This application is related to commonly assigned U.S. patent application Ser. No. 10/658,814 filed Sep. 8, 2003, by Kevin J. Surace and Marc U. Porat, entitled “Accoustical Sound Proofing Material and Methods for Manufacturing Same”, and U.S. patent application Ser. No. 10/938,051 filed Sep. 10, 2004, by Kevin J. Surace and Marc U. Porat, entitled “Acoustical Sound Proofing Material and Methods for Manufacturing Same,” both of which are incorporated by reference herein in their entirety.
This invention relates to an acoustical damping structure which may be utilized for doors, floors, walls and ceilings to prevent the transmission of sounds from one area to another.
Soundproof doors or sound transmission resistant doors have been around for a number of years and have typically been constructed of wood or metal in order to achieve or reduce sound transmission. Although sound transmission through the structure has been reduced, the doors have been rather bulky and heavy. An issue with these doors is how to make them with a high Sound Transmission Class (STC) rating and at the same time avoid the mass requirement of the prior art doors. In the prior art providing an increased STC over standard doors has been achieved by using heavy doors in order to prevent the transmission of acoustic energy from one side of the door to the other. Typical prior art soundproof doors have been made of solid, heavy materials to prevent sound transmission. Typical current soundproof doors have a mass of from about eight to ten pounds per square foot, which can result in a door weighing from three hundred to five hundred pounds, and in some cases as much as one thousand pounds. This significant amount of weight adds stress to the associated structure and in addition is not desirable for household use in view of the significant weight involved. A typical household door of a non-soundproof construction has an STC rating of about twenty-seven as opposed to the prior art, unitary soundproof doors which typically have an STC rating in the forties.
Thus what is required is a soundproof structure which has improved STC ratings, but avoids the heavy weight which has been typical of prior soundproof doors.
The present invention provides a soundproof assembly which has significantly reduced weight, yet provides an STC rating equivalent to solid doors having twice the weight. In accordance with the invention, a soundproof assembly is provided which includes one or more laminar structures which are, in one embodiment, separated by an air gap and in another embodiment separated by a layer of material. In one embodiment, both a front and a rear panel of the structure are laminar, while in another embodiment, one of the front or rear panels is laminated and the other is solid.
In one embodiment, the laminar structure includes interiorly, a constraining layer, with the constraining layer having one or more layers of viscoelastic glue on opposite sides. First and second exterior layers of material, are provided on opposite sides of the viscoelastic glue. The exterior layers may be cellulose or wood based, ceramic, metal or a composite material.
In constructing the soundproof assembly, the front and rear portions may be separated by spacers to provide an air gap intermediate the front and rear sections.
In another embodiment, a wood surround is provided about the peripheral edges of the soundproof structure. Additionally, for appearance purposes a veneer may be provided. The veneer merely serves a cosmetic function and it is not necessary for the achievement of improved STC characteristics of the soundproof structure.
In a further embodiment of the present invention, a method of forming a soundproof assembly is provided. In this method, a first panel having a laminar structure is supported adjacent to a second panel with the first and second panels being spaced apart by one or more spacers to provide an air gap between the adjacent surfaces of the first and second panels.
In a second embodiment, both the first and second panels have a laminar structure.
In providing a panel having a laminar structure, the laminar structure is produced by providing a first layer of material which is cellulose or wood based, applying one or more layers of viscoelastic glue to a surface of the first layer of cellulose material, providing a constraining layer of material, and placing this constraining layer of material on the exposed surface of the viscoelastic glue. Next, one or more layers of viscoelastic glue are provided on the exposed surface of the constraining layer and a second layer of material which is cellulose or wood based is placed on the viscoelastic glue which is exposed on the constraining layer of material. Alternative materials for the first and second layers of material include ceramic, metal, or a composite material. In one embodiment, the constraining layer of material is a layer of metal and in other embodiments, the constraining layer of material may be a solid petroleum-based synthetic material such as vinyl, plastic composite, rubber, ceramic, a composite material or any other material that has a Young's Modulus of 10 GigaPascals (GPa) or greater.
In another embodiment, the laminar structure is constructed by utilizing three layers of material which are cellulose or wood based and two layers of a constraining material interior of and intermediate the three layers of cellulose or wood based material. The constraining layers have a viscoelastic glue layer interposed between each of them and the adjacent layer of cellulose material. In the embodiment which includes two constraining layers and three cellulose layers, both of the constraining layers may be formed of a metal, a solid petroleum based synthetic material such as vinyl, plastic composites, rubber, ceramic composite, or another material having a high Young's Modulus above 10 GigaPascals (GPa). Alternatively one of the constraining layers may be one of the foregoing materials and the other may be another of the foregoing materials.
