Structure with rigid projections adapted to traverse a fluid environment

1. A structure adapted to traverse a fluid environment, the structure comprising:

an elongate body having a root, a wingtip, a leading edge and a trailing edge; and

a plurality of rigid projections each extending from a respective position along the trailing edge generally along the same plane as a front surface of the body wherein the projections include a first and a second set of projections extending from the trailing edge, each projection of the plurality of projections having a length, and

wherein the projections of the first set and the second set of projections are discrete projections that alternate with one another extending along the trailing edge;

wherein the lengths of adjacent projections extending from the trailing edge differ from one another; and

wherein the lengths of adjacent projections of the first set and the second set differ from one another at half a wavelength distance of a target sound frequency.

2. The structure of claim 1 , where in the rigid projections extend towards the wingtip.

3. The structure of claim 2 , wherein the rigid projections and the elongate body are connected to each other.

4. The structure of claim 1 , wherein the projections extend from a portion of the leading edge that is less than the entire span of the leading edge.

5. The structure of claim 4 , wherein the rigid projections extend from the leading edge from between about 40% and 96% of the elongate body, where the root of the rotor blade represents 0% and the wingtip represents 100%.

6. The structure of claim 1 , wherein the projections of the first set and the projections of the second set interacting with incident air flow on the trailing edge to cause destructive interference of sound waves generated from the leading edge interacting with the incident air flow.

7. The structure of claim 1 , wherein the structure is a rotor blade.

8. A turbine comprising at least one rotor blade as recited in claim 7 .

9. The rotor blade of claim 1 , wherein a different configuration of projections on the trailing edge is applied as opposed to the leading edge.

10. The rotor blade of claim 9 , wherein the leading edge has projections of larger surface area as compared to the trailing edge.

11. A rotor blade, wherein the rotor blade defines an aerodynamic body having a pressure side, suction side, leading edge, trailing edge and blade tip, the blade body further comprising:

a plurality of projections extending from the aerodynamic body in the vicinity of the trailing edge applied in the range of 40-96% of the rotor blade, where the root of the rotor blade represents 0% and the blade tip represents 100% the projections having an alternating length and width and being non-uniform in dispersement;

a generally decreasing length and width respective to these projections moving towards the blade tip;

a flexible or rigid and/or curvilinear or linear architecture;

a composition of biologically or non-biologically based materials;

wherein the length of each of the plurality of projections is approximately parallel to a local flow streamline defined for that projection;

wherein the rigid projections that may be curvilinear are in the line of the arc of local flow streamline defined for that projection; and

where it may be made of a material with a coefficient of linear thermal expansion (CLTE) between 1.0×10 −4 m/m ° C. and 7.0×10 4 m/m ° C.;

wherein the projections of the first set and the second set of projections are discrete projections that alternate with one another extending along the trailing edge and the corresponding length of each projection of the projections is inversely correlated with a distance from the root;

wherein the lengths of adjacent projections extending from the trailing edge differ from one another; and

wherein the lengths of adjacent projections of the first set and the second set differ from one another at half a wavelength distance of a target sound frequency, the projections of the first set and the projections of the second set interacting with incident air flow on the trailing edge to cause destructive interference of sound waves generated from the leading edge interacting with the incident air flow.

12. The rotor blade of claim 11 , wherein the projections are applied in the region of the trailing edge only.

13. The rotor blade of claim 11 , wherein the projections are applied in the region of the leading edge only.

14. The rotor blade of claim 11 , wherein the projection has a configuration selected from the group consisting of: a serration, brush, comb, riblet, fluting, fimbriae.

15. A wind turbine comprising a rotor blade as recited in claim 11 .

16. A method for increasing the efficiency and/or decreasing the noise emissions of an operating wind turbine comprising a hub and rotor blade(s), wherein at least one rotor blade is connected to the hub and is defined by an aerodynamic body having a pressure side, suction side, leading edge, trailing edge and blade tip, the method comprising:

mounting a plurality of projections on the aerodynamic body that extend in the vicinity of the trailing edge, the applied projections in the range of 40-96% of the rotor blade, where the root of the rotor blade represents 0% and the blade tip represents 100%;

alternating the length and width respective to these projections;

wherein the length of the longer projection is longer than an adjacent projection by ½ the wavelength of the sound wave at a given temperature;

wherein the projections, as the projections travel through a fluid, create a sound wave of a certain wavelength that corresponds with a neighboring sound wave emitted by a component of the rotor blade that elicits destructive interference of the neighboring sound waves.

17. The method of claim 16 , wherein the projections are made from a fibrous material that is embedded within a matrix.