Abstract: Systems and methods are provided for fabricating a hybrid composite part. A method includes braiding a first set of fibers to form a weave having a closed cross-sectional shape, braiding a second set of fibers into the weave that are chemically distinct from the first set of fibers, impregnating the weave with a resin, and hardening the resin within the weave to form a hybrid composite part.

Abstract: Systems and methods are provided for fabricating a hybrid composite part. A method includes braiding a first set of fibers to form a weave having a closed cross-sectional shape, braiding a second set of fibers into the weave that are chemically distinct from the first set of fibers, impregnating the weave with a resin, and hardening the resin within the weave to form a hybrid composite part.

Abstract: Systems and methods are provided for consolidating a preform of braided fiber. One embodiment is a method that includes acquiring a braided preform comprising fibers of unidirectional material that have been woven into a shape having a closed cross-section, disposing the braided preform within a mandrel, disposing an inflatable bladder within the closed cross-section of the braided preform, and iteratively applying pressure to the braided preform via the bladder to consolidate the braided preform against the mandrel.

Abstract: Systems and methods are provided for fabricating a laminate. One method includes laying up a first set of layers comprising tows of unidirectional thermoplastic fiber-reinforced material for the laminate, and laying up a second set of layers comprising tows of braided thermoplastic fiber-reinforced material for the laminate.

Abstract: Systems and methods are provided for fabricating a laminate. One method includes laying up a first set of layers comprising tows of unidirectional thermoplastic fiber-reinforced material for the laminate, and laying up a second set of layers comprising tows of braided thermoplastic fiber-reinforced material for the laminate.

Abstract: Disclosed herein is a method of forming a composite part. The method includes heating an unconsolidated mat including a first thermoplastic, a second thermoplastic, and reinforcing fibers to a first temperature. The first thermoplastic includes a first melting temperature and the second thermoplastic includes a second melting temperature greater than the first melting temperature. The first temperature is greater than the second melting temperature. The method includes compressing the unconsolidated mat, while heated, into a composite fiber-reinforced consolidated sheet. The method includes reheating the composite fiber-reinforced consolidated sheet to a second temperature, wherein the second temperature is above the first melting temperature and below the second melting temperature and, while reheated, forming the composite fiber-reinforced consolidated sheet into a desired shape.

Abstract: Composite laminate structures are produced using partially cured parts. Partial curing of the parts is achieved by applying a catalyst to regions of the parts that are to be fully cured. These regions cure at a lower-than-normal temperature while remaining regions of the part remain uncured, allowing them to be co-bonded or co-cured to other structures.

Abstract: A system for constructing a composite structure includes a braiding machine, a winding tool and a forming machine. The composite structure is constructed of a wound tubular braiding. The wound tubular braiding is constructed of a biaxial or triaxial tubular braid of unidirectional tape.

Abstract: A system for constructing a composite structure includes a braiding machine, a winding tool and a forming machine. The composite structure is constructed of a wound tubular braiding. The wound tubular braiding is constructed of a biaxial or triaxial tubular braid of unidirectional tape.

Abstract: A system for constructing a composite structure includes a braiding machine, a winding tool and a forming machine. The composite structure is constructed of a wound tubular braiding. The wound tubular braiding is constructed of a biaxial or triaxial tubular braid of unidirectional tape.

Abstract: Composite laminate structures are produced using partially cured parts. Partial curing of the parts is achieved by applying a catalyst to regions of the parts that are to be fully cured. These regions cure at a lower-than-normal temperature while remaining regions of the part remain uncured, allowing them to be co-bonded or co-cured to other structures.

Abstract: Systems and methods are provided for designing flat composites that are formed into 3D shapes. One embodiment is a method that includes loading data defining a three dimensional (3D) shape for a composite part, identifying constraints based on dimensions of the 3D shape, simulating flattening of the 3D shape into a planar shape, and acquiring a mandrel having the planar shape. The method also includes placing features at the mandrel which permit a laminate laid-up onto the mandrel to compensate for the constraints during forming of the laminate into the 3D shape, and generating a Numerical Control (NC) program that directs an Automated Fiber Placement (AFP) machine laying up the laminate. The NC program includes instructions for laying up tows of constituent material onto the mandrel having the features, to form layers of the laminate.

Abstract: Composite laminate structures are produced using partially cured parts. Partial curing of the parts is achieved by applying a catalyst to regions of the parts that are to be fully cured. These regions cure at a lower-than-normal temperature while remaining regions of the part remain uncured, allowing them to be co-bonded or co-cured to other structures.

Abstract: Disclosed herein is a method of forming a composite part. The method includes heating an unconsolidated mat including a first thermoplastic, a second thermoplastic, and reinforcing fibers to a first temperature. The first thermoplastic includes a first melting temperature and the second thermoplastic includes a second melting temperature greater than the first melting temperature. The first temperature is greater than the second melting temperature. The method includes compressing the unconsolidated mat, while heated, into a composite fiber-reinforced consolidated sheet. The method includes reheating the composite fiber-reinforced consolidated sheet to a second temperature, wherein the second temperature is above the first melting temperature and below the second melting temperature and, while reheated, forming the composite fiber-reinforced consolidated sheet into a desired shape.

Abstract: Systems and methods are provided for designing flat composites that are formed into 3D shapes. One embodiment is a method that includes loading data defining a three dimensional (3D) shape for a composite part, identifying constraints based on dimensions of the 3D shape, simulating flattening of the 3D shape into a planar shape, and acquiring a mandrel having the planar shape. The method also includes placing features at the mandrel which permit a laminate laid-up onto the mandrel to compensate for the constraints during forming of the laminate into the 3D shape, and generating a Numerical Control (NC) program that directs an Automated Fiber Placement (AFP) machine laying up the laminate. The NC program includes instructions for laying up tows of constituent material onto the mandrel having the features, to form layers of the laminate.

Abstract: A thermoplastic composite structure is produced by consolidating and forming a composite preform to a desired shape. The preform comprises plies of a high melt temperature thermoplastic prepreg that are tacked together by a low melt temperature thermoplastic adhering the plies together in fixed registration.

Abstract: A non-crimp fabric includes a non-crimp layup of one or more non-crimp layers, each one of the non-crimp layers is formed of tows arranged parallel to each other, a nonwoven fabric that includes a nonwoven fabric layer engaged to an outer non-crimp layer of the non-crimp layup, the nonwoven fabric layer is formed of fibers, wherein a portion of the fibers extend at least partially though the non-crimp layup to hold the non-crimp layers and the nonwoven fabric layer together.