GB2189054A - Servovalves - Google Patents

Servovalves Download PDF

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Publication number
GB2189054A
GB2189054A GB08707384A GB8707384A GB2189054A GB 2189054 A GB2189054 A GB 2189054A GB 08707384 A GB08707384 A GB 08707384A GB 8707384 A GB8707384 A GB 8707384A GB 2189054 A GB2189054 A GB 2189054A
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GB
United Kingdom
Prior art keywords
spool
bore
servovalve
flapper
fluid pressure
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.)
Withdrawn
Application number
GB08707384A
Other versions
GB8707384D0 (en
Inventor
David John Steed
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.)
Dowty Boulton Paul Ltd
Original Assignee
Dowty Boulton Paul Ltd
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 Dowty Boulton Paul Ltd filed Critical Dowty Boulton Paul Ltd
Publication of GB8707384D0 publication Critical patent/GB8707384D0/en
Publication of GB2189054A publication Critical patent/GB2189054A/en
Withdrawn legal-status Critical Current

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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F15FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
    • F15BSYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
    • F15B20/00Safety arrangements for fluid actuator systems; Applications of safety devices in fluid actuator systems; Emergency measures for fluid actuator systems
    • F15B20/004Fluid pressure supply failure

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Analytical Chemistry (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Servomotors (AREA)

Abstract

A servovalve comprising a spool 13 which is slidable within a normal range within a bore 12 in the valve body 11 in response to differential fluid pressure acting on the ends of the spool, means 25 to bias the spool to one end of the bore and electro-mechanical control means to control the position of the spool in the body and thereby provide a variable fluid output which is proportional to the electrical signal supplied to the control means, wherein in the event of a failure of supply of fluid pressure, the spool is urged by the bias means to a predetermined failure position beyond the normal range of the spool. <IMAGE>

