GB2222657A - Active control of vibration - Google Patents

Active control of vibration Download PDF

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Publication number
GB2222657A
GB2222657A GB8913273A GB8913273A GB2222657A GB 2222657 A GB2222657 A GB 2222657A GB 8913273 A GB8913273 A GB 8913273A GB 8913273 A GB8913273 A GB 8913273A GB 2222657 A GB2222657 A GB 2222657A
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GB
United Kingdom
Prior art keywords
actuators
intermediate body
vibration mount
vibration
actuator
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
GB8913273A
Other versions
GB2222657B (en
GB8913273D0 (en
Inventor
Sean George Sutcliffe
Graham Paul Eatwell
Stephen Mark Hutchins
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.)
Topexpress Ltd
Original Assignee
Topexpress 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
Priority claimed from GB888821214A external-priority patent/GB8821214D0/en
Priority claimed from GB898906068A external-priority patent/GB8906068D0/en
Application filed by Topexpress Ltd filed Critical Topexpress Ltd
Publication of GB8913273D0 publication Critical patent/GB8913273D0/en
Publication of GB2222657A publication Critical patent/GB2222657A/en
Priority claimed from US07/493,410 external-priority patent/US5052529A/en
Application granted granted Critical
Publication of GB2222657B publication Critical patent/GB2222657B/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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Classifications

    • 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
    • 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
    • F16F15/005Suppression of vibrations in systems; Means or arrangements for avoiding or reducing out-of-balance forces, e.g. due to motion using electro- or magnetostrictive actuation means
    • GPHYSICS
    • G05CONTROLLING; REGULATING
    • G05DSYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D19/00Control of mechanical oscillations, e.g. of amplitude, of frequency, of phase
    • G05D19/02Control of mechanical oscillations, e.g. of amplitude, of frequency, of phase characterised by the use of electric means
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B60VEHICLES IN GENERAL
    • B60GVEHICLE SUSPENSION ARRANGEMENTS
    • B60G2401/00Indexing codes relating to the type of sensors based on the principle of their operation
    • B60G2401/10Piezoelectric elements
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B60VEHICLES IN GENERAL
    • B60GVEHICLE SUSPENSION ARRANGEMENTS
    • B60G2401/00Indexing codes relating to the type of sensors based on the principle of their operation
    • B60G2401/12Strain gauge
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B60VEHICLES IN GENERAL
    • B60GVEHICLE SUSPENSION ARRANGEMENTS
    • B60G2600/00Indexing codes relating to particular elements, systems or processes used on suspension systems or suspension control systems
    • B60G2600/22Magnetic elements

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  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Acoustics & Sound (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • General Physics & Mathematics (AREA)
  • Automation & Control Theory (AREA)
  • Vibration Prevention Devices (AREA)

Abstract

A subject body (10) is mounted on a support (12) by means of an intermediate body (16), and constrictive actuators (22, 24, 26) each of whose dimensions can be changed in a controllable manner by signals supplied from a computer receiving information from sensors on the intermediate body, applies controlled compensating forces to the intermediate body to reduce its vibrations. The actuators are preferably of magnetostrictive or piezoelectric type. <IMAGE>

