FLUID TURBINE WITH ROTOR UPWIND OF RINGED AIRFOIL
The present disclosure relates to a fluid turbine including a rotor and one or more ringed airfoil segments in fluid communication with a wake of the rotor. Each of the ringed airfoil segments includes a leading edge positioned co-planar with or downstream of the rotor plane as measured along the central axis. The ringed airfoil segments may include associated mixing elements. The fluid turbine may include a second ringed airfoil downstream of the one or more ringed airfoil segments.
1 . A fluid turbine system comprising:
a rotor configured to rotate about a central axis, the rotation of the rotor defining a rotor plane; and
one or more ringed airfoil segments disposed around the central axis in fluid communication with a wake of the rotor, each of the ringed airfoil segments including a leading edge co-planar with or downstream of the rotor plane as measured along the central axis.
2 . The fluid turbine system of claim 1 , wherein the one or more ringed airfoil segments form less than half a perimeter of a circle around the central axis.
3 . The fluid turbine system of claim 1 , wherein the one or more ringed airfoil segments form more than half a perimeter of a circle around the central axis.
4 . The fluid turbine system of claim 1 , wherein the one or more ringed airfoil segments fully encircle the central axis.
5 . The fluid turbine system of claim 1 , wherein the one or more ringed airfoil segments are configured to create a maximum in the unit mass flow rate downstream of the rotor plane.
6 . The fluid turbine system of claim 1 , wherein at least some of the one or more ringed airfoil segments include at least one mixing element.
7 . The fluid turbine system of claim 6 , wherein the at least one mixing element includes a mixing lobe.
8 . The fluid turbine system of claim 6 , wherein the at least one mixing element includes a mixing slot.
9 . The fluid turbine system of claim 1 , wherein the fluid turbine further includes a second ringed airfoil downstream of said one or more ringed airfoil segments.
10 . The fluid turbine system of claim 1 , wherein the rotor and each of the one or more ringed airfoil segments are configured to draw blade tip vortices from rotation of the rotor past a surface of the ringed airfoil segment facing toward the central axis.
11 . The fluid turbine system of claim 1 , wherein the rotor and each of the one or more ringed airfoil segments are configured to draw a secondary flow that bypassed the rotor past a surface of the ringed airfoil segment facing toward the central axis.
12 . A fluid turbine system comprising:
a rotor configured to rotate about a central axis, the rotation of the rotor defining a rotor plane; and
one or more ringed airfoil segments disposed around the central axis and configured to create a maximum in the unit mass flow rate at a location downstream of the rotor plane, each of the one or more ringed airfoil segments configured to draw a flow that bypassed the rotor along a surface of the ringed airfoil segment facing toward the central axis.
13 . The fluid turbine system of claim 12 , wherein the rotor and each of the one or more ringed airfoil segments are configured to draw blade tip vortices from rotation of the rotor past the surface of the ringed airfoil segment facing toward the central axis.
14 . The fluid turbine system of claim 12 , wherein the one or more ringed airfoil segments form less than half a perimeter of a circle around the central axis.
15 . The fluid turbine system of claim 12 , wherein the one or more ringed airfoil segments form more than half a perimeter of a circle around the central axis.
16 . The fluid turbine system of claim 12 , wherein the one or more ringed airfoil segments fully encircle the central axis.
17 . The fluid turbine system of claim 12 , wherein at least some of the one or more ringed airfoil segments include at least one mixing element.
18 . The fluid turbine system of claim 17 , wherein the at least one mixing element includes a mixing lobe.
19 . The fluid turbine system of claim 17 , wherein the at least one mixing element includes a mixing slot.
20 . The fluid turbine system of claim 12 , wherein the fluid turbine further includes a second ringed airfoil downstream of said one or more ringed airfoil segments.
21 . The fluid turbine system of claim 12 , wherein, for each ringed airfoil segment, a radius of the rotor plane is less than or equal to a distance from the central axis to an outer surface of the ringed airfoil segment.