WO2011038338A2 - Multi-layer assembly with retention feature - Google Patents
Multi-layer assembly with retention feature Download PDFInfo
- Publication number
- WO2011038338A2 WO2011038338A2 PCT/US2010/050388 US2010050388W WO2011038338A2 WO 2011038338 A2 WO2011038338 A2 WO 2011038338A2 US 2010050388 W US2010050388 W US 2010050388W WO 2011038338 A2 WO2011038338 A2 WO 2011038338A2
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- layer
- retention feature
- layer assembly
- rigid layers
- rigid
- Prior art date
Links
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- 230000007774 longterm Effects 0.000 abstract 1
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- 239000000463 material Substances 0.000 description 21
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- 238000000429 assembly Methods 0.000 description 8
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- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 1
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- Y10T428/24851—Intermediate layer is discontinuous or differential
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/24—Structurally defined web or sheet [e.g., overall dimension, etc.]
- Y10T428/24942—Structurally defined web or sheet [e.g., overall dimension, etc.] including components having same physical characteristic in differing degree
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/29—Coated or structually defined flake, particle, cell, strand, strand portion, rod, filament, macroscopic fiber or mass thereof
- Y10T428/2982—Particulate matter [e.g., sphere, flake, etc.]
- Y10T428/2991—Coated
Definitions
- the present invention generally relates to multi-layer assemblies and, more particularly, to multi-layer assemblies that include one or more rigid and adhesive layers, such as those used in sound damping laminates and other structures.
- a potential challenge when using sound damping laminates can involve the matter of attachment, whether it be attachment of the laminate to some support structure or attachment of some device to the laminate.
- Most sound damping laminates include a pair of rigid layers that sandwich a sound damping adhesive layer.
- the adhesive layer may experience a stress relaxation or compression set over time. If a nut and bolt are used to attach the sound damping laminate to a support structure, for example, it is possible that the amount torque, pressure, stress and/or fastening force of that attachment can diminish as time goes on. This phenomenon may be caused by the compression that the nut/bolt combination exerts on the sound damping laminate, which can cause the adhesive layer to be slowly squeezed out of the surrounding vicinity over time. The loss of some of the adhesive layer in this area— in addition to other factors such as compression set, stress relaxation, spring back, etc. in the various layers and components involved— can cause the nut/bolt combination to become loose.
- a multi-layer assembly comprising: a first rigid layer; a second rigid layer; an adhesive layer that is in contact with the first and second rigid layers such that the adhesive layer bonds the first and second rigid layers together; and a retention featured that is formed in at least one of the first and second rigid layers and includes a side wall.
- the side wall extends away from the adhesive layer such that a space is formed between the first and second rigid layers, and the space is devoid of adhesive from the adhesive layer.
- a multi-layer assembly comprising: a first rigid layer that is made of metal and has an inner surface; a second rigid layer that is made of metal and has an inner surface; an adhesive layer that is in contact with the inner surfaces of the first and second rigid layers such that the adhesive layer bonds the first and second rigid layers together; and a retention feature that is formed in at least one of the first and second rigid layers. Attachment of a fastening device to the multi-layer assembly causes a deformation of the retention feature such that the inner surfaces of the first and second rigid layers contact each other and form a metal-to-metal interface that is devoid of adhesive from the adhesive layer.
- FIG. 1 is a cross-sectional view of an exemplary multi-layer assembly lacking a retention feature
- FIG. 2 is a top-down view of an exemplary multi-layer assembly having a retention feature
- FIG. 4 is a cross-sectional view of the multi-layer assembly of FIG. 2, where a fastening device has been attached to the multi-layer assembly;
- FIG. 5 is a top-down view of another exemplary multi-layer assembly having a retention feature, where the retention feature shown here is designed to accommodate several fastening devices;
- FIG. 6 is a top-down view of another exemplary multi-layer assembly having a retention feature, where the retention feature shown here includes an additional inner side wall;
- FIG. 7 is a cross-sectional view of the multi-layer assembly of FIG. 6, where a fastening device has not been attached to the multi-layer assembly;
- FIG. 9 is a top-down view of another exemplary multi-layer assembly having a retention feature, where the retention feature shown here is designed to accommodate several fastening devices;
- FIG. 13 is a cross-sectional view of another exemplary multi-layer assembly having a retention feature, where the retention feature is formed in both the first and second rigid layers;
- FIG. 14 is a perspective view of another exemplary multi-layer assembly having a retention feature, where the retention feature is formed along an edge of a rigid layer;
- FIG. 15 is a cross-sectional view of the multi-layer assembly of FIG. 14;
- FIG. 17 is a cross-sectional view of the multi-layer assembly of FIG. 16.