Description

SPECIFICATION Servovalves This invention relates to servovalves and in particular those of the type known as flappernozzle servovalves.
Servovalves are known which comprise a valve body having a bore therein, at least one supply port to connect the bore to a source of pressurised fluid, at least one output port to connect the bore to pressure responsive actuator means, a spool having two distal end faces and being axially movable within the bore in response to differential fluid pressure acting on the distal end faces of the spool and electro-mechanical means to control the position of the spool within a normal range within the bore to provide a variable fluid output from the servovalve which is proportional to the electrical signal supplied to the electromechanical control means.
It is a disadvantage of such servovalves that, in the event of a fluid pressure failure, secondary means, for example a solenoid valve, are required to provide an immediate response to such a failure and provide for the pressure responsive actuator means to be disabled in a safe manner. The present invention is concerned with servovalves which are biassed so that, in the event of such failure, a secondary means, for example by-pass, can be performed by the valve itself.
In accordance with the invention, there is provided a servovalve comprising a body having a bore therein, at least one supply port for connecting the bore to a source of pressurised fluid, at least one output port for connecting the bore to a pressure responsive actuator means, a spool having two distal end faces and being axially movable within the bore in response to differential fluid pressure acting on the two distal end faces of the spool from the source of pressurised fluid, means to bias the spool towards one end of the bore and electro-mechanical control means to control the position of the spool within a normal range within the bore to provide a variable fluid output from the servovalve that is proportional to the electrical signal supplied to the electro-mechanical control means, wherein, in the event of a failue of supply of fluid pressure from the source, the spool is urged rapidly by the bias means to a predetermined failure position beyond the normal range of the spool.
The electro-mechanical control means is preferably a servo-motor driving a flapper for cooperation with one or other of a pair of nozzles. The flapper may also have attached thereto a resilient feedback member to engage a flange on the spool and thereby relay information regarding the spool position within the bore back to the control means.
Preferably the feedback member, conveniently with a part-spherical end, may be biassed against or within a spool flange when the spool is in the normal range. However, the engagement between the flapper and the spool must be such, for example a single flange on the spool, that the spool can be moved beyond its normal range.
The bias means may be either a spring acting, for example, on a distal end face of the spool or alternatively a mechancial offset of a servo-motor/flapper arrangement with regard to the longitudinal axis of the bore.
In the latter case in particular, the flapper may be physically offset towards one of the nozzles at least when there is no electrical signal supplied to the servo-motor.
The flapper may be physically offset in the direction to cause the spool to be moved by fluid pressure in the same direction as that in which it is urged by spring means in which case an electrical bias signal must be supplied to the servo-motor to move the flapper and thereby restore the spool to a position within the normal range of movement.
Alternatively, the flapper may be physically offset in the direction to cause the spool to be moved by fluid pressure against the action of the spring means in which case no electrical bias signal is required to bring the spool to a position within the normal range of movement.
To exemplify the invention, reference is now made to the accompanying drawings in which: Figure 1 is a schematic cross-section through a servovalve of the invention, Figure 2 is a schematic cross-section similar to Fig. 1 but showing a spool in a position beyond its normal range, Figure 3 is a simplified schematic cross-section through a further servovalve of the invention, and Figure 4 is a simplified schematic cross-section through another servovalve of the invention.
With reference to Figs. 1 and 2, the servovalve has a valve body 11 defining a bore 12 therein and a spool 13 slidable in the bore 12. The valve body 11 has a pair of inlet ports 14, 15 to connect the bore 12 in use to a source of pressurised fluid (not shown), three ports 16, 17, 18 to allow fluid to return to a reservoir (not shown) associated with the source of pressurised fluid and three supply ports 19, 20, 21 to connect the bore 12 in use to a pressure responsive actuator means 22.
The spool 13 has a pair of distal end faces 23, 24 against one of which a compression spring 25 acts to bias the spool 13 towards one end of the bore 12. The travel of the spool 13 in the bore 12 is limited by stop means 26 against which the other end face 24 of the spool 13 will abut.
The position of the spool 13 in the bore 12 is varied by altering the relative fluid pressures supplied to the two distal end faces 23, 24.
The fluid pressure is supplied from source of fluid at pressure to each of the end faces 23, 24 through respective control ports 27, 28, each of which has a restrictor 29, 30 fitted in it to reduce the flow of fluid and is connected to a nozzle 31, 32 forming part of an electromechanical control means.
The electro-mechanical control means further comprises an electric servo-motor 33, a flapper 34 for cooperation with the nozzles 31, 32 and a resilient feedback member 35 having a part-spherical end 36 for cooperation with one face of a flange 37 on the spool 13.
If desired, the servo-motor 33 can be tilted relative to the longitudinal axis of the bore 12 in the manner shown in Fig. 3 thereby bringing the flapper 34 closer to the nozzle 32 than to the nozzle 31 when no electrical signal is supplied to the servo-motor 33.
In using the servovalve, when no electrical power or fluid pressure is supplied the spool 13 is in the position shown in Fig. 2 due to the effect of the spring 25. However, in the case of the embodiment shown in Fig. 3, when fluid pressure is supplied to the servovalve, the spool 13 will remain against the end stop 26 because of the offset of the flapper 34 which increases the pressure supplied through the port 28 relative to the pressure supplied through the port 27. To bring the spool 13 back into the normal range it is necessary to apply an electrical bias signal to the servo-motor 33 to move the flapper 34 to a position in which the fluid pressure supplied to the port 27 balances the fluid pressure supplied to the port 28 plus the force generated by the spring 25.
Once this has been effected, operation of the servovalve is the same as with any other flapper-nozzle servovalve of this type, i.e. a small variation in the applied signal to the servo-motor 33 will produce a proportional variation in the fluid pressure output from the servovalve.
In the event of a loss of fluid pressure the spool 13 will be urged rapidly by the spring 25 to a predetermined failure position beyond the normal range of movement of the spool 13 (as shown in Fig. 2). In this failure position the feedback member 35 will become disengaged from the flange 37 and so all proportional contact is lost.
With the spool 13 in this failure position, the actuator means 22 is left in a floating condition, the supply ports 19 and 20 cooperating with the return ports 16 and 17.
Similarly, if there is a failure of the control signal supplied to the servo-motor 33 the flapper 34 will return to the position shown in Fig. 3 and the resulting increase in pressure in the control port 28 will drive spool member 13 to the left until it contacts the end stop 26. With the spool member 13 in this position the actuator means 22 is again left in a floating condition.
Irrespective of the mode of failure of the servovalve, therefore, the actuator means 22 is always rapidly restored to a safe condition.
In the embodiment shown in Fig. 4, the only significant difference of construction is that the servo-motor 33 is tilted in the opposite direction to that shown in Fig. 3, thereby bringing the flapper 34 towards the nozzle 31.
In using this serovalve, when no electrical power or fluid pressure is supplied to the servovalve the spool 13 takes up a position abutting the end stop 26 due to the effect of the spring 25. However, when a supply of fluid pressure is connected to the servovalve, the spool 13 will move to a normal position as the offset in the flapper 34 raises the fluid pressure in the port 27 sufficiently to balance the combined effect of the spring 25 and the pressure supplied to the port 28.
Standard servovalve operation then applies except that in the event of a fluid pressure failure the spool 13 will be driven to the left by the spring 25 until it contacts the end stop 26, in which position the actuator means 22 is left in a floating condition and the ports 19 and 20 cooperate with the ports 16 and 17.
The ports of servovalves of the invention can in general be designed so that, in a failed mode, the actuator means is locked by trapped fluid pressure in a predetermined position. Preferably, the ports will be designed so that, even if the supply of fluid pressure should fail in such a manner as to urge the spool member against the spring, the pressure responsive actuator means will be left in a floating or locked condition.
As an alternative to the embodiments described above, the displacement of the flapper towards one or other of the nozzles may be achieved by rectilinearly displacing the servomotor relative to the nozzles rather than tilting it. Equaliy, the displacement of the flapper towards one or other of the nozzles may be achieved by magnetically biassing the armature of the servo-motor.
The spool may also be moved into said failure position by means of a greater than normal electrical signal applied to the servo-motor to move the flapper in a direction to increase the fluid pressure to the right-hand side (as shown in the drawings) of the spool member.