Description

Title: Active Control of Vibration Field of the Invention This invention relates to the active control of vibration.
Background to the Invention When a vibrating body is mounted on a support body, it is often desired to control or minimise the transmission of vibration from the vibrating body to the support body. It is known to reduce the transmission of vibration passively by providing vibration isolators of various forms between the two bodies. It is also known to reduce vibration actively, often in conjunction with the use of passive isolators.
In copending International Patent Application No PCT/GB87/00902 there is described an arrangement for active vibration control in which an intermediate body is mounted between the vibrating body and the support body.
The vibration of the intermediate body is sensed and in response thereto controlling forces are applied to the intermediate body by inertial shakers mounted thereon to minimise the vibrations induced by the vibrating body.
Whilst such a vibration mount operates satisfactorily, it has been found that for some applications such a mount may be undesirably large and/or heavy.
Summary of the Invention According to the present invention there is provided a method of active vibration control in which a subject body, being a vibrating body or a body to be isolated from external vibrations, is mounted on a support by a vibration mount which includes an intermediate body between the subject body and the support, wherein the vibration imparted to the intermediate body is reduced by applying controlled compensating forces to the intermediate body by means of at least one constrictive actuator.
The invention also extends to such a vibration mount by means of which a subject body is mounted on a support and which includes an intermediate body between the subject body and the support, wherein at least one constrictive actuator is provided for applying controlled compensating forces to the intermediate body, so as to reduce vibration of the intermediate body, over at least a part of the frequency range for which control of vibrations is required.
By the term "constrictive actuator" as used herein is meant an acutator whose dimensions can be changed in a controllable way. Examples of constrictive actuators are electrodynamic, piezoelectric, hydraulic and magnetrostrictive actuators. In each case the constrictive actuator acts to increase or decrease its dimensions in response to a control signal, which in this case is typically derived from a sensor on the intermediate body.
The intermediate body is preferably a substantially rigid member over the frequency range of vibrations to be controlled.
Where the subject body is a vibrating body to be isolated from the support, the or each constrictive actuator is mounted between the vibrating body and the intermediate body. Alternatively in the case where, for example, sensitive equipment is to be isolated from a vibrating support, the or each actuator may be mounted between the intermediate body and the support.
By having the or each actuator thus mainly supported either by the subject body or the support, so the weight of the intermediate body is kept to a minimum in contrast to that of the inertial shakers disclosed in the above mentioned PCT application.
Typically the actuator is controlled by a computer.
A passive resilient element may be provided between the intermediate body and the subject body where the latter is vibrating, and/or between the intermediate body and the support where the latter is vibrating, so that where the intermediate body is not sufficiently rigid to prevent the passage of high frequency vibrations, or the computer which controls the or each actuator has restricted processing capabilities and cannot respond to these high frequencies, the resilient element is able to absorb such vibrations.
Where the intermediate member has up to six degrees of freedom an appropriate plurality of constrictive actuators are preferably arranged to control the relatively low frequency vibrations over all six degrees of freedom of movement of the intermediate member. Where the vibration of the intermediate member only occurs along three linear orthogonal axes (ie without rotational vibrations) then a correspondingly smaller number of actuators are required.
As the or each actuator will generally be required to take also the static load of the vibrating body, eg the weight of machinery mounted on the vibration mount, it is preferred for the or each actuator to be piezoelectric or magnetostrictive, as the design constraints imposed upon such actuators to permit them to support high static loads are less severe than for other actuators.
Alternatively, exceptionally large static loads may be supported on a passive element (eg a compliant or resilient element) in parallel with the or each actuator.
This has the added advantage that the total number and/or size of actuators may be reduced.
The recent development of rare earth alloys (for example the alloy Tb 0.27 Dy 0.73 Fe 1.95) which display large magnetostrictive strain constants, suggests that magnetostrictive actuators are particularly suited where large vibrational displacements must be accommodated.
Magnetostrictive actuators require a bias magnetic field which may be supplied by a permanent magnet or by a direct current in a surrounding coil (or both), while the fluctuating magnetic field required may be supplied by an alternating current in a coil which, if a coil is employed to produce the bias field, may be the same coil.
Where the actuators have to be prestressed this may be achieved by prestressing bolts, having due regard to the static load to be supported.
