Weatherability and durability of low-density polyethylene nanocomposites with clay, silica and zinc oxide
US-9221953-B1 · Dec 29, 2015 · US
US9808969B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9808969-B2 |
| Application number | US-201113817300-A |
| Country | US |
| Kind code | B2 |
| Filing date | Aug 12, 2011 |
| Priority date | Aug 16, 2010 |
| Publication date | Nov 7, 2017 |
| Grant date | Nov 7, 2017 |
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The present invention relates to sheet-form fiber composite components which are obtainable by impregnating fibers with a reactive resin mixture comprising polyisocyanates, polyepoxides, polyols and optionally additives, and to a process for the production thereof.
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The invention claimed is: 1. A sheet-form fibre composite component prepared by the vacuum-assisted resin transfer moulding process, for use in the production of rotor blades of wind turbines, comprising a fibre layer impregnated with polyurethane, wherein the polyurethane is obtainable from a reaction mixture comprising A) one or more polyisocyanates; B) one or more polyether polyols comprising an addition product of propylene oxide on a di-functional or poly-functional starter molecule, the polyether polyol(s) comprising at least 80% secondary OH groups; C) one or more polyepoxides; and D) optionally additives, wherein the reaction mixture has a viscosity at 35° C. of from 50 to 250 mPa and a ratio of the number of NCO groups to the number of OH groups of component B) of from 1.3:1 to 10:1 and a ratio of the number of NCO groups to the number of epoxide groups of component C) of from 1.1:1 to 10:1, and wherein the one or more polyisocyanates consists of mixtures of diphenylmethane diisocyanate and polyphenylenepolymethylene polyisocyanate with a monomer content of from 70 to 95 wt. % in the polyisocyanate component of A) based on the total weight of the polyisocyanate components. 2. The sheet-form fibre composite component of claim 1 , wherein one or more gelcoat layers are present on one side of the polyurethane-containing fibre layer. 3. The sheet-form fibre composite component of claim 2 , wherein a spacer layer is present on the side of the polyurethane-containing fibre layer that is remote from the gelcoat layer, which spacer layer is followed by a further polyurethane-containing fibre layer. 4. The sheet-form fibre composite component of claim 1 , wherein a spacer layer is present on one side of the polyurethane-containing fibre layer, which spacer layer is followed by a further polyurethane-containing fibre layer. 5. A process for producing the sheet-form fibre composite component of claim 1 by the vacuum-assisted resin transfer moulding process, comprising a) preparing a mixture of A) one or more polyisocyanate; B) one or more polyether polyols comprising an addition product of propylene oxide on a di-functional or poly-functional starter molecule, the polyether polyol(s) comprising at least 80% secondary OH groups; C) one or more polyepoxides; and D) optionally additives, wherein the mixture has a viscosity at 35° C. of from 50 to 250 mPa and a ratio of the number of NCO groups to the number of OH groups of component B) of from 1.3:1 to 10:1 and a ratio of the number of NCO groups to the number of epoxide groups of component C) of from 1.1:1 to 10:1, and wherein the one or more polyisocyanates consists of mixtures of diphenylmethane diisocyanate and polyphenylenepolymethylene polyisocyanate with a monomer content of from 70 to 95 wt. % in the polyisocyanate component of A) based on the total weight of the polyisocyanate components; b) laying a fibre material in a mould half; c) introducing the mixture prepared in step a) into the fibre material of step b) to produce an impregnated fibre material; and d) curing the impregnated fibre material at a temperature of from 20 to 120° C. 6. The process of claim 5 , wherein step d) is performed at a temperature of from 70 to 90° C. 7. The process of claim 5 , wherein before step b), b′) one or more gelcoat layers are introduced into the mould half. 8. The process of claim 5 , wherein after step b) and before step c) a spacer material layer and then a fibre material layer are introduced into the mould half. 9. A rotor blade for wind turbines, a bodywork component for motor vehicles, an aircraft, a building, a road, or a structure which is subjected to high stress comprising the sheet-form fibre composite component of claim 1 .
Polyethers containing at least three hydroxy groups (C08G18/4833 - C08G18/5096 take precedence) · CPC title
Epoxy resins {(C08G18/42, C08G18/48 take precedence; reaction products of epoxy resins with at least equivalent amounts of compounds containing active hydrogen C08G18/6407, with at least equivalent amounts of amines C08G18/6415; polymeric products of isocyanates or isothiocyanates with epoxy compounds having no active hydrogen C08G18/003)} · CPC title
characterised by the choice of material · CPC title
Mixtures of compounds of group C08G18/58 with other macromolecular compounds · CPC title
Impregnating materials with prepolymers which can be polymerised in situ, e.g. manufacture of prepregs · CPC title
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