The present disclosure relates to fasteners used to join trim components having blade elements to body panels of automotive vehicles.
This section provides background information related to the present disclosure which is not necessarily prior art.
Fasteners are currently known for fastening panels, such as body panels and automobile interior trim pieces to a vehicle chassis. A body panel may be, for example, an interior or exterior body panel on an automobile vehicle, or any polymeric or other material interior trim component. The panel may also be an exterior body panel. The body panels are often required to attach to the chassis of the automobile vehicle with a low level of insertion force while yet providing for a high extraction force. Conventional fasteners used for this purpose do not also provide for the capability to eliminate a noise transmission path between the body panel and the trim component.
Further, known body panels when attached to the vehicle using known fasteners are not also capable of securing the panel to the chassis under the wide variety of environmental conditions necessary, including under vibration at various levels that also induce noise transmission. For example, the fastener device should prevent or minimize rattling or any other type of noise that may be audible to the occupants of the vehicle.
Known fasteners for attaching body panels to an automobile chassis may include one or more retaining tabs to permit a blade for example from a trim rib tower to be inserted. However, the fasteners do not fully isolate the blade from the body panel. Thus, known clip designs do not completely isolate vibration and noise sources between the vehicle body panel and the trim component.
This section provides a general summary of the disclosure, and is not a comprehensive disclosure of its full scope or all of its features.
According to several aspects, a fastener includes a first portion having first and second legs. A second portion having opposed first and second wings defines a V-shape. A frictionally coupled two-piece joined assembly of the first and second body portions is created when a force applied to the first portion drives the first portion into a cavity of the second portion between the first and second wings. The first portion is thereafter retained by contact between a first catch member of the first leg and a second catch member of the second leg extending into a window created in each of the first and second wings and directly contacting an edge of each window.
According to further aspects, a fastener includes a first portion having first and second legs defining an upside-down A-shape. A second portion includes opposed first and second wings defining a V-shape. The first and second wings are individually initially integrally coupled to one of the legs by a frangible joint in an as-molded condition of the fastener. A frictionally coupled two-piece joined assembly of the first and second body portions is created when a force applied to the first portion drives the first portion into a cavity of the second portion between the first and second wings fracturing the frangible joint. The first portion is thereafter retained with the second portion by a first foot of the first leg and a second foot of the second leg oppositely positioned about and contacting a body end of the second portion, preventing rocking motion between the first and second portions.
According to other aspects, a fastener system includes a fastener first portion having first and second legs defining an upside-down A-shape. A first flange is integrally connected to the first leg and a second flange is integrally connected to the second leg. A fastener second portion having opposed first and second wings defines a V-shape. A frictionally coupled two-piece joined assembly of the first and second body portions is created when a force applied to the first portion drives the first portion into a cavity of the second portion between the first and second wings. The first portion is thereafter retained by contact between a first catch member of the first leg and a second catch member of the second leg individually positioned in direct contact with an edge of a window created in each of the first and second wings. The two-piece joined assembly is adapted to be engaged in an aperture of a vehicle body panel, having the first and second flanges contacting a first surface of the body panel and the first and second wings contacting an oppositely facing second surface of the body panel such that when a trim component is connected by the two-piece joined assembly to the body panel a rib of the trim component is received between the first and second legs and a tower of the trim component contacts the first and second flanges preventing direct contact between the trim component and the body panel.
According to other aspects, a method for forming a fastener, includes the steps of: forming a fastener first portion having first and second legs defining an upside-down A-shape; simultaneously co-forming a fastener second portion having opposed first and second wings defining a V-shape; initially integrally coupling each one of the first and second wings to an individual one of the legs by a frangible joint defining an as-molded condition of the fastener; and applying a force to the first portion thereby fracturing the frangible joint; continuing application of the force to drive the first portion into the cavity of the second portion between the first and second wings; and retaining the first portion together with the second portion by positioning a first catch member of the first leg and a second catch member of the second leg individually in direct contact with an edge of a window created in each of the first and second wings to create a frictionally coupled two-piece joined assembly of the first and second body portions.
Further areas of applicability will become apparent from the description provided herein. The description and specific examples in this summary are intended for purposes of illustration only and are not intended to limit the scope of the present disclosure.
The drawings described herein are for illustrative purposes only of selected embodiments and not all possible implementations, and are not intended to limit the scope of the present disclosure.
Corresponding reference numerals indicate corresponding parts throughout the several views of the drawings.
Example embodiments will now be described more fully with reference to the accompanying drawings.
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The second portion 14 includes oppositely directed first and second wings 46, 48 facing outwardly with respect to each other that are initially integrally connected by the first and second frangible joints 16, 18 to the first and second legs 24, 26. The second portion 14 further includes an outwardly tapering first tension leg 50 tapering outwardly to an apex 51, and an outwardly tapering second tension leg 52 tapers outwardly to an apex 53. From apexes 51, 53 first and second support legs 54, 56 extend downwardly and taper inwardly toward each other as viewed in
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The assembly of the rib tower 84 and the two-piece joined assembly 19 of fastener 10 can then be inserted through a slot 106 created in a body panel 108 of a vehicle. A width Z1 of slot 106 is less than the spacing between apexes 51, 53 therefore the first and second tension legs 50, 52 and the first and second support legs 54, 56 together inwardly deflect during passage through slot 106, and then outwardly rebound when in the installed position shown. The juncture between the first and second tension legs 50, 52 and the first and second support legs 54, 56 defines a flexing point which allows the second portion 14 to inwardly compress in the slot 106, with a subsequent outward biasing force created to help hold the first and second tension legs 50, 52 in contact with the body panel 108. In addition, the width Z1 of slot 106 is greater than a width Z2 of the first and second tapering legs 92, 94 passing through slot 106, therefore contact between first and second tension legs 50, 52 is prevented with the inner wall of slot 106, which prevents contact between material of the rib tower 84 and body panel 108, thereby preventing acoustic or vibration transmission.
