Classifications

• • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
  • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
  • F16B—DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
  • F16B5/00—Joining sheets or plates, e.g. panels, to one another or to strips or bars parallel to them
  • F16B5/02—Joining sheets or plates, e.g. panels, to one another or to strips or bars parallel to them by means of fastening members using screw-thread
  • F16B5/0241—Joining sheets or plates, e.g. panels, to one another or to strips or bars parallel to them by means of fastening members using screw-thread with the possibility for the connection to absorb deformation, e.g. thermal or vibrational
• • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
  • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
  • F16B—DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
  • F16B5/00—Joining sheets or plates, e.g. panels, to one another or to strips or bars parallel to them
  • F16B5/02—Joining sheets or plates, e.g. panels, to one another or to strips or bars parallel to them by means of fastening members using screw-thread
  • F16B5/0258—Joining sheets or plates, e.g. panels, to one another or to strips or bars parallel to them by means of fastening members using screw-thread using resiliently deformable sleeves, grommets or inserts
• • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
  • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
  • F16B—DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
  • F16B19/00—Bolts without screw-thread; Pins, including deformable elements; Rivets
  • F16B19/02—Bolts or sleeves for positioning of machine parts, e.g. notched taper pins, fitting pins, sleeves, eccentric positioning rings

Definitions

• the present invention relates generally to insertable grommets, and, more particularly, to grommets used in panels, and, still more particularly, to grommets and compression limiters used with fasteners in automotive applications.
• Grommets are used in many applications as isolators in mountings or connections of an assembly.
• a grommet can be used to line an opening or hole, and may include a sleeve extending into or through the hole with a radially outwardly extending flange on at least one end of the sleeve, or on both ends of the sleeve.
• flanges are provided at both ends of the sleeve, on opposite sides of an object to be mounted, such as a panel.
• a fastener placed through the grommet can be anchored in a second component.
• One flange of the grommet serves as an isolator between the head of the fastener and an outer surface of the first component
• the second flange of the grommet serves as an isolator between an opposite side of the first component and a confronting surface of the second component.
• Simple grommets such as this are sometimes referred to as an "H"-shaped grommet.
• Grommets have many applications in automotive assemblies, including relatively recent uses for securing sound deadening engine covers of plastic or the like on to cam covers and other structures of an automobile engine.
• the grommets serve to isolate the engine cover from the engine components and to limit the transmission of vibrations or sounds so that the engine cover functions to deaden noise from the engine.
• While grommets have been used for many years with success, they are not without disadvantages. Depending on the materials used, the required thickness and stiffness of the grommet, the relative sizes of the holes and the thickness of components, the length of the grommet and other factors, it is sometimes difficult to insert a grommet into its receiving hole.
• the grommet has a large and/or stiff flange, forcing one of the flanges through the mounting hole can be both difficult and time consuming. If not fully inserted properly, the grommet can be distorted, making it difficult or impossible to insert the fastener; and a proper connection will not be created without the grommet properly positioned.
• Compression limiters are used in connections to limit the compressive force on components in the connection.
• a compression limiter in a connection having a grommet can limit the compression applied against the flange or flanges of the grommet, so that a desired compression is achieved without over compression that may limit the effectiveness of the isolating properties for which the grommet is used.
• the easy insertion grommets disclosed herein are easy to assemble or insert from one side of a panel or other component by having a not- yet-formed or not-fully-formed flange at the lead end of the grommet that is placed into and through a hole in the panel or component. Without the flange fully formed, the grommet slides easily through the hole.
• the structure of the grommet includes a deformable portion that allows for compression of the grommet to create the flange on the lead end after the grommet has been fully inserted through the receiving hole.
• the grommet can include a compression limiter for clamping against, and can be provided in both two piece constructions with a grommet and compression limiter, and a three piece construction with a grommet, and a two- piece compression limiter.
• Each can be provided as a simple panel grommet, or can have a captured fastener included therewith, such as a captured nut or a captured bolt.
