EP1441327A1 - Structure mécanique présentant une propriété vibratoire modifiable - Google Patents
Structure mécanique présentant une propriété vibratoire modifiable Download PDFInfo
- Publication number
- EP1441327A1 EP1441327A1 EP03293329A EP03293329A EP1441327A1 EP 1441327 A1 EP1441327 A1 EP 1441327A1 EP 03293329 A EP03293329 A EP 03293329A EP 03293329 A EP03293329 A EP 03293329A EP 1441327 A1 EP1441327 A1 EP 1441327A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- flexible
- polymer
- plate
- structure according
- fixed
- 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- Withdrawn
Links
- 229920000642 polymer Polymers 0.000 claims abstract description 15
- 229910052500 inorganic mineral Inorganic materials 0.000 claims abstract description 3
- 239000011707 mineral Substances 0.000 claims abstract description 3
- 239000002245 particle Substances 0.000 claims abstract description 3
- 244000043261 Hevea brasiliensis Species 0.000 claims 1
- 229920003052 natural elastomer Polymers 0.000 claims 1
- 229920001194 natural rubber Polymers 0.000 claims 1
- 229920001296 polysiloxane Polymers 0.000 claims 1
- 229920002635 polyurethane Polymers 0.000 claims 1
- 239000004814 polyurethane Substances 0.000 claims 1
- 229920003051 synthetic elastomer Polymers 0.000 claims 1
- 239000005061 synthetic rubber Substances 0.000 claims 1
- 239000000945 filler Substances 0.000 abstract description 4
- 239000002184 metal Substances 0.000 abstract 1
- 239000002861 polymer material Substances 0.000 abstract 1
- 239000000463 material Substances 0.000 description 7
- 230000009471 action Effects 0.000 description 5
- 230000000694 effects Effects 0.000 description 5
- 229920005570 flexible polymer Polymers 0.000 description 5
- 230000004048 modification Effects 0.000 description 3
- 238000012986 modification Methods 0.000 description 3
- 230000005284 excitation Effects 0.000 description 2
- 230000005855 radiation Effects 0.000 description 2
- 229920000049 Carbon (fiber) Polymers 0.000 description 1
- 230000006978 adaptation Effects 0.000 description 1
- 238000004026 adhesive bonding Methods 0.000 description 1
- 230000003042 antagnostic effect Effects 0.000 description 1
- 230000002238 attenuated effect Effects 0.000 description 1
- 239000004917 carbon fiber Substances 0.000 description 1
- 230000008859 change Effects 0.000 description 1
- 239000003365 glass fiber Substances 0.000 description 1
- 230000006872 improvement Effects 0.000 description 1
- 230000004807 localization Effects 0.000 description 1
- 230000000116 mitigating effect Effects 0.000 description 1
- 239000003607 modifier Substances 0.000 description 1
- 239000012763 reinforcing filler Substances 0.000 description 1
- 230000004044 response Effects 0.000 description 1
- 239000003351 stiffener Substances 0.000 description 1
Images
Classifications
-
- G—PHYSICS
- G10—MUSICAL INSTRUMENTS; ACOUSTICS
- G10K—SOUND-PRODUCING DEVICES; METHODS OR DEVICES FOR PROTECTING AGAINST, OR FOR DAMPING, NOISE OR OTHER ACOUSTIC WAVES IN GENERAL; ACOUSTICS NOT OTHERWISE PROVIDED FOR
- G10K11/00—Methods or devices for transmitting, conducting or directing sound in general; Methods or devices for protecting against, or for damping, noise or other acoustic waves in general
- G10K11/16—Methods or devices for protecting against, or for damping, noise or other acoustic waves in general
- G10K11/172—Methods or devices for protecting against, or for damping, noise or other acoustic waves in general using resonance effects
-
- G—PHYSICS
- G10—MUSICAL INSTRUMENTS; ACOUSTICS
- G10K—SOUND-PRODUCING DEVICES; METHODS OR DEVICES FOR PROTECTING AGAINST, OR FOR DAMPING, NOISE OR OTHER ACOUSTIC WAVES IN GENERAL; ACOUSTICS NOT OTHERWISE PROVIDED FOR
- G10K11/00—Methods or devices for transmitting, conducting or directing sound in general; Methods or devices for protecting against, or for damping, noise or other acoustic waves in general
- G10K11/16—Methods or devices for protecting against, or for damping, noise or other acoustic waves in general
- G10K11/162—Selection of materials
Definitions
- the present invention relates to a mechanical structure of which we use an acoustic property, for example the critical frequency or the response of the structure to a vibration transmitted by a structure carrier.
