CYLINDER LINER AND SEALING STRUCTURE FOR CYLINDER LINER

Abstract

A cylinder liner includes: a small diameter portion configured to form a cooling water passage between the small diameter portion and an inner peripheral surface of the cylinder block; a large diameter portion disposed adjacent to the small diameter portion in the axial direction and formed to have a larger diameter than the small diameter portion; and at least one seal groove formed on an outer peripheral surface of the large diameter portion in an annular shape along a circumferential direction. The large diameter portion includes a one-side wall portion formed between the cooling water passage and a cooling-water-passage-side seal groove which is a seal groove disposed closest to the cooling water passage in the axial direction, and an other-side wall portion disposed farther from the cooling water passage than the cooling-water-passage-side seal groove is in the axial direction. The one-side wall portion is configured to have, in at least part in a circumferential direction including a thrust direction of the piston, a larger distance to the inner peripheral surface of the cylinder block than a distance from the other-side wall portion to the inner peripheral surface of the cylinder block.

Claims

1. A cylinder liner mounted on a cylinder block of an internal combustion engine and slidably accommodating a piston along an axial direction, the cylinder liner comprising: a small diameter portion configured to form a cooling water passage between the small diameter portion and an inner peripheral surface of the cylinder block; a large diameter portion disposed adjacent to the small diameter portion in the axial direction and formed to have a larger diameter than the small diameter portion; and at least one seal groove formed on an outer peripheral surface of the large diameter portion in an annular shape along a circumferential direction, wherein the large diameter portion includes a one-side wall portion formed between the cooling water passage and a cooling-water-passage-side seal groove which is a seal groove disposed closest to the cooling water passage in the axial direction, and an other-side wall portion disposed farther from the cooling water passage than the cooling-water-passage-side seal groove is in the axial direction, and wherein the one-side wall portion is configured to have, in at least part in a circumferential direction including a thrust direction of the piston, a larger distance to the inner peripheral surface of the cylinder block than a distance from the other-side wall portion to the inner peripheral surface of the cylinder block.

2. The cylinder liner according to claim 1, wherein the one-side wall portion is configured to have, over the entire circumference in the circumferential direction, a larger distance to the inner peripheral surface of the cylinder block than a distance from the other-side wall portion to the inner peripheral surface of the cylinder block.

3. The cylinder liner according to claim 1, wherein the one-side wall portion has a cooling water passage side surface facing the cooling water passage, the cooling water passage side surface being formed such that, in at least part in the circumferential direction including the thrust direction of the piston, a distance to the inner peripheral surface of the cylinder block gradually increases with an increase in distance from the seal groove.

4. The cylinder liner according to claim 3, wherein the cooling water passage side surface is formed such that, over the entire circumference in the circumferential direction, a distance to the inner peripheral surface of the cylinder block gradually increases with an increase in distance from the seal groove.

5. The cylinder liner according to claim 1, further comprising a seal member mounted on the cooling-water-passage-side seal groove, wherein the seal member includes an O-ring, and a back-up ring disposed closer to the cooling water passage than the O-ring is, the back-up ring being configured to have, in at least part in the circumferential direction including the thrust direction of the piston, a smaller distance to the inner peripheral surface of the cylinder block than a distance from the one-side wall portion to the inner peripheral surface of the cylinder block.

6. A cylinder liner mounted on a cylinder block of an internal combustion engine and slidably accommodating a piston along an axial direction, the cylinder liner comprising: a small diameter portion configured to form a cooling water passage between the small diameter portion and an inner peripheral surface of the cylinder block; a large diameter portion disposed adjacent to the small diameter portion in the axial direction and formed to have a larger diameter than the small diameter portion; and at least one seal groove formed on an outer peripheral surface of the large diameter portion in an annular shape along a circumferential direction, wherein the large diameter portion includes a one-side wall portion formed between the cooling water passage and a cooling-water-passage-side seal groove which is a seal groove disposed closest to the cooling water passage in the axial direction, and wherein the one-side wall portion has a cooling water passage side surface facing the cooling water passage, the cooling water passage side surface being formed such that, in at least part in a circumferential direction including a thrust direction of the piston, a distance to the inner peripheral surface of the cylinder block gradually increases with an increase in distance from the seal groove.

7. The cylinder liner according to claim 6, wherein the cooling water passage side surface is formed such that, over the entire circumference in the circumferential direction, a distance to the inner peripheral surface of the cylinder block gradually increases with an increase in distance from the seal groove.

8. A sealing structure for a cylinder liner mounted on a cylinder block of an internal combustion engine, the sealing structure comprising: the cylinder block; the cylinder liner according to claim 1; and a seal member mounted on the cooling-water-passage-side seal groove.

Description

BRIEF DESCRIPTION OF DRAWINGS

[0028] FIG. 1 is a schematic cross-sectional view of an internal combustion engine including a cylinder liner according to an embodiment of the present invention including the axis of the internal combustion engine, and shows the state where the cylinder liner is mounted on a cylinder block.

[0029] FIG. 2 is a schematic partial enlarged cross-sectional view of a thrust side of the sealing structure of the cylinder liner according to an embodiment of the present invention.

