Method for making a full round bushing

• US 4,751,777 A
• Filed: 09/02/1986
• Issued: 06/21/1988
• Est. Priority Date: 09/02/1986
• Status: Expired due to Term

• Current Assignee: Dana Corporation (Dana, Inc.)
• Original Assignee: JPI/V Acquisition
• Inventors: Savel, Frank J. III
• Primary Examiner(s): Eley, Timothy V.
• Application Number:
  US06/902,538
• Time in Patent Office: 658 Days
• Field of Search: 29/149.56, 29/149.5 DP, 29/149.5 R, 29/149.55, 29/149.5 NM, 219/121 L, 219/121 LD
• US Class Current: 29/898.056
• CPC Class Codes: B21D 53/10 parts of bearings; sleeves; valve seats or the like
• CPC Class Codes: B23K 2103/04 Steel or steel alloys
• CPC Class Codes: B23K 26/24 Seam welding
• CPC Class Codes: B23K 26/244 Overlap seam welding
• CPC Class Codes: B23K 26/262 of longitudinal seams of tubes
• CPC Class Codes: Y10T 29/49671 Strip or blank material shaping

Abstract

A full round bushing is formed by laser welding opposed edges of a bimetal member deformed into a generally cylindrical configuration. The laser beam parameters are closely controlled so as to limit any adverse effect on a bearing metal layer. The weld only reaches a depth approximating 20% to 75% of a steel reinforcing layer. The beam approaches the seam at an angle of incidence approximating 10° to 45° and at a laser focal point offset 5% tp 70% of the spot diameter of the laser beam. An overlap of the pulse spot-welding approximating 50% to 75% is preferable.

Claims

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

supplying a hollow generally cylindrial 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; 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 laser welding step includes welding to a depth of approximately 20% to 75% of the radial thickness of said other of said metal layers.

3. 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.

4. 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.

5. 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.

6. 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.

7. 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.

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

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

supplying a multiple layered member having a first layer defining a bearing surface and a second reinforcing layer;

forming said member into a generally cylindrical configuration in which said first layer is disposed along an inner peripheral portion thereof and opposed edges are disposed in close-spaced relation along a longitudinal length thereof; and

,

laser welding said opposed edges of said second layer to form an integral structure wherein said laser welding is essentially limited to said second layer wherein said bearing surface is not degraded by said welding step.

10. The method as defined in claim 11 wherein said laser welding step includes welding to a depth of approximately 20% to 75% of the radial thickness of said second layer.

11. The method as defined in claim 9 wherein said laser welding step includes welding to a depth of approximately 50% of the radial thickness of said second layer.

12. The method as defined in claim 9 wherein said laser welding step includes welding with a laser beam disposed at an angle to a radial plane defined between said opposed edges.

13. The method as defined in claim 9 wherein said laser welding step includes welding at an angle approximating 10°

to 45°

to a radial plane defined between said opposed edges.

14. The method as defined in claim 9 further including the step of post-weld tempering by laser.

15. A bushing made in accordance with the method of claim 11.

16. The method as defined in claim 9 wherein said laser welding step includes welding with a beam oriented at an angle approximating 20 degrees to 25 degrees to said radial plane defined between said opposed edges.

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

18. The method as defined in claim 9 wherein said laser welding step includes welding with a beam with its focal point offset from one edge a dimension approximating 10% to 30% of a spot diameter of the laser beam.

19. The method as defined in claim 9 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.

20. A method of making full round bushings comprising the steps of:

supplying a multiple layered member having a first layer defining a bearing surface and a second layer defining a reinforcing metal;

forming said member into a generally cylindrical configuration in which said first layer is disposed along the inside surface of said member and opposed edges defining a seam are disposed in close spaced relation along a longitudinal length thereof; and

,

laser welding said opposing edges of said second layer to form an integral structure using a laser beam which welds to a depth of approximately 20% to 75% of the radial thickness of said second layer, whereby said bearing surface is not degraded by said welding step, said laser beam 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.

21. The method as defined in claim 20 wherein said laser welding step includes welding to a depth of approximately 50% of the radial thickness of said other of said second layer.

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

23. The method as defined in claim 20 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.

24. The method as defined in claim 20 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.