of said valve core within said housing so that rotational bending moments upon said valve core produced by fluid pressure in said passageways are balanced at all times.

21. A rotory valve according to Claim 21 wherein said valve housing and said valve core both have first and second ends, and said ports are comprised of a first end inlet port, a second end inlet port, a central inlet port, a first end outlet port, a second end outlet port, and a central outlet port; and said end inlet and outlet ports are each equal in area to each other and are each half the area of each of said central ports, and said first end inlet port, said central outlet port and said second end inlet port are angularly aligned with each other and said central outlet port lies midway between said end inlet ports in a longitudinal direction, and said first end outlet port, said central inlet port and said second end outlet port are angularly aligned with each other and said central inlet port lies midway between said end outlet ports, and said first and second end inlet ports are angularly displaced 180 degrees from said first and second end outlet ports and said central inlet port is angularly displaced 180 degrees from said central outlet port.

22. A rotory valve according to Claim 21 wherein said first and second end inlet ports are respectively located diametrically opposite said first and second end outlet ports.

23. A rotory valve according to Claim 20 wherein all of said ports are rectangular in cross section and are equal in angular width.

24. A force balanced rotory valve comprising: a hollow cylindrical valve housing having a longitudinal axis and first and second opposite ends and defining a central radial inlet port therein and a central radial outlet port therein equal in area to each other and located in axial alignment and one hundred eighty degrees in angular displacement from each other, first end and second end radial inlet ports respectively located in said first and second ends of said valve housing in angular alignment with each other and with said central outlet port and longitudinally displaced equidistantly from said central outlet port, and first end and second end radial outlet ports respectively located in said first and second ends of said valve housing in angular alignment with each other and with said central inlet port and axially displaced equidistantly from said central inlet port, and each of said first and second end inlet and outlet ports has an area half that of each of said central ports, and a valve closure element of cylindrical configuration rotatably mounted within said valve housing and defining central, first end and second end transverse passages therethrough which are respectively longitudinally aligned with said central ports, said first end ports, and said second end ports, and said first end passageways and said second end passageways are each of a cross-sectional area one-half that of each of said central passageways, and said passageways extend in a transverse direction.

25. A valve according to Claim 24 wherein said passageways are straight and parallel to each other.

26. A valve according to Claim 25 wherein each of said ports has a rectangular shape and all of said ports are of equal angular width.

27. A rotory valve comprising: a hollow cylindrical valve housing having a longitudinal axis and first and second opposite ends and defining a central inlet port and a central outlet port equal in area to each other and longitudinally aligned and angularly displaced one hundred eighty degrees from each other, a first end inlet port and a first end outlet port equal in area to each other and each equal to half the area of each of said central ports and longitudinally aligned and angularly displaced one hundred eighty degrees from each other and located in said first end of said valve housing at a longitudinal offset distance from said central ports, a second end inlet port and a second end outlet port equal in area to each other and each equal to half the area of each of said central ports and longitudinally aligned and angularly displaced one hundred eighty degrees from each other and located in said second end of said valve housing at said same longitudinal offset distance from said central ports, and a valve core of cylindrical configuration rotatably mounted within said valve housing and having central, first end, and second end passageways defined therethrough which are respectively longitudinally aligned with said central, first end and second end ports, and said first end and second end passageways each have a cross- sectional area half that of said central passageway, and said passageways are oriented so as to provide concurrent fluid flow through said passageways through all of said ports when said valve core is rotated to an open position within said valve housing and so as to concurrently block all of said passageways when said valve core is rotated to a closed position within said valve housing.

28. A rotory valve according to Claim 27 wherein all of said ports are of equal angular width and have a rectangular shape.

