Title:
CIRCULAR WING FOR VERTICAL FLIGHT
Document Type and Number:
WIPO Patent Application WO/2015/096842
Kind Code:
A3
Abstract:
According to the invention, the assembly of the half-sphere airplane wing made it possible to create another form of flight (vertical flight), controlling air flow only on the top surface of the circular wing, said assembly being a perfect re-adhesion and tangential to the smooth surface of the top circular wing surface. While the air speed on the bottom surface of the circular wing is equal to zero, the air flow will make it possible to create vertical thrust below the circular wing which will increase in proportion with air speed. Said technique, which has a wide range of industrial uses and will put an end to critical problems, can be cited as follows: 1) on motor vehicles and for monitoring roads; 2) in military service; air transport; and 3) in space; transporting satellites.
Inventors:
GUERFI MOHAMED (DZ)
Application Number:
PCT/DZ2014/000005
Publication Date:
April 07, 2016
Filing Date:
December 24, 2014
Export Citation:
Assignee:
GUERFI MOHAMED (DZ)
International Classes:
B64C11/18; B64C21/04; B64D27/02
Foreign References:
| US20090173834A1 | 2009-07-09 | |||
| US20120234968A1 | 2012-09-20 | |||
| DE3339866A1 | 1985-05-15 |
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