• a fixed flange can be provided at the head end of the grommet, or a second deformable portion can be provided so that grommet flanges are formed at each grommet end upon axial compression of the grommet.
• a grommet assembly is provided with a grommet having a barrel, a first flange at one end of the barrel, and a deformable portion at an opposite end of the barrel from the first flange.
• a compression limiter extends into the barrel, and the deformable portion is adapted and configured for outward projection upon axial compression of the barrel, to form a second flange at the opposite end of the barrel.
• a grommet assembly is provided with a grommet having a barrel with an axial length and a first deformable portion near a first end of the barrel; and a compression limiter including a tube extending into the barrel and a radial flange at one end of the tube, the radial flange disposed outwardly of the barrel, and the tube having an axial length less than the axial length of the barrel.
• the deformable portion is adapted and configured to mushroom outwardly upon axial compression of the barrel, to form a grommet flange at the first end of the barrel.
• a grommet assembly is provided with a grommet having a barrel, a first flange at one end of the barrel, and a segmented second flange at a deformable portion of the barrel at an opposite end of the barrel from the first flange.
• a compression limiter includes a tube extending into the barrel and a radial flange at one end of the tube, the radial flange disposed outwardly of the first flange at the one end of the barrel.
• the barrel has an uninstalled length longer then the length of the tube.
• An opposite end of the tube engages the opposite end of the barrel in the grommet assembly for holding the deformable portion in an outwardly mushroomed configuration.
• FIG. 1 is a perspective view of an easy insert grommet assembly
• Fig. 2 is a perspective view of the grommet assembly inserted in a panel
• FIG. 3 is a perspective view of the grommet assembly inserted in the panel, but illustrating the side opposite the side shown in Fig. 2;
• FIG. 4 is a cross-sectional view of the grommet assembly inserted in the panel
• FIG. 5 is a cross-sectional view of the grommet
• FIG. 6 is a an elevational view of the grommet
• FIG. 7 is a cross-sectional view of a preassembled grommet and compression limiter
• FIG. 8 is a cross-sectional view of another embodiment of the grommet.
• FIG. 9 is a cross-sectional view of yet another embodiment of the grommet.
• FIG. 10 is a cross-sectional view of the installation of a three piece grommet assembly
• FIG. 11 is a cross-sectional view of another embodiment of the three piece grommet assembly.
• FIG. 12 is a cross-sectional view of an installation of the three piece grommet assembly shown in Fig. 11 ;
• FIG. 13 is a perspective view of a compression limiter
• FIG. 14 is a perspective view of another embodiment of a compression limiter
• FIG. 15 is an elevational view of a grommet
• FIG. 16 is an elevational view of another embodiment of a grommet
• FIG. 17 is a perspective view of an inner compression limiter piece
• Fig. 18 is a cross-sectional view of yet another embodiment of a three piece grommet assembly
• Fig. 19 is a cross-sectional view of a final installation of the three piece grommet assembly shown in Fig. 18;
• FIG. 20 is a cross-sectional view of a further embodiment of a three piece grommet assembly
• FIG. 21 is a cross-sectional view of a still further embodiment of a three-piece grommet assembly 18;
• Fig. 22 is an elevational view of yet another embodiment of a grommet
• FIG. 23 is an elevational view of still another embodiment of a grommet
• FIG. 24 is a perspective view of a yet further embodiment of a grommet assembly.
• Fig. 25 is a cross-sectional view of the grommet assembly shown in Fig. 24, the grommet assembly being depicted in an installation with components held thereby.
• Grommet assembly 100 is shown, including a grommet 102 and a compression limiter 104.
• Grommet assembly 100 is depicted installed in a panel 150 (Figs. 2-4).
• Grommet 102 includes a head end 106 defining an outer radial flange 108.
• a sleeve or barrel 110 extends axially from head end 106 and flange 108, and defines a generally cylindrical structure having an axial opening therethrough.
• Barrel 110 defines a plurality of circumferentially spaced, axially extending narrow elongate cutouts 112 inwardly from a lead end 114.
• a plurality of axially oriented bands 116 are defined between adjacent narrow elongate cutouts 112 and are commonly connected at opposite ends by lead end 114 at the distal ends of narrow elongate cutouts 112 and by a non-slit portion 118 of barrel 110 between radial flange 108 and the proximal ends of narrow elongate cutouts 112.
• radial bands 116 collectively form a segmented second flange 120
• compression limiter 104 is a generally cylindrical body that extends through the axial opening defined by barrel 110 of grommet 102, and compression limiter 104 also defines an axial opening therethrough for receiving a fastener.
• Compression limiter 104 further includes a radial flange 130 and a tube 132. At the lead or distal end of tube 132, a slight radial flange or foot 134 may be defined.
• Compression limiter 104 can be preassembled into grommet 102 by inserting the lead end of compression limiter 104 into the opening at the head end 106 of grommet 102, and forcing tube 132 into barrel 110 until radial flange 130 engages the outer surface of radial flange 108.
