An aerofoil having a slat

B - Operations – Transporting – 64 – C

Patent

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Details

B64C 9/24 (2006.01) B64C 9/22 (2006.01)

Patent

CA 2339205

The slat (16) is mounted to extend and retract relative to the aerofoil (10) and a data line (28) supported on a mounting cable (20) extends between the slat (16) and the aerofoil (10). The data line (28) is arranged to wrap around the leading edge (12) of the aerofoil (10) in the fully retracted position of the slat (16) and to extend substantially along a straight line between the aerofoil (10) and the slat (16) when the slat is in its fully extended position.

Selon l'invention, un bec (16) est monté pour s'abaisser et se rétracter par rapport à un profil aérodynamique (10). Une ligne de données (28) soutenue par un câble de montage (20) s'étend entre le bec (16) et le profil aérodynamique (10). Lorsque le bec (16) est complètement rétracté, la ligne de données (28) s'enroule autour du bord d'attaque (12) du profil aérodynamique (10), et lorsque le bec est complètement abaissé, elle s'étend sensiblement le long d'une ligne droite entre le profil aérodynamique (10) et ledit bec (16).

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