COOLING MODULE HAVING A SACRIFICIAL REGION FOR AN ELECTRIC MOTOR VEHICLE

Abstract

A cooling module (22) for a motor vehicle (10) with an electric motor (12) comprises a housing (24) defining a longitudinal channel opening at two ends (24a; 24b) of the housing (24), at least one heat exchanger (301-304) arranged in the channel, and at least one tangential-flow turbomachine (28) capable of creating an air flow in the channel. The housing (24) has a sacrificial region (40) intended to be deformed and/or to break preferentially in the event of an impact, the sacrificial region preferably being located in the vicinity of an end (24a; 24b) of the housing (24).

Claims

1. A cooling module for a motor vehicle with an electric motor, comprising: a casing defining a longitudinal channel opening out at two ends of the casing; at least one heat exchanger arranged in the channel; and at least one tangential-flow turbomachine capable of creating an air flow in the channel; wherein the casing has a sacrificial zone configured to deform and/to break preferentially, in the event of an impact, the sacrificial zone being in the vicinity of one end of the casing.

2. The cooling module as claimed in claim 1, wherein the sacrificial zone forms a longitudinal portion of the casing.

3. The cooling module as claimed in claim 1, wherein the sacrificial zone has a smaller thickness than the rest of the casing.

4. The cooling module as claimed in claim 1, wherein the sacrificial zone is bent.

5. The cooling module as claimed in claim 1, wherein the sacrificial zone is made of a different material than the rest of the casing.

6. The cooling module as claimed in claim 1, wherein the height of the at least one heat exchanger is less than or equal to 350 mm, the cooling module having a height between 70 mm and 300 mm.

7. The cooling module as claimed in claim 1, wherein the at least one heat exchanger has a width between 20 mm and 700 mm.

8. The cooling module as claimed in claim 1, further comprising at least two heat exchangers, said heat exchangers being arranged one after another in the channel.

9. The cooling module as claimed in claim 1, having a longitudinal dimension between 12 mm and 140 mm.

10. A motor vehicle with an electric motor, comprising: a body; a bumper and a cooling module as claimed in claim 1, the body defining at least one cooling opening arranged below the bumper, the cooling module being arranged opposite the at least one cooling opening such that the sacrificial zone is oriented toward the cooling opening.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

[0032] Other characteristics, details and advantages of the invention will become apparent upon reading the detailed description below, and upon analyzing the appended drawings, in which:

[0033] FIG. 1 depicts schematically the front part of a motor vehicle with an electric motor, viewed from the side;

[0034] FIG. 2 is a schematic perspective view of a cooling module which may be used in the motor vehicle from FIG. 1;

[0035] FIG. 3 is a view similar to FIG. 2 of the same cooling module, in which part of the casing has been removed;

[0036] FIG. 4 is an extract view along plane IV-IV of the cooling module from FIG. 2;

[0037] FIG. 5 is a schematic view of a detail of the cooling module from FIG. 2;

[0038] FIG. 6 is a perspective view of the cooling module from FIG. 2 in an opposite orientation;

[0039] FIG. 7a illustrates schematically a first variant of the cooling module;

[0040] FIG. 7b illustrates schematically a second variant of the cooling module;

[0041] FIG. 7c illustrates schematically a third variant of the cooling module; and

[0042] FIG. 8 illustrates schematically a fourth variant of the cooling module.

DESCRIPTION OF EMBODIMENTS

[0043] In the remainder of the description, elements that are identical or perform identical functions bear the same reference sign. In the present description, for the sake of conciseness, these elements are not described in detail within each embodiment. Rather, only the differences between the embodiment variants are described in detail.

[0044] FIG. 1 illustrates schematically the front part of a motor vehicle 10 with an electric motor 12. The vehicle 10 comprises in particular a body 14 and a bumper 16 carried by a chassis (not shown) of the motor vehicle 10. The body 14 defines a cooling opening 18, i.e. an opening through the body 14. Here there is only one cooling opening 18. This cooling opening 18 is situated in the lower part of the front face 14a of the body 14. In the example illustrated, the cooling opening 18 is situated below the bumper 16. A grille 20 may be arranged in the cooling opening 18 to prevent projectiles from being able to pass through the cooling opening 18. A cooling module 22 is arranged opposite the cooling opening 18. The grille 20 in particular provides protection for the cooling module 22.

