Device for laying up a composite product with fibrous rovings made from glass, carbon, aramid and other similar filaments, designed especially for production of composite reinforcements or supporting elements such as the reinforcement of tailgates of personal vehicles, consists of individual unwinding spools (2) of fibrous rovings (21) rotatably arranged around the composite product (1). The unwinding spools (2) are installed on the set of the rotary disc rings (3) which are mounted on a common fixed ring frame (4) and equipped with independent drives (5) with pre-programmed control of direction and speed of their rotation wherein the composite product (1) is during the laying up procedure alternately fixed to individual carrier grippers (8) of at least one program-controlled manipulator (9). In each rotary disc ring (3) as well as in fixed ring frame (4) at least one lateral passage (6) is created for entry and exit of the composite product (1) between the unwinding spools (2).

Device for laying up a composite product with fibrous rovings made from glass, carbon, aramid and other similar filaments, designed especially for production of composite reinforcements or supporting elements such as the reinforcement of tailgates of personal vehicles, consists of individual unwinding spools (2) of fibrous rovings (21) rotatably arranged around the composite product (1). The unwinding spools (2) are installed on the set of the rotary disc rings (3) which are mounted on a common fixed ring frame (4) and equipped with independent drives (5) with pre-programmed control of direction and speed of their rotation wherein the composite product (1) is during the laying up procedure alternately fixed to individual carrier grippers (8) of at least one program-controlled manipulator (9). In each rotary disc ring (3) as well as in fixed ring frame (4) at least one lateral passage (6) is created for entry and exit of the composite product (1) between the unwinding spools (2).

Method for manufacturing a continuous composite tube comprising translating a tube liner through a manufacturing station wherein the manufacturing station comprises a winding station and a consolidation station located at a distance downstream of the winding station; winding a composite tape on the tube liner at the winding station for forming a tape layer; consolidating the composite tape on the tube liner at a consolidation zone of the consolidation station by pressing and heating to the tape.

Methods and systems are disclosed for onsite real-time manufacturing of any length, shape, size, and any thickness pipe. Strips of fabrics saturated with resin are helically wrapped around desired shape mandrels in one direction and removed, at least partially cured, to form such pipes onsite. The system can be mounted on a moving vehicle to manufacture and lay down any length pipe as it moves, or the system can be stationary. Disclosed pipes eliminate almost all weaknesses of plastic, metal and concrete pipes and noticeably reduce costs of transportation as well as manufacturing. One of the advantages of the disclosed pipes is that they have no joints, limiting the leakage and other problems associated with joints in ordinary pipes. Another advantage of the disclosed pipes is that it can have any number of desired layers at any desire cross-section of the pipe.

A helical winding unit includes a plurality of guides arrayed in a peripheral direction of a liner, and adapted to guide each of a plurality of fiber bundles supplied to the helical winding unit to the liner, and an opening member arranged downstream of the plurality of guides in a travelling direction of the fiber bundle, and including an inner peripheral surface for forming a hole, through which the plurality of fiber bundles are inserted from one side to the other side in the axial direction. A plurality of opening surfaces on which the plurality of fiber bundles travel while making contact are formed on the inner peripheral surface of the opening member, and a cross-sectional shape orthogonal to the axial direction of each opening surface is linear.

An expiratory limb for a breathing circuit includes an enclosing wall defining a flexible singular expiratory flow passage between an inlet and an outlet and bounding the flexible singular expiratory flow passage and ambient air. The expiratory limb includes one or more regions of the enclosing wall that made from a material that allows passage of water vapor without allowing passage of liquid water, thereby forming a water vapor flow path from the flexible singular expiratory flow passage to the ambient air through the material. The expiratory limb is configured to allow diffusion of water vapor along the flexible singular expiratory flow passage and dry the flow of expiratory gases between the inlet and the outlet.

An expiratory limb for a breathing circuit includes an enclosing wall defining a flexible singular expiratory flow passage between an inlet and an outlet and bounding the flexible singular expiratory flow passage and ambient air. The expiratory limb includes one or more regions of the enclosing wall that made from a material that allows passage of water vapor without allowing passage of liquid water, thereby forming a water vapor flow path from the flexible singular expiratory flow passage to the ambient air through the material. The expiratory limb is configured to allow diffusion of water vapor along the flexible singular expiratory flow passage and dry the flow of expiratory gases between the inlet and the outlet.

Method for manufacturing a continuous composite tube comprising translating a tube liner through a manufacturing station wherein the manufacturing station comprises a winding station and a consolidation station located at a distance downstream of the winding station; winding a composite tape on the tube liner at the winding station for forming a tape layer; consolidating the composite tape on the tube liner at a consolidation zone of the consolidation station by pressing and heating to the tape.

A guide wheel (26) for fitting a layer of carbon armor wires around a tubular core (24). The guide wheel (26) has a central cavity (32), an internal circular edge (34), and a peripheral circular edge (38) that extends coaxially at a distance from said internal circular edge (34), the guide wheel (26) includes a plurality of guiding devices (46), each of which is capable of guiding in translation a plurality of carbon armor wires, the guiding devices being mounted around said central cavity (32). The guiding device (46) includes a peripheral redirecting member (50) in order to be able to guide the carbon armor wires to the internal circular edge (34), and a central redirecting member (52) in order to be able to guide said carbon armor wires through a second curved passageway.

A guide wheel (26) for fitting a layer of carbon armor wires around a tubular core (24). The guide wheel (26) has a central cavity (32), an internal circular edge (34), and a peripheral circular edge (38) that extends coaxially at a distance from said internal circular edge (34), the guide wheel (26) includes a plurality of guiding devices (46), each of which is capable of guiding in translation a plurality of carbon armor wires, the guiding devices being mounted around said central cavity (32). The guiding device (46) includes a peripheral redirecting member (50) in order to be able to guide the carbon armor wires to the internal circular edge (34), and a central redirecting member (52) in order to be able to guide said carbon armor wires through a second curved passageway.