Technical Field
[0001] This disclosure relates generally to engines of vehicles and machines, for instance
generators. This disclosure relates particularly to coolant flow in engines of vehicles.
Background
[0002] Cooling of an internal combustion engine may be needed due to high temperatures which
may be generated in the engine. Some of the heat generated in the combustion engine
may be transferred to the walls of the engine. The high temperatures may damage parts
of the engine or the materials within the engine.
[0003] During operation of an engine, the engine may be kept in operative mode by using
a coolant. The coolant may transport the heat away from a heat source in order to
prevent overheating of the engine. Some engines may have an oil cooler to cool the
engine oil. Heat from the engine oil may be transferred to the coolant for dissipation
of heat through a radiator.
[0004] An internal combustion engine may include an engine block. An engine block may be
machine cast and are usually made from cast iron or, in modern engines, aluminium
and magnesium. The engine block may contain cylindrically bored holes to accommodate
the pistons of a multi-cylinder combustion engine. The engine block may comprise points
of attachments or recesses for the attachment of engine components for instance the
cylinder head, crankcase, engine mounts, drive housing, engine ancillaries and the
oil cooler. The engine block may also comprise passages for coolants and lubricants
and may have a cast pocket to receive the oil cooler.
[0005] Generally the size and shape of the points of attachments and recesses within the
engine block may not be easily changed, as machining facilities would require extensive
modification. Hence, an oil cooler and the cast pocket in the engine block may be
produced with assembly clearances to prevent the oil cooler from fouling on the cast
pocket during assembly of the engine block. However, the assembly clearance permits
an easy flow of coolant away from the oil cooler in an assembled engine and the transfer
of heat from the oil cooler to the coolant may not be optimal.
[0006] The present disclosure is directed, at least in part, to improving or overcoming
one or more aspects of the prior art system.
Brief Summary of the Invention
[0007] In a first aspect, the present disclosure describes an arrangement to control a flow
in an engine comprising a coolant cavity having a coolant inlet and a coolant outlet
for flow of a coolant; an oil cooler matrix positioned in the coolant cavity and having
a channel for circulation of oil; and at least one baffle arranged in the coolant
cavity to direct the flow of the coolant through the coolant cavity.
[0008] In a second aspect, the present disclosure describes a method of controlling coolant
flow in an engine comprising circulating a coolant through a coolant cavity, the coolant
cavity having an oil cooler matrix; and directing flow of the coolant through the
coolant cavity by a baffle arranged in the coolant cavity.
[0009] Other features and advantages of the present disclosure will be apparent from the
following description of various embodiments, when read together with the accompanying
drawings.
Brief Description of the Drawings
[0010] The foregoing and other features and advantages of the present disclosure will be
more fully understood from the following description of various embodiments, when
read together with the accompanying drawings, in which:
Fig. 1 is a schematic representation of an engine block according to the present disclosure;
Fig. 2 is a isometric view of an oil cooler matrix according to the present disclosure;
Fig. 3 is a first embodiment of a baffle according to the present disclosure;
Fig. 4 is a second embodiment of a baffle according to the present disclosure;
Fig. 5 is schematic representation of a first embodiment of a baffle arrangement in
the coolant cavity;
Fig. 6 is schematic representation of a second embodiment of a baffle arrangement
in the coolant cavity;
Fig. 7 is schematic representation of a third embodiment of a baffle arrangement in
the coolant cavity; and
Fig. 8 is schematic representation of a fourth embodiment of a baffle arrangement
in the coolant cavity.
Detailed Description
[0011] This disclosure generally relates to an arrangement to control coolant flow in an
engine.
[0012] An arrangement
10 of the present disclosure may comprise a coolant cavity
14, an oil cooler matrix
16 and a baffle
18.
[0013] Fig. 1 illustrates an engine block
12. Engine block
12 may be machined cast and may have portions to receive engine components. The engine
block
12 may be assembled with the engine components. The assembled engine block
12 may be used to assemble an engine, for instance a vehicle engine. Engine block
12 may have the coolant cavity
14 machined thereon and may include a coolant rail
20 for passage of coolant fluid.
[0014] Coolant cavity
14 may be formed, for instance through machine casting, according to predetermined requirements.
