EP1285182A1 - Variable or non-variable amplitude vibrating wave damping device - Google Patents

Variable or non-variable amplitude vibrating wave damping device

Info

Publication number
EP1285182A1
EP1285182A1 EP01940625A EP01940625A EP1285182A1 EP 1285182 A1 EP1285182 A1 EP 1285182A1 EP 01940625 A EP01940625 A EP 01940625A EP 01940625 A EP01940625 A EP 01940625A EP 1285182 A1 EP1285182 A1 EP 1285182A1
Authority
EP
European Patent Office
Prior art keywords
walls
damping element
incident surface
damping
deformation
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Withdrawn
Application number
EP01940625A
Other languages
German (de)
French (fr)
Inventor
Alain Le Mehaute
François ANGOULVANT
François TSOBNANG
Carole Challioui
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.)
Ismans - Institut Superieur des Materiaux du Mans
Original Assignee
Ismans - Institut Superieur des Materiaux du Mans
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 Ismans - Institut Superieur des Materiaux du Mans filed Critical Ismans - Institut Superieur des Materiaux du Mans
Publication of EP1285182A1 publication Critical patent/EP1285182A1/en
Withdrawn legal-status Critical Current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

Definitions

  • the present invention relates to a vibratory wave damping device of variable amplitude or not and an element, in particular a construction element, incorporating such a device.
  • shock absorbers formed of elastic blocks, such as rubber blocks, or in elastic synthetic material called “silent-blocks", capable of separating or isolating the vibrating element from its support or, conversely, the element carried from its vibrating support.
  • the major drawback of these devices is linked to their lack of resistance over time and to their low mechanical rigidity which prevent them from being used as a rigid support structure.
  • the connections between the vibrating structure and its environment, in particular a fixed support must have a high rigidity.
  • the filtering capacities of such devices under heavy load are low.
  • Another solution consists in attenuating the emission of vibrations by a device incorporated in parallel with the vibrating structure.
  • This technique allows extremely high intrinsic damping of the structure under low load.
  • An exemplary embodiment of such a structure is described in particular in the international application. O / 97.11451.
  • such structures cannot be used as an element of interposition between vibrating structure and support.
  • such structures are only effective in the case of vibrations normal to the emissive walls.
  • there is another type of damper in which the viscoelastic material is replaced by a suitable geometry in which a liquid flows. This is the case of the damping device described in patent US-A-5,054,753 in which the liquid can compress a spring. Again, the rigidity following a component parallel to the vibratory wave applied to the incident surface of the structure is low and the deformations of this structure uncontrollable.
  • An object of the present invention is to provide a vibration wave damping device, the design of which makes it possible to be interposed between the vibrating structure and the support, ensuring precise maintenance in position of the vibrating structure due to the rigidity of the damping device while ensuring high vibration filtration power.
  • Another object of the present invention is to provide a vibration wave damping device having the advantages of a traditional rubber damping block in terms of absorption of the filtrations while preserving an extremely high rigidity.
  • the subject of the invention is a vibratory wave damping device of variable or not amplitude, intended in particular to be interposed between a vibrating structure and a fixed support structure, characterized in that it is in the form of '' a beam or a section of rigid beam in the axis of the neutral fiber and having, between an incident surface and a radiating surface, rigid connecting walls shaped to present by geometrical construction points or zones of localized geometric weakness ensuring maintenance of the rigidity of said walls in one axis of the neutral fiber while allowing deformation of said walls in two opposite directions under the effect of the vibratory wave applied to the incident surface, said connecting walls urging during their deformation at least a damping element, preferably housed inside the beam or the edge of the beam.
  • this damping device can be interposed between a vibrating structure and a support, ensuring precise maintenance in position of the vibrating structure due to its rigidity, while guaranteeing a high filtering power of vibrations between structure. vibrating and support.
  • Such a damping device has a structure capable of associating a rigid behavior in dynamics and in static with a viscoelastic behavior in precise fields of low frequencies.
  • Another subject of the invention is an element, in particular a construction element, of the type consisting of a network of elementary meshes, characterized in that each elementary mesh is constituted by a damping device of the preceding type.
  • Examples of embodiments include cushioning floors or the like.
  • Figure 1 shows a schematic sectional view of a device according to the invention
  • Figures 2 to 4 show schematic sectional views corresponding to alternative embodiments of the damping device shown in Figure 1.
