| CPC B64D 41/007 (2013.01) [G06F 30/15 (2020.01); G06F 30/28 (2020.01); B64F 5/00 (2013.01); F03D 1/0633 (2013.01); F03D 9/322 (2023.08); F05D 2220/76 (2013.01); F05D 2260/81 (2013.01)] | 27 Claims |

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1. A turbine comprising a plurality of blades with a predetermined airfoil profile and extending from a proximal blade root to a distal blade tip, said blades being mounted to a turbine shaft and arranged around a turbine axis for rotating said turbine shaft in the presence of a fluid flow introduced to a turbine inlet, wherein said blades are configured according to a set of turbine parameters related to the blade geometry, the turbine geometry, and the rate of rotation, for providing a specified weighted combination of a propulsive force in the direction of the turbine axis to an amount of power generated by said turbine when vortical fluid flow is introduced to the turbine inlet.
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