Aerodynamic structure having a ridged solar panel and an associated method
Air vehicles and associated aerodynamic structures are provided which include ridged solar panels to both reduce the drag and increase the solar energy harvested by the solar panel. The air vehicle may include an airframe and a solar panel carried by the airframe and defining an exterior surface thereof. The solar panel may include a plurality of ridged structures extending in a lengthwise direction. The ridged structures may be arranged such that a majority of the airflow over the exterior surface flows in the lengthwise direction. The plurality of ridged structures may include a plurality of lengthwise extending projections spaced about by respective valleys.
1. An air vehicle comprising:
a solar energy harvesting airframe comprising an airfoil and having an exterior surface; and
a solar panel carried by the airframe and defining at least a portion of the exterior surface thereof, wherein the solar panel comprises a plurality of ridged structures having energy absorbing faces extending in a streamwise direction, wherein the ridged structures are arranged such that a majority of air flow over the exterior surface flows in the streamwise direction, wherein the ridged structures are configured such that a respective light ray sequentially impinges upon a plurality of the energy absorbing faces of the ridged structures so as to permit additional solar energy to be captured, and wherein the ridged structures are configured such that the respective light ray initially impinges upon one energy absorbing face and is then reflected to another energy absorbing face.
2. An air vehicle according to claim 1 wherein the ridged structures are arranged such that the streamwise direction is parallel to a predefined air flow direction.
3. An air vehicle according to claim 1 wherein the plurality of ridged structures comprise a plurality of lengthwise extending projections spaced apart by respective valleys.
4. An air vehicle according to claim 3 wherein the plurality of ridged structures are identical.
5. An air vehicle according to claim 1 wherein the airfoil comprises a wing, and wherein the solar panel defines the exterior surface of an upper portion of the wing proximate a trailing edge of the wing.
6. An air vehicle according to claim 1 wherein the airfoil comprises a tail, and wherein the solar panel defines the exterior surface of an upper portion of the tail proximate a trailing edge of the tail.
7. An air vehicle according to claim 1 wherein the airframe comprises a fuselage, and wherein the solar panel defines the exterior surface of an upper portion of the fuselage.
8. An aerodynamic structure comprising:
an aerodynamic surface comprising an airfoil having an exterior surface and configured to support air flow in a predefined air flow direction; and
solar panel defining a portion of the exterior surface of the aerodynamic surface, said solar panel comprising a plurality of ridged structures having energy absorbing faces extending in the predefined air flow direction, wherein the ridged structures are configured such that a respective light ray sequentially impinges upon a plurality of the energy absorbing faces of the ridged structures so as to permit additional solar energy to be captured, and wherein the ridged structures are configured such that the respective light ray initially impinges upon one energy absorbing face and is then reflected to another energy absorbing face.
9. An aerodynamic structure according to claim 8 wherein the plurality of ridged structures comprise a plurality of streamwise extending projections spaced apart by respective valleys.
10. An aerodynamic structure according to claim 9 wherein the plurality of ridged structures are identical.
11. An aerodynamic structure according to claim 9 wherein the airfoil comprises a wing, and wherein the solar panel defines the exterior surface of an upper portion of the wing proximate a trailing edge of the wing.
12. An aerodynamic structure according to claim 9 wherein the airfoil comprises a tail, and wherein the solar panel defines the exterior surface of an upper portion of the tail proximate a trailing edge of the tail.
13. An aerodynamic structure according to claim 8 wherein the aerodynamic structure comprises a fuselage, and wherein the solar panel defines the exterior surface of an upper portion of the fuselage.
14. A method comprising:
providing a solar panel carried by an airframe and defining an exterior surface thereof, wherein providing the solar panel comprises providing a solar panel having a plurality of ridged structures having energy absorbing faces extending in a streamwise direction and arranged such that a majority of air flow over the exterior surface flows in the streamwise direction;
receiving solar energy with the solar panel; and
converting at least some of the solar energy to electrical energy,
wherein providing a solar panel comprise providing a solar panel that is configured such that a respective light ray sequentially impinges upon a plurality of the energy absorbing faces of the ridged structures so as to permit additional solar energy to be captured, wherein providing the solar panel comprises providing the solar panel that is configured such that that the respective light ray initially impinges upon one energy absorbing face and is then reflected to another energy absorbing face.
15. A method according to claim 14 wherein providing the solar panel comprises providing the solar panel having ridged structures arranged such that the streamwise direction is parallel to a predefined air flow direction.
16. A method according to claim 14 wherein providing the solar panel comprises providing the solar panel with the plurality of ridged structures comprising a plurality of streamwise extending projections spaced apart by respective valleys.
17. A method according to claim 16 wherein providing the solar panel further comprises providing the solar panel with a plurality of identical ridged structures.
18. A method according to claim 14 wherein the airfoil comprises a wing, and wherein providing the solar panel comprises providing the solar panel so as to define the exterior surface of an upper portion of the wing proximate a trailing edge of the wing.
19. A method according to claim 14 wherein the airfoil comprises a tail, and wherein providing the solar panel comprises providing the solar panel so as to define the exterior surface of an upper portion of the tail proximate a trailing edge of the tail.
20. A method according to claim 14 wherein the airframe comprises a fuselage, and wherein providing the solar panel comprises providing the solar panel so as to define the exterior surface of an upper portion of the fuselage.
21. An air vehicle according to claim 1 wherein the solar panel is disposed within the airfoil such that a peak of the ridged structures is no higher than a remainder of the airfoil.
22. An aerodynamic structure according to claim 8 wherein the solar panel is disposed within the aerodynamic surface such that a peak of the ridged structures is no higher than a remainder of the aerodynamic surface.
23. A method according to claim 14 wherein the solar panel is disposed within the airfoil such that a peak of the ridged structures is no higher than a remainder of the airfoil.
24. An air vehicle according to claim 1 wherein the solar panel including the plurality of ridged structures defines up to 50% of the exterior surface of the airfoil.
25. An aerodynamic structure according to claim 8 wherein the solar panel including the plurality of ridged structures defines up to 50% of the exterior surface of the airfoil.
26. A method according to claim 14 wherein the solar panel including the plurality of ridged structures defines up to 50% of the exterior surface of the airfoil.