As will be appreciated by reference to
In the embodiment illustrated in
Returning to
Intermediate the interior surfaces 18 and 19 of layers 15 and 16 respectively, are a first layer of viscoelastic glue 20 and a second layer of viscoelastic glue 21. Intermediate glue layers 20 and 21 is a constraining layer indicated by reference character 17. This construction, as will be appreciated by reference to
Constraining layer 17 is, in one embodiment, a layer of metal, which may be for example 30 gauge, galvanized steel. It will of course be appreciated that other thicknesses may be used as well as other materials such as sheets of ultra-light weight titanium and laminated layers of metal including laminate of aluminum and titanium. If galvanized steel is utilized, it should be non-oiled and of regular spackle. The non-oil characteristic is required to ensure that the viscoelastic glue layers 20 and 21 will adhere to the metal. Regular spackle ensures that the metal has uniform properties over its entire area. Constraining layer 17 is constructed of a metal; typical ranges of thicknesses are from 10 gauge to 30 gauge depending on the weight, thickness, and STC desired. Of importance, the constraining layer 17 should not be creased because creasing will ruin the ability of the metal to assist in reducing the transmission of sound. Only completely flat, undamaged pieces of metal can be used in the laminar structure. Constraining layer 17 may alternatively be a layer of ceramic material, or a layer of composite materials, such as, for example, fiberglass, Kevlar or carbon fiber.
Constraining layer 17 may be alternatively mass loaded vinyl or a similar material. A suitable mass-loaded vinyl may be purchased from Technifoam in Minneapolis, Minn., and have a thickness of ⅛ of an inch; however, other thicknesses may of course be used.
As will be appreciated by reference to
The physical solid-state characteristics of QuietGlue include:
1) a broad glass transition temperature which starts below room temperature;
2) mechanical response typical of a rubber (i.e., high elongation at break, low elastic modulus);
3) strong peel strength at room temperature;
4) weak shear strength at room temperature;
5) swell in organic solvents (e.g., Tetrahydrofuran, Methanol);
6) does not dissolve in water (swells poorly);
7) peels off the substrate easily at temperature of dry ice.
In constructing front panel 2, viscoelastic glue layer 21 is applied to interior surface 19 of layer 16. Various thicknesses of glue may be utilized and can range from a few millimeters of up to about ⅛ inch. After application of viscoelastic glue layer 21, constraining layer 17 is placed on viscoelastic glue layer 21. Following that, viscoelastic glue layer 20 is applied to upper surface 22 of constraining layer 17. The thickness of viscoelastic glue layer 20 may be in the range of the thickness used for viscoelastic glue layer 21; however it is not necessary that both of the glue layers be of the same thickness.
Next, layer 15 is placed on the upper surface of the glue layer 20. The assembly is then subjected to dehumidification and drying to allow the panels to dry, typically for 48-hours. Of course, it will be appreciated from
As will be appreciated by reference to
The gap between outer surface 23 of wood layer 15 and outer surface 24 of wood layer 25 is indicated by reference character D1 in
Rear panel 3 may be constructed similarly to front panel 2, but it is not required that such a construction be utilized. Wood cellulose layers 25 and 26 may have similar thicknesses to the thicknesses of layers 15 and 16 in front panel 2; however, different thicknesses may be utilized. Additionally, each of the wood/cellulose layers in the combination are not necessarily required to have the same thickness, although that is true in the embodiments illustrated. In rear panel 3, a constraining layer 27 may be of a material like any of those layers described above with regard to constraining layer 17, but constraining layer 27 may be made of a different material than constraining layer 17.
After front panel 2 and rear panel 3 have been affixed to spacers 4, 5, and 6, the surround covers 7, 8, 9, and 10, are applied and preferably attached to the peripheral edges of rear panel 2 and rear panel 3 by glue, nails or other mechanical fasteners.
As noted above, the veneer 13 and 14 may optionally be applied to the outer surfaces of front and rear panels 2 and 3 respectively.
The interior of a soundproof assembly 33 will be better appreciated by reference to
Front panel 34 in soundproof assembly 33 may be constructed by using, for example, a solid wood or cellulose material or alternatively a plywood layer or one of the alternative materials noted above. The thickness from surface 39 to surface 40 may be for example, ⅝ inch. Another thickness may of course, be utilized, with a greater thickness providing additional improvement in STC. Soundproof assembly 33 may also include the veneers 41 and 42 if it is desirable to provide a more aesthetically pleasing appearance to soundproof assembly 33. The thickness of veneer layers 41 and 42 is a matter of design choice.
