U.S. patent number 3,745,980 [Application Number 05/147,812] was granted by the patent office on 1973-07-17 for cylinder sleeve system for high output engine.
Invention is credited to Eugene Eisenberg, Frank J. Pekar, Jr..
United States Patent |
3,745,980 |
Pekar, Jr. , et al. |
July 17, 1973 |
CYLINDER SLEEVE SYSTEM FOR HIGH OUTPUT ENGINE
Abstract
A cylinder sleeve system for the cylinder block of a high output
internal combustion engine includes a circumferential recess in the
upper region of each cylinder bore wall that forms with a cylinder
sleeve fitted in the bore an annular coolant chamber surrounding
the upper region of the sleeve. The chamber has a shallow radial
depth, preferably of constant cross section, so as to cause high,
generally uniform velocity coolant flow through the chamber,
thereby promoting rapid cooling of the upper region. Coolant
discharged from the chamber flows to a coolant jacket surrounding
the lower region of the cylinder sleeve, where it circulates at
reduced velocity to effect slower cooling of the lower region. The
coolant in the upper chamber is thus in direct contact with the
sleeve while that in the coolant jacket is contained against such
direct contact. The recess is sized and located such that the
cylinder sleeve is directly supported by the cylinder bore wall
over approximately the lower three-fourths of its length. This
configuration permits sleeves of reduced wall thickness to be
used.
Inventors: |
Pekar, Jr.; Frank J.
(Hagerstown, MD), Eisenberg; Eugene (Hagerstown, MD) |
Family
ID: |
22522998 |
Appl.
No.: |
05/147,812 |
Filed: |
May 28, 1971 |
Current U.S.
Class: |
123/41.74;
123/41.72; 92/144 |
Current CPC
Class: |
F02F
1/14 (20130101); F16J 10/04 (20130101); F02F
1/16 (20130101) |
Current International
Class: |
F16J
10/04 (20060101); F16J 10/00 (20060101); F02F
1/02 (20060101); F02F 1/14 (20060101); F02F
1/16 (20060101); F02b 075/18 () |
Field of
Search: |
;123/41.72,41.74,41.79,41.81 ;92/144 ;165/154,155 |
References Cited
[Referenced By]
U.S. Patent Documents
Foreign Patent Documents
Primary Examiner: Myhre; Charles J.
Assistant Examiner: Grossman; Barry
Claims
We claim:
1. A cylinder block for an internal combustion engine,
comprising:
means defining a plurality of vertically extending in-line cylinder
bores adapted for the combustion of a fuel-air mixture in the upper
regions thereof,
a cylinder sleeve located in each bore in snug engagement with the
bore wall, the bore wall extending over substantially the full
length and around the full circumference of the sleeve,
means forming a circumferential recess in the wall of each cylinder
bore opposite the upper region of the sleeve, the recess extending
fully around the sleeve and defining with the opposed wall of the
sleeve an annular chamber surrounding the upper sleeve region,
a coolant inlet to each chamber,
a coolant outlet from each chamber, and
means defining a coolant jacket surrounding the lower regions of
the cylinder sleeves, whereby coolant delivered to the upper
chambers flows therethrough in direct contact with the sleeve
walls, thereby promoting rapid cooling over the upper region of the
sleeves, and coolant delivered to the jacket is contained against
direct contact with the sleeve walls, thereby promoting slower
cooling over the lower regions of the sleeves.
2. A cylinder block according to claim 1 wherein the radial depth
of each upper chamber is smaller than that of the coolant jacket so
as to provide a higher velocity coolant flow in the upper chamber
than in the jacket.
3. A cylinder block according to claim 2 wherein the outlet from
each upper chamber communicates with the coolant jacket, whereby
the coolant delivered to the jacket is preheated by passage through
the upper chamber prior to entering the jacket.
4. A cylinder block according to claim 3 wherein each upper chamber
has a substantially constant cross section over its full
circumferential extent whereby the coolant flows therethrough at a
generally uniform velocity.
5. A cylinder block according to claim 1 wherein the lower end of
each recess is spaced from the upper end of the sleeve by a
distance approximately one-quarter the length of the sleeve,
whereby each sleeve is directly supported by the cylinder bore wall
over approximately three-quarters of its length.
