Aeronautics and astronautics – Aircraft control – Rudders and empennage
Reexamination Certificate
2011-08-30
2011-08-30
Dinh, Tien (Department: 3644)
Aeronautics and astronautics
Aircraft control
Rudders and empennage
C244S088000, C244S099200, C244S099300
Reexamination Certificate
active
08006932
ABSTRACT:
A pivoting coupling system of a large dihedral empennage to the tail fuselage of an aircraft, in which the empennage includes a right lateral box and a left lateral box arranged at a large dihedral angle in the tail fuselage of the aircraft. The pivoting coupling system including a horizontal central box joining the lateral boxes, and which includes a rear spar; and a linkage for horizontally linking the central box to a frame structure of the tail fuselage of the aircraft, which allow the empennage to rotate vertically about a horizontal linkage shaft between a negative maximum angle of incidence and a positive maximum angle of incidence in response to the actuation of an actuator which is connected to the empennage and to a structural element of the fuselage of the aircraft.
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Richardson, D. et al.The Great Book of Modern Warplanes. New York: Salamander Books, 1987. pp. 538-541. ISBN 0-517-63367-1.
García Sacristán Angel
Honorato Ruiz Francisco Javier
Airbus Operations, S.L.
Bonzell Philip J
Dinh Tien
Wenderoth , Lind & Ponack, L.L.P.
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