GB2365945A - A vibration damping system - Google Patents

A vibration damping system Download PDF

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Publication number
GB2365945A
GB2365945A GB0020082A GB0020082A GB2365945A GB 2365945 A GB2365945 A GB 2365945A GB 0020082 A GB0020082 A GB 0020082A GB 0020082 A GB0020082 A GB 0020082A GB 2365945 A GB2365945 A GB 2365945A
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United Kingdom
Prior art keywords
magnetism
vibration damping
damping system
energy dissipating
medium
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Granted
Application number
GB0020082A
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GB0020082D0 (en
GB2365945B (en
Inventor
Bishakh Bhattacharya
Jem Rongong
Geoffrey Railton Tomlinson
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Rolls Royce PLC
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Rolls Royce PLC
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Priority to GB0020082A priority Critical patent/GB2365945B/en
Publication of GB0020082D0 publication Critical patent/GB0020082D0/en
Priority to US09/928,219 priority patent/US6688439B2/en
Publication of GB2365945A publication Critical patent/GB2365945A/en
Application granted granted Critical
Publication of GB2365945B publication Critical patent/GB2365945B/en
Anticipated expiration legal-status Critical
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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/04Antivibration arrangements
    • F01D25/06Antivibration arrangements for preventing blade vibration
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/04Antivibration 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
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/60Efficient propulsion technologies, e.g. for aircraft

Abstract

A vibration damping system 8 wherein the system 8 comprises a magnetism generating medium 12 and a magnetism energy dissipating medium 16 whereby, in use, vibration of the magnetism generating medium 12 generates a magnetic field, the magnetism generating medium 12 and the magnetism energy dissipating medium 16 being so disposed with respect to each other that the magnetic field is then dissipated by the magnetism energy dissipating medium 16 thereby damping the vibrations of the magnetism generating medium 12.

