Variable pivot trailing edge flap

Aeronautics and astronautics – Aircraft sustentation – Sustaining airfoils

Patent

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Details

B64C 904

Patent

active

040492192

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 two flap segments are pivotally joined. Linkage programming the aft flap segment is located and sized so that the two flap segments remain in the same relative position as to each other throughout main flap translation, but the aft flap segment may be rotated in either direction at any position by an actuating device.

REFERENCES:
patent: 2137879 (1938-11-01), Ksoll
patent: 2289704 (1942-07-01), Grant

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