Motor vehicle fan of reduced axial size

Abstract

A fan for a motor vehicle includes an impeller formed by multiple blades (3) extending radially from a hub (4), and a base supporting the impeller. The impeller is rotated about an axis of rotation by an actuator means and is positioned inside a hollow cylindrical cavity having the same axis and formed by an axial wall (25) attached to the base. The base includes an upstream front wall (22) extending externally in a radial plane with reference to the axis, and an outer wall (23) extending axially from the front wall (22). The front wall (22) has a protrusion (24) bordering the impeller, with the protrusion extending axially upstream with respect to the plane of the front wall (22). The upstream end of the protrusion is situated further upstream than the upstream end of the blades (3) of the impeller.

Claims

1. A fan for a motor vehicle, said fan comprising an impeller formed by multiple blades (3) and a base (2) supporting said impeller, said impeller being rotated about an axis of rotation (6), said base comprising an upstream front wall (22) extending externally in a radial plane with reference to said axis, and an outer wall (23) extending axially from said front wall (22), wherein said front wall (22) has a protrusion (24) bordering said impeller, said protrusion extending axially upstream with respect to the plane of said front wall (22), and the upstream end of which is situated further upstream than the upstream end of said blades (3) of said impeller, wherein said blades (3) are connected externally to a shroud (5), wherein said front wall (22) is positioned axially in the same plane as the upstream end of said blades (3) and/or of said shroud (5), and wherein said protrusion has the form of an axisymmetric rib (24) which extends as far as an inner radial end positioned radially inside the outer end of said blades (3) or of said shroud (5).

2. The fan as claimed in claim 1 in which said protrusion is circular, surrounding said impeller.

3. The fan as claimed in claim 1 in which said impeller is positioned inside a hollow cylindrical cavity having the same axis and formed by an axial wall (25) attached to said base (2).

4. The fan as claimed in claim 1 in which said rib (24) has, in radial section, a shape whose slope is continuously variable between said front wall (22) and said axial wall (25).

5. The fan as claimed in claim 1 in which said rib (24) is attached to said axial wall (25) in an axial direction or is oriented in a radial plane at its junction with said axial wall (25).

6. The fan as claimed in claim 1 in which said rib (24) forms a guide duct for the flow circulating between said shroud (5) and said axial wall (25).

7. The fan as claimed in claim 6 in which said rib (24) has, in radial section, a shape whose slope is continuously variable between the radial part of said front wall (22) and its inner radial end.

8. The fan as claimed in claim 1 in which said rib (24) is attached to said axial wall (25) in an axial direction.

9. The fan as claimed in claim 1 in which said rib (24) is oriented in a radial plane at its inner radial end.

10. A motor vehicle cooling module comprising a fan as claimed in claim 1.

Description

(1) The invention will be better understood, and other aims, details, features and advantages thereof will become more clearly apparent, from the following detailed explanatory description of a number of embodiments of the invention given by way of nonlimiting and purely illustrative examples with reference to the appended schematic drawings.

(2) In these drawings:

(3) FIG. 1 is a front view, from the upstream direction, of a fan for a motor vehicle, according to the prior art;

(4) FIG. 2 is a schematic view in radial section of the fan of FIG. 1;

(5) FIG. 3 is a simplified schematic view of FIG. 2;

(6) FIG. 4 is a perspective view of a fan for a motor vehicle, according to one embodiment of the invention;

(7) FIG. 5 is a simplified schematic view, in radial section, of the fan of FIG. 4, in a first embodiment;

(8) FIG. 6 is a simplified schematic view, in radial section, of the fan of FIG. 4, in a variant of the first embodiment;

(9) FIG. 7 is a simplified schematic view, in radial section, of the fan of FIG. 4, in a second embodiment;

(10) FIG. 8 is a simplified schematic view, in radial section, of the fan of FIG. 4, in a variant of the second embodiment; and

(11) FIG. 9 is a simplified schematic view, in radial section, of the fan of FIG. 4, in an additional variant of the first embodiment.