Description

<Desc/Clms Page number 1> A VIBRATION DAMPING SYSTEM AND A METHOD OF DAMPING VIBRATIONS This invention relates to a system and a method for exclusively, those structures undergoing a machining operation.
During a machining operation, for instance milling a metallic component, it is common for chatter to occur if the tooling or workpiece are of insufficient rigidity. Chatter is the vibration of the milling tool relative to the workpiece which results in either a reduction in the quality of the surface finish being machined or an increase in the machining process time where a better surface finish is required. In the manufacture of aero-engine blisks this is of particular importance as the tough nature of the material, titanium, to be machined and the flexibility and low inherent damping of the workpiece severely curtails machining rates.
Current damping techniques include magnetostrictive actuators as disclosed in "Vibration suppression in slender composite beams using magnetos trictive actuation", Journal of Aeronautical Society of India, vol. 48, no. 2, 1996. However, this technique is disadvantaged by being an active system, requiring a power supply, wiring to induce a magnetic field and by incurring a weight penalty. Another damping technique uses piezoelectric shunts, as disclosed in "Non-linear piezoelectric vibration absorbers", Smart Materials and Structures, vol. 5, no. 5, 1996. Such shunts essentially convert mechanical strain, from vibrations, into electrical charge which is then dissipated via an electrical network thus attenuating vibration. This system is disadvantaged by requiring wire connections and added weight. A further damping technique uses visco-elastic material as disclosed in "Vibration damping", John Wiley
<Desc/Clms Page number 2>
and Sons, 1985, but suffers from a weight penalty and the difficulty of maintaining optimal environmental conditions for required performance.
It is the object of the present invention to provide a vibration damping system and a method for damping vibrations of vibrating structures which may accommodate irregular workpiece and tooling geometries, may operate in extreme environmental conditions, may be used where access is limited and which has a reduced weight penalty.
According to the present invention, there is provided a vibration damping system wherein the system comprises a magnetism generating medium and a magnetism energy dissipating medium whereby, in use, vibration of the magnetism generating medium generates a magnetic field, the magnetism generating medium and the magnetism energy dissipating medium being so disposed with respect to each other that the magnetic field is then dissipated by the magnetism energy dissipating medium thereby damping the vibrations of the magnetism generating medium.
Alternatively, the system comprises a body, the magnetism generating medium is applied to the body, so that, in use, when the body vibrates a magnetic field is generated by the magnetism generating medium, the magnetism generating medium and the magnetism energy dissipating medium being so disposed with respect to each other that the magnetic field is then dissipated by the magnetism energy dissipating medium thereby damping the vibrations of the body.
Preferably, the vibration damping system comprises a secondary structure, the magnetism energy dissipating medium is applied to the secondary structure and the secondary structure, in use, is in proximity to the body such that the vibrations of the body are damped.
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Preferably, the secondary structure comprises magnetism energy dissipating medium and, in use, is in proximity to the body such that the vibrations of the body are damped. Alternatively, the magnetism energy dissipating medium is applied to the magnetism generating medium.
Preferably, the magnetism generating medium comprises magnetostrictive material. Alternatively, the magnetism generating medium comprises a matrix and a plurality of magnetostrictive particles dispersed within the matrix.
Preferably, the magnetism energy dissipating medium comprises a matrix and a plurality of magnetostrictive particles dispersed within the matrix.
Preferably, the magnetostrictive particles and the magnetostrictive material each comprise 30% Terbium, 700 Dysprosium and trace Iron. Alternatively, the magnetostrictive particles and the magnetostrictive material each comprise any one or more of the magnetic transition elements. Alternatively, the magnetostrictive particles and the magnetostrictive material each comprise any one or more of the rare earth materials. Alternatively, the magnetostrictive particles and the magnetostrictive material each comprise any one or more of the rare earth materials and any one or more of the magnetic transition elements.
Preferably the magnetism energy dissipating matrix comprises polyurethane. Alternatively, the magnetism energy dissipating medium comprises a matrix, the matrix comprises a visco-elastic magnetism energy dissipating matrix.
Preferably, the magnetism energy dissipating medium includes a visco-elastic magnetism energy dissipating matrix and the magnetism generating medium includes a binder matrix, the binder matrix having an elastic modulus greater than the elastic modulus of the visco-elastic dissipating matrix.
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Preferably, each of the magnetostrictive particles has substantially the same magnetic orientation as the remainder thereof. Alternatively, each of the magnetos trictive particles is oriented substantially in the direction of the magnetic field.
Alternatively, the magnetos trictive particles are each of the same size.
Preferably, the vibrations imposed on the magnetism generating medium are derived from a machining process. Alternatively, the vibrations imposed on the magnetism generating medium are derived from an acoustic source. Preferably, the body is any one of the primary structure, the machine, the tool or any industrially manufactured item which undergoes some form of machining process. Alternatively, the body is a component of a gas turbine engine. Alternatively, the body is a component of an aircraft. Alternatively, the body is a vibrating rotating body.
Preferably, the magnetism generating medium is any one of the primary structure, the machine, the tool or any industrially manufactured item which undergoes some form of machining process. Alternatively, the magnetism generating medium is a component of a gas turbine engine. Alternatively, the magnetism generating medium is a component of an aircraft. Alternatively, the magnetism generating medium is a vibrating rotating body.
