Hydrofoils and airfoils

• US 5,540,406 A
• Filed: 07/26/1995
• Issued: 07/30/1996
• Est. Priority Date: 10/25/1993
• Status: Expired due to Fees

• Current Assignee: Anthony C. Occhipinti
• Original Assignee: Anthony C. Occhipinti
• Inventors: Occhipinti, Anthony C.
• Primary Examiner(s): Kashnikow, Andres
• Assistant Examiner(s): DINH, TIEN QUANG
• Application Number:
  US08/507,811
• Time in Patent Office: 370 Days
• Field of Search: 244/199, 244/200, 244/204, 244/198, 244/201, 244/130, 244/209, 416/225 R, 416/235 R, 416/236 R
• US Class Current: 244/200
• CPC Class Codes: B63B 1/248 Shape, hydrodynamic features, construction of the foil
• CPC Class Codes: B63B 1/36 using mechanical means
• CPC Class Codes: B63H 1/28 Other means for improving propeller efficiency
• CPC Class Codes: B64C 21/10 using other surface properties, e.g. roughness
• CPC Class Codes: Y02T 50/10 Drag reduction
• CPC Class Codes: Y02T 70/10 Measures concerning design or construction of watercraft hulls

Abstract

A low turbulence cambered surface foil, hydrofoil or airfoil, which contains indentations located on maximum camber across which a fluid can be flowed. The indentations create turbulence in the boundary layer downstream of the indentations, changing the characteristics of the flowing fluid to a turbulent boundary layer ahead of the normal point of separation of the fluid from the foil, this causing the fluid to cling close to the surface of the foil and postpone or delay trailing edge separation of the fluid stream from the foil. The noise level is reduced, the performance and efficiency of the foil is improved, or both the noise level is reduced and the performance and efficiency of the foil is improved.

Claims

1. In apparatus characterized as a foil having cambered surface extending from the leading edge to the trailing edge of said foil, between the cambered surface and a fluid of which relative movement can occur, the improvement which comprises

an area completely smooth, without indentations and devoid of projections located between the leading edge of the foil and the area of maximum camber, and

a plurality of surface indentations disposed in a row spanwise on maximum camber which is devoid of projections and, except for the presence of said indentations is smooth, and sufficient to produce a low level boundary level turbulence and cause the fluid stream to attach and cling to the cambered surface in the area of said low level turbulence to postpone trailing edge separation of the stream to reduce noise level and improve the performance and efficiency of the foil as contrasted with a foil otherwise similar except that it contains no indentations on maximum camber, or contains indentations or projections, or both, in the area between the leading edge of the foil and maximum camber.

2. The apparatus of claim 1 wherein the foil is a hydrofoil, and the fluid is water.

3. The apparatus of claim 1 wherein the foil is an airfoil, and the fluid is air.

4. The apparatus of claim 3 wherein the airfoil is a wing, propeller blade, rudder, or strut.

5. The apparatus of claim 3 wherein the airfoil is a propeller the blades of which are provided with a plurality of rows of indentations arrayed on maximum camber, the indentations extending from a location where the inner ends of the blades are joined via a hub to the outer terminal ends of the blades.

6. The apparatus of claim 1 wherein the centers of said indentations are no less than about 2 diameters apart.

7. The apparatus of claim 1 wherein the indentations on the cambered surface are of depth ranging from top to bottom from about 1/64 inch to about 3/32 inch.

8. The apparatus of claim 1 wherein the indentations are contained within a thin veneer which is affixed on the cambered surface.

9. The apparatus of claim 8 wherein the indentations are holes which extend through the veneer from one surface thereof to the other, and the veneer ranges in thickness from about 1/64 inch to about 3/32 inch.

10. The apparatus of claim 8 wherein the veneer is attached to the cambered surface by wrapping the veneer around the foil such that openings are positioned spanwise along the points of maximum camber of the surface by wrapping said veneer beginning and ending at the trailing edge of the foil.

11. The apparatus of claim 1 wherein both sides of the foil are cambered.

12. The apparatus of claim 1 wherein both sides of the foil are cambered, and the indentations are provided by application of a thin perforated veneer to the surfaces of the foil.

23. The apparatus of claim 1 wherein the surface indentations are of circular shape, and the diameter no greater than about 1/8 inch, with said indentations ranging in depth form about 1/64 inch to about 3/32 inch.

24. The apparatus of claim 8 wherein the veneer is one through which holes are extended from one surface thereof to the other to form surface indentations.

13. An airfoil having a cambered surface extending from the leading edge to the trailing edge of said airfoil designed to control the stability, direction, lift, thrust or propulsion capabilities of an aircraft moving in air of which said airfoil is a component, the improvement which comprises

an area completely smooth, without indentations and devoid of projections located between the leading edge of the foil and the area of maximum camber, and

a plurality of surface indentations disposed in a row spanwise on maximum camber which is devoid of projections and, except for the presence of said indentations is smooth, and sufficient to produce a low level boundary level turbulence and cause the stream of air to attach and cling to the cambered surface in the area of said low level turbulence to postpone trailing edge separation of the stream of air to reduce the noise level and improve the performance and efficiency of the airfoil as contrasted with a foil otherwise similar except that it contains no indentations on maximum camber, or contains indentations or projections, or both, in the area between the leading edge of the foil and maximum camber.

14. The apparatus of claim 13 wherein the airfoil is comprised of a propeller the blades of which are provided with a plurality of rows of indentations arrayed on substantially maximum camber, the indentations extending from a location where the inner ends of the blades are joined via a hub to the outer terminal ends of the blades.

15. The apparatus of claim 13 wherein the indentations are contained within a thin veneer which is affixed on the cambered surface.

16. The apparatus of claim 15 wherein the veneer has a thickness no greater than about 0.015 inch through which holes are extended from one surface thereof to the other to form said surface indentations.

17. The apparatus of claim 15 wherein the said veneer is attached to said cambered surface by wrapping said veneer around the said foil such that openings are positioned spanwise along the points of camber of said cambered surface by wrapping said veneer beginning and ending at the trailing edge of the said foil.

18. In a process for producing a foil having a cambered surface extending from the leading edge to the trailing edge of said foil, between the cambered surface and a fluid of which relative movement can occur, the improvement which comprises locating an area completely smooth, without indentations and devoid of projections between the leading edge of the foil and the area of maximum camber, and a plurality of surface indentations disposed in a row spanwise on maximum camber which is devoid of projections and, except for the presence of said indentations is smooth, and sufficient to produce a low level boundary level turbulence which causes the fluid stream to attach and cling to the cambered surface in the area of said low level turbulence to postpone trailing edge separation of the stream to reduce noise level and improve the performance and efficiency of the foil as contrasted with a foil otherwise similar except that it contains no indentations on maximum camber, or contains indentations or projections, or both, in the area between the leading edge of the foil and maximum camber.

19. The process of claim 18 wherein the foil is an airfoil characterized as a wing, propeller blade, rudder, or strut of an aircraft.

20. The process of claim 18 wherein the indentations are contained within a thin veneer which is affixed on the cambered surface.

21. The process of claim 20 wherein the veneer has a thickness ranging from about 1/64 inch to about 3/32 inch through which holes are extended from one surface thereof to the other to form said surface indentations.

22. The process of claim 20 wherein the said veneer is attached to said cambered surface by wrapping said veneer around the said foil such that openings are positioned spanwise along the points of camber of said cambered surface by wrapping said veneer beginning and ending at the trailing edge of the said foil.