- the basic idea of the invention is to act only on the mass term while modifying the term related to elasticity, this being obtained using an element made of one material at a time heavy and flexible.
- the invention thus relates to a mechanical structure having at least one vibratory property, characterized in that it has at least one modifier of said vibratory property which is a flexible and heavy polymer comprising for example fillers mass, and which is integral with a region of the structure.
- the flexible polymer advantageously has a modulus of between 10 4 and 10 7 Pa, and preferably between 10 5 and 10 6 Pa.
- the flexible polymer charged by said mass loads advantageously has a density greater than 2 and less than or equal to 10 and preferably between 3 and 10.
- the charges have advantageously a density between 3 and 18 and a dimension between 10 ⁇ and 2000 ⁇
- the structure is characterized in what it is at least partly constituted by a panel of the nest type bee comprising two external plates between which is disposed a network of cells and in that at least some of said cells are filled with a so-called flexible and heavy polymer element.
- the structure is characterized in what it consists of a supporting frame having at least one opening in which a plate is embedded or fixed and in that it has at least one strip or at least one plate of said polymer flexible and heavy which is fixed on at least part of the periphery of at least a so-called plaque.
- at least one flexible polymer plate and heavy can be fixed on a corner of the plate which is embedded or fixed on the supporting frame.
- the structure is characterized in that it has at least one fixing hole formed around a region of the structure and in that it has at least one ring in one said flexible charged polymer integral with the structure and surrounding said hole fixation.
- Figure 1 shows a honeycomb panel ("nida") which has two plates 1 and 2 between which is sandwiched a network 3 of hexagonal cells 4.
- a number of cells have been filled with a polymer very low modulus (for example between 10 4 and 10 7 Pa and preferably between 10 5 and 10 6 Pa) loaded with heavy loads, for example metallic and / or mineral particles of dimensions for example between 0.01 mm and 2 mm.
- the density of the fillers must be greater than that of the fillers (glass or carbon fibers) usually used as mechanical reinforcing fillers for rubber.
- the choice of the number of cells is a parameter allowing adaptation.
- the choice of the location of the cells 4 filled with material 5 allows localization of the effect obtained.
- Figure 2 shows a plate 10 having a hole fixing 11.
- the plate 10 can be a fixing lug of a structure mechanical or more generally a region of a mechanical structure which can be fixed using a fixing hole 11.
- a ring 12 is fixed to the plate 10.
- flexible polymer comprising mass charges so as to surround the fixing hole 11.
- the ring 12 is concentric with the fixing hole fixation 11.
- the effect obtained is a local modification of the impedance mechanical which results in a reflection of the vibratory waves entering the panel by this point.
- the vibrations communicated to the plate 10 by a fastening element 14 are thus attenuated by the ring 12 whose mass makes it possible to adapt the frequency range mitigation.
- the structure shown in Figure 3 has plates 21 which are embedded at their periphery in openings 22 of a frame carrier 23 in lattice.
- the plates 21 are for example panels of fuselage of aircraft embedded between the frames and the rails.
- One or more narrow strips 24 (for example, width 5 to 10 mm and height 2 to 4 mm) made of a heavy and flexible material as defined above are bonded to the periphery of these plates, i.e. in the immediate vicinity of the interface between the plate 21 and the supporting frame 23 on at least part of their periphery.
- the effect obtained is an attenuation of the acoustic radiation generated by the plate when it is transmitted by the supporting structure (figure 4) for example mechanically excited at a point ( Figure 5).
- the attenuation obtained is between 0 dB and 10 dB (at 100 Hz) in the case of Figure 4 and between 0 dB and 9 dB (at 2000 Hz) in the case of the Figure 5.
- At least one corner of the plate 21 can receive a plate in heavy and flexible material glued, fixed for example by gluing.
- Another example of application is that of the modification of the critical acoustic frequency of a panel by locally bonding plates made of a material that is both heavy and flexible.
- This critical frequency depends on the mass and stiffness of the panel. Any action on any of these factors leads to an action on the other whose effect can be antagonistic according to the frequency range.
- the addition of heavy and flexible material plates allows to play on the mass while having a weak action on the stiffness.
- An element made of heavy and flexible material constituted for example by a flexible polymer comprising mass charges is all the more effective that the modulus of elasticity of the polymer is low and that the density of mass loads is higher.
