The tool (1) has a male type mold (2) comprising a hub (3) and an intermediate element (5) that surrounds the hub partially. Detachable modules (6) are juxtaposed with each other and fixed on an external face of the intermediate element, so that an external surface (7) of the module and element assembly is adapted to an internal surface of the composite material panel. One of the detachable modules is fixed on the intermediate element using mechanical fixation units or a magnetic system. (Incomplete specification, abstract based on available information published by the patent office). An independent claim is also included for a method for realizing a tool for manufacturing a composite material panel of a fuselage of an aircraft.
OUTILLAGE POUR LA FABRICATION D'UN PANNEAU EN MATERIAU COMPOSITE, EN PARTICULIER D'UN FUSELAGE D'AERONEF
2018-03-02
Patent
Electronic Resource
French
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