Aeronautics and astronautics – Aircraft sustentation – Sustaining airfoils
Reexamination Certificate
2011-06-21
2011-06-21
Dinh, Tien (Department: 3644)
Aeronautics and astronautics
Aircraft sustentation
Sustaining airfoils
C244S213000
Reexamination Certificate
active
07963484
ABSTRACT:
A lift-augmenting leading edge flap for a carrying wing of an aircraft, wherein the flap comprises an essentially rigid main body which makes a transition from the first side to the second side of the wing the flap being adjustable by a retention- and actuation mechanism coupled between the flap and wing box, between a first, retracted, position and a second, extended, position, wherein the first transition region of the flap is slidable to rest in each position essentially free of any gap, against the first skin of the wing box or against the wing end cover, in relation to the wing end cover.
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Andreani Luc
Heintjes Mark
Hue Xavier
Raudszus Morten
Schlipf Bernhard
Airbus Deutschland GmbH
Benedik Justin
Dinh Tien
Lerner David Littenberg Krumholz & Mentlik LLP
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