Landscapes
- Physics & Mathematics (AREA)
- Engineering & Computer Science (AREA)
- Acoustics & Sound (AREA)
- Multimedia (AREA)
- Vibration Prevention Devices (AREA)
- Compositions Of Macromolecular Compounds (AREA)
- Laminated Bodies (AREA)
- Soundproofing, Sound Blocking, And Sound Damping (AREA)
Abstract
Description
- les figures 1 à 3 illustrent trois variantes de réalisation de l'invention ;
- et les figures 4 et 5 illustrent l'amélioration acoustique de la structure de la figure 3 dans deux conditions d'excitation.
Claims (8)
- Structure mécanique présentant au moins une propriété vibratoire, caractérisée en ce qu'elle présente au moins un élément (5, 12, 24) modificateur de ladite propriété vibratoire qui est un polymère souple et lourd comportant par exemple des charges massiques, en ce que le polymère souple et lourd présente une densité comprise entre 3 et 10 et en ce que cet élément (5, 12, 24) est solidaire d'une région de la structure.
- Structure selon la revendication 1, caractérisée en ce que ledit polymère présente un module compris entre 104 et 107 Pa.
- Structure selon une des revendications 1 ou 2, caractérisée en ce que le polymère est du polyuréthane, de silicone, du caoutchouc naturel, du caoutchouc synthétique.
- Structure selon une des revendications précédentes, caractérisée en ce qu'elle présente des charges massiques qui sont des particules métalliques et/ou minérales.
- Structure selon une des revendications précédentes, caractérisée en ce qu'elle est au moins en partie constituée par un panneau (1, 2, 3) du type nid d'abeille comprenant deux plaques externes (1, 2) entre lesquelles est disposé un réseau (3) d'alvéoles (4) et en ce qu'au moins certaines desdites alvéoles (4) sont remplies d'un dit élément en polymère souple et lourd.
- Structure selon une des revendications 1 à 4, caractérisée en ce qu'elle est constituée par un cadre porteur (23) présentant au moins une ouverture dans laquelle est encastrée ou fixée une plaque (21) et en ce qu'elle présente au moins une bande ou une plaque (24) en un dit polymère souple et lourd qui est fixée sur au moins une partie du pourtour d'au moins une dite plaque (21) qui est encastrée ou fixée au cadre porteur (23).
- Structure selon la revendications 6, caractérisée en ce qu'elle présente au moins une plaque en un dit polymère souple et lourd sur au moins un coin d'une dite plaque (21) qui est encastrée ou fixée sur le cadre porteur (23).
- Structure selon une des revendications 1 à 4, caractérisée en ce qu'elle présente au moins un trou de fixation (11) ménagé autour d'une région de la structure et en ce qu'elle présente au moins un anneau (12) en un dit polymère souple chargé solidaire de la structure et entourant ledit trou de fixation (11).
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR0300772A FR2850484B1 (fr) | 2003-01-24 | 2003-01-24 | Structure mecanique presentant une propriete vibratoire modifiable |
| FR0300772 | 2003-01-24 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| EP1441327A1 true EP1441327A1 (fr) | 2004-07-28 |
Family
ID=32524999
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| EP03293329A Withdrawn EP1441327A1 (fr) | 2003-01-24 | 2003-12-24 | Structure mécanique présentant une propriété vibratoire modifiable |
Country Status (5)
| Country | Link |
|---|---|
| US (1) | US20040154418A1 (fr) |
| EP (1) | EP1441327A1 (fr) |
| BR (1) | BRPI0400049B1 (fr) |
| CA (1) | CA2454998A1 (fr) |
| FR (1) | FR2850484B1 (fr) |
Families Citing this family (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US9275622B2 (en) | 2011-03-29 | 2016-03-01 | Katholieke Universiteit Leuven | Vibro-acoustic attenuation or reduced energy transmission |
| EP2674091A1 (fr) | 2012-06-13 | 2013-12-18 | Nitto Europe N.V | Amortisseur structurel haute température à base de nid d'abeilles |
Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3644236A (en) * | 1968-02-21 | 1972-02-22 | Bp Chem Int Ltd | Lead filled polyurethane foams |
| GB2070626A (en) * | 1980-03-03 | 1981-09-09 | Toa Nenryo Kogyo Kk | Sound insulating thermoplastic resin compositions |
| WO1990007673A1 (fr) * | 1988-12-30 | 1990-07-12 | Delta Tech Research, Inc. | Systeme amortisseur en materiau visco-elastique |