Based on the known thickness “T2” of body panel 108, tapering outer faces 50a, 52a of first and second tension legs 50, 52 directly contact an underside or first surface 110 of body panel 108 at an intersection of the first surface 110 and the inner wall of slot 106, while simultaneously the membranes 42a, 44a of the first and second flanges 42, 44 directly contact an upper or second surface 112 of body panel 108 to retain the two-piece joined assembly 19 and rib tower 84 in the engaged position. Contact of the bottom facing edges 104, 105 of rib tower 84 with the flat portion 74 of each of the first and second flanges 42, 44 acts as an acoustic barrier preventing noise and vibration transmission between the rib tower 84 (and therefore between the attached trim component) and the body panel 108. The raised outer lip 42b, 44b of each of the first and second flanges 42, 44 extend outward of the first and second tower walls 88, 90 of rib tower 84 which further prevents material of the rib tower 84 from contacting the body panel 108.
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Fasteners of the present disclosure provide multiple advantages, including the fasteners 10, 114 having frangible joints initially coupling first and second portions in an as-molded condition that allow the first portion to be subsequently inserted into and coupled to the second portion by application of a force fracturing the frangible joints. The fasteners 10, 114 have flanges or contact edges that directly contact the vehicle body panel on one face of the body panel while the flexible legs of the fastener contact the second side of the body panel to prevent noise/vibration transmission. The fasteners 10, 114 have first portion legs where the fracture joints are initially located that are repositioned to outward facing sides of the second portion body end to stabilize the assembly of the first and second portions. The use of spring biased legs of the second portion help retain the internally directed inner raised members of the first portion.
Example embodiments are provided so that this disclosure will be thorough, and will fully convey the scope to those who are skilled in the art. Numerous specific details are set forth such as examples of specific components, devices, and methods, to provide a thorough understanding of embodiments of the present disclosure. It will be apparent to those skilled in the art that specific details need not be employed, that example embodiments may be embodied in many different forms and that neither should be construed to limit the scope of the disclosure. In some example embodiments, well-known processes, well-known device structures, and well-known technologies are not described in detail.
The terminology used herein is for the purpose of describing particular example embodiments only and is not intended to be limiting. As used herein, the singular forms “a,” “an,” and “the” may be intended to include the plural forms as well, unless the context clearly indicates otherwise. The terms “comprises,” “comprising,” “including,” and “having,” are inclusive and therefore specify the presence of stated features, integers, steps, operations, elements, and/or components, but do not preclude the presence or addition of one or more other features, integers, steps, operations, elements, components, and/or groups thereof. The method steps, processes, and operations described herein are not to be construed as necessarily requiring their performance in the particular order discussed or illustrated, unless specifically identified as an order of performance. It is also to be understood that additional or alternative steps may be employed.
When an element or layer is referred to as being “on,” “engaged to,” “connected to,” or “coupled to” another element or layer, it may be directly on, engaged, connected or coupled to the other element or layer, or intervening elements or layers may be present. In contrast, when an element is referred to as being “directly on,” “directly engaged to,” “directly connected to,” or “directly coupled to” another element or layer, there may be no intervening elements or layers present. Other words used to describe the relationship between elements should be interpreted in a like fashion (e.g., “between” versus “directly between,” “adjacent” versus “directly adjacent,” etc.). As used herein, the term “and/or” includes any and all combinations of one or more of the associated listed items.
Although the terms first, second, third, etc. may be used herein to describe various elements, components, regions, layers and/or sections, these elements, components, regions, layers and/or sections should not be limited by these terms. These terms may be only used to distinguish one element, component, region, layer or section from another region, layer or section. Terms such as “first,” “second,” and other numerical terms when used herein do not imply a sequence or order unless clearly indicated by the context. Thus, a first element, component, region, layer or section discussed below could be termed a second element, component, region, layer or section without departing from the teachings of the example embodiments.
Spatially relative terms, such as “inner,” “outer,” “beneath,” “below,” “lower,” “above,” “upper,” and the like, may be used herein for ease of description to describe one element or feature's relationship to another element(s) or feature(s) as illustrated in the figures. Spatially relative terms may be intended to encompass different orientations of the device in use or operation in addition to the orientation depicted in the figures. For example, if the device in the figures is turned over, elements described as “below” or “beneath” other elements or features would then be oriented “above” the other elements or features. Thus, the example term “below” can encompass both an orientation of above and below. The device may be otherwise oriented (rotated 90 degrees or at other orientations) and the spatially relative descriptors used herein interpreted accordingly.
The foregoing description of the embodiments has been provided for purposes of illustration and description. It is not intended to be exhaustive or to limit the disclosure. Individual elements or features of a particular embodiment are generally not limited to that particular embodiment, but, where applicable, are interchangeable and can be used in a selected embodiment, even if not specifically shown or described. The same may also be varied in many ways. Such variations are not to be regarded as a departure from the disclosure, and all such modifications are intended to be included within the scope of the disclosure.
This application is a continuation that claims the benefit of U.S. Provisional Application No. 61/931,827 filed on Jan. 27, 2014. The entire disclosure of the above application is incorporated herein by reference.
Number | Date | Country | |
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61931827 | Jan 2014 | US |