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WO/2009/112017 |
The object of the invention, which relates to a method for producing a rotor blade (1) for a wind turbine and to a rotor blade produced according to said method and comprising a rotor blade base for connecting to a hub of the wind turbin...
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WO/2009/112604 |
Head for the automatic positioning of fibre blankets, which determines a path for the fibre blanket (2) to be positioned, as far as a positioning zone (5), passing via a resin-impregnation zone (4) and via a cutting zone (3), including, ...
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WO/2009/112073 |
The present invention relates to a conical fibre reinforced section (10; 20). The conical section (10; 20) hasa substantially circular cross section and a hollow core. The conical section (10; 20) comprises a firstlayer (11;21) with fibr...
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WO/2009/112162 |
The invention relates to a method and device for producing a fiber composite part having a support structure made of fibers under tension and for the use thereof as masts, hulls, aircraft wings, 3D surfaces, prosthetics, T-beams, contain...
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WO/2009/112528 |
The object underlying the invention, which relates to a method for producing a roll for processing strip-shaped material using a core (5) that corresponds to the shape of the roll, a casing (11) forming the outer casing surface (12) of t...
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WO/2009/112694 |
The invention relates to a curved structural part (110) formed of a composite material having a fibrous reinforcement with continuous fibres and of which the cross section comprises at least two wings (10, 12), said fibres (3) extending ...
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WO/2009/112162 |
The invention relates to a method and device for producing a fiber composite part having a support structure made of fibers under tension and for the use thereof as masts, hulls, aircraft wings, 3D surfaces, prosthetics, T-beams, contain...
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WO/2009/112694 |
The invention relates to a curved structural part (110) formed of a composite material having a fibrous reinforcement with continuous fibres and of which the cross section comprises at least two wings (10, 12), said fibres (3) extending ...
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WO/2009/112017 |
The object of the invention, which relates to a method for producing a rotor blade (1) for a wind turbine and to a rotor blade produced according to said method and comprising a rotor blade base for connecting to a hub of the wind turbin...
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WO/2009/111466 |
A high quality finished prototype fuselage structure of an aircraft is manufactured using a cured female tool and an automated composite layup machine, and then touched up by hand to meet a tolerance or other specification. The female to...
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WO/2009/109193 |
This invention relates to a method for manufacturing a composite member, where a number of different material layers including at least one layer of gelcoat are applied in a mould, and where resin is applied for joining of the layers. Th...
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WO/2009/109564 |
The invention relates to a structural panel comprising a core of fibre material and outer layers on opposite sides of the core, wherein the core of fibre material is received in preshaped grooves provided in one outer layer's surface, th...
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WO/2009/109564 |
The invention relates to a structural panel comprising a core of fibre material and outer layers on opposite sides of the core, wherein the core of fibre material is received in preshaped grooves provided in one outer layer's surface, th...
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WO/2009/109193 |
This invention relates to a method for manufacturing a composite member, where a number of different material layers including at least one layer of gelcoat are applied in a mould, and where resin is applied for joining of the layers. Th...
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WO/2009/109441 |
The invention relates to a method for tolerance compensation between two fiber composite components (1, 3) for airplanes. In order to easily compensate tolerances between two fiber composite components to be joined, the method according ...
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WO/2009/106341 |
Disclosed is a pultrusion method for producing a profiled preform or fiber composite-plastic component having cross-sectional portions that extend at an angle from each other from a plurality of semifinished products (1, 2, 3) in a quasi...
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WO/2009/108517 |
A method of forming a composite layup on a substrate comprises: moving an automatic fiber placement head over the substrate; using the fiber placement head to lay down multiple, parallel strips of composite tape (36) on the substrate (10...
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WO/2009/106868 |
A polyetheretherketone film is used in the consolidation of a prepreg so that the film becomes incorporated into the consolidated prepreg, defines an outer layer of the consolidated prepreg and therefore provides the consolidated prepreg...
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WO/2009/106340 |
Disclosed is a method for producing a profiled semifinished fiber composite (FC) product from a semifinished product (2) that is made of dry fiber or prepreg material and is moved through a shaping device (1) in the longitudinal directio...
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WO/2009/108885 |
A method for making a propeller product is disclosed. The propeller is formed using polyurethane cores adhered to a laminate hub to form a core assembly. An encapsulating structural laminate skin is then formed on the core assembly using...
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WO/2009/108885 |
A method for making a propeller product is disclosed. The propeller is formed using polyurethane cores adhered to a laminate hub to form a core assembly. An encapsulating structural laminate skin is then formed on the core assembly using...
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WO/2009/106340 |
Disclosed is a method for producing a profiled semifinished fiber composite (FC) product from a semifinished product (2) that is made of dry fiber or prepreg material and is moved through a shaping device (1) in the longitudinal directio...
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WO/2009/106341 |
Disclosed is a pultrusion method for producing a profiled preform or fiber composite-plastic component having cross-sectional portions that extend at an angle from each other from a plurality of semifinished products (1, 2, 3) in a quasi...
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WO/2009/104040 |
A tape for use in automated tape laying machines that includes a multi-layer substrate composed of a plastic layer that includes at least one plastic film having an outer film surface and an inner film surface. The plastic film is adhere...
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WO/2009/103768 |
The present invention provides a method for producing a fiber-reinforced plastic profile part (103). The method comprises feeding a tubular fiber netting (104) in which a matrix plastic is distributed. A longitudinal section of the fiber...