[0030] FIG. 3 is a schematic partial enlarged cross-sectional view of a thrust side of the sealing structure of the cylinder liner according to another embodiment of the present invention.

[0031] FIG. 4 is a schematic partial enlarged cross-sectional view of a thrust side of the sealing structure of the cylinder liner according to another embodiment of the present invention.

[0032] FIG. 5 is a schematic partial enlarged cross-sectional view of a thrust side of the sealing structure of the cylinder liner according to a comparative example.

[0033] FIG. 6 is a schematic cross-sectional view of the sealing structure of the cylinder liner according to an embodiment of the present invention, perpendicular to the axis of the sealing structure.

[0034] FIG. 7 is a schematic cross-sectional view of the sealing structure of the cylinder liner according to an embodiment of the present invention, perpendicular to the axis of the sealing structure.

[0035] FIG. 8 is a schematic partial enlarged cross-sectional view of a thrust side of the sealing structure of the cylinder liner according to another embodiment of the present invention.

DETAILED DESCRIPTION

[0036] Embodiments of the present invention will now be described in detail with reference to the accompanying drawings. It is intended, however, that unless particularly identified, dimensions, materials, shapes, relative positions, and the like of components described in the embodiments shall be interpreted as illustrative only and not intended to limit the scope of the present invention.

[0037] For instance, an expression of relative or absolute arrangement such as “in a direction”, “along a direction”, “parallel”, “orthogonal”, “centered”, “concentric” and “coaxial” shall not be construed as indicating only the arrangement in a strict literal sense, but also includes a state where the arrangement is relatively displaced by a tolerance, or by an angle or a distance whereby it is possible to achieve the same function.

[0038] For instance, an expression of an equal state such as “same” “equal” and “uniform” shall not be construed as indicating only the state in which the feature is strictly equal, but also includes a state in which there is a tolerance or a difference that can still achieve the same function.

[0039] Further, for instance, an expression of a shape such as a rectangular shape or a cylindrical shape shall not be construed as only the geometrically strict shape, but also includes a shape with unevenness or chamfered corners within the range in which the same effect can be achieved.

[0040] On the other hand, an expression such as “comprise”, “include”, “have”, “contain” and “constitute” are not intended to be exclusive of other components.

[0041] The same features can be indicated by the same reference numerals and not described in detail.

[0042] FIG. 1 is a schematic cross-sectional view of an internal combustion engine including a cylinder liner according to an embodiment of the present invention, including the axis of the internal combustion engine, and shows the state where the cylinder liner is mounted on a cylinder block.

[0043] As shown in FIG. 1, a cylinder liner 1 has a cylindrical shape extending along the direction of the axis LA of the cylinder liner 1, and is mounted on a cylinder block 12 of an internal combustion engine 10. Hereinafter, the direction of the axis LA of the cylinder liner 1 is referred to as “axial direction”, and the direction perpendicular to the axial direction is referred to as “radial direction”.

[0044] As shown in FIG. 1, the internal combustion engine 10 includes the cylinder liner 1, a seal member 8 attached to the cylinder liner 1, the cylinder block 12, a piston 14, a piston pin 15, a connecting rod 16, and a crankshaft 17. A sealing structure 11 for a cylinder liner includes the cylinder liner 1, the seal member 8, and the cylinder block 12.

[0045] Each of the cylinder block 12 and the cylinder liner 1 is made of a metal material. The cylinder block 12 has an inner peripheral surface 121 (bore inner peripheral surface) for accommodating the cylinder liner 1. The cylinder liner 1 is disposed inside the inner peripheral surface 121 of the cylinder block 12, and is configured to form a cooling water passage 13 between the cylinder liner 1 and the inner peripheral surface 121 of the cylinder block 12.

[0046] The cylinder liner 1 has an inner peripheral surface 7 for accommodating the piston 14 slidably along the axial direction. The piston 14 is disposed inside the inner peripheral surface 7 of the cylinder liner 1, and is connected to one longitudinal end of the connecting rod 16 via the piston pin 15. The other longitudinal end of the connecting rod 16 is connected to the crankshaft 17. The crankshaft 17 is configured to be rotatable around the rotation center C1.

[0047] During operation of the internal combustion engine 10, the piston 14 performs a reciprocating motion along the axial direction. The reciprocating motion of the piston 14 is converted to a rotational motion of the crankshaft 17 by the piston pin 15 and the connecting rod 16.

[0048] Due to the reciprocating motion of the piston 14 and the rotational motion of the crankshaft 17, the cylinder liner 1 is subjected to a thrust force from the piston 14 toward the outside in the radial direction. The thrust force acts in a direction perpendicular to the axis LA of the cylinder liner 1 and the axis LB of the piston pin 15 (the right-left direction in FIG. 1).

