EP4164903A1

EP4164903A1 - Ventilation device for a vehicle ventilation, heating and/or air-conditioning system

Info

Publication number: EP4164903A1
Application number: EP21732163.7A
Authority: EP
Inventors: Fabrice Ailloud; Oliver Lauer; SANTOYO Nestor Ismael VARELA; Bruno Demory; BENZAKROUM Mohamed ALAOUI; Manuel Henner; Maxime Laurent
Original assignee: Valeo Systemes Thermiques SAS
Current assignee: Valeo Systemes Thermiques SAS
Priority date: 2020-06-16
Filing date: 2021-06-16
Publication date: 2023-04-19
Also published as: CN115697735A; WO2021255063A1; US20230219394A1; JP7556059B2; FR3111296A1; JP2023529988A

Abstract

The invention relates to a ventilation device (100) for a vehicle ventilation, heating and/or air-conditioning system (200), comprising at least one housing (110) that comprises at least one wall (114) defining an inner volume (210) in which at least one radial propeller (120) capable of being rotated and at least one guide member (130) are received, the radial propeller (120) and the guide member (130) being configured to generate an air flow (FA) having a general direction parallel to an axis of rotation (R) of the radial propeller (120) between an air inlet (126) of the radial propeller (120) and an air outlet (112) formed in the wall (114) of the housing (110) of the ventilation device (100), at least a part of the wall (114) of the housing (110) being configured to straighten the air flow (FA) at the outlet of the radial propeller (120), characterised in that the guide member (130) is configured to direct the air flow (FA) towards the axis of rotation (R) of the radial propeller (120).

Description

VENTILATION DEVICE FOR A VENTILATION, HEATING AND / OR AIR CONDITIONING SYSTEM OF A VEHICLE

The present invention relates to the field of ventilation, heating and / or air conditioning systems intended to be integrated into motor vehicles, for example motor vehicles with electric propulsion.

Motor vehicles conventionally include a ventilation, heating and / or air conditioning system intended for the heat treatment of an air flow intended to be sent into a passenger compartment of this vehicle. These ventilation, heating and / or air conditioning systems comprise at least one casing in which are received at least one heat exchanger and at least one ventilation device. For example, a heat transfer fluid, that is to say a fluid capable of capturing, transporting and transferring calories, circulates in this heat exchanger. This heat exchanger is also crossed by a flow of air which, passing through the heat exchanger, sees its temperature modified before being sent into the passenger compartment so as to heat treat its temperature.

In order to generate the air flow capable of passing through the heat exchanger, the ventilation, heating and / or air conditioning system conventionally comprises at least one ventilation device which comprises at least one propeller received in a housing, this propeller being driven in rotation by a moving member which can also be received in the housing.

The ventilation devices currently implemented include an axial air inlet, that is to say a mouth which allows the air flow to enter the ventilation device in a direction parallel, or substantially parallel, to a axis of rotation of the propeller of this ventilation device, and a radial air outlet where the air flow leaves in a radial direction of the propeller. In other words, such a ventilation device is conventionally arranged in a volute so that the air flow enters the ventilation device in a first direction and leaves this housing in a second direction perpendicular to the first direction.

A drawback of these ventilation devices is that they are particularly bulky due to the radial nature of the air flow leaving the device. They cannot therefore be easily installed in particularly cramped ventilation systems.

Document KR20140054655A describes for example a ventilation device in which the air flow circulates in a general direction parallel to an axis of rotation of a propeller of this ventilation device, between an air inlet of this propeller and an outlet of the device ventilation. A drawback of the ventilation device described in this document lies in the fact that the air flow tends to leave the ventilation device through a peripheral portion of the outlet opening formed in the housing. In other words, a flow rate of the air flow measured in a peripheral portion of the air outlet opening formed in the housing of the ventilation device is greater than a flow rate of this air flow measured in a central portion of this opening. air outlet. The air outlets of this type of ventilation device can be closed by an air filter. Thus, the difference in flow rate between the peripheral portion and the central portion of the air outlet mouth may result in an unoptimized use of such an air filter which may result in a need to change this air filter more. frequently only if the air flow rate was constant, or substantially constant, over the entire surface of the air outlet, that is to say both in the central portion and in the peripheral portion of this air outlet.

The present invention falls within this context and aims to resolve at least the aforementioned drawbacks by proposing a ventilation device the size of which is reduced compared to the ventilation devices of the prior art and in which the air flow presents a substantially constant flow rate at all points of the air outlet.

An object of the present invention thus relates to a ventilation device for a ventilation, heating and / or air conditioning system of a vehicle, comprising at least one housing which comprises at least one wall delimiting an internal volume in which at least one is received. radial propeller adapted to be driven in rotation and at least one guide member, the radial propeller and the guide member being configured to generate an air flow of general direction parallel to an axis of rotation of the radial propeller between an air inlet of the radial propeller and an air outlet mouth formed in the wall of the housing of the ventilation device, at least part of the wall of the housing being configured to straighten the air flow at the outlet of the radial propeller. According to the invention, the guide member is configured to direct the air flow towards the axis of rotation of the radial propeller.

