Strengthening layer attached to cylinder bore

Patent metadata

Field	Value
Publication number	US-10407761-B2
Application number	US-201615343286-A
Country	US
Kind code	B2
Filing date	Nov 4, 2016
Priority date	Nov 4, 2016
Publication date	Sep 10, 2019
Grant date	Sep 10, 2019

Abstract

An engine block and a method of coating an inner surface of an engine cylinder bore of an engine cylinder are provided. The method includes attaching a strengthening layer or ring onto an upper portion of the inner surface of the cylinder bore. The strengthening layer or ring may be attached by laser cladding. The method also includes depositing a thermal spray coating onto the inner surface of the cylinder bore and the strengthening layer or ring.

First claim

What is claimed is:

1. A method of coating an inner surface of an engine cylinder bore of an engine cylinder, the method comprising:
laser cladding a strengthening layer onto an upper portion of the inner surface of the engine cylinder bore; and
depositing a thermal spray coating onto the inner surface of the engine cylinder bore,
the inner surface of the engine cylinder bore defining a piston travel path, the method further comprising attaching the strengthening layer entirely outside of the piston travel path at an open end of the engine cylinder, the method further comprising depositing the thermal spray coating onto the strengthening layer,
the method further comprising forming the strengthening layer from at least one of the following: a nickel alloy, a copper alloy, and a steel alloy, and
the method further comprising providing the strengthening layer having a thickness in the range of 0.1 mm to about 0.4 mm.

2. The method of claim 1 , further comprising providing the strengthening layer having a height in the range of 5 to about 50 mm.

3. The method of claim 2 , further comprising disposing the strengthening layer at a position overlapping with a chamfer extending from the open end of the engine cylinder.

4. The method of claim 3 , further comprising forming an upper groove in the upper portion of the inner surface and disposing the strengthening layer within the upper groove.

5. A method of coating an inner surface of an engine cylinder bore of an engine cylinder, the method comprising:
attaching a strengthening layer onto an upper portion of the inner surface of the engine cylinder bore;
depositing a thermal spray coating onto the inner surface of the engine cylinder bore, the thermal spray coating extending farther into the engine cylinder bore than the strengthening layer;
forming the strengthening layer from at least one of the following: a nickel alloy, a copper alloy, and a steel alloy;
attaching the strengthening layer entirely outside of the piston travel path at an open end of the engine cylinder;
providing the strengthening layer having a thickness in the range of 0.1 mm to about 0.4 mm;
providing the strengthening layer having a height in the range of about 5 to about 50 mm;
forming an upper groove in the upper portion of the inner surface and disposing the strengthening layer within the upper groove;
forming the strengthening layer by laser cladding; and
depositing the thermal spray coating onto the strengthening layer.

6. The method of claim 5 , further comprising disposing the strengthening layer at a position overlapping with a chamfer extending from the open end of the engine cylinder.

7. An engine block comprising:
a plurality of cylinders defining a plurality of cylinder bores, each cylinder bore having an inner surface, each inner surface having a strengthening ring laser clad onto an upper portion of the inner surface;
a thermal spray coating formed on the inner surface of each cylinder bore, the thermal spray coating being adhered to the inner surface and to the strengthening ring, each strengthening ring being disposed entirely outside of a piston travel path at an open end of each cylinder of the plurality of cylinders, wherein the engine block is formed of aluminum, the thermal spray coating is formed of a steel alloy, and the strengthening ring is formed of at least one of the following: a nickel alloy, a copper alloy, and a steel alloy; and
a plurality of pistons, each piston being moveable in a piston travel path along the inner surface of a cylinder bore of the plurality of cylinder bores,
wherein each strengthening ring has a thickness in the range of 0.1 mm to about 0.4 mm and a height in the range of about 5 to about 50 mm.

8. The engine block of claim 7 , each cylinder defining a chamfer area adjacent to the open end, the strengthening ring being disposed at a position overlapping with the chamfer area.

9. The engine block of claim 8 , the upper portion forming an upper groove in the upper portion, the strengthening ring being disposed within the upper groove.

Assignees

• Gm Global Tech Operations Llc

Inventors

• Li Huaxin
• Gerard Dale A
• Kramer Martin S

Classifications

• F02F1/00

  Cylinders; Cylinder heads · CPC title

• C23C4/16

  Wires; Tubes · CPC title

• B23K2101/04

  Tubular or hollow articles · CPC title

• F02F2200/00

  Manufacturing · CPC title

• C23C4/02 Primary

  Pretreatment of the material to be coated, e.g. for coating on selected surface areas · CPC title