  • the vibration damping device of variable or non-variable amplitude, object of the invention is more particularly intended to be disposed between a vibrating structure and a support of said structure. It can therefore be used as a replacement for elastic shock-absorbing blocks used in particular in the naval, aeronautical, space, automobile and railway industries.
  • This device is in the form of a beam 1 or a slice of beam 1 rigid in the axis of the neutral fiber.
  • this structure could be made of metallic, polymer and composite materials.
  • This beam 1 or slice of the beam can be hollow or solid and produced symmetrically or not.
  • This beam or slice of beam also has, between an incident surface 2 and a radiating surface 3, connecting walls 4.
  • These connecting walls 4 rigid in the axis of the neutral fiber to give the device its rigidity, are shaped to be, under the effect of a vibrating o wave, deformable in two opposite directions shown in Dl in the figures.
  • the connecting walls 4 have points or zones 7 of geometrically localized rigid weaknesses ensuring the rigidity of said walls in the neutral fiber axis while allowing deformation along Dl.
  • these connecting walls 4 affect the shape of dihedrons, the edge of the dihedron constituting by construction the zone 7 of weakness, this edge kept rigid along the axis of the neutral fiber allowing deformation of the following dihedron a direction D1 perpendicular to the direction of the vibratory wave o applied to the incident surface.
  • the lateral connecting walls 4 deform in a direction substantially parallel to the incident surface 2. The deformation of the lateral walls 4 due to the construction and the geometric shape of these walls 4 and the presence of the zones 7 of weakness makes it possible to have non-randomly deformable walls while maintaining rigidity along the axis of the neutral fiber.
  • this vibratory wave o can emanate in particular from any vibrating structure, such as a machine tool or the like.
  • the deformations of the connecting walls 4, under the effect of this vibrational wave o will be micro-displacements between the fraction of micron and the meter due to the rigidity of the structure which may be included in the range [1,000 - 200,000] N / mm.
  • At least one component of the deformation 1 of the walls 4 connecting the beam 1 is perpendicular to the direction of the vibratory wave o applied to the incident surface 2.
  • these connecting walls 4 preferably stress in shearing, during their deformation, at least one damping element 5.
  • This damping element 5 is preferably housed inside the beam 1 or the edge of the beam 1.
  • At least one damping element 5 is disposed between the connecting walls 4 and connects the latter between them.
  • At least one damping element 5 constitutes the connection, in particular the joint plane, between two partitions, preferably overlapping, coming from the connecting walls 4 of the beam 1.
  • At least one damping element 5 is disposed between incident surface 2 and radiating surface
  • the damping element 5 can constitute the connection, in particular the joint plane, between two partitions, preferably overlapping, originating from the incident 2 and radiating 3 surfaces.
  • connecting wall 4, incident 2 and radiating 3 surfaces and damping element 5 can define in section two open polygons joined by one of their sides to form in the assembled state a closed structure as shown in Figures 1, 2 and 4
  • connecting wall 4, incident 2 and radiating 3 surfaces and damping element 5 define two open polygons joined by their small base (FIG. 2) or by their large base (FIGS. 1 and 4). for ⁇ form when assembled a closed structure.
  • each elementary mesh is constituted by a damping device of the aforementioned type.
  • the damper element can also affect a large number of shapes.
  • this damping element consists of a viscoelastic material, such as a polymer based on acrylic or natural or synthetic elastomers, based on silicones, phosphazenes.
  • this viscoelastic element is used as a joint plane between two overlapping partitions 6 coming from the connecting walls 4, the viscoelastic material is subjected essentially to shearing forces by the deformation of the beam or the edge of the beam.
  • the damping element could also consist of an oleo-pneumatic member or a pneumatic member without departing from the scope of the invention.
  • the beam 1 or rigid beam section 1 has been shown hollow. However, it could be filled with a viscoelastic material or any other damping device. Similarly, the section of this beam can be arbitrary from the moment when it has rigid deformable connecting walls under the effect of a vibrating wave applied to the incident surface of said beam as illustrated in all the figures.
  • the beam 1 is a symmetrical structure in which the connecting walls are geometrically opposite walls.
  • symmetry is not a mandatory feature of the invention.
  • This damping device can be used in particular as an interposition element between a vibrating structure (not shown) and a support, said support having been shown in the figures by hatching.
  • the applications of this device are numerous, in particular in the automotive field in place of or as a complement to rubber blocks and shock absorbers, in the naval field as a support or structure link in vibration (engine bridges, propeller shaft) in the field rail as support for railway sleepers, in rail structures and finally in the field of aviation for any support or rigid link.

