The present invention relates to snap-in fasteners having particular use for connecting micro-assemblies.
There are many known snap-in fasteners that include an elastically-deformable pin to join two panels together. Such fasteners have a variety of different shapes and are made of a variety of different resilient materials. Jacobs, U.S. Pat. No. 4,973,212, discloses a snap-in fastener of this type. Jacob's fastener includes a head and a deformable lead pin that is fixed at its base to the head and extends distally to its tip. The pin has a lengthwise bifurcation that defines deformable legs 16, 18. The diameter of the deformable lead pin is tapered from a minimum at the distal tip, which is much smaller than the diameter of the panel hole, to a maximum at an intermediate point 20a, 20b, which is larger in its relaxed condition than the diameter of the panel hole. The intermediate point 20a, 20b and the pin base define the boundaries of the pin “seat”, i.e., the critical section of the pin that impinges (after installation) on the underside of the lower panel to secure the components together. As the pin enters the holes of stacked panels 24 and 32, the legs 16 and 18 contact the lower panel 24 and are compressed inwardly. When the underside of the head 26 bottoms out against the top surface of the upper panel 32, the resilience of the legs 16, 18 and the reverse taper of the seat impinging on the underside of the lower panel provide a residual clamping force between the panels.
Snap-in fasteners such as disclosed by Jacobs are useful for joining many sizes of panels but not micro-assembly panels, for example, panels having a combined thickness of about 0.6 mm. For such applications, the tapered lead pin of prior art fasteners is inefficient and insufficient. A single lead taper such as shown in the Jacobs patent is unstable in micro-assemblies because during initial positioning there are only two lateral points of contact with the second panel, which does not prevent the fastener from tipping out of proper alignment during installation. When considering a single lead taper, numerical simulations using finite element analysis (FEA) techniques in addition to experimental investigations demonstrate that the part tends to tip left or right during the installation phase, thereby preventing a successful assembly. Since there is currently no known solution to this problem, it would be desirable to provide a clean, simple and rigid snap-in fastener for the micro-assembling industry that also will not tip out of alignment during installation. It would also be desirable to provide a panel-to-panel micro assembly with fasteners that provides a simple solution to the problems posed by prior art fasteners described above.
The snap-in fastener in accordance with preferred embodiments of the invention satisfies the above-described need in the art of micro-assembly fasteners. The snap-in fastener assembles two panels together without any modification of their initial properties and characteristics, i.e. of their condition before assembly. The snap-in fastener may be used to connect panels of different materials and thicknesses.
In one preferred embodiment, the novel snap-in fastener of the present invention generally comprises a rectangular, generally-planar head having laterally-projecting resilient arms, each of which is fixed at its base to opposed sides of the head. The arms are angled downwardly, i.e., toward the legs. Preferably, the arms are integrally formed with the head. The arms are preferably curved and tapered along their length. In a preferred embodiment, the cross-section of each arm narrows from its base to its distal extremity.
Two resilient legs are fixed at their base and extend transverse to the plane of the head. Each leg has a foot at the distal end. Each foot includes a heel, located at the distal end of each leg, and a barb intermediate the heel and the leg base. The barb projects transverse to the lengthwise axis of the leg. The top or proximal (relative to the leg base) surface of the barb is preferably substantially perpendicular to the lengthwise axis of the leg. The bottom or distal (relative to the leg base) surface of the barb preferably tapers inwardly from the distal end of the top surface and terminates at an undercut between the barb and the heel. The heel preferably has a curved, bulbous shape and defines the end of the leg. The heel functions as a pilot during installation of the snap-in fastener. The undercut lies between the barb and the heel.
During installation, deformation of the inventive fastener occurs in the elastic zone of the material. The addition of the piloting heel makes the fastener self-guided. The fastener can be installed in either rectangular or circular holes in the panels to provide a permanent residual clamp load to the assembly. One main advantage of the present invention is its stable alignment characteristic provided by the addition of the piloting heel ahead of the barb that creates at a multi-point contact with the attached panel. If the hole in the bottom panel is rectangular, the fastener maintains four points of contact in a 2-dimensional plane section (four lines in actuality) between the feet 6 and the lower panel 2 as the fastener 11 is first positioned in the panel stack. If the hole in the bottom panel hole is round, the fastener maintains eight points of contact.
These and other advantages will follow from the foregoing explanation and the following drawings and description of the invention. The preferred embodiments of the invention will provide one of skill in the art with a full understanding of what has been invented. It will thereby be appreciated that the object of the invention to devise a micro-assembly snap-in fastener with various advantages over the prior art has been achieved.
Operation of the present snap-in fastener is based on elastic deformation (inward deflection and outward release or snapping) of its legs during installation, in combination with elastic deformation (loaded deflection) of the arms to ensure a correct and permanent clamp load on the assembly. Portions of the snap-in fastener's structure are based on the design theory of straight beams with variable cross sections that are elastically stressed. The snap-in fastener's structure generally includes two portions that control the function and operation of the device: an upper portion comprising mainly of the head and upper arms; and, a lower portion comprising the lower legs and active barb and heel combination.
Referring to
Two deformable and resilient legs 5 are fixed at their base to one side of the head intermediate the arms 4, and extend transverse to the plane of the head 3. The legs 5 each have a foot 6 at the distal (relative to the head) end. Preferably, each foot 6 is integrally formed at the distal end of the leg 5. Each foot 6 includes a pilot heel 9, located at the distal end of each leg 5, and a barb 7 intermediate the heel 9 and the leg base. The barb 7 projects generally transversely to the lengthwise axis of the leg 5. The top or proximal (relative to the leg base) surface 14 is preferably planar and substantially perpendicular to the axis of the leg 5. The bottom or distal (relative to the leg base) surface 13 preferably tapers inwardly from the distal end of the top surface 14 and terminates at an undercut 8 in between the barb 7 and the heel 9. The inward taper of the bottom surface 13 is shown by the dotted line in
A method of installing the fastener and joining two panels in accordance with a preferred embodiment of the invention is demonstrated in
At this position in the installation process, the fastener 11 maintains multiple points of contact with the second panel 2. Contact points are created between the heels 9 and the side wall of the hole in the second panel 2. Contact points are also created between the bottom surfaces 13 of the barb and the second panel 2. If the hole in the bottom panel is rectangular, the fastener maintains four points of contact in a 2-dimensional plane section (four lines in actuality) between the feet 6 and the lower panel 2 as the fastener 11 is first positioned in the panel stack. If the hole in the bottom panel hole is round, the fastener maintains eight points of contact. The contacts are made possible by the undercut 8 between the heel 9 and barb 7 of each leg 5. The multiple points of contact sufficiently prevent the fastener 11 from limping (leaning) to one side or the other during the initial positioning with the panels as well as during the first installation steps. Unlike prior art fasteners with one point or one line of contact that could define a center or an axis of rotation for the fastener 11, the multiple contact points provide a self-righting or uprighting feature to the fastener 11, which is not disclosed in the prior art. The fastener's construction, which enables the aforementioned multi-point contact, distinguishes this invention from the prior art.
When approaching the final position shown in
When the final operational position presented in
This application is a non-provisional patent application of U.S. provisional patent application No. 62/187,209, entitled “Snap-In Fastener”, filed Jun. 30, 2015, priority from which is hereby claimed.
Number | Date | Country | |
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62187209 | Jun 2015 | US |