Aircraft outboard control

Aeronautics and astronautics – Aircraft sustentation – Sustaining airfoils

Patent

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Details

244 45R, 244 90R, 244 91, 244214, 244199, B64C 508

Patent

active

051563584

ABSTRACT:
An outboard control surface for an aircraft. The control surface is operably connected to wing side edges of the aircraft and includes a forward flap and a rearward flap with at least one of the flaps being movable into and out of alignment with the plane of the wing.

REFERENCES:
patent: 2925233 (1960-02-01), Dunn et al.
patent: 2960285 (1960-11-01), Lopez
patent: 3310262 (1967-03-01), Robins et al.
patent: 4093156 (1978-06-01), Coe, Jr.
patent: 4247062 (1981-01-01), Brueckner
patent: 4293110 (1981-10-01), Middleton et al.
patent: 4466586 (1984-08-01), Burnham
patent: 4478378 (1984-10-01), Capuani
patent: 4485992 (1984-12-01), Rao
patent: 4566657 (1986-01-01), Grow
patent: 4582276 (1986-04-01), Gerhardt
patent: 4598885 (1986-07-01), Waitzman
patent: 4722499 (1988-02-01), Klug
patent: 4729528 (1988-03-01), Borzachillo
General Dynamics "Getol Multibased VP Concept" Sep. 1962.
Naca Research Memorandum "Preliminary Study of Airplane Configuration Having Tail Surfaces Outboard of the Wing Tips", William C. Sleeman, Jr., Mar. 24, 1958.

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