It is well known to use large weather-resistant covers for a variety of vehicles or watercraft in a number of industries. Often, these covers need to be supported over the underlying vehicle or watercraft and finding ways to support the covers from underneath or from above has challenged these industries for decades. One of the problems to be solved is how to securely and durably engage these underlying supports without causing damage to the cover material. Various hardware components have been devised to overcome these challenges. Various methods to attach these hardware components are employed. Methods to attach hardware to fabric or other flexible materials may include welding, mechanical fastening, crimping, sewing or gluing. Large coverings present many challenges for installing hardware. Access to the perimeter of the covering is simple for installing hardware. Many installation methods work well in this situation due to the ease of presenting a tool such as a sewing machine, welder, fixture or crimping press to the cover. Installing hardware in the center of a large covering can be difficult. A sewing machine typically has an arm less than 20″, leaving little space for moving a large covering. Long arm sewing machines are expensive and are not commonly used in smaller industrial sewing businesses.
Covering supports are frequently located in the center of large panels. Many coverings may have reinforcing sewn in areas where a support is located. The support may be held in place by a snap, webbing or other hardware to secure the support in place relative to the covering.
In order to place hardware in the center of a panel, many hardware components for coverings rely on mechanical fastening to secure the hardware in place due to the challenges with using a tool such as a sewing machine in this area.
In order for a mechanically fastened hardware component to work in these applications, the securing hardware must be manufactured from rigid materials. Screw threads, holes and bosses allow these multi-part assemblies to bolt, screw, crimp or clamp to the covering. Mechanically fastening a rigid component to a flexible material requires local reinforcing to prevent hardware from wearing through the covering.
Although fabrication fixtures that allow relative motion between a work piece and a tool are present in other industries such as woodworking and metal, it is difficult to address circular sewing operations in the middle of a large workpiece.
These hardware components have multiple drawbacks. Multiple components in the mechanically fastened assembly add cost and complexity to the manufacturing process. Clamping methods reduce the strength of the covering. Rigid attachments create wear points when the fabric is not aligned with the attachment. Fasteners point load the fabric. Rigid components break when dropped or hit and may crack at low temperatures. Local reinforcing that is added at the installation point adds cost.
Improvements on the prior are desirable to overcome these and other limitations.
While the prior art provides for various cover insert hardware, no design of the prior art includes all of the features of the present disclosure. The present disclosure overcomes the limitations of the prior art by providing a hardware component which may be manufactured as a single, elastomeric, molded component. Such a design overcomes the limitations of the prior art by providing a durable design that is flexible, aligns with loads, distributes load about the hardware and installs easily. By doing so, this design does not cause excess wear on the cover material attached to the cap.
Additionally, the design of the present disclosure is unique because it overcomes the challenges associated with sewing support receivers onto large covers. Sewing a flange onto a large cover is difficult due to several reasons. Cover supports are typically located in the center of the cover where it is the most difficult to sew. Aligning hardware on large covers is difficult due to the inability of an operator to see through the hardware component while sewing. Rotating a part while sewing requires constant realigning of parts. This design solves this manufacturing problem by way of a snap flange designed into the part that that fixes the material in place during the assembly process.
Although typically manufactured as a one-piece unit, the support receiver can be described as comprising three main parts: a central boss which can be configured to accept a support, a sewing flange, and a snap flange. The flange may contain a plurality of external and internal supporting ribs.
The accompanying drawings, which are included to provide further understanding of the disclosure and are incorporated in and constitute a part of this specification illustrate embodiments of the disclosure, and together with the description, serve to explain the principles of the disclosure.
In the Drawings:
Reference will now be made in detail to the embodiments of the present disclosure, examples of which are illustrated in the accompanying drawings. Wherever possible, the same reference numbers will be used throughout the specification to refer to the same or like parts.
The present disclosure provides for a support receiver design manufactured as one piece from one or more elastomeric materials. One embodiment containing vented openings of such a support receiver and associated installation hardware is illustrated by
Referring to
The support receiver 100 may include a base 120 concentric to the central axis 110 of the hollow boss 105. The base 120 may further include a ridge 125 configured to prevent water and other materials from entering the support receiver 100. A first sewing flange 130 having a first diameter 130 and a second snap fit flange having a second diameter 131 may be radially disposed around the perimeter of the hollow boss 105. In one embodiment, the snap fit flange 131 may be located on the underside of the first sewing flange 130. The addition of the snap fit flange 131 overcomes the limitations of the prior art with respect to an operator not being able to see through the support receiver 100. This transition point, between the support receiver and the covering material, may be soft and should not pierce, abrade, or excessively wear the fabric. The flexibility of the sewing flange 130 also helps to prevent premature wear at this transition point.
The support receiver 100 may further include a cap 135. The cap 135 may include a plurality of external supporting ribs 142 and internal supporting ribs 140. The internal supporting ribs 140 may be operably coupled to the base 120 to thereby form a vent opening 146 between the cap 135 and the base 120. The external supporting ribs 142 may be coupled to the bottom of the cap. These supporting ribs 140 and 142 distribute the weight and stress from the central hollow boss 105 over the support receiver 100, to the perimeter of the base 120, and to the fabric. The weight and stress put on the support receiver by the support pole is thereby distributed to over a large area. Such a design is beneficial over designs of the prior art that do not use support ribs or similar structures and provides for stronger, more durable coverings.
In one embodiment 100, illustrated by
Another embodiment 300 of a support receiver according to the present disclosure without vent openings is illustrated by
Referring to
Referring to
Referring to
While the disclosure has been described in detail in reference to specific embodiments thereof, it will be apparent to one skilled in the art that various changes and modifications can be made therein without departing from the spirit and scope of the embodiments. Thus, it is intended that the present disclosure cover the modifications and variations of this disclosure provided they come within the scope of the appended claims and their equivalents.
The present application is a non-provisional application claiming priority to Provisional Application Ser. No. 62/446,402, filed on Jan. 14, 2017, the disclosure of which is incorporated herein by reference. Since the one year anniversary of this provisional filing fell on a Sunday, Jan. 14, 2018, followed by a US federal holiday on Monday, Jan. 15, 2018, this application may be filed no later than Tuesday, Jan. 16, 2018, while still preserving the priority claim.
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Number | Date | Country | |
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20180202089 A1 | Jul 2018 | US |
Number | Date | Country | |
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62446402 | Jan 2017 | US |