Installation for manufacturing fibre stringers for aerospace structures
OwnerManuel Torres Martinezinventor
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Abstract
The present invention relates to an installation for manufacturing fiber stringers for aerospace structures formed by at least one swivel-mounted cylindrical carousel, peripherally incorporating a distribution of male configured tools and in relation to said carousel a bed capable of lateral movement, incorporating a distribution of female configured tools, a fiber strip applicator head for making fiber laminates on the male configured tools also being arranged in relation to the carousel, which allows making omega-shaped or T-shaped stringers by means of the interaction of each male configured tool of the carousel with a respective female configured tool of the bed.
Claims9
An installation for manufacturing fibre stringers for aerospace structures for making omega-shaped or T-shaped fibre stringers intended for being fixed as reinforcements on structures of application, comprising:
- at least one swivel-mounted cylindrical carousel peripherally incorporating a distribution of male configured tools, and in relation to said carousel a bed capable of lateral movement, incorporating a distribution of female configured tools, a fibre strip applicator head for making fibre laminates on the male configured tools of the carousel being arranged on a side of that assembly formed by the carousel and the bed, which fibre laminates are made in determination of omega-shaped or T-shaped stringers by means of the interaction of each male configured tool of the carousel in relation to a respective female configured tool of the bed.
Dependencies are inferred from the claim text.