A method for digitally designing a support with the shape of a fibrous blank obtained by three-dimensional weaving intended to form a fibrous preform of a turbine engine blade or propeller after shaping and compaction in a mold, includes providing a set of points representative of a face of the fibrous blank, the face being intended to form the root of the blade or the propeller and a portion of an aerodynamic profile of the blade or the propeller, generating a web connecting the points of the set of points, and digitally designing the support including at least an imprint of the fibrous blank having the shape of the generated web.

A method for use in ply compaction in forming a composite structure. The method includes positioning a ply of material on a forming tool having a web surface and at least one flange surface extending from the web surface, positioning a chassis at a first location along a length dimension of the forming tool, selectively rotating a flange forming device, that is coupled to the chassis, about a yaw axis based on a relative orientation of the flange forming device to the at least one flange surface, applying, with the flange forming device, the ply of material onto the forming tool, moving the chassis relative to the forming tool to position the chassis at a second location along the length dimension of the forming tool, and repeating the selective rotation and the application steps at the second location.

A ply transporting and compacting apparatus comprises a rigid frame, a top-layer sheet of flexible rubber material fastened to the frame, and a bottom-layer sheet of perforated flexible rubber material having openings. The apparatus also comprises a middle-layer sheet of flow media material disposed in a first plenum area that is defined between the top and bottom layer sheets. The apparatus further comprises a moving device coupled to the frame and arranged to lower the frame and sheets onto a composite ply at a trimming location to pick up the composite ply with a suction force when a vacuum is drawn in the first plenum area to create the suction force through the openings of the bottom-layer sheet.

The present disclosure provides three-dimensional (3D) printing systems, apparatuses, software, and methods for the production of at least one requested 3D object. The 3D printer includes a material conveyance system, filtering system, and unpacking station. The material conveyance system may transport pre-transformed material against gravity. The 3D printing described herein comprises facilitating non-interrupted material dispensing through a component of the 3D printer, such as a layer dispenser.

A system and a method for manufacturing laminated composite components is described. The system may include a cutting station configured to separate component layers from a ply of composition material according to a predefined pattern, a build station configured to stack the component layers according to a predetermined orientation, and a finishing station configured to compact the stacked component layers and provide the laminated composite component to an installation station.

Systems and methods are provided for forming a laminate. The method includes indexing a layup mandrel to a lamination machine disposed at a first location, transporting the lamination machine and the layup mandrel in a process direction from the first location towards a second location, laying up a laminate comprising layers of fiber-reinforced material onto the layup mandrel via the lamination machine while the lamination machine and the layup mandrel are transported in the process direction, removing the layup mandrel and the laminate at the second location, and returning the lamination machine to the first location for laying up another laminate onto another mandrel.

A continuously rotating, non-symmetric preform feed, stretch-blow-moulding machine dedicated to the stretch-blow-moulding of containers from non-symmetric injection moulded preforms; the non-symmetric preforms including an integral handle extending from a first junction point to a second junction point on a body of the preform; the body of the preform and the integral handle constituted from the same material.

A gripping device (76) is provided for lifting a preform for a wind turbine blade from a preform mould (71). The gripping device (76) comprises a base frame (62), a plurality of arms (78) slidably mounted on the base frame (62), each arm (78) having a proximal end and a distal end, a plurality of gripping members (86) for gripping a top surface (75) of the preform. The vertical position of one or more arms (78) of the gripping device (76) relative to the base frame (62) may change when lowering the gripping device (76) towards a preform to reflect the top surface (75) of the perform.

A gripping device (76) is provided for lifting a preform for a wind turbine blade from a preform mould (71). The gripping device (76) comprises a base frame (62), a plurality of arms (78) slidably mounted on the base frame (62), each arm (78) having a proximal end and a distal end, a plurality of gripping members (86) for gripping a top surface (75) of the preform. The vertical position of one or more arms (78) of the gripping device (76) relative to the base frame (62) may change when lowering the gripping device (76) towards a preform to reflect the top surface (75) of the perform.

A multilayer core molding method includes an upstream process of molding using an upstream process molding apparatus, which includes a first upstream process mold including a first upstream process mold cavity surface, and a second upstream process mold including a second upstream process mold cavity surface. The upstream process includes an inner core arrangement step and a covering step to obtain an intermediate molded body, which includes the inner core, and the unvulcanized or semi-vulcanized first outer core material covering only part of a surface of the inner core and integrated with the inner core.