Aeronautics and astronautics – Aircraft – heavier-than-air – Helicopter or auto-rotating wing sustained – i.e. – gyroplanes
Reexamination Certificate
2006-08-15
2006-08-15
Dinh, Tien (Department: 3644)
Aeronautics and astronautics
Aircraft, heavier-than-air
Helicopter or auto-rotating wing sustained, i.e., gyroplanes
Reexamination Certificate
active
07090164
ABSTRACT:
A method of producing a lifting force and a horizontal force by aerodynamic surfaces includes the steps of moving aerodynamic surfaces along a circumference and providing their oscillations; rotating each of the aerodynamic surfaces synchronously with the movement along the circumference, in a direction which is opposite to it, relative to an axis of rotation which is parallel to an axis of the movement along the circumference, with an angular speed which is equal to an angular speed of the movement along the circumference, and performing oscillations of each of the aerodynamic surfaces synchronously with a rotation relative to mutually perpendicular axes located correspondingly in two mutually perpendicular planes which intersect along an axis of rotation of the aerodynamic surfaces, wherein one of them passes through an axis of the movement along the circumference and the axis of rotation.
REFERENCES:
patent: 1922167 (1933-08-01), Leray
patent: 2589826 (1952-03-01), Larsen
patent: 3181816 (1965-05-01), Pfleiderer
patent: 3185410 (1965-05-01), Smart
patent: 3246861 (1966-04-01), Curci
patent: 3360219 (1967-12-01), Wigal
patent: 3762669 (1973-10-01), Curci
Akaro Andrey Igorevich
Denisov Anatoly Alekseevich
Medvedev Mikhail Mikhailovich
Zelinsky Anatoly Mikhailovich
LandOfFree
Method for producing a lift and a horizontal thrust does not yet have a rating. At this time, there are no reviews or comments for this patent.
If you have personal experience with Method for producing a lift and a horizontal thrust, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Method for producing a lift and a horizontal thrust will most certainly appreciate the feedback.
Profile ID: LFUS-PAI-O-3626295