The present invention relates to a novel method and fastener for joining composite honeycomb panels. More particularly, a pointed fastener is provided to penetrate the internal cell structure of honeycomb construction panels without destroying the internal integrity of the honeycomb and without requiring drilling of bores through selected panels prior to insertion of the fasteners.
Existing fasteners utilized in the assembly of the T or L joints with honeycomb panels have been blunt-nosed and have required drilling bores through the first panel and the perpendicularly abutting panel before the insertion of the blunt-nosed, hollow, tubular fastener. After the fastener is in place through the predrilled bores, an adhesive or anchoring material is injected through the center of the hollow fastener and into the internal cell structure. U.S. Pat. No. 4,370,372 teaches currently utilized technologies.
With the introduction of computer numerically controlled (CNC) technology, there has arisen a need to modify the joining processes with existing honeycomb panels. CNC machines precut composite honeycomb panels and pre-drill holes or bores in the flat panel according to design standards. However, abutting panels are not predrilled. Thus, in order to join a first, flat panel with a perpendicularly abutting panel, the panels are first secured in a jig to properly align the panels for drilling (through the predrilled bore into the undrilled abutting panel) and for the insertion of the blunt-nosed fastener.
One embodiment of the present invention eliminates the necessity to pre-drill the abutting panel. A small, pointed fastener of one embodiment of the present invention provides the capability for penetrating the outer sheet member of an abutting composite honeycomb panel, passing through the internal cell structure of the abutting panel without collapsing or destroying the cell integrity in the abutting panel, and joining the predrilled flat panel with the abutting panel. It further allows for the elimination of clumsy and expensive jigs or frames for holding the panel cabinetry during fabrication.
A second panel 40 of similar construction is shown in
The first step in securing panels 30 and 40 in an abutting arrangement is to form all fastener bores 31 at right angles to the plane of panel 30 according to specifications of the design standard. This is most effectively accomplished by the use of computer numerically controlled (CNC) machines, but may be accomplished by other drilling or punching technologies. The predrilled bores 31 are the same diameter as the fastener 11 to allow for ready slidable insertion of the fastener 11 through the bore 31.
Typically, the fastener 11 is a relatively rigid aluminum tube one-and-a-half (1½) to five (5) inches long with a uniform body diameter of {fraction (3/16)} inch to ½ inch. The discharge openings 221 are a serial of {fraction (3/32)} inch (diameter) longitudinally and peripherally spaced circular apertures. The pointed end 181 has a plurality of slotted openings 191 ⅜ inch to one inch in length peripherally disposed. While the fastener is generally metal, other stiff or rigid substitute material compositions may be used.
It should be understood that the diameter of the fastener 11 is greater than the diameter of the cells 34 and 341 so that as the pointed end 191 of the fastener penetrates the abutting panel 40, it creates its own bore. Surrounding cells are ruptured in the same direction as the inserted fastener. This rupturing action creates disjoined cell wall sections 351 which urge against the fastener 11 to cause a frictional force to keep the fastener from disengaging from the penetrated core section. Further, the outer surface of the fastener 11 may be provided with one or more knurled sections 60 which cooperate with the disjoined cell walls 351 to enhance the retention of the fastener in the penetrated bore until the anchoring material is injected and hardens.
It should be noted that the cell core 321 has not collapsed and the overall integrity of the core is maintained except where the pointed end 181 has punctured a cell 341. A clamp or jig would normally be used to hold the panels 30 and 40 in an assembled/joined relation. However, with the present fasteners 11 and 111 this is not necessary as the joint end 181 penetrates the cell structure and creates its own bore.
One purpose of the pointed end 181 of the present invention is to allow for a controlled penetration and rupturing of only the necessary cells.
Although the invention has been described with reference to a specific embodiment, this description is not meant to be construed in a limiting sense. On the contrary, various modifications of the disclosed embodiments will become apparent to those skilled in the art upon reference to the description of the invention. It is therefore contemplated that the appended claims will cover such modifications, alternatives, and equivalents that fall within the true spirit and scope of the invention.
Number | Name | Date | Kind |
---|---|---|---|
4224971 | Muller et al. | Sep 1980 | A |
4370372 | Higgins et al. | Jan 1983 | A |
4712957 | Edwards et al. | Dec 1987 | A |
5145301 | Yamamoto | Sep 1992 | A |
5209805 | Spraggins | May 1993 | A |
Number | Date | Country |
---|---|---|
3733621 | Apr 1989 | DE |
Number | Date | Country | |
---|---|---|---|
20030152438 A1 | Aug 2003 | US |