6. A cylinder block according to claim 1 further comprising means
in each cylinder bore defining a seal for preventing leakage of
coolant from the upper chamber along the interface between the
lower region of the sleeve and the cylinder bore wall.
7. A cylinder block according to claim 1 further comprising:
a coolant gallery extending along one side of the cylinder bores in
the direction of alignment thereof, and wherein the inlet to each
annular upper chamber is located on the gallery side of the chamber
in communication with the gallery for receiving a coolant flow
therefrom.
8. A cylinder block according to claim 7 wherein the outlet from
each annular chamber is located on the opposite side of the chamber
from the inlet, whereby the coolant flows through the chamber in a
direction generally transverse to the direction of alignment of the
cylinder bores.
9. A cylinder sleeve assembly comprising:
a block having at least one cylinder bore formed therein adapted
for the combustion of a fuel-air mixture in the upper region
thereof,
a cylinder sleeve located in the bore in snug engagement with each
bore wall, the bore wall extending over substantially the full
length and around the full circumference of the sleeve,
means forming a circumferential recess in each bore wall opposite
the upper region of the sleeve, the recess extending fully around
the sleeve and defining with the opposed wall of the sleeve an
annular chamber surrounding the upper sleeve region,
a coolant inlet to each chamber,
a coolant outlet from each chamber, and
means, including an outer wall spaced from each cylinder bore wall,
defining a coolant jacket surrounding the lower region of each
sleeve, whereby coolant delivered to each upper chamber flows
therethrough in direct contact with the sleeve wall, thereby
promoting rapid cooling of the upper region of the sleeve, and
coolant delivered to the jacket is contained against direct contact
with the sleeve wall, thereby promoting slower cooling of the lower
region of the sleeve.
10. A cylinder sleeve assembly according to claim 9 wherein the
radial depth of each upper chamber is smaller than that of the
coolant jacket so as to provide a higher velocity coolant flow in
the upper chamber than in the jacket.
11. A cylinder sleeve assembly according to claim 10 wherein the
outlet from each upper chamber communicates with the coolant
jacket, whereby the coolant delivered to the jacket is preheated by
passage through the upper chamber prior to entering the jacket.
12. A cylinder sleeve assembly according to claim 11 wherein each
upper chamber has a substantially constant cross section over its
full circumferential extent, whereby the coolant flows therethrough
at a generally uniform velocity.
13. A cylinder sleeve assembly according to claim 9 wherein the
lower end of each recess is spaced from the upper end of the sleeve
by a distance approximately one-quarter the length of the sleeve,
whereby the sleeve is directly supported by the cyinder bore wall
over approximately three-quarters of its length.
14. A cylinder sleeve assembly according to claim 9 further
comprising means defining a seal for preventing leakage of coolant
from the upper chamber along the interface between the lower region
of the sleeve and the cylinder bore wall.
15. A cylinder block according to claim 8 wherein each upper
chamber has a substantially constant cross section over its full
circumferential extent, whereby the coolant flows therethrough at
generally a uniform velocity.
Description
BACKGROUND OF THE INVENTION
The present invention relates to an improved construction for the
cylinder block of a high output internal combustion engine, and
particularly concerns a cylinder sleeve system for use in such a
block which enhances cooling of vital engine parts while allowing
cylinder centerline spacing to be reduced without sacrifice in
block rigidity.
Due to unfavorable wear conditions in the cylinder bores of heavy
duty internal combustion engines, it has been found necessary to
abandon a piston running in direct contact with the cylinder block
and to adopt an improved construction where the piston runs in a
sleeve, or liner, located within the bore. Two types of sleeve
constructions have been used; namely, a dry-sleeve construction, in
which the coolant does not directly contact the sleeve wall, and a
wet-sleeve construction, wherein it does.
The use of such cylinder sleeves, whether of the wet or dry type,
affords advantages in respect of increased resistance to wear
inasmuch as the sleeves may be centrifugally cast to yield a
significantly more dense and harder bearing surface than can be
cast in the supporting cylinder block. Since the sleeves are
readily removable from the block, there is the added advanatge of
enhanced serviceability.
