Variable pivot trailing edge flap

Aeronautics and astronautics – Aircraft sustentation – Sustaining airfoils

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B64C 920

Patent

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039853195

ABSTRACT:
A double segmented airplane flap with the main flap movable by a four-bar linkage and the aft flap programmed with a linkage pivotally mounted to wing support structure. The linkage programming the aft flap segment extends from the wing support structure to an actuating axis point to convert downward movement of the link into rearward movement of a control linkage to control relative movement of the aft segment of the flap.

REFERENCES:
patent: 2137879 (1938-11-01), Ksoll
patent: 2583405 (1952-01-01), Youngman
patent: 3874617 (1975-04-01), Johnson
A.P.C. Application of J. Ksoll, Serial No. 245,580, Published May 25, 1943.

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