Coolant cavity
14 may be of a suitable size and shape to accommodate the oil cooler matrix
16. Coolant cavity
14 may be substantially rectangular and may have a longitudinal axis. The coolant cavity
14 may have an opening
22 to receive the oil cooler matrix
16. The periphery of the opening
22 may be a contact portion
24 which may include holes
26 for locating and mounting the oil cooler matrix
16 to the engine block
12.
[0015] Opposite the opening
22, the coolant cavity
14 may have a side wall
28. The side wall
28 may have recesses
30 to accommodate protrusions from the oil cooler matrix
16. Circumventing the side wall
28 may be a enclosure wall
32. In an assembled engine block
12 the oil cooler matrix
16 may be spaced from the side wall
28 and the enclosure wall
32. A gap may be formed between the oil cooler matrix
16 and the enclosure wall
32. In an assembled engine, the coolant may flow through the gap.
[0016] Coolant rail
20 may be formed, for instance through machine casting, according to predetermined requirements.
Coolant rail
20 may be a part of continuous coolant circuit. A portion of the coolant rail
20 may lead from the coolant cavity
14 to a radiator and another portion of the coolant rail
20 may lead from the radiator to the coolant cavity.
[0017] In an assembled engine, the coolant rail
20 may carry the coolant to and away from the coolant cavity
14. Coolant may be heated in the coolant cavity and coolant rail
20 may carry the heated coolant to a radiator for dissipation of the heat. Coolant rail
20 may return the cooled coolant to the coolant cavity
14. A pump may be connected to the coolant circuit and may propel the flow of coolant
through the coolant rail
20 and coolant cavity
14.
[0018] Coolant rail
20 may be connected to the opposite ends of the coolant cavity
14. At an end of the coolant cavity
14 the coolant rail
20 may form a coolant inlet
34 at enclosure wall
32. At an opposite end of the coolant cavity
14 the coolant rail
20 may form a coolant outlet
36 at enclosure wall
32. In an assembled engine coolant may enter the coolant cavity
14 through the coolant inlet 34 flow through the coolant cavity
14 and may exit through the coolant outlet
36.
[0019] Coolant inlet
34 and coolant outlet
36 may be formed, for instance through machine casting, according to predetermined requirements.
Coolant inlet
34 and coolant outlet
36 may be located along the longitudinal axis of the coolant cavity
14.
[0020] Fig. 2 illustrates an oil cooler matrix
16. Oil cooler matrix
16 may be supported on a frame
38. Frame
38 may include a reciprocal contact portion
40 to abut the contact portion
24 at the periphery of opening
22. The reciprocal contact portion
40 may be formed in the same shape and size as the contact portion
24. The reciprocal contact portion
40 may have reciprocal holes
42 that may correspond to holes
26 on the contact portion
24. Frame
38 may include locating fasteners
44. Locating fasteners
44 may assist in placement of frame
38 onto engine block
12. In an assembled engine block
12 the reciprocal contact portion
40 and the contact portion
24 may form a seal to prevent leakage of coolant and oil.
[0021] Oil cooler matrix
16 may include internally disposed channels
46a and
46b for flow of engine oil to and from the oil cooler matrix
16. In an assembled engine block
12, channels
46a and
46b may lead from the oil cooler matrix 16 into the engine block
12.
[0022] In an assembled engine, oil may be carried to the oil cooler matrix
16 for dissipation of heat to the coolant in the coolant cavity
14. Channel
46a may carry heated oil into the oil cooler matrix
16 and channel
46b may return the cooled oiled from the oil cooler matrix
16.
[0023] Oil cooler matrix
16 may comprise a series of hollow plates
48. Each plate
48 may be substantially rectangular with a linear side edges
50 and rounded terminal edges
52 and may have a thickness of some millimeters, for instance 3 mm. In an assembled
engine, block
12 the longitudinal axis of the oil cooler matrix
16 may be aligned with the longitudinal axis of the coolant cavity
14. Terminal edges
52 may face coolant inlet
34 and coolant outlet
36 at enclosure wall
32.