• Barrel 110 is of a length that is longer than the length of tube 132, so that foot 134 is at an intermediate position within barrel 132. This preassembled condition of grommet assembly 100 is illustrated in Fig. 7.
• grommet assembly 100 it may not be necessary to preassemble compression limiter 104 into grommet 102 before installing the preassembly into an article. Instead, grommet 102 can be installed in the article in which it is to be used, such as panel 150, and compression limiter 104 can be installed into grommet 102 with the grommet in place in the article. Thereafter, the completion of segmented second flange 120 can be performed as described previously.
• the distal end of compression limiter 104 can define a slightly outwardly extending radial foot 134 for retaining the compressed form of grommet 102 depicted in Figure 4.
• the circumferential band defined by lead end 114 can establish an interference fit on compression limiter 104 to retain grommet 102 in the compressed form thereof.
• Axial compression of grommet 102 to form the mushroomed feature of segmented second flange 120 can be performed by hand, by tooling or can be established when a fastener is inserted through the grommet assembly previously installed in a panel and anchored in a second component to thereby draw panel 150 toward the second component.
• Axial compression of grommet 102 will thereby create the mushroomed form having segmented second flange 120 shown in Figure 4 as final fastening is established.
• a radially inward enlargement 122 can be provided in the bore of grommet 102, at the distal end thereof, to better interfere and engage with tube 132 and radial flange or foot 134 of compression limiter 104.
• Figs 8 and 9 illustrate additional features that can be included in alternate embodiments of a grommet for the grommet assembly.
• a grommet 160 defines an outer flange 162 and a barrel 164.
• External notches 166 and an internal notch 168 are provided in barrel 164 at the desired locations of bending to mushroom the barrel outwardly to define the inner flange.
• the notches are areas of reduced thickness in barrel 164 that act as living hinges at the specific locations. The notches allow the grommet barrel to fold over more easily at the desired locations.
• Barrel 164 can be solid, without axial cutouts therein.
• a grommet 170 includes an outer flange 172 and a barrel 174 with external notches 176 and internal notches 178, substantially as described with respect to grommet 160 shown in Fig. 8.
• grommet 170 is formed so that barrel 174 is molded in a slight pre-bent shape to have a hip 180 to help with predictive compression and buckling of the grommet barrel and may also assist with retention in a panel or other structure such as panel 150 for ease of shipping, handling, assembly or swervicing.
• Fig. 8 illustrates the use of notches only
• Fig. 9 illustrates the use of both notches and the pre-bent formation
• the pre-bent formation can be used alone, without notches, and can provide more predictive buckling than a barrel with neither notches nor a pre- bent formation.
• FIG. 10 illustrates an installation 200 of a three-piece grommet assembly 202 with a bolt 204 to hold an engine cover 206 on a cam cover 208, the cam cover 208 defining a threaded opening 210 for threadedly engaging a threaded end 212 of bolt 204.
• Grommet assembly 202 includes a grommet 220 and a two-piece compression limiter including an outer compression limiter piece 222 and an inner compression limiter piece 224.
• Grommet 220 defines a permanently formed outer flange 226, a barrel 228 and an outwardly mushroomed inner flange 230, the inner flange 230 having been established as bolt 204 was tightened into cam cover 208 and outer compression limiter piece 222 and inner compression limiter piece 224 were drawn toward one another.
• Grommet 220 can be of any of the configurations described previously herein, including those having cutouts, those having notches and those having pre-shaped configurations for directing bending.
• Outer compression limiter piece 222 includes a radial flange 240 and a tube 242.
• Inner compression limiter piece 224 has an optional foot 244 and a tube 246. [49] Yet another three piece grommet assembly is shown in Figs. 11-
• Grommet assembly 302 includes a grommet 320 and a two-piece compression limiter including an outer compression limiter piece 322 and an inner compression limiter piece 324.
• Grommet 320 defines a permanently formed outer flange 326, a barrel 328 and an outwardly mushroomed inner flange 330, the inner flange 330 having been established as the grommet assembly is installed and compression limiter piece 322 and inner compression limiter piece 324 were drawn toward one another.
• Barrel 328 can include a plurality of axial cutouts 332 with defined axial bands 334 therebetween, substantially as described for the barrels, cutouts and bands of previous embodiments.
• An outer support ring 336 (Fig. 16) can be provided at the distal end of barrel 328.
• Grommet 320 also can be of any of the other configurations described previously herein, including those having notches in the barrels thereof and those having pre-shaped barrel configurations for directing bending.
• Outer compression limiter piece 322 includes a radial flange 340 and a tube 342.
• Inner compression limiter piece 324 has an optional foot 344 and a tube 346.