| FR2660787A1 (fr) * | 1990-04-06 | 1991-10-11 | Technologies Speciales Ingenie | Ecran anechouide. |
| US5222694A (en) * | 1992-08-03 | 1993-06-29 | Atr International, Inc. | Aircraft interior panel noise dampening support brackets |
| US5278219A (en) * | 1988-11-25 | 1994-01-11 | Lilley Martin J | Flexible highly filled compositions |
| US6114652A (en) * | 1998-09-10 | 2000-09-05 | Northrop Grumman Corporation | Method of forming acoustic attenuation chambers using laser processing of multi-layered polymer films |
Family Cites Families (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3515625A (en) * | 1965-04-20 | 1970-06-02 | Steve Sedlak | Composite flexible material containing a high proportion of filler particles |
| US3489242A (en) * | 1969-04-01 | 1970-01-13 | Du Pont | Acoustical panel comprising viscoelastic material with heavy filler particles |
| US4690960A (en) * | 1981-01-14 | 1987-09-01 | Nippon Electric Co., Ltd. | Vibration damping material |
| US4367259A (en) * | 1981-07-27 | 1983-01-04 | W. R. Grace & Co. | Sound deadening material |
| US4667768A (en) * | 1986-05-01 | 1987-05-26 | Lockheed Corporation | Sound absorbing panel |
| US5473122A (en) * | 1993-01-04 | 1995-12-05 | Martin Marietta Corporation | Dual-constrained viscoelastic damping mechanism for structural vibration control |
| FR2850410B1 (fr) * | 2003-01-24 | 2006-02-03 | Hutchinson | Panneau d'isolation acoustique |
-
2003
- 2003-01-24 FR FR0300772A patent/FR2850484B1/fr not_active Expired - Fee Related
- 2003-12-24 EP EP03293329A patent/EP1441327A1/fr not_active Withdrawn
-
2004
- 2004-01-08 CA CA002454998A patent/CA2454998A1/fr not_active Abandoned
- 2004-01-14 US US10/756,992 patent/US20040154418A1/en not_active Abandoned
- 2004-01-16 BR BRPI0400049-8A patent/BRPI0400049B1/pt not_active IP Right Cessation
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3644236A (en) * | 1968-02-21 | 1972-02-22 | Bp Chem Int Ltd | Lead filled polyurethane foams |
| GB2070626A (en) * | 1980-03-03 | 1981-09-09 | Toa Nenryo Kogyo Kk | Sound insulating thermoplastic resin compositions |
| US5278219A (en) * | 1988-11-25 | 1994-01-11 | Lilley Martin J | Flexible highly filled compositions |
| WO1990007673A1 (fr) * | 1988-12-30 | 1990-07-12 | Delta Tech Research, Inc. | Systeme amortisseur en materiau visco-elastique |
| FR2660787A1 (fr) * | 1990-04-06 | 1991-10-11 | Technologies Speciales Ingenie | Ecran anechouide. |
| US5222694A (en) * | 1992-08-03 | 1993-06-29 | Atr International, Inc. | Aircraft interior panel noise dampening support brackets |
| US6114652A (en) * | 1998-09-10 | 2000-09-05 | Northrop Grumman Corporation | Method of forming acoustic attenuation chambers using laser processing of multi-layered polymer films |
Also Published As
| Publication number | Publication date |
|---|---|
| FR2850484A1 (fr) | 2004-07-30 |
| BRPI0400049B1 (pt) | 2014-08-26 |
| CA2454998A1 (fr) | 2004-07-24 |
| US20040154418A1 (en) | 2004-08-12 |
| FR2850484B1 (fr) | 2005-12-09 |
| BRPI0400049A (pt) | 2004-09-14 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PUAI | Public reference made under article 153(3) epc to a published international application that has entered the european phase |
Free format text: ORIGINAL CODE: 0009012 |
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| AK | Designated contracting states |
Kind code of ref document: A1 Designated state(s): AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HU IE IT LI LU MC NL PT RO SE SI SK TR |
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| AX | Request for extension of the european patent |
Extension state: AL LT LV MK |
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| 17P | Request for examination filed |
Effective date: 20040810 |
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| AKX | Designation fees paid |
Designated state(s): DE ES FR GB IT SE |
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| 17Q | First examination report despatched |
Effective date: 20161121 |
|
| STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: THE APPLICATION IS DEEMED TO BE WITHDRAWN |
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| 18D | Application deemed to be withdrawn |
Effective date: 20181030 |