Preferably, a means for cooling the secondary structure is provided. Preferably, a means for cooling the magnetism energy dissipating coating is provided. Preferably, the means for cooling comprises any conventional cooling system as known in the art.
Preferably, a method of damping vibrations of a body wherein the method comprises the steps of: (i) applying a magnetism generating medium to a body:
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(ii) applying a magnetism energy dissipating medium to a secondary structure; (iii) disposing the secondary structure in proximity to the body so that the magnetism generating coating and the magnetism energy dissipating medium are so disposed with respect to each other that the magnetic field is then dissipated by the magnetism energy dissipating medium thereby damping the vibrations of the body.
Preferably, the method of damping vibrations of the body comprises the further step of cooling the magnetism energy dissipating medium to optimise operational temperature of the magnetism energy dissipating medium.
Preferably, the method of damping vibrations of the body comprises the further step of cooling the secondary structure.
The present invention will now be described, by way of example, with reference to the accompanying drawings in which: Figure 1 is a sectioned view of a generalised application of the present invention.
Figure 2 is a sectioned view of an idealised magnetos trictive particle undergoing dilation under the effect of an applied magnetic field.
Figure 3 is a second embodiment of the present invention showing an application of the present invention to the milling tool of a machine.
Figure 4 is a third embodiment of the present invention showing the application of the present invention to gas turbine engine components.
Figure 5 shows a fourth embodiment of the present invention.
Figure 6 shows a fifth embodiment of the present invention.
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With reference to figure 1, it can be seen that a vibration damping system 8 comprises a magnetism generating coating 12 applied to a body 10, in this case a primary structure 10. The magnetism generating coating 12 being a magnetism generating medium 12. The primary structure 10 is the vibrating structure to be damped. The system 8 also comprises a magnetism energy dissipating coating 16 which is applied to a secondary structure 14. The magnetism energy dissipating coating 16 being a mc. aetism energy dissipating medium 16.
In operation the secondary structure 14 is in proximity to the vibrating primary structure 10 where a magnetic field, induced by the magnetism generating coating 12, works in operative association with the magnetism energy dissipating coating 16. Thereby, the vibrations of the primary structure 10 may be damped by transference of vibration energy to the magnetism energy dissipating coating 16 applied on the secondary structure 14 via the magnetic field. The magnetism generating coating 12 and the magnetism energy dissipating coating 16 work cooperatively and in accordance with the principle of magnetostriction.
Magnetostriction is a phenomenon where a material undergoes mechanical strain under the influence of a magnetic field and vice-versa. This physical property is found in materials containing magnetic transition elements such as, but not exclusively, Iron, Nickel and rare earth elements like Lanthanum and Terbium. Referring to Figure 2, a particle 18, 20, of these materials normally comprise numerous small randomly oriented magnetic domains, which can rotate and align under the influence of an external magnetic field. Although the amount of magnetostriction is usually small, it has been shown (Clark, A.E., "Magnetos trictive rare earth-Fe2 compounds", Ferromagnetic
<Desc/Clms Page number 7>
Materials, Vol. 1, Ch. 7, North Holland Publishing Co., 1980) that considerable magnetostriction in an alloy of Terbium, Dysprosium and Iron, which is commercially known as Terfenol-DTM, is possible. Terfenol-DTM comprises approximately 30% Terbium and 70% Dysprosium and also traces of Iron.
Currently, magnetostrictive materials like Terfenol- DTM are being used in active damping of structural vibration as they can produce a large amount of actuation (around 2000 micro-strains) and have a stable performance over a frequency range of 0-lOkHz (as disclosed in Anjanappa, M. and Bi, J., "Magnetos trictive mini actuators for smart structure application", Smart Materials and Structures, Vol. 3, 1994, pp. 383-95).
Recently, actuators made from magnetostrictive Terfenol-DTM particles embedded in a compliant polymer have been reported (Sandlund, L., et al, "Magnetostriction, elastic moduli and coupling factors of composite Terfenol- D", Journal of Applied Physics, Vol. 75, 1994, pp. 5656- 8.). The static macroscopic behaviour of these actuators has been characterised (Anjanappa, M. and Wu, Y, "Magnetostrictive particulate actuators: configuration, modelling, and characterisation, Smart Materials and Structures, vol. 6, 1997, pp.393-402) and it has been observed that several parameters such as volume fraction, modulus of elasticity of a binder matrix of the compliant polymer, pre-stressing and orientation of the magnetos trictive particles play a significant role in the performance of the actuator.
The preferred embodiment of the vibration damping system 8 comprises two non-contacting coatings 12, 16. Alternatively, however, one coating 12 may overlay the other coating 16 which is applied on a surface of the body 10. The coatings 12, 16 may be interposed with one
<Desc/Clms Page number 8>
another. The magnetism generating coating 12 comprises a binder matrix 22, having elastic modulus El, and magnetos trictive particles 20 of radius r1. Magnetism energy dissipating coating 16 comprises a visco-elastic magnetism energy dissipating matrix 24, having elastic modulus E2, and dispersed magnetos trictive particles 18 of radius r2. Preferably the visco-elastic magnetism energy dissipating matrix 24 is polyurethane but may be any visco- elastic material. The modulus E2 is usually less than El and r2 is usually less than r1. The magnetism energy dissipating coating 16 is preferably separate from the primary structure 10 and provides the non-contact magnetism energy dissipating medium (magnetism energy dissipating coating 16) while the primary structure 10 vibrates under external dynamic loading as, for example, in rotating discs such as compact discs, fan blades of gas turbine engines and impellers.
