High lift longitudinal axis control system

Aeronautics and astronautics – Aircraft sustentation – Sustaining airfoils

Reexamination Certificate

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Details

C244S198000, C244S201000

Reexamination Certificate

active

11047194

ABSTRACT:
A bipartite, full span airplane flap system having an inboard flap portion and an outboard flap portion, wherein the outboard flap portion includes an integrated aileron mounted on its substantially equivalent spanwise length.

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Flap (B) and aileron (D)—“High Lift Research,” Flight, p. 409-410, Youngman et al., Sep. 30, 1948.

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