Round honeycomb rotor

F - Mech Eng,Light,Heat,Weapons – 04 – D

Patent

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Details

F04D 29/18 (2006.01) B64C 11/00 (2006.01) F01D 5/03 (2006.01) F03B 3/12 (2006.01) F03D 1/06 (2006.01) F03D 3/06 (2006.01) F04D 29/26 (2006.01)

Patent

CA 2536093

The invention relates to a round honeycomb rotor which is intended to improve substantially the efficiency of standard propellers when used as a rotor for aerial vehicles, motor pumps, boats or for any purpose in hydraulic or pneumatic applications. The inventive rotor comprises helical parts which extend from the hub or circular core thereof and which are mounted to one or more concentric tubular cylinders. Moreover, a truncated-cone-shaped part extends from the larger diameter cylinder in order to control and direct the output centrifugal forces. The aforementioned helical parts take the form of helical trapezoids which, when connected to one another, form a round honeycomb in which the outer peripheral edges of said parts are fully enclosed, such that all of the centrifugal forces can be combined and the efficiency of standard propellers can be increased ten times or more for all of the various applications thereof.

L'invention concerne un rotor à structure en nid d'abeille circulaire permettant d'augmenter sensiblement le rendement des hélices conventionnelles, pouvant être utilisé comme rotor dans des aéronefs, des motopompes, des embarcations, ainsi que dans des applications hydrauliques ou pneumatiques. Ce rotor comprend des pièces hélicoïdales qui s'étendent à partir d'un moyeu ou d'un noyau circulaire et qui sont montées sur un ou plusieurs cylindres tubulaires et concentriques, ainsi qu'une pièce conique montée sur le cylindre de diamètre supérieur de façon à prolonger ce dernier, permettant de contrôler et de diriger les forces centrifuges en sortie. Ces pièces hélicoïdales ont la forme de trapèzes hélicoïdaux qui, lorsqu'ils sont disposés les uns sur les autres, forment une structure en nid d'abeille circulaire, fermant totalement les bords extérieures, ce qui permet d'unir toutes les forces centrifuges et d'augmenter par dix ou davantage le rendement des hélices classiques, quelle que soit l'application.

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