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WO/2009/103736 |
A method for producing a composite structure comprising fibre reinforced material by means of vacuum assisted resin transfer moulding is described. The fibre material is impregnated with liquid resin, and the method comprising the steps ...
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WO/2009/103768 |
The present invention provides a method for producing a fiber-reinforced plastic profile part (103). The method comprises feeding a tubular fiber netting (104) in which a matrix plastic is distributed. A longitudinal section of the fiber...
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WO/2009/103736 |
A method for producing a composite structure comprising fibre reinforced material by means of vacuum assisted resin transfer moulding is described. The fibre material is impregnated with liquid resin, and the method comprising the steps ...
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WO/2009/104040 |
A tape for use in automated tape laying machines that includes a multi-layer substrate composed of a plastic layer that includes at least one plastic film having an outer film surface and an inner film surface. The plastic film is adhere...
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WO/2009/102531 |
A method of applying a length of discontinuous fiber material to a surface comprises placing the material between a roller and the surface, urging the roller toward the surface such that the roller causes at least a portion of the length...
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WO/2009/102531 |
A method of applying a length of discontinuous fiber material to a surface comprises placing the material between a roller and the surface, urging the roller toward the surface such that the roller causes at least a portion of the length...
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WO/2009/098006 |
The invention relates to a method for producing a composite part comprising a first layer, at least one resin-impregnated fibre layer that adjoins the first layer and at least one other layer that adjoins the fibre layer and is based on ...
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WO/2009/097853 |
This invention relates to a method for manufacturing a composite part comprising the steps of laying out a number of material layers (101), covering the layers with an outermost vacuum foil (104) along with applying one or more internal ...
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WO/2009/098423 |
The invention relates to a method for making a cellular structure, including a cellular panel (10) and a complementary element (48), said cellular panel including a honeycomb core (12) sandwiched in between two cover plates (16,18). The ...
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WO/2009/098088 |
The invention relates to a method for producing a fibre composite component (1) with a skinning field (2) and a primary component (8) for reinforcing the fibre composite component (1), comprising the steps: application of a pre-preg (4) ...
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WO/2009/098423 |
The invention relates to a method for making a cellular structure, including a cellular panel (10) and a complementary element (48), said cellular panel including a honeycomb core (12) sandwiched in between two cover plates (16,18). The ...
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WO/2009/098088 |
The invention relates to a method for producing a fibre composite component (1) with a skinning field (2) and a primary component (8) for reinforcing the fibre composite component (1), comprising the steps: application of a pre-preg (4) ...
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WO/2009/095335 |
Disclosed is a fiber composite part (1) for an aircraft or spacecraft, comprising electrically conductive fibers (6) in at least some sections. The fibers (6) are coupled to an electric power source to apply electricity in order to heat ...
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WO/2009/095619 |
The subject of the invention is a device for the manufacture of part of an aircraft made of a composite, one surface of which is liable to be in contact with aerodynamic flows, said device comprising, on the one hand, a male mould and, o...
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WO/2009/095335 |
Disclosed is a fiber composite part (1) for an aircraft or spacecraft, comprising electrically conductive fibers (6) in at least some sections. The fibers (6) are coupled to an electric power source to apply electricity in order to heat ...
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WO/2009/095335 |
Disclosed is a fiber composite part (1) for an aircraft or spacecraft, comprising electrically conductive fibers (6) in at least some sections. The fibers (6) are coupled to an electric power source to apply electricity in order to heat ...
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WO/2009/095619 |
The subject of the invention is a device for the manufacture of part of an aircraft made of a composite, one surface of which is liable to be in contact with aerodynamic flows, said device comprising, on the one hand, a male mould and, o...
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WO/2009/095314 |
To produce a hole in a part (1) made of a thermoplastic composite, the part is locally heated to a plastic forming temperature Tf and the fibres (10) of the composite are progressively moved apart at the same time as the matrix (11) in t...
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WO/2009/097514 |
Stiffener tool positioning apparatus (1000) and method are provided. In one embodiment, the apparatus includes a base (1002), a first flipper member (1016) and second flipper member (1018). The first flipper member is slide -ably attache...
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WO/2009/092989 |
A prepreg for manufacturing a fibre-reinforced composite material, the prepreg comprising a layer of dry fibres and a layer of resin material adhered to a surface of the layer of dry fibres, the resin material having a plurality of parti...
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WO/2009/092543 |
A multilayer, flexible planar material for delimiting a matrix supply chamber during the production of fiber-reinforced plastic components made of fiber composite semifinished products comprises a multifunction laminate (40), which compr...
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WO/2009/094113 |
Methods and apparatus are provided for making a rotor blade spar (14) from composite material wherein a multi-component mandrel (10) is used to form the composite spar (14). The mandrel (10) is made using a number of components (38,44, 5...
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WO/2009/094113 |
Methods and apparatus are provided for making a rotor blade spar (14) from composite material wherein a multi-component mandrel (10) is used to form the composite spar (14). The mandrel (10) is made using a number of components (38,44, 5...
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WO/2009/089814 |
A method for depositing a rolled material (3) while maintaining a predetermined end border position, comprising the following steps: providing a material roll on a handling device (2), rotating the material roll (3) in a roll-off directi...
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WO/2009/090218 |
The invention relates to a device and a method for moulding a part made of a high-performance thermoplastic composite material, that comprises injecting a high-performance thermoplastic resin into a fibrous preform placed in a mould (1, ...
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