- the retention features described below may be added to a multilayer assembly, such as a sound damping structure, in order to prevent or reduce a loss of torque that may otherwise occur near a fastening device.
- Multi-layer assemblies such as these may be used in a whole variety of applications including, but certainly not limited to, household appliances like washing machines, dryers, ovens, dishwashers, and microwaves; vehicle components like dash panels or firewalls, hoods, roofs, deck lids, door panels, spare wheel tubs, trunk floors, wheel houses, floor pans, and oil pans; agricultural equipment; lawn and garden equipment; and electronic equipment like disk drives, to name a few.
- multi-layer assemblies are used for improved vibration or sound damping purposes, thermal insulation, added structural integrity, etc.
- Fastening device 18 such as the nut/bolt combination shown here, may be used with multi-layer assembly 10 in order to strengthen the bond or joint between the various layers of the assembly, to secure other components to the multi-layer assembly (e.g., a brake booster could be secured to a multi-layer vehicle firewall, in which case one or more fastening devices would be needed), and/or to attach or mount the multi-layer assembly to some other structure (e.g., a multi-layer vehicle firewall could be mounted to one or more vehicle cross members or other vehicle frame members), to cite several possibilities.
- a "fastening device,” as used herein, broadly includes any type of device, component, etc. that engages a multilayer assembly and creates some type of mechanical lock, such as those described above. Some non-limiting examples of fastening devices include: nuts/bolts, screws, nails, rivets, clamps, spot welds, etc.
- exemplary retention feature 40 which is formed in one or more layers of multi-layer assembly 10 and is located near fastening hole 28.
- Retention feature 40 may impart rigidity and improved stiffness to the area surrounding fastening hole 28 and it may also prevent adhesive layer 14 from being applied in the areas surrounding the fastening hole and thus avoid the problem of the adhesive being squeezed or pushed out when fastening device 18 is torqued down.
- Retention feature 40 may be formed in first rigid layer 12 and/or second rigid layer 16, and can come in many different forms.
- retention feature 140 may be a raised embossment with a side wall 142 and a top wall 144 that create a space (not shown) between the first and second rigid layers. These components are similar to those in the first exemplary embodiment and thus are not described here. [0033] In cases where retention feature 140 has a top wall 144 with a large surface area, it may be difficult to punch out fastening holes 128 once the retention feature is formed due to the lack of support underneath the rather large top wall. One way to address such a situation is to resistance or spot weld the inner surfaces of the first and second rigid layers together at top wall 144 before punching out fastening holes 128.
- the following exemplary process could be used: first, form retention feature 140 in the first and/or second rigid layer; next, apply an adhesive layer to the inner surface or underside of the rigid layer that includes retention feature 140 (this results in the retention feature being generally devoid of adhesive as a roller or other tool simply passes over the indentation created by the retention feature; this is explained below in more detail); the first and second rigid layers are then brought together so that the adhesive layer can set or cure; next, retention feature 140 is resistance welded to the opposing rigid layer at one or more spot welds on top wall 144 so that there are one or more metal-to-metal interfaces between the first and second rigid layers; and finally, the different nut/bolt combinations or other fastening devices could be inserted through fastening holes 128 and installed on the multi-layer assembly.
- the preceding process is only one possibility, as other processes and sequences of steps could be used instead.
- retention feature 240 is shown that is in some ways similar to retention feature 40 of the first exemplary embodiment.
- retention feature 240 has an outer side wall 242, a top wall 244, and an additional inner side wall 248, and creates a space 246 with an underlying first rigid layer 212.
- Outer side wall 242 and top wall 244 are similar to side wall 42 and top wall 44, respectively, of the first exemplary embodiment and thus are not separately described here.
- Inner side wall 248 is connected to top wall 244 at one end (outer radial end of the inner side wall) and extends downwards towards second rigid layer 212.
