A drive shaft for an aircraft according to an example of the present disclosure includes, among other things, an elongated core extending between a pair of opposed couplings, an energy absorption layer made of a composite comprising metal, the energy absorption layer disposed on the core, and a first composite ballistic layer disposed along a length of the core.

A method of fabricating a strut having a hollow central bore includes the steps of providing a mandrel and a quantity of a filament or fiber material, laying the filament or fiber material about the mandrel to form a strut having a central cylindrical section, two opposing connective end sections, a central bore extending through the strut, the central bore having two reduced diameter portions extending through each end section, and an axis extending centrally through the bore, forming a slot or slots extending inwardly from one of the connective section outer ends and terminating within the connective section or the central section, bending at least a portion of the one connective section along the slot to enlarge the bore reduced diameter section at the one end, and displacing the mandrel along the central axis and through the enlarged bore end section until the mandrel is removed from the bore.

A transmissive joint has an elastic response for transmitting a torsional load capable of ensuring the transmission in the absence of coaxiality between two actuating and actuated devices, and allowing the internal passage of cabling or possible accessory components along the axis of transmission/torsion.

A composite vehicle driveshaft is provided with a composite tube and a welded joint system(s) at one or both ends of the composite tube for connecting the composite vehicle driveshaft to driveline components. Each welded joint system may include a sleeve that is bonded to an end of the composite tube and a joint assembly that is welded to the sleeve.

A hybrid propeller shaft may include a CFRP tube layer in which high-strength CFRP or high-elasticity CFRP, the high-strength CFRP, and the high-elasticity CFRP are laminated to form at least two layers while having different wrapping angles by a prepreg wrapping process method; and a protective layer which is formed on an outermost layer of the CFRP tube layer to protect the CFRP tube layer.

A processing equipment is provided, in which a carrier structure with at least one guide pin is arranged in a ring center area of a ring body of a frame, and a wire-supply device disposed on the ring body can supply wires to the center structure, so the wires can be woven around the guide pin and formed on the carrier structure so that the wire covers the carrier structure to form an exposed area around the guide pin.

A composite shaft assembly including a core structure formed by weaving fiber(s) into an open composite structure. The assembly further includes a first end piece and a second end piece having helically shaped groove(s) and/or axially groove(s) on an outer surface of an end portion of the first and second end piece. Woven into the helical and/or axial groove(s) on the first end piece and at least partially within through hole(s) disposed at an end of the groove(s) is the fiber(s) at a first end portion of the of the core structure. Woven into the helical and/or axial groove(s) on the second end piece and at least partially within through hole(s) disposed at an end of the groove(s) is the fiber(s) at a second end portion of the of the core structure. Structural adhesive(s) are applied over the fiber(s) and allowed to cure to form the composite drive shaft.

A connecting shaft including a first shaft made of metal, a second shaft made of resin, and a collar made of metal including a first fitting portion fitting on an outer peripheral surface of the first shaft and a second fitting portion fitting on an outer peripheral surface of the second shaft. A gap between the outer peripheral surface of the second shaft and an inner peripheral surface of the second fitting portion is filled with an adhesive agent, and the adhesive agent is applied to an outer peripheral surface of the collar to cover an end face of the second fitting portion in an axial direction.

A threaded shaft for a ball screw comprising: a shaft of fibre-reinforced polymer material; and a helical ridge formed on an outer surface of said shaft, said helical ridge being formed from a fibre-reinforced polymer material comprising a plurality of helical fibres wound around the shaft in the same sense and grouped together to form the ridge. The helical ridge formed from grouped helical fibres all wound with the same sense provides excellent axial load carrying capability as the fibres run continuously from end to end of the shaft and can thus transmit load from end to end. This adds much greater strength than a shaft formed from plastics only. The load carrying capability of the fibre wound helical ridge can indeed approach that of existing metal threads while still being much lighter in weight.

Systems, methods, and apparatus are disclosed for transferring a rotational force. Apparatus include a shaft member that has a first end configured to receive a rotational force from a first mechanical component, and configured to receive a torsional load in response to receiving the rotational force. The shaft member also includes a second end configured to provide the rotational force to a second mechanical component. Apparatus also include a support member that includes a plurality of lobes coupled to the shaft member and configured to transmit the torsional load of the shaft member, where the plurality of lobes is coupled to each other along a central coupling and extend radially from the central coupling, where the plurality of lobes has a spiral geometry along a length of the support member such that an orientation of the plurality of lobes rotates along the length of the support member.