[0024] Channels
46a and
46b may connect plates
48. Each plate
48 may be spaced from one another and may communicate be positioned at terminal edges
52. Channel
46a may be positioned at a terminal edge
52 and the channel
46b may be positioned at opposite terminal edge
52. Oil may flow through plates comprised in oil cooler matrix
16 may vary according to requirements. In one embodiment, the number of plates may be
between 9 and
13 plates.
[0025] In an assembled engine, coolant flow through the coolant cavity
14 may be directed at the oil cooler matrix
16. The coolant may be directed through the oil cooler matrix
16 between plates
48.
[0026] In another embodiment, oil cooler matrix
16 may comprise of a solid body internally segmented by plates or channels.
[0027] In a further embodiment, oil cooler matrix
16 may comprise of a solid body having clefts or recesses on the body.
[0028] Baffle
18 may be positioned in the coolant cavity
14. The baffle
18 may be positioned along the enclosure wall
32 in the cavity. Baffle
18 may be mounted to a position along the enclosure wall
32. In another embodiment the baffle may be mounted to the side wall
28.
[0029] In another embodiment baffle
18 may be mounted to the oil cooler matrix
16. Baffle
18 may be mounted to a position along the side edges
50 or the terminal edges
52 of the oil cooler matrix
16.
[0030] Baffle
18 may be mounted mechanically for instance by rivets or mechanical coupling. Baffle
18 may be mounted chemically, for instance by adhesives. Baffle
18 may be composed of suitable heat resistant material and may be composed of resilient
material for instance, rubber.
[0031] In an embodiment, baffle
18 may be flexible. A flexible baffle
18 may facilitate mounting thereof to the coolant cavity
14 or the oil cooler matrix
16. The flexible baffle
18 may be again composed of rubber, or plastic. During assembly of the engine block
12, a flexible baffle
18 may deform and thereby allow an efficient assembly.
[0032] In the assembled engine block
12, baffle
18 may be located between the oil cooler matrix
16 and the walls of coolant cavity
14. Baffle
18 may be located between a side edge
50 or a terminal edge
52 of the oil cooler matrix
16 and the enclosure wall
32.
[0033] In the assembled engine, baffle
18 may direct the flow of the coolant through the coolant cavity. Baffle
18 may direct the flow of the coolant at the oil cooler matrix
16.
[0034] Fig. 3 illustrates a first embodiment of baffle
18. Baffle
18 may comprise an arcuate portion 54 and a base portion
56. Arcuate portion
54 may have a support end
58 and tapered end
60. Support end
58 may connect the arcuate portion
54 to the base portion
56. Width of tapered end
60 may substantially equal to the height of the oil cooler matrix
16.
[0035] Baffle
18 may be mounted to the coolant cavity
14 through the base portion
56. Base portion
56 may comprise rivet holes
62 and a mounting plate
64 for mechanical attachment to the coolant cavity
14. In an embodiment base portion
56 may be bonded to the coolant cavity
14.
[0036] In an assembled engine block
12, base portion
56 may be mounted to enclosure wall
32 of the coolant cavity
14 and tapered end
60 of arcuate portion
54 may abut the oil cooler matrix
16.
[0037] In another embodiment, tapered end
60 of arcuate portion
54 may be mounted to the oil cooler matrix
16, for instance by adhesive or mechanical coupling, and base portion
56 may abut enclosure wall
32.
[0038] In an assembled engine, arcuate portion
54 may direct the flow of coolant. Coolant flowing through coolant cavity
14 may impact the arcuate portion
54 and the flow may be diverted towards oil cooler matrix
16.
[0039] Fig. 4 illustrates a second embodiment of baffle
18. Baffle
18 may comprise a guide portion
66, a link portion
68 and a base portion
70. Link portion
68 may connect the guide portion
66 to the base portion
70. Width of guide portion
66 may be substantially greater than the width of the link portion
68. Width of guide portion
66 may substantially equal to the height of the oil cooler matrix
16.
[0040] Baffle
18 may be mounted to the coolant cavity
14 through the base portion
70. Base portion
70 may be mechanically or chemically attached to the coolant cavity
14.
[0041] In an assembled engine block
12, base portion
70 may be mounted to enclosure wall
32 of the coolant cavity
14 and guide portion
66 may abut the oil cooler matrix
16.
