Fluid turbine semi-shroud and associated rotor blade dual-winglet design

1. A rotor blade for a fluid turbine in combination with a semi-annular airfoil comprising:

a rotor blade for a fluid turbine comprising:

an upwind direction; and

a downwind direction; and

a root region; and

a tip region; and

a long axis extending from said root region to said tip region; and

a body extending along said long axis, from said root region to said tip region; and

said body further comprising an airfoil cross section, said airfoil cross section comprising:

a leading edge; and

a trailing edge; and

a lift surface; and

a pressure surface; and

said tip region comprising a first winglet and a second winglet; and

said first winglet extending arcuately away from said lift surface in said downwind direction; and

said leading edge transitioning along said first winglet toward said trailing edge; and

said second winglet extending arcuately away from said pressure surface in said upwind direction; and

said leading edge transitioning along said second winglet toward said trailing edge; said rotor blade rotationally engaged with said fluid turbine wherein said fluid turbine has a central axis about which at least one said rotor blade rotates about thus providing a rotor swept area; and

said rotor swept area in fluid communication with a semi-annular airfoil comprising:

an airfoil cross section; having

an upwind direction; and

a downwind direction; and

a lift surface facing upward; and

a pressure surface facing downward; and

said semi-annular airfoil in fluid communication with said at least one rotor blade, proximal to the perimeter of said rotor swept area located at the lower region of said rotor swept area; wherein

the rotor swept area is in fluid communication with the lift surface of said semi-annular airfoil in the lower region of the rotor swept area.

2. The rotor blade of claim 1 wherein said pressure surface winglet turns arcuately from said pressure surface at an angle between 15° and 35°.

3. The rotor blade of claim 1 wherein said lift surface winglet turns arcuately from said lift surface at an angle between 70° and 120°.

4. The rotor blade of claim 1 wherein:

said first winglet is at least twice as long as said second winglet.

5. A rotor blade for a fluid turbine in combination with a semi-annular airfoil comprising:

a rotor blade for a fluid turbine comprising:

an upwind direction; and

a downwind direction; and

a root region; and

a tip region; and

a long axis extending from said root region to said tip region; and

a body extending from said root region to said tip region; and

said body further comprising airfoil cross sections, said airfoil cross sections each comprising:

a leading edge; and

a trailing edge; and

a lift surface; and

a pressure surface; and

said tip region comprising an arcuate winglet having a airfoil cross sections arrayed along an arcuate centerline; and

said arc being tangent to an imaginary plane that is perpendicular to the end point of said long axis; and

said rotor blade rotationally engaged with said fluid turbine wherein said fluid turbine has a central axis about which at least one said rotor blade rotates about thus providing a rotor swept area; and

said winglet in fluid communication with a semi-annular airfoil comprising:

an airfoil cross section; having

an upwind direction; and

a downwind direction; and

a lift surface facing upward; and

a pressure surface facing downward; and

said semi-annular airfoil in fluid communication with said at least one rotor blade, proximal to the perimeter of said rotor swept area located at the lower region of said rotor swept area; and

the rotor swept area is in fluid communication with the lift surface of said semi-annular airfoil in the lower region of the rotor swept area; wherein

said arcuate centerline is parallel to the lift surface of said semi-annular airfoil.

6. The rotor blade for a fluid turbine in combination with a semi-annular airfoil of claim 5 further comprising:

a region of relatively increased fluid velocity stream over said semi-annular airfoil; and

said winglet rotating through said region of relatively increased fluid velocity stream; wherein said winglet surface area providing contact with said increased fluid velocity stream.

7. A rotor blade for a fluid turbine in combination with a semi-annular airfoil comprising:

a rotor blade for a fluid turbine comprising:

an upwind direction; and

a downwind direction; and

a root region; and

a tip region; and

a long axis extending from said root region to said tip region; and

a body extending from said root region to said tip region; and

said body further comprising airfoil cross sections, said airfoil cross sections each comprising:

a leading edge; and

a trailing edge; and

a lift surface; and

a pressure surface; and

said tip region comprising an arcuate winglet having a airfoil cross sections arrayed along an arcuate centerline; and

said arc being tangent to an imaginary plane that is perpendicular to the end point of said long axis; and

said rotor blade rotationally engaged with said fluid turbine wherein said fluid turbine has a central axis about which at least one said rotor blade rotates about, thus providing a rotor swept area; and

said winglet in fluid communication with a semi-annular airfoil comprising:

an airfoil cross section; having

an upwind direction; and

a downwind direction; and

a lift surface facing upward; and

a pressure surface facing downward; and

said semi-annular airfoil in fluid communication with said at least one rotor blade, proximal to the perimeter of said rotor swept area and having a tip clearance that is the distance from the tip region of the rotor blade to the surface of the semi-annular airfoil; and

the tip clearance at the center of the semi-annular airfoil being smaller than the tip clearance at the ends of the semi-annular airfoil.

8. A rotor blade for a fluid turbine in combination with a semi-annular airfoil comprising:

a rotor blade for a fluid turbine comprising:

an upwind direction; and

a downwind direction; and

a root region; and

a tip region; and

a long axis extending from said root region to said tip region; and

a body extending from said root region to said tip region along said long axis; and

said body further comprising airfoil cross sections, said airfoil cross sections each comprising:

a leading edge; and

a trailing edge; and

a lift surface; and

a pressure surface; and

said tip region comprising a first winglet having an airfoil cross section that transitions arcuately away from said pressure surface toward said trailing edge; and

said first winglet transitioning arcuately to an angle that is between 75° and 85° with respect to said long axis; and

said tip region further comprising a second winglet having an airfoil cross section that transitions arcuately away from said lift surface toward said trailing edge: and

said second winglet transitioning arcuately to an angle that is between 80° and 120° with respect to said long axis; and

said rotor blade rotationally engaged with said fluid turbine wherein said fluid turbine has a central axis about which at least one said rotor blade rotates about, thus providing a rotor swept area; and

said dual winglet in fluid communication with a semi-annular airfoil comprising:

an airfoil cross section; having

an upwind direction; and

a downwind direction; and

a lift surface facing upward; and

a pressure surface facing downward; and

said semi-annular airfoil in fluid communication with said at least one rotor blade, proximal to the dual winglet; wherein the dual winglet passes through a region above the lift surface of the semi-annular airfoil resulting in an increase in the rotor tip-speed ratio that is between 15% and 25% over that of the same rotor without interaction with said semi-annular airfoil.