Rudder of a commercial aircraft

Aeronautics and astronautics – Aircraft control – Rudders and empennage

Reexamination Certificate

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C244S099200, C244S217000

Reexamination Certificate

active

08061652

ABSTRACT:
A rudder of a commercial aircraft is provided that is divided along its longitudinal direction in at least one region and the parts of the rudder can be spread against the air flow surrounding the aircraft by means of an actuator in order to decelerate the aircraft.

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Sakaliyski, Aeroacoustics of Perforated Drag Plates for Quiet Transport Aircraft, Sep. 2005, Massachusetts Institute of Technology, pp. 1-197, Massachusetts, US.
Database WPI Week 200012; Derwent Publications Ltd., London.
Japanese Notice of Allowance, dated Aug. 9, 2011, for Japanese Patent Application No. 2008544858.

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