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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)
  • Vibration Prevention Devices (AREA)

Abstract

The invention concerns a variable or non-variable amplitude vibrating wave damping device. Said device is characterised in that it is in the form of a rigid beam (1) or beam section (1) in the axis of the neutral fibre and having, between an incident surface (2) and a radiating surface (3), rigidly linking walls (4) deformable by geometric construction along two opposite directions under the effect of the vibrating wave (o) applied to the incident surface (2), said linking walls (4) stressing as they are deformed at least a damping element (5), preferably housed inside the beam (1) or the beam section (1).

Description

Dispositif amortisseur d'onde vibratoire d'amplitude variable ou nonVibration wave damping device of variable or non-variable amplitude
La présente invention concerne un dispositif amortisseur d'onde vibratoire d'amplitude variable ou non ainsi qu'un élément, en particulier un élément de construction, incorporant un tel dispositif.The present invention relates to a vibratory wave damping device of variable amplitude or not and an element, in particular a construction element, incorporating such a device.
Lorsqu'une paroi est soit soumise à une onde de pression incidente, soit mise en vibration par des moyens mécaniques, l'onde de pression incidente et/ou les vibrations se transmettent à travers la structure du matériau depuis la surface incidente jusqu'à la surface rayonnante. De manière analogue, lorsqu'une structure génère des vibrations, ces vibrations sont émises par les liaisons aux structures environnantes. Ces ondes transmises peuvent s ' avérer gênantes et être génératrices de vieillissement prématuré.When a wall is either subjected to an incident pressure wave or is vibrated by mechanical means, the incident pressure wave and / or vibrations are transmitted through the structure of the material from the incident surface to the radiant surface. Similarly, when a structure generates vibrations, these vibrations are emitted by connections to surrounding structures. These transmitted waves can be bothersome and cause premature aging.
De nombreux dispositifs ont donc été développés à ce jour pour réduire, voire éliminer les ondes transmises de manière à éviter à un dispositif vibrant de générer une onde vibro-acoustique dans le milieu qui l'entoure, en particulier par la liaison du dispositif vibrant aux structures environnantes . Pour ainsi diminuer l'énergie vibratoire transmise par une paroi ou par une structure vibrante à son support, plusieurs solutions ont été développées à ce jour.Many devices have therefore been developed to date to reduce or even eliminate the transmitted waves so as to prevent a vibrating device from generating a vibro-acoustic wave in the medium which surrounds it, in particular by connecting the vibrating device to the surrounding structures. To reduce the vibrational energy transmitted by a wall or by a vibrating structure to its support, several solutions have been developed to date.
Certaines solutions consistent à utiliser des amortisseurs formés de blocs élastiques, tels que des blocs caoutchoucs, ou en matière de synthèse élastique dits "silent-blocks" , aptes à séparer ou isoler l'élément en vibration de son support ou, inversement, l'élément porté de son support en vibration. L'inconvénient majeur de ces dispositifs est lié à leur absence de tenue dans le temps et à leur faible rigidité mécanique qui empêchent de les utiliser en tant que structure porteuse rigide. Or, dans certains cas, les liaisons entre la structure vibrante et son environnement, en particulier un support fixe, doivent posséder une rigidité importante. Par ailleurs, les capacités de filtrage de tels dispositifs sous forte charge sont faibles. En effet, bien que des tentatives de rigidification des blocs caoutchoucs aient été imaginées comme l'illustre le brevet FR-A-0.904.850, ces solutions ne donnent pas satisfaction car les parois latérales du bloc sont constituées de caoutchouc se déformant de manière aléatoire et amenant à la formation de parois latérales non rigides. Il en est de même dans la solution décrite dans le brevet US-A-3.575.403 dans lequel la structure est constituée d'emplacements élastomères en sandwich entre des surfaces rigides . La présence d ' élastomères engendre la formation de parois latérales déformables et non rigides. Ainsi, lors d'une charge exercée à la surface supérieure de la structure, celle-ci se déforme de manière non linéaire, ce qui a pour conséquence un manque de fiabilité en charge dû au manque de rigidité verticale.Some solutions consist in using shock absorbers formed of elastic blocks, such as rubber blocks, or in elastic synthetic material called "silent-blocks", capable of separating or isolating the vibrating element from its support or, conversely, the element carried from its vibrating support. The major drawback of these devices is linked to their lack of resistance over time and to their low mechanical rigidity which prevent them from being used as a rigid support structure. However, in certain cases, the connections between the vibrating structure and its environment, in particular a fixed support, must have a high rigidity. Furthermore, the filtering capacities of such devices under heavy load are low. Indeed, although attempts to stiffen the rubber blocks have been imagined as illustrated by patent FR-A-0,904,850, these solutions are not satisfactory because the side walls of the block are made of rubber deforming randomly and leading to the formation of non-rigid side walls. It is the same in the solution described in US-A-3,575,403 in which the structure consists of elastomeric locations sandwiched between rigid surfaces. The presence of elastomers results in the formation of deformable and non-rigid side walls. Thus, during a load exerted on the upper surface of the structure, the latter deforms in a non-linear manner, which results in a lack of reliability in load due to the lack of vertical rigidity.
