| 摘要 |
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.
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