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Continuous fiber thermoplastic prepregA pultrusion machine employing a corrugated impregnator vessel to immerse multiple, continuous strand, fiber tow in an impregnating material, and an adjustable metered exit orifice for the impregnator vessel to control the quantity of impregnating material retained by the impregnated fibers, is provided. An adjustable height insert retains transverse rod elements within each depression of the corrugated vessel to maintain the individual fiber tows spread and in contact with the vessel bottom. A series of elongated heating dies, transversely disposed on the pultrusion machine and having flat heating surfaces with radiused edges, ensure adequate temperature exposed dwell time and exert adequate pressure on the impregnated fiber tows, to provide the desired thickness and fiber/resin ratio in the prepreg formed. The prepreg passing through the pulling mechanism is wound on a suitable take-up spool for subsequent use. A formula is derived for determining the cross sectional area opening of the metering device. A modification in the heating die system employs a heated nip roller in lieu of one of the pressure applying flat dies.
Document ID
19930015408
Acquisition Source
Legacy CDMS
Document Type
Other - Patent
Authors
Wilson, Maywood L.
(NASA Langley Research Center Hampton, VA, United States)
Johnson, Gary S.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 15, 2013
Publication Date
April 27, 1993
Subject Category
Composite Materials
Report/Patent Number
Patent Number: NASA-CASE-LAR-14459-1
Patent Number: US-PATENT-5,205,898
Patent Application Number: US-PATENT-APPL-SN-613046
Accession Number
93N24597
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
NASA-CASE-LAR-14459-1|US-PATENT-5,205,898
Patent Application
US-PATENT-APPL-SN-613046
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