GB2053421A - Hydraulic servo valve - Google Patents

Hydraulic servo valve Download PDF

Info

Publication number
GB2053421A
GB2053421A GB8014650A GB8014650A GB2053421A GB 2053421 A GB2053421 A GB 2053421A GB 8014650 A GB8014650 A GB 8014650A GB 8014650 A GB8014650 A GB 8014650A GB 2053421 A GB2053421 A GB 2053421A
Authority
GB
United Kingdom
Prior art keywords
fluid
electroviscous
valve
pilot circuit
flow
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
GB8014650A
Other versions
GB2053421B (en
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
UK Secretary of State for Defence
Original Assignee
UK Secretary of State for Defence
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by UK Secretary of State for Defence filed Critical UK Secretary of State for Defence
Priority to GB8014650A priority Critical patent/GB2053421B/en
Publication of GB2053421A publication Critical patent/GB2053421A/en
Application granted granted Critical
Publication of GB2053421B publication Critical patent/GB2053421B/en
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F15FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
    • F15CFLUID-CIRCUIT ELEMENTS PREDOMINANTLY USED FOR COMPUTING OR CONTROL PURPOSES
    • F15C7/00Hybrid elements, i.e. circuit elements having features according to groups F15C1/00 and F15C3/00
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16KVALVES; TAPS; COCKS; ACTUATING-FLOATS; DEVICES FOR VENTING OR AERATING
    • F16K31/00Actuating devices; Operating means; Releasing devices
    • F16K31/12Actuating devices; Operating means; Releasing devices actuated by fluid
    • F16K31/42Actuating devices; Operating means; Releasing devices actuated by fluid by means of electrically-actuated members in the supply or discharge conduits of the fluid motor
    • F16K31/423Actuating devices; Operating means; Releasing devices actuated by fluid by means of electrically-actuated members in the supply or discharge conduits of the fluid motor the actuated members consisting of multiple way valves
    • F16K31/426Actuating devices; Operating means; Releasing devices actuated by fluid by means of electrically-actuated members in the supply or discharge conduits of the fluid motor the actuated members consisting of multiple way valves the actuated valves being cylindrical sliding valves

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Theoretical Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Servomotors (AREA)

Abstract

A hydraulic servo valve suitable for controlling flow of a pressurised fluid in dirty and explosive environments comprises a control valve (1) actuated by a contamination- free sealed pilot circuit (22) of electroviscous fluid commanded by electroviscous valves (25-28) requiring minimal electrical power. Fluid is circulated in the pilot circuit by pressure pulses derived from the pressurised fluid by means of a fluidic oscillator (11) and transmitted to the pilot circuit via flexible diaphragms (18). <IMAGE>

