Staggered channel wing-type aircraft

Aeronautics and astronautics – Aircraft sustentation – Sustaining airfoils

Patent

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244 45R, B64C 306, B64C 340

Patent

active

040531252

ABSTRACT:
A staggered channel aircraft having a forward pair of wings and a rearward pair of wings. The forward pair of wings are substantially horizontal and are swept backward from the fuselage to join at their tips the pair of rearward wings. The rearward wings are sloping and are swept backward from their tips to join the fuselage in a substantially triangular-like configuration.

REFERENCES:
patent: 1264037 (1918-04-01), Emmons
patent: 2461805 (1949-02-01), Barker
patent: 2576294 (1951-11-01), Geraci
patent: 2699300 (1955-01-01), Trotter et al.

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