(12) FIG. 1 shows a front view of a fan 1 in which an impeller is inserted into a hollow cylindrical cavity placed at the center of a base 2 of parallelepipedal shape. The base has a substantially planer front wall 22 facing the ventilation air flow and an outer wall 23 which surrounds the front wall 22 and which forms a duct for feeding air into the fan 1. The impeller of the fan comprises a series of blades 3 which are attached, at their central end, to a hub 4 and, here, at their peripheral end, to a circular shroud 5. The fan 1 turns about a central axis 6 driven by an actuator means, in particular an electric motor 7 (visible in FIG. 2). FIG. 2 shows stator vanes 8 positioned downstream of the blades 3, the object of which is to serve as a support for the electric motor 7 and as a guide for the air flow leaving the fan. As on all fans there is an air recirculation current which passes from the downstream direction of the fan upstream while running around the ends of the blades 3 and which should be minimized. For this purpose, there has already been proposed a ring 9 in the form of a quarter-torus, visible in FIG. 2, which is placed between the downstream end of the blades 2 and the upstream end of the stator vanes 8 and which extends radially from the outer wall toward the inside of the fan. This quarter-torus 9 has the aim, using the Coanda effect, of preferentially deviating the air flow downstream of the blades 2 toward the stator 8 and thus preventing it from being oriented to the periphery, in the direction of the walls of the base 2, and from supplying the recirculation circuit. The Coanda effect consists in an attraction of a fluid jet by a wall when it circulates close thereto. It is generally used for producing a deviation of the orientation of the jet, choosing a curved wall for the wall, which is the case here with the quarter-torus shape of the ring 9.

(13) To reduce this recirculation flow further still, the shroud 5 has been given, in radial section, an L shape, the axial branch of which forms the support for the ends of the blades 3 and the radial branch of which covers the radially innermost cylindrical part 21 of the support 2. This inner radial part 21 forms the cylindrical cavity in which the impeller is positioned. To house the radial branch of the shroud 5, the support 2 has consequently been modified with the introduction of a shoulder formed by an L-shaped cutout between its inner radial part 21 and its front wall 22. This L-shaped cutout has a first radial wall 26, which is parallel to the radical branch of the shroud 5, and an axial wall 25 which faces this end of the radial branch of the shroud and which is connected to the front wall 22 of the base. Finally, as indicated above, the outer wall 23 is attached to the outer radial end of the front wall 22, said outer wall extending axially and forming a duct for feeding air into the fan. Axially, this outer wall 23 extends from the front wall 22 over a length which is determined by mechanical strength considerations for the assembly and which cannot be reduced without a harmful consequence.

(14) The resulting axial spacing between the upstream face of the shroud 5 and the upstream end of the outer wall 23 increases the overall axial size d of the fan, as can be seen in FIG. 3. This is what the invention proposes to correct.

(15) FIG. 4 shows a fan according to a first embodiment of the invention. The front wall 22 of the base 2 is not planar, as is the case in the prior art, but it has, at its inner radial end, a protrusion in the form of a lip 24 which extends upstream from the front wall 22 and which is connected, in an axial direction, to the axial wall 25 of the L-shaped cutout of the support 2. Consequently, the front wall 22 of the support 2 is in a position less advanced in the upstream direction with respect to the upstream face of the shroud 5 than in the prior art. In addition, therefore, the outer wall 23, which extends from this front wall and which may have the same axial extension as in the prior art, is, for its part too, less advanced axially with respect to the upstream face of the hub 4 or of the shroud 5. The axial size d of the fan is thus reduced.

(16) FIG. 5 shows, in a simplified manner, a first variant of the fan in the first embodiment. According to this variant, the lip 24 is inflected, going from the periphery inward, with a shape whose slope changes continuously, without break, before joining up with the axial wall 25 in an axial direction while being tangential thereto.

