Abstract: An infrared camera is directed aft of a compaction roller of a composite laying head. Heat is applied to a substrate by a heater mounted forward of the compaction roller. Infrared images are captured of composite tows laid down on a substrate by the compaction roller. Whether the composite tows have sufficient contact is determined using the infrared images.

Abstract: An illustrative example of the present disclosure provides a method. A first set of composite plies including a first outer ply of a first composite structure is laid up. A first intermediate surface of the first outer ply is measured to form a first set of measurements. A laydown surface for a tool path of a composite placement machine is modified to form a modified tool path, wherein modifying the laydown surface comprises modifying the laydown surface such that a laydown surface of the modified tool path matches the first set of measurements. A composite ply is laid down using the composite placement machine and the modified tool path.

Abstract: Systems and methods are provided for dynamically managing heater position for an Automated Fiber Placement (AFP) machine. One embodiment is a method that includes retrieving distance data indicating predicted distances of a heating surface of a heater of the AFP machine to a surface of a laminate being laid-up by the AFP machine, for each of multiple locations along a path. The method also includes directing the AFP machine to lay up the laminate in accordance with a Numerical Control (NC) program, identifying a current location of the heater in the path, determining a speed at which the heater of the AFP machine is moving, correlating the current location of the heater with a predicted distance, and adjusting an amount of power for the heater at the current location based on the predicted distance that was correlated with the current location, and the speed at the current location.

Abstract: An end effector transports, places and forms a composite ply on a tool having complex tool surfaces. The end effector includes a combination of vacuum and Bernoulli grippers for holding the composite ply while it is being transported and formed, and a set of mechanical actuators that form the composite ply down over the tool surfaces. The Bernoulli grippers allow the composite ply to slip while being held and formed.

Abstract: Systems and methods are provided for dynamically managing heater position for an Automated Fiber Placement (AFP) machine. One embodiment is a method that includes retrieving distance data indicating predicted distances of a heating surface of a heater of the AFP machine to a surface of a laminate being laid-up by the AFP machine, for each of multiple locations along a path. The method also includes directing the AFP machine to lay up the laminate in accordance with a Numerical Control (NC) program, identifying a current location of the heater in the path, determining a speed at which the heater of the AFP machine is moving, correlating the current location of the heater with a predicted distance, and adjusting an amount of power for the heater at the current location based on the predicted distance that was correlated with the current location, and the speed at the current location.

Abstract: Closed-loop systems and methods for controlling the temperature at the compaction point as an automated fiber placement (AFP) machine is placing material over complex surface features at varying speeds. The closed-loop system starts with multiple infrared temperature sensors directed at the layup surface in front of the compaction roller and also at the new layup surface behind the compaction roller. These sensors supply direct temperature readings to a control computer, which also receives speed data and a listing of active tows from the AFP machine and is also programmed with the number of plies in the current layup. In accordance with one embodiment, the heater control system uses a proportional-integral-derivative loop to control the temperature at the compaction point (e.g., at the interface of the compaction roller and a newly laid tow) and regulate the heater power to achieve the desired temperature.

Abstract: A heating apparatus for heating a reinforcing layer of a composite material structure is disclosed. The heating apparatus includes a housing having a base and a housing body defining a housing interior space. A radiant heating assembly is disposed within the housing and configured to transfer radiant heat to the reinforcing layer. Additionally, a convection heating assembly is formed within the housing including at least one convection assembly gas passage. The heating apparatus further includes a convection assembly gas outlet coupled to the convection assembly gas passage and a convection assembly gas flows from the convection assembly gas outlet. The convection assembly gas flows along to heat the convection assembly gas. The heating apparatus further includes a redirection gas passage coupled to a redirection nozzle formed at a convection heat application point. A redirection gas flows from the redirection nozzle to direct the convection assembly gas towards the reinforcing layer.

Abstract: A fiber placement system including a fiber placement station at a first location, the fiber placement station including a tool and a fiber placement assembly configured to construct a reinforcement layup on the tool, the first fiber placement assembly including a compaction roller rotatable about an axis of rotation, the compaction roller at least partially defining a nip, a thermoplastic composite ply extending through the nip and a heating unit positioned to heat the thermoplastic composite ply proximate the nip, and a consolidation station at a consolidation location, the consolidation location being different from the first location, the consolidation station including a consolidation tool and a consolidation system configured to consolidate a reinforcement layup assembly that includes the reinforcement layup.

Abstract: A fiber placement system including a fiber placement station at a first location, the fiber placement station including a tool and a fiber placement assembly configured to construct a reinforcement layup on the tool, the first fiber placement assembly including a compaction roller rotatable about an axis of rotation, the compaction roller at least partially defining a nip, a thermoplastic composite ply extending through the nip and a heating unit positioned to heat the thermoplastic composite ply proximate the nip, and a consolidation station at a consolidation location, the consolidation location being different from the first location, the consolidation station including a consolidation tool and a consolidation system configured to consolidate a reinforcement layup assembly that includes the reinforcement layup.