The term “radial propeller” is understood to mean a propeller in which the air flow enters in a first direction, in this case parallel to the axis of rotation of this propeller, and leaves it in a second transverse direction, for example perpendicular. , to the axis of rotation of this propeller. In other words, the radial propeller, within the meaning of the invention, comprises an axial air inlet and a radial air outlet. By "at least part of the wall of the housing is configured to straighten the air flow" is meant the fact that this wall has a calculated shape of so that when the air flow leaves the radial propeller, it comes into abutment against this part of the wall of the housing which causes a deviation of this air flow in order to straighten it, that is to say to direct it towards the guide member. Thus, the shape of the housing of this ventilation device and the member for guiding the air flow received in this ventilation device make it possible, jointly, to channel the air flow generated by the rotation of the radial propeller so that the general size of this ventilation device compared to the ventilation devices of the prior art is reduced. The air outlet of the ventilation device according to the invention can thus be placed in the axial extension of the radial helix, which makes it possible to reduce the radial size of such a device. As a result, the ventilation device according to the invention can be installed more easily in small-sized vehicles, such as, for example, vehicles with at least partly electric propulsion. For example, the radial propeller can be driven in rotation by a setting member. Optionally, a support for this moving member can be received in the internal volume of the case. The ventilation device according to the invention makes it possible to obtain a homogeneous distribution of the air flow over an entire surface of the outlet opening formed in the wall of the housing, even in the presence of the support placed axially in the center of the outlet opening. formed in the wall of the housing, by inclining the air flow so that it joins the part of the outlet mouth where the axis of rotation of the radial propeller passes.

According to the invention, the air flow guide member may include a plurality of fixed blades arranged axially between the radial propeller and the air outlet. For example, at least one fixed blade of the air flow guide member comprises at least one outer end integral with the wall of the housing. Advantageously, each fixed blade of the air flow guide member comprises an external end integral with the wall of the housing.

According to one characteristic of the invention, the radial propeller comprises a plurality of movable blades, each movable blade comprising an internal edge turned towards the axis of rotation of the radial propeller and an external edge turned away from the internal ridge, at least one external ridge extending parallel to the axis of rotation of the radial helix. Advantageously, the outer edges of each of the movable blades each extend in a direction parallel to the axis of rotation of the radial propeller.

According to another characteristic of the invention, an internal radius of the radial propeller measured between the axis of rotation of the radial propeller and the internal edge of one of the movable blades of the radial propeller, in a plane perpendicular to the axis of rotation of the radial propeller is included between 36 mm and 54 mm. For example, an external radius of this radial propeller, measured between its axis of rotation and the external edge of one of the mobile blades of the radial propeller, in the plane perpendicular to the axis of rotation, can be between 64 mm and 96 mm.

Advantageously, the internal edge of a mobile blade has a height measured parallel to the axis of rotation of the radial propeller greater than a height of the external edge of this mobile blade, measured parallel to the axis of rotation of the radial propeller. For example, provision could be made for a ratio between the height of the internal edge of a mobile blade of the radial propeller and the height of the external edge of this mobile blade of the radial propeller to be between 1, 1 and 1.9. For example, the internal edge of a movable blade of the radial propeller may have a height of between 36 mm and 54 mm and the outer edge of this same movable blade of the radial propeller may have a height of between 29 mm and 44 mm. Also, the internal edge of a movable blade of the radial propeller and the outer edge of this movable blade of the radial propeller can have different positions, that is to say present an offset one by one. relative to each other, along the axis of rotation of the radial propeller.

More particularly, the movable blades of the radial propeller extend, respectively, between a bowl of the propeller and an edge of the propeller, the bowl of the propeller having a convex shape seen from the movable blades of this propeller radial, the height of the internal edge of a mobile blade and the height of the external edge of this mobile blade being respectively measured between the bowl of the propeller and the edge of the propeller, parallel to the axis of rotation of this radial propeller.

According to one characteristic of the invention, each movable blade of the radial propeller is delimited by at least one upper line facing towards the air inlet of the radial propeller and by at least one lower line facing towards the outlet mouth. air formed in the wall of the housing, and the upper line of at least one movable blade of this radial propeller has at least a first portion which projects from the edge of the radial propeller, in the direction of the axis of rotation of this radial helix, and a second portion covered by this edge of the radial helix. Advantageously all the upper lines of the movable blades of the radial propeller have this first portion and this second portion. The bowl of the radial propeller is more particularly arranged so as to connect the lower lines of the movable blades of this radial propeller. Advantageously, this bowl of the radial propeller can be closed, that is to say that this bowl extends continuously between two successive mobile blades. As a result, all of the air flow generated by the rotation of the radial propeller leaves this radial propeller through its radial air outlet. According to another characteristic of the invention, the housing of the ventilation device comprises at least an upper part which houses the radial propeller and a lower part which houses the guide member, the upper part comprising at least one first convex curvature seen from the axis of rotation of the radial helix and at least one second concave curvature seen from the axis of rotation of the radial helix, the first curvature covering the edge of the radial helix and the second curvature being arranged opposite of the radial air outlet of the radial propeller. More particularly, the first curvature covers the edge of the radial helix, seen in a plane perpendicular to the axis of rotation of this radial helix. Likewise, the second curvature is arranged opposite the radial air outlet of the radial propeller, in a plane perpendicular to the axis of rotation of this radial propeller. In other words, the second curvature of the upper part of the housing is arranged so that the air flow which leaves the radial propeller abuts against this second curvature, so that this second curvature forms the configured part of the housing. to straighten the air flow leaving the radial propeller.

According to one characteristic of the invention, the air flow guide member comprises a plurality of fixed blades, at least one fixed blade of this air flow guide member comprising an intrados and an extrados connected to each other by a leading edge and a trailing edge, the fixed blade comprising a cross section, seen in a plane perpendicular to a radial extension axis of the fixed blade concerned, which extends along a line of camber between the edge of 'attack and the trailing edge, this line of camber being inscribed in a circle, a first angle being formed between a tangent to the circle at the level of the leading edge and the line of camber at the level of the leading edge and a second angle being formed between the tangent to the circle at the leading edge and the camber line at the trailing edge, the first angle being between 3 ° and 10 ° and the second angle being between 79 ° and 128 °. For example, the fixed blades of the guide member can be arranged in a circular profile, a center of this circular profile forming a center of the guide member. Advantageously, all the fixed blades of the air flow guide member can be structurally identical.