Une autre solution consiste à atténuer l'émission de vibrations par un dispositif incorporé en parallèle à la structure vibrante. Cette technique permet un amortissement intrinsèque de la structure extrêmement élevé sous charge faible. Un exemple de réalisation d'une telle structure est notamment décrit dans la demande internationale O/97.11451. De telles structures ne peuvent toutefois pas être utilisées en tant qu'élément d'interposition entre structure vibrante et support. Par ailleurs, de telles structures ne sont efficaces que dans le cas de vibrations normales aux parois émissives. Il existe enfin un autre type d'amortisseur dans lequel le matériau viscoélastique est remplacé par une géométrie adaptée dans laquelle flue un liquide. Tel est le cas du dispositif amortisseur décrit dans le brevet US-A-5.054.753 dans lequel le liquide peut mettre en compression un ressort. A nouveau, la rigidité suivant une composante parallèle à l'onde vibratoire appliquée à la surface incidente de la structure est faible et les déformations de cette structure incontrôlables.Another solution consists in attenuating the emission of vibrations by a device incorporated in parallel with the vibrating structure. This technique allows extremely high intrinsic damping of the structure under low load. An exemplary embodiment of such a structure is described in particular in the international application. O / 97.11451. However, such structures cannot be used as an element of interposition between vibrating structure and support. Furthermore, such structures are only effective in the case of vibrations normal to the emissive walls. Finally, there is another type of damper in which the viscoelastic material is replaced by a suitable geometry in which a liquid flows. This is the case of the damping device described in patent US-A-5,054,753 in which the liquid can compress a spring. Again, the rigidity following a component parallel to the vibratory wave applied to the incident surface of the structure is low and the deformations of this structure uncontrollable.
Un but de la présente invention est de proposer un dispositif amortisseur d'onde vibratoire dont la conception permet d'être interposé entre structure vibrante et support en garantissant un maintien précis en position de la structure vibrante du fait de la rigidité du dispositif amortisseur tout en assurant un haut pouvoir de filtration des vibrations.An object of the present invention is to provide a vibration wave damping device, the design of which makes it possible to be interposed between the vibrating structure and the support, ensuring precise maintenance in position of the vibrating structure due to the rigidity of the damping device while ensuring high vibration filtration power.
Un autre but de la présente invention est de proposer un dispositif amortisseur d'onde vibratoire présentant les avantages d'un bloc amortisseur caoutchouc traditionnel en terme d'absorption des filtrations tout en préservant une rigidité extrêmement importante.Another object of the present invention is to provide a vibration wave damping device having the advantages of a traditional rubber damping block in terms of absorption of the filtrations while preserving an extremely high rigidity.
A cet effet, l'invention a pour objet un dispositif amortisseur d'onde vibratoire d'amplitude variable ou non, destiné notamment à être interposé entre une structure vibrante et une structure fixe support, caractérisé en ce qu'il se présente sous forme d'une poutre ou d'une tranche de poutre rigide dans 1 ' axe de la fibre neutre et présentant, entre une surface incidente et une surface rayonnante, des parois de liaison rigides conformées pour présenter par construction géométrique des points ou zones de faiblesse géométrique localisées assurant un maintien de la rigidité desdites parois dans 1 ' axe de la fibre neutre tout en autorisant une déformation desdites parois suivant deux directions opposées sous l'effet de l'onde vibratoire appliquée à la surface incidente, lesdites parois de liaison sollicitant au cours de leur déformation au moins un élément amortisseur, de préférence logé à l'intérieur de la poutre ou de la tranche de poutre.To this end, the subject of the invention is a vibratory wave damping device of variable or not amplitude, intended in particular to be interposed between a vibrating structure and a fixed support structure, characterized in that it is in the form of '' a beam or a section of rigid beam in the axis of the neutral fiber and having, between an incident surface and a radiating surface, rigid connecting walls shaped to present by geometrical construction points or zones of localized geometric weakness ensuring maintenance of the rigidity of said walls in one axis of the neutral fiber while allowing deformation of said walls in two opposite directions under the effect of the vibratory wave applied to the incident surface, said connecting walls urging during their deformation at least a damping element, preferably housed inside the beam or the edge of the beam.
Grâce à la conception de ce dispositif amortisseur, ce dernier peut être interposé entre une structure vibrante et un support en assurant un maintien précis en position de la structure vibrante du fait de sa rigidité, tout en garantissant un haut pouvoir de filtration des vibrations entre structure vibrante et support.Thanks to the design of this damping device, the latter can be interposed between a vibrating structure and a support, ensuring precise maintenance in position of the vibrating structure due to its rigidity, while guaranteeing a high filtering power of vibrations between structure. vibrating and support.
