Methods of fabricating a multi-region U-shaped composite structure, the methods comprising the steps of laying up a first composite material on a first tool piece to form a first sidewall, laying up the second composite material on a second tool piece tool to form a second sidewall, re-orienting the first tool piece and the second tool piece to a consolidation orientation, laying up the third composite material to form a nose wall, and overlapping at least a portion of the third composite material with at least a portion of the first composite material and at least a portion of the second composite material.

A system is disclosed for additively manufacturing a composite structure. The system may include a support, and a print head connected to and moveable by the support. The print head may have a first tool center point associated with discharge of a first material, and a second tool center point associated with discharge of a second material that is a type different than the first material.

A composite article manufacturing facility comprising: a plurality of forming stations (1), each forming station being capable of forming pieces from a feedstock of a laminar reinforcement material; a plurality of lay-up stations (3), each lay-up station being capable of arranging a stack of the formed pieces in overlapping fashion; a transfer mechanism (2) configured to simultaneously transport formed portions from multiple ones of the forming stations towards multiple ones of the lay-up stations; a memory (93) storing a first sequence of pieces to be laid up at a first one of the lay-up stations and a second sequence of pieces to be laid up at a second one of the lay-up stations; and a controller (90) coupled to the forming stations, the lay-up stations and the transfer mechanism for controlling the operations thereof, the controller having access to the memory and being configured to, when a formed piece of the first sequence and a formed piece of the second sequence are loaded on the transfer mechanism, cause the transport mechanism to simultaneously transport them towards the first and second lay-up stations respectively.

Disclosed herein is an automated fiber placement system that comprises a robot, an end effector, and a creel assembly that is coupled to the robot and movable with the robot. The creel assembly comprises a spool of a tow and a tow tensioner. The tow tensioner comprises an arm assembly that is pivotable toward and away from a tow direction between a forward position and a rearward position, inclusive, and configured to secure the tow from the spool as the tow unwinds from the spool and moves in the tow direction. The tow tensioner also comprises a biasing member that is coupled to the arm assembly and configured to bias the arm assembly into a neutral position between the forward position and the rearward position. The tow tensioner additionally comprises a potentiometer that is coupled to the arm assembly and configured to detect a position of the arm assembly.

Methods of fabricating a multi-region U-shaped composite structure, the methods comprising the steps of laying up a first composite material on a first tool piece to form a first sidewall, laying up the second composite material on a second tool piece tool to form a second sidewall, re-orienting the first tool piece and the second tool piece to a consolidation orientation, laying up the third composite material to form a nose wall, and overlapping at least a portion of the third composite material with at least a portion of the first composite material and at least a portion of the second composite material.

A method for manufacturing a fibrous tubular structure including lobes, in which fibers are draped/deposited on a mandrel having a shape corresponding to that of the fibrous structure, includes draping/deposition carried out such that at least one group of fibers has a same orientation with respect to the axis (A) of said fibrous structure, then, the fibers having been draped over an angular sector less than the total periphery of the mandrel, one of the ends of the fibrous structure is separated from the mandrel in order to allow the continuation of the draping on the same mandrel.

An apparatus for applying a liquid matrix to a fiber tow includes a belt press arranged to receive the fiber tow and compress it between two moving belts and a matrix application roller arranged to receive liquid matrix and transfer it to the fiber. The apparatus also includes a second matrix application component arranged adjacent to the matrix application roller so as to form a first gap between the component and the matrix application roller. The matrix application roller is positioned adjacent to the belt press so as to form a second gap between the matrix application roller and a belt of the belt press; and wherein the second gap is larger than the first gap.

Disclosed is an automated fiber placement (AFP) device for preform manufacturing. The AFP device includes a feeder configured to feed a sheet-type fiber composite material, a molding part configured to mold a sheet-type structure by allowing a roller member to compress the sheet-type fiber composite material, and a compressing part configured to compress an upper surface of the structure, thereby disposing the sheet-type structure on a substrate in a state of maintaining the shape of the sheet-type structure. Particular, the compressing part moves from one end to the other end of the substrate, thereby compressing the sheet-type structure.

A method for forming a fiber-reinforced thermoplastic control surface may comprise: stacking plies of thermoplastic composite sheets to a first desired thickness to form a first skin; stacking plies of thermoplastic composite sheets to a second desired thickness to form a second skin; forming the first skin in a first contour; forming the second skin in a second contour; forming a stiffening member including a thermoplastic resin, the stiffening member including a shape having a plurality of peaks and troughs; assembling the stiffening member between the first skin and the second skin; and joining the stiffening member to the first skin and the second skin.

A system is disclosed for use in additively manufacturing a structure. The system may include an additive manufacturing machine, a memory having computer-executable instructions stored thereon, and a processor. The processor may be configured to execute the computer-executable instructions to determine a plurality of tension vectors to be generated within the structure, and to generate a plan for manufacturing the structure. The plan may include tool paths that arrange continuous fibers within the structure to generate the plurality of tension vectors. The processor may also be configured to execute the computer-executable instructions to cause the additive manufacturing machine to follow the plan and manufacture the structure.