WO1992002107A1 - Hydraulic lever actuator - Google Patents

Hydraulic lever actuator Download PDF

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Publication number
WO1992002107A1
WO1992002107A1 PCT/GB1991/001210 GB9101210W WO9202107A1 WO 1992002107 A1 WO1992002107 A1 WO 1992002107A1 GB 9101210 W GB9101210 W GB 9101210W WO 9202107 A1 WO9202107 A1 WO 9202107A1
Authority
WO
WIPO (PCT)
Prior art keywords
piston
hydraulic lever
electromagnetic actuator
hydraulic
actuator according
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.)
Ceased
Application number
PCT/GB1991/001210
Other languages
French (fr)
Inventor
Owen Jones
Michael Charles John Trinder
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.)
Active Noise and Vibration Technologies Inc
Original Assignee
Active Noise and Vibration Technologies Inc
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 Active Noise and Vibration Technologies Inc filed Critical Active Noise and Vibration Technologies Inc
Priority to EP91913607A priority Critical patent/EP0542784B1/en
Priority to US07/969,272 priority patent/US5676353A/en
Priority to DE69120079T priority patent/DE69120079T2/en
Publication of WO1992002107A1 publication Critical patent/WO1992002107A1/en
Anticipated expiration legal-status Critical
Ceased legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B60VEHICLES IN GENERAL
    • B60KARRANGEMENT OR MOUNTING OF PROPULSION UNITS OR OF TRANSMISSIONS IN VEHICLES; ARRANGEMENT OR MOUNTING OF PLURAL DIVERSE PRIME-MOVERS IN VEHICLES; AUXILIARY DRIVES FOR VEHICLES; INSTRUMENTATION OR DASHBOARDS FOR VEHICLES; ARRANGEMENTS IN CONNECTION WITH COOLING, AIR INTAKE, GAS EXHAUST OR FUEL SUPPLY OF PROPULSION UNITS IN VEHICLES
    • B60K5/00Arrangement or mounting of internal-combustion or jet-propulsion units
    • B60K5/12Arrangement of engine supports
    • B60K5/1283Adjustable supports, e.g. the mounting or the characteristics being adjustable
    • 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
    • F15B7/00Systems in which the movement produced is definitely related to the output of a volumetric pump; Telemotors
    • F15B7/005With rotary or crank input
    • 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
    • F16FSPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
    • F16F15/00Suppression of vibrations in systems; Means or arrangements for avoiding or reducing out-of-balance forces, e.g. due to motion
    • F16F15/02Suppression of vibrations of non-rotating, e.g. reciprocating systems; Suppression of vibrations of rotating systems by use of members not moving with the rotating systems
    • F16F15/023Suppression of vibrations of non-rotating, e.g. reciprocating systems; Suppression of vibrations of rotating systems by use of members not moving with the rotating systems using fluid means
    • 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
    • F16FSPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
    • F16F15/00Suppression of vibrations in systems; Means or arrangements for avoiding or reducing out-of-balance forces, e.g. due to motion
    • F16F15/02Suppression of vibrations of non-rotating, e.g. reciprocating systems; Suppression of vibrations of rotating systems by use of members not moving with the rotating systems
    • F16F15/023Suppression of vibrations of non-rotating, e.g. reciprocating systems; Suppression of vibrations of rotating systems by use of members not moving with the rotating systems using fluid means
    • F16F15/027Suppression of vibrations of non-rotating, e.g. reciprocating systems; Suppression of vibrations of rotating systems by use of members not moving with the rotating systems using fluid means comprising control arrangements
    • 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
    • F16FSPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
    • F16F15/00Suppression of vibrations in systems; Means or arrangements for avoiding or reducing out-of-balance forces, e.g. due to motion
    • F16F15/02Suppression of vibrations of non-rotating, e.g. reciprocating systems; Suppression of vibrations of rotating systems by use of members not moving with the rotating systems
    • F16F15/03Suppression of vibrations of non-rotating, e.g. reciprocating systems; Suppression of vibrations of rotating systems by use of members not moving with the rotating systems using magnetic or electromagnetic means
    • HELECTRICITY
    • H04ELECTRIC COMMUNICATION TECHNIQUE
    • H04RLOUDSPEAKERS, MICROPHONES, GRAMOPHONE PICK-UPS OR LIKE ACOUSTIC ELECTROMECHANICAL TRANSDUCERS; ELECTRIC HEARING AIDS; PUBLIC ADDRESS SYSTEMS
    • H04R1/00Details of transducers, loudspeakers or microphones
    • H04R1/42Combinations of transducers with fluid-pressure or other non-electrical amplifying means

