This application is a National Stage of International Patent Application No. PCT/EP2012/069503, filed Oct. 2, 2012, which claims priority to and all the advantages of French Patent Application No. FR 11/58953, filed Oct. 4,2011, the content of which is incorporated herein by reference.
The invention relates to a heat exchanger, notably for a motor vehicle.
More particularly, the invention relates to a heat exchanger for a motor vehicle engine air supply circuit.
The invention relates to the general field of the supply of air to motor vehicle engines, more particularly to engines the charge air of which comes from a compressor or a turbocharger, so that it is then referred to as supercharged charge air.
It is known practice to cool the supercharged charge air leaving the compressor using a heat exchanger which is also referred to as a charge air cooler (or CAC for short).
In this case, the CAC heat exchanger allows the supercharged engine charge air to be cooled by exchange of heat with another fluid such as external air or a liquid such as the water from the engine cooling circuit, thus forming an exchanger of the air/air or liquid/air type.
Such exchangers generally comprise a heat exchange core bundle comprising a stack of tubes or plates defining respective circulation canals for the fluids, so as to allow an exchange of heat between the two fluids circulating within the core bundle.
The core bundle is, in the known way, housed in a casing. Such a casing may comprise end plates on each side of the stack of plates or of the tubes of the core bundle defining the fluid circulation canals, and generally one or more side walls connecting these end plates.
To allow the fluid to be admitted to and then removed from the core bundle, fluid inlet and outlet header tanks are, according to a known solution, attached to the casing that houses the heat exchange core bundle.
The casing that houses the core bundle has a structural role by contributing to the rigidity of the exchanger.
However, in operation, the boost pressure may deform the casing, particularly the side walls of the casing.
This pressure leads to a level of mechanical stress which may exceed the limit of the material used.
It is known practice to increase the thickness of the material or even to provide additional components in order to withstand such mechanical stresses.
Moreover, in order notably to limit the cost of manufacture of an exchanger there is an increasing tendency toward a reduced thickness of materials. However, that leads to reduced ability to withstand the mechanical stresses.
It is an objective of the invention to propose a heat exchanger that does not have the disadvantages of the prior art.
To this end, one subject of the invention is a heat exchanger, notably for a motor vehicle, said exchanger comprising:
characterized in that said casing has at least one stress absorption zone adjacent to said at least one inlet header tank so as to withstand the mechanical stresses applied to said casing as said fluid flows through said core bundle from said fluid inlet tank toward said fluid outlet tank.
Said exchanger may further comprise one or more of the following features, considered separately or in combination:
Other features and advantages of the invention will become more clearly apparent from reading the following description, given by way of nonlimiting illustration, and from studying the attached drawings in which:
In these figures, elements that are substantially identical bear the same references.
This exchanger is intended to be placed in an engine air supply circuit.
Such an exchanger 1 is notably configured to cool the supercharged charge air for a combustion engine of the motor vehicle.
This exchanger 1 comprises a core bundle of tubes or plates for exchange of heat between a first fluid such as the supercharged charge air and a second fluid such as a liquid coolant.
This core bundle of tubes or plates is housed in a casing 3.
The exchanger 1 further comprises a first header tank 5 for the inlet of the first fluid, and a second header tank 7 for the outlet of the fluid.
According to the embodiment described, the outlet tank 7 is fixed to the cylinder head of the engine (the engine is not depicted) to allow cooled air to be admitted, and therefore forms an admission tank for the first fluid.
According to the example illustrated, the casing 3 comprises for example:
According to the embodiment illustrated, the exchanger 1 comprises a first side wall 11 adjacent to the inlet tank 5, and a second side wall 12.
The first side wall 11 is arranged near the inlet tank 5 and is therefore situated substantially level with the arrival of the supercharged charge air relative to the direction in which the air flows.
It is therefore referred to as a frontal wall 11 relative to the direction in which the fluid flows. The rear part of the exchanger 1 is defined by the outlet tank 7 mounted on the cylinder head of the engine (the engine is not depicted).