According to one characteristic of the invention, at least one fixed blade of the air flow guide member comprises a first portion, a second portion and a third portion, aligned in this order, along the axis of radial extension of the fixed blade, towards the wall of the housing, a ratio between the first angle and the second angle measured in the first portion being between 0.03 and 0.07, the ratio between the first angle and the second angle measured in the second portion being between 0.05 and 0.12 and the ratio between the first angle and the second angle measured in the third portion being between 0.02 and 0.07. Advantageously, the first portion, the second portion and the third portion come from material, that is to say they form a single whole which cannot be separated without causing the deterioration of at least one of these. portions.

According to the invention, the radial propeller is adapted to be driven in rotation by at least one member for setting in motion, the housing comprising at least one support adapted to receive at least one member for setting the propeller in motion. radial, and the guide member being interposed between the support adapted to receive the at least one movement member and the wall of the housing. According to a particular example of application of the invention, a center of the guide member and a center of the support of the movement member are coincident.

According to an exemplary embodiment of the invention, the air flow guide member comprises a plurality of fixed blades, at least one fixed blade of this air flow guide member comprising at least one internal end integral with the support adapted to receive the member for setting in motion and at least one external end integral with the wall of the housing. In other words, it is understood that the air flow guide member is fixed relative to the housing. Advantageously, all of the fixed blades of the air flow guide member may include an internal end integral with the support of the movement member and at least one external end integral with the wall of the housing. Optionally, the housing, the air flow guide member and the support for the movement member can be in one piece, that is to say form a single assembly which cannot be separated without causing damage. at least the housing, the air flow guide member and / or the support.

Optionally, an air filter can be arranged opposite the air outlet opening formed in the wall of the housing. Advantageously, the air filter can close the air outlet of the housing. In other words, the air flow guide member then makes it possible, by deflecting the air flow which leaves the radial propeller, to use the entire surface area of the available air filter, thus improving the efficiency and the longevity of this air filter.

Advantageously, the ventilation device comprises the member for setting the radial propeller in motion. For example, the member for setting the radial propeller in motion can be a direct current electric motor which comprises a motor shaft adapted to be received in the hub of the radial propeller. It will be understood from the foregoing that, where appropriate, the moving member is received in the housing, on the support provided for this purpose.

The present invention also relates to a ventilation, heating and / or air conditioning system for a vehicle, comprising at least one ventilation device as mentioned above, the ventilation system comprising at least one heat exchanger configured to operate a heat exchange. between the air flow generated by the radial propeller and a cooling fluid. By "coolant" is meant a fluid configured to transport and exchange calories with or without changing state.

Other characteristics, details and advantages will emerge more clearly on reading the detailed description given below, by way of indication, in relation to the various views of the invention illustrated in the following figures:

[Fig. 1] illustrates, schematically, part of a ventilation, heating and / or air conditioning system according to the invention comprising at least one ventilation device according to the invention;

[Fig. 2] illustrates, in perspective, the ventilation device according to the invention;

[Fig. 3] illustrates, in perspective, a radial helix of the ventilation device according to the invention

[Fig. 4] illustrates, in perspective and seen from below, an air guide member of the ventilation device according to the invention;

[Fig. 5] illustrates a cross section made along a first transverse plane AA shown in Figure 4, of a first section of a fixed blade of the air flow guide member shown in Figure 4;

[Fig. 6] illustrates a cross section made along a second transverse plane BB shown in Figure 4, of a second section of the fixed blade of the air flow guide member shown in Figure 5;

[Fig. 7] illustrates a cross section made along a third transverse plane CC illustrated in Figure 4, of a third section of the fixed blade of the air flow guide member shown in Figure 5;

[Fig. 8] illustrates a vertical section taken along a vertical plane DD illustrated in FIG. 1, of the ventilation device according to the invention. The characteristics, variants and the different embodiments of the invention can be associated with each other, in various combinations, as long as they are not incompatible or exclusive to each other. It is in particular possible to imagine variants of the invention comprising only a selection of characteristics described below in isolation from the other characteristics described, if this selection of characteristics is sufficient to confer a technical advantage or to differentiate the invention from in the state of the prior art.

Figure 1 illustrates, schematically, part of a ventilation, heating and / or air conditioning system 200 according to the invention. This ventilation, heating and / or air conditioning system 200 - hereinafter called “system 200” - is intended to be integrated into a motor vehicle, for example an electrically propelled motor vehicle, so as to heat treat a flow of gas. air FA before it is sent to a vehicle cabin for heat treatment. In other words, this FA airflow is used to cool or heat the vehicle interior. The system 200 according to the invention comprises at least one casing 201 in which is housed at least one heat exchanger 202 configured to operate a heat exchange between a cooling fluid and the air flow FA intended to be sent into the passenger compartment. of the vehicle and at least one ventilation device 100 according to the invention configured to generate the air flow FA. The housing 201 advantageously makes it possible to direct the flow of treated air FA to the vehicle interior. By "coolant" is meant here a fluid configured to transport and exchange calories with or without changing state.

As shown, the ventilation device 100 according to the invention comprises at least one housing 110 which comprises at least one wall 114 which defines an internal volume 210 in which are received at least one movement member 140, a radial propeller 120 , at least one guide member 130 of the air flow FA and at least one air filter 113. Advantageously, the air filter 113 is arranged axially between the guide member 130 and the heat exchanger 202. The member movement 140 is configured to drive the radial propeller 120 in rotation about an axis of rotation R so as to generate the air flow FA and the guide member 130 participates in turn, together with at least a part of the wall 114 of the housing 110, to straighten the air flow FA so that the latter has a general direction of movement, between an air inlet 126 of the radial propeller 120 and an outlet mouth formed in the wall 114 of the housing 110, parallel to the axis of rotation R d e the radial propeller 120. As more fully detailed below, at least one support 131 of the member 140 for setting the radial propeller 120 in motion is also received in the internal volume 210 of the housing 110 of the ventilation device, the guide member 130 of the air flow FA being interposed between this support 131 and the wall 114 of the housing 110.