In this embodiment, glue layer 50 is applied to surface 49 and thereafter a constraining layer 51 is placed on the surface of glue layer 50, which is opposite to surface 49 of first outer layer 47. Constraining layer 51 may be any of the above described constraining layers discussed in the embodiments of
Next, glue layers 54 and 55 are provided on opposite sides of a second constraining layer 56. Glue layers 54 and 55 may be of the type described above with regard to the embodiments of
In constructing laminar panel 46, typically glue layer 50 is rolled onto surface 49 of first outer layer 47, and glue layer 52 is rolled onto surface 60 of pine laminar sheet 53. Glue layer 54 is applied by rolling it onto surface 61 of pine laminar sheet 53. Glue layer 55 is applied also by roller or another suitable technique to surface 58 of second outer layer 57. Constraining layer 51 is then sandwiched between the surfaces of glue layers 50 and 52, and constraining layer 56 is placed intermediate to glue layers 54 and 55 and the entire structure is then subjected to a compression force of about 1 pound per square inch. When a suitable pressure is described prescribed, the compressive force may be applied for a length of time such as from about 24 to 48 hours. The entire structure then becomes a laminar panel suitable for use in a soundproof structure.
Referring to
In an alternate embodiment of the present invention soundproof assembly 75 is provided, this assembly being illustrated in
Turning to
As illustrated in
Turning to
Number | Name | Date | Kind |
---|---|---|---|
1807395 | Ellis | May 1931 | A |
1925453 | Mazer | Sep 1933 | A |
2079878 | Sabine | May 1937 | A |
2177393 | Johns | Oct 1939 | A |
2872710 | Cox | Feb 1959 | A |
3111787 | Chamberlain | Nov 1963 | A |
3215225 | Kirschner | Nov 1965 | A |
3305993 | Nelsson | Feb 1967 | A |
3319738 | Wehe, Jr. | May 1967 | A |
3462899 | Sherman | Aug 1969 | A |
3642511 | Cohn et al. | Feb 1972 | A |
3828504 | Egerborg et al. | Aug 1974 | A |
4073093 | Ookawa et al. | Feb 1978 | A |
4375516 | Barrall | Mar 1983 | A |
4487291 | Walker | Dec 1984 | A |
4548854 | Wach | Oct 1985 | A |
4571915 | Barman | Feb 1986 | A |
4663224 | Tabata et al. | May 1987 | A |
4956321 | Barrall | Sep 1990 | A |
5026593 | O'Brien | Jun 1991 | A |
5063098 | Niwa et al. | Nov 1991 | A |
5210984 | Eckel | May 1993 | A |
5256223 | Alberts et al. | Oct 1993 | A |
5342465 | Bronowicki et al. | Aug 1994 | A |
5416285 | Niehaus | May 1995 | A |
5473122 | Kodiyalam et al. | Dec 1995 | A |
5474840 | Landin | Dec 1995 | A |
5691037 | McCutcheon et al. | Nov 1997 | A |
6123171 | McNett et al. | Sep 2000 | A |
6173534 | Dupin | Jan 2001 | B1 |
6177180 | Bodine et al. | Jan 2001 | B1 |
6182407 | Turpin et al. | Feb 2001 | B1 |
6266936 | Gelin | Jul 2001 | B1 |
6286280 | Fahmy et al. | Sep 2001 | B1 |
6342284 | Yu | Jan 2002 | B1 |
6381196 | Hein et al. | Apr 2002 | B1 |
6533877 | Davisson et al. | Mar 2003 | B1 |
6632550 | Yu et al. | Oct 2003 | B1 |
6800161 | Takigawa | Oct 2004 | B2 |
6803110 | Drees et al. | Oct 2004 | B2 |
6815049 | Veramasuneni | Nov 2004 | B2 |
6822033 | Yu | Nov 2004 | B2 |
7041377 | Miura et al. | May 2006 | B2 |
7181891 | Surace et al. | Feb 2007 | B2 |
7216464 | Neal et al. | May 2007 | B2 |
20030066707 | Quam et al. | Apr 2003 | A1 |
20030114064 | Fu et al. | Jun 2003 | A1 |
20030192279 | Hughart | Oct 2003 | A1 |
20040177590 | Nudo et al. | Sep 2004 | A1 |
Number | Date | Country |
---|---|---|
2219785 | Oct 1996 | CA |
09-203153 | Aug 1997 | JP |
WO 9634261 | Oct 1996 | WO |
WO 9719033 | May 1997 | WO |
WO 0024690 | May 2000 | WO |
Number | Date | Country | |
---|---|---|---|
20060108175 A1 | May 2006 | US |