[0049] Hereinafter, a side in the direction perpendicular to the axis LA of the cylinder liner 1 and the axis LB of the piston pin 15 and downstream of the rotational direction of the crankshaft 17 at the top dead center (the right side in the figure) is referred to as “thrust side”, and a direction toward the thrust side is referred to as “thrust direction T”. Further, a side in the direction perpendicular to the axis LA of the cylinder liner 1 and the axis LB of the piston pin 15 and upstream of the rotational direction of the crankshaft 17 at the top dead center (the left side in the figure) is referred to as “anti-thrust side”, and a direction toward the anti-thrust side is referred to as “anti-thrust direction AT”. In other words, the anti-thrust direction AT is opposite to the thrust direction T.

[0050] FIG. 2 is a schematic partial enlarged cross-sectional view of the thrust side of the sealing structure of the cylinder liner according to an embodiment of the present invention. FIGS. 3 and 4 are each a schematic partial enlarged cross-sectional view of the thrust side of the sealing structure of the cylinder liner according to another embodiment of the present invention.

[0051] As shown in FIG. 1, the cylinder liner 1 includes a small diameter portion 2 configured to form the cooling water passage 13 between the small diameter portion 2 and the inner peripheral surface 121 of the cylinder block 12, a large diameter portion 3 disposed adjacent to the small diameter portion 2 in the axial direction and formed to have a larger diameter than the small diameter portion 2, and at least one seal groove 6 formed on an outer peripheral surface 31 of the large diameter portion 3 in an annular shape along the circumferential direction.

[0052] In the illustrated embodiment, the large diameter portion 3 is located at a side closer to the crankshaft 17 than the small diameter portion 2 is in the axial direction (the bottom side in the figure). The at least one seal groove 6 includes three (a plurality of) seal grooves 6 arranged in the axial direction.

[0053] In the illustrated embodiment, as shown in FIGS. 2 to 4, the seal groove 6 includes a near passage side surface 61 disposed closest to the cooling water passage 13 in the axial direction (the top side in the figure), a far passage side surface 62 disposed farther away from the cooling water passage 13 than the near passage side surface 61 in the axial direction, and a bottom surface 63 connecting the inner peripheral end of the near passage side surface 61 with the inner peripheral end of the far passage side surface 62. Each of the near passage side surface 61 and the far passage side surface 62 extends along the direction perpendicular to (crossing) the axial direction. The bottom surface 63 extends along the axial direction.

[0054] As shown in FIGS. 2 to 4, the seal member 8 is mounted in the seal groove 6. In the illustrated embodiment, the seal member 8 includes an annular O-ring 81 having a circular or elliptical cross-sectional shape. The O-ring 81 is made of an elastic material such as rubber. The O-ring 81 is shrunk along the radial direction and is in contact with the bottom surface 63 and the inner peripheral surface 121 of the cylinder block 12. The O-ring 81 seals the gap between the outer peripheral surface 31 of the large diameter portion 3 and the inner peripheral surface 121 of the cylinder block 12 over the entire circumference in the circumferential direction to prevent cooling water in the cooling water passage 13 from leaking to the crank case side (the bottom side in the figure), which is not shown.

[0055] As shown in FIGS. 2 to 4, the large diameter portion 3 includes a one-side wall portion 4 formed between the cooling water passage 13 and a cooling-water-passage-side seal groove 6A which is a seal groove disposed closest to the cooling water passage 13 in the axial direction (the top side in the figure), and an other-side wall portion 5 disposed farther from the cooling water passage 13 than the cooling-water-passage-side seal groove 6A is in the axial direction.

[0056] In the illustrated embodiment, the one-side wall portion 4 has a cooling water passage side surface 42 facing the cooling water passage 13, a near passage side surface 61A (61) of the cooling-water-passage-side seal groove 6A, and an outer peripheral surface 41 contiguous with the cooling water passage side surface 42 and the near passage side surface 61A and connecting the outer peripheral end of the cooling water passage side surface 42 and the outer peripheral end of the near passage side surface 61A. The outer peripheral surface 41 of the one-side wall portion 4 extends along the axial direction. The other-side wall portion 5 has a far passage side surface 62A (62) of the cooling-water-passage-side seal groove 6A, and an outer peripheral surface 51 contiguous with the far passage side surface 62A and extending from the outer peripheral end of the far passage side surface 62A along the axial direction in a direction away from the cooling water passage 13.

[0057] As shown in FIGS. 2 to 4, the cooling water passage 13 communicates with a cooling water narrow passage 13A. The cooling water narrow passage 13A is formed between the outer peripheral surface 41 of the one-side wall portion 4 and the inner peripheral surface 121 of the cylinder block 12, and a part of the cooling water narrow passage 13A is delimited by the O-ring 81 inserted in the cooling-water-passage-side seal groove 6A. Hereinafter, the cooling water narrow passage 13A is also referred to as a portion of the cooling water passage 13 in the vicinity of the cooling-water-passage-side seal groove 6A.

[0058] As shown in FIGS. 2 to 4, D1 is a distance in the radial direction between the outer peripheral surface 41 of the one-side wall portion 4 and the inner peripheral surface 121 of the cylinder block 12. D2 is a distance in the radial direction between the outer peripheral surface 51 of the other-side wall portion 5 and the inner peripheral surface 121 of the cylinder block 12. D3 is a distance in the radial direction between the outer peripheral surface 21 of the small diameter portion 2 and the inner peripheral surface 121 of the cylinder block 12.

