Aerodynamic wing device and method of making same

• US 4,558,898 A
• Filed: 05/22/1984
• Issued: 12/17/1985
• Est. Priority Date: 05/22/1984
• Status: Expired due to Term

• Current Assignee: Dann T. Deaver
• Original Assignee: Dann T. Deaver
• Inventors: Deaver, Dann T.
• Primary Examiner(s): SONG, ROBERT
• Application Number:
  US06/613,054
• Time in Patent Office: 574 Days
• Field of Search: 296/1 S, 244/123, 416/233, D12/88
• US Class Current: 296/180.1
• CPC Class Codes: B62D 35/007 Rear spoilers B62D35/001 takes precedence
• CPC Class Codes: Y02T 10/82 Elements for improving aerodynamics
• CPC Class Codes: Y10T 29/49826 Assembling or joining

Abstract

A light-weight aerodynamic wing device is adapted for mounting on a vehicle in a generally horizontal orientation and in a generally vertically spaced-apart relationship with the vehicle. The wing device is preferably extruded from aluminum and includes generally horizontal upper and lower peripheral walls interconnected to enclose a hollow elongated body. The body can be horizontally and/or vertically swept after extrusion into desired swept configurations for particular vehicular installations. The wall thickness of one or both of the peripheral wall portions is greatest at the compressed portion of the elongated body in order to substantially prevent buckling during horizontal sweep forming. One or more vertical reinforcing members can also be included in the hollow elongated body and extend between the upper and lower peripheral walls. The wing device also preferably includes air-retaining end caps at opposite ends of the elongated body, with the end caps being adapted to be snapped into the open opposite ends of the hollow extruded body. Mounting means, preferably including one or more universally-adapted stanchion members, are also provided and are adapted to be laterally adjustable along the length of the elongated extruded body in order to accommodate a wide variety of vehicular installations.

Claims

1. An aerodynamic wing device adapted to be mounted horizontally on an automotive type vehicle, said aerodynamic wing device including a substantially hollow elongated body having generally horizontal upper and lower peripheral wall portions interconnected to enclose said body, said body being formed by bending into a predetermined horizontally swept configuration, said peripheral wall portions having a wall thickness that decreases from a generally compressed inner side portion of said body to a generally tensioned outer portion of said body, said wall thickness tapering from approximately 0.1 inch to approximately 0.06 inch, said wall thickness being greater at said generally compressed inner side portion of said horizontally swept body in order to substantially prevent buckling of said horizontal peripheral wall portions at said compressed inner side portion during bending to form said horizontally swept configuration, said swept configuration being in the range of a zero sweep to approximately a No. 15 sweep without buckling.

2. An aerodynamic wing device according to claim 1, wherein said hollow elongated body further includes a generally vertical reinforcing member extending between said upper and lower wall portions and attached thereto, said vertical reinforcing member being located proximate at said compressed inner side portion of said horizontally swept body.

3. An aerodynamic wing device according to claim 2, with said body being constructed of extruded aluminum and with buckling being prevented with said body having a width of approximately 6.5 inches and a height of approximately 0.84 inch and wherein said upper wall portion tapers in thickness for approximately 3.75 inches and said lower wall portion tapers in thickness for approximately 3.00 inches and with said vertical member being located approximately 1.3 inches from the edge of said compressed inner side portion.

4. An aerodynamic wing device adapted to be mounted horizontally on a land vehicle or the like, said aerodynamic wing device including a substantially hollow elongated body having generally horizontal upper and lower peripheral wall portions interconnected to enclose said body, said body being formed by bending into a predetermined horizontally swept configuration, said peripheral wall portions having wall thicknesses that decrease from a generally compressed inner side portion of said body to a generally tensioned outer side portion of said body, said wall thicknesses being greater at said generally compressed inner side portion of said horizontally swept body in order to substantially prevent buckling of said horizontal peripheral wall portions at said compressed inner side portion during bending to form said horizontal swept configuration.

5. An aerodynamic wing device according to claim 4, wherein said elongated body is also formed into a predetermined vertically swept configuration.

6. An aerodynamic wing device according to claim 4, wherein said hollow elongated body further includes at least one generally vertical reinforcing member extending between said upper and lower wall portions and attached thereto, said vertical reinforcing member being located generally at said compressed inner side portion of said horizontally swept body.

7. An aerodynamic wing device according to claim 6, wherein said body is horizontally swept toward a generally rearward direction, said vertical reinforcing member being located at a generally forward compressed inner side portion of said horizontally swept body.

8. An aerodynamic wing device according to claim 6, wherein the horizontal distance between said vertical reinforcing member and the innermost edge of said compressed inner side portion of said body is approximately 20 percent of the horizontal distance between said innermost edge and the outermost edge of said tapered outer side portion of said body.

9. An aerodynamic wing device according to claim 4, further including end caps at opposite ends of said body, said end caps having protuberances thereon and said opposite ends of said body being generally open for receiving said protuberances of the respective end caps therein.

10. An aerodynamic wing device according to claim 9, wherein said protuberances on said end caps have a cross-sectional shape complementary to that of said open ends and are adapted to be relatively tightly received therein.

