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An apparatus energized by a flowing fluid includes at least one turbine blade having a trailing edge angle and an elastic deformation member connected to the at least one turbine blade. The deformation of the elastic deformation member changes an orientation of a trailing edge angle of the at least

An apparatus energized by a flowing fluid includes at least one turbine blade having a trailing edge angle and an elastic deformation member connected to the at least one turbine blade. The deformation of the elastic deformation member changes an orientation of a trailing edge angle of the at least one turbine blade.

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1. An apparatus energized by a flowing fluid, comprising: at least one turbine blade having leading edge and a trailing edge angle, the at least one turbine blade rotating around a first long axis; andan elastic deformation member connected to the at least one turbine blade, wherein a deformation of

1. An apparatus energized by a flowing fluid, comprising: at least one turbine blade having leading edge and a trailing edge angle, the at least one turbine blade rotating around a first long axis; andan elastic deformation member connected to the at least one turbine blade, wherein a deformation of the elastic deformation member rotates the leading edge in a direction opposite to a rotation of the trailing edge, the rotations being about the first long axis and changing an orientation of the trailing edge angle of the at least one turbine blade. 2. The apparatus of claim 1, wherein the at least one turbine blade deforms the elastic deformation member when the at least one turbine blade rotates about an axis that always intersects the at least one turbine blade as the at least one turbine blade rotates around the first long axis. 3. The apparatus of claim 2, wherein a center of gravity of the at least one turbine blade is axially spaced from a connection between the at least one turbine blade and the elastic deformation member, the center of gravity rotating the at least one turbine blade about the axis that always intersects the at least one turbine blade. 4. The apparatus of claim 1, wherein the at least one turbine blade comprises a plurality of turbine blades, and further comprising a ring to which the plurality of turbine blades are connected, wherein the elastic deformation member connects to the ring and the at least one turbine blade rotates about a connection with the elastic deformation member. 5. The apparatus of claim 1, wherein the elastic deformation member include a front elastic element and a back elastic element, each of which separately connects to the at least one turbine blade. 6. The apparatus of claim 5, wherein the at least one turbine blade has a leading edge, a trailing edge, and a center of gravity, wherein the front elastic element is positioned between the leading edge and the center of gravity, and wherein the back elastic element is position between the trailing edge and the center of gravity. 7. The apparatus of claim 6, wherein the at least one turbine blade comprises a plurality of turbine blades, and further comprising a ring to which the plurality of turbine blades are connected, and further comprising a hub, wherein the back elastic element connects at one end to the hub and connects at another end to the ring. 8. An apparatus of claim 7, further comprising an enclosure surrounding the hub and at least partially enclosing the front elastic element and the back elastic element. 9. A method for controlling a speed of a turbine drive assembly energized by a flowing fluid, comprising: reducing a rate at which a rotational speed of a plurality of turbine blades increases as a flow rate of the flowing fluid increases by reducing a tip speed ratio of the plurality of turbine blades, the tip speed ratio being the rotational speed divided by the flow rate of the flowing fluid, the reduction being done by connecting at least one elastic deformation member to the plurality of turbine blades associated with the turbine drive assembly, wherein a deformation of the at least one elastic deformation member changes an orientation of a trailing edge angle of the at least one turbine blade. 10. The method of claim 9, wherein each of turbine blade of the plurality of turbine blades has a leading edge and a trailing edge, wherein each turbine blade rotates about an axis that always intersects the associated turbine blade. 11. An apparatus energized by a flowing fluid, comprising: a hub;a plurality of turbine blades arrayed around the hub, each turbine blade having a leading edge, a trailing edge, a center of gravity, and a trailing edge angle;a front elastic element including plurality of spokes, each spoke connecting an associated turbine blade to the hub; anda back elastic element including a plurality spokes, each spoke connecting an associated turbine blade to the hub,wherein the front elastic element and the back elastic element deform when the hub rotates, and wherein the deformations rotate the leading edges in a direction opposite to a rotation of the trailing edges, the rotations being about a long axis of the hub and changing the orientation of the trailing edge angle of each the plurality of turbine blades. 12. The apparatus of claim 11, wherein each turbine blade has an axis that always intersects the associated turbine blade, wherein each turbine blade deforms an associated elastic deformation member when each turbine blade rotates about the axis that intersects that turbine blade. 13. The apparatus of claim 11, wherein a center of gravity of each turbine blade is axially spaced from a connection between each turbine blade and the front elastic element. 14. The apparatus of claim 11, wherein the at least one turbine blade rotates about a connection with the elastic deformation member. 15. The apparatus of claim 1, wherein the deformation is one of: (i) bending, (ii) twisting, and (iii) stretching, (iv) expanding, (v) shrinking, and (vi) contracting. 16. The apparatus of claim 1, wherein the elastic deformation member connects the at least one turbine blade to a hub, wherein a tip speed ratio is defined as an inclination of a line defining a relationship between a flow rate of a fluid flowing along the at least one turbine blade and a rotation speed of the hub, and wherein the elastic deformation member deforms to reduce the tip speed ratio of the at least one turbine blade as the flow rate increases. 17. The apparatus of claim 11, further comprising a ring to which the plurality of turbine blades connect, and wherein the back elastic element connects the ring to the hub.