Vision enhanced method for making a full round bushing

• US 5,026,967 A
• Filed: 07/09/1990
• Issued: 06/25/1991
• Est. Priority Date: 07/09/1990
• Status: Expired due to Term

• Current Assignee: Mahle Engine Systems UK Ltd (MAHLE-STIFTUNG GmbH)
• Original Assignee: JPI Transportation Products Incorporated
• Inventors: Bell, Bruce A., Landis, Donald G.
• Primary Examiner(s): Albritton, C. L.
• Application Number:
  US07/550,084
• Time in Patent Office: 351 Days
• Field of Search: 219/121, 219/63, 219/121.64, 219/118, 219/121.78, 219/121.79, 219/121.75, 219/121.85, 29/149.5 R
• US Class Current: 219/121.64
• CPC Class Codes: B23K 2103/04 Steel or steel alloys
• CPC Class Codes: B23K 26/04 Automatically aligning, aiming or focusing the laser beam, e.g. using the back-scattered light
• CPC Class Codes: B23K 26/044 Seam tracking

Abstract

A full round bushing is formed by laser welding opposed edges of a bimetal member deformed into a generally cylindical configuration. The laser beam parameters are closely controlled so as to limit any adverse affect on a bearing metal layer. The weld only reaches a depth approximately 20% to 75% of a steel reinforcing layer. The beam approaches the seam between opposed edges at an angle of incidence approximately 10° to 45° and at a laser focal point offset 5% to 70% of the spot diameter of the laser beam. An overlap of the pulse spot-welding approximately 50% to 75% is preferable. A machine vision control system is used to locate the seam, moving the bushing to position the seam as desired relative to the laser and to trigger the laser to perform the welding operation.

Claims

1. A method of making a full round bushing comprising the steps of:

supplying a hollow generally cylindrical member having an open longitudinal seam defined by opposed edges disposed in generally facing relation, said cylindrical member having at least first and second different metal layers in generally concentric relation, one of said layers defining a bearing surface;

securing said cylindrical member in a fixture clamp;

taking a picture of a predetermined portion of said cylindrical member, said portion including said seam;

analyzing said picture to locate said seam;

rotating said cylindrical member to position said seam at a predetermined location relative to a laser source; and

laser welding said opposed edges to form an integral structure wherein said laser welding is essentially limited to the other of said metal layers such that said bearing surface is not degraded by said welding step.

2. The method as defined in claim 1 wherein said cylindrical member is welded by moving said cylindrical member longitudinally across a laser beam.

3. The method as defined in claim 1 wherein said picture is a first picture adjacent one longitudinal end of said cylindrical member and further comprising the steps of:

taking a second picture of a portion of said cylindrical member adjacent the opposite longitudinal end including said seam;

analyzing said second picture to locate said seam; and

laser welding along a line defined by the location of the seam in said first and second pictures.

4. The method as defined in claim 1 wherein said laser welding step includes welding to a depth of approximately 20% to 75% of the radial thickness of said other of said metal layers.

5. The method as defined in claim 1 wherein said laser welding step includes welding to a depth of approximately 50% of the radial thickness of said other of said metal layers.

6. The method as defined in claim 1 wherein said laser welding step includes welding with a laser beam disposed at an angle to a radial plane defined between said opposed edges.

7. The method as defined in claim 1 wherein said laser welding step includes welding with a beam oriented at an angle approximating 10 degrees to 45 degrees to a radial plane defined between said opposed edges.

8. The method as defined in claim 1 wherein said laser welding step includes welding with a beam oriented at an angle approximating 20 degrees to 25 degrees to a radial plane defined between said opposed edges.

9. The method as defined in claim 1 wherein said laser welding step includes welding with a beam with its focal point offset from one of said edges a dimension approximating 5% to 70% of a spot diameter of the laser beam.

10. The method as defined in claim 1 wherein said laser welding step includes welding with a beam with its focal point offset from one of said edges a dimension approximating 10% to 30% of a diameter of the laser beam.

11. The method as defined in claim 1 wherein said laser welding step includes forming individual spot welds which are overlapped approximately 50% to 70% of the spot diameter of the laser beam.

12. The method as defined in claim 1 further including the step of post-weld tempering by laser.

13. A bushing made in accordance with the method of claim 5.

14. The method as defined in claim 1 wherein said laser welding step includes welding to a depth of approximately 20% to 75% of the radial thickness of said other of said metal layers, said laser beam being oriented at an angle approximately 10 degrees to 45 degrees to the radial plane defined between said opposing edges and wherein the focal point of said laser beam is offset from one of said edges a dimension approximately 5% to 70% of the spot diameter of said laser beam.

15. The method as defined in claim 14 wherein said laser welding step includes welding to a depth of approximately 50% of the radial thickness of said other of said second layer.

16. The method as defined in claim 14 wherein said laser welding step includes welding with a beam oriented at an angle approximating 20 degrees to 25 degrees to said radial plane.

17. The method as defined in claim 14 wherein said laser welding step includes welding with a beam with its focal point offset from one of said edges a dimension approximating 10% to 30% of a spot diameter of the laser beam.

18. The method as defined in claim 14 wherein said laser welding step includes forming individual spot welds which are overlapped approximately 50% to 70% of the spot diameter of said laser beam.

19. The method as defined in claim 1 wherein the step of analyzing said picture includes the steps of:

dividing said picture into rows of pixels substantially parallel to said seam,

examining said rows in a predetermined order looking for a row having an intensity darker than a predetermined intensity value; and

after finding a darker row, searching rows on both sides of said darker row to determine the width of a darker band formed by said seam.

20. The method as defined in claim 19 wherein said predetermined order of examining said rows includes alternating between two halves of said picture a given number of rows from the center of said picture.

21. The method as defined in claim 20 wherein said given number of rows is four.