Aeronautics and astronautics – Aircraft sustentation – Sustaining airfoils
Reexamination Certificate
2007-11-13
2007-11-13
Eldred, J. Woodrow (Department: 3641)
Aeronautics and astronautics
Aircraft sustentation
Sustaining airfoils
C244S212000, C244S215000, C244S216000
Reexamination Certificate
active
10483380
ABSTRACT:
Lift flap mechanism for adjusting a lift flap assigned to an airplane wing by means of a driving system, the lift flap mechanism comprising a main connection mechanism and a secondary connection mechanism in the form of a guide lever disposed in an articulated manner on the lift flap and the flap track, the main connection mechanism having a steering lever arrangement with at least one steering lever which has a first steering lever joint and a second steering lever joint, the at least one steering lever by way of a pendulum coupled to the first steering lever joint being connected with the flap track, and the second steering lever joint being guided such that, by means of a defined angular position of the at least one steering lever, the positions of the main connection joint and of the secondary connection joint are unambiguously determined.
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Bechheim Claudia
Perez-Sanchez Juan
Voglsinger Martin
Crowell & Moring LLP
EADS Deutschland GmbH
Eldred J. Woodrow
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