With high output engines, the wet-sleeve construction is especially
desired because of its superior cooling capability, particularly
with regard to the piston and piston rings. However, the use of
such sleeves leads to a detrimental increase in the cylinder
centerline spacing and thus of the overall size of the engine. The
greater distance between cylinder centerlines is required to
achieve satisfactory block strength and rigidity and sleeve
resistance to cavitation damage, and results chiefly from increases
in both the cylinder sleeve thickness and block wall thickness
attendant to the accomplishment of these requirements.
The present invention overcomes these and other objectionable
aspects of the prior art.
SUMMARY OF THE INVENTION
In a preferred embodiment, the sleeve system of the invention
includes a recess formed in the cylinder bore wall opposite the
upper, i.e., the hottest, region of the sleeve which defines with
the opposed sleeve wall an annular chamber for directing coolant
flow around the upper sleeve region. Preferably the chamber is
given a shallow radial depth, so that the coolant flows through the
chamber at high velocity in contact with the sleeve. The coolant
exiting from the chamber, now heated, is received by a jacket
formed around the lower region of the sleeve, where it is
circulated more slowly and contained against direct contact with
the sleeve wall. Cooling of the lower sleeve region therefore goes
forward at a retarded rate relative to that in the upper region. By
this arrangement, heat transfer is carried out most efficiently and
most rapidly at the hottest, i.e., combustion, region of the
cylinder sleeve where maximum cooling is required, but is reduced
over the lower region, which receives little of the heat load from
combustion. The result is that a more uniform temperature
distribution between the upper and lower sleeve regions is
obtained.
As another feature of the invention, the upper chamber desirably
has a constant cross-section throughout its length, the velocity of
the coolant thereby remaining generally uniform as it circulates
around the cylinder sleeve. This further improves cooling
characteristics by promoting uniform temperature distributions
circumferentially of the sleeve. Furthermore, the recess is sized
and located such that the sleeve is directly supported by the
cylinder bore wall over approximately three-fourths the length of
the sleeve. This load-bearing support allows the sleeve to be made
thinner in the upper region than comparable wet sleeves of
conventional design, which further enhances cooling of the piston
and the piston rings, without cavitation damage. Block walls of
reduced thickness may also be used, notwithstanding that the
advantages of a wet-sleeve construction in respect of cooling is
obtained at the upper region of the cylinder, because the
combustion loads are borne both by the cylinder bore wall and the
outer coolant jacket wall.
BRIEF DESCRIPTION OF THE DRAWINGS
For a better understanding of the invention, reference may be made
to the following description of an exemplary embodiment, taken in
conjunction with the figures of the accompanying drawings, in
which:
FIG. 1 is an end elevational view, in section, of a
multiple-cylinder engine block incorporating the improved cylinder
sleeve system of the invention; and
FIG. 2 is a partial side elevational view, in section, of the
cylinder block of FIG. 1.
DESCRIPTION OF AN EXEMPLARY EMBODIMENT
For convenience of description and illustration, the novel cylinder
sleeve system of the invention is described and shown herein in
connection with a cylinder block having a plurality of in-line
cylinder bores, and where the coolant is assumed to be water. It
will be understood, however, that like advantages in respect of
improved cooling characteristics and savings in engine weight and
size are afforded by the invention with other cylinder
arrangements, and whether one or a plurality of cylinders are
provided. In a similar vein, although the coolant has been referred
to herein as water, it will be understood that any suitable coolant
may be used.
As illustrated in FIGS. 1 and 2, the cylinder block of 10 of a high
output internal combustion engine typically is formed with a
plurality of in-line cylinder bores 12 that extend vertically
between a cylinder head 14 at their upper ends and a crankcase 16
at their lower ends. A cylinder sleeve 18, i.e., a liner, is
located in each bore 12 in snug engagement with the bore wall 20,
and is securely held in place by means of a circumferential flange
21 that is received in a cooperating recess 22 in the bore wall. A
groove 24 may be provided in the upper surface of the flange 21 for
sealing cooperation with the head 14 upon its attachment to the
block 10.
In a vertically oriented cylinder block ofthe type portrayed,
combustion of course goes forward in the upper regions of the
cylinders, and it is these regions which require the greatest
degree of cooling. To that end, a recess 26 is formed in the upper
region of each bore wall 20. Preferably, the recess is of a
relatively shallow but substantially uniform radial depth
throughout its circumferential extent. It forms, therefore, an
annular chamber 28 with the opposed wall of the sleeve 18 of
generally constant cross section and relatively small radial width.