- Inner side wall 248 can be angled similarly to outer side wall 242, as already described with reference to side wall 42, although it can be angled differently as well.
- retention feature 340 has an annular configuration but could be rectangular, elliptical, or another suitable shape.
- retention feature embodiments are designed to avoid or at least reduce the application of adhesive to certain areas in and/or around the retention features during the manufacturing process of the multi-layer assembly, which reduces the potential loss of torque issue at the area surrounding the fastening hole.
- the exact manufacturing process can vary and will depend in part on whether the multi-layer assembly is provided in patch form or laminate form, among other factors.
- the first and/or second rigid layers can be formed into appropriately sized pieces or patches by a blanking process, a stamping process, or any other suitable process.
- the particular retention feature can be formed in the first and/or second rigid layer before, during, or after the blanking process by a stamping process such as a coining, embossing, or another suitable process.
- the adhesive layer can then be applied to the rigid layer by a roll-coating process or the like.
- the adhesive layer is applied to the inner surface of the rigid layer by way of a roller that is wheeled over the inner surface and makes contact with the surface where it is not recessed due to the retention feature; i.e., the unraised portions of the rigid layer. Where it is recessed, such as at the retention feature, the inner surface of the rigid layer is spaced away from the roller as it wheels over the retention feature and the adhesive material on the roller is not painted or applied to underside of the recess.
- the adhesive layer may be applied with a draw down bar or other material application technique, or to be prepared and cut into thin strips of adhesive so that the film-like strips can be applied to the first and/or second rigid layer.
- the adhesive layer may be a non-solvent- based or 100% reactable material, as opposed to a solvent-based material that includes a carrier or solvent component that evaporates out of the adhesive over time. Materials that are 100% reactable are usually thinner than corresponding solvent-based layers because they do not have the solvent or carrier component that can account for about half of the overall thickness of the adhesive layer. Accordingly the retention features do not have to be recessed as much (i.e., they can be shallower) and still avoid adhesive during the application process.
- the now combined multi-layer assembly can be blanked into individual pieces or can be recoiled for shipping and subsequent processing.
- a piercing process or another suitable process can be performed in order to put one or more fastening holes in the first and second rigid layers.
- the piercing process can be performed separately to each of the layers as they are being brought together, for example, can be performed to the layers simultaneously after they are adhered together, or can be performed at another time and in another way.
- the manufacturing process of the multi-layer assembly can vary in different embodiments in both the patch and laminate forms.
- the above-described steps and processes can be performed at different times with respect to one another and need not all necessarily be performed, and additional steps and/or processes not described here can be performed as well.
- any or all of the steps and processes could be used on the first rigid layer.
- the retention feature or turned-up flange 820 may be bent or otherwise forced back into alignment with the rest of the blank so that the edges can be fastened together.
- the edges of the first and second rigid blanks 812, 816 are laser, mash seam, or otherwise welded together and because there is no intervening adhesive material in the area of the weld, the weld is not contaminated by the adhesive; a condition that can occur during laser welding when the laser melts the adhesive material so that the byproducts makes the weld undesirably porous.
- retention feature 820 is merely exemplary and that retention features having different shapes and configuration may be used instead.
