A system for fusing thermoplastic composite structures includes a skin and a substructure on an inner surface of the skin. The system also includes a shaping surface of a tool, with the skin laid up on the shaping surface. The shaping surface is configured to maintain the shape of an outer mold line. The system further includes at least one insulation layer applied over a flange of the substructure and over exposed portions of the inner surface of the skin not in contact with the substructure, and a vacuum bag at least partly enclosing the skin and the substructure. Heat can be applied to the shaping surface to fuse the substructure to the skin such that the skin exceeds its melting point and at least a portion of a raised segment of the substructure does not exceed its melting point.

Methods and devices enabling an optimized cure cycle with an optimized control of operation parameters in an autoclave. To monitor the curing and providing a real time control, a sample having sensors for measuring a component parameter which depends from the curing state is placed in the autoclave. A first cure cycle is obtained by modelling the component and its curing, especially by GIM and simulations. Then the actual monitored curing rate and measured properties of the cured sample is compared with the model, and the cure cycle is updated when needed. Further, a similar sample may be used for calibrating the curing during a first component production or during further productions of subsequent components.

A method and a device for producing a component from a fiber composite material. The method includes introducing multiple layers of fibers impregnated with a matrix onto an inner mold, placing a membrane sealed against an outer mold onto the fibers impregnated with the matrix, such that a cavity extending along the shell surface of the outer mold forms between the outer mold and the membrane, and applying a temperature-controllable pressure fluid to the cavity at a temperature greater than the melting point of the matrix and at a pressure greater than the ambient pressure. To produce a component having at least one reinforcing layer, at least one reinforcing layer having fibers oriented in a predominantly parallel manner is placed locally onto a portion of a side of a the base layer facing the outer mold with the aid of an insertion device and a membrane with an average surface roughness of below 1.0 μm, preferably below 0.1 μm, subsequently exerts a set pressure in the cavity on the component.

This temperature monitoring device (100) can be placed in a furnace together with a composite material. The temperature monitoring device (100) includes: a pair of internal components (10) that each have a temperature detection surface (11) and are layered such that the temperature detection surfaces (11, 11) face each other; a temperature detection unit (30) disposed so as to be sandwiched between the temperature detection surfaces (11, 11); at least a pair of external components (20) that are respectively disposed on reverse sides from the temperature detection surfaces (11); and an adjustment part (50) capable of adjusting the sizes of the thickness-direction gaps between the internal components (10) and external components (20).

A system for manufacturing a composite part including a conductive flexible facesheet and an automated tape layup (ATL) machine for laying up composite tape onto the facesheet that is laid flat on a flat surface. The system also includes a curved tooling surface for transferring the facesheet with the composite material thereon to the curved tooling surface for attachment of substructures and curing into the composite part. System may also include insulation placed below the facesheet and insulation placed above the composite material, as well as a source of electricity and heat for heating the conductive facesheet to cure, melt, or fuse the composite tape and substructures without heating the tooling surface and other tooling used in the composite curing process. Heating of the facesheet may be performed using joule heat provided by a single turn transformer inducing current to conductive wires attached at opposing ends to the facesheet.

A method for manufacturing a composite part by laying up courses of composite tape using an automated tape layup (ATL) machine onto a conductive flexible facesheet laid flat on a flat surface, and then transferring the facesheet with the composite material thereon to a curved tooling surface for attachment of substructures and curing into the composite part. The method may also include applying insulation below the facesheet and above the composite material, then heating the conductive facesheet to cure the composite tape and fuse the composite tape to the substructures without heating the tooling surface or any other items used to compress and cure the composite material into the composite part. Heating of the facesheet may be performed using joule heat provided by a single turn transformer inducing current to a plurality of conductive wires attached at opposing ends to the facesheet.

Systems and methods are provided for curing a composite part. The method includes the steps of: disposing a heat blanket at a composite material; applying, with a controller, power to heaters distributed across multiple cells of a heat blanket to heat the composite material at the heat blanket; monitoring, with the controller, a temperature of the composite material at each of the multiple cells via thermocouples distributed across the multiple cells; and individually adjusting, with the controller, an amount of power applied to the heaters, for each of the multiple cells, in response to the monitored temperature and a target temperature.

A bonded structure is described. The bonded structure includes an outer structure including a close tolerance hole associated with a first accuracy level. The bonded structure includes an interior structure comprising an oversized hole associated with a second accuracy level that is different from the first accuracy level. The bonded structure includes an elastomeric grommet disposed in the oversized hole. The bonded structure includes one or more spacers between the outer structure and the interior structure providing a space between the outer structure and the interior structure. The bonded structure includes a fastener positioned in the close tolerance hole and in the oversized hole. The bonded structure includes a bonding media disposed in the space between the outer structure and the interior structure via one or more channels of the fastener. The bonding media, elastomeric grommet, and oversized hole collectively position the interior structure relative to the outer structure.

Systems and methods for curing complex fiber-reinforced composite structures utilize two distinct heat sources. A first heat source is utilized for heating a complex fiber-reinforced composite structure from within an internal portion of the complex fiber-reinforced composite structure. A second heat source is utilized for heating the complex fiber-reinforced composite structure from an external surface of the complex fiber-reinforced composite structure.

Methods of manufacturing a belt include laying up a first elastomeric layer of a belt build on a mandrel, laying up a tensile reinforcement layer on the first elastomeric layer, where the tensile reinforcement layer contains cords coated with a water based urethane compound, and laying up a second elastomeric layer on the first elastomeric layer and the tensile reinforcement layer. The belt build may be cured in a profile-forming mold, and afterward, cut to a predetermined belt width and/or length.