This application is a U.S. national stage application of International Application No. PCT/FR2017/052184, filed on Aug. 3, 2017, which claims priority to French Patent Application No. 1657776, filed on Aug. 16, 2016.
The present invention relates to a closure element for closing a recess of a heat-transfer-fluid pump included in a heat engine of a vehicle, in particular in a cylinder block of the engine.
The invention also relates to a cylinder block including such a closure element as well as an engine including the cylinder block.
The invention also relates to a vehicle, in particular a motor vehicle, including such an engine.
In the prior art, a heat engine typically comprises a cylinder block sealed by a cylinder head. For the proper operation of the engine, the blocks must be cooled. To that end, the engine includes a cooling circuit in which a heat transfer fluid is circulated using a pump and which, in turn, is cooled by extending through a radiator. Such a pump is traditionally arranged in an outer surface of the engine, in particular on a distribution wall also referred to as an accessory wall of the engine. The pump in particular includes a pulley, which drives a blade, or turbine, suitable for circulating the fluid in the cooling circuit. The pulley of the pump is driven by a transmission belt, which as a general rule drives other elements of the vehicle such as the alternator, the assisted steering pump, etc.
It has been discovered that such an arrangement, however, has the drawback of being relatively bulky and complex to implement. It indeed causes them to be so bulky so as not to be suitable for the size of the engine compartment of modern vehicles, in particular in a context in which automobile builders and/or drivers are seeking, in light of the size of such compartments, to produce increasingly compact engines that nevertheless have improved performance in terms of power and/or efficiency, which often involves an increase in thermal loads in terms of the latter.
The present invention aims to overcome the drawbacks related to the prior art.
One aim of the invention is to reduce the size of the engine while making the cooling circuit more compact and easier to implement.
To that end, the invention relates to a closure element for sealing a recess of a heat-transfer-fluid pump included in a heat engine of a vehicle, in particular in a cylinder block of the engine, the closure element including an element for guiding the flow of heat transfer fluid to an inlet port of the pump.
In other embodiments:
The invention also relates to a cylinder block including such a closure element.
In other embodiments:
The invention also relates to a heat engine including such a cylinder block.
The invention also relates to a vehicle, in particular a motor vehicle, including such a heat engine.
Other advantages and features of the invention will be better manifested upon reading the description that follows of one preferred embodiment, done in reference to the figures, provided as an indicative and non-limiting example:
In the following description, identical reference numbers denote identical parts or parts having similar functions.
The cylinder block 1 includes a recess 3 in which the pump 4 is arranged. The recess 3 includes an inlet 17a connected to a heat transfer fluid supply pipe 21a included in the cooling circuit. The supply pipe 21a is defined in whole or in part in the cylinder block 1. The inlet 17a and the outlet 17b of the recess 3 are included in inner walls 22a, 22b of the recess 3.
The inlet 17a and the outlet 17b of the recess 3 respectively include axes of symmetry A2 and A3 that are substantially perpendicular to an axis of symmetry A1 of the pump 4. The axis A1 is also an axis of symmetry of a rotary device 26 of the pump 4 suitable for circulating fluid in the cooling circuit and that may be a blade or a turbine. In another embodiment, the inlet 17a of the recess 3 may be defined in the first part 7a of the closure element 2 with an axis of symmetry A2 of the inlet 17a that is combined with the axis of symmetry A1 of the pump 4.
The cylinder block 1 includes a closure element 2 that is arranged in the recess 3 in order to sealingly and removably seal the recess 3. In
The third part 7c includes a plurality of ports 30 to allow the low-pressure heat transfer fluid to pass through the third part 7c and to the turbine 26 of the pump 4.
When the closure element 2 is arranged in the recess 3, the first and second parts 7a, 7b separate/compartmentalize the recess 3 into two chambers 16a, 16b: a low-pressure chamber 16a and a high-pressure chamber 16b. The low-pressure chamber 16a is included between the first and second surfaces 8a, 9a of the first and second parts 7a, 7b, and is defined in the continuation of the heat transfer fluid supply pipe 21a. The high-pressure chamber 16b in turn is included between the second surface 9b of the second part 7b and a bottom wall 23 of the recess 3 and is defined in the continuation of the heat transfer fluid discharge pipe 21b.