The internal strain in the primary structure 10 induced during vibration is first transmitted to the magnetostrictive particles 20 of magnetism generating coating 12. This generates a magnetic field which in turn induces a magnetic moment in the particles 18 of the magnetism energy dissipating coating 16 making the particles 18 vibrate in the magnetism energy dissipating matrix 24 and thus resulting in a net energy loss.
In figure 2, a magnetos trictive particle 18, 20, in an unconstrained state 18A, 20A, dilates to a dilated state 18B, 20B, under the effect of a magnetic field M and the free-strain along the direction of an applied magnetic field M is given by equation 1,
<Desc/Clms Page number 9>
where dm is the magneto-mechanical constant, H is the magnetic field strength, sf is the free-strain, r and r' being the initial and final radius along the direction of the magnetic field M. Though the magnetos triction is known to induce only extensional strains, by applying an initial field called a bias, both compressive and extensional strains can be realised. For a particle 18, 20 in a constrained medium 12, 16, the bias static strain can be derived from the theory of direct magnetos triction. The biasing magnetic field will then be related to the net strain by equation 2,
where, sj;u, is the bias strain, a is the elastic stress, EH is the Young's Modulus in a constant magnetic field and Hbias is the applied magnetic field. During vibration of the primary structure 10, an additional strain s,, is produced and the resultant magnetic field is given by equation 3, Hef = jD,,,_'(c, - eh;,,.,, )I .................. (3) For a two particle system the net magnetic field is given by equation 4,
where, ,u, is the relative magnetic field permeability between the two particles; r1, r12 and r2 are respectively, the radius of the field generator magnetos trictive particle 18A, 20A, the distance between the generating particle 20
<Desc/Clms Page number 10>
and the magnetic energy dissipating particle 18 and the radius of the magnetic energy dissipating dilated particle 18B. M1 and MZ are the magnetic dipole moments. The net effective magnetic field Hnet will induce magnetostrictive strain on the magnetic energy dissipating particles 18 such that: einduced - dM' Hnet .................. (5 Thus for an applied strain,c,, in the magnetism generating coating 12, an induced strain si"dn,,,d is produced resulting in dynamic motion of the particles 18 in the magnetism energy dissipating coating 16. The magnetic energy is then converted into thermal energy as the particles 18 dilate and contract imparting work on the magnetism energy dissipating medium 16. This product, of the work done by the particles 18 on the magnetism energy dissipating medium 16, converts into thermal energy, which is then dissipated from the magnetism energy dissipating medium 16.
It is an advantage to provide cooling to the magnetism eneray dissipating medium 16 to optimise working temperature. Cooling may be achieved by any conventional form of cooling and in particular by a fluid such as a flow of air or liquid over or through the magnetism energy dissipating medium 16 or its host secondary structure 14.
In consideration for designing a preferable embodiment of the present invention for any given application, it is observed in equations 4 and 5 that the magnitude of the induced strain is influenced by the following: dipole moments for the magnetostrictive particles 18, 20; magnetic field permeability; ratio rl/r12; geometry and size of the particles 18, 20.
Furthermore, it may be observed that the size of the particles 18 in the magnetism energy dissipating coating 16
<Desc/Clms Page number 11>
play a significant role. Although larger particle size results in more induced strain, from a magnetism energy dissipating point of view, it would be preferable to have relatively small sized particles 18 with high volume fill fraction so that the net dissipation will be enhanced. It should also be noted that the density of the magnetos trictive particles 18, 20 in the coatings 12, 16 may be determined for each application and to attenuate a particular mode of vibration. Similarly, the thickness of the coatings 12, 16 may also be optimised for each application to provide suitable damping of the vibrating body 10.
It should also be noted that the magnetic field strength, H, derived from the magnetism generating coating 12 during vibration, reduces with distance away from the magnetism generating coating 12. Thus the effectiveness of the vibration damping system 8 is dependant on the distance between the magnetism generating coating 12 and the magnetism energy dissipating coating 16.
The preferred embodiment of the present invention and that having the most effective magnetic field generation from the Terfenol-D particles 20 in the magnetism generating coating 12, is where the particles 20 have identical magnetic orientation. This is achieved by magnetising or biasing the particles 20 of the coatings 12 by initially applying a suitable magnetic field to the coatings 12.
Referring again to figure 1, the primary structure or body 10, may be any industrially manufactured item which undergoes some form of machining process, for example milling, cutting, turning, drilling or grinding that may result in the body 10 vibrating. The object of the present invention being to provide vibration damping to such an item during a machining process.
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It is an advantage of the present invention for the magnetism generating coating 12 and the magnetism energy dissipating coating 16 to be non-contacting, but positioned as close as possible to give the greatest vibration damping available. It is also an advantage for the magnetism generating coating 12 and the magnetism energy dissipating coating 16 to be applied to separate structures 10, 14, so that cooling may be applied to the magnetism energy dissipating coating 16. It may also be an advantage in a high temperature environment or where the magnetism generating coating 12 is heated, to position the magnetism energy dissipating coating 16 further away from the magnetism generating coating 12 so that the magnetism energy dissipating coating 16 may be maintained at its optimum operating temperature.
In figure 3 the non-contact vibration damping system 8 may be applied to a tool 26 driven by a machine 28. In this case the tool 26 is a milling tool. The magnetism generating coating 12 and magnetism energy dissipating coating 16 may be applied to both the workpiece 10 and the machine tool 26. Where the vibration damping system 8 is applied to the tool 26, the tool 26 is coated with the magnetism generating medium 12 and substantially surrounded and separated a distance apart from the magnetism energy dissipating medium 16, which is itself coated to a substantially annular secondary structure 30.
