Wiper blade assembly and method of forming the same

• US 20070017056A1
• Filed: 07/19/2005
• Published: 01/25/2007
• Est. Priority Date: 07/19/2005
• Status: Abandoned Application

• Current Assignee: Valeo Electrical Systems Incorporated (Valeo SE)
• Original Assignee: Valeo Electrical Systems Incorporated (Valeo SE)
• Inventors: Jallet, Sebastien, Kokic, Steve, Cooke, Walter, Harris, Daryl, Dreher, Thomas
• Application Number:
  US11/184,443
• Publication Number:
  US 20070017056A1
• Time in Patent Office: Days
• US Class Current: 15/250.201
• CPC Class Codes: B60S 1/3808 Spoiler integral with the squeegee
• CPC Class Codes: B60S 1/381 Spoilers mounted on the squeegee or on the vertebra
• CPC Class Codes: B60S 1/3881 in additional element, e.g. spoiler
• CPC Class Codes: B60S 2001/3836 characterised by cross-sectional shape

Abstract

A wiper blade assembly includes a wiper blade member and an airfoil member operatively connected to the wiper blade member. The airfoil member extends longitudinally along at least a portion of the length of the wiper blade member. The airfoil member also has a cross-sectional profile that is symmetrical about a plane of symmetry extending through a center of the airfoil member and longitudinally through the airfoil member.

Claims

1. A wiper blade assembly, comprising:

a wiper blade member having a length; and

an airfoil member operatively connected to the wiper blade member, the airfoil member extending longitudinally along at least a portion of the wiper blade member length, the airfoil member having a cross-sectional profile that is symmetrical about a plane of symmetry extending through a center of the airfoil member and longitudinally through the airfoil member.

2. The wiper blade assembly as defined in claim 1 wherein the cross-sectional profile substantially prevents wiper blade assembly lift while reducing pullback when the assembly is subjected to aerodynamic forces during vehicle operation.

3. The wiper blade assembly as defined in claim 2 wherein the wiper blade assembly experiences during use, at air speeds of about 50 m/s, a lift force ranging from about 3 N/m to about 14 N/m and a drag force ranging from about 11 N/m to about 22 N/m.

4. The wiper blade assembly as defined in claim 2 wherein the pullback ranges from about 1 cm to about 3 cm.

5. The wiper blade assembly as defined in claim 1 wherein the cross-sectional profile is substantially a bell curve shape having sides and a top, the sides substantially defined by a side circular arc having a center external to the cross-sectional profile and the top substantially defined by a top circular arc having a center substantially on the plane of symmetry and internal to the cross-sectional profile.

6. The wiper blade assembly as defined in claim 1 wherein the cross-sectional profile is substantially a cardioid shape having sides and a top, the sides substantially defined by a side circular arc having a center internal to the cross-sectional profile and the top substantially defined by a top circular arc having a center substantially on the plane of symmetry and internal to the cross-sectional profile.

7. The wiper blade assembly as defined in claim 1 wherein the cross-sectional profile is substantially a triangular shape having substantially straight sides, each of the sides substantially equidistant from the plane of symmetry.

8. The wiper blade assembly as defined in claim 1, further comprising a supporting member positioned between the airfoil member and the wiper blade member, the supporting member being spaced from the airfoil member, thereby defining at least one groove therebetween, the at least one groove adapted to slidingly engage a wiper blade spline.

9. The wiper blade assembly as defined in claim 8 wherein the supporting member is integral with each of the wiper blade member and the airfoil member.

10. The wiper blade assembly as defined in claim 1, further comprising a supporting member positioned between the airfoil member and the wiper blade member, the supporting member having a channel extending substantially longitudinally therethrough, the channel adapted to engage a wiper blade spline.

11. The wiper blade assembly as defined in claim 10 wherein the airfoil member is integral with the supporting member, and the supporting member is adapted to engage the wiper blade member.

12. The wiper blade assembly as defined in claim 1 wherein the assembly is adapted to wipe a vehicle windshield.

13. The wiper blade assembly as defined in claim 1 wherein the wiper blade assembly is rotatable about 180°

about a rotation axis that is substantially perpendicular to the wiper blade member length.

14. A method for forming a wiper blade assembly, the method comprising operatively connecting an airfoil member to a wiper blade member having a length, the airfoil member extending longitudinally along at least a portion of the wiper blade member length, the airfoil member having a cross-sectional profile that is symmetrical about a plane of symmetry extending through a center of the airfoil member and longitudinally through the airfoil member.

15. The method as defined in claim 14 wherein the symmetrical cross-sectional profile substantially prevents wiper blade assembly lift while reducing pullback when the assembly is subjected to aerodynamic forces during vehicle operation.

16. The method as defined in claim 15 wherein the wiper blade assembly experiences during use, at air speeds of about 50 m/s, a lift force ranging from about 3 N/m to about 14 N/m and a drag force ranging from about 11 N/m to about 22 N/m.

17. The method as defined in claim 15 wherein the pullback ranges from about 1 cm to about 3 cm.

18. The method as defined in claim 14 wherein the cross-sectional profile is substantially a bell curve shape having sides and a top, the sides substantially defined by a side circular arc having a center external to the cross-sectional profile and the top substantially defined by a top circular arc having a center substantially on the plane of symmetry and internal to the cross-sectional profile.

19. The method as defined in claim 14 wherein the cross-sectional profile is substantially a cardioid shape having sides and a top, the sides substantially defined by a side circular arc having a center internal to the cross-sectional profile and the top substantially defined by a top circular arc having a center substantially on the plane of symmetry and internal to the cross-sectional profile.

20. The method as defined in claim 14 wherein the cross-sectional profile is substantially a triangular shape having substantially straight sides, each of the sides substantially equidistant from the plane of symmetry.

21. The method as defined in claim 14, further comprising establishing a supporting member between the wiper blade member and the airfoil member and spaced from the airfoil member so as to define at least one groove therebetween, the at least one groove adapted to slidingly engage a wiper blade spline.

22. The method as defined in claim 21 wherein the supporting member is formed integrally with each of the wiper blade member and the airfoil member.

23. The method as defined in claim 14, further comprising establishing a supporting member between the airfoil member and the wiper blade member, the supporting member having a channel extending substantially longitudinally therethrough, the channel adapted to engage a wiper blade spline.

24. The method as defined in claim 14 wherein the wiper blade member is integral with the airfoil member.

25. The method as defined in claim 14 wherein the wiper blade assembly is adapted to wipe a vehicle windshield.

26. The method as defined in claim 14 wherein the wiper blade assembly is rotatable about 180°

about a rotation axis that is substantially perpendicular to the wiper blade member length.

27. The method as defined in claim 14 wherein operatively connecting is accomplished by at least one of extrusion processes, co-molding processes, bonding processes, mechanical attachment processes, and combinations thereof.

28. A method for extending a useful life of a symmetrical wiper blade assembly, the method comprising forming a symmetrical wiper blade assembly adapted to be used in a vehicle windshield wiper system for a predetermined time interval after which the wiper blade assembly is adapted to be rotated about 180°

about a rotation axis that is substantially perpendicular to a length of the wiper blade assembly;

wherein the wiper blade assembly includes;

a wiper blade member which substantially defines the length of the wiper blade assembly; and

an airfoil member operatively connected to the wiper blade member, the airfoil member extending longitudinally along at least a portion of the wiper blade member length, the airfoil member having a cross-sectional profile that is symmetrical about a plane of symmetry extending through a center of the airfoil member and longitudinally through the airfoil member.