The side wall or walls 11, 12 have zones of connection to the end plates 9.
In the example illustrated, the side walls 11, 12 respectively have peripheral borders 15, 17 which are bent over for connection to the end plates.
These borders 15, 17 are bent over along a bent edge 19.
These borders 15, 17 are held on the end plates 9 for example by crimping.
The assembly is then for example brazed thereafter.
The casing 3 further comprises at least one stress absorption zone for withstanding the stresses applied to the casing 3 as the supercharged charge air flows.
The absorption zone or zones are arranged adjacent to the inlet tank 5.
According to the embodiment illustrated in
This for example involves providing a substantially convex surface 13 on the side wall 11, as indicated schematically in
The convex face is oriented in the general direction of stresses applied to the casing 3 as the supercharged charge air flows, as schematically indicated by the arrow F.
This convex surface 13 is in this instance arranged substantially at the center of the side wall 11.
In addition, this convex surface 13 extends substantially over the whole of the side wall 11.
This surface 13 therefore extends substantially over the whole height and over the whole width of the side wall 11.
Such a convex surface 13 makes it possible to limit the movements of the surface of the side wall 11 as the supercharged charge air flows from the inlet tank 5 toward the outlet tank 7.
Specifically, a side wall 11 is obtained that is more rigid and therefore better able to withstand the mechanical stresses applied to the side wall 11 as the supercharged charge air flows toward the engine (not depicted).
It is therefore possible, for the same order of ability to withstand the mechanical stresses, to provide a side wall 11 that is thinner than in the prior art. By way of example, for the same order of strength, it is possible to come down from a wall 3 mm thick to a wall 1.5 mm thick having such a convex surface 13.
According to an alternative form of the embodiment, provision may be made for the side wall 11 to have two convex surfaces 13 rather than just one, as illustrated in
With these two convex surfaces 13, the side wall 11 is even stronger, making it possible to reduce the thickness of the wall 11 still further.
The casing 3 may also have stiffening means (not depicted in the figures).
These stiffening means are formed as one with the casing 3. For example, the stiffening means are produced by deforming the casing 3.
The stiffening means are, for example, formed at the stress absorption zone or zones of the casing 3.
As an alternative or in addition to the convex surface 13, the side wall 11 may have such stiffening means.
By way of example of stiffening means, mention may be made of substantially cross-shaped deformations. Such a cross-shaped deformation may be provided substantially in the center of the side wall 11 or in the center of the convex surface or surfaces 13 of the wall 11.
As an alternative, deformations produced substantially in the form of domes may be provided.
According to an alternative form of the embodiment, the first side wall 11 may have stiffening means at the bent edge 19 of the peripheral borders 15 which are bent over for connection to the end plates 9.
Such stiffening means may for example be produced by deforming the material of the wall 11, for example by forming a boss, at the bent edge 19. These stiffening means have, for example, a substantially triangular shape with its vertex level with the bent edge 19 and its base connecting the bent-over peripheral border 15 and the side wall 11. Such stiffening means are generally referred to as “bulldozers”.
Furthermore, the casing 3 may comprise stress limitation means 21 in one or more zones of connection of the side wall or walls 11, 12 to the end plates 9.
According to the embodiment illustrated, the first side wall 11 comprises such limitation means 21 on its peripheral contours.
By way of example, the limitation means may comprise limitation grooves 21 (cf.
According to the embodiment illustrated, the first side wall 11 therefore comprises limitation grooves 21 on its peripheral contours forming zones of connection to the end plates 9.
Moreover, the casing 3 may also comprise inlet and outlet nozzles 23 for the second fluid (cf.
Referring once again to
The header tanks 5 and 7 are arranged in such a way that having passed through the core bundle, the cooled air leaves the exchanger 1 to be supplied to the engine.
For that, the inlet tank 5 communicates with an air inlet duct 25.