Similarly, but not shown, the vibration damping system 8 may be equally applied to the machine 28 or a combination of both the tool 26 and the machine 28.
Referring to figure 4, the vibration damping system 8 may be also applied to other mechanical devices, for example a component of a gas turbine engine 32 which is susceptible to vibration such as a compressor blade 34, stator vane 36, a disc 38, a blisk, a bling, an engine
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casing or an accessory. The vibrations imparted on the vibrating component 34, 36, 38 to be damped may be attributable to rotational out of balance forces for example. These out of balance forces are as a result of a mass imbalance or an aerodynamic loading imbalance and are well known in the art of aero-engine design. In this embodiment the magnetism energy dissipating medium 16 may be applied to a static structure such as a casing 40 surrounding an annular array of radially extending blades 34, themselves coated, either wholly or in part, with magnetism generating medium 12.
However, the primary structure 10 also may be damped to suppress airborne noise, for example in relation to aero-engine blades 34, stator vanes 36 and other aerofoils. The primary structure 10 may also be a compact disc, a read / write laser system, a machine drive shaft, components of aircraft such as flaps and other bodies having weight and shape restrictions. The present invention is particularly applicable in hot environments and to hot components such as fuel pipes as the magnetism energy dissipating medium 16 may be disposed a distance away from the fuel pipe itself and cooling means may be readily provided to the magnetism energy dissipating medium 16 or the secondary structure 14.
Referring to figure 5, which shows a second generalised application of the present invention, where the present invention does not require a non-contacting damping system 8, the magnetism energy dissipating coating 16 is applied directly to the magnetism generating coating 12 on the primary structure 10. In this example the primary structure 10 may be a thin shell structure such as a metallic air conditioning duct.
Furthermore, other embodiments of the present invention may easily be made, but are intended to be within the scope of the present invention. For example, the
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magnetism generating medium 12 may be applied to part of the body 10 to be damped or all of the body 10 or primary structure 10. The magnetism energy dissipating medium 16, applied to part or a11 of the secondary structure 14 and the secondary structure 14 may surround some or a11 of the body 10. A plurality of secondary structures 14 may be provided, each secondary structure 14 may have substantially the same magnetism energy dissipating coating 16 or alternatively different magnetism energy dissipating coatings 16 each adapted to damp vibrations of different frequencies. The magnetism energy dissipating coatings 16 may vary in the size of the particles, the thickness of the coating, the elastic modulus of the visco-elastic magnetism energy dissipating matrix 24. The magnetism energy dissipating medium 16 may comprise layers or discrete regions of coatings, each coating adapted to damp a range of vibratory frequencies.
A further example of the application of this system to damp vibrations of a primary structure 10 is for reducing the noise of vehicular traffic. In this example the carriageway is lined with panels, each panel being coated with the magnetism generating coating 12 and in juxtaposition with a secondary structure 14 having a coating of magnetism energy dissipating medium 16. Thereby, the acoustic vibrations of the panel may be absorbed and not merely reflected. This may also be used along runways at airports to attenuate the noise of aircraft. A preferred embodiment of this example is where the magnetism generating coating 12 is of sufficient integrity to form the panel itself, the magnetism energy dissipating coating 16 then being applied to the magnetism generating medium 12.
A further application for absorbing acoustic vibrations is to apply the coatings 12, 16 directly to a
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primary structure. The coatings 12, 16 overlay each other on the primary structure. For example, and as shown on figure 6, the low pressure fan casing 42 of a gas turbine engine 32 which conventionally comprises a noise suppressing liner (not mown) is replaced by the magnetism generating coating 12 overlaying the magnetism energy dissipating coating 16. In this example it is the magnetism generating coating 12 that is directly excited by acoustic vibrations. Furthermore, it is possible for the magnetism generating coating 12, overlaid with the magnetism energy dissipating coating 16, to form part of or all of a containment casing, as known in the art, to retain a fan blade in the event of a fan blade off incident.
The present invention also relates to a method of damping vibrations wherein the method comprises the steps of: disposing a magnetism generating medium to a body; applying a magnetism energy dissipating medium to a secondary structure; disposing the secondary structure in proximity to the body so that the magnetism generating coating and the magnetism energy dissipating medium are so disposed with respect to each other that the magnetic field is then dissipated by the magnetism energy dissipating medium thereby damping the vibrations of the body. Furthermore, the method of damping vibrations may comprise the further step of providing cooling to the magnetism energy dissipating medium to optimise operational temperature of the magnetism energy dissipating medium. Alternatively, the method of damping vibrations comprises the further step of providing cooling the secondary structure.
Whilst endeavouring in the foregoing specification to draw attention to those features of the invention believed to be of particular importance it should be understood that the Applicant claims protection in respect of any
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patentable feature or combination of features hereinbefore referred to and/or shown in the drawings whether or not particular emphasis has been placed thereon.
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Claims (36)