According to the example illustrated in FIG. 1, the housing 110 of the ventilation device and the housing 201 of the system 200 are made from one material, that is to say they form a single assembly which cannot be separated without causing damage to the housing 110 and / or the housing 201.

With reference to Figures 2 to 8, we will more fully describe the ventilation device 100 according to the invention.

FIG. 2 illustrates, in perspective, this ventilation device 100 which comprises at least the housing 110 in which are formed at least one air inlet port 111 and one air outlet port 112, the outlet port d 'air 112 being for example at least partially closed by an air filter 113. More particularly, the air inlet 111 and the air outlet 112 are respectively formed in the wall 114 of the housing 110. Advantageously , the air filter 113 can completely close the air outlet 112, which ensures that all of the air expelled from the ventilation device 100 passes through this air filter 113 before be sent to the vehicle interior.

According to the example illustrated, the ventilation device 100 extends along a straight line of main extension D, the air inlet port 111 and the air outlet port 112 extending in parallel and perpendicular planes. , or substantially parallel and perpendicular, to this main extension line D.

The housing 110, and more specifically the wall 114 of this housing 110, has the general shape of a bell, that is to say that this housing 110 has a section seen in a plane perpendicular to the main extension line D of the housing 110, the dimensions of which increase from the air inlet 111 to the air outlet 112.

As mentioned above, the wall 114 of the housing 110 defines an internal volume of the ventilation device 100 which houses at least the radial propeller 120 configured to be driven in rotation by the movement member 140 and the guide member 130 configured to direct at least part of the air flow generated by the rotation of the radial propeller 120 in the direction of the axis of rotation R of this radial propeller 120, after it has passed through the member guide 130. The radial propeller 120 is adapted to be driven in rotation by the setting member 140 received in the support 131. For example, the setting member in motion 140 may be an electric motor which comprises at least one stator and at least one rotor, the rotor being connected in rotation with a shaft received in a hub 121 of the radial propeller 120. In other words, the axis of rotation R of the radial helix 120 extends parallel to this hub 121.

In Figure 2, the moving member 140 as well as its support 131, the radial propeller 120 and the guide member 130 are schematically shown in broken lines. As illustrated, the radial propeller 120 and the guide member 130 are arranged, in this order, along the axis of rotation R of the radial propeller 120, between the inlet mouth 111 and the outlet mouth 112 formed in the wall 114 of the housing 110. The guide member 130 is interposed between the movement member 140 and the wall 114 of the housing 110. More particularly, the guide member 130 is interposed between the support 131 of this moving member 140 and the wall 114 of the housing 110. The term “radial helix” is understood to mean a helix in which the air enters in a direction parallel to the axis of rotation R of this helix and leaves it in a direction transverse to the rate of rotation R of the propeller. As detailed below, Rotation rate R of the radial propeller in the example shown is parallel to the main extension rate D of housing 110.

The housing 110 includes at least an upper part 115 which houses the radial propeller 120 and a lower part 116 which houses the guide member 130 of the air flow. For example, the upper part 115 and the lower part 116 of this housing 110 can be in one piece, that is to say that they then form a single assembly which cannot be separated without causing the deterioration of at least one of the units. these parts.

The upper part 115 comprises at least a first portion 117 flared in the direction of the outlet mouth 112 formed in the wall 114 of the housing 110, at the end of which the air inlet mouth 111 and at least a second portion are formed. 118 at least partially curved. As shown, the first flared portion 117 has an axis of revolution coincident with the main extension line D of the housing 110 and the second cylindrical portion 118 has an axis of revolution also coincident with the main extension line D of the housing 110 More particularly, the first portion 117 extends between a first end 117a at the level of which the air inlet mouth 111 is formed and a second end 117b opposite to the first end 117a, along the line of. main extension D of the housing 110. The second portion 118 for its part extends between a first end 118a and a second end 118b opposite one another. along the main extension line D of the housing 110. As shown, the first end 118a of the second portion 118 and the second end 117b of the first portion 117 are coincident.

The first portion 117 of the upper portion 115 of the housing 110 has a first curvature 117c which extends between the first end 117a and the second end 117b. The second portion 118 for its part comprises at least a second curvature 118c which extends the first portion 117, this second curvature 118c being extended by a straight portion 118d. In other words, this second curvature 118c is interposed between the first curvature 117c of the first portion 117 and the straight portion 118d of the second portion 118. As shown, the first curvature 117c of the first portion 117 and the second curvature 118c of the second portion 118 are curved in opposite directions. In other words, the first curvature 117c of the first portion 117 is convex seen from the axis of rotation R of the radial helix and the second curvature 118c is in turn concave seen from this axis of rotation R of the radial helix. In other words, the first curvature 117c is inscribed in a circle whose center is disposed in an environment which surrounds the ventilation device according to the invention, while the second curvature 118c is inscribed in a circle whose center is arranged in the internal volume of the ventilation device according to the invention. For example, the second curvature 118c may have a radius of curvature, measured in a plane perpendicular to the rate of rotation R of the radial helix, over an angular sector of 45 °, between 23.1 mm and 34.7 mm. Advantageously, the second curvature 118c has a radius of curvature equal to or substantially equal to 28.9 mm. As will be detailed below, the second curvature 118c forms the portion of the wall 114 of the housing 110 configured to straighten the air flow leaving the radial propeller 120.

It follows from this arrangement that, according to the example illustrated, the air flow enters the ventilation device 100 through the air inlet port 111 in a first direction and leaves this ventilation device 100 through the air outlet. air outlet 112 in a second direction, parallel or substantially parallel to the first direction. In the example shown here, the first direction and the second direction are also parallel to the main extension rate D of the housing 110, and therefore also to the rotation rate R of the radial propeller 120.

