Method and mould for creating an aerodynamic element comprising riblets
AssigneeSafran
InventorsNicolas Pierre Lanfant, Emilie Goncalves
Life of this patent
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Abstract
A method for making an aerodynamic element, particularly for an aircraft, including an external face and a plurality of parallel ribs and/or grooves formed on the external face, the method including making the element and its ribs and/or its grooves simultaneously with a mold, including a step to supply a film made of a deformable material that includes ribs and/or grooves complementary to the ribs and/or grooves of the element, a step to position the film on a wall of the mold, a step in which the element is molded, a step in which the element is separated from the mold simultaneously with the film, and a step in which the film is separated from the element.
Claims9
A method for making an aerodynamic element comprising an external face on which an air flow circulates longitudinally and a top face and a plurality of parallel ribs and grooves formed on said external face, the method comprising:
- supplying a film made of a deformable material that comprises ribs and grooves complementary to the ribs and grooves of said aerodynamic element, the film including a smooth face, and an external surface comprising the ribs and grooves,
- positioning the film on a wall of a mold such that only the film is in the mold and the smooth face of the film abuts the wall of the mold, the mold delimiting a volume that is complementary to the aerodynamic element, and the wall of the mold on which the film is positioned being smooth and corresponding to the external face of the aerodynamic element,
- molding the aerodynamic element with the mold so as to make the aerodynamic element and the ribs and grooves on the external face of the aerodynamic element simultaneously,
- separating the aerodynamic element from the mold simultaneously with said film, and
- separating the film from the external face of the aerodynamic element such that there is no displacement of the film parallel to the top face of the aerodynamic element and no transverse or longitudinal action is applied to the ribs of the aerodynamic element.
Dependencies are inferred from the claim text.