Fluid energy converting method and apparatus

• US 4,184,805 A
• Filed: 03/09/1978
• Issued: 01/22/1980
• Est. Priority Date: 03/09/1978
• Status: Expired due to Term

• Current Assignee: Lee Arnold
• Original Assignee: Lee Arnold
• Inventors: Arnold, Lee
• Primary Examiner(s): Powell, Jr., Everette A.
• Application Number:
  US05/884,816
• Time in Patent Office: 684 Days
• Field of Search: 416/64-68
• US Class Current: 416/1
• CPC Class Codes: F03D 5/06 the wind-engaging parts swinging to-and-fro and not rotating
• CPC Class Codes: F05B 2210/16 Air or water being indistinctly used as working fluid, i.e. the machine can work equally with air or water without any modification
• CPC Class Codes: F05B 2240/124 Cascades, i.e. assemblies of similar profiles acting in parallel
• CPC Class Codes: Y02E 10/70 Wind energy

Abstract

There is disclosed a method and apparatus for converting the kinetic energy of a moving fluid stream into useful work by means of a cascade of thin airfoils positioned therein. In one embodiment, the airfoils are provided with at least two degrees of freedom and adjacent airfoils are movable out of phase. The airfoils are subjected to the aerodynamically induced oscillations caused by the aeroelastic phenomenon known as flutter and the oscillatory movement is then harnessed to do useful work. In an alternate embodiment, a cascade of airfoils is mechanically oscillated within a moving fluid stream to increase the propulsion of the fluid. Where the fluid is a liquid, the cascade includes a plurality of hydrofoils.

Claims

1. A method for converting the kinetic energy of a fluid stream into useful work comprising the steps of positioning a device including a pair of parallel plates and a thin airfoil equally spaced from each plate and having at least two degrees of freedom within a moving fluid stream with the plates parallel to the free stream and the airfoil at zero angle of attack when undisturbed to define an aerodynamic system, adjusting the system until the velocity of the fluid is sufficient to induce flutter oscillations, disturbing the airfoil, and then utilizing the resultant oscillations to produce useful work.

2. A method according to claim 1, wherein the oscillations of the airfoil are used to produce alternating current.

3. A method according to claim 1, wherein the oscillations of the airfoil are utilized to operate a pump.

4. A method according to claim 3, wherein the pump includes a cascade of airfoils in another fluid stream and wherein the oscillations of the airfoil are utilized to oscillate the second cascade.

5. A method according to claim 1, wherein the device includes a plurality of airfoils each having two degrees of freedom and arranged in a cascade and additional flat plates, wherein the airfoils are equally spaced from each other and from adjacent flat plates when the system is undisturbed.

6. A method according to claim 5, wherein the airfoils are interconnected to oscillate in phase.

7. A method according to claim 1, wherein the device includes means for adjusting the parameters associated with the device, and wherein said adjusting step includes operating said adjusting means.

8. A method according to claim 7, further including the step of controlling the operation of said adjusting means in response to variations in fluid velocity to maintain the system at critical velocity.

9. A method according to claim 1 further including the step of applying mechanical oscillations to the airfoils to maintain and enhance the flutter oscillations.

10. A method according to claim 1, wherein the resultant oscillations are utilized to oscillate another airfoil positioned in a bounded fluid stream in a direction having a component substantially perpendicular to the direction of fluid flow.

11. A method according to claim 10, wherein said airfoil is oscillated in plunge.

12. A method according to claim 11, wherein said airfoil is also oscillated in pitch.

13. A method according to claim 10, wherein a cascade of airfoils is positioned in the bounded fluid stream and adjacent airfoils are oscillated substantially 180°

out of phase.

14. Apparatus for converting the kinetic energy of a fluid stream into useful work comprising a support structure open at opposite ends to permit fluid flow therethrough and including a plurality of equally spaced flat plates extending parallel to the direction of fluid flow, a plurality of airfoils, means for mounting said airfoils within said support structure in a cascade with each airfoil having at least two degrees of freedom and being equally spaced between adjacent flat plates at zero angle of attack when undisturbed, means interconnecting said airfoils to oscillate in phase, and means operatively associated with said airfoils to utilize the oscillatory movement thereof to produce useful work.

15. Apparatus according to claim 14, further including means for adjusting the conditions under which said airfoils will begin to oscillate.

16. Apparatus according to claim 15, wherein said adjusting means includes at least one movable mass mounted on said mounting means.

17. Apparatus according to claim 14, further including a control means for maintaining the oscillatory movement when the velocity of the fluid stream varies, said control means including a detector and feedback means for controlling said adjusting means in response to a detection signal.

18. Apparatus according to claim 17, wherein said detector includes means for detecting the amplitude of the airfoil oscillations.

19. Apparatus according to claim 17, wherein said detector includes an anemometer.

20. Apparatus according to claim 14, further including mechanical oscillating means to maintain and enhance the flutter oscillations.

21. Apparatus according to claim 14, wherein said airfoils have zero camber.

22. Apparatus according to claim 14, wherein said airfoils have a high aspect ratio and are rectangular in plan form.

23. Apparatus according to claim 14, further including means to disturb at least one of said airfoils.

24. Apparatus according to claim 14, further including a vane on said support structure and wherein said support structure is pivotally mounted upon a support within a fluid stream.

25. Apparatus according to claim 14 wherein said mounting means includes means enabling adjacent airfoils to oscillate freely in both pitch and plunge.

26. Apparatus according to claim 14, wherein each airfoil includes a pivotally mounted flap adjacent to its trailing edge.

27. Apparatus according to claim 26, wherein said mounting means includes means enabling adjacent airfoils to oscillate freely in plunge.

28. Apparatus according to claim 26, wherein said mounting means includes means enabling adjacent airfoils to oscillate freely in pitch.

29. Apparatus according to claim 14, wherein said utilizing means is an alternating current producing means.

30. Apparatus according to claim 14 wherein said utilizing means is a pump.

31. Apparatus according to claim 30, wherein said pump includes at least one airfoil positioned in another fluid stream which is movable in a direction having a component substantially perpendicular to the direction of fluid flow.

32. Apparatus according to claim 31, wherein said pump includes a cascade of airfoils.

33. Apparatus according to claim 32, wherein adjacent airfoils of said cascade are movable substantially 180°

out of phase.