Definitions

  • the present Invention relates to an improved electromagnetic actuator for use in vibration cancellation systems.
  • actuators are of the moving-iron type, wherein a magnetic field is produced which interacts with a metal armature to generate a force thereon. The armature then moves under the influence of the generated force.
  • a disadvantage of these actuators is that the force generated is non-linear with respect to armature displacement. It is, therefore, an object of the present invention to provide an actuator having more linear characteristics than moving-iron type actuators by employing either a constant or variable volume hydraulic lever.
  • an electromagnetic actuator comprising a moving-coil electrical signal-to-displacement transducer and a hydraulic lever wherein the hydraulic lever transforms the transducer output.
  • an electromagnetic actuator comprising a rotary electric motor and a hydraulic lever wherein the hydraulic lever transforms the motor output.
  • the motor drives an Archimedean screw in order to transfer hydraulic fluid between a hydraulic fluid reservoir and a hydraulic lever working chamber.
  • Archimedean screw in order to transfer hydraulic fluid between a hydraulic fluid reservoir and a hydraulic lever working chamber.
  • two counter-rotating Archimedean screws may be used in order to balance out stator rotational reaction forces.
  • the actuator according to the present invention may be employed as an engine mounting as part of a vibration cancellation system.
  • Figure 1 shows an actuator according to the first aspect of the present invention
  • Figure 2 shows a single screw version of an actuator according to the second aspect of the present invention
  • Figure 3 shows a double screw actuator according to the second aspect of the present invention
  • Figure 4 shows an active vibration control system applied to an internal combustion engine.
  • an actuator 1 includes a body 2, formed from an annular permanent magnet 3 having first and second axial extremities 3a,3b, a disc-shaped first end-piece 4 and a dish-shaped second end-piece 5.
  • the first end-piece has a diameter substantially the same as the outer diameter of the magnet 3 and is affixed coaxially across the first axial extremity 3a thereof.
  • the second end-piece 5 has the same diameter as the first end-piece 4 and is similarly affixed across the second axial extremity 3b of the magnet 3 with its wall portion 5a extending away from the magnet 3.
  • the second end-piece 5 is provided with an aperture 6 in the centre of its planar portion.
  • a column 7 extends coaxially from the centre of the first end-piece 4 in the direction of the second end-piece 5, passes through the aperture 6 therein.
  • a first piston 8, comprising a tube having a closed end, supports an energisable coil 9 wound about the tubular portion adjacent the closed end thereof.
  • the first piston 8 is mounted for axial movement relative to the column 7 and is supported by a pair of spiders 10, 11 extending radially inwardly from the inner wall of the magnet 3 such that a portion of the coil 9 is within the aperture 6.
  • a chamber 12 is defined by the outwardly facing planar surface and the inner surface of the wall portion of the second end-piece 5, and the equivalent surfaces of a dish-shaped second piston 13, coaxially located within the second end-piece 5.
  • An annular sealing member 14 is provided between the outer surface of the wall portion of the second piston 13 and the inner surface of the wall portion of the second end-piece 5. The sealing member 14 ensures a fluid-tight seal between the second piston 13 and the second end-portion 5.
  • the inner surface of the wall portion of the second end-piece 5 and the outer surface of the wall portion of the second piston 13 cooperate to relieve pressure from the sealing member 14 so as to provide a reliable seal.
  • the actuator 1 is provided with a quantity of hydraulic fluid 15 which occupies the chamber 12 and a portion of an airtight-sealed space 16 within the magnet 3.
  • the space 16 within the magnet 3 communicates with the chamber 12 by means of the restricted gap in aperture 6 between the coil 9 and the second pole piece.
  • a pair of threaded studs 17, 18 extend axially outwardly from the first end-piece 4 and the second piston 13 repectively for mounting the actuator between a support and a load.