Where the subject body is to be free to vibrate, the intermediate body conveniently may be surrounded by a generally cup shaped member and be connected thereto by a plurality of constrictive actuators. Where the cup shaped member is prestressed by bolts extending therethrough and through the intermediate body, clearance holes may be provided in the intermediate body to avoid direct contact between it and the bolts.
The intermediate body may be substantially flat and rectangular in shape, and a pair of actuators may then be disposed at each side, and two pairs of actuators may be provided respectively above and below.
Alternatively, instead of having the actuators thus arranged in opposed pairs, one of each such actuators in an opposed pair may be replaced by a passive element, thus halving the number of actuators required. Preferably such passive elements are arranged at the upper or static load bearing side of the intermediate body, thereby reducing the size of the opposite actuator.
Alternatively, a simpler form may be adopted if constrictive actuators capable of deforming in shear in response to a control signal are used. For example, the piezoelectric material lead zirconate titanate, also known as PZT, is capable of this. In this case, a minimum of three compound actuators may be provided above the intermediate body. Each compound actuator is to comprise a stack of three constrictive actuators. One of these is to be capable of deforming in shear in a direction normal to the axis of the stack in response to a control signal; another is to be capable of deforming in extension or compression parallel to the axis of the stack. Thus the top of each stack may be caused to move in any direction relative to the intermediate body to which it is fixed at its base.The subject body may then be supported on the tops of the three or more compound actuators; this may conveniently be done via a cap plate resting on the compound actuators but not fixed rigidly to them.
Where the subject body comprises, for example, one or more machines mounted on a rectangular raft or table, a mount constructed in accordance with the invention may be provided at each corner thereof.
A vibration mount in accordance with the invention operates to keep the intermediate body substantially stationary, or to allow very limited (eg very low frequency) displacement to occur. The control for the mount may be broadband or periodic, and in general will be multichannel, using a number of sensors to determine the drives to the actuators. The sensors may be accelerometers, for example, which may be mounted on the appropriate part or parts of the mount.
Although prior published literature describes constrictive actuators employed for vibration control, such actuators have not been utilised in combination with an intermediate body. For example an electrostrictive actuator system is known from French Patent Specification No 1547529, in which a rigid table containing sensitive equipment is isolated from a support by a plurality of single degree of freedom actuators to prevent vibrations from the support from reaching the table. Up to six degrees of freedom of the table are covered. However, any lack of rigidity in the table in such a system, allows vibrations to be imparted to the sensitive equipment, which is avoided by the present invention.
Brief Description of the Drawings The invention will now be described, by way of example only, with reference to the accompanying drawings in which: Figure 1 is a side view, partly in section, of a vibration mount in accordance with the invention; Figure 2 is a sectional plan view of the mount taken on the line II-II in Figure 1; Figure 3 is a view similar to Figure 1 but showing prestressing bolts in the mounts; and Figure 4 is a side view similar to Figure 1 showing a modified vibration mount; Figure 5 is a side view of a raft or table which is mounted on a plurality of vibration mounts, Figure 6 is a side view, partly in section, of a vibration mount in accordance with the invention, which utilises compound stacks of constrictive actuators capable of deforming in shear and extension, and Figure 7 is a sectional view of the mount of Figure 6 taken on the line II - II.
Detailed Description of the Drawings Referring first to Figures 1 and 2 there is shown generally at 10 (Figure 1) a vibrating body supported by a support 12, with an active vibration mount 14 disposed therebetween.
The mount 14 comprises an intermediate body 16 of generally rectangular shape supported from the support 12 by a resilient element 18 of elastomeric material. The body 16 is generally surrounded by a cup shaped structure 20 secured to the vibrating body 10.
Disposed between the upper surface of the intermediate body 16 and the inside horizontal surface of the structure 20 are arranged two pairs of constrictive actuators 22.
Similarly disposed between each of the four edges of the intermediate body 16 and the corresponding surfaces of the structure 20 are four pairs of actuators 24. Between the lower surface of the intermediate body and the corresponding lower parts of the structure 20 are arranged two further pairs of constrictive actuators 26. These latter actuators 26 are shown displaced from the upper actuators 22, although they may instead be arranged to be aligned therewith.
Each of the actuators making up the pairs of actuators 22, 24, 26 is a magnetostrictive actuator, for example one made of the rare earth alloy Tb 0.27 Dy 0.73 Fe 1.95. Each actuator is cylindrical in shape and is surrounded by a coil 28.
