Servo valve
11530755 · 2022-12-20
Assignee
Inventors
Cpc classification
F16K11/07
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F15B13/044
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F15B13/0402
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
Abstract
A servo valve comprising: a fluid transfer valve assembly comprising a supply port and a control port (P.sub.A, P.sub.B); a moveable valve spool arranged to regulate flow of fluid from the supply port to the control port in response to a control signal; and a drive means configured to axially move the valve spool relative to the fluid transfer assembly in response to the control signal to regulate the fluid flow; wherein the drive means comprises a piezo actuator element mounted within and axially movable with the valve spool, the piezo actuator configured to extend axially in response to the control signal to cause corresponding axially movement of the spool.
Claims
1. A servo valve comprising: a fluid transfer valve assembly comprising: a housing; a supply port, a return port and a control port defined in the housing; a moveable valve spool located in the housing arranged to allow flow of fluid through the moveable valve spool from the supply port to the return port when the moveable valve spool is in a neutral position relative to the housing and to allow flow of fluid from the supply port to the control port through the moveable valve spool when the moveable valve spool is in a position axially spaced from the neutral position; and a drive means configured to axially move the moveable valve spool relative to the housing in response to the control signal to regulate the fluid flow; wherein the drive means comprises a piezo actuator element located fully within the housing and extending from a first spool end of a spool body, the piezo actuator configured to have a first length defining the neutral position of the moveable valve spool and to change its length axially in response to a control signal to cause corresponding axially movement of the moveable valve spool to the position axially displaced from the neutral position; wherein the piezo actuator element is mounted to the first spool end of the moveable valve spool and extends into the spool body from the first spool end; and the servo valve further comprising a spring element located at a second spool end of the moveable valve spool opposite the first spool end arranged to bias the moveable valve spool to the neutral position in an axial direction opposite the direction in which the piezo actuator element moves the spool.
2. The servo valve of claim 1, wherein the control signal is in the form of an electric potential applied to the piezo actuator element to cause the piezo actuator element to change its length in the axial direction.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
(1)
(2)
(3)
(4)
(5)
DETAILED DESCRIPTION
(6) A servo valve as described below can, for example, be used in an actuator control system. The servo valve is controlled by a drive assembly to control a flow of fluid that is output to control the movement of an actuator. The actuator can control e.g. ailerons or elevator flaps of an aircraft.
(7) Conventional jet pipe and flapper servo valves will first be described with reference to
(8) A typical flapper servo valve is shown in
(9) Therefore, when the control signal is such as to cause the drive assembly to apply greater fluid pressure to one end of the spool, by diverting more fluid to that end via channel 12, as compared to channel 11, the spool 2 will move to the right. If greater fluid pressure is applied via channel 11, the spool 2 will move to the left. In the flapper arrangement, shown, the control signal is applied to a torque motor 16 and armature 5 which causes a flapper-type drive member 6 to deflect left or right. The flapper 6 is positioned between orifices 9, 10 at the ends of channels 11,12 respectively. If the control signal, via armature 5, causes the flapper 6 to move to the left thus closing off orifice 10 of channel 12, then essentially all of the hydraulic fluid in channel 12, will be directed to the end of the spool as it can no longer exit orifice 10, thus increasing the pressure at the left end of the spool 2 and causing the spool to move to the right. If the control signal is such as to cause the flapper 6 to move to the right, closing orifice 9 of channel 11, then more pressure is provided to the other end of the spool 2 via channel 11, causing the spool 2 to move to the left.
(10) A positioning mechanism may be provided at the ends of the valve spool, e.g. a torsion spring 14,15 at each of the respective ends of the valve spool or some other mechanical or electrical position feedback arrangement.
(11) The principles of operation are similar for the jet-pipe type assembly, but instead of the drive member being a flapper 6 that moves to close off a respective channel, the drive member is a pipe 7 with a nozzle which is deflected left or right responsive to the control signal and from which fluid is ejected to either the left or the right end of the spool.
(12) In a conventional jet-pipe type assembly, as shown in
(13) In an example, the assembly is arranged to control an actuator based on the fluid flow from the control port e.g. via a butterfly valve. The servo valve controls an actuator which, in turn, controls an air valve such as a butterfly valve.
(14) Supply pressure is provided to the servo valve housing via the supply port and to the spool via spool supply ports. The pressure at the return port is a return pressure which will vary depending e.g. on the altitude of the aircraft in flight. Control ports provide a controlled pressure, dependant on the nozzle/flapper position and resulting spool position, to be provided to an actuator.
(15) The spool is in the form of a tubular member arranged in a valve block (not shown) to be moved axially by the hydraulic fluid.
(16) In more detail, both in the conventional flapper or jet-pipe type assemblies, to open the servo valve, control current is provided to coils of the motor (e.g. a torque motor) creating electromagnetic torque opposing the sum of mechanical and magnetic torque already ‘present’ in the torque motor. The bigger the electromagnetic force from the coils, the more the jet pipe nozzle turns or the flapper pivots. The more it turns/pivots, the greater the linear or axial movement of the spool. A torque motor usually consists of coil windings, a ferromagnetic armature, permanent magnets and a mechanical spring (e.g. two torsional bridge shafts). This arrangement provides movement of the nozzle/flapper proportional to the input control current.
(17) Jet-pipe arrangements can operate at high frequency but only for average pressure levels. In contrast, the flapper arrangements can operate at higher pressures but at lower frequency.
(18) As mentioned above, with torque motor-driven pipes or flappers, the extreme positions of the valves are not achieved in an efficient manner.
(19) The inventors have found a solution to this problem by replacing the torque motor and associated drive stage with a piezo actuator located entirely in the valve stage in the valve spool body. This avoids the need for a separate motor and drive stage and the hydraulic system required by conventional systems to move the flapper or jet pipe to change the position of the spool.
(20) As can be seen in
(21) A piezo actuator element 25 is mounted in the spool body 20 extending from one end thereof and extending into the spool body 20 from that end. A spring is provided at the other end of the spool body 20 to bias the spool body away from that end.
(22) In a neutral position, the spring force acting on one end of the spool is such as to position the spool to define flow channels from the oil supply 23 and the return port 24. To control the spool body 20 to move left or right (with regard to the drawings) a force is applied by the piezo actuator element 25 on the spool body against the force of the spring, thus moving the spool body so that different ports and channels are aligned so as to change the flow path for the hydraulic fluid through the valve. The oil will then be directed through control ports to move the actuator.
(23) The piezo actuator element 25 is caused to deform or extend in response to application of an electric potential to the element which corresponds to the control signal of conventional systems. The applied potential determines the extent to which the piezo actuator element expands along the direction of the spool body length, which determines the amount the spool body moves in that direction, pushed by the piezo actuator element. The ports and channels then align and misalign as in existing systems to define appropriate flow paths.
(24) The rest of the operation of the spool assembly is analogous to that of the flapper and jet-pipe arrangements.
(25) As can be seen in
(26) According to the disclosure, with such an arrangement, the conventional two stages of a valve assembly are combined into a single stage. The piezo actuator element acts directly on the spool body in proportion to the control signal. A piezo actuator has at least three to four time greater frequency than conventional torque motor assemblies.
(27) Thus, a servo valve assembly according to this disclosure is much smaller, lighter and simpler than existing designs.
(28) Although this disclosure has been described in terms of preferred examples, it should be understood that these examples are illustrative only and modifications and alterations are possible within the scope of the claims.