Patent classifications
B29C70/882
Conductive Pre-Impregnated Composite Sheet and Method for Making the Same
A method for making a conductive pre-impregnated composite sheet includes the steps of joining a nanomaterial composite sheet, a fiber-reinforcing sheet and a resin system to form a combined sheet, heating the combined sheet, compacting the combined sheet, and cooling the combined sheet to form conductive pre-impregnated composite sheet including the fiber-reinforcing sheet, and the nanomaterial composite sheet coupled to the fiber-reinforcing sheet, wherein the fiber-reinforcing sheet and the nanomaterial composite sheet are embedded in the resin system.
GENERATING A THREE-DIMENSIONAL OBJECT
In an example, an apparatus for generating a three-dimensional object includes a build area platform, a build material distributor, a secondary material ejection device, a coalescing agent ejection device, and a controller. The controller may control the secondary material ejection device to eject a secondary material in a predefined pattern over the build area platform, control the build material distributor to distribute a layer of the build material around the ejected secondary material, control the coalescing agent ejection device to eject the coalescing agent onto the layer of the build material, and control an energy source to apply energy onto the ejected coalescing agent to cause the build material in contact with the ejected coalescing agent to coalesce and solidify.
LOW-COST CARBON FIBER-BASED LIGHTNING STRIKE PROTECTION
A method of manufacturing a wind turbine blade with integrated lightning strike protection is provided. The method includes forming a plurality of fiber reinforced plies having carbonized textile-grade PAN fibers. The fiber reinforced plies are then stacked on a surface of a mold, wetted with a resin, and cured to form at least part of a wind turbine blade. Because the textile-grade PAN fibers are electrically conductive, the resultant structure provides both electrical conductivity and structural integrity. Laboratory testing of carbon fiber structures against simulated lightning strikes demonstrated high resilience due to their high electrical conductivity both in-plane and in through-thickness directions, with no significant damages, e.g., fiber breakage, resin evaporation, or delamination. High-temperature epoxy helped to improve the performance of the CFRP against the lightning strikes.
Method of manufacturing a functionally graded article
Disclosed herein are methods for manufacturing a functionally graded polymer material. The methods comprise preparing a melted polymer mixture comprising a thermoplastic polymer and a magnetic filler dispersed in the thermoplastic polymer, molding the melted polymer mixture and applying a magnetic field to a portion of the melted polymer mixture to form a functionally graded polymer material. The resulting functionally graded polymer material has a magnetic filler gradient formed through a thickness of the material.
CONTROLLER AND MANUFACTURING METHOD THEREOF
A controller (1) includes a primary molded portion (11) in which a resin molded body (10) is integrated with a bus bar (100) using a resin, causing one end of the bus bar (100) to function as a connector terminal which protrudes into connector portions (13) to (15), and configured to form electronic component disposition portions (16a) to (16d) in which an electronic component (40) is disposed and a power device disposition portion (17) in which a power device (50) is disposed, and a secondary molded portion (21) integrated with the electronic component (40), the power device (50), and the primary molded portion (11) in a state in which the electronic component (40) is disposed at the electronic component disposition portions (16a) to (16d) and the power device (50) is disposed at the power device disposition portion (17).
Lining Panel With Integrated Electric Lines For An Aircraft And Method For Manufacturing A Lining Panel
A method for manufacturing a lining panel with integrated electric lines for a lining of a passenger cabin of an aircraft or spacecraft includes using an additive manufacturing (AM) or 3D printing technique to form the electric lines on or into a panel body of the lining panel. A lining panel with integrated electric lines for a lining of a passenger cabin of an aircraft or spacecraft includes a panel body and electric lines being formed on or into the panel body using an AM or 3D printing technique.
FIBER-COMPOSITE PARTS WITH INSERTS AND METHOD FOR INTEGRATION THEREOF
A molding method for fabricating a composite part having inserts is provided including disposing preforms in a mold, each having co-aligned, resin-impregnated fibers, placing the inserts in the mold adjacent to at least one of the preforms, wherein each insert has securement features for receiving a portion of the co-aligned resin-impregnated fibers from at least one preform, and applying heat and pressure in an amount sufficient to consolidate the resin-impregnated fibers into a resin matrix, thereby forming the part, including consolidating the fibers and resin within the securement features. A fiber composite part is also provided including continuous, co-aligned fibers within a resin matrix, and at least one insert disposed in the matrix, the insert comprising at least one securement feature having a second plurality of the fibers therein, the second plurality of fibers extending into the resin matrix and overlapping with some of the first plurality of fibers.
Increasing electrical conductivity at selected locations of a 3D object
A device includes a coater, a dispenser, and a treatment portion. The coater is to coat, layer-by-layer, a build material relative to a build pad to form a 3D object. The dispenser is to at least dispense a fluid including a first at least potentially electrically conductive material. In at least some selected locations of an external surface of the 3D object. The treatment portion is to treat the 3D object to substantially increase electrically conductivity on the external surface of the 3D object at the at least some selected locations.
Manufacturing a wind turbine blade shell part
The present invention relates to a method for manufacturing a wind turbine blade part. The method comprises providing one or more wind turbine blade components including a wind turbine blade component comprising a fibre material element, an electrically conductive element, a magnetic field generator for generating an Eddy current in the electrically conductive element; arranging the electrically conductive element, the magnetic field generator, and the fibre material element such that at least a part of the fibre material element is positioned between the electrically conductive element and the magnetic field generator; generating an Eddy current in the electrically conductive element using the magnetic field generator; generating, using a magnetic sensor, a signal representing a magnetic field induced by the generated Eddy current, and forming the wind turbine blade part by assembling the wind turbine blade components.
MULTI-MATERIAL FIBERS AND METHODS OF MANUFACTURING THE SAME
Methods of manufacturing multi-material fibers having one or more electrically-connectable devices disposed therein are described. In certain instances, the methods include the steps of: positioning the electrically-connectable device(s) within a corresponding pocket provided in a preform material; positioning a first electrical conductor longitudinally within a first conduit provided in the preform material; and drawing the multi-material fiber by causing the preform material to flow, such that the first electrical conductor extends within the multi-material fiber along a longitudinal axis thereof and makes an electrical contact with a first electrode located on each electrically-connectable device. A metallurgical bond may be formed between the first electrical conductor and the first electrode while drawing the multi-material fiber and/or, after drawing the multi-material fiber, the first electrical conductor may be located substantially along a neutral axis of the multi-material fiber.