WO1992020523A1 - Sound-damping sandwich material and a method for its manufacture - Google Patents
Sound-damping sandwich material and a method for its manufacture Download PDFInfo
- Publication number
- WO1992020523A1 WO1992020523A1 PCT/SE1992/000337 SE9200337W WO9220523A1 WO 1992020523 A1 WO1992020523 A1 WO 1992020523A1 SE 9200337 W SE9200337 W SE 9200337W WO 9220523 A1 WO9220523 A1 WO 9220523A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- gaps
- sandwich structure
- cut
- core
- structure according
- Prior art date
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B5/00—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts
- B32B5/18—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by features of a layer of foamed material
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B3/00—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar form; Layered products having particular features of form
- B32B3/10—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar form; Layered products having particular features of form characterised by a discontinuous layer, i.e. formed of separate pieces of material
- B32B3/18—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar form; Layered products having particular features of form characterised by a discontinuous layer, i.e. formed of separate pieces of material characterised by an internal layer formed of separate pieces of material which are juxtaposed side-by-side
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B38/00—Ancillary operations in connection with laminating processes
- B32B38/18—Handling of layers or the laminate
- B32B38/1858—Handling of layers or the laminate using vacuum
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B7/00—Layered products characterised by the relation between layers; Layered products characterised by the relative orientation of features between layers, or by the relative values of a measurable parameter between layers, i.e. products comprising layers having different physical, chemical or physicochemical properties; Layered products characterised by the interconnection of layers
- B32B7/04—Interconnection of layers
- B32B7/12—Interconnection of layers using interposed adhesives or interposed materials with bonding properties
-
- E—FIXED CONSTRUCTIONS
- E04—BUILDING
- E04C—STRUCTURAL ELEMENTS; BUILDING MATERIALS
- E04C2/00—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels
- E04C2/02—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by specified materials
- E04C2/10—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by specified materials of wood, fibres, chips, vegetable stems, or the like; of plastics; of foamed products
- E04C2/20—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by specified materials of wood, fibres, chips, vegetable stems, or the like; of plastics; of foamed products of plastics
- E04C2/205—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by specified materials of wood, fibres, chips, vegetable stems, or the like; of plastics; of foamed products of plastics of foamed plastics, or of plastics and foamed plastics, optionally reinforced
-
- 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
- G10K11/168—Plural layers of different materials, e.g. sandwiches
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2266/00—Composition of foam
- B32B2266/02—Organic
- B32B2266/0214—Materials belonging to B32B27/00
- B32B2266/0221—Vinyl resin
- B32B2266/0235—Vinyl halide, e.g. PVC, PVDC, PVF, PVDF
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2266/00—Composition of foam
- B32B2266/08—Closed cell foam
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2305/00—Condition, form or state of the layers or laminate
- B32B2305/08—Reinforcements
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2307/00—Properties of the layers or laminate
- B32B2307/10—Properties of the layers or laminate having particular acoustical properties
Definitions
- the present invention relates to a sandwich structure which is comprised of a cellular-plastic core sandwiched between two reinforcing layers made, for instance, of metal or of a laminated fibre-glass fabric.
- the core is built-up of individual, cut shapes, preferably disposed in a checkered pattern, wherein the gaps defined by adjacent shapes are filled with a binder.
- the core material is referred to as checkered cut material, although it will be understood that the pattern formed by the cut shapes need not be a checkered pattern.
- Such sandwich structures are known, for instance, from SE-A-89 00 981-5, in which the binder used is comprised of a filler to which small plastic spheres have been added, this filler completely filling the aforesaid gaps and thereby providing a structure of high mechanical strength.
- Checkered cut core material has been used hitherto because of the need to be able to manufacture arched or curved sandwich structures.
- Flat, imperforate sheets are normally used for the manufacture of flat sandwich structures.
- a first object of the present invention is to provide a sandwich structure of the aforedescribed kind which inhibits the occurrence of bodyborne sound in constructions built from such material structures.
- Another object of the present invention is to provide a general sound-damping material, by which is meant a material which can be used for sound insulation purposes between rooms for instance, and which thus dampens air ⁇ borne sound.
- a cellular plas- tic material which is cut into individual shapes, pref ⁇ erably a checkered cut cellar material, in which the gaps defined by mutually adjacent shapes are filled with an elastomeric polymer binder.