  • the first piston 8 is required to have a long travel relative to the travel of the second piston 13 and it might be thought that a fluid tight sliding member would be required for the piston 8 in order to seal the chamber 12.
  • the aperture 6 is provided between the coil 9 and the second end piece 5. At low frequencies fluid from the chamber 12 can flow through the aperture 6 to the chamber 15 and vice versa, but at high frequencies the small aperture 6 prevents rapid fluid flow, thus effectively sealing chamber 12 and allowing force to be transmitted to the piston 13.
  • the construction also prevents the static loading of the actuator displacing the coil 9 away from its central quiescent position (shown in the drawing).
  • the sealed air chamber 16 and the resulting air-gap between the column 7 and the piston 8 means that upon movement of the piston, no hydraulic fluid has to be forced thereby from between the column 7 and piston 8, which would otherwise impede high frequency movement of the piston. Furthermore, the immersion of the coil 9 in the hydraulic fluid 15 leads to improved cooling of the coil.
  • the actuator shown in Figure 1 will function in the orientation shown. However, if the actuator 1 is to be used angled or inverted, a high compliance membrane will be required, fixed between the inner wall of the magnet 3 and the first piston 8, such that it retains the hydraulic fluid substantially as shown in Figure 1 at all orientations of the actuator 1.
  • an actuator 20 comprises a cylindrical body 21 having first and second axial extremities 21a, 21b.
  • a rotary electric motor 23 is mounted in a motor chamber 22, defined within the body 21 adjacent the first axial extremity thereof.
  • a reservoir chamber 24, for storing hydraulic fluid, is located within the body 21 adjacent the motor chamber 22, from which it is separated by a wall 25.
  • the wall 25 has a centrally located aperture 25a through which the shaft 27 of the motor 23 passes.
  • a fluid tight seal 26 is formed between the shaft 27 and the wall 25.
  • a resiliently flexible annular membrane 28 is located within the reservoir chamber 24, its outer margin being sealingly fixed to the wall 25, where it meets the body 21, and its inner margin being sealingly attached to the shaft seal 26.
  • a working chamber 29 is defined by a cylindrical recess extending into the body 21 from the second axial extremity 21b thereof and a piston 30, arranged to travel a small distance into and out of the cylindrical recess.
  • a sealing member 31 is located between the periphery of the piston 30 and the radial wall of the cylindrical recess.
  • the working chamber 29 is connected to the reservoir chamber 24 by a passageway 32.
  • the shaft 27 of the motor 23 extends through the length of the passageway 32 wherein it supports an Archimedean screw 33.
  • control signals are supplied to the motor 23 causing it to rotate.
  • the rotation of the motor 23 drives the Archimedean screw 33, either causing hydraulic fluid to be transferred from the reservoir chamber 24 to the working chamber 29 or vice versa.
  • the piston 30 is caused to moved out of and into the cylindrical recess in sympathy with the changing volume of hydraulic fluid within the working chamber 29.
  • the annular membrane 28 flexes into and out of the reservoir chamber 24 as the volume of hydraulic fluid therein changes. This arrangement allows a relatively low torque motor to produce high forces on the piston with moderate displacements.
  • a working chamber 34 is provided with two opposed Archimedean screw feeds 36, 37 arranged with their axes normal to the direction of travel of the piston 35.
  • the frequency response of the actuator may be tailored to suit a particular application.
  • the function of the member 28 is performed by a compressible air-filled bag located in the reservoir chamber 24.
  • Actuators according to the present invention may be employed as part of a vibration cancellation systems, for example, for an i.e. engine in a vehicle.
  • the actuator serving as an engine mount.
  • a sensor 40 detects vibrations din a vehicle body caused by an engine 41 and an electronic control circuit 42 produces an actuator energising current in response thereto which drives an actuator 43. High frequency vibrations are thereby cancelled.
  • the structure of the actuators of the present invention means that low frequency force changes e.g. those due to cornering, do not propagate through the actuator.

