An aircraft fin and rudder

Details An aircraft fin and rudder An aircraft fin and rudder

B - Operations, Transporting

64

C

B64C 9/00 (2006.01) B64C 5/06 (2006.01)

Patent

CA 2339208

The fin (12) has an end plate (16) mounted at its upper end and the end plate covers the upper end of the rudder, so that the rudder (14) seals against the end plate at all rudder deflections. The fin and rudder lift curved slopes are increased by the effect of the end plate (16).

Selon cette invention, la dérive (12) possède une plaque terminale (16) montée à son extrémité supérieure et recouvrant l'extrémité supérieure du gouvernail. De cette manière, le gouvernail (14), quelle que soit sa déflexion, est maintenu appliqué à la plaque terminale. L'effet de la plaque terminale (16) augmente l'inclinaison incurvée de la dérive et du gouvernail.

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