Flexible aerofoils

Aeronautics and astronautics – Aircraft sustentation – Sustaining airfoils

Patent

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B64C 348

Patent

active

041132106

ABSTRACT:
A flexible aerofoil has a series of members extending chordwise from a structure such as a main spar. The members are rotatably connected at points adjacent the pressure skin and are secured to the pressure skin. Rods, movable in a spanwise direction, act on the members at positions adjacent the suction skin to rotate the members relative to one another and therefore to alter the aerofoil camber.

REFERENCES:
patent: 1365346 (1921-01-01), Schenkel
patent: 1868748 (1932-07-01), Hogan
patent: 2448712 (1948-09-01), Hampshire
patent: 3179357 (1965-04-01), Lyon
patent: 3698668 (1972-10-01), Cole
patent: 3836099 (1974-09-01), O'Neill et al.

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