The present invention in general relates to compression molding and in particular to a fastener insert to improve manufacturability of irregular features in sheet molding compound and pre-preg compression molding.
Composite materials are engineered or naturally occurring materials made from two or more constituent materials with significantly different physical or chemical properties which remain separate and distinct at the macroscopic or microscopic scale within the finished structure. There are two categories of constituent materials: matrix and reinforcement. At least one portion of each type is required. The matrix material surrounds and supports the reinforcement materials by maintaining their relative positions. The reinforcements impart their special mechanical and physical properties to enhance the matrix properties. A synergism produces material properties unavailable from the individual constituent materials, while the wide variety of matrix and strengthening materials allows the designer of the product or structure to choose an optimum combination.
Commercially produced composites often use a polymer matrix material often called a resin solution. There are many different polymers available depending upon the starting raw ingredients which may be placed into several broad categories, each with numerous variations. Examples of the most common categories for categorizing polymers include polyester, vinyl ester, epoxy, phenolic, polyimide, polyamide, polypropylene, PEEK, and others.
The reinforcement materials for composites are typically fibers but also may be commonly ground minerals. Fiber-reinforced composite materials can be divided into two main categories normally referred to as short fiber-reinforced materials and continuous fiber-reinforced materials. Continuous reinforced materials often constitute a layered or laminated structure. The woven and continuous fiber styles are typically available in a variety of forms, being pre-impregnated with the given matrix (resin), dry, uni-directional tapes of various widths, plain weave, harness satins, braided, and stitched. Various methods have been developed to reduce the resin content of the composite material, by increasing the fiber content. Typically, composite materials may have a ratio that ranges from 60% resin and 40% fiber to a composite with 40% resin and 60% fiber content. The strength of a product formed with composites is greatly dependent on the ratio of resin to reinforcement material.
Pre-preg is the general term used for “pre-impregnated” composite fibers where a material, such as epoxy is already present. As described above, pre-preg fibers usually have of a weave or are uni-directional. Pre-preg materials already contain an amount of the matrix material used to bond the pre-impregnated fibers together and to other components during manufacture. Pre-preg materials are mostly stored in cooled areas since activation is most commonly done by heat. Hence, composite structures built of pre-pregs typically require an oven or autoclave to cure out.
Pre-preg compression molding utilizes pre-preg materials, which are typically made from continuous fiber reinforced materials, that have been cut into sheets or plies with specific patterns. During the compression molding process, the pre-preg plies are hand assembled into a preform made up of multiple layers of the pre-preg ply material, and then the preform is placed into a mold and compressed, which consolidates the layers of pre-preg material and cures the pre-preg. However, since pre-preg material typically has a continuous fiber format, the pre-preg material typically will not flow in the mold to any significant degree. Consequently, when there are irregular thicknesses or features that standout from the surface, such as a fastener boss (as best seen in
Thus, there exists a need for devices and methods that form more reliable and robust surface features that are free of material voiding, where the surface features standout above a compression molded surface including surface features such as bosses that accommodate fastener inserts.
An insert is provided that has a cylindrical center space extending from a counter bore within an interior of the insert with a series of threads. The center space is defined by cylinder wall to accommodate a fastener. A multi-faced region with a plurality of flat faces is provided at the distal end of the recessed area. A tapered region extends from the multi-faced region that terminates in a sharpened leading edge.
A method for forming an elevated surface feature for compression molded assemblies includes the placement of an afore-mentioned insert onto an actuated fixture pin with the pin initially in a retracted position. An upper portion of a mold configured with said retracted actuated fixture pin over a preform of pre-preg plies placed on the bottom portion of the mold is then closed. The fixture pin is actuated towards the pre-preg plies when a flowable material fills a molding cavity in the upper portion of the mold. The cavity is configured to form the elevated surface feature with the advancing action of the insert packs out the surface feature under the pressure of the pin to eliminate porosity in the elevated surface feature in the molding cavity.
The present invention has utility as a device and method to form more reliable and robust surface features for compression molded assemblies that are free of material voiding, where the surface features standout above the molded surface including surface features such as bosses that accommodate fastener inserts.
Embodiments of the invention provide an insert that is insert-molded into features of compression molded designs such as in irregular or elevated surfaces whereby the inventive insert is placed onto a pin that can be actuated with a hydraulic cylinder to advance the pin or retract the pin. Initially during the molding process, an embodiment of the inventive insert is placed onto a fixture pin and the pin is in a retracted position. Subsequently, as the mold is closed onto a preform of pre-preg plies, the pin holding an embodiment of the inventive insert is in a retracted position to allow for more space for additional material to move into position within the elevated surface feature, such as a boss, as shown in
Referring now to the figures,
The foregoing description is illustrative of particular embodiments of the invention, but is not meant to be a limitation upon the practice thereof. The following claims, including all equivalents thereof, are intended to define the scope of the invention.
This application claims priority of U.S. Provisional Patent Application Ser. No. 61/650,097 filed May 22, 2012, which is incorporated herein by reference.
Filing Document | Filing Date | Country | Kind |
---|---|---|---|
PCT/US2013/042257 | 5/22/2013 | WO | 00 |
Publishing Document | Publishing Date | Country | Kind |
---|---|---|---|
WO2013/177298 | 11/28/2013 | WO | A |
Number | Name | Date | Kind |
---|---|---|---|
979361 | Vulpescu | Dec 1910 | A |
1456215 | Brightman | May 1923 | A |
2972730 | Abrams | Feb 1961 | A |
3364806 | Chaivre | Jan 1968 | A |
3530921 | Ernest | Sep 1970 | A |
3742995 | Confer et al. | Jul 1973 | A |
3960047 | Liffick | Jun 1976 | A |
4143578 | Becker | Mar 1979 | A |
4673542 | Wigner et al. | Jun 1987 | A |
4869440 | Toral et al. | Sep 1989 | A |
5391029 | Fardell | Feb 1995 | A |
5492452 | Kirsch et al. | Feb 1996 | A |
5800109 | Carruthers | Sep 1998 | A |
5810534 | Carlisle et al. | Sep 1998 | A |
5870870 | Utzman | Feb 1999 | A |
5890842 | Dahill | Apr 1999 | A |
D427511 | Weld | Jul 2000 | S |
6173460 | Mitchell | Jan 2001 | B1 |
6244073 | Kaping, Jr. | Jun 2001 | B1 |
6692207 | Bailey | Feb 2004 | B1 |
7077613 | Rudolph et al. | Jul 2006 | B2 |
D549568 | Schaeffer | Aug 2007 | S |
7284940 | Lee | Oct 2007 | B2 |
7374384 | Sutt, Jr. | May 2008 | B2 |
7665942 | Tadros et al. | Feb 2010 | B2 |
7682116 | Cabrele | Mar 2010 | B2 |
7955024 | Driscoll et al. | Jun 2011 | B2 |
20060276905 | Calamel | Dec 2006 | A1 |
20110281133 | Moessinger | Nov 2011 | A1 |
20120168994 | Dai | Jul 2012 | A1 |
Number | Date | Country |
---|---|---|
1969833 | Oct 1967 | DE |
102006010148 | Sep 2007 | DE |
1447205 | Aug 2004 | EP |
376704 | Jul 1932 | GB |
2011116890 | Sep 2011 | WO |
Entry |
---|
Extended Search Report from European Patent Office dated Dec. 12, 2015 for application No. PCT/US2013/042257. |
Number | Date | Country | |
---|---|---|---|
20150176632 A1 | Jun 2015 | US |
Number | Date | Country | |
---|---|---|---|
61650097 | May 2012 | US |