(17) In FIG. 6, which shows a second variant of the first embodiment, the axial position of the front wall 22 is unchanged with respect to the first variant, so as to keep the saving obtained in terms of the overall axial size d. But, by contrast with the first variant, the lip 24 has a break in its slope with a right angle at its connection with the axial wall 25 of the L-shaped cutout. The slope of the lip thus changes continuously until reaching a radial orientation, precisely where the lip is connected to the axial wall 25.

(18) In the first variant, the air which runs along the front part is subjected to a Coanda effect associated with the curve shape of the lip 24 and is directed more axially as it arrives at the end of the blades 3, thereby facilitating its mixture with the main air flow which traverses them. The second variant promotes, for its part, the return of the circulation air at the end of the blades toward the main flow, injecting the flow circulating along the front wall 22 in a radial direction, above the recirculation circuit.

(19) FIGS. 7 and 8 show, for their part, two variants of a second embodiment of the invention. In this second embodiment, the lip 24 is extended, at its most upstream part, toward the inside of the fan, such that it protrudes beyond and covers the outer radial end of the shroud 5. FIG. 7 represents the first variant with, as above, a rounded apex which is inflected, coming toward the inside, in the direction of the axial direction. Beyond this apex, the lip 24 is terminated by a turned-in point, from which it returns toward the outside while being directed downstream, in order to join up with the axial wall 25 of the L-shaped cutout in an axial orientation. This rounded shape makes it possible, as in the first embodiment, for the air flow which circulates along the front wall 22 to benefit from the Coanda effect and to straighten it in a more axial direction.

(20) FIG. 8 represents the second variant of the second embodiment with, as above, a radial orientation at the apex of the lip. In the same manner, it has a turned-in point and returns outward while being directed downstream, in order to join up with the axial wall 25 of the L-shaped cutout in an axial orientation. This second variant promotes, for its part too, the return, toward the main flow, of the circulation air at the end of the blades, by injecting the flow which circulates along the front wall 22 in a radial direction, above the recirculation circuit.

(21) In the above FIGS. 5 to 8, the front wall 22 is positioned axially in the same plane as said upstream end of the blades 3 and/or of the shroud 5.

(22) As illustrated in FIG. 9, this may also be situated downstream. It is here illustrated with a protrusion identical to that of FIG. 5 but it could of course be a protrusion having different shapes such as those illustrated in FIGS. 6 to 8.

(23) The principle of the invention therefore consists, with respect to the prior art, in reducing the axial size of the fan by offsetting downstream the front wall 22, and more particularly its upstream face, forming the front face of the parallelepipedal support 2, while keeping the same length for the outer wall 23. In order to compensate for this offset of the front wall 22 and once again find the improved aerodynamic operation which is associated with an injection of air circulating on the front wall 22 above the peripheral shroud 5, a lip 24 is introduced at the inner radial end of this front wall 22. This lip has the form of a rib, for example a rounded circular rib, which extends axially upstream above the front wall 22 and which is here connected in an axial orientation to the axial wall 25 facing the shroud 5. Thus, the air circulating on the front wall 22 is raised upstream to be injected into the main air flow without generating a vortex and therefore creating the least possible disturbance in this main flow.

(24) In the second embodiment, the lip 24 is extended above the outer radial end of the shroud 5, thus forming a guide duct for the recirculation flow which circulates between the shroud 5 and the axial wall 25 of the support 2. Moreover, it serves as a separator between the recirculation flows and the flow circulating on the front wall 22 prior to its injection into the main flow which traverses the blades 3.

(25) In a variant, not shown, of the second embodiment, it is possible to install guides below the part of the lip 24 which extends between the turned-in point and the axial wall 25, in order to straighten the recirculation flow and prevent it from acquiring a tangential speed by an entrainment effect of the shroud. These guides are plates oriented essentially radially which extend from the inner circle to the lip 24 and which have, on the opposite side to this circle, either a diagonal or curved edge facing the end of the shroud 5. By reducing the tangential component of the recirculation flow, it is thus possible to better manage the mixing thereof with the main flow.