  1. Claims 1. A vibration damping system wherein the system comprises a magnetism generating medium and a magnetism energy dissipating medium whereby, in use, vibration of the magnetism generating medium generates a magnetic field, the magnetism generating medium and the magnetism energy dissipating medium being so disposed with respect to each other that the magnetic field is then dissipated by the magnetism energy dissipating medium thereby damping the vibrations of the magnetism generating medium.
  2. 2. A vibration damping system as claimed in claim 1 wherein the system comprises a body, the magnetism generating medium is applied to the body, so that, in use, when the body vibrates a magnetic field is generated by the magnetism generating medium, the magnetism generating medium and the magnetism energy dissipating medium being so disposed with respect to each other that the magnetic field is then dissipated by the magnetism energy dissipating medium thereby damping the vibrations of the body.
  3. 3. A vibration damping system as claimed in any one of claims 1-2 wherein a secondary structure is provided, the magnetism energy dissipating medium is applied to the secondary structure and the secondary structure, in use, is in proximity to the body such that the vibrations of the body are damped.
  4. 4. A vibration damping system as claimed in any one of claims 1-3 wherein a secondary structure is provided, the secondary structure comprises magnetism energy dissipating medium and, in use, is in proximity to the body such that the vibrations of the body are damped.
  5. 5. A vibration damping system as claimed in any one of claims 1-3 wherein the magnetism energy dissipating medium is applied to the magnetism generating medium.
    <Desc/Clms Page number 18>
  6. 6. A vibration damping system as claimed in any one of claims 1 to 5 wherein the magnetism generating medium comprises magnetostrictive material.
  7. 7. A vibration damping system as claimed in any one of claims 1 to 5 wherein the magnetism generating medium comprises a matrix and a plurality of magnet ostrictive particles dispersed within the matrix.
  8. 8. A vibration damping system as claimed in any one of claims 1 to 5 and 7 wherein the magnetism energy dissipating medium comprises a matrix and a plurality of magnetos trictive particles dispersed within the matrix.
  9. 9. A vibration damping system as claimed in any one of claims 6 to 8 wherein the magnetostrictive particles and the magnetostrictive material each comprise any one or more of the magnetic transition elements.
  10. 10. A vibration damping system as claimed in any one of claims 6 to 8 wherein the magnetostrictive particles and the magnetostrictive material each comprise any one or more of the rare earth materials.
  11. 11. A vibration damping system as claimed in any one of claims 6 to 8 wherein the magnetostrictive particles and the magnetostrictive material each comprise 30% Terbium, 70% Dysprosium and trace Iron.
  12. 12. A vibration damping system as claimed in any one of claims 7 to 8 wherein the magnetostrictive particles and the magnetos trictive material each comprise any one or more of the rare earth materials and any one or more of the magnetic transition elements.
  13. 13. A vibration damping system as claimed in any one of claims 8 to 12 wherein the magnetism energy dissipating medium comprises a matrix, the matrix comprises a visco- elastic magnetism energy dissipating matrix.
    <Desc/Clms Page number 19>
  14. 14. A vibration damping system as claimed in claim 13 wherein the magnetism energy dissipating matrix comprises polyurethane.
  15. 15. A vibration damping system as claimed in any one of claims 1 to 14 wherein the magnetism energy dissipating medium includes a visco-elastic magnetism energy dissipating matrix and the magnetism generating medium comprises a binder matrix, the binder matrix having an elastic modulus greater than the elastic modulus of the visco-elastic magnetism energy dissipating matrix.
  16. 16. A vibration damping system as claimed in any one of claims 7 to 15 wherein each of the magnetostrictive particles has substantially the same magnetic orientation as the remainder thereof.
  17. 17. A vibration damping system as claimed in any one of claims 7 to 16 wherein each of the magnetostrictive particles is oriented substantially in the direction of the magnetic field.
  18. 18. A vibration damping system as claimed in any one of claims 7 to 17 wherein the magnetostrictive particles are of the same size.
  19. 19. A vibration damping system as claimed in any one of claims 1 to 18 wherein the vibrations imposed on the magnetism generating medium are derived from a machining process.
  20. 20. A vibration damping system as claimed in any one of claims 1 to 18 wherein the vibrations imposed on the magnetism generating medium are derived from an acoustic source.
  21. 21. A vibration damping system as claimed in any one of claims 2 to 5, 7 to 20 wherein the body is any one of the primary structure, the machine, the tool or any industrially manufactured item which undergoes some form of machining process.
    <Desc/Clms Page number 20>
  22. 22. A vibration damping system as claimed in any one of claims 2 to 5, 7 to 20 wherein the body is a component of a gas turbine engine.
  23. 23. A vibration damping system as claimed in any one of claims 2 to 5, 7 to 20 wherein the body is a component of an aircraft.
  24. 24. A vibration damping system as claimed in any one of claims 2 to 5, 7 to 20 wherein the body is a vibrating rotating body.
  25. 25. A vibration damping system as claimed in any one of claims 1, 6 wherein the magnetism generating medium is any one of the primary structure, the machine, the tool or any industrially manufactured item which undergoes some form of machining process.
  26. 26. A vibration damping system as claimed in any one of claims 1, 6 wherein the magnetism generating medium is a component of a gas turbine engine.
  27. 27. A vibration damping system as claimed in any one of claims 1, 6 wherein the magnetism generating medium is a component of an aircraft.
  28. 28. A vibration damping system as claimed in any one of claims 1, 6 wherein the magnetism generating medium is a vibrating rotating body.
  29. 29. A vibration damping system as claimed in any one of claims 1 to 28 wherein a means for cooling the secondary structure is provided.
  30. 30. A vibration damping system as claimed in any one of claims 1 to 28 wherein a means for cooling the magnetism energy dissipating coating is provided.
  31. 31. A vibration damping system as claimed in any one of claims 29 to 30 wherein the means for cooling comprises any conventional cooling system as known in the art.
  32. 32. A method of damping vibrations of a body wherein the method comprises the steps of:
    <Desc/Clms Page number 21>
    (i) applying a magnetism generating medium to a body; (ii) applying a magnetism energy dissipating medium to a secondary structure; (iii) disposing the secondary structure in proximity to the body so that the magnetism generating coating and the magnetism energy dissipating medium are so disposed with respect to each other that the magnetic field is then dissipated by the magnetism energy dissipating medium thereby damping the vibrations of the body.
  33. 33. A method of damping vibrations of a body as claimed in claim 32 wherein the method comprises the further step of cooling the magnetism energy dissipating medium to optimise operational temperature of the magnetism energy dissipating medium.
  34. 34. A method of damping vibrations of a body as claimed in any one of claims 31 or 32 wherein the method comprises the further step of cooling the secondary structure.
  35. 35. A vibration damping system substantially as described in this specification and with reference to figures 1-5 of the accompanying drawings.
  36. 36. A method for damping vibrations substantially as described in this specification and with reference to figures 1-5 of the accompanying drawings.
GB0020082A 2000-08-16 2000-08-16 A vibration damping system and a method of damping vibrations Expired - Fee Related GB2365945B (en)