Claims (6)

1. A servovalve comprising a body having a bore therein, at least one supply port for connecting the bore to a source of pressurised fluid, at least one output port for connecting the bore to a pressure responsive actuator means, a spool having two distal end faces and being axially movable within the bore in response to differential fluid pressure acting on the two distal end faces of the spool from the source of pressurised fluid, means to bias the spool towards one end of the bore and electro-mechanical means to control the position of the spool within a normal range within the bore to provide a variable fluid output from the servovalve that is proportional to the electrical signal supplied to the electro-mechanical control means, wherein, in the event of a failure of supply of fluid pressure from the source, the spool is urged rapidly by the bias means to a predetermined failure position beyond the normal range of the spool.
2. A servovalve according to claim 1 in which the electro-mechanical control means is a servo-motor driving a flapper for cooperation with one or other of a pair of nozzles.
3. A servovalve according to claim 1 or claim 2 in which the bias means is a spring acting on a distal end face of the spool.
4. A servovalve according to claim 1 or claim 2 in which the bias means is a mechanical offset of a servo-motor/flapper arrangement.
5. A servovalve according to any one of claims 2 to 4 in which the flapper has attached thereto a resilient feedback member to engage a flange on the spool.
6. A servovalve according to claim 1 substantially as herein described with reference to any one of Figs. 1 to 4 inclusive.
GB08707384A 1986-03-27 1987-03-27 Servovalves Withdrawn GB2189054A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB868607720A GB8607720D0 (en) 1986-03-27 1986-03-27 Servovalve

Publications (2)

Publication Number Publication Date
GB8707384D0 GB8707384D0 (en) 1987-04-29
GB2189054A true GB2189054A (en) 1987-10-14

Family

ID=10595381

Family Applications (2)

Application Number Title Priority Date Filing Date
GB868607720A Pending GB8607720D0 (en) 1986-03-27 1986-03-27 Servovalve
GB08707384A Withdrawn GB2189054A (en) 1986-03-27 1987-03-27 Servovalves

Family Applications Before (1)

Application Number Title Priority Date Filing Date
GB868607720A Pending GB8607720D0 (en) 1986-03-27 1986-03-27 Servovalve

Country Status (1)

Country Link
GB (2) GB8607720D0 (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2371846A (en) * 2000-12-19 2002-08-07 Snecma Moteurs A fail safe valve
FR2847641A1 (en) * 2002-11-25 2004-05-28 Snowstar S R L Control valve for snow gun has slide which is moved by spindle and nut system, 3-way electromagnetic valve acting as auxiliary operating system if spindle and nut system becomes inoperative
GB2432886A (en) * 1990-03-16 2007-06-06 Lucas Ind Plc Gas turbine engine reheat fuel control system and control valves therefor
US7413141B1 (en) 1989-05-10 2008-08-19 Goodrich Control Systems Limited Gas turbine engine fuel control system and regulating valves therefor

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1140221A (en) * 1965-01-21 1969-01-15 Weston Instruments Inc Improvements in or relating to fluid flow control
GB1401626A (en) * 1971-11-13 1975-07-16 Lucas Industries Ltd Electro hydraulic actuator arrangement
GB2002926A (en) * 1977-08-22 1979-02-28 Eaton Corp Control for a variable displacement pump or motor

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1140221A (en) * 1965-01-21 1969-01-15 Weston Instruments Inc Improvements in or relating to fluid flow control
GB1401626A (en) * 1971-11-13 1975-07-16 Lucas Industries Ltd Electro hydraulic actuator arrangement
GB2002926A (en) * 1977-08-22 1979-02-28 Eaton Corp Control for a variable displacement pump or motor

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7413141B1 (en) 1989-05-10 2008-08-19 Goodrich Control Systems Limited Gas turbine engine fuel control system and regulating valves therefor
GB2432886A (en) * 1990-03-16 2007-06-06 Lucas Ind Plc Gas turbine engine reheat fuel control system and control valves therefor
GB2432886B (en) * 1990-03-16 2007-12-05 Lucas Ind Plc Gas turbine engine fuel control system and regulating valve therefor
GB2371846A (en) * 2000-12-19 2002-08-07 Snecma Moteurs A fail safe valve
GB2371846B (en) * 2000-12-19 2004-08-11 Snecma Moteurs A fail-freeze servovalve
FR2847641A1 (en) * 2002-11-25 2004-05-28 Snowstar S R L Control valve for snow gun has slide which is moved by spindle and nut system, 3-way electromagnetic valve acting as auxiliary operating system if spindle and nut system becomes inoperative
WO2004051123A1 (en) * 2002-11-25 2004-06-17 Snowstar S.R.L. Slide control valve

Also Published As

Publication number Publication date
GB8607720D0 (en) 1986-04-30
GB8707384D0 (en) 1987-04-29

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WAP Application withdrawn, taken to be withdrawn or refused ** after publication under section 16(1)