Precision air flow routing devices and method for thermal spray coating
US-11879173-B2 · Jan 23, 2024 · US
US9624869B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9624869-B2 |
| Application number | US-201414463891-A |
| Country | US |
| Kind code | B2 |
| Filing date | Aug 20, 2014 |
| Priority date | Aug 20, 2014 |
| Publication date | Apr 18, 2017 |
| Grant date | Apr 18, 2017 |
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A cylinder liner associated with an internal combustion engine includes a cooling moat to reduce temperatures at an upper cylinder liner seal. The cooling moat may have a gap extending upwardly toward an inner running surface of the cylinder liner to supply coolant to an upper portion of the cylinder liner. The cooling moat may be provided at a location between the inner running surface of the cylinder liner and a groove for the upper cylinder liner seal.
Opening claim text (preview).
We claim: 1. A cylinder liner for an engine, comprising: a hollow cylindrical sleeve extending from a lower end and an upper end, the hollow cylindrical sleeve having an outer surface and an inner running surface; an annular flange extending radially from the upper end of the hollow cylindrical sleeve and having a circumferential land portion and a seal groove disposed above the circumferential land portion; and a cooling moat defined by the sleeve, the cooling moat having a gap extending upwardly from a bottom surface of the annular flange toward the inner running surface of the hollow cylindrical sleeve and between the seal groove and the inner running surface, wherein the cooling moat includes a first moat wall and a second moat wall, the first moat wall and the second moat wall each extend upwardly from the bottom surface of the annular flange at an angle of between 20° and 60° with respect to a longitudinal axis defined by an outer longitudinal surface of the annular flange. 2. The cylinder liner of claim 1 , wherein a depth of the cooling moat from the bottom surface of the annular flange is between 1.5 mm and 11 mm. 3. The cylinder liner of claim 2 , wherein the depth of the cooling moat from the bottom surface of the annular flange is 3 mm. 4. The cylinder liner of claim 1 , wherein the cooling moat includes at least one moat wall. 5. The cylinder liner of claim 1 , wherein the first moat wall and the second moat wall are parallel to each other. 6. The cylinder liner of claim 1 , wherein the first moat wall and the second moat wall each extend upwardly from the bottom surface of the annular flange at an angle of 30° with respect to the longitudinal axis. 7. The cylinder liner of claim 1 , wherein a width between the first moat wall and the second moat wall is between 3 mm and 8 mm. 8. The cylinder liner of claim 7 , wherein the width between the first moat wall and the second moat wall is 3 mm. 9. An internal combustion engine, comprising: an engine block having at least one engine cylinder; and a cylinder liner mounted in the at least one engine cylinder, the cylinder liner including: a hollow cylindrical sleeve extending from a lower end and an upper end, the hollow cylindrical sleeve having an outer surface and an inner running surface, an annular flange extending radially from the upper end of the hollow cylindrical sleeve and having a circumferential land portion and a seal groove disposed above the circumferential land portion, and a cooling moat defined by the sleeve, the cooling moat having a gap extending upwardly from a bottom surface of the annular flange toward the inner running surface of the hollow cylindrical sleeve and between the seal groove and the inner running surface, wherein the cooling moat includes a first moat wall and a second moat wall, the first moat wall and the second moat wall each extend upwardly from the bottom surface of the annular flange at an angle of between 20° and 60° with respect to a longitudinal axis defined by an outer longitudinal surface of the annular flange. 10. The internal combustion engine of claim 9 , wherein a depth of the cooling moat from the bottom surface of the annular flange is between 1.5 mm and 11 mm. 11. The internal combustion engine of claim 9 , wherein the cooling moat of the cylinder liner includes a first moat wall and a second moat wall, and wherein the first moat wall and the second moat wall each extend upwardly from the bottom surface of the annular flange at an angle of between 20° and 60°, with respect to a longitudinal axis defined by an outer longitudinal surface of the annular flange. 12. The internal combustion engine of claim 9 , wherein a width between the first moat wall and the second moat wall is between 3 mm and 8 mm. 13. An internal combustion engine, comprising: an engine block having at least one engine cylinder; a cylinder liner mounted in the at least one engine cylinder; and an O-ring seal installed onto the cylinder liner, wherein the cylinder liner includes: a hollow cylindrical sleeve extending from a lower end and an upper end, the hollow cylindrical sleeve having an outer surface and an inner running surface, an annular flange extending radially from the upper end of the hollow cylindrical sleeve, the annular flange having a circumferential land portion and an upper cylinder liner seal groove disposed above the circumferential land portion, and a cooling moat defined by the sleeve, the cooling moat having a gap extending upwardly from a bottom surface of the annular flange toward the inner running surface of the hollow cylindrical sleeve and between the upper cylinder liner seal groove and the inner running surface, wherein the cooling moat includes a first moat wall and a second moat wall, the first moat wall and the second moat wall each extend upwardly from the bottom surface of the annular flange at an angle of between 20° and 60° with respect to a longitudinal axis defined by an outer longitudinal surface of the annular flange, and wherein the O-ring seal is installed onto the upper cylinder liner seal groove of the annular flange of the cylinder liner.
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