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US09/928,219 US6688439B2 (en) 2000-08-16 2001-08-13 Vibration damping system and a method of damping vibrations

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Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2256302A1 (en) * 2009-05-05 2010-12-01 Rolls-Royce plc A duct wall for a fan of a gas turbine engine
EP2273076A1 (en) * 2009-05-05 2011-01-12 Rolls-Royce plc A duct wall for a fan of a gas turbine engine
EP3002414A3 (en) * 2014-09-09 2016-05-18 Rolls-Royce Corporation Piezoelectric damping rings
US10697320B2 (en) 2017-01-20 2020-06-30 Rolls-Royce Corporation Piezoelectric vibratory control for static engine components

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7451966B1 (en) * 2001-07-02 2008-11-18 Knowles Gareth J Isolator mount for shock and vibration
JP4649136B2 (en) * 2003-07-31 2011-03-09 キヤノン株式会社 Actuator, exposure apparatus, and device manufacturing method
GB0410778D0 (en) * 2004-05-13 2004-06-16 Rolls Royce Plc Blade arrangement
US7270517B2 (en) * 2005-10-06 2007-09-18 Siemens Power Generation, Inc. Turbine blade with vibration damper
DE102006002617A1 (en) * 2006-01-19 2007-07-26 Mtu Aero Engines Gmbh Method for milling components
DE102011114471B4 (en) 2011-09-28 2013-05-08 Eads Deutschland Gmbh Membrane arrangement for sound generation
US8915718B2 (en) * 2012-04-24 2014-12-23 United Technologies Corporation Airfoil including damper member
US9725154B2 (en) * 2014-05-13 2017-08-08 The Boeing Company Method and apparatus for reducing structural vibration and noise
CN114101801B (en) * 2021-12-28 2023-05-12 松德刀具(长兴)科技有限公司 Damping vibration attenuation cutter