11. An aerodynamic wing device according to claim 4, wherein said body further includes end members at opposite ends thereof, said end members having vertically extending portions thereon, said vertically extending portions tending to contain air flowing over said body between said opposite ends thereof.

12. An aerodynamic wing device according to claim 4, wherein said body includes an elongated opening on the lower side thereof, said opening communicating with an internal receptacle means formed along said horizontal lower peripheral wall portion for interlockingly receiving a partially enlarged fastener means therein, said internal receptable being generally continuously elongated for interlockingly receiving said fastener at various locations along the length of said body.

13. An aerodynamic wing device according to claim 4, further including at least one stanchion member for supporting said body on said vehicle in a generally vertically spaced relationship therewith, and means for securing said body and said stanchion member to said vehicle.

14. A generally horizontal aerodynamic wing device for a land vehicle or the like, said aerodynamic wing device including an extruded generally hollow elongated body having generally horizontal upper and lower wall portions interconnected to enclose the generally hollow extruded body, said extruded body being horizontally formed into a predetermined horizontally swept configuration, the vertical cross-sectional thickness of at least one of said horizontal wall portions being tapered from a relatively larger thickness at a generally compressed inner side portion of said horizontally swept extruded body to a relatively smaller thickness at a generally tensioned outer side portion, at least one generally vertical reinforcing member being integrally extruded between said upper and lower wall portions generally at said compressed inner side portion, and mounting means for mounting said horizontal aerodynamic wing device on said vehicle in a generally horizontal orientation and in a generally vertically spaced relationship therefrom.

15. An aerodynamic wing device according to claim 14, wherein said extruded elongated body is also vertically formed into a predetermined vertically swept configuration, said extruded elongated body being horizontally swept toward a generally rearward direction and vertically swept toward a generally upward direction.

16. An aerodynamic wing device according to claim 14, further including end caps at opposite ends of said extruded elongated body, and means for securing said end caps to said opposite ends of said body at any of a number of preselected angular relationships therewith.

17. An aerodynamic wing device according to claim 16, wherein said end caps have protuberances thereon, said opposite ends of said extruded elongated body being generally open for receiving said protuberances of the respective end caps therein in a relatively tight press-fit relationship therewith.

18. An aerodynamic wing device according to claim 14, wherein the horizontal distance between said vertical reinforcing member and the innermost edge of said compressed side portion of said body is in the range of approximately 15 percent to approximately 25 percent of the horizontal distance between said innermost edge of said compressed side portion and the outermost edge of said stretched side portion of said body.

19. An aerodynamic wing device according to claim 14, wherein the horizontal distance between said vertical reinforcing member and the innermost edge of said compressed side portion of said body is approximately 20 percent of the horizontal distance between said innermost edge of said compressed side portion and the outermost edge of said stretched side portion of said said body.

20. A method of making an aerodynamic wing device for a land vehicle or the like, said method comprising the steps of:

extruding an elongated generally hollow body member having a generally inverted airfoil wing shape, said body member including generally vertically spaced apart horizontal walls, with at least one of said walls being extruded with a tapered vertical wall thickness that decreases in a horizontal direction from a first side portion of said elongated body to a second opposite side portion thereof;

horizontally sweep-forming said elongated body into a predetermined horizontally swept configuration, said body being horizontally swept in a direction so that said first side portion of said body having said horizontal wall of a relatively greater thickness is generally compressed during said horizontal sweep-forming with said second opposite side portion of said body being generally tensioned during said horizontal sweep-forming said relatively greater thickness tending to resist buckling during said horizontal sweep-forming and said relatively lesser thickness facilitating tensioning during said horizontal sweep-forming.

21. A method according to claim 20, further including the step of simultaneously and integrally extruding a generally vertical reinforcing member extending between said upper and lower walls generally at said first side portion having the horizontal walls of said relatively greater thickness.

22. A method according to claim 21, wherein said vertical reinforcing member is integrally extruded at a location such that the horizontal distance between said vertical reinforcing member and the edge of said first outer side portion is approximately 20 percent of the distance between the edges of said first and second side portions.

23. A method according to claim 22, further comprising the steps of providing a stanchion member for mounting said body in a generally vertically spaced relationship from said vehicle, and removing a generally lower portion of said stanchion member to form a predetermined configuration adapted to match a predetermined contour of said vehicle.

24. A method according to claim 23, further comprising the steps of providing end caps and securing said end caps to opposite ends of said elongated body.

25. A method according to claim 20, further comprising the steps of simultaneously and integrally extruding an elongated opening and a channel-shaped receptacle in said lower horizontal wall, providing a partially-enlarged fastener and inserting and positioning said fastener at a predetermined location in said channel, said fastener being adapted for securing said body to said vehicle in a generally vertically spaced relationship therefrom.

26. A method according to claim 21, wherein said wall thickness of one of said walls tapers from approximately 0.1 inch to approximately 0.06 inch over a horizontal distance of approximately 3.75 inches out of a total cross-sectional horizontal width of said wing device of approximately 6.5 inches, and said wall thickness of the other of said walls tapering from approximately 0.1 inch to approximately 0.08 inch over a horizontal distance of approximately 3.0 inches, said generally elliptical body having a maximum cross-sectional height of approximately 0.84 inch, said vertical reinforcing member being located a horizontal distance of approximately 1.3 inches from the edge of said first side portion.