Title:
JET-PROPELLED AIRCRAFT
Document Type and Number:
Japanese Patent JP06255590
Kind Code:
A
Abstract:
PURPOSE: To reduce the risk of an accident and the intense consumption of fuel in a jet-propelled aircraft using respective turbines.
CONSTITUTION: An aircraft fuselage 1 is in the shape of a lens and is provided with a pair of rotary wheels 8 provided with mass having large inertia force in addition to a cockpit, a cabin, a landing gear, a stabilizing rudder, a reactor, etc., in itself. The wheels 8 are mounted on a vertical center shaft and have mass having large inertia force bringing a gyro effect which highly stabilizes the aircraft 1. The wheels 8 are rotated in completely reverse directions by the relative operation of the respective reactor 6 and a turbine connected to the wheels 8.
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Inventors:
Jose, Maria Ronsero Blasquez
Application Number:
JP1993000047781
Publication Date:
September 13, 1994
Filing Date:
March 09, 1993
Export Citation:
Assignee:
JOSE MARIA RONSERO BLASQUEZ
International Classes:
B64C17/06; B64C39/06; B64C17/00; B64C39/00; (IPC1-7): B64C17/06; B64C39/06