Flap mechanism

Aeronautics and astronautics – Aircraft sustentation – Sustaining airfoils

Patent

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Details

B64C 350

Patent

active

045428697

ABSTRACT:
A mechanism for supporting and translating a wing trailing edge flap system. The flap is pivotally supported by a carriage and track at one point and the free ternary link of a four-bar linkage at a second point, to combine and form an overall six-bar linkage system of the Stephenson III type.

REFERENCES:
patent: 2608364 (1952-08-01), Gordon et al.
patent: 2688455 (1954-09-01), Clark
patent: 3853289 (1974-12-01), Nevermann et al.
patent: 4172575 (1979-10-01), Cole
patent: 4381093 (1983-04-01), Rudolph

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