29. A rotory servovalve comprising: a fluid transfer valve housing having a wall of annular cross section and a plurality of fluid inlet ports coupled to a common fluid inlet line, a plurality of fluid outlet ports coupled to a common fluid outlet line, a plurality of first fluid control ports coupled to a common first fluid control line, and a plurality of second fluid control ports coupled to a common second fluid control line, and at least two of said inlet ports are angularly displaced from each other by one hundred eighty degrees and are longitudinally offset from each other in said housing, at least two of said outlet ports are angularly displaced from each other by one hundred eighty degrees and are longitudinally offset from each other in said housing , at least two of said first fluid control ports are angularly displaced from each other by one hundred eighty degrees and are longitudinally offset from each other in said housing, and at least two of said second fluid control ports are angularly displaced from each other by one hundred eighty degrees and are longitudinally offset from each other in said housing, and said inlet and outlet ports are each angularly displaced from said control ports by ninety degrees.

30. A rotory servovalve comprising: a valve housing of a cylindrical shape and having a valve cavity of circular cross section defined therewithin and defining at least two rectangular inlet ports to said valve cavity, and at least one of said fluid inlet ports is angularly offset one hundred eighty degrees from at least one other of said fluid inlet ports, at least two rectangular outlet ports from said valve cavity and at least one of said fluid outlet ports is angularly offset one hundred eighty degrees from at least one other of said fluid outlet ports, and at least two first rectangular fluid control ports in communication with said valve cavity and at least one of said first fluid control ports is angularly offset one hundred eighty degrees from at least one other of said first fluid control ports, and at least two second rectangular fluid control ports in communication with said valve cavity and at least one of said second control ports is angularly offset one hundred eighty degrees from one other of said second fluid control ports and said first and second fluid control ports are all angularly offset equidistantly from all of said inlet and outlet ports, a bidirectional valve closure element having a gate portion with at least two pairs of two mutually parallel, flow directing faces of rectangular shape, and said pairs of flow directing faces are longitudinally offset from each other and are longitudinally aligned with said ports and said flow directing faces in each pair are longitudinally aligned with each other and laterally spaced from each other, whereby pairs of longitudinally offset parallel flow paths are established through said valve housing and through said gate portion of said valve closure element, and said valve closure element is located within said valve cavity and is coaxially aligned and rotatable therewithin to, in the alternative: (1) permit concurrent fluid flow therethrough in opposite directions within each pair of mutually parallel flow paths, and (2) concurrently block all of said inlet ports and all of said outlet ports.

31. In a rotory servovalve system in which fluid is directed through an inlet port, an outlet port, a first fluid control port, and a second fluid control port in a valve housing as directed by a movable valve gate element rotatable within said housing in opposite directions of angular rotation from a position prohibiting fluid flow through any of said ports to alternative positions permitting fluid flow in alternative opposite directions through each of said first and second fluid control ports, the improvement comprising a plurality of each of said ports as aforesaid, and at least two of said inlet ports are located on opposite sides of said valve housing from each other, at least two of said outlet ports are located on opposite sides of said valve housing from each other, at least two of said first fluid control ports are located on opposite sides of said valve housing from each other, and at least two of said second fluid control ports are located on opposite sides of said valve housing from each other, and said ports are located in said valve housing such that offsetting bending forces are created on said movable valve element by fluid pressure within said valve.

32. A precision control device comprising: a rotary magnetic solenoid having an electrically activated stator and an armature with at least one permanent magnet thereon alternatively rotatable relative to said stator in opposing angular directions from a null position and said at least one permanent magnet returns said armature to said null position when said stator is deactuated, a sensor located proximate to said rotary magnetic solenoid to provide a feedback signal indicative of the position and direction of rotation of said armature relative to said null position, and a proportional, integral and derivative control circuit responsive to said sensor to provide a feedback electrical signal to said stator to move said armature to a target angular orientation relative to said stator.

33. A precision control device according to Claim 32 wherein said control circuit provides a correction signal to said stator that is proportional to said feedback signal over a frequency range of at least about sixty hertz.

34. A precision control device according to Claim 32 wherein said control circuit provides a correction signal to said stator that is proportional to said feedback signal over a frequency range of at least about sixty hertz.

