Trailing edge flap operation in wings

Aeronautics and astronautics – Aircraft sustentation – Sustaining airfoils

Patent

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Details

241213, 241217, B64C 918

Patent

active

047968400

ABSTRACT:
Flap carriers fold spanwise (about chordwise axes) into the wing but are moved down together through pivotal linkage; the flaps are protracted and retracted through pivoting of the carriers relative to each other on spanwise axes. On retraction, the entire assembly fits into the wing so that the flow determining contour thereof remains undisturbed.

REFERENCES:
patent: 2591000 (1952-04-01), O'Brien
patent: 2688455 (1954-09-01), Clark
patent: 3977630 (1976-08-01), Lewis et al.
patent: 4172575 (1979-10-01), Cole
patent: 4434959 (1984-03-01), Rudolph
patent: 4444368 (1984-04-01), Andrews

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