Un tel dispositif amortisseur présente une structure capable d'associer un comportement rigide en dynamique et en statique à un comportement viscoélastique dans des domaines précis de basses fréquences.Such a damping device has a structure capable of associating a rigid behavior in dynamics and in static with a viscoelastic behavior in precise fields of low frequencies.
L'invention a encore pour objet un élément, en particulier élément de construction, du type constitué d'un réseau de mailles élémentaires, caractérisé en ce que chaque maille élémentaire est constituée par un dispositif amortisseur du type précédent.Another subject of the invention is an element, in particular a construction element, of the type consisting of a network of elementary meshes, characterized in that each elementary mesh is constituted by a damping device of the preceding type.
A titre d'exemples de réalisation, on pourra citer des planchers amortissants ou similaires.Examples of embodiments include cushioning floors or the like.
L'invention sera bien comprise à la lecture de la description suivante d'exemples de réalisation, en référence aux dessins annexés dans lesquels :The invention will be clearly understood on reading the following description of exemplary embodiments, with reference to the appended drawings in which:
la figure 1 représente une vue schématique en coupe d'un dispositif conforme à l'invention ;Figure 1 shows a schematic sectional view of a device according to the invention;
les figures 2 à 4 représentent des vues schématiques en coupe correspondant à des variantes de réalisation du dispositif amortisseur représenté à la figure 1.Figures 2 to 4 show schematic sectional views corresponding to alternative embodiments of the damping device shown in Figure 1.
Comme cela a été mentionné ci-dessus, le dispositif amortisseur d'onde vibratoire d'amplitude variable ou non, objet de l'invention, est plus particulièrement destiné à être disposé entre une structure vibrante et un support de ladite structure. Il peut donc être utilisé en substitution de blocs amortisseurs élastiques utilisés notamment dans des industries navale, aéronautique, spatiale, automobile, ferroviaire. Ce dispositif se présente sous forme d'une poutre 1 ou d'une tranche de poutre 1 rigide dans l'axe de la fibre neutre. A titre d'exemple, cette structure pourra être réalisée en des matériaux métalliques, polymères et composites.As mentioned above, the vibration damping device of variable or non-variable amplitude, object of the invention, is more particularly intended to be disposed between a vibrating structure and a support of said structure. It can therefore be used as a replacement for elastic shock-absorbing blocks used in particular in the naval, aeronautical, space, automobile and railway industries. This device is in the form of a beam 1 or a slice of beam 1 rigid in the axis of the neutral fiber. By way of example, this structure could be made of metallic, polymer and composite materials.
Cette poutre 1 ou tranche de poutre peut être creuse ou pleine et réalisée de manière symétrique ou non. Cette poutre ou tranche de poutre présente encore, entre une surface incidente 2 et une surface rayonnante 3, des parois 4 de liaison. Ces parois 4 de liaison, rigides dans l'axe de la fibre neutre pour conférer au dispositif sa rigidité, sont conformées pour être, sous l'effet d'une onde o vibratoire, déformables suivant deux directions opposées représentées en Dl aux figures. A cet effet, les parois 4 de liaison présentent des points ou zones 7 de faiblesse rigides géométriquement localisées assurant un maintien de la rigidité desdites parois dans l'axe fibre neutre tout en autorisant une déformation suivant Dl. Ainsi, dans certains exemples représentés, ces parois 4 de liaison affectent la forme de dièdres, l'arête du dièdre constituant par construction la zone 7 de faiblesse, cette arête maintenue rigide suivant l'axe de la fibre neutre autorisant une déformation du dièdre suivant une direction Dl perpendiculaire a la direction de l'onde o vibratoire appliquée sur la surface incidente. En d'autres termes, les parois 4 latérales de liaison se déforment suivant une direction sensiblement parallèle à la surface incidente 2. La déformation des parois 4 latérales due à la construction et à la forme géométrique de ces parois 4 et à la présence des zones 7 de faiblesse permet de disposer de parois déformables de manière non aléatoire tout en maintenant une rigidité suivant 1 ' axe de la fibre neutre.This beam 1 or slice of the beam can be hollow or solid and produced symmetrically or not. This beam or slice of beam also has, between an incident surface 2 and a radiating surface 3, connecting walls 4. These connecting walls 4, rigid in the axis of the neutral fiber to give the device its rigidity, are shaped to be, under the effect of a vibrating o wave, deformable in two opposite directions shown in Dl in the figures. For this purpose, the connecting walls 4 have points or zones 7 of geometrically localized rigid weaknesses ensuring the rigidity of said walls in the neutral fiber axis while allowing deformation along Dl. Thus, in certain examples shown, these connecting walls 4 affect the shape of dihedrons, the edge of the dihedron constituting by construction the zone 7 of weakness, this edge kept rigid along the axis of the neutral fiber allowing deformation of the following dihedron a direction D1 perpendicular to the direction of the vibratory wave o applied to the incident surface. In other words, the lateral connecting walls 4 deform in a direction substantially parallel to the incident surface 2. The deformation of the lateral walls 4 due to the construction and the geometric shape of these walls 4 and the presence of the zones 7 of weakness makes it possible to have non-randomly deformable walls while maintaining rigidity along the axis of the neutral fiber.
