Cross-reference to related applications
Technical field
[0002] This invention relates to a supercharging compressor for an internal combustion engine,
in particular for vehicle traction.
Background
[0003] In the field of vehicles with internal combustion engines, the latter may be supercharged,
that is, supplied with combustive air that is compressed by means of a compressor,
actuated by an electric motor, or by a turbine arranged along the exhaust gas line
coming out of the engine.
[0004] Compression, as is well known, causes an increase in air temperature. This increase
in temperature can be problematic, particularly with regard to the reduction in volumetric
efficiency in the combustion chambers of internal combustion engines, when compressing
the air inside them, and with regard to the risks of knocking in petrol thermal engines.
[0005] To overcome these drawbacks, as is well known, the combustive air coming out of the
supercharging compressor is cooled by means of a heat exchanger, generally referred
to as an "intercooler".
[0006] For internal combustion engines having a high specific power output, intercoolers
and supercharging compressors tend to have a large footprint, which can make space
design in the vehicle engine compartment problematic.
[0007] Therefore, there is a need to refine the known solutions just described, even though
they are widely used, in such a way that the size and/or mechanical power absorbed
by the supercharging compressor can be reduced, and/or in such a way that the overall
dimensions of this intercooler can be reduced.
[0008] To meet this requirement, some known solutions are configured to cool the combustive
air via ducts that allow a coolant to circulate at an outlet area of the supercharging
compressor.
[0009] This additional cooling tends to reduce the temperature rise due to compression and
proves beneficial. For example, it makes it possible to reduce the heat exchange surface
area required, at the intercooler, to cool the air after compression (and thus makes
it possible to reduce the footprint of the intercooler itself) when the other operating
parameters are the same (compressor size and power, compressor rotation speed, impeller
structure, etc.); it makes it possible to increase engine performance, in terms of
torque, power and responsiveness of the engine (also referred to as "turbo-lag") during
supercharging; moreover, with the same compressor geometry and the same engine performance,
it makes it possible to reduce the speed of rotation of the compressor shaft.
[0010] However, known solutions of the type just described are unsatisfactory, as they achieve
relatively little advantage in terms of temperature control, and are relatively complex
to design and implement, due to the ducts and hydraulic connections required to make
the coolant flow to the outlet of the supercharging compressor.
[0011] There is, therefore, a need for an alternative and improved solution to cool the
air at the supercharging compressor.
[0012] The purpose of this invention is to provide a supercharging compressor for a vehicle
internal combustion engine, which enables the above requirements to be fulfilled in
a simple and/or economical and/or effective manner.
Summary
[0013] According to this invention, a supercharging compressor for a vehicle internal combustion
engine is provided as defined in claim 1.
[0014] The dependent claims define preferred embodiments according to this invention.
Brief Description of the Drawings
[0015] In order to better understand this invention, a number of non-limiting embodiments
thereof will now be described by way of example with reference to the attached drawings,
in which:
- Figure 1 is a perspective view of a preferred embodiment of the supercharging compressor
for a vehicle internal combustion engine according to this invention;
- Figure 2 shows the supercharging compressor, schematically and in a cutaway view,
according to the cross-section plane indicated by line II-II in Figure 1; and
- Figure 3 shows a detail of the supercharging compressor, on an enlarged scale and
in cross section according to the cross-section plane indicated by the line III-III
in Figure 1.
Description of preferred embodiments
[0016] In Figure 1, reference number 1 denotes a compressor used to supercharge combustive
air in an internal combustion engine 2, illustrated schematically in Figure 2. With
reference to this figure, the compressor 1 is arranged upstream of a heat exchanger
3, usually referred to as an intercooler, along a supply line 4 that conveys combustive
air from an external atmosphere through a suction port 5 and ends at an intake manifold
6 coupled to the engine 2. Specifically, the compressor 1 comprises an inlet port
8, connected to the suction port 5, and an outlet port 9 connected to an inlet of
the heat exchanger 3. In particular, the compressor 1 comprises a support body 10
and an impeller 11 (schematically illustrated), which is arranged in a housing 12
of the body 10 in such a way that it can rotate about its axis 13, under the action
of an actuation component 14 (schematically illustrated), which may be defined as
a turbine driven by a flow of exhaust gases produced, in use, by the engine 2, or
by an electric motor.
[0017] The impeller 11 has a known blade structure such that it draws air in from the inlet
port 8 and compresses it towards the outlet port 9 when rotated about its axis 13.