[0045] The cooling module 22 is more clearly visible on FIG. 2.

[0046] As illustrated on FIG. 2, the cooling module 22 essentially comprises a casing 24 forming an internal channel between two opposite ends 24a, 24b. The end 24a is intended to be arranged opposite the cooling opening 18. The opening of the casing 24 at this front end 24a of the channel may be partially blocked by means of a mesh 26.

[0047] The casing 24 is here made in two parts 24.sub.1, 24.sub.2 which are fixed together by any means accessible to the person skilled in the art. In this case, the two parts 24.sub.1, 24.sub.2 are screwed together at a collar. The front part 24.sub.1 has substantially the form of a rectangular parallelepiped open on two opposite faces. The rear part 24.sub.2 has a substantially more complex form. This rear part 24.sub.2 here in particular forms the volute of the tangential-flow turbomachine 28.

[0048] FIG. 3 illustrates the cooling device 22 in which the front part 24.sub.1 of the casing 24 has been removed. FIG. 3 thus illustrates the presence of a plurality of heat exchangers 30.sub.1-30.sub.4 in the conduit formed inside the casing 24. Here, four heat exchangers 30.sub.1-30.sub.4 are provided. Of course, this number of heat exchangers is nonlimiting. Rather, a different number of heat exchangers may be provided in the casing, in particular at least one heat exchanger, and preferably between four and seven heat exchangers, even more preferably four or five heat exchangers. The heat exchangers 30.sub.1-30.sub.4 are illustrated schematically in FIG. 3 in the form of substantially rectangular plates. In practice and notably, the heat exchangers 30.sub.1-30.sub.4 have in particular a height h.sub.30, measured in a substantially vertical direction, which is less than or equal to 350 mm. The heat exchangers 30.sub.1-30.sub.4 are thus particularly well dimensioned for being in contact with an air flow passing through the cooling opening 18.

[0049] In the example illustrated in FIG. 3, all heat exchangers 30.sub.1-30.sub.4 are identical and all have a same height h.sub.30. In the case where the heat exchangers 30.sub.1-30.sub.4 have different heights, it is preferred that all these heights are less than or equal to 350 mm.

[0050] Preferably, the height h.sub.30 of the heat exchangers 30.sub.1-30.sub.4 is between 70 mm and 300 mm. This indeed ensures a satisfactory performance of the heat exchangers 30.sub.1-30.sub.4 while retaining a reduced size of these heat exchangers, the size being particularly suitable for the use of a single cooling opening 18. Here again, in the case where the heat exchangers 30.sub.1-30.sub.4 have different heights, it is preferred that the height of each heat exchanger 30.sub.1-30.sub.4 is between 70 and 300 mm.

[0051] Even more preferably, the cooling module 22 has a height h.sub.22 between 70 mm and 300 mm. It is understood that the height h.sub.30 of the heat exchangers 30.sub.1-30.sub.4 is always substantially less than the height h.sub.22 of the cooling module 22.

[0052] To compensate for the relatively low height of the heat exchangers 30.sub.1-30.sub.4, these may be relatively numerous, in particular up to four or five heat exchangers 30.sub.1-30.sub.4, even up to seven heat exchangers. Indeed, to achieve performance levels comparable to those of conventional cooling modules, the number of heat exchangers may be doubled by arranging them in pairs, in series, in the circuit of the fluid passing through them. In other words, a heat exchanger of a conventional cooling module may correspond to two heat exchangers or more in the cooling module 22, through which the same fluid passes. In this case in particular it is useful if the heat exchangers are arranged one behind the other in the conduit formed by the casing 24. The order of the heat exchangers may be determined as a function of a temperature of the fluid passing through them, or a distance of the heat exchanger concerned from a heat source in the circuit of fluid passing through them. Thus the heat exchangers through which a hot fluid flows are arranged further from the end 24a of the casing 24, intended to be arranged just behind the cooling opening 18, than heat exchangers through which a colder fluid flows.