Appliquée à la surface incidente 2, cette onde o vibratoire peut émaner notamment d'une structure vibrante quelconque, telle qu'une machine outil ou autre. Les déformations des parois 4 de liaison, sous l'effet de cette onde o vibratoire seront des micro-déplacements compris entre la fraction de micron et le mètre en raison de la rigidité de la structure qui pourra être comprise dans la plage [1 000 - 200 000] N/mm.Applied to the incident surface 2, this vibratory wave o can emanate in particular from any vibrating structure, such as a machine tool or the like. The deformations of the connecting walls 4, under the effect of this vibrational wave o will be micro-displacements between the fraction of micron and the meter due to the rigidity of the structure which may be included in the range [1,000 - 200,000] N / mm.
Pour obtenir une efficacité maximale en termes de filtrage, au moins une composante de la déformation 1 des parois 4 de liaison de la poutre 1 est perpendiculaire à la direction de l'onde o vibratoire appliquée à la surface incidente 2.To obtain maximum efficiency in terms of filtering, at least one component of the deformation 1 of the walls 4 connecting the beam 1 is perpendicular to the direction of the vibratory wave o applied to the incident surface 2.
De manière caractéristique à l'invention, ces parois 4 de liaison sollicitent de préférence en cisaillement, au cours de leur déformation, au moins un élément 5 amortisseur. Cet élément 5 amortisseur est de préférence logé à l'intérieur de la poutre 1 ou de la tranche de poutre 1.Characteristically with the invention, these connecting walls 4 preferably stress in shearing, during their deformation, at least one damping element 5. This damping element 5 is preferably housed inside the beam 1 or the edge of the beam 1.
Dans les exemples représentés aux figures 1 à 3 correspondant à une solution préférée de l'invention, au moins un élément 5 amortisseur est disposé entre les parois 4 de liaison et relie ces dernières entre elles.In the examples shown in Figures 1 to 3 corresponding to a preferred solution of the invention, at least one damping element 5 is disposed between the connecting walls 4 and connects the latter between them.
Dans un mode de réalisation encore particulier, au moins un élément 5 amortisseur constitue la liaison, en particulier le plan de joint, entre deux cloisons, de préférence chevauchantes, issues des parois 4 de liaison de la poutre 1.In a still particular embodiment, at least one damping element 5 constitutes the connection, in particular the joint plane, between two partitions, preferably overlapping, coming from the connecting walls 4 of the beam 1.
Dans un autre mode de réalisation moins efficace et représenté à la figure 4, au moins un élément 5 amortisseur est disposé entre surface incidente 2 et surface rayonnanteIn another less efficient and shown in Figure 4, at least one damping element 5 is disposed between incident surface 2 and radiating surface
3 de la poutre 1. Dans ce cas, à nouveau, l'élément amortisseur 5 peut constituer la liaison, en particulier le plan de joint, entre deux cloisons, de préférence chevauchantes, issues des surfaces incidente 2 et rayonnante 3.3 of the beam 1. In this case, again, the damping element 5 can constitute the connection, in particular the joint plane, between two partitions, preferably overlapping, originating from the incident 2 and radiating 3 surfaces.
En fonction de son positionnement et de la conception géométrique des parois 4 de liaison, l'élément 5 amortisseur peut être soumis à des forces de cisaillement ou à des forces de traction ou de compression. La soumission à des forces de cisaillement est une solution préférée comme 1 ' illustrent les figures car elle permet un filtrage plus important. De manière analogue, l'ensemble de la poutre 1 peut affecter un grand nombre de formes. Ainsi, paroi 4 de liaison, surfaces incidente 2 et rayonnante 3 et élément 5 amortisseur peuvent définir en coupe deux polygones ouverts accolés par un de leurs côtés pour former à l'état assemblé une structure fermée comme le montrent les figures 1, 2 et 4. Dans l'exemple de réalisation de ces figures, paroi 4 de liaison, surfaces incidente 2 et rayonnante 3 et élément 5 amortisseur définissent deux polygones ouverts accolés par leur petite base (figure 2) ou par leur grande base (figures 1 et 4) pour^ former à l'état assemblé une structure fermée.Depending on its positioning and the geometric design of the connecting walls 4, the damping element 5 may be subjected to shear forces or to tensile or compressive forces. Submission to shear forces is a preferred solution as illustrated by the figures because it allows more filtering. Similarly, the entire beam 1 can have a large number of shapes. Thus, connecting wall 4, incident 2 and radiating 3 surfaces and damping element 5 can define in section two open polygons joined by one of their sides to form in the assembled state a closed structure as shown in Figures 1, 2 and 4 In the exemplary embodiment of these figures, connecting wall 4, incident 2 and radiating 3 surfaces and damping element 5 define two open polygons joined by their small base (FIG. 2) or by their large base (FIGS. 1 and 4). for ^ form when assembled a closed structure.
Bien évidemment, cette structure élémentaire peut encore être accolée à d' autres structures pour former par exemple un élément de construction tel qu'un plancher apte à supporter des efforts statiques importants et à filtrer les vibrations générées par les chocs subis. Toute autre application pourra bien évidemment être envisagée sur la base d'un tel assemblage. Dans ce cas, chaque maille élémentaire est constituée par un dispositif amortisseur du type précité.Obviously, this elementary structure can also be added to other structures to form, for example, a building element such as a floor capable of withstanding significant static forces and of filtering the vibrations generated by the shocks undergone. Any other application could obviously be envisaged on the basis of such an assembly. In this case, each elementary mesh is constituted by a damping device of the aforementioned type.