[0059] In the illustrated embodiment, as shown in FIGS. 2 to 4, the distance D1 is smaller than the distance D2 at the circumferential position corresponding to the distance D1 over the entire circumference in the circumferential direction.

[0060] FIG. 5 is a schematic partial enlarged cross-sectional view of the thrust side of the sealing structure of the cylinder liner according to a comparative example.

[0061] As shown in FIG. 5, a one-side wall portion 4A in the sealing structure 11A of the cylinder liner according to the comparative example is configured to have, over the entire circumference in the circumferential direction, the same distance to the inner peripheral surface 121 of the cylinder block 12 as the distance from the other-side wall portion 5 to the inner peripheral surface 121 of the cylinder block 12. In other words, as shown in FIG. 5, the distance D1 (D4) has the same length as the distance D2 at the circumferential position corresponding to the distance D1 over the entire circumference in the circumferential direction.

[0062] In the sealing structure 11A of the cylinder liner according to the comparative example, when the thrust force F acts on the cylinder liner 1, the cylinder liner 1 moves in the thrust direction T for a short time. At this time, cooling water in the cooling water narrow passage 13A (the portion of the cooling water passage 13 in the vicinity of the cooling-water-passage-side seal groove 6A) is pushed from the cooling water narrow passage 13A by the pressure applied from the one-side wall portion 4A of the cylinder liner 1, so that the flow velocity is increased. If the difference in flow velocity between cooling water pushed from the cooling water narrow passage 13A into the cooling water passage 13 and cooling water in the cooling water passage 13 is large, a negative pressure area may be generated in the cooling water passage 13. If the negative pressure area is generated in the cooling water passage 13, cavitation is likely to occur in the cooling water passage 13.

[0063] The cylinder liner 1 according to some embodiments includes the small diameter portion 2, the large diameter portion 3 including the one-side wall portion 4 and the other-side wall portion 5, and the at least one seal groove 6, as shown in FIGS. 2 to 4. The one-side wall portion 4 is configured to have, in at least part in the circumferential direction including the thrust direction T of the piston 14, a larger distance to the inner peripheral surface 121 of the cylinder block 12 than the distance from the other-side wall portion 5 to the inner peripheral surface 121 of the cylinder block 12. In other words, in at least part in the circumferential direction including the thrust direction T of the piston 14, the distance D1 (D5) is larger than the distance D2 at the circumferential position corresponding to the distance D1.

[0064] According to the above configuration, the one-side wall portion 4 of the cylinder liner 1 is configured to have, in at least part in the circumferential direction including the thrust direction T of the piston 14, a larger distance to the inner peripheral surface 121 of the cylinder block 12 than the distance from the other-side wall portion 5 to the inner peripheral surface 121 of the cylinder block 12. In other words, the cooling water narrow passage 13A (the portion of the cooling water passage 13 in the vicinity of the cooling-water-passage-side seal groove 6A) has a large volume in at least part in the circumferential direction including the thrust direction T of the piston 14. Since the cylinder liner 1 has a large volume in the cooling water narrow passage 13A to increase the volume of cooling water in the cooling water narrow passage 13A, the pressure applied to cooling water in the cooling water narrow passage 13A can be dispersed when the cylinder liner 1 moves in the thrust direction T for a short time. As a result, it is possible to suppress the increase in flow velocity of cooling water pushed from the cooling water narrow passage 13A to the cooling water passage 13. By suppressing the increase in flow velocity of cooling water pushed from the cooling water narrow passage 13A, the cylinder liner 1 can suppress the occurrence of negative pressure area in the cooling water passage 13, and thus suppress the occurrence of cavitation.

[0065] FIG. 6 is a schematic cross-sectional view of the sealing structure of the cylinder liner according to an embodiment of the present invention, perpendicular to the axis of the sealing structure.

[0066] In some embodiments, as shown in FIG. 6, the one-side wall portion 4 is configured to have, in part in the circumferential direction including the thrust direction T of the piston 14, a larger distance to the inner peripheral surface 121 of the cylinder block 12 than the distance from the other-side wall portion 5 to the inner peripheral surface 121 of the cylinder block 12.

[0067] In the illustrated embodiment, as shown in FIG. 6, the one-side wall portion 4 includes a short portion 44 where the outer peripheral surface 41 is disposed radially inward of the outer peripheral surface 51 of the other-side wall portion 5 at the corresponding circumferential position, and a same-diameter portion 47 where the outer peripheral surface 41 overlaps in the radial direction with the outer peripheral surface 51 of the other-side wall portion 5 at the corresponding circumferential position.

[0068] In the illustrated embodiment shown in FIG. 6, the short portion 44 is formed continuously along the circumferential direction from a step surface 45, connecting the short portion 44 and the same-diameter portion 47 and formed at a position rotated by a predetermined angle θ1 from the thrust direction T to one side (the counterclockwise direction in the figure) around the axis LA of the cylinder liner 1, to a step surface 46, connecting the short portion 44 and the same-diameter portion 47 and formed at a position rotated by a predetermined angle θ2 from the thrust direction T to the other side (the clockwise direction in the figure) around the axis LA of the cylinder liner 1.