[0042] In another embodiment, guide portion
66 may be mounted to the oil cooler matrix
16, for instance by adhesive or mechanical coupling, and base portion
70 may abut enclosure wall
32.
[0043] Link portion
68 may be supported from enclosure wall
32, for instance a projection from the enclosure wall
32 or from the link portion
68.
[0044] In an assembled engine, guide portion
66 may direct the flow of coolant. Coolant flowing through coolant cavity
14 may abut the guide portion
66 and the flow may be diverted towards oil cooler matrix
16.
[0045] In a further embodiment, baffle
18 may be a flat panel which may be mounted to the side wall
28, enclosure wall
32 or oil cooler matrix
16. In an assembled engine, the flat panel may direct the flow of coolant. Coolant flowing
through coolant cavity
14 may abut the flat panel and the flow may be diverted towards oil cooler matrix
16.
[0046] The baffle
18 may be suitably arranged to direct the flow of coolant through the coolant cavity
14 in an assembled engine. In further embodiments, more than one baffle may be provide
to direct the flow of coolant through the coolant cavity
14.
[0047] Baffles
18 may be suitably provided. Baffles
18 may be positioned to direct the flow of coolant at the oil cooler matrix
16. Baffles
18 may be mounted to the oil cooler matrix
16 or to the coolant cavity
14 as described in the foregoing paragraphs.
[0048] Fig. 5 illustrates a first embodiment of a baffle arrangement in an assembled engine.
A first baffle
18 and a second baffle
18 may be positioned between side edge
50 of the oil cooler matrix
16 and the enclosure wall
32 of coolant cavity
14. The baffles
18 may be located proximate to the coolant inlet
34. The baffles
18 may be located proximate to a terminal edge
52 facing the coolant inlet
34.
[0049] Coolant flowing from the coolant inlet
34 may flow towards the oil cooler matrix
16 and into gaps in the coolant cavity
14 between the oil cooler matrix
16 and the enclosure wall
32.
[0050] Baffles
18 located between the oil cooler matrix
16 and the enclosure wall
32 may direct the coolant flow from the gaps to the oil cooler matrix
16. Coolant may be directed by the baffles to flow through the oil cooler matrix
16 comprising a series of plates
48. Coolant may be directed to flow between plates
48.
[0051] Fig. 6 illustrates a second embodiment of a baffle arrangement in an assembled engine.
A first baffle
18 and a second baffle
18 may be positioned between terminal edge
52 of the oil cooler matrix
16 and the enclosure wall
32 of coolant cavity
14. The baffles
18 may be located proximate to the coolant inlet
34. The baffles
18 may be located between terminal edge
52 and the coolant inlet
34.
[0052] Coolant flowing from the coolant inlet
34 may flow towards baffles
18. Baffles
18 may direct the coolant flow at the oil cooler matrix
16. Coolant may be directed by the baffles to flow through the oil cooler matrix
16 comprising a series of plates
48. Coolant may be directed to flow between plates
48.
[0053] Fig. 7 illustrates a third embodiment of a baffle arrangement in an assembled engine.
A first baffle
18 and a second baffle
18 may be positioned between side edge
50 of the oil cooler matrix
16 and the enclosure wall
32 of coolant cavity
14. The baffles
18 may be located proximate to the coolant inlet
34. The baffles
18 may be located proximate to a terminal edge
52 facing the coolant inlet
34. Baffles
18 may extend along side edges
50 towards the opposite terminal edge
52. The opposite terminal edge
34 may face coolant outlet
36.
[0054] Coolant flowing from the coolant inlet
34 may flow towards the oil cooler matrix
16 and into gaps in the coolant cavity
14 between the oil cooler matrix
16 and the enclosure wall
32.
[0055] Baffles
18 located between the oil cooler matrix
16 and the enclosure wall
32 direct the coolant flow from the gaps to the oil cooler matrix
16. Coolant may be directed by the baffles to flow through the oil cooler matrix
16 comprising a series of plates
48. Coolant may be directed to flow between plates
48. Coolant flow between the plates
48 may be maintained by the extended baffles
18.