35. A precision control device according to Claim 32 wherein said control circuit includes: a comparator circuit for receiving said feedback signal and an externally generated command signal and for providing an error signal representing the difference between said feedback signal and said command signal, an error signal processing circuit including a proportional amplifier circuit, a differential amplifier circuit, and an integral amplifier circuit, each of which provides a separate output, and a combining circuit that receives all of said outputs from said processing circuit to produce a frequency compensated error signal proportional to the difference between said feedback signal and said command signal.

36. A precision control device according to Claim 35 further comprising an absolute value amplifier circuit coupled to said combining circuit and providing an absolute value error output signal proportional to the amplitude of said frequency compensated error signal irrespective of the polarity thereof, a polarity indicating amplifier circuit coupled to said combining circuit to produce an output indicative of the polarity of said frequency compensated error signal, and a current flow regulation circuit that drives said stator of said rotary magnetic solenoid to cause said armature to rotate in an angular direction which is determined by said polarity indicating amplifier circuit to an angle of displacement from said null position which is determined by said absolute value amplifier circuit.

37. A precision control device according to Claim 35 wherein said frequency compensated error signal is proportional to the difference between said feedback signal and said command signal over a frequency range of at least about sixty hertz.

38. A precision control device according to Claim 32 wherein said armature has an axis of rotation and said permanent magnet has a direction of magnetization parallel to said axis of rotation.

39. A precision controller comprising a rotary solenoid having a stator and an armature with at least one permanent magnet rotatable within said stator between two extreme positions and biased toward a null position midway between said two extreme positions by magnetic force from said permanent magnet, an electrical control circuit responsive to rotation of said armature and including a sensor located proximate to said rotary solenoid and which detects the direction and extent of angular rotation of said solenoid armature from said null position and which provides an electrical position feedback signal indicative thereof, a position command signal source that provides an electrical position command signal, a comparator that receives said position feedback signal and said position command signal and which produces a position error signal, frequency sensitive circuitry coupled to said comparator to condition said position error signal and provide a conditioned output error signal having an amplitude that is proportionally responsive to said position feedback signal, and a current flow regulation circuit coupled to receive said conditioned output error signal and provide control outputs to operate said rotary solenoid and which provides no current to said rotary solenoid when said position feedback signal is equal to said position command signal.

40. A precision controller according to Claim 39 wherein said permanent magnet has a direction of magnetization and said armature has an axis of rotation that is parallel to said direction of magnetization.

41. A precision controller according to Claim 39 wherein said frequency sensitive circuitry includes a differential amplifier circuit, a proportional amplifier circuit and an integral amplifier circuit which are connected in parallel to each receive said position error signal, and a combining circuit which receives the outputs from said differential, proportional, and integral amplifier circuits and which provides said conditioned output error signal.

42. A precision controller according to Claim 41 further comprising a rectifier circuit coupled to receive said conditioned output error signal and to provide an absolute value error output signal of a predetermined polarity and having an amplitude proportional to said conditioned output error signal, and a polarity indicating amplifier circuit coupled to receive said conditioned output error signal and to provide a polarity indicating output governed by the polarity of said conditioned output error signal, and a full bridge power amplifier motor driver circuit that receives said absolute value error output signal and said polarity indicating output and which drives said stator of said rotary solenoid in accordance therewith.

43. A precision controller comprising: a rotary solenoid having a stator and an armature with at least one permanent magnet rotatable within said stator between two extreme positions and biased toward a null position midway between said two extreme positions by magnetic force from said permanent magnet, a magnetic sensor located proximate to said armature to detect rotation of said armature relative to said stator and which provides an electrical feedback signal indicative of direction and extent of angular rotation of said armature relative to said stator, and a control circuit that receives said feedback signal and an externally generated command signal and which generates an error signal indicative of the difference between said feedback signal and said error signal, and a feedback loop coupled to receive said command and error signals and to provide outputs to said rotary solenoid armature to rotate it in a direction and to an extent so as to minimize said error signal.