[0069] In an embodiment, each of the predetermined angles θ1 and θ2 is equal to or more than 30 degrees. Each of the predetermined angles θ1 and θ2 is preferably equal to or more than 45 degrees, more preferably equal to or more than 60 degrees.

[0070] FIG. 7 is a schematic cross-sectional view of the sealing structure of the cylinder liner according to an embodiment of the present invention, perpendicular to the axis of the sealing structure.

[0071] In some embodiments, as shown in FIG. 7, the one-side wall portion 4 is configured to have, over the entire circumference in the circumferential direction, a larger distance to the inner peripheral surface 121 of the cylinder block 12 than the distance from the other-side wall portion 5 to the inner peripheral surface 121 of the cylinder block 12.

[0072] In the illustrated embodiment, as shown in FIG. 7, the one-side wall portion 4 has the short portion 44 over the entire circumference in the circumferential direction including the thrust direction T and the anti-thrust direction AT.

[0073] With the above configuration, since the cylinder liner 1 has a large volume in the cooling water narrow passage 13A (the portion of the cooling water passage 13 in the vicinity of the cooling-water-passage-side seal groove 6A) to increase the volume of cooling water in the cooling water narrow passage 13A over the entire circumference in the circumferential direction, the pressure applied to cooling water in the cooling water narrow passage 13A can be dispersed even when the cylinder liner 1 moves in the anti-thrust direction AT (direction opposite to thrust direction T) for a short time. As a result, it is possible to suppress the increase in flow velocity of cooling water pushed from the cooling water narrow passage 13A to the cooling water passage 13. By suppressing the increase in flow velocity of cooling water pushed from the cooling water narrow passage 13A over the entire circumference in the circumferential direction, the cylinder liner 1 can suppress the occurrence of negative pressure area in the cooling water passage 13, and thus suppress the occurrence of cavitation over the entire circumference in the circumferential direction including the anti-thrust direction AT.

[0074] Further, with the above configuration, since the cylinder liner 1 has the short portion 44 over the entire circumference in the circumferential direction, the cylinder liner 1 can be mounted on the cylinder block 12 without considering the circumferential position. Thus, with the above-described cylinder liner 1, compared to the case where the short portion 44 is formed partially in the circumferential direction, it is possible to improve the workability of mounting the cylinder liner 1 on the cylinder block 12.

[0075] In some embodiments, as shown in FIGS. 3 and 4, the one-side wall portion 4 has the cooling water passage side surface 42 facing the cooling water passage 13. The cooling water passage side surface 42 is formed such that, in at least part in the circumferential direction including the thrust direction T of the piston 14, a distance to the inner peripheral surface 121 of the cylinder block 12 gradually increases with an increase in distance from the seal groove 6. In other words, the cooling water passage side surface 42 includes a cooling water passage side surface 42B formed such that, in at least part in the circumferential direction including the thrust direction T of the piston 14, a distance to the inner peripheral surface 121 of the cylinder block 12 gradually increases with an increase in distance from the seal groove 6.

[0076] As shown in FIGS. 3 and 4, one end P1 (the lower end in the figure) of the cooling water passage side surface 42B in the axial direction is connected to an end (the lower end in the figure) of the outer peripheral surface 41 of the one-side wall portion 4 closer to the cooling water passage 13, and the other end P2 (the upper end in the figure) in the axial direction is connected to an end (the lower end in the figure) of the outer peripheral surface 21 of the small diameter portion 2 closer to the seal groove 6.

[0077] D6 is a distance in the radial direction between the cooling water passage side surface 42B and the inner peripheral surface 121 of the cylinder block 12. From one end P1 to the other end P2 in the axial direction, the distance D6 gradually increases from the same length as the distance D1 (D5) to the same length as the distance D3.

[0078] As shown in FIGS. 3 to 4, between the cooling water passage 13 and the cooling water narrow passage 13A, a cooling water connection passage 13B is formed. The cooling water narrow passage 13A communicates with the cooling water passage 13 via the cooling water connection passage 13B. The cooling water connection passage 13B is formed between the cooling water passage side surface 42B and the inner peripheral surface 121 of the cylinder block 12. Hereinafter, the cooling water connection passage 13B is also referred to as “portion of the cooling water passage 13 contiguous with the portion in the vicinity of the cooling-water-passage-side seal groove 6A”.

[0079] According to the above configuration, the one-side wall portion 4 of the cylinder liner 1 has the cooling water passage side surface 42 (42B) formed such that, in at least part in the circumferential direction including the thrust direction T of the piston 14, a distance to the inner peripheral surface 121 of the cylinder block 12 gradually increases with an increase in distance from the seal groove 6. In other words, the cooling water connection passage 13B (the portion of the cooling water passage 13 contiguous with the portion in the vicinity of the cooling-water-passage-side seal groove 6A) has a gradual volume change in at least part in the circumferential direction including the thrust direction T of the piston 14. Since the cylinder liner 1 has a gradual volume change in the cooling water connection passage 13B, cooling water in the cooling water narrow passage 13A can easily flow to the cooling water connection passage 13B when the cylinder liner 1 moves in the thrust direction T for a short time. As a result, it is possible to suppress the increase in flow velocity of cooling water pushed from the cooling water narrow passage 13A. By suppressing the increase in flow velocity of cooling water pushed from the cooling water narrow passage 13A, the cylinder liner 1 can suppress the occurrence of negative pressure area in the cooling water passage 13, and thus suppress the occurrence of cavitation.

