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Method for Fabricating Composite Structures Using Pultrusion ProcessingA method for fabricating composite structures at a low-cost, moderate-to-high production rate. A first embodiment of the method includes employing a continuous press forming fabrication process. A second embodiment of the method includes employing a pultrusion process for obtaining composite structures. The methods include coating yarns with matrix material, weaving the yarn into fabric to produce a continuous fabric supply and feeding multiple layers of net-shaped fabrics having optimally oriented fibers into a debulking tool to form an undebulked preform. The continuous press forming fabrication process includes partially debulking the preform, cutting the partially debulked preform and debulking the partially debulked preform to form a netshape. An electron-beam or similar technique then cures the structure. The pultrusion fabric process includes feeding the undebulked preform into a heated die and gradually debulking the undebulked preform. The undebulked preform in the heated die changes dimension until a desired cross-sectional dimension is achieved. This process further includes obtaining a net-shaped infiltrated uncured preform, cutting the uncured preform to a desired length and electronbeam curing (or similar technique) the uncured preform. These fabrication methods produce superior structures formed at higher production rates, resulting in lower cost and high structural performance.
Document ID
20000050219
Acquisition Source
Langley Research Center
Document Type
Other - Patent
Authors
Farley, Gary L.
(NASA Langley Research Center Hampton, VA United States)
Date Acquired
September 7, 2013
Publication Date
March 7, 2000
Subject Category
Composite Materials
Report/Patent Number
Patent Application Number: US-Patent-Appl-SN-511568
Patent Number: NASA-Case-6,033510
Patent Number: US-Patent-6,033,510
Patent Application Number: US-Patent-Appl-SN-933735
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
NASA-Case-6,033510|US-Patent-6,033,510
Patent Application
US-Patent-Appl-SN-511568|US-Patent-Appl-SN-933735
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