[0053] The arrangement of heat exchangers 30.sub.1-30.sub.4 one behind the other in the axial direction X of the cooling module 22 may also limit the size of the cooling module 22 in its two other lateral and vertical dimensions. This preferably, the depth p.sub.22 of the cooling module 22 is between 12 mm and 140 mm. Also, the width L.sub.30 of the heat exchangers 30.sub.1-30.sub.4 or of each heat exchanger 30.sub.1-30.sub.4 may lie between 12 mm and 140 mm.

[0054] In addition, because of the shape of the heat exchangers 30.sub.1-30.sub.4, a tangential-flow turbomachine 28 is preferred. In fact a propeller fan would be unable to create a substantially uniform air flow in contact with the heat exchangers 30.sub.1-30.sub.4, in particular over substantially the entire length of these heat exchangers 30.sub.1-30.sub.4, a length measured in the lateral direction Y.

[0055] Here, the tangential-flow turbomachine 28 comprises a turbine 32 (or tangential impeller). The turbine 32 has a substantially cylindrical form, as is shown particularly clearly on FIG. 5. The turbine 32 comprises several stages of blades 34 (or vanes), in this case sixteen stages of blades 34. Naturally, this number of stages of blades 34 is not limiting, and the turbine 32 may more generally comprise at least one stage of blades 34.

[0056] Each stage of blades 34 comprises a same number of blades 34 evenly distributed angularly around the rotational axis A.sub.32 of the turbine 32. Advantageously, the stages of blades 34 are angularly offset such that the blades 34 are not aligned, preferably such that no blade 34 is aligned with another blade 34 of another stage of blades 34 in the lateral direction Y of the cooling module 22. This then avoids the blades 34 of the turbine 32 generating noise, particularly because of the fact that all the blades 32 would be working in synchrony. By offsetting the blades 34, it is possible rather to ensure that the blades 34 work in separate groups, which makes it possible to reduce the noise generated. This gives a tangential-flow turbomachine 28 in which the sound nuisance can be limited. This is particularly important in the case of a cooling module 22 for a motor vehicle with electric motor, since an electric motor is known to be less noisy than an internal combustion engine. In addition, the cooling module 22 is intended to be used also when the electric motor has stopped, in particular when the batteries are being recharged. The noise of the tangential-flow turbomachine 28 may then be considered a nuisance by users.

[0057] The blades 34 of each stage may in particular be offset by half the spacing between the blades 34, with respect to each of the two neighboring stages. Thus, a first half of the stages of blades 34 have blades 34 which are aligned with one another and which are offset by half the angular spacing between the blades 34 relative to the blades 34 of the other half of the stages of blades 34. The noise generated by the rotating turbine 22 can thus theoretically be substantially halved, which corresponds to a reduction of the order of 3 dB in the noise emitted.

[0058] Alternatively, the angular offset of the blades 34 between two adjacent stages of blades 34 corresponds to the thickness of a blade 34.

[0059] Alternatively or in addition, the spacing between the blades 34 may be divided into substantially as many intermediate positions as there are stages of blades 34. Thus, the blades 34 of the various stages of blades 34 may be offset step-by-step in the same angular direction, along a longitudinal direction of the turbine 32. The blades 34 of the various stages therefore extend substantially in a helix along the various stages of blades 34. In this particular case, all the blades 34 of all the stages of blades 34 are offset with respect to all the blades 34 of all the other stages of blades 34. This allows an even greater reduction in the noise generated by the rotating turbine 32.

[0060] Of course, numerous other configurations are accessible to those skilled in the art, allowing all the blades 34 of all the stages of blades 34 to be offset relative to all the other blades 34 of all the other stages of blades 34. In particular, based on the preceding configuration in which the blades 34 of the various stages 34 extend in the manner of the helix, it is possible to swap the various stages around, without altering their orientation about the longitudinal axis of the turbine 32.

[0061] The turbomachine 28 also comprises a motor 36 (or gear motor) able to drive the turbine 32 in rotation about its rotational axis A.sub.32. Advantageously, the rotational axis A.sub.32 of the turbine 32, which corresponds to the height direction of the turbine 32, is oriented substantially parallel to the lateral direction Y of the heat exchangers 30.sub.1-30.sub.4. The turbomachine 28 is thus able to create a substantially constant air flow over the entire width of a same heat exchanger 30.sub.1-30.sub.4. In order to optimize the air flow created, the height h.sub.32 of the turbine 32 is substantially equal to the width L.sub.30 of the heat exchangers 30.sub.1-30.sub.4.