[0080] The present embodiment can be implemented independently, as described below.

[0081] In some embodiments, as shown in FIGS. 3 and 4, the cooling water passage side surface 42B is configured to have a curved shape recessed inward in the radial direction. In this case, since the cooling water passage side surface 42B is configured to have a curved shape recessed inward in the radial direction, compared to a virtual inclined plane connecting one end P1 to the other end P2 in a straight line, the volume of the cooling water connection passage 13B can be increased. Since the volume of the cooling water connection passage 13B is increased to increase the volume of cooling water in the cooling water connection passage 13B, cooling water in the cooling water narrow passage 13A can easily flow to the cooling water connection passage 13B when the cylinder liner 1 moves in the thrust direction T for a short time. As a result, it is possible to effectively suppress the increase in flow velocity of cooling water pushed from the cooling water narrow passage 13A.

[0082] In some embodiments, as shown in FIG. 6, the cooling water passage side surface 42 is formed such that, in part in the circumferential direction including the thrust direction T of the piston 14, a distance to the inner peripheral surface 121 of the cylinder block 12 gradually increases with an increase in distance from the seal groove 6. In other words, the cooling water passage side surface 42 includes the cooling water passage side surface 42B in part in the circumferential direction including the thrust direction T of the piston 14.

[0083] In the illustrated embodiment, as shown in FIG. 6, the cooling water passage side surface 42 includes the cooling water passage side surface 42A (see FIG. 2) extending along the direction perpendicular to (crossing) the axial direction and the cooling water passage side surface 42B.

[0084] In the embodiment shown in FIG. 6, the cooling water passage side surface 42B is formed continuously along the circumferential direction from the step surface 45 formed at a position rotated by a predetermined angle θ1 from the thrust direction T to the step surface 46 formed at a position rotated by a predetermined angle θ2 from the thrust direction T.

[0085] In some embodiments, as shown in FIG. 7, the cooling water passage side surface 42 is formed such that, over the entire circumference in the circumferential direction, a distance to the inner peripheral surface 121 of the cylinder block 12 gradually increases with an increase in distance from the seal groove 6. In other words, the cooling water passage side surface 42 includes the cooling water passage side surface 42B over the entire circumference in the circumferential direction.

[0086] According to the above configuration, the one-side wall portion 4 of the cylinder liner 1 has the cooling water passage side surface 42 (42B) formed such that, over the entire circumference in the circumferential direction, a distance to the inner peripheral surface 121 of the cylinder block 12 gradually increases with an increase in distance from the seal groove 6. Since the cylinder liner 1 has a gradual volume change in the cooling water connection passage 13B (the portion contiguous with the cooling water narrow passage 13A) over the entire circumference in the circumferential direction, cooling water in the cooling water narrow passage 13A can easily flow to the cooling water connection passage 13B even when the cylinder liner 1 moves in the anti-thrust direction AT (direction opposite to thrust direction T) for a short time. As a result, it is possible to suppress the increase in flow velocity of cooling water pushed from the cooling water narrow passage 13A. By suppressing the increase in flow velocity of cooling water pushed from the cooling water narrow passage 13A over the entire circumference in the circumferential direction, the cylinder liner 1 can suppress the occurrence of negative pressure area in the cooling water passage 13, and thus suppress the occurrence of cavitation over the entire circumference in the circumferential direction including the anti-thrust direction AT.

[0087] In some embodiments, as shown in FIG. 4, the cylinder liner 1 includes the seal member 8 mounted on the cooling-water-passage-side seal groove 6A. The seal member 8 includes the O-ring 81 and a back-up ring 82 disposed closer to the cooling water passage 13 than the O-ring 81 is. The back-up ring 82 is configured to have, in at least part in the circumferential direction including the thrust direction T of the piston 14, a smaller distance to the inner peripheral surface 121 of the cylinder block 12 than the distance from the one-side wall portion 4 to the inner peripheral surface 121 of the cylinder block 12.

[0088] In the illustrated embodiment, the back-up ring 82 is made of a resin material excellent in heat and water resistance and having less elasticity than the O-ring 81. The back-up ring 82 is formed in an arc shape with facing ends in the longitudinal direction of the back-up ring 82. The two ends may extend in the direction perpendicular to the longitudinal direction or may extend in a direction oblique to the longitudinal direction. The back-up ring 82 can be temporarily expanded when it is installed in the cooling-water-passage-side seal groove 6A, which facilitates the installation process in the cooling-water-passage-side seal groove 6A.

[0089] As shown in FIG. 4, D7 is a distance in the radial direction between an outer peripheral surface 821 of the back-up ring 82 and the inner peripheral surface 121 of the cylinder block 12.

