WO1992020523A1 - Sound-damping sandwich material and a method for its manufacture - Google Patents

Sound-damping sandwich material and a method for its manufacture Download PDF

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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
Application number
PCT/SE1992/000337
Other languages
English (en)
French (fr)
Inventor
Ingvar Andersson
Bengt Segerström
Original Assignee
Divinycell International Ab
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 Divinycell International Ab filed Critical Divinycell International Ab
Priority to EP92917462A priority Critical patent/EP0647181B1/en
Priority to DE69207437T priority patent/DE69207437T2/de
Publication of WO1992020523A1 publication Critical patent/WO1992020523A1/en

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B5/00Layered 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
    • B32B5/18Layered 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
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B3/00Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form
    • B32B3/10Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form characterised by a discontinuous layer, i.e. formed of separate pieces of material
    • B32B3/18Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer 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
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B38/00Ancillary operations in connection with laminating processes
    • B32B38/18Handling of layers or the laminate
    • B32B38/1858Handling of layers or the laminate using vacuum
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B7/00Layered 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
    • B32B7/04Interconnection of layers
    • B32B7/12Interconnection of layers using interposed adhesives or interposed materials with bonding properties
    • EFIXED CONSTRUCTIONS
    • E04BUILDING
    • E04CSTRUCTURAL ELEMENTS; BUILDING MATERIALS
    • E04C2/00Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels
    • E04C2/02Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by specified materials
    • E04C2/10Building 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
    • E04C2/20Building 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
    • E04C2/205Building 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
    • GPHYSICS
    • G10MUSICAL INSTRUMENTS; ACOUSTICS
    • G10KSOUND-PRODUCING DEVICES; METHODS OR DEVICES FOR PROTECTING AGAINST, OR FOR DAMPING, NOISE OR OTHER ACOUSTIC WAVES IN GENERAL; ACOUSTICS NOT OTHERWISE PROVIDED FOR
    • G10K11/00Methods 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
    • G10K11/16Methods or devices for protecting against, or for damping, noise or other acoustic waves in general
    • G10K11/162Selection of materials
    • G10K11/168Plural layers of different materials, e.g. sandwiches
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2266/00Composition of foam
    • B32B2266/02Organic
    • B32B2266/0214Materials belonging to B32B27/00
    • B32B2266/0221Vinyl resin
    • B32B2266/0235Vinyl halide, e.g. PVC, PVDC, PVF, PVDF
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2266/00Composition of foam
    • B32B2266/08Closed cell foam
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2305/00Condition, form or state of the layers or laminate
    • B32B2305/08Reinforcements
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2307/00Properties of the layers or laminate
    • B32B2307/10Properties 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.

Landscapes

  • Engineering & Computer Science (AREA)
  • Architecture (AREA)
  • Physics & Mathematics (AREA)
  • Wood Science & Technology (AREA)
  • Civil Engineering (AREA)
  • Structural Engineering (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Acoustics & Sound (AREA)
  • Multimedia (AREA)
  • Laminated Bodies (AREA)
  • Building Environments (AREA)
  • Soundproofing, Sound Blocking, And Sound Damping (AREA)
  • Casting Or Compression Moulding Of Plastics Or The Like (AREA)
PCT/SE1992/000337 1991-05-21 1992-05-20 Sound-damping sandwich material and a method for its manufacture WO1992020523A1 (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
EP92917462A EP0647181B1 (en) 1991-05-21 1992-05-20 Sound-damping sandwich material and a method for its manufacture
DE69207437T DE69207437T2 (de) 1991-05-21 1992-05-20 Schalldämpfendes sandwichmaterial und verfahren zu seiner herstellung

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
SE9101527-1 1991-05-21
SE9101527A SE468793B (sv) 1991-05-21 1991-05-21 Ljuddaempande sandwichmaterial jaemte foerfarande foer dess framstaellning

