Gull wing aircraft

Aeronautics and astronautics – Aircraft sustentation – Sustaining airfoils

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Details

244 45A, 244 89, B64C 316, B64C 504

Patent

active

055426255

ABSTRACT:
A vehicle, lacking an empennage, has a gull wing with ailerons movably mounted at the trailing edges of the wing for controlling pitch, yaw and roll, or has a wing and a gull tail with flaps movably mounted at the trailing edges of the tail surface for controlling pitch, yaw and roll.

REFERENCES:
patent: 3954231 (1976-05-01), Fraser
patent: 4116405 (1978-09-01), Bacchi et al.
patent: 4365773 (1982-12-01), Wolkovitch
patent: 4417708 (1983-11-01), Negri
patent: 5224665 (1993-07-01), Goldsberry et al.
Heincke, PCT Publication WO 84/01926 May 1984.
Hall, PCT Publication WO 88/06551 Sep. 1988.

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