Aircraft wing with extendible nose flap

Aeronautics and astronautics – Aircraft sustentation – Sustaining airfoils

Reexamination Certificate

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Details

C244S210000, C244S211000, C244S212000, C244S213000, C244S214000, C244S215000, C244S216000, C244S217000

Reexamination Certificate

active

07484694

ABSTRACT:
An aircraft wing including a wing box and a nose flap moveably connected to the wing box by first and second folding hinges. A first transverse link is pivotally connected to first portions of the first and second folding hinges. A second transverse link is pivotally connected to second portions of the first and second folding hinges. An actuator is connected diagonally between the first and second transverse links for moving the nose flap between a retracted position and an extended position. The instant abstract is neither intended to define the invention disclosed in the specification nor intended to limit the scope of the invention in any way.

REFERENCES:
patent: 7063292 (2006-06-01), Perez-Sanchez
patent: 103 28 717 (2004-12-01), None

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