Fluid turbine rotor blade

A vertical axis fluid turbine comprising:

• a rotor assembly having at least two rotor blades, each rotor blade in said rotor assembly comprising:
• a segment of a spherical surface residing on a datum sphere, having a first end proximal to the top of the rotor blade, and a second end proximal to the bottom of the rotor blade;
• and a curved surface extending between said first end and said second end, having a concave side and a convex side, a vertical edge;
• and a vertical central axis parallel to the vertical edge, extending through a center of said datum sphere, and through the center of said rotor assembly;
• and an empty space extending between said first end and said second end and proximal to said vertical central axis and proximal to said vertical edge of said curved surface;
• and an array of holes in said segment of the spherical surface second end, proximal to the bottom of the rotor blade;
• wherein fluid flowing over one of said at least two rotor blades exerts a force on said curved surface concave side, flows without obstruction through said empty space between said first end and said second end and proximal to said vertical central axis and then flows over, and exerts a force on, a second of said at least two rotor blades curved surface concave side, as the fluid exits the rotor assembly;
• while updraft fluid flow passes through said array of holes, causing a vortex that in turn exerts a force on said curved surface concave side of each of said at least two rotor blades, wherein:
• each rotor blade in said rotor assembly further comprises:
• a deflector surface offset from, and joined to, said segment of the spherical surface second end, and proximal to said array of holes;
• wherein fluid moves through said array of holes, is deflected by said deflector surface, resulting in a relatively higher pressure proximal to the holes and a relatively lower pressure in the area of the blade above said deflector surface, drawing fluid flow from said relatively higher pressure to said relatively lower pressure forming a vortex which results in a force on said concave side of said curved surface of each said rotor blade in said rotor assembly.