According to an exemplary embodiment not illustrated here, provision could be made for the first curvature 117c to also be concave, seen from the axis of rotation R of the radial propeller 120. FIG. 3 is a perspective view of the radial helix 120 adapted to be received in the internal volume of the housing. In the remainder of the description, the terms “radial helix” and “helix” will be used without distinction.

The radial propeller 120 comprises a plurality of movable blades 122 connected to each other by means of a bowl 123 of the radial propeller 120 on the one hand and by virtue of an edge 124 of this radial propeller on the other hand. More particularly, each movable blade 122 comprises at least one upper line 125 facing an air inlet 126 of the radial propeller 120 and at least one lower line 127 facing away from the corresponding upper line 125. The edge 124 of the radial propeller 120 connects the upper lines 125 of the movable blades 122 of this propeller 120 and the bowl 123 connects the lower lines 127 of these movable blades 122.

The upper lines 125 of the movable blades 122 more particularly comprise at least a first portion 125a which projects from the edge 124, in the direction of the axis of rotation R of the propeller 120, and a second portion 125b here covered by the edge 124 of the propeller 120. Each mobile blade 122 further comprises at least one internal edge 129 and at least one external edge 220 which connect the upper line 125 to the lower line 127 of this mobile blade 122, the internal edges 129 of these movable blades 122 being turned towards the axis of rotation R of the propeller 120 and the external ridges 220 being turned radially away from this axis of rotation R.

The internal ridges 129 of the moving blades 122 thus define an internal perimeter PI of the propeller 120 while the external ridges 220 of these moving blades 122 define an external perimeter P2 of the propeller 120. Advantageously, a portion of the edge 124 of the 'propeller participates in delimiting the air inlet 126 of the propeller 120. According to the example illustrated, the internal edge 129 of at least one of the movable blades 122 forms a leading edge of the propeller 120. Advantageously, the internal ridges 129 of each of the movable blades 122 form leading edges of the movable blades 122 of this propeller 120.

The propeller bowl 123 connects the lower lines 127 of the movable blades 122. As partially visible in Figure 3, the bowl 123 is closed. In other words, each space 222 formed between two successive mobile blades 122 is closed. This bowl 123 of the propeller 120 will be further described below with reference to Figure 8.

As mentioned, the radial propeller 120 comprises at least the air inlet 126 through which the air enters the propeller 120, in a direction parallel to the axis of rotation R of this propeller 120, and at least one radial air outlet 221 through which the air leaves this propeller 120, according to a direction transverse to the axis of rotation R of this propeller 120. According to the example illustrated here, this radial air outlet 221 is formed on the external perimeter P2 of the propeller 120, that is to say that this radial air outlet 221 is formed on the outer perimeter P2 of the propeller 120. radial air outlet 221 is delimited axially on one side by the edge 124 of the propeller 120 and on the other by the bowl 123 of this propeller 120. In other words, at least the outer edge 220 d 'at least one movable blade 122 forms the trailing edge of the radial propeller 120. Advantageously, the outer edges 220 of all the movable blades 122 form, respectively, a trailing edge of the radial propeller 120. The bowl 123 of the 'propeller 120 being closed, it will be understood that all of the air flow generated by the rotation of the propeller 120 leaves this propeller 120 through the radial air outlet 221.

Finally, according to the example illustrated in FIG. 3, the movable blades 122 of the propeller 120 each have a curved shape, that is to say they extend in the form of an arc-de- circle between their internal ridge 129 and their external ridge 220. Advantageously, the propeller 120 can be in one piece, that is to say form a single assembly which cannot be separated without causing deterioration of the hub 121, of the movable blades 122 , the bowl 123 and / or the edge 124 of the propeller 120.

According to the invention, the ventilation device 100 also comprises the air flow guide member 130 adapted to direct the air flow towards the axis of rotation R of the radial propeller, subsequent thereto. FIG. 4 illustrates an exemplary embodiment of this guide member 130. More particularly, FIG. 4 is a perspective view, from below, of this guide member 130 illustrated together with a portion of the wall 114 of the housing.

According to the example illustrated, the guide member 130 of the air flow is interposed radially between the support 131 of the member for setting in motion and the wall 114 of the housing. This guide member 130 is more particularly formed of a plurality of fixed blades 132 which extend respectively between the support 131 and the wall 114 of the housing. Each of these fixed blades 132 extends along a radial extension axis X between an inner end 133 in contact with the support 131 and an outer end 134 in contact with the wall 114. For example, at least one inner end 133 of the 'one of the fixed blades 132 is integral with the support 131, the outer end 134 of this fixed blade 132 being integral with the wall 114. According to the example illustrated, all of the internal ends 133 of the fixed blades 132 are integral with the support 131 and all of the outer ends 134 of these fixed blades 132 are integral with the wall 114. For example, the guide member 130, the support 131 and the wall 114 of the housing can be from material, that is to say they form a single whole which cannot be separated without causing deterioration of the guide member 130, of the support 131 or of the wall 114.

Each of the fixed blades 132 also comprises at least one leading edge 135 through which the air flow enters the guide member 130 and at least one trailing edge 136 through which the air flow leaves this guide member. 130. The leading edge 135 is thus turned towards the air inlet mouth formed in the housing when the guide member 130 is in position in this housing and the trailing edge 136 is in turn turned towards the. outlet 112 of this housing. The leading edge 135 and the trailing edge 136 are also interconnected by a lower surface 137 and by an upper surface 138.

Advantageously, these fixed blades 132 can be distributed regularly, that is to say a space 139 which separates the lower surface 137 of a first fixed blade 132 from the upper surface 138 of a second fixed blade 132 successive to this first fixed blade 132, may have dimensions equivalent, or substantially equivalent, to the dimensions of the space 139 which separates the lower surface 137 of the second fixed blade 132 from the upper surface of a third fixed blade 132 which immediately follows the second fixed blade 132.

