초록 ▼

The invention relates to a method of cutting off laminate layers for use in a fiber-reinforced laminate object comprising a number of combined laminate layers, wherein, along a section of the at least one rim of the laminate layer, a tapering cut is performed through the thickness of the laminate la

The invention relates to a method of cutting off laminate layers for use in a fiber-reinforced laminate object comprising a number of combined laminate layers, wherein, along a section of the at least one rim of the laminate layer, a tapering cut is performed through the thickness of the laminate layer, whereby the thickness of the laminate layer is reduced. Since not only the number of laminate layers, but also the thickness of the individual laminate layers are reduced, a laminate layer is accomplished that can be used in a laminate object, by which both the issues of areas rich in resin, air pockets and the risk of delamination are reduced. The invention also relates to a laminate layer for use in a fiber-reinforced laminate object comprising a number of combined laminate layers and a fiber-reinforced laminate object in the form of the blade of a wind turbine, wherein the blade of the wind turbine comprises a number of combined laminate layers.

대표청구항 ▼

1. A fiber reinforcement layer for use in a fiber-reinforced laminate plastic composite comprising a number of combined laminate layers, wherein each fiber reinforcement layer along a section of at least one rim is tapered through the thickness of the fiber reinforcement layer, the fiber reinforceme

1. A fiber reinforcement layer for use in a fiber-reinforced laminate plastic composite comprising a number of combined laminate layers, wherein each fiber reinforcement layer along a section of at least one rim is tapered through the thickness of the fiber reinforcement layer, the fiber reinforcement layer comprising: a layer of glass fibers or carbon fibers,wherein the fiber reinforcement layer is not-hardened, andwherein the fiber reinforcement layer comprises fibers which are laid primarily in one direction or the fibers are laid biaxially in two directions at some angle or other in relation to each other. 2. The fiber reinforcement layer according to claim 1, wherein the fiber reinforcement layer is non-impregnated. 3. The fiber reinforcement layer according to claim 1, wherein the fiber reinforcement layer is tapered at an end face of the fiber reinforcement layer. 4. A fiber-reinforced laminate object comprising a number of combined laminate layers, wherein at least one of said number of combined laminate layers is formed from a fiber reinforcement layer according to claim 1. 5. A fiber-reinforced blade for a wind turbine, the fiber-reinforced blade comprising a number of combined laminate layers, wherein at least one of said number of combined laminate layers is formed from a fiber reinforcement layer according to claim 1. 6. A fiber reinforcement layer for use in a fiber-reinforced laminate plastic composite comprising a number of combined laminate layers, wherein each fiber reinforcement layer along a section of at least one rim is tapered through the thickness of the fiber reinforcement layer, the fiber reinforcement layer comprising: a layer of glass fibers or carbon fibers,wherein the fiber reinforcement layer is not-hardened,wherein the fiber reinforcement layer comprises fibers which are laid primarily in one direction or the fibers are laid biaxially in two directions at some angle or other in relation to each other, andwherein the fiber reinforcement layer is non-impregnated.