The first surface 8a of the first part 7a of the closure element 2 includes a guiding element 5 of the heat transfer fluid that circulates in the recess 3 coming from the supply pipe 21a. The second surface 8b of the first part 7a forms a cavity contributing to improving the gripping comfort of the closure element 2 in order to arrange it in the recess 3 and decrease the weight of the closure element 2. The second surface 8b also includes at least one attachment area 15 making it possible to mechanically connect the closure element 2 to an outer surface 24 of the cylinder block 1 by screwing, clipping or snapping. Each attachment area 15 is preferably included at an edge 25 defining a perimeter of the second surface 8b. Thus, the closure element 2 is attached removably to the cylinder block 1. Such a configuration makes it possible to facilitate access to the pump 4 in order to perform maintenance and/or assembly/disassembly operations of the latter.
The second part 7b of the closure element 2 includes an opening 12. The opening 12 is defined to receive a part of the pump 4 provided with an inlet port 6 for the heat transfer fluid. The part of the pump 4 includes a supply inlet area 28 for an enclosure 18 of the pump 4 in which the rotary device 26 is arranged. In particular, the opening 12 includes a wall 13 comprising a guiding area 14 of the inlet area 28 provided with the inlet port 6 for supplying the pump 4 with fluid. The inlet area 28 of the enclosure 18 has a circular section having a diameter adjusted to that defined by the guiding area 14 of the opening 12 in order to guarantee a reduced play to encourage the heat transfer fluid to pass through the inlet area 28, while allowing the rotary device 26 to rotate in the guiding area 14.
The enclosure 18 of the pump 4 is arranged in the high-pressure chamber 16b of the recess 3. It includes ports 29 through which the pressurized heat transfer fluid is discharged after it passes through the rotary device 26 of the pump 4. The pressurized heat transfer fluid is discharged into the part of the pressurized chamber 16b forming the volute of the pump 4, also referred to as the receiving chamber of the pump 4. The rotary device 26 is mounted on one end of a pump shaft 19 connected to a pump body (not shown).
The first and second parts 7a, 7b of the closure element 2 each include at least one sealing element 10a, 10b. These two parts 7a, 7b include peripheral walls 11a, 11b where the sealing elements 10a, 10b protrude. Indeed, the peripheral wall 11a, 11b of each first and second part 7a, 7b includes a slot in which the sealing element 10a, 10b is arranged. The sealing element 10a, 10b is preferably a sealing O-ring. When the sealing element 2 is arranged in the recess 3, the sealing elements 10a, 10b cooperate with the inner walls 22a, 22b of the recess 3 so as to provide a hermetic connection. Thus, the sealing elements 10a, 10b contribute to making the low-pressure and high-pressure chambers 16a, 16b tight in the recess 3. It will be noted that these inner walls 22a, 22b are defined in the recess 3 according to a stepping that is necessary for the assembly of the O-rings 10a, 10b.
In the sealing element 2, the guiding element 5 is defined over all or part of the first surface 8a so as to steer the heat transfer fluid toward the inlet port 6 of the pump 4 and therefore toward the axis of the rotary device 26. The guiding element 5 includes a protuberance on the first surface 8a of the first part 7a of the closure element 2. The protuberance preferably has an essentially pyramidal or conical shape. Under these conditions, the protuberance has an apex 27 that extends in a direction perpendicular to the median plane P1 of the first part 7a, toward the inlet port 6 of the pump 4 and therefore toward the axis of the rotary device 26. The guide element 5 includes an axis of symmetry A4 that passes through its apex 27 and that is combined with the axes of symmetry A1, A5 respectively of the pump 4 and the opening 12 of the second part 7b of the closure element 2.
Thus, when the closure element 2 is arranged in the recess 3, the heat transfer fluid circulates in the recess along the direction of the arrows shown in
Number | Date | Country | Kind |
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16 57776 | Aug 2016 | FR | national |
Filing Document | Filing Date | Country | Kind |
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PCT/FR2017/052184 | 8/3/2017 | WO | 00 |
Publishing Document | Publishing Date | Country | Kind |
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WO2018/033670 | 2/22/2018 | WO | A |
Number | Name | Date | Kind |
---|---|---|---|
20110088638 | Yamagata | Apr 2011 | A1 |
20160084259 | Chiba | Mar 2016 | A1 |
Number | Date | Country |
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2016176712 | Nov 2016 | WO |
Number | Date | Country | |
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20200182126 A1 | Jun 2020 | US |