[0090] In the illustrated embodiment, in at least part in the circumferential direction including the thrust direction T of the piston 14, the distance D7 is smaller than the distance D1 (D5). Further, the back-up ring 82 has a surface 822 on one side in the thickness direction in contact with the near passage side surface 61, and a surface 823 on the other side in the thickness direction in contact with the O-ring 81.

[0091] If a distance between the inner peripheral surface 121 of the cylinder block 12 and the one-side wall portion 4 is large, the O-ring 81 can easily come out of the cooling-water-passage-side seal groove 6A, which may reduce the workability of the process of mounting the cylinder liner 1 on the cylinder block 12.

[0092] According to the above configuration, the back-up ring 82 is disposed closer to the cooling water passage 13 than the O-81 ring is, and is configured to have, in at least part in the circumferential direction including the thrust direction T of the piston 14, a smaller distance to the inner peripheral surface 121 of the cylinder block 12 than a distance from the one-side wall portion 4 to the inner peripheral surface 121 of the cylinder block 12. Thus, when the cylinder liner 1 is mounted on the cylinder block 12, it is possible to prevent the O-ring 81 from coming out of the cooling-water-passage-side seal groove 6A. Thus, the back-up ring 82 can improve the workability of mounting the cylinder liner 1 on the cylinder block 12.

[0093] FIG. 8 is a schematic partial enlarged cross-sectional view of the thrust side of the sealing structure of the cylinder liner according to another embodiment of the present invention. The cylinder liner 1 shown in FIG. 8 differs from the cylinder liner 1 shown in FIG. 3 in that the one-side wall portion 4 does not include the short portion 44.

[0094] The cylinder liner 1 according to some embodiments includes the small diameter portion 2, the large diameter portion 3 including the one-side wall portion 4, and the at least one seal groove 6, as shown in FIG. 8. The one-side wall portion 4 has a cooling water passage side surface 42 (42C) facing the cooling water passage 13. The cooling water passage side surface 42 (42C) is formed such that, in at least part in the circumferential direction including the thrust direction T of the piston 14, a distance to the inner peripheral surface 121 of the cylinder block 12 gradually increases with an increase in distance from the seal groove 6. In other words, the cooling water passage side surface 42 includes a cooling water passage side surface 42C formed such that, in at least part in the circumferential direction including the thrust direction T of the piston 14, a distance to the inner peripheral surface 121 of the cylinder block 12 gradually increases with an increase in distance from the seal groove 6.

[0095] As shown in FIG. 8, one end P3 (the lower end in the figure) of the cooling water passage side surface 42C in the axial direction is connected to an end (the lower end in the figure) of the outer peripheral surface 41 of the one-side wall portion 4 closer to the cooling water passage 13, and the other end P2 (the upper end in the figure) in the axial direction is connected to an end (the lower end in the figure) of the outer peripheral surface 21 of the small diameter portion 2 closer to the seal groove 6.

[0096] As shown in FIG. 8, between the cooling water passage 13 and the cooling water narrow passage 13A, a cooling water connection passage 13C is formed. The cooling water narrow passage 13A communicates with the cooling water passage 13 via the cooling water connection passage 13C. The cooling water connection passage 13C is formed between the cooling water passage side surface 42C and the inner peripheral surface 121 of the cylinder block 12. Hereinafter, the cooling water connection passage 13C is also referred to as “portion of the cooling water passage 13 contiguous with the portion in the vicinity of the cooling-water-passage-side seal groove 6A”.

[0097] In the illustrated embodiment, since the one-side wall portion 4 has the same-diameter portion 47 over the entire circumference in the circumferential direction, the distance D1 (D4) has the same length as the distance D2 at the circumferential position corresponding to the distance D1 over the entire circumference in the circumferential direction. D8 is a distance in the radial direction between the cooling water passage side surface 42C and the inner peripheral surface 121 of the cylinder block 12. From one end P3 to the other end P2 in the axial direction, the distance D8 gradually increases from the same length as the distance D1 (D4) to the same length as the distance D3.

[0098] According to the above configuration, the one-side wall portion 4 of the cylinder liner 1 has the cooling water passage side surface 42 (42C) formed such that, in at least part in the circumferential direction including the thrust direction T of the piston 14, a distance to the inner peripheral surface 121 of the cylinder block 12 gradually increases with an increase in distance from the seal groove 6. In other words, the cooling water passage side surface 42C (the portion of the cooling water passage 13 contiguous with the portion in the vicinity of the cooling-water-passage-side seal groove 6A) has a gradual volume change in at least part in the circumferential direction including the thrust direction T of the piston 14. Since the cylinder liner 1 has a gradual volume change in the cooling water passage side surface 42C, cooling water in the cooling water narrow passage 13A can easily flow to the cooling water connection passage 13B when the cylinder liner 1 moves in the thrust direction T for a short time. As a result, it is possible to suppress the increase in flow velocity of cooling water pushed from the cooling water narrow passage 13A. By suppressing the increase in flow velocity of cooling water pushed from the cooling water narrow passage 13A, the cylinder liner 1 can suppress the occurrence of negative pressure area in the cooling water passage 13, and thus suppress the occurrence of cavitation.