A steady magnetic bias field is provided either by a direct current flowing in the coil 28 and/or by means of a permanent magnet (not shown). Expansion and contraction of the actuator length is achieved by varying the current flowing in the coil and "vibration" of the actuator is achieved using an alternating current of appropriate frequency.
Referring now to Figure 3, there are shown a number of prestressing bolts 30 fitted to the structure 20 in order to prestress the respective actuators. Where a bolt passes through a hole in the intermediate body 16, such as hole 32, the hole is made oversize to provide clearance and thereby avoid direct contact between the structure 20 and the intermediate body 16.
In use sensors (not shown), such as accelerometers, are fitted to the intermediate body 16, and signals from these are fed to a control system which includes a microprocessor (not shown) to produce a correction signal corresponding to the corrective action required to counteract the vibration sensed. Typically this correction signal comprises an alternating current of appropriate amplitude and frequency which flows in the coils associated with the respective actuator(s) which are thus caused to cyclically change in length to neutralize any vibration of the intermediate body.
By providing these pairs of constrictive actuators, as illustrated, it is possible to control vibration in all six degrees of freedom of motion.
Refering next to Figure 4, there is shown a modified vibration mount 54 in which the number of actuators is half that for the first embodiment of Figures 1 and 2.
As with the first embodiment, the mount 54 is disposed between an upper vibrating body 53 and a support 52. The mount 54 again comprises a rectangular intermediate body 56 carried by the support 52 through a resilient passive element 58.
Surrounding the body 56 is a generally cup-shaped structure 59, secured to the vibrating body 53. A compliant passive element 62 supports the structure 59 from the upper surface of the body 56. Between the lefthand edge of the body 56 and the corresponding inside surface of the structure 59 is disposed a smaller passive element 62; a passive element (not shown) is also disposed between the rear edge of the body 56 (as viewed in Figure 4) and the corresponding inside surface of the structure 59. As with the mount 14 of Figures 1 and 2, a pair of constrictive actuators 60 is arranged at each side between the lower surface of the body 56 and the corresponding parts of the structure 59. A pair of actuators 60 are also disposed between the right-hand edge of the body 56 and the corresponding inside surface of the structure 59, with a similar pair 60 being disposed between the front edge of body 56 (as viewed in Figure 4) and the corresponding inside surface of the structure 59. Thus there are four pairs of actuators 60 in the present mount 54, instead of eight pairs as in the previously described mount 14, since one actuator of each of the opposing pairs of Figures 1 and 2 is replaced by a compliant passive element. The stiffness of these passive elements is calculated with due regard to the stiffness of the actuators and the size of the displacements to be controlled.
An added feature of this arrangement is that the static load of the upper vibrating body can be supported on a passive element which may reduce the size of constrictive actuators required, especially where extremely large static loads are present.
In the arrangements of Figures 1, 2 and 4, a shear isolation may additionally be provided between two or more orthogonally mounted actuators by inserting a passive compliance element (not shown) at both ends of each actuator to allow lateral and rocking movements at both ends thereof.
Referring now to Figure 5 there is shown a rectangular raft or table 40 on which is mounted a vibrating machine 42. Four vibration mounts 44, each similar to the vibration mount 14 described above, are situated one at each corner of the raft. This isolates vibrations of the machine 42 from the support, typically the ground, sven when the raft is not itself completely rigid.
An arrangement similar to Figure 5 may also be utilised where sensitive equipment is to be isolated from a support (which may be the ground) and which itself may be subject to vibration. However in this case each vibration mount 44 has its cup shaped structure 20 inverted and secured to the support or the ground, so that vibrations between the support or ground and the intermediate bodies 16 of the mounts 44 are counteracted by the constrictive actuators.
A resilient element, such as element 18, is disposed between the raft and each intermediate body (not shown) in each mount to absorb high frequency vibrations. This arrangement again reduces the transfer of vibrations from the support or the ground to the sensitive equipment even where the raft is not a rigid member.
Referring to Figures 6 and 7, these show an active vibration mount employing compound stacks of shear and extension actuators. A vibrating body 10 is supported on the upper plate 20 of the active vibration mount. This in turn is supported on the tops of the actuator stacks, which may be surmounted by hemispherical hard caps 9.
These caps are intended to produce point contacts with the upper plate 20 and thus to prevent the upper plate from exerting torques on the actuator stacks. Each stack includes an actuator 8 to produce vertical displacements of the cap, and two mutually orthogonal directions. The bases of the stacks are supported by the intermediate body 16, which in turn may be supported on a resilient element 18.