To allow cooled air to be admitted to each of the cylinders of the engine (not depicted), the outlet tank 7 is open to allow the cooled air to pass toward the engine.
The positioning of the inlet tank 5 and outlet tank 7 is given by way of illustration.
Thus, the supercharged charge air enters the exchanger 1 via the inlet tank 5 for the first fluid, circulates through the heat-exchange core bundle 3 then leaves the exchanger 1 via the outlet tank 7 for the first fluid so as to be fed to the engine (not depicted).
As for the second fluid, that enters the heat-exchange core bundle via an inlet nozzle 23 for the second fluid, circulates through the heat-exchange core bundle to exchange heat with the supercharged charge air that is to be cooled and then leaves the heat-exchange core bundle via an outlet nozzle 23 for the second fluid.
It will therefore be appreciated that such a heat exchanger casing 3 for admitting supercharged charge air to the combustion engine is better able to withstand the stresses applied as the air flows through the exchanger 1 because of the absorption zone provided for example by one or more convex surfaces of the side wall 11 adjacent to the inlet tank 5 and/or because of the variable-geometry deformations of this side wall 11.
Number | Date | Country | Kind |
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11/58953 | Oct 2011 | FR | national |
Filing Document | Filing Date | Country | Kind |
---|---|---|---|
PCT/EP2012/069503 | 10/2/2012 | WO | 00 |
Publishing Document | Publishing Date | Country | Kind |
---|---|---|---|
WO2013/050395 | 4/11/2013 | WO | A |
Number | Name | Date | Kind |
---|---|---|---|
4461348 | Toge | Jul 1984 | A |
5667004 | Kroetsch | Sep 1997 | A |
6675883 | De Keuster | Jan 2004 | B1 |
7631688 | Brost | Dec 2009 | B2 |
8844504 | Raduenz | Sep 2014 | B2 |
8905008 | Leroux | Dec 2014 | B2 |
9377252 | Garret | Jun 2016 | B2 |
20030145979 | Beddome et al. | Aug 2003 | A1 |
20030196785 | Knecht | Oct 2003 | A1 |
20040168791 | Batt | Sep 2004 | A1 |
20050016717 | Lamich | Jan 2005 | A1 |
20050161206 | Ambros | Jul 2005 | A1 |
20060048759 | Hendrix | Mar 2006 | A1 |
20060048923 | Domen | Mar 2006 | A1 |
20060278377 | Martins | Dec 2006 | A1 |
20070240863 | Kim | Oct 2007 | A1 |
20090194265 | Nakamura | Aug 2009 | A1 |
20110056652 | Neher | Mar 2011 | A1 |
20110120151 | Cutting | May 2011 | A1 |
20110168366 | Garret | Jul 2011 | A1 |
20140231054 | Martins | Aug 2014 | A1 |
Number | Date | Country |
---|---|---|
1134510 | Sep 2001 | EP |
2855604 | Dec 2004 | FR |
2933176 | Jan 2010 | FR |
WO2008138803 | Nov 2008 | WO |
WO2009156365 | Dec 2009 | WO |
WO2013050394 | Apr 2013 | WO |
Entry |
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English language abstract and machine-assisted English translation for FR2855604 extracted from espacenet.com database on Jul. 7, 2014, 12 pages. |
English language abstract for FR2933176 extracted from espacenetcom database on Jul. 7, 2014, 2 pages. Also see English equivalent US2011/0168366. |
English language abstract for WO2009156365 extracted from espacenet.com database on Jul. 7, 2014, 2 pages. Also see English equivalent US2011/0168366. |
International Search Report for PCT/EP2012/069502 dated Nov. 8, 2012, 7 pages. |
International Search Report for PCT/EP2012/069503 dated Nov. 7, 2012, 5 pages. |
U.S. Appl. No. 14/349,502, filed Apr. 3, 2014, 15 pages. This is the English Language Appln equivalent to WO 2013/050394. |
Number | Date | Country | |
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20140246181 A1 | Sep 2014 | US |