In particular, the compressor 1 is a centrifugal compressor, whereby the impeller
11 draws in air along the axis 13 and compresses it in a radial direction; for example,
the outlet port 9 is arranged tangentially, at one end of a spiral 15 defined by the
body 10 to progressively collect the air compressed by the impeller 11.
[0018] According to this invention, the compressor 1 comprises a Peltier cell cooling device,
which is denoted by reference number 19, is arranged in an intermediate position between
the inlet port 8 and the impeller 11 (considering the direction of the air flow),
and is supplied by means of electrical wiring 20 (schematically illustrated) to cool
the combustive air sucked in.
[0019] With reference to Figure 3, the device 19 comprises a tubular body 21, which extends
along an axis 22 and defines a passage 23 for the combustive air. In the particular
example illustrated, the tubular body 21 is defined by four sectors, fixed with respect
to each other.
[0020] The passage 23 is preferably engaged by one or more walls 24, which extend radially
from the tubular body 21 with respect to the axis 22 and have, each, two outer faces
which are opposite to each other and are exposed to the combustive air flowing in
the passage 23.
[0021] In the attached figures, the walls 24 have a flat shape, but this should not be understood
as a limiting feature; for example, they could alternatively have an airfoil. For
example, the device 19 comprises four walls 24, spaced 90° apart from each other.
[0022] The device 19 comprises one or more Peltier cells 25, which are subjected, in use,
to a potential difference by means of the electrical wiring 20, in a known way not
illustrated in detail. Each Peltier cell 25 has two opposing faces, 26 and 27; when
subjected to a potential difference, it is configured in a known way to generate a
temperature difference between the faces 26 and 27 in order to cause a flow of heat
from the face 26, at a cooler temperature, towards the face 27, at a warmer temperature;
the face 26 of the Peltier cell 25 is turned towards the passage 23, and is preferably
arranged in such a position as to be directly exposed to the flow of air flowing through
the passage 23.
[0023] In the example shown, the Peltier cells 25 are embedded in the walls 24, each with
the face 27 turned towards the inside of the corresponding wall 24. Specifically,
in each Peltier cell 25, the face 26 coincides with one of the two external faces
of the corresponding wall 24. More specifically, each wall 24 comprises two Peltier
cells 25, one on each of its external faces: for example, the configuration of each
wall 24 is symmetrical with respect to a plane of symmetry extending radially with
respect to the axis 22.
[0024] Specifically, each wall 24 has a frame 28, which surrounds and supports the two Peltier
cells 25. The frames 28 of the walls 24 preferably consist of a single piece with
the tubular body 21.
[0025] In each wall 24, the faces 27 of the two Peltier cells 25 are separated from each
other, in a tangential direction, by an insert 29, which has the function of absorbing
heat from the faces 27 and transferring it radially towards the tubular body 21 and
thus to the outside. In other words, in use, the face 27 transmits heat (both that
coming from the face 26, and that produced internally by the Peltier cell itself)
by thermal conduction to the insert 29, and the latter, in turn, transfers heat by
thermal conduction radially so that it can then be transferred to the external atmosphere
surrounding the tubular body 21, essentially by unforced convection. Each insert 29
is preferably integral with a respective finned sector 30, arranged on an external
surface 31 of the tubular body 21. The finned sector 30 receives heat from the insert
29 by thermal conduction and has multiple fins protruding cantilevered outwards, so
as to increase the heat exchange surface area (and thus increase heat dissipation
by convection) towards the external atmosphere.
[0026] According to a variant not illustrated, one or more Peltier cells 25 are embedded
in the tubular body 21, with the face 26 arranged at an internal surface 32 radially
delimiting the passage 23. In this case, the walls 24 may possibly be absent.
[0027] According to variants not illustrated, heat could be transferred by thermal conduction
to the tubular body 21, and the latter could be directly fitted with fins for heat
exchange with the external atmosphere (without fitting additional finned sectors 30).
[0028] The device 19 is preferably arranged coaxially with the impeller 11, so that the
axis 22 shown in Figure 3 coincides with the axis 13 in Figure 2.
[0029] As shown in Figure 2, for example, the tubular body 21 is defined by an end portion
of the body 10; according to a different and preferred embodiment, not illustrated,
the tubular body 21 may be defined by a piece that is distinct from the body 10 and
is connected to the latter in a fixed position.