As more fully detailed below, each of these fixed blades 132 can be virtually divided into at least three portions S1, S2, S3 which have specific characteristics which allow each of these fixed blades 132 to direct the air flow. to Rate of rotation of the radial propeller.

Figures 5 to 7 illustrate, respectively, a cross section of a first portion S1 of one of these fixed blades 132, a cross section of a second portion S2 of the same fixed blade 132 and a cross section of a third portion S3 of this fixed blade 132, the cross section of the first portion SI being produced along a first transverse plane AA located at a first distance r1 from a center 230 of the guide member 130, the cross section of the second portion S2 being produced according to a second transverse plane BB located at a second distance r2 from the center 230 of the guide member 130 and the cross section of the third portion S3 being produced according to a third transverse plane CC located at a third distance r3 from the center 230 of the guide member 130, the first transverse plane AA, the second transverse plane BB and the third transverse plane CC each being perpendicular to the radial extension axis X of the fixed blade 1 32 concerned. As shown, the first distance r1, the second distance r2 and the third distance r3 are measured between the center 230 of the guide member 130, in this case merged with a center of the support 131 of the member for setting the propeller in motion, and the leading edge 135 of the fixed blade 132 concerned. According to the example illustrated here, the first distance r1 is equal to or substantially equal to 80 mm, the second distance r2 is equal to or substantially equal to 90 mm and the third distance r3 is equal or substantially equal to 100 mm. In other words, the first portion SI, the second portion S2 and the third portion S3 of a fixed blade 132 are aligned, in this order along the axis of radial extension X of the fixed blade 132 concerned, between the internal end 133 of the fixed blade 132 concerned and the external end 134 of this fixed blade 132.

According to the example illustrated, a first angular difference al measured between a first straight line DI passing through the leading edge 135 in the first portion SI and a second straight line D2 passing through the leading edge 135 in the second portion S2 is included between 2.5 ° and 4.5 °. A second angular difference a2 measured between the second straight line D2 and a third straight line D3 passing through the leading edge 135 in the third portion S3 is between 3 ° and 5 °. More particularly, the first straight line DI passes through the center 230 of the guide member and a point of the leading edge 135 of the fixed blade 132 located at the first distance r1 from this center 230 of the guide member, the second straight line D2 passes through the center 230 of the guide member and a point of the leading edge 135 of the fixed blade 132 located at the second distance r2 from this center 230 and the third straight line D3 passes through the center 230 of the 'guide member and a point on the leading edge 135 of the fixed blade 132 located at the third distance r3 from this center 230.

With reference to Figures 5 to 7, we will first describe the characteristics common to the cross sections of each of these three portions S1, S2, S3 before giving the characteristics specific to each.

Thus, as described above, each fixed blade 132 comprises an intrados 137 and an extrados 138 interconnected by a leading edge 135 and by a trailing edge 136. It is noted that the cross section of a fixed blade 132 extends along a line of camber C between the leading edge 135 and the trailing edge 136. This line of camber C is inscribed in a circle C1, C2, C3, schematically and partially shown in dotted lines on the figures. figures.

The cross sections of the fixed blades 132 have a number of common dimensions. In particular, each fixed blade 132 has at least one chord line Ch and at least one maximum camber Hmax. The chord line Ch of a fixed blade 132 corresponds to the straight portion which extends between the leading edge 135 and the trailing edge 136 of this blade fixed 132. According to the example illustrated here, this chord line Ch has a dimension between 20.2 mm and 30.4 mm. The maximum camber Hmax of a fixed blade 132 corresponds for its part to a dimension of this fixed blade 132 measured between the chord line Ch and the line of camber C, parallel to a straight line d which extends perpendicular to the line of chord and which crosses the camber line C, the maximum camber Hmax corresponding to the largest dimension that can be measured in this way. According to the example illustrated, the maximum camber Hmax is between 3.1 mm and 4.7 mm. Also, a distance P. Hmax measured between the leading edge 135 of the fixed blade 132 and a point of intersection between the lower surface 137 and the line d perpendicular to the aforementioned chord line Ch and along which is measured the maximum camber, Hmax, is between 10 mm and 15.2 mm.

The cross sections of the portions of each fixed blade 132 are also characterized by a ratio between a first angle b 1 measured between the camber line C at the level of the leading edge 135 of the fixed blade 132 and a tangent to the circle C1, C2 , C3, at the leading edge 135 of this fixed blade 132 and a second angle b2 measured between the camber line C at the level of the trailing edge 136 and the tangent to the circle C1, C2, C3 at the level of the edge d attack 135 of this fixed blade 132.

According to the example illustrated, the ratio between the first angle bΐ and the second angle b2 measured in the first portion SI is between 0.03 and 0.07, the ratio between the first angle bΐ and the second angle b2 measured in the second portion S2 is between 0.05 and 0.12 and the ratio between the first angle bΐ and the second angle b2 measured in the third portion S3 is between 0.02 and 0.07. In other words, this ratio is substantially identical in the first portion S1 and in the third portion S3 and it is greater in the second portion S2.

These different ratios reflect the change in the curvature taken by each of the fixed blades 132 of the guide member 130 and which guides the air flow in the direction of the axis of rotation of the radial propeller. The operation of the ventilation device 100 according to the invention is more fully detailed below with reference to Figure 8.

For example, the first angle bΐ measured in the first portion SI is between 4 ° and 6.2 ° and the second angle b2 measured in this first portion S2 is between 85 ° and 128 °. The first angle bΐ measured in the second portion S2 can meanwhile be between 6 ° and 9.3 ° and the second angle b2 measured in this second portion S2 is included between 79.5 ° and 119.3 ° Finally, the first angle bΐ measured in the third portion S3 is between 3.4 ° and 5.2 ° and the second angle b2 measured in the third portion S3 is between 79 , 4 ° and 119.3 °.

