1. Field of the Invention
The present invention relates to a screw for use in composite wood, and in particular a screw including axial wings for granulating the composite wood as the screw is driven into the material.
2. Description of the Related Art
A deck adds beauty, utility and value to a home or business. Traditionally, woods such as pressure-treated yellow pine have been used for the structure of the deck for their low cost and high resistance to insect and moisture damage. However, yellow pine decks tend to check, split, warp and/or splinter after prolonged exposure to the elements. Additionally, the chemical insecticide-preservative may present health issues. It is also known to form decks from redwood, cedar and tropical hardwood. While these woods are better able to resist the elements, they are a more costly alternative and require proper maintenance and care to maintain their appearance.
In response to some of the deficiencies with pure wood decks, many homeowners and contractors are now specifying alternative materials for decking, including for example engineered vinyl systems and plastic-wood composites. Plastic-wood composites typically blend 30% to 50% recycled plastic with wood fibers. Composite woods are becoming more popular for use in decking and railings due to their low maintenance, resistance to moisture rot, insects and UV rays, and the fact that they do not splinter. A sample of a composite wood is disclosed in U.S. Pat. No. 5,088,910 to Goforth, entitled, “System For Making Synthetic Wood Products From Recycled Materials.”
Conventional tools and screw fasteners can be used to secure composite wood, for example, to underlying joists in a decking application. However, one problem with the use of conventional screws with composite woods is an event referred to as “flagging.” When a conventional wood screw is driven into composite wood, the composite wood gets displaced radially outward from the screw. Thus, for example, when the head of the screw is driven into the composite material to form the counterbore, the composite material at the surface is forced upward, out of the screw hole. The result is flagging, where the upper surface of the composite material is deformed with a raised annular ring about the screw head. This raised annular ring presents an undesirable appearance.
One solution to the problem of flagging is proposed in U.S. Pat. No. 6,616,391 to Druschel, entitled, “Screw For Plastic Composite Lumber.” That reference discloses a screw having a bore consisting of radially projecting helical flutes wrapped around the screw shank. The helical flutes have an opposed helical orientation to the screw threads. This opposed relationship causes the flutes to push displaced plastic lumber material down along the shank, away from the screw head. Thus, the flutes bore a space beneath the screw head.
Another problem with driving conventional screws into composite materials is that the material is relatively dense, especially where the material has been displaced radially outward by the screw. The result is that it is difficult to create a counterbore where the head is countersunk to be at least flush with the surface. Often, the screw threads strip before the screw head is pulled into the material.
The present invention, roughly described, relates to a tapping screw for use in composite wood material. The tapping screw includes wings extending radially outward from the screw shank. In embodiments, there may be a pair of wings spaced 180° from each other. The wings may extend from the shank to a diameter just less than the diameter of the screw head. The wings may be positioned at various locations along the shank, for example just above the screw threads or just below the screw head.
As the winged screw is driven down into a composite wood material, the wings shear off the composite material and granulate the composite material with which the wings come into contact to form a counterbore capable of receiving the screw head. As the granulated material moves upward along the shank, when the screw head enters the composite material, the granulated material at the top of the screw bore is forced out of the screw bore and is removed. The counterbore created by the wings prevents the formation of an annular ring at the surface and allows the screw head to be countersunk into the composite material. Granulated material which is not removed from the counterbore formed by the wings may be pulled down into the screw hole by means of annular rings formed around the diameter of the screw.
The present invention will now be described with reference to
Referring now to
Tip 104 may be sharpened to an angle between 20° and 30°, and more particularly about 26°, in embodiments of the invention. It is understood that tip 104 may be sharpened to angles smaller than 20° and larger than 30° in alternative embodiments. Head 106 includes a shaped recessed section 108 (
The shank 102 may have a diameter of 0.133 inches, though it may be larger or smaller than that in alternative embodiments. Shank 102 may further include four distinct sections. A first section adjacent to tip 104 may include threads 112 for pulling tapping screw 100 into a composite wood upon rotation of screw 100. Threads 112 may have a pitch of ten threads per inch, but it is understood that the threads may have a higher or smaller pitch than that in alternative embodiments. The outer diameter of threads 112 may be 0.19 inches in embodiments of the invention. It is understood that the outer diameter of the threads may vary from that in further embodiments of the invention.
Shank 102 may include a second section having wings 116 for granulating the wood composite material as screw 100 is driven into the wood composite material as explained hereinafter. Shank 102 may further include a third section between threads 112 and the head 106 having annular rings 118, each ring 118 being oriented in a plane generally perpendicular to an axis of rotation of screw 100. In embodiments, shank 102 may include four annular rings 118 each including an outer diameter of 0.19 inches and each being spaced from each other approximately 0.1 inches. It is understood that the outer diameter and spacing of annular rings 118 may vary in alternative embodiments of the present invention. In further embodiments of the present invention, such as for example shown in
Shank 102 may further include a blank section 120 between collar 110 and the annular rings 118. Blank section 120 is devoid of threads and rings, and may have a diameter of approximately 0.147 inches. It is understood that blank section 120 may have a diameter larger or smaller than 0.147 inches in alternative embodiments of the present invention.
According to embodiments of the present invention, screw 100 may include a pair of diametrically opposed wings 116 formed along the length of shank 102. In embodiments, wings 116 may be located between threads 112 and annular rings 118. However, it is understood that wings 116 may be located at a variety of positions along shank 102. For example, as shown in
Wings 116 have a length, parallel to the axis of rotation, of 0.144 inches, though the length may be greater or smaller than that in alternative embodiments of the present invention. As seen for example in
Wings 116 may be evenly spaced around the diameter of shank 102. Thus, in an embodiment including two wings, the wings 116 may be 180° apart from each other. It is understood that more than two wings may be provided around shank 102 in further embodiments of the present invention. In one embodiment each wing 116 may have a thickness of approximately 0.018 inches. However, it is understood that the thickness of each of the wings 116 may be less than or greater than that in further embodiments of the present invention. In embodiments, wings 116 may be oriented parallel to the axis of rotation of tapping screw 100. However, as shown for example in
The operation of wings 116 will now be explained with reference to
In a further embodiment of the present invention (not shown), the wings 116 may be formed on screw 100 with a predetermined yield strength such that, when wings 116 enter a predetermined distance into the composite material 130, the wings 116 shear off upon continued driving of the screw 100 into material 130. Upon being sheared off, no further granulation of the material 130 is provided by wings 116. Thus the depth to which wings 116 granulate the material 130 is predetermined and controlled.
The foregoing detailed description of the invention has been presented for purposes of illustration and description. It is not intended to be exhaustive or to limit the invention to the precise form disclosed. Many modifications and variations are possible in light of the above teaching. The described embodiments were chosen in order to best explain the principles of the invention and its practical application to thereby enable others skilled in the art to best utilize the invention in various embodiments and with various modifications as are suited to the particular use contemplated. It is intended that the scope of the invention be defined by the claims appended hereto.