- the invention relates to a method of manufacturing such material, in accordance with Claim 7.
- the actual sandwich structure may be either flat or curved or arched, according to the use for which it is intended.
- the inventive materi ⁇ al thus dampens both bodyborne sound and airborne sound.
- the airborne-sound reduction number, or factor, of a panel is, among other things, dependent on the surface weight of the panel, its flexural rigidity, inner losses and frequency.
- One important parameter with regard to the acoustic properties of the panel is the so-called coincidence frequency. This parameter is determined by the surface weight and the flexural rigidity of the panel concerned. A decrease in the flexural rigidity of the panel will result in an increase in the coincidence frequency.
- the reduction number, or factor may be in ⁇ creased for frequencies at and above the coincidence frequency, provided that the inner losses are increased.
- the core of the sandwich structure or panel is cut into separate shapes disposed in a checkered pattern and the gaps between these shapes are filled with a mate- rial of low rigidity, the flexural rigidity of the panel is reduced for higher frequencies. This results in an increase in the coincidence frequency, and the reduction factor is increased at levels beneath coincidence.
- the elastic material present in the gaps will also impair the dynamic coupling between the two laminates which embrace the core, thereby also resulting in some improve ⁇ ment in the reduction factor.
- a vibrating panel or sheet will radiate sound.
- the sound radiating effect of the panel or sheet is contingent on the vibrating velocity of the panel at right angles to the panel surface and also on the acoustic coupling of the panel to the ambient medium, for example ambient air.
- a reduction in the flexural rigidity of the panel or sheet will result in a reduction in the sound radiating ability of the panel. The greater the losses, the lower the panel velocity. Both effects are achieved by filling the gaps in the core with an elastomeric material in accordance with the invention.
- elastomer a material which exhibits rubber ⁇ like, elastic properties.
- a two-component polyurethane material is preferred, although the use of other materials is also conceivable, provided that they are suitable for use from the aspect of manufacture. Examples of such materials include silicones, plasticized epoxy, urethane modified polyester and soft acrylates.
- the rubber-like material used will preferably have a hardness within the range of 10-75, preferably within the range of 20-30 as measured according to Shore D. If the material is too hard, the desired sound-damping effect will not be achieved. If the material is too soft, the mechanical strength is jeopardized. Since corresponding sandwich structures or materials provided with air-filled channels are used at present in many instances, the use of a relatively soft material as a sound-damping means may nevertheless be defended.
- the loss factor of said material is the loss factor of said material.
- the loss factor ⁇ can be under ⁇ stood as being the imaginary part of the E-modulus: where ⁇ is a function of both frequency and temperature and is greatest at the glass temperature of the elasto ⁇ meric material.
- ⁇ is a function of both frequency and temperature and is greatest at the glass temperature of the elasto ⁇ meric material.
- the binder In manufacture, it is preferred to apply surface material to both sides of the cellular plastic core, and then to inject a binder into the still empty gaps defined by adjacent cut shapes in the cellular plastic, so as to fill said gaps with binder.
- the binder must be relatively flowable or liquid when applying the binder and should afford good adhesion after solidifying and preferably exhibit only small shrinkage.
- two shape-cut sheets are joined together by means of an elastomeric material, and the resultant unit is used as a core with elastomer-filled gaps between adjacent shapes, which provides a further improvement.
- Checkered-cut cellular plastic material in which the square shapes are fastened to a thin carrier web is commercially available .
- the core material is produced by fastening a carrier web to a complete cellular plastic sheet, whereafter the checkers or shapes are produced by sawing or milling away interspaces to leave a cut check ⁇ ered web, for instance.
- the interspaces, or gaps between said shapes are then filled with an elastomeric thermosetting resin.
- manufacture can also be carried out in another way, at least in the manufacture of flat sheets, without departing from the concept of the invention.
- a cellular plastic sheet can be divided into long strips and the strips joined to extruded strips of rect ⁇ angular cross-section, to form a new sheet which is then divided into strips with sections extending at angles thereto (preferably 90°) , these strips then being joined to elastomeric strips in a similar way.
- the first men- tioned sheet may, alternatively, be formed by joining cellular plastic sheets and elastomeric sheets to form a sandwich structure from which strips are cut, these strips thus comprising elastomeric strips joined to cellular plastic strips.
