The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
Jul. 28, 2020

Filed:

Dec. 22, 2016
Applicant:

Toray Industries, Inc., Tokyo, JP;

Inventors:

Ichiro Taketa, Ehime, JP;

Shiori Kawamoto, Ehime, JP;

Hiroaki Sakata, Ehime, JP;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B29C 70/20 (2006.01); B32B 5/24 (2006.01); B32B 27/28 (2006.01); B32B 27/38 (2006.01); B32B 27/34 (2006.01); B32B 27/08 (2006.01); B32B 5/02 (2006.01); C08J 5/24 (2006.01); C08J 5/04 (2006.01); B32B 1/00 (2006.01); B32B 5/12 (2006.01); B32B 5/26 (2006.01); B32B 27/12 (2006.01); B29K 105/08 (2006.01); B29K 307/04 (2006.01);
U.S. Cl.
CPC ...
B29C 70/205 (2013.01); B32B 1/00 (2013.01); B32B 5/022 (2013.01); B32B 5/12 (2013.01); B32B 5/24 (2013.01); B32B 5/26 (2013.01); B32B 27/08 (2013.01); B32B 27/12 (2013.01); B32B 27/286 (2013.01); B32B 27/34 (2013.01); B32B 27/38 (2013.01); C08J 5/042 (2013.01); C08J 5/24 (2013.01); B29K 2105/0881 (2013.01); B29K 2307/04 (2013.01); B32B 2250/03 (2013.01); B32B 2250/05 (2013.01); B32B 2250/40 (2013.01); B32B 2255/02 (2013.01); B32B 2255/26 (2013.01); B32B 2260/021 (2013.01); B32B 2260/023 (2013.01); B32B 2260/046 (2013.01); B32B 2262/106 (2013.01); B32B 2264/0264 (2013.01); B32B 2270/00 (2013.01); B32B 2307/516 (2013.01); B32B 2307/558 (2013.01); B32B 2307/718 (2013.01); B32B 2307/732 (2013.01); B32B 2605/18 (2013.01); C08J 2363/00 (2013.01);
Abstract

A prepreg includes a fiber layer containing unidirectionally arranged carbon fibers impregnated with a thermosetting resin and a resin layer existing on at least one side of the fiber layer and containing a thermosetting resin and a thermoplastic resin insoluble in the thermosetting resin. The prepreg contains carbon fibers having an areal weight of fibers of 120 to 300 g/mand has a weight fraction of resin of 25 to 50 mass %. An extreme value frequency of a surface geometry along a straight line perpendicular to the fibers of the prepreg is 30 points/mm or less when the prepreg has been exposed, for 24 hours, to a temperature at which a coefficient of interlayer friction is the lowest. Using sheets of the prepreg which are laid up, the coefficient of interlayer friction of the prepreg is measured at 10° C. intervals in a temperature range of 40 to 80° C. under the conditions: a pulling speed of 0.2 mm/min, a perpendicular stress of 0.1 bar, and a pulling displacement of 1 mm. The prepreg is suitable for aircraft structural members that exhibits high impact strength as a fiber-reinforced plastic and has excellent drapeability when formed into a prepreg laminate which is made to conform to a three dimensional shape.


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