Abstract: An eyewear frame enables lenses and/or temples to be replaced by a wearer without specialized tools and without the assistance of an eyewear professional. The eyewear frame includes one or more regions having distinct materials composition and/or one or more regions having distinct fiber alignment, in conjunction with one or more lens or temple retaining features.

Abstract: 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.

Abstract: A method for designing fiber-composite parts in which part performance and manufacturing efficiency can be traded-off against one another to provide an “optimized” design for a desired use case. In some embodiments, the method involves generating an idealized fiber map, wherein the orientation of fibers throughout the prospective part align with the anticipated load conditions throughout the part, and then modifying the idealized fiber map by various fabrication constraints to generate a process-compensated preform map.

Abstract: A preform charge is formed by forming an assemblage of preforms, wherein preforms in the assemblage are bonded to a neighboring preform such that the preform charge effectively becomes a single unit. The preform charge can then be added to a mold to fabricate a part via compression molding.

Abstract: An ultrasonic manipulator for processing three-dimensional composite preforms is provided, including at least one end effector, the end effector having an ultrasonic cutting device, an ultrasonic machining device, an ultrasonic inspecting device, and an ultrasonic bonding device. A method for creating three-dimensional preforms for use in molding composite parts is also provided, and includes the steps of grasping a preform/towpreg, inspecting the composite object using ultrasound, cutting a preform from the composite object using ultrasound, and at least some of the steps of shaping the preform using ultrasound, machining the preform using ultrasound, assembling a plurality of preforms, bonding the assembled preforms together to create a preform charge, and placing the preform charge in an injection mold.

Abstract: A preformer capable of simultaneously forming plural preforms includes a forming surface and source of heat. The forming surface includes guides to keep fiber bundles, the nascent form of the preforms, spaced apart and to maintain their cross-sectional dimension. In some embodiments, the preformer further includes a source of energy, and in some embodiments, the preformer includes a source of energy and a cooling source. A method for forming preforms is also disclosed.

Abstract: A multi-material molding apparatus and method includes a single mold having, within a mold cavity, one or more movable partitions that segregate at least first and second molding materials. The first molding material is processed to form a first molded portion of the multi-material part. The second molding material is then flowed, through the movable partition, into contact with the first molded portion. That second molding material is then solidified to form a second molded portion of the multi-material part.

Abstract: A method for bending towpreg to yield a desired amount of axial force during bending to form a preform is provided including inserting towpreg into a bending die, applying an initial axial force to the towpreg, and moving the gripped end of the towpreg in an involute path using a cam, a cam follower and a gripper, the gripper disposed on the cam follower. Axial force between the gripped end and the stationary end of the towpreg from a point where the towpreg contacts a surface of the bending die is applied tangent to the surface of the bending die while bending the towpreg. An apparatus for bending towpreg to form a preform is provided including bending dies disposed in fixed positions, and a follower. Axial involute cam mechanism having a drive shaft, a cam, a cam follower that follows an involute path around the cam, a gripper and a clamp.

Abstract: A method for designing fiber-composite parts in which part performance and manufacturing efficiency can be traded-off against one another to provide an “optimized” design for a desired use case. In some embodiments, the method involves generating an idealized fiber map, wherein the orientation of fibers throughout the prospective part align with the anticipated load conditions throughout the part, and then modifying the idealized fiber map by various fabrication constraints to generate a process-compensated preform map.

Abstract: A method of reprocessing a fiber composite part to form a preform is provided including determining a location having a longest stretch of continuous, unidirectional fibers in the part, determining an axis generally closest to and parallel to the fibers at the location, suspending the part from an anchor point within a heated cavity, heating the part to a temperature above a glass transition temperature and below a melting temperature of the resin of the part, and applying at least one force vector to the composite part, the sum of such vectors being parallel to the axis, wherein fibers of the part realign in a direction generally parallel to the sum of the force vectors, and wherein the composite part yields in the direction of the at least one applied force vector to provide a preform.