Claims (24)

Claims
1. A method of active vibration control in which a subject body, being a vibrating body or a body to be isolated from external vibrations, is mounted on a support by a vibration mount which includes an intermediate body between the subject body and the support, wherein the vibration imparted to the intermediate body is reduced, over at least a part of the frequency range for which vibration control is required, by applying controlled compensating forces to the intermediate body by means of at least one constrictive actuator (as hereinbefore defined).
2. A method according to claim 1, wherein the or each constrictive actuator acts to increase or decrease its dimensions in response to a control signal.
3. A vibration mount by means of which a subject body is mounted on a support and which includes an intermediate body between the subject body and the support, wherein at least one constrictive actuator (as hereinbefore defined) is provided for applying controlled compensating forces to the intermediate body, so as to reduce vibration of the intermediate body, over at least a part of the frequency range for which control of vibrations is required.
4. A vibration mount according to claim 3, wherein the or each constrictive actuator acts to increase or decrease its dimensions responsively to a control signal derived from a sensor, such as an accelerometer, on the intermediate body.
5. A vibration mount according to claim 2 or claim 3, wherein the intermediate body is a substantially rigid member over the frequency range of vibrations to be controlled.
6. A vibration mount according to claim 3 or claim 4 or claim 5, wherein the subject body is a vibrating body to be isolated from the support, and the or each constrictive actuator is mounted between the vibrating body and the intermediate body.
7. A vibration mount according to claim 3 or claim 4 or claim 5, wherein the subject body is to be isolated from a vibrating support, and the or each actuator is mounted between the intermediate body and the support.
8. A vibration mount according to any of claims 3 to 7, wherein the actuator is controlled by a computer.
9. A vibration mount according to any of claims 3 to 8, wherein a passive resilient element is provided between the intermediate body and the subject body where the latter is vibrating, and/or between the intermediate body and the support where the latter is vibrating.
10. A vibration mount according to any of clams 3 to 9, wherein the intermediate member has up to six degrees of freedom, and an appropriate plurality of constrictive actuators are arranged to control the relatively low frequency vibrations over all six degrees of freedom of movement of the intermediate member.
11. A vibration mount according to any of claims 3 to 10, wherein large static loads are supported on a passive element in parallel with the or each actuator.
12. A vibration mount according to any of claims 3 to 11, wherein the or each actuator is piezoelectric.
13. A vibration mount according to any of claims 3 to 11, wherein the or each actuator is magnetostrictive.
14. A vibration mount according to claim 13, wherein a bias magnetic field for the magnetostrictive actuator is supplied by a permanent magnet or by a direct current in a surrounding coil (or both), while the fluctuating magnetic field required is supplied by an alternating current in a coil which, if a coil is employed to produce the bias field, may be the same coil.
15. A vibration mount according to any of claims 3 to 14, having one or more prestressed actuators, prestressing being effected by prestressing bolts.
16. A vibration mount according to any of claims 2 to 15, wherein the subject body is to be free to vibrate, and the intermediate body is surrounded by a generally cup shaped member and connected thereto by a plurality of constrictive actuators.
17. A vibration mount according to claim 16 when appendant to claim 15, wherein the cup shaped member is prestressed by bolts extending therethrough and through the intermediate body, clearance holes being provided in the intermediate body to avoid direct contact between it and the bolts.
18. A vibration mount according to any of claims 3 to 17, wherein the intermediate body is substantially flat and rectangular in shape, and a pair of actuators are disposed at each side, and opposed pairs of actuators are provided respectively above and below.
19. A vibration mount according to claim 18, wherein one of each pair of actuators in an opposed pair is replaced by a passive element, such passive elements being arranged at the upper or static load bearing side of the intermediate body, thereby reducing the size of the opposite actuator.
20. A vibration mount according to any of claims 3 to 17, having a minimum of three compound actuators provided above the intermediate body, each compound actuator comprising a stack of three constrictive actuators, one capable of deforming in shear in a direction normal to the axis of the stack in response to a control signal, and another capable of deforming in extension or compression parallel to the axis of the stack.
21. A vibration mount according to claim 20, wherein the subject body is supported on the tops of the three or more compound actuators via a cap plate resting on the compound actuators but not fixed rigidly to them.
22. A vibration mount according to any of claims 3 to 21, wherein the control for the mount is broadband or periodic, and is multichannel, incorporating a plurality of sensors to determine the drives to the actuators.
23. A method of active vibration control substantially as hereinbefore described.
24. A vibration mount substantially as hereinbefore described with reference to the accompanying drawings.
GB8913273A 1988-09-09 1989-06-09 Active control of vibration Expired - Fee Related GB2222657B (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
GB888821214A GB8821214D0 (en) 1988-09-09 1988-09-09 Active control of vibration
GB898906068A GB8906068D0 (en) 1989-03-16 1989-03-16 Active control of vibration
US07/493,410 US5052529A (en) 1989-03-16 1990-03-14 Active control of vibration

Publications (3)

Publication Number Publication Date
GB8913273D0 GB8913273D0 (en) 1989-07-26
GB2222657A true GB2222657A (en) 1990-03-14
GB2222657B GB2222657B (en) 1992-10-07

