Flap hinge mechanism for an aircraft aerodynamic surface

Details Flap hinge mechanism for an aircraft aerodynamic surface Flap hinge mechanism for an aircraft aerodynamic surface

B - Operations, Transporting

64

C

B64C 9/32 (2006.01) B64C 7/00 (2006.01) B64C 9/02 (2006.01) B64C 9/34 (2006.01)

Patent

CA 2428137

- Device for articulating a flap to an aircraft aerodynamic surface. - According to the invention, the cutout (12) made in the rear edge of the aerodynamic surface (2) for the passage of the fitting (11) is blanked off by a blanking piece (16) borne by a linkage (18).

- Dispositif d'articulation d'un volet sur une surface aérodynamique d'aéronef. - Selon l'invention, l'échancrure (12), pratiquée dans le bord arrière de la surface aérodynamique (2) pour le passage de la ferrure (11), est obtu- rée par un obturateur (16) porté par une tringlerie (18).

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