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 ( )
AU (1) AU1874792A ( )
DE (1) DE69207437T2 ( )
DK (1) DK0647181T3 ( )
ES (1) ES2081623T3 ( )
SE (1) SE468793B ( )
WO (1) WO1992020523A1 ( )

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2770448A1 (fr) * 1997-11-06 1999-05-07 Euramax Coated Products Sa Plaque composite directement formable a froid, procede de fabrication et utilisation pour enseignes
EP1118729A2 (en) * 2000-01-20 2001-07-25 Plasticino S.r.l. Indoor and outdoor covering panels and shapes
EP1217605A1 (fr) * 2000-12-21 2002-06-26 AIRBUS FRANCE (Société par Actions Simplifiée) Procédé de fabrication d'un panneau à couche d'amortissement acoustique protégée et panneau acoustique ainsi obtenu
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 (zh) * 2016-03-31 2016-08-17 西安航天动力研究所 一种多孔橡胶填充波纹板复合材料及其制备方法
CN112628485A (zh) * 2019-10-08 2021-04-09 中国石油化工股份有限公司 一种基于真空辅助层的管道降噪装置
CN114083838A (zh) * 2021-12-03 2022-02-25 青岛理工大学 一种具有低比模量插入层的夹层结构及其制备方法

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
PL2090621T3 (pl) 2008-02-18 2010-06-30 Preform Gmbh Dźwiękochłonny układ piankowy

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2909725A1 (de) * 1979-03-13 1980-09-18 Kunststoffabrik Erich Dittrich Schichtplatte
DE3506488A1 (de) * 1985-02-23 1986-09-04 Daimler-Benz Ag, 7000 Stuttgart Geraeuschdaemmender schichtkoerper
SE464514B (sv) * 1989-03-20 1991-05-06 Diab Barracuda Ab Saett att tillverka baatskrov av plast i sandwichkonstruktion

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2909725A1 (de) * 1979-03-13 1980-09-18 Kunststoffabrik Erich Dittrich Schichtplatte
DE3506488A1 (de) * 1985-02-23 1986-09-04 Daimler-Benz Ag, 7000 Stuttgart Geraeuschdaemmender schichtkoerper
SE464514B (sv) * 1989-03-20 1991-05-06 Diab Barracuda Ab Saett att tillverka baatskrov av plast i sandwichkonstruktion

Cited By (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2770448A1 (fr) * 1997-11-06 1999-05-07 Euramax Coated Products Sa Plaque composite directement formable a froid, procede de fabrication et utilisation pour enseignes
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 (fr) * 2000-12-21 2002-06-28 Eads Airbus Sa Procede de fabrication d'un panneau a couche d'amortissement acoustique protegee et panneau acoustique ainsi obtenu
EP1217605A1 (fr) * 2000-12-21 2002-06-26 AIRBUS FRANCE (Société par Actions Simplifiée) Procédé de fabrication d'un panneau à couche d'amortissement acoustique protégée et panneau acoustique ainsi obtenu
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 (zh) * 2016-03-31 2016-08-17 西安航天动力研究所 一种多孔橡胶填充波纹板复合材料及其制备方法
CN112628485A (zh) * 2019-10-08 2021-04-09 中国石油化工股份有限公司 一种基于真空辅助层的管道降噪装置
CN114083838A (zh) * 2021-12-03 2022-02-25 青岛理工大学 一种具有低比模量插入层的夹层结构及其制备方法

Also Published As

Publication number Publication date
AU1874792A (en) 1992-12-30
EP0647181B1 (en) 1996-01-03
EP0647181A1 (en) 1995-04-12
ES2081623T3 (es) 1996-03-16
DE69207437D1 (de) 1996-02-15
SE468793B (sv) 1993-03-22
DK0647181T3 (da) 1996-05-20
DE69207437T2 (de) 1996-06-05
SE9101527D0 (sv) 1991-05-21
SE9101527L (sv) 1992-11-22

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