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Mechanical Engineering (AREA)
  • Acoustics & Sound (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Signal Processing (AREA)
  • Fluid Mechanics (AREA)
  • Combustion & Propulsion (AREA)
  • Transportation (AREA)
  • Electromagnetism (AREA)
  • Combined Devices Of Dampers And Springs (AREA)
  • Actuator (AREA)
  • Supply Devices, Intensifiers, Converters, And Telemotors (AREA)
  • Vibration Prevention Devices (AREA)
  • Reciprocating, Oscillating Or Vibrating Motors (AREA)

Abstract

An actuator having a linear current force characteristic comprises a moving coil transducer and a hydraulic lever. The moving coil (9) is capable of producing only a relatively low force but with a relatively large displacement. The coil (9) is formed on a piston (8) which acts as an input piston to a hydraulic lever. An output piston (13) has a much larger area than the input piston (8). Thus, the long throw, low force input to the hydraulic lever is converted into a short throw, high force output at the second piston (13).

Description

HYDRAULIC LEVER ACTUATOR
DESCRIPTION
The present Invention relates to an improved electromagnetic actuator for use in vibration cancellation systems.
It has been proposed to cancel vibrations in a mechanical system by sensing the vibrations and utilising an electronic control circuit to drive a mechanical actuator in order to apply vibrations to the system which tend to cancel out the original source of vibration. For example, it has been proposed to use a mechanical actuator in association with an engine mount for an internal combustion engine to apply cancelling vibrations to the engine for producing smooth running.
Known actuators are of the moving-iron type, wherein a magnetic field is produced which interacts with a metal armature to generate a force thereon. The armature then moves under the influence of the generated force. A disadvantage of these actuators is that the force generated is non-linear with respect to armature displacement. It is, therefore, an object of the present invention to provide an actuator having more linear characteristics than moving-iron type actuators by employing either a constant or variable volume hydraulic lever.
According to a first aspect the present invention there is provided an electromagnetic actuator comprising a moving-coil electrical signal-to-displacement transducer and a hydraulic lever wherein the hydraulic lever transforms the transducer output.
According to a second aspect of the present invention there is provided an electromagnetic actuator comprising a rotary electric motor and a hydraulic lever wherein the hydraulic lever transforms the motor output. Preferably, the motor drives an Archimedean screw in order to transfer hydraulic fluid between a hydraulic fluid reservoir and a hydraulic lever working chamber. However, other forms of reversible rotary pump may usefully be employed. Advantageously, two counter-rotating Archimedean screws may be used in order to balance out stator rotational reaction forces.
Conveniently, the actuator according to the present invention may be employed as an engine mounting as part of a vibration cancellation system.
Embodiments of the present invention will now be described, by way of example, with reference to the accompanying drawings, in which:
Figure 1 shows an actuator according to the first aspect of the present invention;
Figure 2 shows a single screw version of an actuator according to the second aspect of the present invention;
Figure 3 shows a double screw actuator according to the second aspect of the present invention; and Figure 4 shows an active vibration control system applied to an internal combustion engine.
Referring to the Figure 1, an actuator 1 includes a body 2, formed from an annular permanent magnet 3 having first and second axial extremities 3a,3b, a disc-shaped first end-piece 4 and a dish-shaped second end-piece 5. The first end-piece has a diameter substantially the same as the outer diameter of the magnet 3 and is affixed coaxially across the first axial extremity 3a thereof. The second end-piece 5 has the same diameter as the first end-piece 4 and is similarly affixed across the second axial extremity 3b of the magnet 3 with its wall portion 5a extending away from the magnet 3.
The second end-piece 5 is provided with an aperture 6 in the centre of its planar portion. A column 7 extends coaxially from the centre of the first end-piece 4 in the direction of the second end-piece 5, passes through the aperture 6 therein. A first piston 8, comprising a tube having a closed end, supports an energisable coil 9 wound about the tubular portion adjacent the closed end thereof. The first piston 8 is mounted for axial movement relative to the column 7 and is supported by a pair of spiders 10, 11 extending radially inwardly from the inner wall of the magnet 3 such that a portion of the coil 9 is within the aperture 6.
A chamber 12 is defined by the outwardly facing planar surface and the inner surface of the wall portion of the second end-piece 5, and the equivalent surfaces of a dish-shaped second piston 13, coaxially located within the second end-piece 5. An annular sealing member 14 is provided between the outer surface of the wall portion of the second piston 13 and the inner surface of the wall portion of the second end-piece 5. The sealing member 14 ensures a fluid-tight seal between the second piston 13 and the second end-portion 5. The inner surface of the wall portion of the second end-piece 5 and the outer surface of the wall portion of the second piston 13 cooperate to relieve pressure from the sealing member 14 so as to provide a reliable seal.
The actuator 1 is provided with a quantity of hydraulic fluid 15 which occupies the chamber 12 and a portion of an airtight-sealed space 16 within the magnet 3. The space 16 within the magnet 3 communicates with the chamber 12 by means of the restricted gap in aperture 6 between the coil 9 and the second pole piece.
A pair of threaded studs 17, 18 extend axially outwardly from the first end-piece 4 and the second piston 13 repectively for mounting the actuator between a support and a load.
