1. Field of the Invention
The present invention relates to the manufacturing of composite parts, particularly; to the use of a heat-shrinkable sleeve during the manufacturing of composite parts as a release layer on tooling, or to provide a compression force on the composite part.
2. Description of Related Art
Prior art methods for molding a composite structure around a tool, such as a mandrel, have required tape wrapping or painting the mandrel with a release coating. The tape and/or paint layer protects the composite part from sticking to the mandrel. Similarly, the prior art teaches tape wrapping the composite after molding to provide a consolidation force to the composite. However, such taping and painting methods are time consuming and expensive. Further, such processes are not easily controlled.
Applicants have determined that one way to avoid tape wrapping and painting a mandrel, or tape wrapping a molded composite, is to employ a heat-shrinkable sleeve having self-releasing properties. Continuously molded heat-shrinkable sleeves are known for other applications in the prior art, however the material for such sleeves is expensive and the processes to produce them are time consuming and expensive. Furthermore, such sleeves would generally require a release coating.
To overcome deficiencies in the prior art, applicants have invented a novel heat-shrinkable sleeve and method for using the same during the manufacturing process of composite parts.
In a first aspect there is provided an apparatus comprising a heat-shrinkable sleeve. The heat shrinkable-sleeve has an inner surface and an outer surface and a linear seam. The sleeve contracts along a diameter of the sleeve upon application of heat to the sleeve, and the sleeve comprises at least one material selected from ETFE, ECTFE, FEP, PFA, MFA, PVDF, PVF, PTFE, Nylon, BOPP, or PMP. The heat shrinkable sleeve can comprise multiple layers of heat-shrinkable material and can shrink in a machine direction or grow in a machine direction.
In another aspect there is provided a method of manufacturing a composite part. The method comprises placing a heat-shrinkable sleeve over a tool prior to placement of material to be formed into the composite part on the heat-shrinkable sleeve.
In an even further aspect there is provided a method of manufacturing a composite part. The method comprises placing a heat-shrinkable sleeve over a material to be formed into a composite part and applying heat to the heat-shrinkable sleeve to cause the heat-shrinkable sleeve to shrink to fit the composite part. In one embodiment, the heat-shrinkable sleeve applies a consolidating force to the composite part during curing, and in another embodiment the heat-shrinkable sleeve is used as a release layer.
In the foregoing methods, the heat-shrinkable sleeve has an inner surface and an outer surface and a linear seam. The sleeve comprises at least one heat-shrinkable material, and the sleeve contracts along a diameter of the sleeve upon application of heat to the sleeve. The heat-shrinkable sleeve can comprise multiple layers of heat-shrinkable material. The inner and/or the outer surface can be self-releasing or have a release coating. Further, the heat-shrinkable sleeve can either grow or shrink in a machine direction.
The foregoing and other features and advantages of the present invention will become apparent to those skilled in the art to which the present invention relates upon reading the following description with reference to the accompanying drawings, in which:
An example embodiment of a device that incorporates aspects of the present invention is shown in the drawings. It is to be appreciated that the shown example is not intended to be a limitation on the present invention. For example, one or more aspects of the present invention can be utilized in other embodiments and even other types of devices.
A heat-shrinkable sleeve 3 is provided as shown in
The heat-shrinkable sleeve 3 can be constructed of a material that can shrink in the transverse direction, shrink slightly or not at all in the machine direction, or grow in the machine direction. Some heat-shrinkable materials for the heat-shrinkable sleeve 3 can be polyester, or polyester-glycol films such as PETG. A further list of materials useful in the present invention includes other heat-shrinkable materials, such as, for example, PEEK, PEI, PSU, PPSU, PPS, polyimides and the like. The material may also be a multi-layer sheet of heat-shrinkable materials.
In some embodiments, the heat-shrinkable material 1 also exhibits self-releasing characteristics. The terms release and self-releasing as used herein are intended to refer to a sleeve that does not adhere to, or allows for ease of removal of the sleeve from material with which the sleeve comes into contact. Thus, a self-releasing sleeve can be made of a material that does not adhere to, or is easily released from, material with which the sleeve will be brought into contact, without requiring any additional release material. Such materials can be, for example, ETFE, ECTFE, FEP, PFA, MFA, PVDF, PVF, PTFE, Nylon, BOPP, PMP or multi-layer sheets using a combination of the foregoing materials, such as ETFE-Nylon-ETFE or FEP-PTFE, for example.
A heat-shrinkable sleeve 3 having a linear overlap seam 5, as discussed herein, can be used in the manufacture of composite parts, among other things. As depicted in
The heat-shrinkable sleeve 3 may also be used as a release layer on the outside of a composite part 9, such as shown in
In addition the heat-shrinkable sleeve 3 as described herein also can be used to provide a consolidating force to a composite part 9 during the manufacturing process. The heat-shrinkable sleeve 3 may be placed over a prior placed release layer on the composite part 9, or the heat-shrinkable sleeve 3 may be placed directly over the material to be used to form the composite part 9. When heat 25 is applied to the heat-shrinkable sleeve 3 during the curing process, the sleeve material will shrink in the transverse direction causing the sleeve to contract in its diameter 27. Contraction in the sleeve diameter can cause the sleeve to apply a consolidating force to the outside of the composite part 9 while the composite part is curing, helping consolidation of the composite.
The rate and amount of shrinkage in the transverse direction of the sleeve material can be controlled to ensure the precise amount of contraction in the sleeve's diameter, ensuring the desired consolidating force is applied to the composite part 9. Likewise, the growth or shrinkage in the machine direction along the sleeve can also be controlled according to the needs of the process. As one of ordinary skill in the art will appreciate, control of shrinkage can be based on the orientation of the sleeve material and its base properties, which include, but are not limited to, the machine direction shrinkage, transverse direction shrinkage, shrink force, sleeve material thickness, number of layers of sleeving employed, and the temperature and time of heat application, for example. A sleeve that can shrink in the machine direction could be useful for curved parts, as would a sleeve that could grow in a machine direction. Among other things, growth or shrinkage in the machine direction would help eliminate any potential wrinkles in the shrink sleeve on the inside or outside surfaces of the part.
Although it is preferred that the material of the heat-shrinkable sleeve 3 is self-releasing, the material may have a release coating 23 on a contact surface 19 as shown in example
After employing the heat-shrinkable sleeve 3 in a process of manufacturing a composite part 9 as described herein, the heat-shrinkable sleeve 3 can be removed from the composite part 9 as depicted in
The invention has been described with reference to various example embodiments. Obviously, modifications and alterations will occur to others upon a reading and understanding of this specification. It is intended to include all such modifications and alterations insofar as they come within the scope of the appended claims or the equivalents thereof.
This application claims the benefit of U.S. Provisional Application No. 60/106,673 filed Oct. 20, 2008.
Number | Date | Country | |
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61106673 | Oct 2008 | US |
Number | Date | Country | |
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Parent | 12582484 | Oct 2009 | US |
Child | 13495123 | US |