Thermal spray coating for connecting rod small end

Patent metadata

Field	Value
Publication number	US-9599148-B2
Application number	US-201414551604-A
Country	US
Kind code	B2
Filing date	Nov 24, 2014
Priority date	Oct 17, 2011
Publication date	Mar 21, 2017
Grant date	Mar 21, 2017

Abstract

A connecting rod having a small end and a large end, the small end including a pin bore defined by a pin bore surface. A thermal spray coating applied to at least a portion of the pin bore surface and a method of applying the thermal spray coating to the pin bore surface using a thermal spray technique.

First claim

What is claimed is:

1. A method, comprising:
providing a connecting rod having a piston pin end, a crankshaft pin end, and a beam extending therebetween;
forming a piston pin bore in the piston pin end, including forming a piston pin bore surface having a first portion and a second portion forming an entire circumference of the piston pin bore, wherein the first portion of the pin bore surface is recessed with respect to the second portion of the pin bore surface by a recess distance;
forming a crankshaft pin bore in the crankshaft pin end, the crankshaft pin bore defined by a crankshaft surface, the crankshaft pin bore being larger than the piston pin bore; and
applying a thermal spray coating to the first portion of the pin bore surface such that the second portion of the pin bore surface is uncoated.

2. The method of claim 1 , further comprising forming edges of the thermal spray coating at opposing ends of the first portion of the pin bore surface substantially flush with corresponding edges of the second portion of the pin bore surface.

3. The method of claim 1 , wherein applying the thermal spray coating includes applying an excess amount of coating material along opposing edges of the thermal spray coating.

4. The method of claim 3 , further comprising machining the at least one edge of the thermal spray coating, including the removing the excess amount of the coating material such that an adjacent component of the uncoated second portion of the pin bore surface is machined generally simultaneously with the machining of the thermally sprayed coating material, thereby forming the first portion of the pin bore surface substantially flush with the corresponding edges of the second portion of the pin bore surface.

5. The method of claim 1 , further comprising determining a high load area of the pin bore surface; and establishing the first portion of the pin bore surface as corresponding to the high load area of the pin bore surface.

6. The method of claim 5 , wherein the connecting rod is formed of a material, and the high load area is determined at least in part from a property of the material.

7. The method of claim 1 , further comprising forming recess transitions leading from opposing sides of the first portion of the pin bore surface, the recess transitions each leading to the second portion of the pin bore surface, the recess transitions each defining an oblique angle with respect to the adjacent first and second pin bore surfaces.

8. The method of claim 1 , further comprising forming recess transitions leading from opposing sides of the first portion of the pin bore surface, the recess transitions each leading to the second portion of the pin bore surface, the recess transitions each substantially parallel to a beam axis extending between the piston pin bore and the crankshaft pin bore.

9. The method of claim 1 , further comprising forming the first and second portions of the piston pin bore such that the first portion of the piston pin bore defines a first radius with respect to a bore center of the piston pin bore, and the second portion of the piston pin bore defines a second radius with respect to the bore center of the piston pin bore, wherein the first radius is larger than the second radius.

10. The method of claim 1 , further comprising establishing the thermal spray coating as including at least one of a copper alloy, an iron alloy, a nickel alloy, a cobalt alloy, a molybdenum alloy, a tungsten alloy, a tin alloy, and an aluminum alloy.

11. The method of claim 1 , wherein applying the thermal spray coating includes applying the thermal spray coating to define a coating thickness, the coating thickness substantially equal to the recess distance of the first portion of the pin bore surface.

12. The method of claim 1 , wherein applying the thermal spray coating includes applying the thermal spray coating to define a coating thickness, wherein the coating thickness is in a range of about 50 to 300 microns (μm).

13. The method of claim 1 , wherein applying the thermal spray coating includes applying the thermal spray coating such that the first portion of the bore surface has an angular extent of between approximately 70 and 120 degrees.

14. The method of claim 13 , wherein the angular extent is approximately 90 degrees.

15. The method of claim 7 , further comprising establishing the oblique angle as between approximately 10 and 80 degrees.

16. The method of claim 15 , wherein the oblique angle is approximately 45 degrees.

17. A method, comprising:
providing a connecting rod having a piston pin end, a crankshaft pin end, and a beam extending therebetween;
forming a piston pin bore in the piston pin end, including forming a piston pin bore surface having a first portion and a second portion forming an entire circumference of the piston pin bore, wherein the first portion of the pin bore surface is recessed with respect to the second portion of the pin bore surface by a recess distance;
forming a crankshaft pin bore in the crankshaft pin end, the crankshaft pin bore defined by a crankshaft surface, the crankshaft pin bore being larger than the piston pin bore; and
applying a thermal spray coating to the first portion of the pin bore surface such that the second portion of the pin bore surface is uncoated;
wherein the thermal spray coating defines a coating thickness, wherein the coating thickness is in a range of about 50 to 300 microns (μm); and
wherein applying the thermal spray coating includes applying the thermal spray coating such that the first portion of the bore surface has an angular extent of between approximately 70 and 120 degrees.

18. The method of claim 17 , further comprising forming edges of the thermal spray coating at opposing ends of the first portion of the pin bore surface substantially flush with corresponding edges of the second portion of the pin bore surface.

19. The method of claim 17 , further comprising determining a high load area of the pin bore surface; and establishing the first portion of the pin bore surface as corresponding to the high load area of the pin bore surface.

20. The method of claim 17 , further comprising forming the first and second portions of the piston pin bore such that the first portion of the piston pin bore defines a first radius with respect to a bore center of the piston pin bore, and the second portion of the piston pin bore defines a second radius with respect to the bore center of the piston pin bore, wherein the first radius is larger than the second radius.

Assignees

• Domanchuk David
• Lapp Michael T
• Rein Wolfgang
• Hall Christopher
• Stong Thomas
• Mahle Int Gmbh

Inventors

• Domanchuk David
• Lapp Michael T
• Rein Wolfgang
• Hall Christopher
• Stong Thomas

Classifications

• F16C7/023 Primary

  for piston engines, pumps or the like · CPC title

• Y10T74/2162

  Engine type · CPC title

• F16J7/00

  Piston-rods · CPC title

• F16J1/16

  with gudgeon-pin; Gudgeon-pins · CPC title

• F16C9/04

  Connecting-rod bearings; Attachments thereof · CPC title