- the invention provides a sandwich structure which is effective in dampening sound and from which an effective sound-insulating wall can be constructed, and also exhibit damping properties with regard to the propagation of mechanical waves whose frequencies lie within the audible frequency range.
- Figure 1 is a sectional view of a flat sandwich material
- Figure 2 is a sectional view of a curved sandwich materi ⁇ al;
- Figure 3 is a sound-conducting curve of sandwich material constructed with an uncut cellular plastic core
- Figures 4-8 are curves which illustrate the conductance of sound at different frequencies, measured logarith- mically and drawn relative to the curve used as standard in Figure 1;
- Figure 9 illustrates damping of airborne sound in three different materials.
- Figures 1 and 2 are sectional views of two sandwich materials or structures, the only difference between these structures being that one is curved and may be double-curved (not shown) , while the other is flat.
- a checkered-cut core 2 of cellular plastic material is placed between two reinforcing layers 1 which are glued to the core material 2 by glue joints 3.
- the core mate ⁇ rial has been cut into shaped pieces to present gaps or channels which are filled with an elastomeric material 4.
- the gaps in the case of a flat sandwich structure are straight, while the gaps in the curved sandwich structure are wedge-shaped, due to bending of the structure.
- a thin intermediate layer 5 is often included on one side of the sandwich structure. The function of this interme ⁇ diate layer is to hold the cut shapes together, subse- quent to forming the core, until the core can be embodied in the sandwich structure.
- the core carrier layer may comprise an open-mesh fabric, non-woven fabric or the like, such that the carrier layer will not prevent the glue layer 3 from holding the core material 2 and the reinforcing layers 1 together.
- the reinforcing layers, or strength lay ⁇ ers, of the sandwich structure will normally comprise a fibre-glass fabric and polyester laminate, although a metal layer, such as an aluminium, aluminium-alloy or steel layer may often be used.
- a sandwich structure of this kind is normally manufac ⁇ tured by first fastening the reinforcement layers 1 onto the core material 2, by glue joints 3, while leaving the gaps 4 between the shaped pieces of core material 2 essentially empty.
- a lowly viscous elastomeric material is then injected into the gaps, suitably starting from the lowest point of the sandwich structure, particularly through holes formed at the points of intersection of the gaps 4, said openings being disposed at the top of the structure and the elastomeric material being caused to displace air from the gaps as it flows therethrough and also to fill said gaps, by delivering the elastomeric material under pressure and/or under the influence of a vacuum generated at the openings provided at the top of the structure.
- a combination of these latter alterna ⁇ tives is often to be preferred, since an excessively high pressure may cause the joints between reinforcement layers and core material to rupture.
- a sandwich structure was manufactured as a reference structure and was comprised of a core made of PVC-cellu- lar plastic with closed cells, our product DIVINYCELL®, quality H60 (60 kg/m 2) , thickness 20 mm, not checkered- cut.
- the reinforcement layers were comprised of 1 mm fibre-glass fabric and polyester resin laminates. The sheet weighed 6.8 kg per square meter.
- Example 2 There was manufactured a sample structure similar to the structure of Example 1, but with the exception that the core comprised a checkered-cut sheet having square shapes with side measurements of 39 mm and surrounded by gaps of
- the sheet had a square meter weight 9.17 kg.
- Example 2 There was manufactured a structure similar to the struc- ture of Example 2, but with the exception that two checkered-cut sheets having a thickness of 10 mm were glued together with polyurethane glue. The sheet weighed 7.17 kg per square meter.
- a sandwich structure was manufactured similar to the structure according to Example 1, but with the exception that instead of a non-cut sheet of 20 mm thickness, there were used instead two sheets each having a thickness of 10 mm and joined together by a layer of the same poly- urethane glue as that used in Examples 2-5. Thus, this sandwich structure had only one damping layer parallel with the sheet.
- Figure 3 is a sound conductivity curve with logarithmic dB-scale for damping in dB/m, plotted or recorded, between 50 Hz and 4000 Hz.
- This curve is representative of known sandwich materials having a hard foamed-plastic core with fibre glass layers laminated thereon, such as those structures used at present in the manufacture of boats and vehicles. This curve was therefore taken as a reference and the sound conductivity of the structures produced in accordance with the other Examples were related to this reference as a standard, in that the zero-line in Figures 4-8 cor- responds to the result achieved with Example 1, taken as normal.