Description

SPECIFICATION A hydraulic servo valve This invention relates to a hydraulic servo valve suitable for use in dirty and explosive environments.
Hydraulic machinery is often called upon to operate in situations in which it is exposed to dust, dirt and explosive atmospheres, a coal mine for example. In machinery for use in coal mines it is found that the working hydraulic fluid is frequently contaminated with dust etc which tends to jam electro-hydrauiic servo valves. To overcome this, the electrical actuators of the servo valves are made to be unusually powerful, so that the spool can displace grit in the seatings. However, such powerful electrical actuation requires that relatively high levels of electrical power must be supplied, which may well be sufficient to initiate an explosion in a "fiery" mine, should any failure of insulation occur.For this reason, it is at present necessary to enclose the electro-hydraulic valves of mining equipment in expensive flame-proof enclosures, which are of sufficient thickness to withstand explosion of the atmosphere within.
Electroviscous valves employing electroviscous fluids are known for use in the control of hydraulic servo valves, as described in UK Patent Specification No 1511658 for example.
Electroviscous fluids undergo a change in shear resistance when they are exposed to electric fields, typically of 2 kV over a 1 mm gap, which property is exploited in an electroviscous valve, the fluid being passed between electrodes to which suitably variable voltages can be applied so as to vary the fluid flow rate through the valve.
Although the voltages required are high, the current requirement is very low and the total electrical power demanded would generally be insufficient to initiate an explosion in an explosive atmosphere. For additional safety, a high impedance source can be employed to eliminate explosion risk in the event of a short circuit. In principle therefore, it is possible to make an electroviscous device inherently safe, so that it does not require a flameproof enclosure. However, in an environment in which contamination of working fluids is likely to occur, electroviscous fluid cannot be used as the primary working fluid, nor as a secondary control fluid in an open circuit, as dirt in the fluid would rapidly lead to failure due to arcing at the electroviscous valve electrodes.
The present invention seeks to provide a hydraulic servo valve controlled by means of an entirely enclosed electroviscous fluid circuit requiring relativeiy little electrical command power.
In accordance with the present invention a hydraulic servo valve having an adjustable control valve for controlling flow of a pressurised primary fluid includes: a sealed pilot circuit of electroviscous fluid having pressure transmitting means for adjusting the control valve and electrically controlled valve means for varying electroviscous fluid pressure at the transmitting means; and a pumping means driveable by the primary fluid for circulating the electroviscous fluid within the sealed pilot circuit.
The control valve may be linearly or rotatably adjustable, linear movement being directly imparted to the valve by the pressure transmitting means and rotary movement being indirectly imparted via suitable torsional elements.
The electrically controlled valve means and the pressure transmitting means may be conveniently combined in an integral arrangement of two opposed-flow electroviscous valves having a common movable core, as described in UK Patent Application Number 47545/78, the movable core comprising the pressure transmitting means and being directly coupled with the control valve.
Alternatively, the electrically controlled valve means may comprise a known "Wheatstone Bridge" arrangement of four electroviscous valves disposed as series pairs in two parallel flow paths of the pilot circuit, two flexible-walled chambers comprising the pressure transmitting means, being respectively located intermediate each series pair. In this arrangement, the control valve preferably comprises a spool valve, the spool having two opposing end faces arranged in contact with the two flexible-walled chambers respectively.
The pumping means is preferably isolated from the electroviscous fluid to avoid the possibility of dirt entering the pilot circuit, such as may occur through the sliding seals of conventional in-circuit pumps. A suitable isolated pumping means includes: a fluidic oscillator located in a subsidiary flow line of the primary fluid for directing primary fluid to flow alternately through two parallel outlet flow lines; fluid pressure coupling means for communicating pressure of the primary fluid flowing through each of the two outlet flow lines respectively to the electroviscous fluid in the pilot circuit at two pumping stations thereof; and oneway flow means located in the pilot circuit intermediate the pumping stations.
An embodiment of the invention will now be described by way of example only, with reference to the accompanying drawing which is a diagrammatic representation of a spool valve controlled by a hydraulically driven electroviscous pilot circuit.
A spool valve 1 having a spool 2 and two opposing end faces 3 and 4 is connected to direct a flow of pressurised primary fluid 5 from an inlet line 6 to one or other of two outlet lines 7 and 8. A portion of the primary fluid flow in the line 6 is diverted to flow via a branch flow line 9 to a pumping means 10 which includes a fluidic oscillator 11 having a flow splitter 12 and conventional fluidic control means (not shown) which induce the incoming flow to oscillate between two outlet flow lines 13 and 14. These two outlet lines then re-unite and the fluid is returned via a line 1 5 to a low pressure return line of the primary hydraulic circuit (not shown).
The pumping means 10 further includes two pumping stations 1 6 and 1 7 each comprising two chambers 1 6a, 1 6b and 1 7a, 1 7b respectively, separated by a flexible diaphragm 18, and chambers 1 6a and 1 7a being connected via ducts 19 and 20 to the lines 1 3 and 14 respectively. The chambers 1 6b and 1 7b are both open to electroviscous fluid 21 contained in a sealed pilot circuit 22.
Two free non-return valves 23 and 24 comprising the one-way flow means of the pilot circuit, also form part of the pumping means 10 and are located in the pilot circuit 22, one at each side of the chamber 1 7b.
In operation, the action of the oscillator 11 powered by primary fluid flow in the line 9, causes the fluid pressure within the chambers 1 6a and 1 7a to rise and fall in antiphase at a frequency linearly dependent upon the primary fluid flow rate in the line 9. These pressure pulsations are superimposed, via the diaphragms 18, upon the electroviscous fluid in the chambers 1 6b and 1 7b respectively, where they operate in conjunction with the non-return valves 23 and 24, to circulate the electroviscous fluid in the pilot circuit 22. The flow rate generated in the pilot circuit 22 is thus dependent upon the operation of the oscillator 11, which in turn depends upon the primary fluid flow rate in the line 9.The flow rate in the line 9 may be selected by means of an optional restrictor valve 32 in the line 1 5, to enable a constant flow rate to be set up in the pilot circuit 22, whatever the pressure may be of the specific primary fluid supply to which the servovalve is to be applied.
The remaining components of the pilot circuit 22 include four electroviscous valves 25, 26, 27, 28 disposed in a conventional "Wheatstone Bridge" arrangement, and a pressure transmitting means comprising two chambers 29 and 30 located respectively between the valves 25 and 26 and the valves 27 and 28. The chambers 29 and 30 are each closed with a flexible diaphragm 31 sealed respectively to the end faces 3 and 4 of the spool 2.
Electrical connections (not shown) are provided to each of the four valves 25 to 28, by means of which variable voltages can be applied to modify the rate of flow of electroviscous fluid through each valve so as to vary differentially the electroviscous fluid pressures within the two chambers 29 and 30, thereby to actuate the spool 2 to switch the inlet line 6 from one to the other of the outlet lines 7 and 8.
It will be apparent to those skilled in the art that various alternative arrangements of a servo valve in accordance with the present invention are possible. For example, pumping pulses for circulating the electroviscous fluid within the sealed pilot circuit could be derived from a hydraulic motor running in.a a primary fluid flow, but although this arrangement would provide a higher pumping efficiency than a fluidic oscillator, it would suffer from the disadvantage that contamination in the primary fluid could cause the hydraulic motor to jam. Further, various arrangements of electroviscous valves may be used in the pilot circuit to operate the control valve, and the one-way flow means of the pilot circuit may comprise fluidic valves or electroviscous valves operating in synchronism with the pumping pulses.
The completely sealed electroviscous pilot circuit of the present invention has the attendant advantage that the servo valve may be preassembled in a clean atmosphere and can also be embedded in a solid medium, if further protection is desired, as at no point is the system open to atmosphere. Furthermore, electroviscous valves do not demand the close dimensional tolerances of conventional hydraulic valves and, because the electroviscous fluid flow rate in the pilot circuit is effectively independent of the primary fluid supply pressure, single-size electroviscous valves may be used to serve over a wide range of applications.