Abstract: A composite structure is fabricated by laying up at least one ply of fiber reinforcement and at least one layer of resin on a tool. The resin film layer is formed by laying strips of resin film. The fiber reinforcement is infused with resin from the resin layer.

Abstract: Systems and methods are provided for dynamically managing heater position for an Automated Fiber Placement (AFP) machine. One embodiment is a method that includes retrieving distance data indicating predicted distances of a heating surface of a heater of the AFP machine to a surface of a laminate being laid-up by the AFP machine, for each of multiple locations along a path. The method also includes directing the AFP machine to lay up the laminate in accordance with a Numerical Control (NC) program, identifying a current location of the heater in the path, determining a speed at which the heater of the AFP machine is moving, correlating the current location of the heater with a predicted distance, and adjusting an amount of power for the heater at the current location based on the predicted distance that was correlated with the current location, and the speed at the current location.

Abstract: A composite structure is fabricated by laying up at least one ply of fiber reinforcement and at least one layer of resin on a tool. The resin film layer is formed by laying strips of resin film. The fiber reinforcement is infused with resin from the resin layer.

Abstract: A pressure bulkhead for a pressurized vehicle such as an aircraft employs a plurality of layers of composite fiber material having uni-directional fibers arranged in a single direction within the composite fiber material. The pressure bulkhead incorporates non-traditional radial and circumferential stiffening members into a composite laminate and aligns the radial stiffening members with the direction of dominant load paths. The radial and circumferential stiffening members are interlaid between full layers of the composite fiber material. Related methods of manufacturing the pressure bulkhead include using automated fiber placement equipment to form each layer of the pressure bulkhead and discretely orient the integral stiffeners and the uni-directional fibers in each layer.

Abstract: A fiber placement system including a fiber placement station at a first location, the fiber placement station including a tool and a fiber placement assembly configured to construct a reinforcement layup on the tool, the first fiber placement assembly including a compaction roller rotatable about an axis of rotation, the compaction roller at least partially defining a nip, a thermoplastic composite ply extending through the nip and a heating unit positioned to heat the thermoplastic composite ply proximate the nip, and a consolidation station at a consolidation location, the consolidation location being different from the first location, the consolidation station including a consolidation tool and a consolidation system configured to consolidate a reinforcement layup assembly that includes the reinforcement layup.

Abstract: A composite automation method and apparatus for the generation of short path course application of a composite lamina is realized by reconfiguring the functional mechanisms of the fiber placement head. Separating the fiber advance and retract functions, nesting the activation cylinders, and making use of push only activation results in a simplified, compact AFP delivery head. Uniform cutting is provided by a circular configuration fiber cutting blade, were at activation the blade both provides a progressive cutting force and rotates to providing a new cutting edge, and requires limited cutting edge guidance as all orientations cut equally well. The mechanism nested in functions and placed in close proximity to the compaction roller reduces the overall fiber course to the application point.

Abstract: To apply a course on a layup mold, a ply boundary that defines a ply area on the layup mold is determined and a tape of composite material is applied on the ply area at an oblique angle relative to the ply boundary. In addition, a leading edge of the tape is butt cut and the leading edge, and the ply boundary essentially converge. Furthermore, a trailing edge is generated. The trailing edge is a butt cut and the trailing edge and the ply boundary essentially converge.

Abstract: An anomaly detection and cataloging system is described that includes a handheld probe having a probe tip, a user interface, and a communications interface. The system further includes a system controller and a probe locating device. The probe is operable, via the user interface, for transmitting, via the communications interface, a user selected anomaly type to the system controller, the anomaly type being associated with a manufactured part or airplane on the ground (AOG). The probe locating device is operable to provide to the system controller a location associated with the probe tip, and the system is programmed to associate the user selected anomaly type with the location associated with the probe tip.

Abstract: A composite structure is fabricated by laying up at least one ply of fiber reinforcement and at least one layer of resin on a tool. The resin film layer is formed by laying strips of resin film. The fiber reinforcement is infused with resin from the resin layer.

Abstract: A composite laminate has a pattern of holes therein. The holes are formed by laying down plies of unidirectional pre-preg material having varying fiber orientations. The tows are spaced apart and located to form holes through the laminate.

Abstract: A composite automation method and apparatus for the generation of short path course application of a composite lamina is realized by reconfiguring the functional mechanisms of the fiber placement head. Separating the fiber advance and retract functions, nesting the activation cylinders, and making use of push only activation results in a simplified, compact AFP delivery head. Uniform cutting is provided by a circular configuration fiber cutting blade, were at activation the blade both provides a progressive cutting force and rotates to providing a new cutting edge, and requires limited cutting edge guidance as all orientations cut equally well. The mechanism nested in functions and placed in close proximity to the compaction roller reduces the overall fiber course to the application point.