Curable prepregs with surface openings

Patent metadata

Field	Value
Publication number	US-10821680-B2
Application number	US-201916254151-A
Country	US
Kind code	B2
Filing date	Jan 22, 2019
Priority date	Dec 21, 2012
Publication date	Nov 3, 2020
Grant date	Nov 3, 2020

Abstract

Curable prepregs possessing enhanced ability for the removal of gases from within prepregs and between prepreg plies in a prepreg layup prior to and/or during consolidation and curing. Each curable prepreg is a resin-impregnated, woven fabric that has been subjected to a treatment to create an array of openings in at least one major surface. Furthermore, the location of the openings is specific to the weave pattern of the fabric.

First claim

What is claimed is:

1. A method for fabricating a curable composite material with an array of surface openings, the method comprising:
(a) partially impregnating a woven fabric with a curable, hot-melt resin such that a continuous resin film covers each face of the fabric and penetrates partially through the thickness of the fabric leaving an inner section of the fabric, in the thickness direction, substantially free of said resin,
wherein the woven fabric has two opposing faces and a weaving pattern in which a tow in a first weaving direction passes over another tow in a second weaving direction, then pass under an adjacent tow in the second weaving direction, and interstices are defined between adjacent tows; and
(b) heating the partially impregnated fabric so that the resin film on at least one face of the fabric becomes flowable, and subsequently, portions of the resin film over the interstices break open, thereby creating openings in the resin film that correspond to locations of the interstices,
wherein the openings are configured to provide fluid flow paths from the inner section of the fabric to at least one outer surface of the composite material, or from at least one outer surface of the composite material to the inner section, or from one outer surface of the composite material to an opposite surface, or combination thereof.

2. The method of claim 1 , wherein the outer surface of the resin film is covered with a release paper or polyester film during heating.

3. A method for fabricating a curable composite part comprising:
laying down a plurality of prepreg plies to form a prepreg layup, wherein at least some prepreg plies are porous prepreg plies with surface openings, and each porous prepreg ply is the composite material formed by the method according to claim 1 .

4. A method for fabricating a curable composite part comprising:
forming a broad composite material according to the method of claim 1 ;
cutting the composite material into prepreg plies of pre-determined sizes;
laying down the prepreg plies to form a prepreg layup,
wherein the heating step is carried out to form openings in the broad composite material before the material is cut.

Assignees

• Cytec Ind Inc

Inventors

• Roman Mark
• Howard Stephen J
• Boyd Jack D

Classifications

• B29C70/22 Primary

  oriented in at least two directions forming a two-dimensional [2D] structure · CPC title

• B29B15/12 Primary

  of reinforcements of indefinite length · CPC title

• C08J5/243

  using carbon fibres · CPC title

• D03D13/00

  Woven fabrics characterised by the special disposition of the warp or weft threads, e.g. with curved weft threads, with discontinuous warp threads, with diagonal warp or weft · CPC title

• B32B2262/10

  Inorganic fibres · CPC title