Claims (7)

1. A hydraulic servo valve having an adjustable control valve for controlling flow of a pressurised primary fluid and including: a sealed pilot circuit of electroviscous fluid having pressure transmitting means for adjusting the control valve and electrically controlled valve means for varying electroviscous fluid pressure at the transmitting means; and a pumping means driveable by the primary fluid for circulating the electroviscous fluid within the sealed pilot circuit.
2. A servo valve as claimed in Claim 1 wherein the electrically controlled valve means comprises four electroviscous valves disposed as series pairs in two parallel flow paths of the pilot circuit and the pressure transmitting means comprises two flexible-walled chambers respectively located intermediate each series pair.
3. A servo valve as claimed in Claim 2 wherein the control valve comprises a spool valve, having a spool disposed so as to have two opposing end faces in contact with the two flexible-walled chambers respectively.
4. A servo valve as claimed in Claim 1 wherein the electrically controlled valve means comprises two opposed-flow electroviscous valves having a common movable core which core comprises the pressure transmitting means.
5. A servo valve as claimed in any of the preceding claims wherein the pumping means includes: a fluidic oscillator located in a subsidiary flow line of the primary fluid for directing primary fluid to flow alternately through two parallel outlet flow lines; fluid pressure coupling means for communicating pressure of the primary fluid flowing in each of the two outlet flow lines to the electroviscous fluid in the pilot circuit at two respective pumping stations thereof; and one-way flow means located in the pilot circuit intermediate the pumping stations.
6. A servo valve as claimed in any one of Claims 1 to 4 wherein the pumping means comprises a hydraulic motor.
7. A servo valve substantially as hereinbefore described with reference to the accompanying drawing.
GB8014650A 1979-05-15 1980-05-02 Hydraulic servo valve Expired GB2053421B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB8014650A GB2053421B (en) 1979-05-15 1980-05-02 Hydraulic servo valve