44. A precision controller according to Claim 43 wherein said armature has a response that is frequency dependent and further comprising signal conditioning circuitry for receiving said error signal and for compensating for frequency variations in said command signal so that said outputs to said rotary solenoid armature produce uniform responses by said armature over a frequency range by said command signal of at least about sixty hertz.

45. A precision controller according to Claim 43 wherein said armature has a response that is frequency dependent and further comprising signal conditioning circuitry for receiving said error signal and for compensating for frequency variations in said command signal so that said outputs to said rotary solenoid armature produce uniform responses by said armature over a frequency range by said command signal of at least about sixty hertz.

46. A precision controller according to Claim 43 wherein said control circuit receives an externally generated command signal and said control circuitry includes a comparator circuit to compare said feedback signal with said command signal and to provide an error signal in accordance with the difference therebetween, and a frequency compensation circuitry coupled to receive said error signal and provide conditioned outputs that are not dependent upon frequency over a range of at least about sixty hertz.

47. A rotary servovalve system according to Claim 46 further comprising a full bridge motor driver amplifier circuit connected between said frequency compensation circuitry and said rotary magnetic solenoid for providing actuating signals to said stator.

48. A precision controller according to Claim 43 wherein said permanent magnet has a direction of magnetization and said armature has an axis of rotation that is parallel to said direction of magnetization.

49. A control circuit for controlling a rotary servovalve system comprising: a comparator circuit for receiving said feedback signal and an externally generated command signal and for providing an error signal representing the difference between said feedback signal and said command signal, an error signal processing circuit including a proportional amplifier circuit, a differential amplifier circuit, and an integral amplifier circuit, each of which provides a separate output, and a combining circuit that receives all of said outputs from said processing circuit to produce a frequency compensated error signal proportional to the difference between said feedback signal and said command signal over a frequency range of at least about sixty hertz.

50. A control circuit according to Claim 49 further comprising an absolute value amplifier circuit coupled to said combining circuit and providing an absolute value error output signal proportional to the amplitude of said frequency compensated error signal irrespective of the polarity thereof, a polarity indicating amplifier circuit coupled to said combining circuit to produce an output indicative of the polarity of said frequency compensated error signal, and a current flow regulation circuit that drives said stator of said rotary magnetic solenoid to cause said armature to rotate in an angular direction which is determined by said polarity indicating amplifier circuit to an angle of displacement which is determined by said absolute value amplifier circuit.

51. A control circuit according to Claim 50 wherein said frequency compensated error signal is proportional to the difference between said feedback signal and said command signal over a frequency range of at least about sixty hertz.

ROTARY SERVOVALVE AND CONTROL SYSTEM

Abstract

An improved rotary servovalve system employs a rotary magnetic solenoid having an armature that includes at least one permanent magnet. The armature is rotatable relative to a stator formed as an electromagnet which is energizable to create alternative electromagnetic fields having opposite polarities from each other. When deenergized, the stator allows the armature to return to a neutral, null position from positions of extreme rotation in opposite angular directions due to the magnetic force of the permanent magnet of the armature. The armature is coupled to carry a movable valve element in angular rotation therewith, so that flow through the servovalve of the system can occur in alternative directions. Also, the valve element is biased toward a position in which all of the valve ports are closed when power is removed from the rotary solenoid. The control circuit employed in the rotary servovalve system expands the bandwidth of response of the solenoid actuator by compensating for frequency variations in the input command signal and in the feedback signal. This compensation is achieved utilizing a combined proportional, integral, and differential amplification circuit. Also, imbalance of fluid forces within the servovalve mechanism can be avoided by utilizing a pair of inlet orifices, a pair of outlet orifices, a pair of first fluid control orifices, and a pair of second fluid control orifices. The orifices within each pair are located on opposite sides of the valve housing from each other.