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Process for manufacturing liquefied methane |
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Nitrogen-methane separation process and system |
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Process for separating methane and nitrogen |
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Two-stage rectification for the separation of hydrocarbons |
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Process to produce liquid cryogen |
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High functional regenerated cellulose composition |
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Papermaking compositions, process using same, and paper produced therefrom |
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Fire-resistant strap fabric, article and method |
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Woven fabric having multi-layer structure and composite material comprising the woven fabric
| Details |
Inventors: Takenaka, Koji; Sato, Eiji;
Assignee: Asahi Kasei Kogyo Kabushiki Kaisha (Osaka, JP)
Primary Examiner: Cannon; James C.
Assistant Examiner:
Attorney, Agent or Firm: Finnegan, Henderson, Farabow, Garrett & Dunner
Disclosed is a woven fabric having a plurality of fabric layers which are integrated through combined portions formed by interlacing warps or wefts of one of adjacent layers of some of warps or wefts of said one layer and warps or wefts of the other layer or some of warps or wefts of said other layer with common wefts or warps, wherein a set of adjacent four layers comprises recurring structural units comprising (A) a part having one combined portion formed by intermediate two layers, (B) a first non-combined part having no combined portion, (C) a part having two combined portions formed by subsequent two layers, respectively, and (B) a second non-combined part having no combined portion. A honeycomb structure having cells of a shape of tetragons, hexagons or a combination thereof is formed among the entire layers when the multi-layer fabric is expanded. 40-100 wt. % of the fibers constituting the fabric are organic fibers which are infusible or have a melting point of at least 300.degree. C. and have an initial modulus of at least 250 g/d, and 0-60 wt. % of the fibers constituting the fabric are inorganic fibers or metal fibers. A composite material comprising the multi-layer fabric as a reinforcer and a thermoplastic resin as a matrix has good mechanical strengths and thermal resistance and is valuable, e.g., as a structural material for an aircraft. |
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DETAILED DESCRIPTION It is a primary object of the present invention to provide a woven fabric especially suitable for the production of a composite material which has a light weight, shows an excellent compression strength in a broad temperature range, is not broken when stress is imposed repeatedly, and has an excellent impact resistance, and further, to provide a composite material in which the above-mentioned properties are most effectively exerted, by using this woven fabric. More specifically, in accordance with one aspect of the present invention, there is provided a woven fabric having a multi-layer structure, which comprises a plurality of woven fabric layers which are integrated through combined portions formed by interlacing warps or wefts of one of adjacent woven fabric layers or some of warps or wefts of said one woven fabric layer and warps or wefts of the other woven fabric layer or some of warps or wefts of said other woven fabric layer with common wefts or warps, wherein a set of adjacent four woven fabric layers comprises recurring structural units comprising (A) a part having one combined portion formed by intermediate two woven fabric layers, (B) a first non-combined part having no combined portion, (C) a part having two combined portions each formed by adjacent two woven fabric layers, respectively, and (B) a second non-combined part having no combined portion; a honeycomb structure having a plurality of cells having a shape of tetragons, hexagons or a combination of tetragons and hexagons is formed among the entire woven fabric layers when the multi-layer woven fabric is expanded in the thickness direction; and 40 to 100% by weight of the fibers constituting the woven fabric are organic fibers which are infusible or have a melting point of at least 300. degree. C. and have an initial modulus of at least 250 g/d, and 0 to 60% by weight of the fibers constituting the woven fabric are inorganic fibers or metal fibers. In accordance with another aspect of the present invention, there is provided a composite material having a honeycomb structure, which comprises as a matrix a thermoplastic resin having a heat distortion temperature of at least 150
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