The operation of the actuator will now be described. When the coil 9 is energised a magnetic field is generated within the body portion 2 which interacts with magnetic field produced by the magnet 3. As a result of this interaction a force is generated on the coil 9 which moves it axially thus moving the first piston 8 into or out of the chamber 12. The movement of the first piston 8 is transfered to the piston 13 by means of the hydraulic fluid in the chamber 12. Since the area of the piston 13 is greater than that of the first piston 8, the piston 13 moves axially a smaller distance than the first piston 8 but exerts a greater force, and thus the arrangement acts as an hydraulic lever.
The first piston 8 is required to have a long travel relative to the travel of the second piston 13 and it might be thought that a fluid tight sliding member would be required for the piston 8 in order to seal the chamber 12. However, in this example of the invention the aperture 6 is provided between the coil 9 and the second end piece 5. At low frequencies fluid from the chamber 12 can flow through the aperture 6 to the chamber 15 and vice versa, but at high frequencies the small aperture 6 prevents rapid fluid flow, thus effectively sealing chamber 12 and allowing force to be transmitted to the piston 13. The construction also prevents the static loading of the actuator displacing the coil 9 away from its central quiescent position (shown in the drawing). The sealed air chamber 16 and the resulting air-gap between the column 7 and the piston 8 means that upon movement of the piston, no hydraulic fluid has to be forced thereby from between the column 7 and piston 8, which would otherwise impede high frequency movement of the piston. Furthermore, the immersion of the coil 9 in the hydraulic fluid 15 leads to improved cooling of the coil.
The actuator shown in Figure 1 will function in the orientation shown. However, if the actuator 1 is to be used angled or inverted, a high compliance membrane will be required, fixed between the inner wall of the magnet 3 and the first piston 8, such that it retains the hydraulic fluid substantially as shown in Figure 1 at all orientations of the actuator 1.
The actuator 1 has the advantage that the moving coil device has a linear current force characteristic. The hydraulic lever transforms the low force, long throw output of the moving coil device into a higher force over a shorter throw, which is particularly suited for use in vibration cancellation systems. Referring to Figure 2, an actuator 20 comprises a cylindrical body 21 having first and second axial extremities 21a, 21b. A rotary electric motor 23 is mounted in a motor chamber 22, defined within the body 21 adjacent the first axial extremity thereof. A reservoir chamber 24, for storing hydraulic fluid, is located within the body 21 adjacent the motor chamber 22, from which it is separated by a wall 25. The wall 25 has a centrally located aperture 25a through which the shaft 27 of the motor 23 passes. A fluid tight seal 26 is formed between the shaft 27 and the wall 25.
A resiliently flexible annular membrane 28 is located within the reservoir chamber 24, its outer margin being sealingly fixed to the wall 25, where it meets the body 21, and its inner margin being sealingly attached to the shaft seal 26.
A working chamber 29 is defined by a cylindrical recess extending into the body 21 from the second axial extremity 21b thereof and a piston 30, arranged to travel a small distance into and out of the cylindrical recess. A sealing member 31 is located between the periphery of the piston 30 and the radial wall of the cylindrical recess.
The working chamber 29 is connected to the reservoir chamber 24 by a passageway 32. The shaft 27 of the motor 23 extends through the length of the passageway 32 wherein it supports an Archimedean screw 33.
In operation, control signals are supplied to the motor 23 causing it to rotate. The rotation of the motor 23 drives the Archimedean screw 33, either causing hydraulic fluid to be transferred from the reservoir chamber 24 to the working chamber 29 or vice versa. As hydraulic fluid is pumped into and out of the working chamber 29 the piston 30 is caused to moved out of and into the cylindrical recess in sympathy with the changing volume of hydraulic fluid within the working chamber 29. The annular membrane 28 flexes into and out of the reservoir chamber 24 as the volume of hydraulic fluid therein changes. This arrangement allows a relatively low torque motor to produce high forces on the piston with moderate displacements. Furthermore, the return path for the hydraulic fluid through the screw thread, between the working chamber 29 and the reservoir chamber 24, limits the static pressure that can be generated on the piston 30. However, with rapidly changing forces, the mass of hydraulic fluid within the screw thread presents an impediment to the motion of the hydraulic fluid thus effectively closing it to high frequency pressure changes. Likewise, static forces acting on the piston 30 will not cause rotation of the motor armature. This makes the actuator particularly suitable for use in active engine mounts where it is necessary for the system to ignore the slowly changing forces associated with cornering etc. of a vehicle.
Should rotational reaction forces on the motor stator be undesirable, they may be balanced out by using two counter-rotating Archimedean screws 32, 33, as shown in Figure 3. In Figure 3, a working chamber 34 is provided with two opposed Archimedean screw feeds 36, 37 arranged with their axes normal to the direction of travel of the piston 35.
By proper design of the Archimedean screws the frequency response of the actuator may be tailored to suit a particular application.
In an alternative embodiment, the function of the member 28 is performed by a compressible air-filled bag located in the reservoir chamber 24.
Actuators according to the present invention may be employed as part of a vibration cancellation systems, for example, for an i.e. engine in a vehicle. The actuator serving as an engine mount. Referring to Figure 4, a sensor 40 detects vibrations din a vehicle body caused by an engine 41 and an electronic control circuit 42 produces an actuator energising current in response thereto which drives an actuator 43. High frequency vibrations are thereby cancelled. However, the structure of the actuators of the present invention means that low frequency force changes e.g. those due to cornering, do not propagate through the actuator.