[0062] The motor 36 is for example able to drive the turbine 32 in rotation at a speed between 200 rpm and 14,000 rpm. This allows in particular a limitation of the noise generated by the turbomachine 28.

[0063] The diameter D.sub.32 of the turbine 32 is for example between 35 mm and 200 mm as limits. The turbomachine 28 is thus compact.

[0064] As already stated, the rear part 24.sub.2 of the casing 24 forms the volute of the turbomachine 28, as can be seen more particularly from FIGS. 4 and 5. In addition, the cross-section of the conduit formed in the casing 24 is significantly greater at the end 24a than at its opposite end 24b. This allows the turbomachine 28 to create an air flow in the casing 24 which has a specific pressure, in order to facilitate the passage of said air flow through the conduit through the casing 24, despite the presence of the heat exchangers 30.sub.1-30.sub.4.

[0065] Also, notably, the casing 24 of the cooling module 22 has here a sacrificial zone 40 intended to deform and/or to break preferentially, in the event of an impact, in particular in the event of a frontal impact. The sacrificial zone 40 is preferably in the vicinity of a front end 24a, intended to be closest to the bumper 16 and/or the cooling opening 18 of the motor vehicle 10, when the cooling module 22 is mounted in the vehicle 10. In particular, the sacrificial zone 40 is preferably arranged longitudinally between the end 24a and the heat exchanger 30.sub.1 arranged closest to this end 24a. Thus, the deformation and/or breaking of the sacrificial zone 40 is advantageously realized before any damage to the heat exchangers 30.sub.1-30.sub.4 and the turbomachine 28.

[0066] In the example illustrated, the sacrificial zone 40 is in the form of a longitudinal portion of the casing 24, for example in the form of a strip. To promote the deformation of and/or damage to the sacrificial zone 40, the latter may in particular: [0067] have a smaller thickness than the rest of the casing 24; and/or [0068] be bent, in particular in one or more transverse directions; and/or [0069] be made of a different material than the rest of the casing 24, in particular of a material more ductile than the rest of the casing 24.

[0070] The invention is not limited to the exemplary embodiments described with respect to the figures, and further embodiments will be clearly apparent to a person skilled in the art. In particular, the various examples can be combined, provided they are not contradictory.

[0071] For example, in the example illustrated above and illustrated schematically in FIG. 7a, the turbomachine 28 is in a top position, in particular in the upper third of the casing 24, preferably in the upper quarter of the casing 24. This in particular allows protection of the turbomachine 28 in the case of submersion, and/or limits the space taken up by the cooling module 22 in its bottom portion. Rather, a bottom position of the turbomachine 28, illustrated in FIG. 7c, in particular in the lower third of the casing 24, limits the space taken up by the cooling module 22 in its top portion. Alternatively, the turbomachine 28 can be in a median position, illustrated in FIG. 7b, in particular in the middle third of the height of the casing 24, for example for reasons of integration of the cooling module 24 in its environment.

[0072] Also, according to the example illustrated in FIG. 8, the turbomachine 28, and more particularly the turbine 32 of this turbomachine 28, is movable relative to the heat exchangers 30.sub.1-30.sub.4 in the height direction of these heat exchangers 30.sub.1-30.sub.4. Such a configuration may for example allow precise temporal management of the cooling of some of the heat exchangers 30.sub.1-30.sub.4.

[0073] Also, in the examples illustrated, the turbomachine 28 functions by suction, i.e. it draws in ambient air and conducts it into contact with the various heat exchangers 30.sub.1-30.sub.4. Alternatively however, the turbomachine 28 operates by blowing, blowing the air towards the different heat exchangers 30.sub.1-30.sub.4.

[0074] Also, whereas in the example described with reference to FIGS. 2 to 6, the turbomachine is situated in the casing of the cooling module, the turbomachine may be arranged outside the casing at one end or another end of this casing, depending on whether or not it functions by suction or blowing.

[0075] In FIGS. 7a-7c and 8, the sacrificial zone 40 is not illustrated for the sake of clarity of the figures. However, this sacrificial zone 40 can also be present on the casing 24 of the cooling modules illustrated in these figures.