B29C31/08

SYSTEM AND METHOD FOR FABRICATING A COMPOSITE STRUCTURE

A system for fabricating a composite structure includes a ply carrier including a ply support surface configured to support at least one composite ply. The system includes a carrier transfer device configured to convey the ply carrier. The system includes a lamination system configured to selectively apply the at least one composite ply to the ply support surface of the ply carrier. The system includes a transfer system configured to remove the ply carrier from the carrier transfer device and to apply the at least one composite ply to at least a portion of a forming surface of a forming tool. The system includes a forming system configured to form the at least one composite ply over the at least a portion of the forming surface of the forming tool.

CONTINUOUS-LINE MANUFACTURING SYSTEM AND METHOD FOR COMPOSITE PARTS

A method for depositing composite material onto a tool using an automated machine. The method includes coupling a first mobile platform with a second mobile platform to form a coupled system, the first mobile platform supporting the automated machine and the second mobile platform supporting the tool. The method further includes indexing the automated machine relative to the tool. The method further includes depositing composite material from the automated machine onto the tool while the coupled system moves along a production line.

Continous-Line Fabrication for Composite Parts
20220152943 · 2022-05-19 ·

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.

Fabrication of Curved Composite Preforms for Aircraft via Assembly Lines
20220153446 · 2022-05-19 ·

Systems and methods are provided for fabricating curved preforms of fiber reinforced material. Methods include laying up at least one ply onto a carrier of flexible material at a lamination station, loading the carrier onto a rail system, routing the carrier to a particular Ply-By-Ply (PBP) forming station at the rail system, separating the at least one ply from the carrier, and making the at least one ply into the preform via the particular PBP forming station.

A GRIPPING DEVICE FOR LIFTING A PREFORM FOR A WIND TURBINE BLADE
20220143874 · 2022-05-12 ·

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 FOR LIFTING A PREFORM FOR A WIND TURBINE BLADE
20220143874 · 2022-05-12 ·

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.

Rapid manufacturing of tailored preforms

A method for rapid manufacturing of three dimensional discontinuous fiber preforms is provided. The method includes the deposition of a polymeric material containing fibers on a surface to form a tailored charge for compression molding. The reinforced polymeric material may be a thermoplastic or a reactive polymer with viscosity low enough to allow flow through an orifice during deposition, yet high enough zero shear viscosity to retain the approximate shape of the deposited charge. The material can be deposited in a predetermined pattern to induce the desired mechanical properties through alignment of the fibers. This deposition can be performed in a single layer or in multiple layers. The alignment is achieved passively by shear alignment of the fibers or actively through fiber orientation control or mixing. The fibers can be of the desired material, length, and morphology, including short and long filaments.

CONSTRUCTION OF TUBULAR ASSEMBLIES

A method and apparatus for constructing a tubular assembly 40 comprising an inner portion (24) and a further portion (23) surrounding the inner portion. The inner portion (24) comprises reinforcement (37) and the further portion (23) being formed from a strip (50) of material comprising two opposed longitudinal marginal side portions (53). The apparatus comprises an assembly station (220) comprising a wall (253). The apparatus comprises means for advancing the inner portion (21) along a first path (231) extending passed the wall (253), and means for advancing the strip (50) along a second path (232) and causing the strip to encircle the wall (253) and thereby wrap about and surround the inner portion (21). The apparatus further comprises means (321) for introducing resinous binder into the reinforcement (37) as the strip (50) is being wrapped about the inner portion (21).

CONSTRUCTION OF TUBULAR ASSEMBLIES

A method and apparatus for constructing a tubular assembly 40 comprising an inner portion (24) and a further portion (23) surrounding the inner portion. The inner portion (24) comprises reinforcement (37) and the further portion (23) being formed from a strip (50) of material comprising two opposed longitudinal marginal side portions (53). The apparatus comprises an assembly station (220) comprising a wall (253). The apparatus comprises means for advancing the inner portion (21) along a first path (231) extending passed the wall (253), and means for advancing the strip (50) along a second path (232) and causing the strip to encircle the wall (253) and thereby wrap about and surround the inner portion (21). The apparatus further comprises means (321) for introducing resinous binder into the reinforcement (37) as the strip (50) is being wrapped about the inner portion (21).

Ply transporting and compacting apparatus and method therefor

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.