LIQUID-COOLED INTERNAL COMBUSTION ENGINE

Abstract

A liquid-cooled internal combustion engine, including at least one cylinder block which has a cooling jacket and multiple cylinders. The cooling jacket has a base facing toward a crank chamber and a top facing toward a cylinder head sealing plane. The base has an undulating profile in which a first distance, as measured in the direction of the cylinder axis, between the base of the cooling jacket and the top in the region of at least one first engine transverse plane which encompasses the cylinder axis is greater than a second distance in the region of at least one second engine transverse plane between two adjacent cylinders. In order to reduce cylinder deformation, the cooling jacket has three different heights, in which a third distance between the base of the cooling jacket and the top is smaller in at least one face-end region of the cooling jacket.

Description

TECHNICAL FIELD

The invention relates to a liquid-cooled internal combustion engine, comprising at least one cylinder block which has a cooling jacket and multiple cylinders, wherein the cooling jacket has a base facing toward a crank chamber and a top facing toward a cylinder head sealing plane, and the base has an undulating profile as seen in a side view of the cylinder block, wherein a first distance, measured in the direction of the cylinder axis, between the base of the cooling jacket and the top in the region of at least one first engine transverse plane which encompasses the cylinder axis is greater than a second distance in the region of at least one second engine transverse plane between two adjacent cylinders.

BACKGROUND

U.S. Pat. No. 5,080,049 A describes a cylinder block for an internal combustion engine with several cylinders, wherein the cylinders are surrounded by a cooling jacket. The cooling jacket has an undulating profile on one longitudinal side of the cylinder block, wherein the distance of the base of the cooling jacket from the cylinder head sealing plane is smaller in the region of an engine transverse plane containing the cylinder head screw axes than in the region of a first transverse engine plane which contains the cylinder axis.

A liquid-cooled internal combustion engine with a similarly shaped cooling jacket is also known from Austrian Patent Publication No. AT 504 983 B1.

Japanese Patent Publication No. JP 2011-106 398 A1 discloses a cooling structure for an internal combustion engine, wherein the cooling jacket has a uniform height in the first and second engine transverse planes. The distance between the base and the top of the cooling jacket is only smaller in the region of a face side than in the other area.

WO 95/21323 A1 discloses a cooling system of a two-stroke internal combustion engine with several cylinders which are surrounded by a cooling jacket. The base of the cooling jacket is provided with an undulating profile and is flow-connected to a bottom coolant collector via U-shaped branch passages and vertical channel sections in the region of the engine transverse plane between two cylinders.

A cooling jacket for a crankcase is further known from Chinese Patent Publication No. CN 2 751 151 Y, whose cooling jacket base is formed in an undulating fashion as seen in a side view. The cooling jacket has a smaller distance from the cylinder head sealing plane in the region of a first engine transverse plane containing the cylinder axis than in the region of a second engine transverse plane between two cylinders. The cooling of thermally highly loaded regions is thus to be improved.

Relatively large cylinder deformations can especially occur in the region of the outer cylinders.

SUMMARY

It is the object of the invention to avoid this disadvantage and to reduce the deformations of the outer cylinders.

This is achieved in accordance with the invention in such a way that the cooling jacket has three different heights, wherein a third distance between the base of the cooling jacket and the top is smaller in at least one face-end region of the cooling jacket—preferably in the region of an engine longitudinal plane spanned by cylinder axes—than in the region of the second engine traverse plane between two adjacent cylinders.

Especially good results can be achieved if the distance between the base and the top in at least one face-end region is up to approximately 90%, preferably between approximately 50% and 70%, of the distance between the base and the top.

As a result of the constriction in the direction of the cylinder axis in the face-end region of a cooling jacket, cooling in this region can be reduced on the one hand and thus a constant temperature profile of the cylinder block is achieved, and the structure of the cylinder block can be stiffened decisively on the other hand and deformations can thus be reduced to a substantial extent.

DRAWINGS

The invention will be explained below in greater detail by reference to the drawings, wherein:

FIG. 1 illustrates a cooling jacket of a cylinder block in accordance with the invention in a side view in a first embodiment.

FIG. 2 illustrates the cooling jacket in a top view.

FIG. 3 illustrates the cooling jacket in a front view.

FIG. 4 illustrates a cooling jacket of a cylinder block in accordance with the invention in a side view in a second embodiment.

FIG. 5 illustrates fourth-order deformations for an outer cylinder in a known cylinder block and a cylinder block in accordance with the invention.