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB7916838 1979-05-15
GB8014650A GB2053421B (en) 1979-05-15 1980-05-02 Hydraulic servo valve

Publications (2)

Publication Number Publication Date
GB2053421A true GB2053421A (en) 1981-02-04
GB2053421B GB2053421B (en) 1983-01-12

Family

ID=26271528

Family Applications (1)

Application Number Title Priority Date Filing Date
GB8014650A Expired GB2053421B (en) 1979-05-15 1980-05-02 Hydraulic servo valve

Country Status (1)

Country Link
GB (1) GB2053421B (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1997049924A2 (en) * 1996-06-25 1997-12-31 Er Fluid Developments Limited Improvements in, or relating to, high speed actuators and vibrators based on electro-rheological fluids

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1997049924A2 (en) * 1996-06-25 1997-12-31 Er Fluid Developments Limited Improvements in, or relating to, high speed actuators and vibrators based on electro-rheological fluids
WO1997049924A3 (en) * 1996-06-25 1998-03-12 Er Fluid Dev Improvements in, or relating to, high speed actuators and vibrators based on electro-rheological fluids
US6272852B1 (en) 1996-06-25 2001-08-14 Er Fluid Developments Limited High speed actuators and vibrators based on electro-rheological fluids

Also Published As

Publication number Publication date
GB2053421B (en) 1983-01-12

Similar Documents

Publication Publication Date Title
US4342334A (en) Hydraulic servo valve
US3874269A (en) Hydraulic actuator controls
US3279323A (en) Electrohydraulic actuator
US3928968A (en) Power transmission
US4667472A (en) Electric integrated actuator with variable gain hydraulic output
GB2129528A (en) Valve with internal pilot
US3757823A (en) Valve
US3211182A (en) Servo valve with rotary first stage
US3709257A (en) Electro-hydraulic servomechanism
US3643699A (en) Torque motor operated valve
US4473751A (en) Non-conventional reciprocating hydraulic-electric power source
US4574686A (en) Digital proportional spool position control of compensated valves
US4568292A (en) Hydraulic assistance device for use in a steering system
SE8502089L (en) Multifunction valve
JP4071960B2 (en) Fail-freeze servo valve
GB2053421A (en) Hydraulic servo valve
US3646754A (en) Motor operated servo pump
US3400541A (en) Manipulator apparatus
SE8503569D0 (en) DEVICE OF A HYDRAULIC CIRCUIT INCLUDING A PRESSURE FLUID BELL AND AT LEAST A HYDRAULIC ENGINE
US4651045A (en) Electromagnetically interference-proof flight control device
US3580281A (en) Control valve
US5570718A (en) Multiplexing valve
US3877486A (en) Electrical-to-fluidic interface device
US2976848A (en) Linearized parallel control valve for control systems
JPS5983808A (en) Servo valve and its driving method

Legal Events

Date Code Title Description
732 Registration of transactions, instruments or events in the register (sect. 32/1977)
732 Registration of transactions, instruments or events in the register (sect. 32/1977)
PCNP Patent ceased through non-payment of renewal fee

Effective date: 19930502