Layers of plies of composite material are laid on a convex tool surface. A first layer is placed with a first ply of a first section having a gap edge adjacent a gap edge of a first ply of a second section, the edges being parallel and a contraction distance from each other. A second layer is placed with a second ply of the first section having a gap edge adjacent a gap edge of a second ply of the second section, the edges being parallel and a contraction distance from each other, the second ply of the second section overlapping onto the first ply of the first section by a splice distance. Consolidation and curing cause contraction of the layers toward the tool, allowing the adjacent gap edges of each layer to be in close proximity or in contact after moving toward each other during the contraction.

Layers of plies of composite material are laid on a convex tool surface. A first layer is placed with a first ply of a first section having a gap edge adjacent a gap edge of a first ply of a second section, the edges being parallel and a contraction distance from each other. A second layer is placed with a second ply of the first section having a gap edge adjacent a gap edge of a second ply of the second section, the edges being parallel and a contraction distance from each other, the second ply of the second section overlapping onto the first ply of the first section by a splice distance. Consolidation and curing cause contraction of the layers toward the tool, allowing the adjacent gap edges of each layer to be in close proximity or in contact after moving toward each other during the contraction.

A composite stiffener for a stiffener reinforced panel is disclosed. The stiffener has a longitudinal direction and a run-out region which terminates at an end of the stiffener. The stiffener also has a constant section region inboard of the run-out region in the longitudinal direction and having a constant cross section transverse to the longitudinal direction with a crown between adjacent foot portions. The run-out region has a changing cross section transverse to the longitudinal direction with a crown between adjacent foot portions and the crown reduces in height towards the end of the stiffener forming a ramp. The composite stiffener comprises a number of blankets of non-crimp fabric layers.

A composite stiffener for a stiffener reinforced panel is disclosed. The stiffener has a longitudinal direction and a run-out region which terminates at an end of the stiffener. The stiffener also has a constant section region inboard of the run-out region in the longitudinal direction and having a constant cross section transverse to the longitudinal direction with a crown between adjacent foot portions. The run-out region has a changing cross section transverse to the longitudinal direction with a crown between adjacent foot portions and the crown reduces in height towards the end of the stiffener forming a ramp. The composite stiffener comprises a number of blankets of non-crimp fabric layers.

Provided are multilayer structures and articles comprising same. The multilayer structure comprises: a biaxially-oriented polyethylene film comprising a skin layer with a matte surface and a core, the core comprising one or more core layers; a sealant film; and an adhesive adhering the sealant film to the matte surface of the skin layer of the biaxially-oriented polyethylene film. The multilayer structure can exhibit an enhanced adhesive bonding force in comparison to other multilayer structures.

Provided are multilayer structures and articles comprising same. The multilayer structure comprises: a biaxially-oriented polyethylene film comprising a skin layer with a matte surface and a core, the core comprising one or more core layers; a sealant film; and an adhesive adhering the sealant film to the matte surface of the skin layer of the biaxially-oriented polyethylene film. The multilayer structure can exhibit an enhanced adhesive bonding force in comparison to other multilayer structures.

The present disclosure relates to a polyester film and a preparation method of the same. Since the polyester film includes a resin layer formed from a mixture comprising a polyester resin, which includes a first diol moiety derived from isosorbide and a second diol moiety derived from cyclohexanedimethanol in a controlled ratio, and polyethylene terephthalate in a specific ratio, it is possible to exhibit improved heat resistance and adhesion with excellent light transmittance.

A charge is formed of a plurality of layers of fiber-reinforced sheets. The charge includes an outermost-layer multi-stack member disposed at each end section in a layering direction; and an intermediate-layer multi-stack member disposed in an intermediate section in the layering direction. The outermost-layer multi-stack member includes a fiber-reinforced sheet in which fibers extend in an X-axis direction in which compression force or tensile force acts when the charge is subjected to bending processing; and has formed therein a plurality of incisions that penetrate in the layering direction and extend in a Y-axis direction. The plurality of incisions are disposed side by side at prescribed intervals in the Y-axis direction and the X-axis direction. An incision that penetrates in the layering direction and extends in the Y-axis direction is formed in the intermediate-layer multi-stack member. The incision extends roughly the entire region affected by compression force or tensile force.

A charge is formed of a plurality of layers of fiber-reinforced sheets. The charge includes an outermost-layer multi-stack member disposed at each end section in a layering direction; and an intermediate-layer multi-stack member disposed in an intermediate section in the layering direction. The outermost-layer multi-stack member includes a fiber-reinforced sheet in which fibers extend in an X-axis direction in which compression force or tensile force acts when the charge is subjected to bending processing; and has formed therein a plurality of incisions that penetrate in the layering direction and extend in a Y-axis direction. The plurality of incisions are disposed side by side at prescribed intervals in the Y-axis direction and the X-axis direction. An incision that penetrates in the layering direction and extends in the Y-axis direction is formed in the intermediate-layer multi-stack member. The incision extends roughly the entire region affected by compression force or tensile force.

A useful composite layer can be a single layer composite of fiber lengths dispersed in a polymer. A useful laminate composite can have a minimum structure of three or more layers. The laminate can have a center layer combined with two outside single layers.