Claims

1. An electromagnetic actuator comprising an electrical signal-to-displacement transducer and a hydraulic lever wherein the hydraulic lever transforms the transducer output.
2. An electromagnetic actuator according to claim 1, wherein the hydraulic lever comprises first piston means, for transmitting an input displacement, second piston means, for transmitting an output displacement, and a fluid filled chamber therebetween.
3. An electromagnetic actuator according to claim 1 or 2 wherein the transducer is a moving coil transducer.
4. An electromagnetic actuator according to claim 3, wherein the coil of said displacement transducer is mounted on said first piston means.
5. An electromagnetic actuator according to any preceding claim, wherein a chamber is substantially defined by and within said displacement transducer, said chamber serving as a reservoir for hydraulic fluid for the hydraulic lever.
6. An electromagnetic actuator comprising a rotary electric motor and a hydraulic lever wherein the hydraulic lever transforms the motor output.
7. An electromagnetic actuator according to claim 6 wherein the motor drives an Archimedean screw such that hydraulic fluid is transferred between a hydraulic fluid reservoir emd a hydraulic lever working chamber.
8. An electromagnetic actuator according to claim 7 comprising two counter-rotating Archimedean screws.
9. An active vibration cancellation system including an actuator according to any preceding claim.
10. An active vibration cancellation system according to claim 9 wherein the actuator acts as an engine mounting.
PCT/GB1991/001210 1990-07-20 1991-07-19 Hydraulic lever actuator Ceased WO1992002107A1 (en)

Priority Applications (3)

