Thermal barrier coating member

Patent metadata

Field	Value
Publication number	US-11840981-B2
Application number	US-202017791032-A
Country	US
Kind code	B2
Filing date	Jun 25, 2020
Priority date	Feb 18, 2020
Publication date	Dec 12, 2023
Grant date	Dec 12, 2023

Abstract

At least one thermal barrier coating member mounted on an inner wall surface, facing a combustion chamber of an engine, of a cylinder liner accommodating a piston slidably along an axial direction, is provided with: a base layer configured to be detachably fitted into a recess formed in the inner wall surface of the cylinder liner; and a thermal barrier coating layer formed on an opposite side of the base layer from the inner wall surface of the cylinder liner. The thermal barrier coating layer is disposed above a piston ring which is positioned at an uppermost position in the axial direction of the cylinder liner when the piston reaches top dead center.

First claim

The invention claimed is:

1. A thermal barrier coating member, at least one of which is mounted on an inner wall surface of a cylinder liner accommodating a piston slidably along an axial direction, the inner wall surface facing a combustion chamber of an engine, the thermal barrier coating member comprising:
a base layer configured to be detachably fitted into a recess formed in the inner wall surface of the cylinder liner; and
a thermal barrier coating layer formed on an opposite side of the base layer from the inner wall surface of the cylinder liner,
wherein the thermal barrier coating layer is disposed above a piston ring which is positioned at an uppermost position in the axial direction of the cylinder liner when the piston reaches top dead center,
wherein the base layer includes:
a coated portion on which the thermal barrier coating layer is formed; and
an exposed portion on which the thermal barrier coating layer is not formed, and

wherein at least a part of the exposed portion has a protrusion which protrudes to the opposite side from the inner wall surface with respect to the thermal barrier coating layer formed on the coated portion.

2. The thermal barrier coating member according to claim 1 ,
wherein the protrusion includes a lower protrusion formed at a lower end portion of the base layer in the axial direction, and
wherein the coated portion is disposed above the lower protrusion in the axial direction.

3. The thermal barrier coating member according to claim 2 ,
wherein the coated portion has a first inner surface extending along the axial direction.

4. The thermal barrier coating member according to claim 2 ,
wherein the coated portion has a second inner surface inclined such that a distance from a center axis of the cylinder liner increases toward an upper side in the axial direction.

5. The thermal barrier coating member according to claim 2 ,
wherein the protrusion further includes an upper protrusion disposed above the lower protrusion in the axial direction.

6. The thermal barrier coating member according to claim 1 ,
wherein, in a plan view of the combustion chamber viewed from below in the axial direction, the protrusion is formed within a range of at least ±30° in a circumferential direction of the cylinder liner with respect to a first straight line extending from a center axis of the cylinder liner in a direction perpendicular to an axis of a piston pin which rotatably supports the piston.

7. The thermal barrier coating member according to claim 1 ,
wherein at least one of an upper edge or a lower edge of the thermal barrier coating layer is tapered toward a tip side.

8. A thermal barrier coating member, at least one of which is mounted on an inner wall surface of a cylinder liner accommodating a piston slidably along an axial direction, the inner wall surface facing a combustion chamber of an engine, the thermal barrier coating member comprising:
a base layer configured to be detachably fitted into a recess formed in the inner wall surface of the cylinder liner; and
a thermal barrier coating layer formed on an opposite side of the base layer from the inner wall surface of the cylinder liner,
wherein the thermal barrier coating layer is disposed above a piston ring which is positioned at an uppermost position in the axial direction of the cylinder liner when the piston reaches top dead center,
wherein the base layer includes:
a coated portion on which the thermal barrier coating layer is formed; and
an exposed portion on which the thermal barrier coating layer is not formed, and

wherein, in a plan view of the combustion chamber viewed from below in the axial direction, the coated portion is formed in a range other than ±30° in a circumferential direction of the cylinder liner with respect to a first straight line extending from a center axis of the cylinder liner in a direction perpendicular to an axis of a piston pin which rotatably supports the piston.

9. A thermal barrier coating member, at least one of which is mounted on an inner wall surface of a cylinder liner accommodating a piston slidably along an axial direction, the inner wall surface facing a combustion chamber of an engine, the thermal barrier coating member comprising:
a base layer configured to be detachably fitted into a recess formed in the inner wall surface of the cylinder liner; and
a thermal barrier coating layer formed on an opposite side of the base layer from the inner wall surface of the cylinder liner,
wherein the thermal barrier coating layer is disposed above a piston ring which is positioned at an uppermost position in the axial direction of the cylinder liner when the piston reaches top dead center,
wherein the base layer includes:
a coated portion on which the thermal barrier coating layer is formed; and
an exposed portion on which the thermal barrier coating layer is not formed, and

wherein, in a plan view of the combustion chamber viewed from below in the axial direction, the coated portion is formed in a range other than ±15° in a circumferential direction of the cylinder liner with respect to a second straight line extending from a center axis of the cylinder liner and passing through center of an intake port.

Assignees

• Mitsubishi Heavy Ind Engine & Turbocharger Ltd

Inventors

• Terakado Kiyoshi
• Bessho Yuji
• Maehata Kimihiko

Classifications

• F02F1/004 Primary

  Cylinder liners (F02F1/08, F02F1/16 take precedence) · CPC title

• F02F2001/006

  having a ring at the inside of a liner or cylinder for preventing the deposit of carbon oil particles, e.g. oil scrapers · CPC title

• F02F2001/008

  Stress problems, especially related to thermal stress · CPC title