Single slotted flap with sliding deflector flap and...

Aeronautics and astronautics – Aircraft sustentation – Sustaining airfoils

Reexamination Certificate

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Details

C244S213000, C244S215000, C244S217000

Reexamination Certificate

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08066228

ABSTRACT:
A device for adjusting the lift characteristics of an aircraft with a high lift device that is movably attachable to a wing element and that includes at least one slot covering device, where the at least one slot covering device, is movably attachable to the wing element. The slot covering device is designed to regulate the size of a slot between the wing element and the high lift device.

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patent: 1407964 (2004-04-01), None
patent: 5-238488 (1993-09-01), None
patent: 2187445 (2002-08-01), None
patent: 96/36532 (1996-11-01), None

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