US2005138891A1PendingUtilityA1
Monolithic hurricane resistant structural panels made from low density composites
Priority: Oct 17, 2003Filed: Oct 14, 2004Published: Jun 30, 2005
Est. expiryOct 17, 2023(expired)· nominal 20-yr term from priority
E04C 2/22B29C 70/443E04C 2/36B29C 70/086B29C 70/865E04B 7/22
50
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Claims
Abstract
A three dimensional composite panel structure is provided having a thickness less than about 22.5 cm, overall density less than 0.2 g/cm, and exhibiting a global modulus greater than 1.2 GPa and stiffness greater than 15 kN-m 2 . The composite panel structure includes at least two fiber-reinforced mats interconnected in a spaced substantially parallel configuration by a skeletal web and a closed cell foam filling the spaces between the panels. The fiber-reinforced mats include a plurality of fibers in a low viscosity cured thermosetting resin matrix.
Claims
exact text as granted — not AI-modified1 . A three dimensional composite panel structure having a thickness less than about 22.5 cm, overall density less than 0.2 g/cm, and exhibiting a global modulus greater than 1.2 GPa and stiffness greater than 15 kN-m 2 , the composite panel structure comprising:
(a) at least two fiber-reinforced mats interconnected in a spaced substantially parallel configuration by a skeletal web; and (b) a closed cell foam filling the spaces between said fiber-reinforced mats; wherein said fiber-reinforced mats comprise a plurality of fibers in a low viscosity cured thermosetting resin matrix.
2 . The three dimensional composite panel structure of claim 1 wherein said panel is sized and shaped to form a unitary roof panel for a building.
3 . The three dimensional composite panel structure of claim 2 wherein said thermosetting resin is natural resin, a synthetic resin, or a combination thereof.
4 . The three dimensional composite panel structure of claim 2 , wherein the material of said resin is Acrylated Epoxidized Soybean Oil.
5 . The three dimensional composite panel structure of claim 2 wherein said closed cell foam is natural, synthetic, or combinations thereof.
6 . The three dimensional composite panel structure of claim 2 wherein said composite panel comprises resin in an amount of between about 30 and 40 wt %, fiber-reinforced mats in an amount of between about 20 and 40 wt %, and foam in an amount of between about 30 and 40 wt % of the total composite weight.
7 . The three dimensional composite panel structure of claim 2 , wherein the material of said fibers is natural.
8 . The three dimensional composite panel structure of claim 7 , wherein the material of said fibers is flax, hemp, pulp, cellulose, or chicken feathers.
9 . The three dimensional composite panel structure of claim 2 , wherein the material of said fibers is synthetic.
10 . The three dimensional composite panel structure of claim 9 , wherein the material of said fibers is glass, carbon, or poly-paraphenylene terephthalamide.
11 . A method of making a three dimensional composite panel structure having a thickness less than about 22.5 cm, overall density less than 0.2 g/cm, and exhibiting a global modulus greater than 1.2 GPa and stiffness greater than 15 kN-m 2 , the method comprising the steps of:
placing a composite panel preform in a one-sided mold; vacuum bagging the composite panel preform; applying a uniform negative pressure over the entire composite panel preform utilizing a vacuum at one side of the preform; drawing resin into the composite panel preform; permeating resin into all parts of the composite structure; curing the resin at room temperature; maintaining the composite panel under vacuum to improve consolidation; increasing the composite mechanical properties and fiber content by reducing void percentage; and demolding the composite panel.
12 . A method for making a hurricane resistant roof for a building, the method comprising forming said roof with a three dimensional composite panel sized and shaped to form said roof, said three dimensional composite panel structure having a thickness less than about 22.5 cm, overall density less than 0.2 g/cm, and exhibiting a global modulus greater than 1.2 GPa and stiffness greater than 15 kN-m 2 , the method comprising forming said three dimensional panel by:
placing a composite panel preform in a one-sided mold; vacuum bagging the composite panel preform; applying a uniform negative pressure over the entire composite panel preform utilizing a vacuum at one side of the preform; drawing resin into the composite panel perform, said resin being a natural resin, a synthetic resin, or a combination thereof; permeating resin into all parts of the composite structure; curing the resin at room temperature; maintaining the composite panel under vacuum to improve consolidation; increasing the composite mechanical properties and fiber content by reducing void percentage; and demolding the composite panel.
13 . The method of claim 12 wherein said perform comprises flax, hemp, pulp, cellulose, chicken feathers, and combinations thereof.
14 . The method of claim 13 wherein said resin is Acrylated Epoxidized Soybean Oil.Cited by (0)
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