A pressure deck for an aircraft comprises a flat composite laminate base panel having integrated tear straps to enhance damage arrestment. The tear straps include a plurality of multi-ply, spaced apart longitudinal and lateral tear straps interspersed with the plies of the base panel.

A fiber-reinforced resin hollow body includes an axial-direction fiber layer containing reinforcing fibers aligned parallel to an axial direction of the hollow body, and a non-axial-direction fiber layer provided on top of at least one of an internal and an external side of the axial-direction fiber layer, and containing reinforcing fibers oriented in a direction different from a direction in which the reinforcing fibers contained in the axial-direction fiber layer are aligned. The non-axial-direction fiber layer has end portions in a peripheral direction of the hollow body, the end portions overlapping each other.

A golf club head includes a striking face, a crown and a sole. The crown and/or the sole includes an FRP member formed by a fiber reinforced plastic that contains a fiber and a matrix resin. The FRP member has an average flexural modulus of greater than or equal to 25 GPa. The fiber may contain a carbon fiber. The carbon fiber may have a tensile elastic modulus of greater than or equal to 300 GPa. The fiber may contain a metallic fiber. The FRP member may have a resin content of less than or equal to 40% by weight. The matrix resin may have a glass transition temperature of higher than or equal to 150° C.

A reinforced substrate is used for molding a composite material. The reinforced substrate includes a first region and a second region. The first region includes reinforcing fibers extending in a fiber direction that is aligned in a single direction. The second region includes the reinforcing fibers aligned in the same direction as the fiber direction and being thinner than the first region. The first region and the second region are lined up in alternating fashion in a plane along a direction intersecting the fiber direction.

Some embodiments are directed to a preform including reinforcing fibres and shape memory alloy (SMA) wires, a composite material including a polymer matrix with a preform embedded therein, articles including a composite material, methods of making preforms, composite materials and articles.

In a method for producing workpieces comprising fibre composite material, in which a base unit (5) held by retaining means (97) of a conveying device is guided by at least one application station (2, 14, 17, 20, 23, 27, 29,2, 14, 17, 20, 23, 27, 29, 39-41, 67-72) and, in order to form the workpieces at the application station (2, 14, 17, 20, 23, 27, 29,2, 14, 17, 20, 23, 27, 29, 39-41, 67-72) or at least at one of the application stations (2, 14, 17, 20, 23, 27, 29,2, 14, 17, 20, 23, 27, 29, 39-41, 67-72), during a translational movement of the base unit (5) through the application station (2, 14, 17, 20, 23, 27, 29,2, 14, 17, 20, 23, 27, 29, 39-41, 67-72) in question at least one strip (6) belonging to the fibre composite material is placed on the base unit (5), it is proposed that the spatial orientation of the base unit (5) is altered by means of at least one rotation relative to the retaining means (97) before the application station (2, 14, 17, 20, 23, 27, 29,2, 14, 17, 20, 23, 27, 29, 39-41, 67-72) or before at least one of the application stations (2, 14, 17, 20, 23, 27, 29,2, 14, 17, 20, 23, 27, 29, 39-41, 67-72) in the conveying direction. The invention furthermore relates to an apparatus suitable therefor.

A ballistic-resistant articles, and methods for their preparation, based on sheets of UHMWPE films with discontinuous film splits, which combine flexibility and good ballistic properties, making them suitable for both soft-ballistic and hard-ballistic applications.

Disclosed herein are internally fluted shafts for sporting goods such as archery arrows, crossbow bolts, and golf clubs, as well as methods of manufacturing shafts with fluted internal diameters or bracing.

In an example, a composite structure having a variable gage is described. The composite structure includes a first end having a first gage, a second end having a second gage, which is less than the first gage, a plurality of continuous plies, and a plurality of drop-off plies. Each continuous ply extends from the first end to the second end. Each drop-off ply includes a tip having a tapered shape. Each drop-off ply extends from the first end to a respective position of the tip of the drop-off ply between the first end and the second end. The tips of the plurality of drop-off plies are arranged in a monotonically-inward pattern.

The present invention relates to a composite material comprising one or more fibre layers composed of a fibre material and an aromatic polycarbonate-based matrix material. The fibre layer(s) is/are embedded in the matrix material. The present invention further relates to a process for producing these fibre composite materials, to multilayer composite materials comprising several layers of fibre composite material, and to the use of the composite materials for production of components or housing components or housings, and to the components, housing components or housings themselves.