Improved slat configuration for fixed-wing aircraft

Details Improved slat configuration for fixed-wing aircraft Improved slat configuration for fixed-wing aircraft

B - Operations, Transporting

64

C

B64C 9/24 (2006.01)

Patent

CA 2719163

A slat (7) for fixed-wing aircraft that includes a leading edge (3), a trailing edge (5), a chord (C), and an inboard edge (6) that includes particular dimensions (C1, delta) to affect airflow over the wing (2).

L'invention porte sur un bec de bord d'attaque (7) pour un aéronef à voilure fixe, lequel bec de bord d'attaque comporte un bord d'attaque (3), un bord de fuite (5), une corde (C) et un bord interne (6) qui comporte des dimensions particulières (C1, delta) pour modifier l'écoulement d'air au-dessus de l'aile (2).

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