[0056] Fig. 8 illustrates a fourth embodiment of a baffle arrangement in an assembled engine.
A first baffle
18 and a second baffle
18 may be positioned between side edge
50 of the oil cooler matrix
16 and the enclosure wall
32 of coolant cavity
14. The first and second baffles
18 may be located proximate to the coolant inlet
34. The first and second baffles
18 may be located proximate to a terminal edge
52 facing the coolant inlet
34.
[0057] A third and fourth baffles
18a may be positioned between side edge
50 of the oil cooler matrix
16 and the enclosure wall
32 of coolant cavity
14. The third and fourth baffles
18a may be located proximate to the coolant outlet
36. The third and fourth baffles
18a may be located proximate to a terminal edge
52 facing the coolant outlet
36.
[0058] Coolant flowing from the coolant inlet
34 may flow towards the oil cooler matrix
16 and into gaps in the coolant cavity
14 between the oil cooler matrix
16 and the enclosure wall
32.
[0059] First and second baffles
18 located between the oil cooler matrix
16 and the enclosure wall
32 direct the coolant flow from the gaps to the oil cooler matrix
16. Coolant may be directed by the first and second baffles
18 to flow through the oil cooler matrix
16 comprising a series of plates
48. Coolant may be directed to flow between plates
48.
[0060] Coolant may flow through the plates
48 and may flow towards the gaps in the coolant cavity
14 between the oil cooler matrix
16 and the enclosure wall
32. Coolant flow may be diverted by the third and fourth baffles
18a to the oil cooler matrix
16.
Industrial Applicability
[0061] This disclosure describes at least one baffle
18 for control of coolant flow through a coolant cavity
14.
[0062] Heat transfer from oil in the oil cooler matrix
16 may depend on the flow rate and flow path of the coolant. A greater heat transfer
may occur with an increased flow rate at the oil cooler matrix
16. A greater heat transfer may occur with a coolant flowing through the oil cooler
matrix
16 between plates
48. Further heat transfer may be achieved with an increased coolant flow rate between
the plates 48.
[0063] The arrangement of baffle
18 and oil cooler matrix
16 in a coolant cavity may be used in engines of vehicles to achieve increased heat
transfer rates for the engine oil to the coolant.
[0064] Tests have shown that the volume of coolant flowing between the plates may be increased
by baffles. A baseline cooler has shown slow moving flow over much of the surface,
with some areas of higher velocity flow near to the edges of the plates. The addition
of baffles has shown jets of higher velocity flow extending over much of the plates.
Results have been compared indicating a noticeable increase of flow rate. Particularly,
a baseline model showed a low flow rate at the entry to the cooler, which reduced
gradually along the cooler length. A model with baffles according to the disclosure
has shown greatly increased flow at the upstream end of the cooler, which decreases
as the flow redistributes and enters the gaps around the cooler.
[0065] Additionally, a baseline cooler generally shows fairly uniform Heat Transfer Coefficient
(HTC) on plates of the oil cooler matrix over the surfaces of the plates. The HTCs
are raised near the front of the cooler and along the edges, as high velocity coolant
enters the cooler. The jets of high velocity fluid generated by the baffles create
regions with very high HTC values. The jets dissipate as they pass through the cooler,
significantly increasing the HTCs over the rear part of the cooler.
[0066] The industrial applicability of the baffle arrangement for control of coolant flow
through a coolant cavity 14 as described herein will have been readily appreciated
from the foregoing discussion.
[0067] Accordingly, this disclosure includes all modifications and equivalents of the subject
matter recited in the claims in any claim are followed by references signs, the reference
signs have been included for the sole purpose of increasing the intelligibility of
the claims and accordingly, neither the reference signs nor their absence have any
limiting effect on the technical features as described above or on the scope of any
claim elements.
[0068] One skilled in the art will realise the disclosure may be embodied in other specific
forms without departing from the disclosure or essential characteristics thereof.
The foregoing embodiments are therefore to be considered in all respects illustrative
rather than limiting of the disclosure described herein. Scope of the invention is
thus indicated by the appended claims, rather than the foregoing description, and
all changes that come within the meaning and range of equivalence of the claims are
therefore intended to be embraced therein.