Application Number Priority Date Filing Date Title
EP91913607A EP0542784B1 (en) 1990-07-20 1991-07-19 Hydraulic lever actuator
US07/969,272 US5676353A (en) 1990-07-20 1991-07-19 Hydraulic lever actuator
DE69120079T DE69120079T2 (en) 1990-07-20 1991-07-19 ACTUATOR WITH HYDRAULIC LEVER

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB9015984.9 1990-07-20
GB909015984A GB9015984D0 (en) 1990-07-20 1990-07-20 Hydraulic lever actuator

Publications (1)

Publication Number Publication Date
WO1992002107A1 true WO1992002107A1 (en) 1992-02-06

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Family Applications (1)

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PCT/GB1991/001210 Ceased WO1992002107A1 (en) 1990-07-20 1991-07-19 Hydraulic lever actuator

Country Status (8)

Country Link
US (1) US5676353A (en)
EP (1) EP0542784B1 (en)
JP (1) JP3280964B2 (en)
AU (1) AU8232591A (en)
DE (1) DE69120079T2 (en)
ES (1) ES2088010T3 (en)
GB (1) GB9015984D0 (en)
WO (1) WO1992002107A1 (en)

Cited By (4)

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Publication number Priority date Publication date Assignee Title
EP0537927A1 (en) * 1991-10-15 1993-04-21 Lord Corporation Fluid mount with active vibration control
FR2703121A1 (en) * 1993-03-25 1994-09-30 Bertin & Cie Anti-vibration device for supporting a vibrating mass
WO1998045615A1 (en) * 1997-04-08 1998-10-15 Lord Corporation Active fluid mounting
WO1998049461A1 (en) * 1997-04-26 1998-11-05 Bayer Aktiengesellschaft Adjustment and damping device

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US5732143A (en) 1992-10-29 1998-03-24 Andrea Electronics Corp. Noise cancellation apparatus
US6363345B1 (en) 1999-02-18 2002-03-26 Andrea Electronics Corporation System, method and apparatus for cancelling noise
US6594367B1 (en) 1999-10-25 2003-07-15 Andrea Electronics Corporation Super directional beamforming design and implementation
JP2006057750A (en) * 2004-08-20 2006-03-02 Honda Motor Co Ltd Actuator drive controller

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US3456755A (en) * 1963-07-29 1969-07-22 John Walker Hydraulic loudspeakers
DE2210608A1 (en) * 1971-03-15 1972-09-28 G B Boucherie Nv Device for the step-by-step conveyance of machine parts, workpieces, tools and the like

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Publication number Priority date Publication date Assignee Title
FR714339A (en) * 1930-07-16 1931-11-12 Device for the transformation of mechanical vibrations into electrical vibrations and vice versa
US3456755A (en) * 1963-07-29 1969-07-22 John Walker Hydraulic loudspeakers
DE2210608A1 (en) * 1971-03-15 1972-09-28 G B Boucherie Nv Device for the step-by-step conveyance of machine parts, workpieces, tools and the like

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Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0537927A1 (en) * 1991-10-15 1993-04-21 Lord Corporation Fluid mount with active vibration control
FR2703121A1 (en) * 1993-03-25 1994-09-30 Bertin & Cie Anti-vibration device for supporting a vibrating mass
WO1998045615A1 (en) * 1997-04-08 1998-10-15 Lord Corporation Active fluid mounting
US5957440A (en) * 1997-04-08 1999-09-28 Lord Corporation Active fluid mounting
WO1998049461A1 (en) * 1997-04-26 1998-11-05 Bayer Aktiengesellschaft Adjustment and damping device
US6463736B1 (en) 1997-04-26 2002-10-15 Bayer Aktiengesellschaft Adjustment and damping device

Also Published As

Publication number Publication date
US5676353A (en) 1997-10-14
DE69120079D1 (en) 1996-07-11
AU8232591A (en) 1992-02-18
JPH06500848A (en) 1994-01-27
EP0542784B1 (en) 1996-06-05
GB9015984D0 (en) 1990-09-05
JP3280964B2 (en) 2002-05-13
EP0542784A1 (en) 1993-05-26
DE69120079T2 (en) 1997-01-23
ES2088010T3 (en) 1996-08-01

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