Process for repairing a cylinder running surface by means of plasma spraying processes

• US 8,877,285 B2
• Filed: 11/20/2012
• Issued: 11/04/2014
• Est. Priority Date: 11/22/2011
• Status: Active Grant

• Current Assignee: Ford Global Technologies, LLC (Ford Motor Company)
• Original Assignee: Ford Global Technologies, LLC (Ford Motor Company)
• Inventors: Silk, Mark Robert, Schramm, Leander, Puetz, Wolfgang, Verpoort, Clemens Maria
• Primary Examiner(s): MILLER, JR, JOSEPH ALBERT
• Application Number:
  US13/681,674
• Publication Number:
  US 20130129939A1
• Time in Patent Office: 714 Days
• Field of Search: None
• US Class Current: 427/140
• CPC Class Codes: B05D 5/005 Repairing damaged coatings
• CPC Class Codes: B23P 6/02 Pistons or cylinders
• CPC Class Codes: C23C 4/02 Pretreatment of the material to be coated, e.g. for coating on selected surface areas
• CPC Class Codes: C23C 4/12 characterised by the method of spraying
• CPC Class Codes: C23C 4/131 Wire arc spraying
• CPC Class Codes: C23C 4/134 Plasma spraying
• CPC Class Codes: C23C 4/18 After-treatment

Abstract

A method of repairing an inner surface of a cylinder liner housed in an engine block. Material is removed from the inner surface to produce a reduced-thickness region, the reduced-thickness region extending axially relative to the cylinder and stopping short of an end of the liner to leave a region of original diameter between the reduced thickness region and the end of the liner. The surface the reduced-thickness region is then roughened, for example by hammer brushing. A plasma coating is applied to the reduced-thickness region and to at least a portion of the region of original diameter. The coating is then finish-machined to produce a uniform internal diameter equal to an original internal diameter of the region of original diameter prior to the application of the coating.

Claims

1. A method of repairing a cylinder liner comprising:

machining the liner to produce a reduced-thickness region extending above a damaged top-dead-center region and into an undamaged head region above the top-dead-center region, but stopping short of a lip of the engine block adjacent to an upper end of the liner to leave an un-machined region of the liner at the upper end thereof;

roughening a surface of the reduced-thickness region;

applying a coating to cover the reduced-thickness region, the un-machined region, and at least a portion of the lip; and

finish-machining the coating to produce a desired internal diameter, the coating being substantially completely removed from a transition between the un-machined region and the lip.

2. The method of claim 1, wherein the step of applying the coating comprises a plasma spraying process.

3. The method of claim 2, wherein the plasma spraying process comprises a plasma transfer wire arc coating process.

4. The method of claim 1, wherein the machining step produces an inclined plane between the reduced-thickness region and the un-machined region.

5. The method of claim 1, wherein the roughening step comprises a hammer brushing process.

6. The method of claim 1, wherein the finish-machining step comprises honing.

7. A method of repairing a damaged region of a cylinder liner housed in an engine block comprising:

machining the cylinder liner to produce a reduced-thickness region extending above the damaged region but stopping short of an upper end of the liner adjacent to a lip of the engine block to leave an un-machined region of the liner adjacent to the upper end;

roughening a surface the reduced-thickness region;

applying a coating to the reduced-thickness region, the coating extending onto the un-machined region of the liner; and

finish-machining the coating to produce a desired internal diameter equal to a diameter of the un-machined region prior to the application of the coating, such that the coating is substantially completely removed from a transition between the upper end of the liner and the lip.

8. The method of claim 7, wherein the application of the coating further extends axially onto the lip of the engine block, and the finish-machining substantially completely removes the coating from the lip.

9. The method of claim 7, wherein the coating is applied by a plasma transfer wire arc coating process.

10. The method of claim 7, wherein the machining step produces an inclined plane between the reduced-thickness region and the un-machined region.

11. The method of claim 7, wherein the roughening step comprises a hammer brushing process.

12. The method of claim 7, wherein the finish-machining step comprises honing.

13. A method of repairing an inner surface of a cylinder liner housed in an engine block comprising:

removing material from the inner surface to produce a reduced-thickness region extending axially relative to the cylinder and stopping short of an upper end of the liner adjacent to a lip of the engine block to leave a region of original diameter between the reduced thickness region and the upper end of the liner;

roughening a surface of the reduced-thickness region;

applying a coating to the reduced-thickness region and to at least a portion of the region of original diameter; and

finish-machining the coating to produce a uniform internal diameter equal to an original internal diameter of the region of original diameter prior to the application of the coating, such that the coating is substantially completely removed from a transition between the upper end of the liner and the lip.

14. The method of claim 13, wherein the application of the coating further extends axially onto the lip of the engine block, and the finish-machining substantially completely removes the coating from the lip.

15. The method of claim 13, wherein the coating is applied by a plasma transfer wire arc coating process.

16. The method of claim 13, wherein the roughening step comprises a hammer brushing process.

17. The method of claim 13, wherein the finish-machining step comprises honing.