A method for closing an injection mold for manufacturing a revolution part made of composite material, the mold including a mandrel supporting a fiber preform and angular sectors comprising an annular base to come into contact with the fiber texture, the annular base extending between first and second side edges along a circumferential direction. The method includes successive positioning and fixing the angular sectors on the mandrel, the annular base of each sector compacting the fiber preform portion present oppositely, the side edges of the annular base of each angular sector being in contact with the side edges of the annular base of the adjacent sectors. Before the positioning and fixing of the angular sectors on the mandrel, strip s are placed on the exposed surface of the fiber preform, each strip covering an area of the fiber preform located facing a junction area between two adjacent angular sectors.

A method for closing an injection mold for manufacturing a revolution part made of composite material, the mold including a mandrel supporting a fiber preform and angular sectors comprising an annular base to come into contact with the fiber texture, the annular base extending between first and second side edges along a circumferential direction. The method includes successive positioning and fixing the angular sectors on the mandrel, the annular base of each sector compacting the fiber preform portion present oppositely, the side edges of the annular base of each angular sector being in contact with the side edges of the annular base of the adjacent sectors. Before the positioning and fixing of the angular sectors on the mandrel, strip s are placed on the exposed surface of the fiber preform, each strip covering an area of the fiber preform located facing a junction area between two adjacent angular sectors.

There is disclosed an apparatus for winding filaments to form a structure. The apparatus includes a carrier which mounts spools of fiber, a mandrel, and a guide element which directs fiber tows, comprising filaments from the spools, onto the mandrel. The system further includes a heating element which applies heat to the fiber tows, and a diaphragm element which defines an orifice about the mandrel. The diaphragm element includes one or more displaceable portions which define a physical dimension of the orifice and which: displace to vary the physical dimension of the orifice; and apply a predetermined pressure to the fiber tows disposed on the mandrel. Also disclosed and described is a related method.

There is disclosed an apparatus for winding filaments to form a structure. The apparatus includes a carrier which mounts spools of fiber, a mandrel, and a guide element which directs fiber tows, comprising filaments from the spools, onto the mandrel. The system further includes a heating element which applies heat to the fiber tows, and a diaphragm element which defines an orifice about the mandrel. The diaphragm element includes one or more displaceable portions which define a physical dimension of the orifice and which: displace to vary the physical dimension of the orifice; and apply a predetermined pressure to the fiber tows disposed on the mandrel. Also disclosed and described is a related method.

A thermoforming method includes forming a skin comprising a plurality of plies thermoplastic resin and fiber, securing an edge of the skin to a mandrel, heating, via a heating element, the skin to a forming temperature, moving a thermoforming apparatus with respect to the mandrel, rolling at least one roller of the thermoforming apparatus along the skin in a direction away from the clamped edge of the skin in response to the thermoforming apparatus moving with respect to the mandrel, and in response to the at least one roller of the thermoforming apparatus rolling along the skin, compressing the skin between the at least one roller and the mandrel, consolidating the plurality of plies of material, and bending the skin to conform to a shape of the mandrel. The consolidated and formed skin is then cooled and removed from the mandrel.

A thermoforming method includes forming a skin comprising a plurality of plies thermoplastic resin and fiber, securing an edge of the skin to a mandrel, heating, via a heating element, the skin to a forming temperature, moving a thermoforming apparatus with respect to the mandrel, rolling at least one roller of the thermoforming apparatus along the skin in a direction away from the clamped edge of the skin in response to the thermoforming apparatus moving with respect to the mandrel, and in response to the at least one roller of the thermoforming apparatus rolling along the skin, compressing the skin between the at least one roller and the mandrel, consolidating the plurality of plies of material, and bending the skin to conform to a shape of the mandrel. The consolidated and formed skin is then cooled and removed from the mandrel.

In a method for manufacturing a high-pressure tank, a fiber bundle impregnated with a thermosetting resin base material is wound around an outer surface of a liner in a state where tension is applied to the fiber bundle in a filament winding step. The filament winding step includes a pressure-bonding step and a cutting step. In the pressure-bonding step, a terminal end portion which is a winding end of the fiber bundle is thermocompression-bonded to an outer peripheral portion of the fiber bundle wound around the liner. In the cutting step, a surplus portion of the fiber bundle is cut by a cutting tool.

The tube body intermediate includes: a carbon fiber disposed with respect to an outer circumferential surface of a mandrel such that the carbon fiber extends in an axial direction of the mandrel in a manner of being wound by less than one turn; and a first fixing member wound with respect to an outer circumferential surface of the mandrel such that the first fixing member extends in the axial direction of the mandrel in a manner of being wound over the carbon fiber by one or more turns in a circumferential direction.

A tube body production method includes: a disposing step of disposing carbon fibers with respect to an outer circumferential surface of a mandrel so that the carbon fibers extend in the axial direction of the mandrel; and a molding step of impregnating the fiber body with a resin on the outer circumferential surface of the mandrel and then heating the resin to mold the resin, wherein the disposing step and the molding step are performed in a state where the axial direction of the mandrel coincides with an up-down direction.

A method of manufacturing a high-pressure composite pressure vessel for high-pressure being at or above 70 bar (1000 PSI or 7 MPa) includes providing an expandable core vessel defining a hoop section between end domes. An aligned discontinuous fiber composite material is wrapped over the expandable core vessel aligning with a plurality of load paths present in the expandable core vessel being over the hoop section and end domes. The aligned discontinuous fiber composite material has fibers in a prepreg tape that are at least 5 mm in length to 100 mm in length or less. Next, a continuous fiber-reinforced composite is wrapped over the aligned discontinuous fiber-reinforced composite along the hoop section and not wrapped along the end domes. The expandable core vessel may be pressurized and heated to consolidate the composite overwrap. Finally, the vessel is cooled under pressure resulting in the high-pressure composite pressure vessel.