[0099] In some embodiments, as shown in FIG. 8, the cooling water passage side surface 42C is configured to have a curved shape recessed inward in the radial direction. In this case, since the cooling water passage side surface 42C is configured to have a curved shape recessed inward in the radial direction, compared to a virtual inclined plane connecting one end P3 to the other end P2 in a straight line, the volume of the cooling water connection passage 13C can be increased. Since the volume of the cooling water connection passage 13C is increased to increase the volume of cooling water in the cooling water connection passage 13C, cooling water in the cooling water narrow passage 13A can easily flow to the cooling water connection passage 13C when the cylinder liner 1 moves in the thrust direction T for a short time. As a result, it is possible to effectively suppress the increase in flow velocity of cooling water pushed from the cooling water narrow passage 13A.

[0100] In some embodiments, the cooling water passage side surface 42C is formed in part in the circumferential direction including the thrust direction T of the piston 14 as with the cooling water passage side surface 42B. In an embodiment, the cooling water passage side surface 42C is formed continuously along the circumferential direction from a position rotated by a predetermined angle θ1 from the thrust direction T to a position rotated by a predetermined angle θ2 from the thrust direction T, as shown in FIG. 6.

[0101] In some embodiments, as shown in FIG. 8, the cooling water passage side surface 42 is formed such that, over the entire circumference in the circumferential direction, a distance to the inner peripheral surface 121 of the cylinder block 12 gradually increases with an increase in distance from the seal groove 6. In other words, the cooling water passage side surface 42 includes the cooling water passage side surface 42C over the entire circumference in the circumferential direction.

[0102] According to the above configuration, the one-side wall portion 4 of the cylinder liner 1 has the cooling water passage side surface 42 (42C) formed such that, over the entire circumference in the circumferential direction, a distance to the inner peripheral surface 121 of the cylinder block 12 gradually increases with an increase in distance from the seal groove 6. Since the cylinder liner 1 has a gradual volume change in the cooling water connection passage 13C (the portion contiguous with the cooling water narrow passage 13A) over the entire circumference in the circumferential direction, cooling water in the cooling water narrow passage 13A can easily flow to the cooling water connection passage 13C even when the cylinder liner 1 moves in the anti-thrust direction AT (direction opposite to thrust direction T) for a short time. As a result, it is possible to suppress the increase in flow velocity of cooling water pushed from the cooling water narrow passage 13A. By suppressing the increase in flow velocity of cooling water pushed from the cooling water narrow passage 13A over the entire circumference in the circumferential direction, the cylinder liner 1 can suppress the occurrence of negative pressure area in the cooling water passage 13, and thus suppress the occurrence of cavitation over the entire circumference in the circumferential direction including the anti-thrust direction AT.

[0103] The sealing structure 11 for a cylinder liner according to some embodiments includes the cylinder block 12, the cylinder liner 1, and the seal member 8 mounted on the cooling-water-passage-side seal groove 6A described above.

[0104] According to the above configuration, since the sealing structure 11 for a cylinder liner includes the cylinder block 12, the cylinder liner 1, and the seal member 8, when a thrust force of the piston 14 acts on the cylinder liner 1, the cylinder liner 1 can suppress the increase in flow velocity of cooling water pushed from the cooling water narrow passage 13A (the portion of the cooling water passage 13 in the vicinity of the cooling-water-passage-side seal groove 6A), and thus suppress the occurrence of cavitation.

[0105] The present invention is not limited to the embodiments described above, but includes modifications to the embodiments described above, and embodiments composed of combinations of those embodiments.

REFERENCE SIGNS LIST

[0106] 1 Cylinder liner [0107] 2 Small diameter portion [0108] 21 Outer peripheral surface [0109] 3 Large diameter portion [0110] 31 Outer peripheral surface [0111] 4, 4A One-side wall portion [0112] 41 Outer peripheral surface [0113] 42, 42A to 42C Cooling water passage side surface [0114] 44 Short portion [0115] 45, 46 Step surface [0116] 47 Same-diameter portion [0117] 5 Other-side wall portion [0118] 51 Outer peripheral surface [0119] 6 Seal groove [0120] 6A Cooling-water-passage-side seal groove [0121] 61, 61A Near passage side surface [0122] 62, 62A Far passage side surface [0123] 63 Bottom surface [0124] 7 Inner peripheral surface [0125] 8 Seal member [0126] 81 O-ring [0127] 82 Back-up ring [0128] 821 Outer peripheral surface [0129] 10 Internal combustion engine [0130] 11 Sealing structure of cylinder liner [0131] 11A Sealing structure of cylinder liner according to comparative example [0132] 12 Cylinder block [0133] 121 Inner peripheral surface [0134] 13 Cooling water passage [0135] 13A Cooling water narrow passage [0136] 13B, 13C Cooling water connection passage [0137] 14 Piston [0138] 15 Piston pin [0139] 16 Connecting rod [0140] 17 Crankshaft [0141] AT Anti-thrust direction [0142] C1 Rotation center [0143] D1 to D8 Distance [0144] F Thrust force [0145] LA, LB Axis [0146] T Thrust direction