Method for producing a fibre composite component for air and space technology
AssigneeAirbus Operations GmbH
InventorChristian Nitsch
Life of this patent
Estimating the term…
Abstract
A method for producing a fiber composite component, in particular for aerospace, the method comprising the following steps: forming a mold core from a material comprising cork by a molding tool to establish an outer geometry of said mold core; arranging the so formed mold core adjacent to an at least partly hardened stiffening element on a base element of said composite component to be produced for the shaping of at least one molded portion of said fiber composite component to be produced; and multistage exposure of at least said molded portion to heat and/or pressure to produce said fiber composite component; a corresponding mold core and a corresponding fiber composite component.
Claims8
A method for producing a fibre composite component for the aviation and aerospace industry, which comprises the following steps:
- forming a mould core by a compression moulding process using a core tool for establishing an outer shape of the mould core, wherein the mould core is formed from a cork-containing material as a solid profiled part or as a hollow core with a core inner space, wherein the cork-containing material consists of a cork powder mixed with a binder and filler or a compound of cork granules and rubber granules, wherein the cork containing material is introduced into the core tool and brought into the desired shape with the cross section of the mould core, and wherein the mould core is provided with at least one fixing element;
- arranging the mould core formed thus such that it rests against an at least part cured reinforcing element on a base component of the fibre composite component to be produced for forming at least one mould portion of the fibre composite component to be produced, and for fixing the mould core on the reinforcing element, the at least one fixing element of the mould core cooperates magnetically with at least one fixing aid element which is removably attached to the reinforcing element;
- and
- charging in multiple stages at least the mould portion with heat and/or pressure to produce the fibre composite component;
- wherein the mould core is at least partly provided with a reinforcing layer consisting of tear-proof woven fabric, and wherein the reinforcing layer forms a separating layer preventing the material of the mould core from adhering to the core tool during forming or the reinforcing element during charging.
A mould core for producing a fibre composite component for the aviation and aerospace industry, wherein the mould core is formed by a compression moulding process from a cork-containing material as a solid profiled part or as a hollow core with a core inner space, wherein the cork-containing material consists of a cork powder mixed with a binder and filler or a compound of cork granules and rubber granules, and wherein the mould core is provided with at least one fixing element, wherein the mould core is at least partially provided with a reinforcing layer consisting of a tear-proof woven fabric, and wherein the reinforcing layer forms a separating layer preventing the material of the mould core from adhering to the core tool during forming or a reinforcing element during charging.
Dependencies are inferred from the claim text.