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Physics & Mathematics (AREA)
- Acoustics & Sound (AREA)
- Chemical & Material Sciences (AREA)
- Organic Chemistry (AREA)
- General Engineering & Computer Science (AREA)
- Chemical Kinetics & Catalysis (AREA)
- General Chemical & Material Sciences (AREA)
- Multimedia (AREA)
- Connection Of Plates (AREA)
- Standing Axle, Rod, Or Tube Structures Coupled By Welding, Adhesion, Or Deposition (AREA)
- Laminated Bodies (AREA)
- Vibration Prevention Devices (AREA)
- Vehicle Interior And Exterior Ornaments, Soundproofing, And Insulation (AREA)
Abstract
Description
Claims
Priority Applications (6)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201080042913.XA CN102576525B (en) | 2009-09-25 | 2010-09-27 | There is the multilayer module of holding structure |
KR1020127010493A KR101757721B1 (en) | 2009-09-25 | 2010-09-27 | Multi-layer assembly with retention feature |
US13/395,044 US9012006B2 (en) | 2009-09-25 | 2010-09-27 | Multi-layer assembly with retention feature |
JP2012531100A JP5856959B2 (en) | 2009-09-25 | 2010-09-27 | Multilayer assembly having retention features |
EP10819597.5A EP2481046B1 (en) | 2009-09-25 | 2010-09-27 | Multi-layer assembly with retention feature |
MX2012003625A MX2012003625A (en) | 2009-09-25 | 2010-09-27 | Multi-layer assembly with retention feature. |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US24573109P | 2009-09-25 | 2009-09-25 | |
US61/245,731 | 2009-09-25 |
Publications (2)
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WO2011038338A2 true WO2011038338A2 (en) | 2011-03-31 |
WO2011038338A3 WO2011038338A3 (en) | 2011-08-25 |
Family
ID=43796517
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/US2010/050388 WO2011038338A2 (en) | 2009-09-25 | 2010-09-27 | Multi-layer assembly with retention feature |
Country Status (7)
Country | Link |
---|---|
US (1) | US9012006B2 (en) |
EP (1) | EP2481046B1 (en) |
JP (1) | JP5856959B2 (en) |
KR (1) | KR101757721B1 (en) |
CN (1) | CN102576525B (en) |
MX (1) | MX2012003625A (en) |
WO (1) | WO2011038338A2 (en) |
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JP2012225358A (en) * | 2011-04-15 | 2012-11-15 | Nippon Steel Corp | Joint of metal member and method for manufacturing the same |
JP2013068255A (en) * | 2011-09-21 | 2013-04-18 | Kobe Steel Ltd | Composite panel molded body, mounting structure therefor, and mounting and fixing method therefor |
WO2014086331A1 (en) * | 2012-12-05 | 2014-06-12 | Eads Deutschland Gmbh | Indication bolt for monitoring adhesive bonds in structural elements |
WO2017097917A1 (en) * | 2015-12-09 | 2017-06-15 | Jaguar Land Rover Limited | Thermally insulating panel for a vehicle |
CN108495778A (en) * | 2016-01-27 | 2018-09-04 | 欧拓管理公司 | Body bottom panel with installation point |
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DE102016106152A1 (en) * | 2016-04-05 | 2017-10-05 | Elringklinger Ag | Fastening device for a decoupling device on a shielding part, decoupling device comprising the fastening device and shielding part comprising the decoupling device |
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JP2012225358A (en) * | 2011-04-15 | 2012-11-15 | Nippon Steel Corp | Joint of metal member and method for manufacturing the same |
JP2013068255A (en) * | 2011-09-21 | 2013-04-18 | Kobe Steel Ltd | Composite panel molded body, mounting structure therefor, and mounting and fixing method therefor |
WO2014086331A1 (en) * | 2012-12-05 | 2014-06-12 | Eads Deutschland Gmbh | Indication bolt for monitoring adhesive bonds in structural elements |
US10071817B2 (en) | 2012-12-05 | 2018-09-11 | Airbus Defence and Space GmbH | Indication bolt for monitoring adhesive bonds in structural elements |
WO2017097917A1 (en) * | 2015-12-09 | 2017-06-15 | Jaguar Land Rover Limited | Thermally insulating panel for a vehicle |
US10829061B2 (en) | 2015-12-09 | 2020-11-10 | Jaguar Land Rover Limited | Thermally insulating panel for a vehicle |
CN108495778A (en) * | 2016-01-27 | 2018-09-04 | 欧拓管理公司 | Body bottom panel with installation point |
CN112105823A (en) * | 2018-05-17 | 2020-12-18 | 阿特拉斯·科普柯Ias(英国)有限公司 | Method for connecting two workpieces |
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Also Published As
Publication number | Publication date |
---|---|
KR20120085789A (en) | 2012-08-01 |
EP2481046A2 (en) | 2012-08-01 |
KR101757721B1 (en) | 2017-07-14 |
JP2013505862A (en) | 2013-02-21 |
JP5856959B2 (en) | 2016-02-10 |
WO2011038338A3 (en) | 2011-08-25 |
US20120171413A1 (en) | 2012-07-05 |
CN102576525A (en) | 2012-07-11 |
US9012006B2 (en) | 2015-04-21 |
MX2012003625A (en) | 2012-04-20 |
EP2481046A4 (en) | 2014-01-01 |
CN102576525B (en) | 2016-01-06 |
EP2481046B1 (en) | 2016-11-09 |
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