Fixed-wing aircraft with tandem supporting surfaces

Aeronautics and astronautics – Aircraft control – Automatic

Patent

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Details

244 45A, 244178, 364435, 364442, B64C 1316

Patent

active

045988889

ABSTRACT:
A fixed-wing aircraft with tandem lifting surfaces has monoplane main wings secured in an intermediate area of the fuselage and a horizontal tail surface with at least one stabilizer plane mounted at the tail of the fuselage. A third supporting surface on the fuselage is in tandem arrangement with the other supporting surfaces. The third supporting surface is a canard surface positioned ahead of the center of gravity of the aircraft.

REFERENCES:
patent: 2402311 (1946-06-01), Bissett
patent: 2541620 (1951-02-01), Stalker
patent: 2601962 (1952-07-01), Douglas
patent: 2924400 (1960-02-01), Ruget
patent: 3240447 (1966-03-01), Olshausen
patent: 3253809 (1966-05-01), Robertson
patent: 3362659 (1968-01-01), Razak
patent: 3680816 (1972-08-01), Mello
patent: 3848833 (1974-11-01), Rauschelbach
patent: 3954231 (1976-05-01), Fraser
patent: 4159088 (1979-06-01), Cosley

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