Rudder of a commercial aircraft

B - Operations – Transporting – 64 – C

Patent

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Details

B64C 9/32 (2006.01) B64C 23/06 (2006.01)

Patent

CA 2628325

The application describes a rudder of a commercial aircraft. According to the invention, the rudder (100) is divided along its longitudinal direction in at least one region, and the parts (100a, 100b) of the rudder (100) can be spread against the air flow surrounding the aircraft by means of an actuator (103) in order to decelerate the aircraft.

La présente invention concerne une gouverne de direction d~aéronef commercial. Selon la présente invention, la gouverne de direction (100) est séparée le long de sa direction longitudinale en au moins une région et les parties (100a, 100b) de la gouverne de direction (100) peuvent être écartées contre l~écoulement d~air entourant l~aéronef au moyen d~un actionneur (103) afin de ralentir l~aéronef.

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