- Figure 4-8 illustrate sound-propagation test results which are normalized in relation to the sheet according to Example 1 for respective Examples 2-6.
- FIG. 9 illustrates the result obtained with the reference sample according to Example 1 compared with the result obtained with the structure according to Example 2, thus with the sole difference that in one case the material was not check ⁇ ered-cut and in the other case the material was checkered-cut and the gaps defined between adjacent shapes were filled with elastomeric material. It will be seen from the Figures that the difference in damping was significant and that this damping increases very consid ⁇ erably when the frequency increases to above 500 Hz. Samples measuring 100 x 120 cm were secured around their respective edges in a wall between a transmitter room (106 m 3) and a recei.ver room (120 m3) .
- a further advantage afforded by the use of an elastomeric material as compared with a conventional binder is that a less fatigue can be expected due to the increased uptake of energy.
Abstract
Description
Claims
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE69207437T DE69207437T2 (en) | 1991-05-21 | 1992-05-20 | SOUND ABSORBING SANDWICH MATERIAL AND METHOD FOR THE PRODUCTION THEREOF |
EP92917462A EP0647181B1 (en) | 1991-05-21 | 1992-05-20 | Sound-damping sandwich material and a method for its manufacture |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SE9101527A SE468793B (en) | 1991-05-21 | 1991-05-21 | SOUND-SOILING SANDWICH MATERIALS MADE PROCEDURES FOR ITS PREPARATION |
SE9101527-1 | 1991-05-21 |
Publications (1)
Publication Number | Publication Date |
---|---|
WO1992020523A1 true WO1992020523A1 (en) | 1992-11-26 |
Family
ID=20382787
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/SE1992/000337 WO1992020523A1 (en) | 1991-05-21 | 1992-05-20 | Sound-damping sandwich material and a method for its manufacture |
Country Status (7)
Country | Link |
---|---|
EP (1) | EP0647181B1 (en) |
AU (1) | AU1874792A (en) |
DE (1) | DE69207437T2 (en) |
DK (1) | DK0647181T3 (en) |
ES (1) | ES2081623T3 (en) |
SE (1) | SE468793B (en) |
WO (1) | WO1992020523A1 (en) |
Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2770448A1 (en) * | 1997-11-06 | 1999-05-07 | Euramax Coated Products Sa | Composite metal and plastic panel, used in buildings and signs |
EP1118729A2 (en) * | 2000-01-20 | 2001-07-25 | Plasticino S.r.l. | Indoor and outdoor covering panels and shapes |
EP1217605A1 (en) * | 2000-12-21 | 2002-06-26 | AIRBUS FRANCE (Société par Actions Simplifiée) | Method of manufacturing a panel with a protected acoustic sound damping layer and acoustic panel thereby created |
EP1460194A1 (en) * | 2003-03-18 | 2004-09-22 | Plasticino S.r.l. | Panel for external use |
WO2008138840A1 (en) * | 2007-05-15 | 2008-11-20 | Airbus Operations Gmbh | Multilayer board for reducing solid-borne sound |
CN105856666A (en) * | 2016-03-31 | 2016-08-17 | 西安航天动力研究所 | Porous rubber filled corrugated sheet composite material and preparation method thereof |
CN112628485A (en) * | 2019-10-08 | 2021-04-09 | 中国石油化工股份有限公司 | Pipeline noise reduction device based on vacuum auxiliary layer |
CN114083838A (en) * | 2021-12-03 | 2022-02-25 | 青岛理工大学 | Sandwich structure with low-specific-modulus insertion layer and preparation method thereof |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
ES2338612T3 (en) | 2008-02-18 | 2010-05-10 | Preform Gmbh | SOUND ABSORPTION FOAM SYSTEM. |
Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE2909725A1 (en) * | 1979-03-13 | 1980-09-18 | Kunststoffabrik Erich Dittrich | Laminated plate highly resistant to bending and tension - has rib plate cavities filled with polyethylene-bonded sand |
