Opposed Piston Two Stroke Engine Liner Construction
US-2016252043-A1 · Sep 1, 2016 · US
US9845764B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9845764-B2 |
| Application number | US-201514675340-A |
| Country | US |
| Kind code | B2 |
| Filing date | Mar 31, 2015 |
| Priority date | Mar 31, 2015 |
| Publication date | Dec 19, 2017 |
| Grant date | Dec 19, 2017 |
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Official abstract text for this publication.
A cylinder liner for an opposed-piston engine, and corresponding methods of extending engine durability and thermal management therewith, has opposite ends and a bore with a longitudinal axis for supporting reciprocating movement of a pair of opposed pistons. An intermediate portion of the liner extends between the opposite ends and includes an annular liner portion within which the pistons reach respective TC locations. A liner ring is seated in a portion of the bore in the annular liner portion, between the TC locations, for scraping carbon from top lands of the pistons and/or increasing the thermal resistance of the annular liner portion.
Opening claim text (preview).
The invention claimed is: 1. A cylinder liner for an opposed-piston engine, comprising: a cylindrical wall with an interior surface defining a bore centered on a longitudinal axis of the liner, the bore having a first diameter relative to the longitudinal axis; intake and exhaust ports formed in the cylindrical wall near respective opposite ends of the liner; an intermediate portion of the liner extending between the ends and including an annular liner portion containing piston top center (TC) locations; the annular liner portion defined between first and second top ring reversal planes extending orthogonally to the longitudinal axis, in which the first top ring reversal plane is at a first axial position where the topmost ring of a first piston is located when the piston is at its TC location, and the second top ring reversal plane is at a second axial position where the topmost ring of a second piston is located when the piston is at its TC location; an annular groove in a portion of the bore in the annular liner portion; and, a liner ring seated in the annular groove, in which the liner ring has an interior annular surface with a second diameter relative to the longitudinal axis that is less than the first diameter; wherein: grooves on an outer annular surface of the liner ring that form one or more air resistors with the bore which act between the liner ring and the bore; and, the liner ring is formed from a material having a first thermal resistance and the cylinder liner is formed from a material having a second thermal resistance less than the first thermal resistance. 2. An opposed-piston engine including one or more cylinders, each cylinder comprising a cylinder tunnel in a cylinder block and a cylinder liner according to claim 1 seated in the cylinder tunnel.
for use in engines with two or more pistons reciprocating within same cylinder · CPC title
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
Making specific metal objects by operations not covered by a single other subclass or a group in this subclass · CPC title
Cylinder liners (F02F1/08, F02F1/16 take precedence) · CPC title
the pistons having equal strokes · CPC title
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