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Cited By (23)

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DE4110601A1 (en) * 1990-04-03 1991-10-10 Toyo Tire & Rubber Co Vibration isolating unit for vehicle engine - uses intermediate piezoelectric washer(s) for one or two fixings
GB2242956A (en) * 1989-12-25 1991-10-16 Nissan Motor Power plant suspension device
EP0470064A2 (en) * 1990-07-31 1992-02-05 AVL Gesellschaft für Verbrennungskraftmaschinen und Messtechnik mbH.Prof.Dr.Dr.h.c. Hans List Internal combustion engine
DE4142885A1 (en) * 1990-12-28 1992-07-02 Nissan Motor BEARING FOR DRIVE MACHINES
EP0509911A1 (en) * 1991-04-16 1992-10-21 Societe De Mecanique Magnetique S.A. Hybrid vibration damper with active magnetic vibrator
FR2677415A1 (en) * 1991-06-07 1992-12-11 Thomson Csf Active device for compensating for mechanical vibrations
EP0545264A1 (en) * 1991-11-26 1993-06-09 Honda Giken Kogyo Kabushiki Kaisha Vibration control system
FR2692017A1 (en) * 1992-06-03 1993-12-10 Clausin Jacques Active vibration suppressor using piezoelectric sensor and actuator - has microprocessor to calculate cancelling signal from digitalised sensor signal for analogue conversion to supply actuator
EP0676558A1 (en) * 1994-04-04 1995-10-11 Applied Power Inc. Stiff actuator active vibration isolation system
EP0756103A1 (en) * 1995-07-27 1997-01-29 Deutsches Zentrum für Luft- und Raumfahrt e.V. Interface apparatus for vibration damping in structural dynamic systems
US5695027A (en) * 1995-11-15 1997-12-09 Applied Power Inc. Adaptively tuned vibration absorber
US5710714A (en) * 1995-11-15 1998-01-20 Applied Power Inc. Electronic controller for an adaptively tuned vibration absorber
EP0907036A2 (en) * 1997-09-11 1999-04-07 DaimlerChrysler AG Mechanical resonator with variable resonance frequency
US5920173A (en) * 1995-11-15 1999-07-06 Applied Power Inc. Feedback enhanced adaptively tuned vibration absorber
FR2776815A1 (en) * 1998-03-28 1999-10-01 Eurocopter Deutschland INSTALLATION FOR SUPPRESSING NOISE EMITTED BY PARTS PARTICULARLY INTENDED FOR A SUPPORTING STRUCTURE AND PARTICULARLY A SPACER OF THE MAIN TRANSMISSION OF A HELICOPTER
GB2343494A (en) * 1998-11-04 2000-05-10 Marconi Electronic Syst Ltd Active vibration control
DE10110822A1 (en) * 2001-03-07 2002-09-26 Daimler Chrysler Ag Method and device for influencing the transmission of vibrations of a vibration generator to an associated object, in particular engine vibrations on the body of a motor vehicle
WO2005010399A1 (en) * 2003-07-22 2005-02-03 Fraunhofer-Gesellschaft zur Förderung der angewandten Forschung e.V. Modular interface for damping mechanical vibrations
WO2005100816A1 (en) * 2004-04-16 2005-10-27 Fraunhofer-Gesellschaft zur Förderung der angewandten Forschung e.V. Pushing force deviating interface for damping mechanical vibrations
WO2006077143A1 (en) * 2005-01-21 2006-07-27 Fraunhofer-Gesellschaft zur Förderung der angewandten Forschung e.V. Device for dynamically load testing a sample
US7234153B2 (en) 2001-08-08 2007-06-19 Isic A/S Vibration damper for dampening vibrations at low frequencies
DE102013015610A1 (en) * 2013-09-19 2015-03-19 Bundesrepublik Deutschland, vertreten durch das Bundesministerium der Verteidigung, vertreten durch das Bundesamt für Ausrüstung, Informationstechnik und Nutzung der Bundeswehr Actuator for vibration decoupling
CN109751360A (en) * 2018-12-26 2019-05-14 山东科技大学 Magnetostriction system for wind tower

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Cited By (40)

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Publication number Priority date Publication date Assignee Title
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GB2222657B (en) 1992-10-07
GB8913273D0 (en) 1989-07-26

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