DE3506488A1 (en) * | 1985-02-23 | 1986-09-04 | Daimler-Benz Ag, 7000 Stuttgart | Noise-damping laminate |
SE464514B (en) * | 1989-03-20 | 1991-05-06 | Diab Barracuda Ab | SET TO MANUFACTURE PLASTIC REQUIREMENTS OF SANDWICH CONSTRUCTION |
-
1991
- 1991-05-21 SE SE9101527A patent/SE468793B/en not_active IP Right Cessation
-
1992
- 1992-05-20 DK DK92917462.1T patent/DK0647181T3/en active
- 1992-05-20 WO PCT/SE1992/000337 patent/WO1992020523A1/en active IP Right Grant
- 1992-05-20 ES ES92917462T patent/ES2081623T3/en not_active Expired - Lifetime
- 1992-05-20 AU AU18747/92A patent/AU1874792A/en not_active Abandoned
- 1992-05-20 DE DE69207437T patent/DE69207437T2/en not_active Expired - Fee Related
- 1992-05-20 EP EP92917462A patent/EP0647181B1/en not_active Expired - Lifetime
Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE2909725A1 (en) * | 1979-03-13 | 1980-09-18 | Kunststoffabrik Erich Dittrich | Laminated plate highly resistant to bending and tension - has rib plate cavities filled with polyethylene-bonded sand |
DE3506488A1 (en) * | 1985-02-23 | 1986-09-04 | Daimler-Benz Ag, 7000 Stuttgart | Noise-damping laminate |
SE464514B (en) * | 1989-03-20 | 1991-05-06 | Diab Barracuda Ab | SET TO MANUFACTURE PLASTIC REQUIREMENTS OF SANDWICH CONSTRUCTION |
Cited By (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2770448A1 (en) * | 1997-11-06 | 1999-05-07 | Euramax Coated Products Sa | Composite metal and plastic panel, used in buildings and signs |
EP1118729A3 (en) * | 2000-01-20 | 2002-07-10 | Plasticino S.r.l. | Indoor and outdoor covering panels and shapes |
EP1118729A2 (en) * | 2000-01-20 | 2001-07-25 | Plasticino S.r.l. | Indoor and outdoor covering panels and shapes |
US6820337B2 (en) | 2000-12-21 | 2004-11-23 | Airbus France | Process for making a panel with a protected acoustic damping layer and acoustic panel as made |
FR2818581A1 (en) * | 2000-12-21 | 2002-06-28 | Eads Airbus Sa | PROCESS FOR MANUFACTURING A PANEL WITH A PROTECTED ACOUSTIC CUSHIONING LAYER AND ACOUSTIC PANEL THUS OBTAINED |
EP1217605A1 (en) * | 2000-12-21 | 2002-06-26 | AIRBUS FRANCE (Société par Actions Simplifiée) | Method of manufacturing a panel with a protected acoustic sound damping layer and acoustic panel thereby created |
US7257894B2 (en) | 2000-12-21 | 2007-08-21 | Airbus France | Process for making a panel with a protected acoustic damping layer |
EP1460194A1 (en) * | 2003-03-18 | 2004-09-22 | Plasticino S.r.l. | Panel for external use |
WO2008138840A1 (en) * | 2007-05-15 | 2008-11-20 | Airbus Operations Gmbh | Multilayer board for reducing solid-borne sound |
US7997384B2 (en) | 2007-05-15 | 2011-08-16 | Airbus Operations Gmbh | Multilayer board for reducing solid-borne sound |
CN105856666A (en) * | 2016-03-31 | 2016-08-17 | 西安航天动力研究所 | Porous rubber filled corrugated sheet composite material and preparation method thereof |
CN112628485A (en) * | 2019-10-08 | 2021-04-09 | 中国石油化工股份有限公司 | Pipeline noise reduction device based on vacuum auxiliary layer |
CN114083838A (en) * | 2021-12-03 | 2022-02-25 | 青岛理工大学 | Sandwich structure with low-specific-modulus insertion layer and preparation method thereof |
Also Published As
Publication number | Publication date |
---|---|
SE9101527D0 (en) | 1991-05-21 |
EP0647181B1 (en) | 1996-01-03 |
DK0647181T3 (en) | 1996-05-20 |
SE9101527L (en) | 1992-11-22 |
EP0647181A1 (en) | 1995-04-12 |
DE69207437D1 (en) | 1996-02-15 |
ES2081623T3 (en) | 1996-03-16 |
AU1874792A (en) | 1992-12-30 |
SE468793B (en) | 1993-03-22 |
DE69207437T2 (en) | 1996-06-05 |
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