• Outer compression limiter piece 322 and inner compression limiter piece 324 are inserted into opposite ends of grommet 320.
• tube 342 of outer compression limiter piece 322 and tube 346 of inner compression limiter piece 324 slide telescopically past one another. It should be understood that various interference fit sizes and configurations, such as notches and depressions, or an enlarged interference ring 348 can be provided in the confronting surfaces of tubes 342 and 346, perhaps also with grommet 320, to hold the preassembled compression of grommet 320.
• FIGs. 18 & 19 illustrate a further embodiment similar to that described for Figs 11-17, including grommet 320 and inner compression limiter piece 324.
• an outer compression limiter piece 350 has an extended radial flange 352 and a tube 354, extended radial flange 352 being adaptable and deformable to capture a nut 360 as shown in Fig. 19.
• FIG. 20 a further grommet assembly is shown, which also is similar to grommet assembly 300 described previously and includes a grommet 320 and an inner compression limiter piece 324.
• An outer compression limiter piece 370 has a radial flange 372 and a tube 374, the tube 374 defining internal projections 376.
• a bolt 380 includes a head 382 and a shaft 384, with a circumferential, radially outward projecting ring 386 that can be forced past projections 376 so as to retain bolt 380 within the assembled grommet assembly.
• FIG. 21 illustrates a three-piece easy insertion grommet with retention features for retaining the assembly in a panel.
• a grommet assembly 400 includes a grommet 402 assembled with an outer compression limiter piece 404 and an inner compression limiter piece 406, substantially similar to those described previously.
• Grommet 402 includes an outwardly projecting knob or ring 408 to retain grommet 402 within a panel 410, along with outer compression limiter piece 404 and an inner compression limiter piece 406, which are assembled together with grommet 402.
• the retention feature established by ring 408 allows for pre-assembly of the grommet in a panel before handling and/or shipment for final use. It also retains the grommet in the panel during servicing.
• Figs 22 & 23 illustrate modifications that can be made in the barrels for any of the grommets described previously herein.
• Grommet 420 includes an outer flange 422 and a barrel 424 with slits 426 therein rather than narrow elongate cutouts.
• Grommet 430 includes an outer flange 432 and a barrel 434 with slits 436 having circular cutouts 438 at the ends thereof to prevent tear propagation.
• the grommets have included preformed, fixed outer flanges at the head end thereof and deformable portions that mushroom outwardly to form segmented inner flanges near an opposite and of the grommet, the mushrooming occurring during installation and tightening of a fastener with the grommet in an assembly.
• grommets having the various features described herein also can include multiple deformable regions to form more than a single flange by mushrooming the deformable regions outwardly as part of the installation process. Figs.
• Grommet assembly 502 includes a grommet 520 and a compression limiter 522.
• Compression limiter 522 includes a radial flange 524 and a tube 526.
• Grommet 520 is a tube or sleeve-like structure comprising a barrel 530.
• Barrel 530 defines a first plurality of circumferentially spaced, axially extending cutouts 532 near one end thereof and a second plurality of circumferentially spaced, axially extending cutouts 534 near the opposite end thereof. Accordingly, a first plurality of axially oriented bands 536 is defined between adjacent cutouts 532 and a second plurality of axially oriented bands 538 is defined between adjacent cutouts 534.
• Each of the pluralities of axially extending bands 536, 538 is compressed axially during final installation, whereby the bands mushroom outwardly, with bands 536 forming a first segmented flange 540 at one end of grommet 520 and bands 538 forming a second segmented flange 542 at the opposite end of grommet 520.
• the various other modifications described herein for the structures of grommets such as, for example and not limitation, the use of a radial inward enlargement such as enlargement 122, the use of external notches 166 and/or internal notches 168 and/or pre-bent shapes to include one or more hip 180 also can be incorporated as features of grommet 520.
• the various other alternatives for features of compression limiters described previously herein, including the variations for both single piece and double piece compression limiters and the fastener capturing features can be used together with or in place in place of compression limiter 522.
• grommets described herein can be made of, for example, rubber, synthetic rubber, and other suitably malleable and deformable materials.
• the compression limiters described herein can be made of, for example, metals and other suitably rigid and strong materials.

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• Engineering & Computer Science (AREA)
• General Engineering & Computer Science (AREA)
• Mechanical Engineering (AREA)
• Insulating Bodies (AREA)

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Cited By (6)

Citations (5)

• 2013
  • 2013-06-21 WO PCT/US2013/047126 patent/WO2013192558A1/fr not_active Ceased

Patent Citations (5)

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