Abstract: Disclosed is a panel for an aircraft structure, including a laminated skin of layers of metal of which in each case two are joined together by a fibre-reinforced adhesive layer, as well as a laminated doubler of layers of metal and at least one fibre-reinforced adhesive layer in each case between two layers of metal, wherein the doubler has a smaller size of perimeter than the skin and is bonded to an outermost layer of metal of the laminated skin by a fibre-reinforced supplementary adhesive layer, with the feature that at least one part of the perimeter of the fibre-reinforced supplementary adhesive layer is staggered inwards relative to the corresponding perimeter of the doubler and that that part of the inwards-staggered perimeter of the fibre-reinforced supplementary adhesive layer is delimited by a glued edge. Also disclosed is a method for manufacturing such a panel.

Abstract: Disclosed is a panel for an aircraft structure, including a laminated skin of layers of metal of which in each case two are joined together by a fibre-reinforced adhesive layer, as well as a laminated doubler of layers of metal and at least one fibre-reinforced adhesive layer in each case between two layers of metal, wherein the doubler has a smaller size of perimeter than the skin and is bonded to an outermost layer of metal of the laminated skin by a fibre-reinforced supplementary adhesive layer, with the feature that at least one part of the perimeter of the fibre-reinforced supplementary adhesive layer is staggered inwards relative to the corresponding perimeter of the doubler and that that part of the inwards-staggered perimeter of the fibre-reinforced supplementary adhesive layer is delimited by a glued edge. Also disclosed is a method for manufacturing such a panel.

Abstract: A laminate of metal layers and plastic bonding layers situated between the metal layers includes two external metal layers extending substantially continuously and at least one internal metal layer. At least one of the internal metal layers has at least one opening, and at the position of the opening the other metal layers and plastic bonding layers are bonded together to the form of a packet of lower thickness. The relatively thick parts of the laminate can be used for the transfer of forces.

Abstract: In a laminate, comprising at least one series of metal layers and fiber-reinforced plastic layers which are attached to one another, at least two different series are provided, these series including a transition, and at the location of the transition at least one of the internal layers is discontinuous and all the other layers are continuous.

Abstract: A laminate has alternating metal layers and at least one plastic bonding layer. The metal layers each comprise at least two metal layer sections that have mutually overlapping edges bonded to one another. To even out the differences in thickness, a fill is provided which has at least a thickness such that at the location of the fill the laminate has a thickness equal to the thickness at the location of the overlapping edges.

Abstract: A method for the production under elevated pressure and temperate of a laminate (1, 1?) consisting of a pack with alternating metal layers (2) and plastic bonding layers (3), comprises stacking a first series (8) of layers on top of one another in a mould, then stacking at least a second series (7, 7?) of layers on top of the first series (8) of layers, with the formation of the pack of layers such that at at least one edge of the pack at least one (7 7?) of the series is stepped back with respect to the other series (8), an auxiliary tool (12) being placed alongside the stepped-back series (7, 7?) and on the other, non-stepped-back series (8) and a gap (13) being formed between the stepped-back series (7, 7?) and that side (14)of the auxiliary tool (12) facing said series, raising the temperature and the pressure on the pack and the auxiliary (12) tool such that the binder in the plastic bonding layers (3) is made to flow and some of the binder present in the stepped-back series (7, 7?) collects in said gap

Abstract: A method for the production under elevated pressure and temperature of a laminate (1, 1?) consisting of a pack with alternating metal layers (2) and plastic bonding layers (3), comprises stacking a first series (8) of layers on top of one another in a mould, then stacking at least a second series (7, 7?) of layers on top of the first series (8) of layers, with the formation of the pack of layers such that at at least one edge of the pack at least one (7, 7?) of the series is stepped back with respect to the other series (8), an auxiliary tool (12) being placed alongside the stepped-back series (7, 7?) and on the other, non-stepped-back series (8) and a gap (13) being formed between the stepped-back series (7, 7?) and that side (14) of the auxiliary tool (12) facing said series, raising the temperature and the pressure on the pack and the auxiliary (12) tool such that the binder in the plastic bonding layers (3) is made to flow and some of the binder present in the stepped-back series (7, 7?) collects in said

Abstract: A method for the production of a laminate consisting of metal layers as well as at least one fibre-reinforced bonding layer (5–7) that is located between the metal layers (1–4), which laminate has at least one region (9) that has a smaller number (3, 4, 7) of layers than the reminder of the laminate, comprises the following steps: forming a stack (8) consisting of metal layers (1–4) and at least one fibre layer (5–7) impregnated with a binder, which stack (8) has a first series (11) of successive layers (1, 2, 5, 6) with a different surface size to a second series (12) of successive layers (3, 4, 7), such that one (12) of the series of layers protrudes with respect to the other series (11) of layers, placing an auxiliary tool (14) at the protruding portion (19) of the protruding series (12) of layers alongside the other series (11) of layers, which auxiliary tool (14) has a make-up that is the same as that of said other series (11) of layers, activating the fibre-reinforced bonding layers (5, 6, 7) under e