Aeronautics and astronautics – Aircraft structure – Fuselage and body construction
Patent
1998-02-05
2000-06-06
Poon, Peter M.
Aeronautics and astronautics
Aircraft structure
Fuselage and body construction
244119, 244117R, B64C 130
Patent
active
06070831&
ABSTRACT:
Aircraft for carrying passengers and/or freight based on a known aircraft design with a fuselage having a nose section, center section, and tail section and with airfoils mounted on the center section near the center of gravity of the aircraft and calculated for the required lift and with vertical and/or horizontal stabilizers located in the vicinity of the tail section for creating stabilizing and steering moments, with the fuselage of said aircraft being stretched by means of an additional section inserted between the nose section and the center of gravity of the aircraft model in order to increase the carrying capacity of the aircraft based on predetermined known aircraft designs, and with the additional section, as viewed in the direction of flight, being equipped forward of the airfoils of the aircraft model that serve as the main airfoils with airfoils that serve as additional airfoils, with previously designed and calculated airfoils of suitable size from a known aircraft design being used as the additional airfoils.
REFERENCES:
patent: 2597563 (1952-05-01), Breazeale, Jr.
patent: 2697569 (1954-12-01), Westcott, Jr.
patent: 3481567 (1969-12-01), Stearman
patent: 4165058 (1979-08-01), Whitener
patent: 4390150 (1983-06-01), Whitener
patent: 4417708 (1983-11-01), Negri
patent: 4449679 (1984-05-01), McComas
Eibel Karl-Heinz
Vassiliev Anatoli J.
Comer Vagnola K.
Poon Peter M.
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