Abstract: A cartridge for storing and transporting fiber-bundle-based preform charges includes a plurality of cells arranged within the housing, wherein each cell is physically adapted to receive a preform charge and prevent it from moving therein as the cartridge is transported. In some embodiments, the cartridge and preform charges it conveys are serialized.

Abstract: Methods for fabricating fiber-composite truss structures comprise a) individually molding multiple unit cells of a given size, and subsequently fusing them together in a repeating pattern, b) cross members are consolidated with longerons while maintaining continuity of fiber in the longerons, and c) compression-molded truss components are unioned to continuous fiber beams by means of mechanically interlocking joints.

Abstract: A method useful for forming a composite part having regions in which fibers align with the principle stress vectors as well as regions having a randomized fiber alignment. To form the randomized fiber alignment, a preform cavity is formed in a preform arrangement, and the preform arrangement is molded in accordance with compression molding protocols to form a part.

Abstract: A method for rapid heat cycle compression molding comprises placing an assemblage of feed constituents in a mold, placing the mold between two hot platens of a hot press, heating the mold by pressing the two hot platens against the mold, placing the mold between two cold platens of a cold press, cooling the mold by pressing the two cold platens against the mold, and ejecting the part from the mold.

Abstract: A hybrid preform comprises a bundle of unidirectionally aligned fibers, and at least one partial cut that extends part of the way, but not all of the way, through a transverse cross section of the bundle of fibers at least one location along the length of the bundle.

Abstract: A fiber-composite part having one or more electronic components that are located in arbitrary regions of the internal volume of the part are fabricated using a preform charge. The preform charge has a structure that corresponds to that of the mold cavity in which the part is being formed. By incorporating the electronic components in the preform charge, such components are then precisely located, spatially oriented, and constrained, and such location and orientation is maintained during molding to produce a part with the electronic components in the desired locations and orientations within its internal volume.

Abstract: An apparatus for molding a part includes a plunger cavity, a plunger, and a mold cavity, wherein the plunger is oriented out-of-plane with respect to a major surface of the mold cavity, and first and second vents couples to respective first and second portions of the mold cavity. In a method, resin and fiber are forced into the mold cavity from a plunger cavity, and at least some of the fibers and resin are preferentially flowed to certain region in the mold cavity via the use of vents.

Abstract: A preform-charge fixture creates a preform charge, which is a partially consolidated assemblage of preforms that can be efficiently transferred to a mold to create a finished part in a molding process, such as compression molding. In the illustrative embodiment, the preform-charge fixture includes peripheral cleats that are movable towards a central cleat to create a small gap therebetween that receives and constrains preforms in a desired position. The fixture also includes clamps, which are operable to engage an uppermost layer of preforms in the gap and apply a slight amount of downward pressure thereto to assure that the preforms are properly seated. The fixture also accommodates an energy source that heats the preforms so that, in conjunction with downforce applied by the clamps and/or gravity, the preforms can be tacked together, forming the preform charge.

Abstract: Some embodiments of a compression mold for forming a rib-and-sheet part includes a mold cavity and a mold insert. A sheet is placed in the mold cavity, and the mold insert is placed on the sheet. A preform assemblage is placed in a gap that is formed between the mold insert and the wall of the mold cavity. A mold core is biased above the preform assemblage, prior to molding operations, via a compression spring.

Abstract: Rib-and-sheet structures include a rib comprising continuous, aligned fibers. The rib is fabricated via compression molding from continuous, aligned fiber, thereby providing an aligned, continuously reinforced rib. In one embodiment, rib-and-sheet structures are produced in a two-step compression-molding process, wherein a near net-shape rib is molded, in a first mold, from fiber-bundle based preforms, and then a rib-and-sheet part is molded by placing, in a second mold, the rib with either: (i) a preformed sheet, (ii) plies that form a laminate/sheet or (iii) chopped fibers that form a sheet during the molding process. In another embodiment, rib-and-sheet structures are fabricated in a one-step compression-molding process, wherein fiber-bundle-based preforms and (i) a preformed sheet, (ii) plies that form a laminate/sheet, or (iii) chopped fibers are combined in a single mold and molded in a single step.