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1415304A (en) * 1971-11-09 1975-11-26 Spodig Heinrich Method of and apparatus for damping vibrations and parasitic oxcillations in machine tools
GB2216601A (en) * 1988-03-23 1989-10-11 Lucas Ind Plc Throttle valve assembly
GB2221743A (en) * 1988-07-07 1990-02-14 Marconi Gec Ltd Machinery mounting for marine vessels
GB2222279A (en) * 1988-08-25 1990-02-28 Westinghouse Electric Corp For actively controlling vibrations
GB2251049A (en) * 1990-10-20 1992-06-24 Atsugi Unisia Corp Electromagnetic strut assembly
GB2313170A (en) * 1996-05-14 1997-11-19 Fmc Corp A linear motion conveyor having an intermittently actuated damper

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4023651A (en) * 1973-03-31 1977-05-17 The Production Engineering Research Association Damping vibrations in sheet material
US3817356A (en) * 1973-05-29 1974-06-18 Minnesota Mining & Mfg Vibration damping
US4406642A (en) * 1981-04-13 1983-09-27 Dresser Industries, Inc. Shaft dampening apparatus
US5300355A (en) * 1991-05-31 1994-04-05 Nichias Corporation Vibration damping material
US5810126A (en) * 1993-10-26 1998-09-22 Byelocorp Scientific, Inc. Electroheological fluid composite structures
US5538774A (en) * 1994-07-29 1996-07-23 Minnesota Mining And Manufacturing Company Internally damped rotatable storage article
FR2740349B1 (en) * 1995-10-30 1997-11-21 Dynastar Skis Sa VIBRATION DAMPING DEVICE FOR MOUNTING ON A SPORTS ARTICLE
US5855353A (en) * 1996-05-31 1999-01-05 Owens Corning Fiberglas Technology, Inc. Vibration damping system
US5965249A (en) * 1997-08-07 1999-10-12 Gore Enterprise Holdings, Inc. Vibration damping composite material
US6191510B1 (en) * 1997-12-19 2001-02-20 3M Innovative Properties Company Internally damped stator, rotor, and transformer and a method of making
US6285525B1 (en) * 1998-07-01 2001-09-04 3M Innovative Properties Company Damped spacer articles and disk drive assemblies containing damped spacer articles
GB9926199D0 (en) * 1999-11-05 2000-01-12 Rolls Royce Plc A particle vibration damper for a non-rotating component of a gas turbine engine

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1415304A (en) * 1971-11-09 1975-11-26 Spodig Heinrich Method of and apparatus for damping vibrations and parasitic oxcillations in machine tools
GB2216601A (en) * 1988-03-23 1989-10-11 Lucas Ind Plc Throttle valve assembly
GB2221743A (en) * 1988-07-07 1990-02-14 Marconi Gec Ltd Machinery mounting for marine vessels
GB2222279A (en) * 1988-08-25 1990-02-28 Westinghouse Electric Corp For actively controlling vibrations
GB2251049A (en) * 1990-10-20 1992-06-24 Atsugi Unisia Corp Electromagnetic strut assembly
GB2313170A (en) * 1996-05-14 1997-11-19 Fmc Corp A linear motion conveyor having an intermittently actuated damper

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2256302A1 (en) * 2009-05-05 2010-12-01 Rolls-Royce plc A duct wall for a fan of a gas turbine engine
EP2273076A1 (en) * 2009-05-05 2011-01-12 Rolls-Royce plc A duct wall for a fan of a gas turbine engine
US8434995B2 (en) 2009-05-05 2013-05-07 Rolls-Royce Plc Duct wall for a fan of a gas turbine engine
US8506234B2 (en) 2009-05-05 2013-08-13 Rolls-Royce Plc Duct wall for a fan of a gas turbine engine
EP3002414A3 (en) * 2014-09-09 2016-05-18 Rolls-Royce Corporation Piezoelectric damping rings
US10557352B2 (en) 2014-09-09 2020-02-11 Rolls-Royce Corporation Piezoelectric damping rings
US10697320B2 (en) 2017-01-20 2020-06-30 Rolls-Royce Corporation Piezoelectric vibratory control for static engine components

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US20030213660A1 (en) 2003-11-20
GB0020082D0 (en) 2000-10-04
GB2365945B (en) 2004-02-11

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