The invention relates to the field of heat exchangers and more specifically to heat exchangers having a bundle of tubes and comprising end flanges.
Heat exchangers, for example air/heat-transfer fluid exchangers, generally include a heat exchange bundle comprising a plurality of stacked tubes. At the ends of the heat exchange bundle is arranged a manifold inside which the heat-transfer fluid is intended to circulate so that it circulates within the tubes. The air circulates between the tubes.
On either side of the stack of tubes of the heat exchange bundle, the heat exchanger generally comprises end flanges brazed to the heat exchange bundle. These end flanges allow in particular the attachment of an aerodynamic element such as a deflector or a seal in order to block or deflect the circulation of air on the sides of the heat exchanger. In order to attach this aerodynamic element, the edges of the end flange are raised to form a rim with which the aerodynamic element engages.
However, the fact that the edges of the end flange are raised may result in a decrease in the surface area for contact between said end flange and the heat exchange bundle. Consequently, the useful surface area for brazing between the end flange and the heat exchange bundle is also reduced and this can lead to end flange attachment defects. This is particularly the case with thin heat exchangers, for example having a thickness between 12 and 18 mm.
One of the aims of the present invention is to at least partially overcome the drawbacks of the prior art and to provide a heat exchanger with improved attachment of the end flanges.
The present invention therefore relates to a heat exchanger, in particular for a motor vehicle, comprising:
This difference in width makes it possible to increase the general surface area of the flat body and in particular its second surface. Thus, the useful surface area for attaching the end flange to the heat exchange bundle is enlarged and allows better attachment. This is particularly useful in the case of thin heat exchangers which have a width of between 12 and 18 mm, for example.
According to one aspect of the invention, an extension is arranged between each pair of attachment tabs arranged along the sides of said flat body.
According to another aspect of the invention, the attachment tabs on a first side of the flat body are arranged facing the attachment tabs on a second side opposite to the first side, and that the extensions on the first side of the flat body are arranged facing the extensions on the second side.
According to another aspect of the invention, the attachment tabs on a first side are arranged facing the extensions on a second side opposite to the first side, and that the extensions on the first side are arranged facing the attachment tabs on the second side.
According to another aspect of the invention, the attachment tabs have at their top a hooking rim configured to retain the aerodynamic element.
According to another aspect of the invention, the attachment tabs on a same side are connected at their top by the hooking rim.
According to another aspect of the invention, the attachment tabs and the extensions of the flat body are integral with said flat body.
According to another aspect of the invention, the attachment tabs and the extensions of the flat body are produced by stamping.
Further features and advantages of the invention will emerge more clearly on reading the following description, provided by way of illustrative and non-limiting example, and the appended drawings, in which:
In the various figures, identical elements bear the same reference numbers.
The following embodiments are examples. Although the description refers to one or more embodiments, this does not necessarily mean that each reference relates to the same embodiment, or that the features apply only to a single embodiment. Individual features of different embodiments can also be combined and/or interchanged to provide other embodiments.
In the present description, certain elements or parameters may be designated as first element or second element, for example, or first parameter and second parameter or first criterion and second criterion, etc. In this case, it is simply a designation to differentiate between and name elements or parameters or criteria that are similar but not identical. Such designation does not imply that one element, parameter or criterion has priority over another and such names can easily be interchanged without departing from the scope of the present description. Such designation also does not imply any chronological order, for example in assessing any given criterion.
Between the tubes 5 are arranged interfering elements (not shown), for example fins, for disturbing the flow of the second heat-transfer fluid, for example air, intended to circulate between said tubes 5.
On each side of the stack of tubes 5, there is an end flange 13. This end flange 13 is made of metal, preferably the same metal as the tubes 5 or the interfering elements. The end flange 13 is brazed to the heat exchange bundle 3. It may be brazed directly to a tube 5 or to a disturbing element placed on the side of the stack of tubes 5. This end flange 13 is configured to allow the attachment of an aerodynamic element 15, for example a deflector, or a seal in order to block or deflect the circulation of the second heat-transfer fluid on the sides of the heat exchanger 1.
The end flange 13 also has attachment tabs 132 configured to receive the aerodynamic element 15. These attachment tabs 132 are arranged on the sides of said flat body 130 and project in the opposite direction to the heat exchange bundle 3.
These attachment tabs 132 may in particular include, at their top, a hooking rim 136 configured to retain the aerodynamic element 15. This hooking rim 136 may in particular constitute a recess in the attachment tab 132 on which is hooked a hooked rim 154 (visible in
The attachment tabs 132 may in particular be integral with the flat body 130. The attachment tabs 132 may thus be produced by stamping. The hooking rim 136 must be contained within the total width of the end flange 13 and thus, in the area of the attachment tabs 132, the width of the flat body 130 and therefore the second surface 130b is reduced accordingly.
The aerodynamic element 15 may also include a leg 152 intended to bear on the first surface 130a of the end flange 13. The aerodynamic element 15 may be made of plastic or elastomer. The aerodynamic element 15 may be fitted on the end flange 13 by elastic deformation so that its hooked rims 154 engage with the hooking rims 136 of the attachment tabs 132 on both sides of the end flange 13. The aerodynamic element 15 may also be fitted on the end flange 13 by sliding along the end flange 13.
According to a first variant shown in
According to a second variant shown in
Returning to
These extensions 134 are in particular arranged between the attachment tabs 132 of the pair of attachment tabs 132 such that the width L1 of the flat body 130 between the pair of attachment tabs 132 and an attachment tab 132 arranged on the opposite side of said flat body 130, facing the pair of attachment tabs 132, is less than the width L2 of the flat body 130 at the at least one extension 134. This difference in width makes it possible to increase the general surface area of the flat body 132 and in particular its second surface 130b. Thus the useful surface area for attaching the end flange 13 to the heat exchange bundle 3 is enlarged and allows better attachment. This is particularly useful in the context of thin heat exchangers 1 which have a width of between 12 and 18 mm, for example. These extensions 134 preferably have a length such that the total width of the sealing flange 13 does not exceed that of the heat exchanger 1.
The extensions 134 may also in particular be integral with the flat body 130. The extensions 134 may thus be produced by stamping.
The fact that the extensions 134 and the attachment tabs 132 may be integral with the flat body 130 allows the end flange 13 to be produced in one piece, which gives it greater strength. More particularly the extensions 134 and the attachment tabs 132 may be produced by stamping.
Thus, it can be clearly seen that by virtue of the structure of the end flange 13 with alternating attachment tabs 132 and extensions 134, the second surface 130b is increased, allowing better attachment by brazing of the end flange 13 to the heat exchange bundle 3.
Number | Date | Country | Kind |
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1873426 | Dec 2018 | FR | national |
Filing Document | Filing Date | Country | Kind |
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PCT/FR2019/053198 | 12/19/2019 | WO | 00 |