90 degree rotation aircraft wing

Aeronautics and astronautics – Aircraft sustentation – Sustaining airfoils

Patent

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Details

244328, 244 39, 244201, 244203, B64C 338

Patent

active

049986899

ABSTRACT:
A high speed aircraft fitted with a unitary, rotatable wing coupled to the craft's fuselage at a hollow turret or solid pivot pin, enabling it to operate with the wing in either of two ninety degree opposed positions.

REFERENCES:
patent: 3155344 (1964-11-01), Vogt
patent: 4453426 (1984-06-01), Groutage et al.
patent: 4842218 (1989-06-01), Groutage et al.

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