The chamber 28 is formed, preferably on opposed sides, with an
inlet 30 and an outlet 32 for receiving and discharging,
respectively, a flow of cooling water. A seal ring 34 of
appropriate design is positioned at the lower end of the recess 26
to prevent leakage of the water along the interface between the
lower region of the sleeve and the facing bore wall 20.
A water gallery 36, communicating with the water pump (not shown)
through a fitting 38, extends along one side of the cylinder bores
12 in the direction of their alignment, with the inlet 30 to each
chamber 28 opening directly into the gallery 36. A flow of cool
water is thus delivered from the gallery 36 to the chambers 28,
where, by virtue of the shallow radial depth of the chamber, it
flows at a controlled high velocity around the sleeves 18 in a
direction generally transverse to the direction of alignment of the
bores 12. Since the chambers 28 are of constant cross section, the
velocity of the water flowing therethrough remains generally
uniform, hence promoting uniform temperature distributions
circumferentially of the sleeves 18. Moreover, the shallow radial
configuration of the chambers 28 utilized to achieve the high
velocity flow inherently reduces the block wall thickness required
as compared to conventional cast water spaces typically used in wet
sleeve systems. As illustrated in FIG. 2, this contributes to
closer cylinder centerline spacing.
Upon leaving the outlet 32 from the chambers 28, the water, now
heated as a result of heat transferred to it from the upper regions
of the sleeves, enters the upper end of a common water jacket 40
formed between adjacent cylinder bore walls 20 (see FIG. 2) and the
sidewalls 42 and 44 (see FIG. 1) of the block 10. The water jacket
40 is sized to have a cross section significantly larger than that
of the chambers 28, so that the velocity of the water within the
jacket 40 is considerably reduced from that in the chambers 28.
This feature, together with the use of the already heated water
exiting from the chambers 28 as the coolant for the lower regions
of the sleeve 18, results in a much slower rate of heat dissipation
in those regions. As the lower regions receive very little of the
heat load from combustion, not only is a high heat flow rate not
required, but slowing or retardation of the heat flow in the lower
regions aids in attenuating temperature gradients between the upper
and lower sleeve regions, with consequent alleviation of thermal
stresses. It will be appreciated also that this dry-sleeve type
construction, i.e., a metal-to-metal interface, over the lower
sleeve regions contains the cooling water against direct contact
with the sleeves 18, and hence further retards heat flow to it from
the sleeves.
The water leaves the water jacket 40 through passages 46 to enter
the cylinder head 14 for ultimate return to the water pump. If
desired, a direct connection 48 may be made between the gallery 36
and the cylinder head 14 for cooling of the hotter regions of the
head.
The axial extent of the chambers 28 is sized to afford the desired
degree of cooling for a given application. According to a preferred
configuration, the lower end of each recess 26 is spaced below the
top of the sleeve by a distance approximately one-fourth the length
of the sleeve, or, in other words, the lower three-fourths of the
sleeve is supported directly by the bore wall 20. The load-bearing
support given to the sleeves 18 by this arrangement allows them to
be made thinner at the upper region than is practicable, from the
standpoint of cavitation damage, with conventional wet-sleeve
designs. Thinning of the upper sleeve region in this manner not
only allows a further reduction in cylinder centerline spacing, but
additionally enhances cooling of the piston and piston rings. For
example, with the sleeve 18 supported in the foregoing manner over
approximately three-quarters of its length, the thickness of the
sleeve 18 may be reduced to approximately two-thirds of that of a
comparable wet sleeve without encountering damage due to
cavitation.
The foregoing wet-sleeve/dry-sleeve construction affords the still
further advantage of allowing the cylinder block wall thicknesses
between sleeves to be reduced without loss of rigidity of the
cylinder block 10 becuase the combustion loads are taken in large
part by both the associated bore wall 20 and the outer walls 42 and
44 of the water jacket. This is to be contrasted with the normal
wet-sleeve design, where only an outer water jacket wall is
provided to receive loads from the sleeve.
Although the invention has been described with reference to a
specific embodiment thereof, many modifications and variations may
be made by one skilled in the art without departing from the
inventive concepts disclosed. Accordingly, all such modifications
and variations are intended to be included within the spirit and
scope of the appended claims.
* * * * *