DESCRIPTION

FIGS. 1 to 3 illustrate a cooling jacket 1 of a cylinder block (not illustrated in closer detail) of an internal combustion engine with four cylinders 9, said cooling jacket 1 surrounding cylinder liners. As illustrated in the side view of FIG. 1, the base 2 of the cooling jacket 1 is shaped in an undulating fashion, so that the distance H of the base 2 increases and decreases from the cylinder head plane 3, as seen in the longitudinal direction of the cylinder block. In detail, the distance H in the region of a first engine transverse plane 5 containing the cylinder axis 4 is greater than in the region of a second engine transverse plane 7 extending between two cylinders, e.g., through the axes 6 of the cylinder head screw bores for the cylinder head screws.

The distance H2 between the base 2 and the top 3 of the cooling jacket 1 is smaller in the face-end region 8 of the outer cylinders 9, especially in the region of the engine longitudinal plane 13 spanned by the cylinder axes 4, than in the region of the second engine transverse planes 7 between the two cylinders 9. The distance H2 between the top 3 and the base 2 is approximately 50% to 80% of the maximum distance H in the face-end region 8 of the front side 1a, 1b between the top 3 and the base 2 in the region of the first engine transverse plane 5.

FIG. 4 and FIG. 6 illustrate a cooling jacket 1 for a three-cylinder internal combustion engine, in which the profile of a known cooling jacket is illustrated in FIG. 4 in comparison with the proposal in accordance with the invention with the dashed lines 10. A considerable improvement in the cylinder deformation of the fourth order in the region designated with reference numeral 11 of the deformation diagram shown in FIG. 5 is achieved by reducing the distance from H2′ to H2. The original deformation profile is designated with the dashed line 12′ in the deformation diagram of FIG. 5 and the deformation profile with reduced distance H2 is designated with reference numeral 12.

The stiffness of the cylinder block can be increased substantially by reducing the distance H2 between the top 3 and the base 2 of the cooling jacket 1 in the face-end region 8 of the cooling jacket 1 adjacent to the outer cylinders.

Claims

1-5. (canceled)

6. A liquid-cooled internal combustion engine, comprising: at least one cylinder block which has a cooling jacket and a plurality of cylinders, wherein: the cooling jacket has a base facing toward a crank chamber and a top facing toward a cylinder head sealing plane, the base having an undulating profile as seen from in a side view of the cylinder block, in which a first distance, as measured in a direction of a cylinder axis, between the base and the top in a first region of at least one first engine transverse plane which encompasses the cylinder axis, is greater than a second distance in a second region of at least one second engine transverse plane between adjacent cylinders; andthe cooling jacket has three different heights, in which a third distance between the base and the top is smaller in at least one face-end region of the cooling jacket than in the region of the second engine traverse plane between two adjacent cylinders.

7. The internal combustion engine of claim 6, wherein the third distance between the base and the top is smallest in at least one face-end region.

8. The internal combustion engine of claim 6, wherein the third distance between the base and the top in at least one face-end region is up to approximately 90% of the distance between the base and the top.

9. The internal combustion engine of claim 6, wherein the third distance between the base and the top in at least one face-end region is up to between approximately 50% and 70% of the distance between the base and the top.

10. The internal combustion engine of claim 6, wherein the third distance is formed in both face-end regions of the cylinder block between the base and the top.

11. The internal combustion engine of claim 6, wherein the base has a circular profile in at least one face-end region. preferably in both face-end regions (8).

12. The internal combustion engine of claim 6, wherein the base has a circular profile in both face-end regions.

13. A liquid-cooled internal combustion engine, comprising: at least one cylinder block having a plurality of cylinders; anda cooling jacket surrounding the at least one cylinder block, the cooling jacket having a base facing toward a crank chamber and which has an undulating profile, a top facing toward a cylinder head sealing plane, and a plurality of heights that differ from each other,wherein: a first distance, as measured in a direction of the cylinder axis, between the base and the top in a first region of at least one first engine transverse plane which encompasses the cylinder axis, is greater than a second distance in a second region of at least one second engine transverse plane between adjacent cylinders; anda third distance between the base and the top is smaller in at least one third region of an engine longitudinal plane spanned by cylinder axes, than in fourth region of the second engine traverse plane between adjacent cylinders.

14. The internal combustion engine of claim 13, wherein the third distance between the base and the top is smallest in at least one face-end region.

15. The internal combustion engine of claim 13, wherein the third distance between the base and the top in at least one face-end region is up to approximately 90% of the distance between the base and the top.

16. The internal combustion engine of claim 13, wherein the third distance between the base and the top in at least one face-end region is up to between approximately 50% and 70% of the distance between the base and the top.

17. The internal combustion engine of claim 13, wherein the third distance is formed in both face-end regions of the cylinder block between the base and the top.

18. The internal combustion engine of claim 13, wherein the base has a circular profile in at least one face-end region. preferably in both face-end regions.

19. The internal combustion engine of claim 13, wherein the base has a circular profile in both face-end regions.