Aircraft having multiple fuselages

Aeronautics and astronautics – Aircraft – heavier-than-air – Airplane sustained

Patent

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244117R, 244119, 244218, 244120, 244219, 244135R, B64C 100

Patent

active

06047923&

ABSTRACT:
An aircraft having a central fuselage, a first side fuselage positioned immediately adjacent to and independent of the central fuselage, and a second side fuselage positioned immediately adjacent to and independent of the central fuselage located on the opposite side of the first side fuselage is disclosed. All of the engines powering the aircraft are located either on the wings outboard of the side fuselages or in the rear of the aircraft aft of the wings. Further, the aircraft may include wings positioned laterally from both side fuselages which may be partially retracted during flight.

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Gunster, Bill, Giants of the Sky, 1991, pp. 267-270 Sparaco/Toulouse, Pierre, "Airbus Pursues UHCA Design Studies", Aviation Week & Space Technology (Jun. 7, 1993), pp. 115 & 116.

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