L'élément 5 amortisseur peut également affecter un grand nombre de formes. Dans les exemple de réalisation représentés, cet élément amortisseur est constitué par un matériau viscoélastique, tel qu'un polymère à base d'acrylique ou d' élastomères naturels ou synthétiques, à base de silicones, de phosphazènes.The damper element can also affect a large number of shapes. In the exemplary embodiments shown, this damping element consists of a viscoelastic material, such as a polymer based on acrylic or natural or synthetic elastomers, based on silicones, phosphazenes.
Dans le cas des exemples représentés où cet élément viscoélastique est utilisé comme plan de joint entre deux cloisons 6 chevauchantes issues des parois 4 de liaison, le matériau viscoélastique est soumis essentiellement à des forces de cisaillement par la déformation de la poutre ou de la tranche de poutre. Dans d'autres modes de réalisation, non représentés, l'élément amortisseur pourrait être encore constitué d'un organe oléo-pneumatique ou d'un organe pneumatique sans sortir du cadre de 1 ' invention.In the case of the examples shown where this viscoelastic element is used as a joint plane between two overlapping partitions 6 coming from the connecting walls 4, the viscoelastic material is subjected essentially to shearing forces by the deformation of the beam or the edge of the beam. In other embodiments, not shown, the damping element could also consist of an oleo-pneumatic member or a pneumatic member without departing from the scope of the invention.
Dans tous les exemples représentés aux figures, la poutre 1 ou tranche de poutre 1 rigide a été représentée creuse. Toutefois, elle pourrait être remplie d'un matériau viscoélastique ou de tout autre dispositif amortisseur. De même, la section de cette poutre peut être quelconque à partir du moment où elle présente des parois de liaison rigides déformables sous l'effet d'une onde vibratoire appliquée à la surface incidente de ladite poutre comme l'illustrent toutes les figures.In all the examples shown in the figures, the beam 1 or rigid beam section 1 has been shown hollow. However, it could be filled with a viscoelastic material or any other damping device. Similarly, the section of this beam can be arbitrary from the moment when it has rigid deformable connecting walls under the effect of a vibrating wave applied to the incident surface of said beam as illustrated in all the figures.
Dans les exemples représentés, la poutre 1 est une structure symétrique dans laquelle les parois de liaison sont des parois géométriquement opposées. Toutefois, la symétrie ne constitue par une caractéristique obligatoire de 1 ' invention.In the examples shown, the beam 1 is a symmetrical structure in which the connecting walls are geometrically opposite walls. However, symmetry is not a mandatory feature of the invention.
La fabrication d'un dispositif amortisseur est extrêmement aisée. Ainsi, il suffit, dans les exemples de réalisation représentés aux figures 1 et 2, de disposer de deux polygones ouverts formés respectivement par exemple l'un de la surface incidente, 1 ' autre de la surface rayonnante d'une partie des parois de liaison et d'au moins une cloison issue de la paroi de liaison. Il convient ensuite d'accoler les deux polygones ouverts, en l'occurrence les trapèzes, par un de leur côté d'une part au moyen d'un liaison rigide, d'autre part au moyen de l'élément viscoélastique constitutif de l'élément amortisseur, par exemple simplement par trempage de la structure dans un bain de matériau viscoélastique. Le dispositif amortisseur est alors achevé.The manufacture of a damping device is extremely easy. Thus, in the embodiments shown in FIGS. 1 and 2, it suffices to have two open polygons respectively formed, for example, one of the incident surface, the other of the radiating surface. a part of the connecting walls and at least one partition coming from the connecting wall. It is then necessary to join the two open polygons, in this case the trapezoids, by one on their side on the one hand by means of a rigid connection, on the other hand by means of the viscoelastic element constituting the damping element, for example simply by soaking the structure in a bath of viscoelastic material. The damping device is then completed.
Ce dispositif amortisseur pourra être utilisé notamment comme élément d'interposition entre une structure vibrante (non représentée) et un support, ledit support ayant été représenté aux figures par des hachures. Les applications de ce dispositif sont nombreuses en particulier dans le domaine automobile en lieu et place ou complément des blocs caoutchouc et des amortisseurs, dans le domaine naval comme support ou lien de structure en vibration (ponts moteurs, arbre d'hélice) dans le domaine ferroviaire comme support de traverses de voies de chemin de fer, dans les structures de rail et enfin dans le domaine de l'aviation pour tout support ou lien rigide. This damping device can be used in particular as an interposition element between a vibrating structure (not shown) and a support, said support having been shown in the figures by hatching. The applications of this device are numerous, in particular in the automotive field in place of or as a complement to rubber blocks and shock absorbers, in the naval field as a support or structure link in vibration (engine bridges, propeller shaft) in the field rail as support for railway sleepers, in rail structures and finally in the field of aviation for any support or rigid link.

