Method for manufacturing an aircraft structure component
A method for manufacturing an aircraft structure component of fiber composite material, wherein a semifinished first part made of a dry fiber preform is provided, a semifinished second part made of either a dry fiber preform or a hardened fiber matrix composite is provided, a semifinished aircraft structure component is prepared by placing the semifinished first part against the semifinished second part, such that a first connection surface rests against a second connection surface, matrix material is infused through the semifinished aircraft structure component, and the semifinished aircraft structure component is cured. Before infusing matrix material through the semifinished aircraft structure component, an intermediate layer for assisting adhesion is applied between the first connection surface and the second connection surface.
» Number: US2017151710A1 (A1)
» Publication Date: 01/06/2017
» Applicant: AIRBUS OPERATIONS GMBH?[DE]
» Inventor: BARLAG CARSTEN?[DE]
This project has received funding from the European Union's Horizon 2020 research and innovation programme under grant agreement Nº 768737