Method for producing a sandwich construction, in particular a sandwich construction for the aeronautical and aerospace fields
View Patent ↗The present invention provides a method of producing a construction, in particular a sandwich construction for the aeronautical and aerospace fields, comprising the following steps. A heating material is initially applied on one side of a core construction material. In a further step a reinforcing element is introduced into the core construction material and the heating material in such a way that the reinforcing element extends through the core construction material and the heating material and has a portion which projects beyond the heating material. The heating material is then heated to soften the projecting portion at least in regions and said projecting portion is subsequently deformed using the softened region as a pivot point to engage the core construction material from behind and to form the construction. This method is distinguished in particular by the fact that it allows the portions to be heated substantially simultaneously, and not sequentially as in the state of the art. The time saved as a result in turn has a positive effect on production costs.
1. A method of producing a construction, in particular a sandwich construction for the aeronautical and aerospace fields, comprising the following steps:
applying a heating material on one side of a core construction material;
introducing a reinforcing element into the core construction material and the heating material in such a way that the reinforcing element extends through the core construction material and the heating material and has a portion which projects beyond the heating material;
connecting a power source to the heating material;
heating the heating material to soften the projecting portion at least in a region adjacent the heating material by
sending a current generated by the power source through the heating material;
and
deforming the projecting portion using the region that has been softened as a pivot point to form the construction.
2. The method according to claim 1 , wherein the projecting portion is deformed in such a way that it comes to lie on the heating material or on an intermediate material applied thereon.
3. The method according to claim 1 , wherein a cover material is applied on the heating material or an intermediate material, including the projecting portion of the reinforcing element which lies thereon.
4. The method according to claim 1 , wherein the heating material, an intermediate material and/or a cover material comprises a matrix which becomes free-flowing by heating the heating material, causing the matrix to flow into an annular gap between the reinforcing element and the core construction material and thus to seal said annular gap.
5. The method according to claim 1 , wherein an intermediate material is applied on the other side of the core construction material, at least in the region of an annular gap between the reinforcing element and the core construction material, a matrix in the intermediate material becoming free-flowing by heating the heating material, causing the matrix to flow into the annular gap and thus seal said annular gap.
6. The method according to claim 1 , wherein the heating material, an intermediate material, the reinforcing element and/or a cover layer comprises a matrix which is cured by heating the heating material.
7. The method according to claim 1 , wherein at least the projecting portion of the reinforcing element comprises a thermosetting polymer material which is cross-linked only in part, a thermoplastic polymer material and/or fibres.
8. The method according to claim 1 , wherein the heating material is formed as a resistive heating material comprising electrical contacts for connection to said power source.
9. The method according to claim 1 , wherein the heating material is formed from a carbon material and/or glass.