Claims

REVENDICATIONS
1. Dispositif amortisseur d'onde vibratoire d'amplitude variable ou non, destiné notamment à être interposé entre une structure vibrante et une structure fixe support, caractérisé en ce qu'il se présente sous forme d'une poutre (1) ou d'une tranche de poutre (1) rigide dans l'axe de la fibre neutre et présentant, entre une surface incidente (2) et une surface rayonnante ( 3 ) , des parois ( 4 ) de liaison rigides conformées pour présenter par construction géométrique des points (7) ou zones de faiblesse géométrique localisées assurant un maintien de la rigidité desdites parois dans l'axe de la fibre neutre tout en autorisant une déformation desdites parois déformables suivant deux directions (Dl) opposées sous l'effet de l'onde (o) vibratoire appliquée à la surface (2) incidente, lesdites parois (4) de liaison sollicitant au cours de leur déformation au moins un élément (5) amortisseur, de préférence logé à l'intérieur de la poutre (1) ou de la tranche de poutre ( 1 ) .1. Vibration wave damping device of variable or not amplitude, intended in particular to be interposed between a vibrating structure and a fixed support structure, characterized in that it is in the form of a beam (1) or of a slice of beam (1) rigid in the axis of the neutral fiber and having, between an incident surface (2) and a radiating surface (3), rigid connecting walls (4) shaped to present points by geometric construction (7) or zones of localized geometric weakness ensuring the rigidity of said walls in the axis of the neutral fiber while allowing deformation of said deformable walls in two opposite directions (Dl) under the effect of the wave (o ) vibration applied to the incident surface (2), said connecting walls (4) urging during their deformation at least one damping element (5), preferably housed inside the beam (1) or the edge from p addition (1).
2. Dispositif selon la revendication 1, caractérisé en ce qu'au moins un élément (5) amortisseur est disposé entre lesdites parois (4) de liaison et/ou entre surface incidente (2) et surface rayonnante (3) et relie ces dernières entre elles.2. Device according to claim 1, characterized in that at least one damping element (5) is disposed between said connecting walls (4) and / or between incident surface (2) and radiating surface (3) and connects the latter between them.
3. Dispositif selon l'une des revendications 1 et 2, caractérisé en ce qu'au moins une composante de la déformation (Dl) des parois (4) de liaison de la poutre (1) est perpendiculaire à la direction de l'onde (o) vibratoire appliquée à la surface incidente (2).3. Device according to one of claims 1 and 2, characterized in that at least one component of the deformation (Dl) of the walls (4) connecting the beam (1) is perpendicular to the direction of the wave (o) vibration applied to the incident surface (2).
4. Dispositif selon l'une des revendications 1 à 3, caractérisé en ce qu'au moins un élément (5) amortisseur constitue la liaison, en particulier le plan de joint, entre deux cloisons (6), de préférence chevauchantes, issues des parois (4) de liaison ou respectivement des surfaces incidente (2) et rayonnante (3).4. Device according to one of claims 1 to 3, characterized in that at least one damping element (5) constitutes the connection, in particular the joint plane, between two partitions (6), preferably overlapping, from connecting walls (4) or respectively incident (2) and radiant (3) surfaces.
5. Dispositif selon l'une des revendications 1 à 4, caractérisé en ce que parois (4) de liaison, surfaces incidente (2) et rayonnante (3) et élément (5) amortisseur définissent en coupe deux polygones ouverts accolés par un de leurs côtés pour former à l'état assemblé une structure fermée.5. Device according to one of claims 1 to 4, characterized in that walls (4) of connection, incident surface (2) and radiating (3) and element (5) damper define in section two open polygons joined by one of their sides to form in the assembled state a closed structure.
6. Dispositif selon l'une des revendications 1 à 5, caractérisé en ce que parois (4) de liaison, surfaces incidente (2) et rayonnante (3) et élément (5) amortisseur définissent en coupe deux trapèzes ouverts accolés par leur petite base ou leur grande base pour former à l'état assemblé une structure fermée.6. Device according to one of claims 1 to 5, characterized in that walls (4) of connection, incident (2) and radiating (3) and damping element (5) define in section two open trapezoids joined by their small base or their large base to form in the assembled state a closed structure.
7. Dispositif selon l'une des revendications 1 à 6, caractérisé en ce que l'élément (5) amortisseur est soumis essentiellement à des forces de cisaillement par la déformation de la poutre ou de la tranche de poutre.7. Device according to one of claims 1 to 6, characterized in that the damping element (5) is subjected essentially to shear forces by the deformation of the beam or of the beam edge.
8. Dispositif selon l'une des revendications 1 à 7, caractérisé en ce que l'élément amortisseur est un matériau viscoélastique.8. Device according to one of claims 1 to 7, characterized in that the damping element is a viscoelastic material.
9. Dispositif selon l'une des revendications 1 à 6, caractérisé en ce que l'élément amortisseur est un organe oléo-pneumatique ou pneumatique.9. Device according to one of claims 1 to 6, characterized in that the damping element is an oleopneumatic or pneumatic member.
10. Dispositif selon l'une des revendications 1 à 9, caractérisé en ce que la rigidité des parois (4) de liaison est comprise dans la plage [1 000 - 200 000] N/mm.10. Device according to one of claims 1 to 9, characterized in that the rigidity of the walls (4) of connection is included in the range [1,000 - 200,000] N / mm.
11. Elément, en particulier élément de construction, du type constitué d'un réseau de mailles élémentaires, caractérisé en ce que chaque maille élémentaire est constituée par un dispositif amortisseur conforme à l'une des revendications 1 à 10. 11. Element, in particular construction element, of the type consisting of a network of elementary meshes, characterized in that each elementary mesh is constituted by a damping device according to one of claims 1 to 10.
EP01940625A 2000-05-31 2001-05-29 Variable or non-variable amplitude vibrating wave damping device Withdrawn EP1285182A1 (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
FR0007050 2000-05-31
FR0007050A FR2809785B1 (en) 2000-05-31 2000-05-31 VIBRATION WAVE DAMPER DEVICE WITH VARIABLE OR NON-VARIABLE AMPLITUDE
PCT/FR2001/001661 WO2001092754A1 (en) 2000-05-31 2001-05-29 Variable or non-variable amplitude vibrating wave damping device

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EP1285182A1 true EP1285182A1 (en) 2003-02-26

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AU (1) AU2001274144A1 (en)
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WO (1) WO2001092754A1 (en)

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Publication number Priority date Publication date Assignee Title
CN106907418B (en) * 2017-01-20 2019-05-24 上海交通大学 Phonon crystal negative poisson's ratio honeycomb vibration isolation anti-impact device
CN110296172A (en) * 2019-06-17 2019-10-01 江苏科技大学 A kind of vibration isolation anti-impact device and preparation method thereof

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FR904850A (en) * 1943-03-31 1945-11-16 Continental Gummi Werke Ag Metal and rubber shock absorber for elastic seating of combustion engines
US3575403A (en) * 1968-03-21 1971-04-20 Pneumatiques Caoutchouc Mfg Rubber-containing spring means
DE2159391A1 (en) * 1970-12-02 1972-06-29 Abex Corp., New York, N.Y. (V.StA.) Spring device for absorbing and damping shock loads
US4790521A (en) * 1985-10-03 1988-12-13 Nissan Motor Company, Limited Anti-vibration apparatus for mounting a power unit on a supporting body with suppression of vibrations
DE3906466A1 (en) * 1988-05-13 1989-11-23 Polus Michael DAMPING DEVICE FOR SHOCKING LOADS
NL9000294A (en) * 1990-02-07 1991-09-02 Willy Van Goubergen VIBRATION DAMPER.
AT402368B (en) * 1991-11-14 1997-04-25 Franz Scheruebl Ski having a bottom sheet and a top sheet and method for its production
GB2314399A (en) * 1996-06-20 1997-12-24 Rover Group A device for damping the transmission of vibration

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See references of WO0192754A1 *

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AU2001274144A1 (en) 2001-12-11
WO2001092754A1 (en) 2001-12-06
FR2809785B1 (en) 2005-09-23
FR2809785A1 (en) 2001-12-07

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