[0030] Still with reference to Figure 2, at one end, the passage 23 ends at the inlet port
8 of the compressor 1 and, at the opposite end, communicates with the housing 12 through
a duct 35, which is defined by a tubular portion 36 of the body 10 and represents
a converging nozzle (converging in the direction of the air from the outlet of the
passage 23 towards the inlet of the housing 12).
[0031] The diameter of the passage 23 is preferably constant; according to a variant not
illustrated, the passage 23 could be convergent (that is, it could have a decreasing
diameter, going towards the impeller 11) and possibly replace at least part of the
duct 35.
[0032] In use, as mentioned above, when supplied by the wiring 20, the Peltier cells 25
remove heat from the combustive air sucked in, in order to cool it. This cooling reduces
the volume of air treated by the compressor 1 and/or reduces the air temperature at
the outlet port 9.
[0033] For example, thanks to the device 19 it is possible to reduce the heat exchange surface
areas at the intercooler 3, other factors being equal. Otherwise, the device 19 makes
it possible to proportionally increase the mass of air treated by the compressor 1
and entering the engine 2, to the benefit of the performance of the engine 2.
[0034] At the same time, the technique implemented to cool the combustive air by means of
the device 19 does not involve the passage of a coolant, but is based on the Peltier
effect, so the proposed solution is relatively simple to install. In particular, no
specific modification to the body 10 is required. In fact, in the simplest embodiment,
it may be sufficient to add the device 19 immediately in front of the portion 36 defining
the duct 35 of an existing common compressor.
[0035] Moreover, the generation of the temperature difference, and thus the removal of heat
from the air flowing through the passage 23, are almost immediate, as they are the
direct consequences of an electrical potential difference (and not the consequence
of a heat transfer fluid, which tends to take a relatively long time to remove heat).
[0036] From the above, finally, it is apparent that modifications and variations may be
made to the compressor 1 described herein without departing from the scope of protection
of the attached claims.
[0037] In particular, the shape and size of the passage 23, as well as the structure, shape
and number of walls 24, may differ from what is shown as an example.
[0038] In addition, a fitting could be provided to connect the inlet of the duct 35 to the
outlet of the passage 23 defined by the tubular body 21.
1. A supercharging compressor (1) for an internal combustion engine (2), comprising:
- an inlet port (8),
- an outlet port (9),
- a support body (10),
- an impeller (11) coupled to the support body (10) so as to rotate about an axis
(13) and configured so as to draw air from said inlet port (8) and compress said air
towards said outlet port (9) when subjected to rotation;
- a cooling device for cooling said air;
characterised in that said cooling device is a Peltier cell cooling device (19) comprising at least one
Peltier cell (25), that has a first face (26) and a second face (27), opposite each
other, and is powered by an electrical wiring (20) to generate, in use, a difference
in temperature between said first face (26) and second face (27), and therefore a
heat transfer from said first face (26) to said second face (27); said first face
(26) faced towards a passage (23) through which said air flows.
2. The supercharging compressor according to claim 1, wherein said first face (26) is
arranged at said passage (23) so as to be directly exposed to said air during use.
3. The supercharging compressor according to claim 1 or 2, wherein said passage (23)
is arranged between said inlet port (8) and said impeller (11).
4. The supercharging compressor according to claim 3, wherein said Peltier cell cooling
device (19) comprises a tubular body (21) having an internal surface (32) defining
said passage (23) and an external surface (31) faced towards an external atmosphere;
said second face (27) being arranged in such a position as to transfer heat by thermal
conduction towards said external surface (31).
5. The supercharging compressor according to claim 4, wherein said Peltier cell cooling
device (19) further comprises a plurality of fins that project outwardly from said
external surface (31).
6. The supercharging compressor according to any one of claims 3 to 5, wherein said support
body (10) defines a convergent duct (35) arranged between said passage (23) and said
impeller (11).
7. The supercharging compressor according to any one of the preceding claims, wherein
said Peltier cell cooling device (19) further comprises at least one wall (24) arranged
inside said passage (23); said Peltier cell (25) being at least partially embedded
in said wall (24).
8. The supercharging compressor according to claim 7, wherein said wall (24) comprises
two Peltier cells (25), arranged respectively at two external faces of said wall (24),
opposite each other in the tangential direction.
9. The supercharging compressor according to claim 7 or 8, wherein said Peltier cell
cooling device (19) comprises a plurality of walls (24) arranged inside said passage
(23); each of said walls (24) comprising at least one respective Peltier cell (25).
10. The supercharging compressor according to any of the preceding claims, wherein said
passage (23) has a constant diameter.