FIG. 8 illustrates the ventilation device 100 in a vertical section taken along a vertical plane DD for example illustrated in FIG. 2 and thus makes visible the internal volume 210 of the housing 110 as well as the arrangement, in particular, of the propeller 120 and the member 130 for guiding the air flow within this internal volume 210 of the housing 110.

As mentioned above, the housing 110 extends along a main extension straight line D, between an air inlet port 111 and an air outlet port 112. The air inlet port 111 , the propeller 120, the guide member 130 and the air outlet 112 are aligned, in this order, along the main extension line D of the housing 110.

The propeller 120 is more particularly arranged so that its air inlet 126 opens onto the air inlet mouth 111 formed in the wall 114 of the housing 110. Under this propeller 120, that is to say between this propeller 120 and the air outlet 112, are arranged the support 131 of the member for setting the propeller in motion 120 and the air guide member 130, this air guide member 130 being interposed between the support 131 of the moving member and the wall 114 of the housing 110. As described above, the moving member - not shown here - can for example take the form of a electric motor and include a motor shaft which extends in the hub 121 of the propeller 120. Thus, the motor shaft drives the hub 121 in rotation, which makes it possible to drive the entire propeller 120 in rotation. , and in particular the movable blades 122 of this propeller 120, so as to generate the air flow LA.

As described above, the movable blades 122 of the propeller 120 extend between the bowl 123 of the propeller 120 and the edge 124 of this propeller 120. The bowl 123 of the propeller 120 presents, seen from the internal perimeter of the propeller 120, a convex shape. This bowl 123 is also crossed by the hub 121 of the propeller 120 adapted to receive the motor shaft of the actuator. As illustrated, the outer edge 220 of at least one movable blade 122 of the propeller 120 extends parallel to the rate of rotation R of the propeller 120. Advantageously, the outer edges 220 of all the movable blades 122 extend, respectively, parallel to the axis of rotation R of the propeller 120.

Note also that the internal edge 129 and the external edge 220 of each movable blade 122 have different heights and a different position. By "position different "the fact that the internal edge 129 of a movable blade 122 and the outer edge 220 of this movable blade 122 have an offset, along the axis of rotation R of the propeller 120, one by one. compared to each other. The term “height of an edge” is understood to mean a dimension of this edge measured parallel to the axis of rotation R of the propeller, between the bowl 123 and the edge 124 of this propeller 120. Thus, the internal edge 129 of a movable blade 122 of the propeller 120 has a height h1 greater than a height h2 of the external edge 220 of this propeller 120. In particular, it is possible for example to provide that the height h1 of the internal edge 129 d a movable blade 122 is between 36.6 mm and 55 mm and that the height h2 of the outer edge 220 of this same movable blade 122 is between 29 mm and 44 mm. In other words, a ratio between the height h1 of the internal edge 129 of a blade and the height h2 of the external edge 220 of this mobile blade 122 is between 1.1 and 1.9. The propeller 120 can also be characterized by an internal radius RI, this internal radius RI being measured in a plane perpendicular to the axis of rotation R of the propeller 120, between the axis of rotation R of the propeller 120 and a point of the bowl 123 located at the right of the internal edge 129 of one of the movable blades 122 of the propeller 120. In other words, this internal radius RI is measured between a center of the hub 121 and the internal edge 129 of one of the movable blades 122 of the propeller 120. For example, the internal radius RI of the propeller 120 is between 36 mm and 54 mm. Finally, the propeller 120 has an external radius R2 measured in the plane perpendicular to the axis of rotation R of the propeller 120, between this axis of rotation R and a point of the bowl 123 located to the right of the external edge 220 of one of the movable blades 122 of this propeller 120. For example, the external radius R2 of the propeller 120 may be between 64 mm and 96 mm.

As shown, this air flow FA enters the housing 110 through the air inlet 111, then enters the propeller 120 through the air inlet 126 of this propeller 120 before being there. evacuated by the radial air outlet 221 of this propeller 120. The first curvature 117c of the wall 114 of the housing 110 covers the edge 124 of the propeller 120 and the second curvature 118c of this wall 114 is arranged opposite the outlet radial air 221 of the propeller 120.

The air flow FA which leaves the propeller 120 thus abuts against the second curvature 118c of the wall 114 which causes a modification of the trajectory of this air flow FA which is thus directed towards the guide member 130 of air flow. In order to allow this straightening of the air flow FA at the outlet of the radial propeller 120, the second curvature 118c has, as previously described, a radius of curvature of between 23.1 mm and 34.7 mm, advantageously equal to or substantially equal to 28.9 mm. The air flow FA then enters the guide member 130 through the leading edges 135 of the fixed blades 132 of this control member. guide 130. As described above, these fixed blades 132 have a particular conformation which makes it possible to deflect at least part of the air flow FA which joins the guide member 130 to direct it towards the axis of rotation R of the 'propeller 120. The conformation of these fixed blades 132 is also such that another part of the air flow is little or not deviated by its passage through the guide member 130. In other words, it is understood that the shape of the wall 114 of the housing 110 and the shape of the fixed blades 132 of the guide member 130, as well as the spaces 139 formed between the successive fixed blades 132 of the guide member 130 make it possible to direct the air flow FA of so that the latter has a general direction between the air inlet 126 of the propeller 120 and the air outlet mouth 112 formed in the wall 114 parallel to the main extension line D of the housing 110, it even merged with the axis of rotation R of the propeller 120. Advantageously, the air flow FA is thus directed over an entire surface of the air outlet 112, including at its center where the axis of rotation R passes, which makes it possible to use the entire surface of the air filter 113 which covers this air outlet 112, thus improving the efficiency and the longevity of this air filter 113. It is understood from the above that the present invention provides a ventilation device in which the air flow moves according to a single general direction between the air inlet of the propeller and the air outlet of the housing.

The present invention should not, however, be limited to the means and configurations described and illustrated here and it also extends to any equivalent means and configuration as well as to any technically operative combination of such means. In particular, the shape and characteristics of the radial helix and of the air flow guide member could be changed without harming the invention as long as they fulfill the functions described in this document.

Claims

1. Ventilation device (100) for a system (200) for ventilation, heating and / or air conditioning of a vehicle, comprising at least one housing (110) which comprises at least one wall (114) delimiting an internal volume (210 ) in which are received at least one radial propeller (120) adapted to be driven in rotation and at least one guide member (130), the radial propeller (120) and the guide member (130) being configured to generate an air flow (FA) of general direction parallel to an axis of rotation (R) of the radial propeller (120) between an air inlet (126) of the radial propeller (120) and an outlet mouth air (112) formed in the wall (114) of the housing (110) of the ventilation device (100), at least part of the wall (114) of the housing (110) being configured to straighten the air flow (FA) at the outlet of the radial propeller (120), characterized in that the guide member (130) is configured to direct the air flow (FA) towards the axis of rotation (R) of the radi propeller ale (120).

2, A ventilation device (100) according to the preceding claim, wherein the guide member (130) of the air flow (FA) comprises a plurality of fixed blades (132) arranged axially between the radial propeller ( 120) and the air outlet (112).

3. Ventilation device (100) according to the preceding claim, wherein at least one fixed blade (132) of the guide member (130) of the air flow (FA) comprises at least one outer end (134) integral of the wall (114) of the housing (110).

4, A ventilation device (100) according to any preceding claim, wherein the radial propeller (120) comprises a plurality of movable blades (122), each movable blade (122) comprising an internal ridge (129) turned. towards the axis of rotation (R) of the radial helix (120) and an outer edge (220) facing away from the inner edge (129), at least one outer edge (220) extending in parallel to the axis of rotation (R) of the radial propeller (120).

5, A ventilation device (100) according to the preceding claim, wherein an internal radius (RI) of the radial propeller (120), measured between the axis of rotation (R) of the radial propeller (120) and l the internal edge (129) of one of the movable blades (122) of the radial propeller (120) in a plane perpendicular to the axis of rotation (R) of the radial propeller (120), is between 36 mm and 54 mm.

6. Ventilation device (100) according to any one of claims 4 or 5, wherein the internal edge (129) of a movable blade (122) has a height (hl), measured. parallel to the axis of rotation (R) of the radial propeller (120), greater than a height (h2) of the outer edge (220) of this movable blade (122), measured parallel to the axis of rotation (R) of the radial propeller (120).

7. A ventilation device (100) according to any one of claims 2 to 6, in the housing (110) of the ventilation device (100) comprises at least one upper part (115) which accommodates the radial propeller (120) and a lower part (116) which houses the guide member (130), the upper part (115) comprising at least a first convex curvature (117c) seen from the axis of rotation (R) of the radial propeller ( 120) and at least a second concave curvature (118c) seen from the axis of rotation (R) of the radial helix (120), the first curvature (117c) covering an edge (124) of the radial helix (120 ) and the second curvature (118c) being arranged opposite a radial air outlet (221) of the radial propeller (120).

8. Ventilation device (100) according to any one of the preceding claims, wherein the guide member (130) of the air flow (FA) comprises a plurality of fixed blades (132), at least one fixed blade. (132) of this guide member (130) of the air flow (FA) comprising an intrados (137) and an extrados (138) interconnected by a leading edge (135) and a trailing edge (136) ), the fixed blade (132) comprising a cross section, seen in a plane perpendicular to a radial extension axis (X) of the fixed blade (132) concerned, which extends along a camber line (C) between the leading edge (135) and the trailing edge (136), this line of camber (C) being inscribed in a circle (Cl, C2, C3), a first angle (bΐ) being formed between a tangent to the circle (Cl, C2, C3) at the leading edge (135) and the camber line (C) at the leading edge (135) and a second angle (b2) is formed between the tangent to the circle (Cl, C2, C3) at the leading edge (135) and the camber line (C) at the level of the trailing edge (136), the first angle (bΐ) being between 3 ° and 10 ° and the second angle (b2) being between 79 ° and 128 °.

9. Ventilation device (100) according to the preceding claim, wherein at least one fixed blade (132) of the guide member (130) of the air flow (FA) comprises a first portion (SI), a second portion (S2) and a third portion (S3), aligned in this order, along the axis of radial extension (X) of the blade (132) towards the wall (114) of the housing (110), a ratio between the first angle (bΐ) and the second angle (b2) measured in the first portion (SI) being between 0.03 and 0.07, the ratio between the first angle (bΐ) and the second angle (b2) measured in the second portion (S2) being between 0.05 and 0.12 and the ratio between the first angle (bΐ) and the second angle (b2) measured in the third portion (S3) being between 0.02 and 0.07.

10. Ventilation device (100) according to any one of the preceding claims, wherein the radial propeller (120) is adapted to be driven in rotation by at least one moving member (140), the housing (110). ) comprising at least one support (131) adapted to receive at least one member (140) for moving the radial propeller (120), and in which the guide member (130) is interposed between the support (131) adapted to receive at least one moving member (140) and the wall (114) of the housing (110).

11. Ventilation device (100) according to the preceding claim, wherein the guide member (130) of the air flow (FA) comprises a plurality of fixed blades (132) and wherein at least one fixed blade (132 ) of this guide member (130) of the air flow (FA) comprises at least one internal end (133) integral with the support (131) adapted to receive the member for setting in motion (140) and at least one end external (134) integral with the wall (114) of the housing (110).

12. A ventilation, heating and / or air conditioning system (200) for a vehicle, comprising at least one ventilation device (100) according to any one of the preceding claims, the ventilation system (200) comprising at least one heat exchanger. heat (202) configured to effect a heat exchange between the air flow (FA) channeled by the ventilation device (100) and a cooling fluid.