The present disclosure relates to a heat exchanger. More particularly, the present disclosure relates to a multi-cooling heat exchanger for cooling two or more fluids while reducing the strain on the heat exchanger which occurs due to the different temperatures of the two or more fluids.
This section provides background information related to the present disclosure which is not necessarily prior art.
The conventional multi-cooling heat exchanger includes a core portion having a plurality of tubes, a header tank attached to both ends of the tubes, a plurality of fins disposed between adjacent tubes and an insert or side plate that provides stability to the heat exchanger. The header tanks are separated along their length to provide two or more separate cooling sections for the heat exchanger. A first fluid flows through the first section of the header tanks and tubes and a second fluid flows through the second section of the header tanks and tubes. Typical examples of the first fluid is refrigerant from an air conditioning system and a typical example for the second fluid is transmission oil. Both fluids are cooled as they pass through the plurality of tubes.
These multi-cooler heat exchangers develop a high amount of thermal strain. This is due to one of the fluids having a higher operating temperature than the other fluid. This temperature difference leads to a higher thermal expansion in the cooling section which cools the higher temperature fluid. Since both sections of the tubes are constrained by the header tanks, thermal strain occurs.
To alleviate this thermal strain, it is known to saw cut one or both of the header tanks to allow the higher temperature fluid section to expand freely and reduce the thermal strain. This method is effective but it adds labor and production time to the process. Another method for reducing this thermal strain is to make a saw cut in the insert or side plate. During cold weather operation, the plurality of tube expand due to increased temperature and the insert or side plate tends to heat up at a slower rate which causes a second source of thermal strain. The saw cut in the insert or side plate reduces this thermal strain but it still requires additional labor and production time.
This section provides a general summary of the disclosure, and is not a comprehensive disclosure of its full scope or all of its features.
The present disclosure allows for the cooling of two or more fluids which flow in parallel through different sections of the plurality of tubes. The thermal strain is reduced in the present disclosure by providing intermediate tanks between the two header tanks. The two tanks are spaced from each other to define an open gap between them which allows for the difference in thermal expansion of the different sections of the heat exchanger.
Further areas of applicability will become apparent from the description provided herein. The description and specific examples in this summary are intended for purposes of illustration only and are not intended to limit the scope of the present disclosure.
The drawings described herein are for illustrative purposes only of selected embodiments and not all possible implementations, and are not intended to limit the scope of the present disclosure.
Corresponding reference numerals indicate corresponding parts throughout the several views of the drawings.
Example embodiments will now be described more fully with reference to the accompanying drawings. Referring now to
Each of the first, second and third plurality of tubes 12, 14, 16 are arranged in parallel to each other and each tube is flat so that the direction of the air flow (perpendicular to the page in
First and second header tanks 30 and 32 extend in the stacking direction of the plurality of tubes 12, 14, 16 and the plurality of fins 18, 20, 22 perpendicular to the length of the plurality of tubes 12, 14, 16. First header tank 30 includes a first inlet 42, a first outlet 44 and a second outlet 46. A first internal baffle (not shown) separates first inlet 42 from first outlet 44 and a second baffle (not shown) separates first inlet 42 from second outlet 46. Second header tank 32 includes a second inlet 48. A third internal baffle separates second inlet 48 from the lower portion of second header tank 32. First and second intermediate tanks 34 and 36 are disposed adjacent each other as shown in
First side plate 24 extends along the lower end of the first plurality of fins 18. Second side plate 26 extends along the upper end of the second plurality of fins 20. Third side plate 28 extends along the upper end of the third plurality of fins 22. First, second and third side plates 24, 26 and 28 provide support for core portion 40.
The first plurality of tubes 12 are in fluid communication with first and second header tanks 30 and 32. The second plurality of tubes 14 are in fluid communication with first header tank 30 and first intermediate tank 34. The third plurality of tubes 16 are in fluid communication with the second intermediate tank 36 and the second header tank 32. As discussed above, first intermediate tank 34 is in fluid communication with second intermediate tank 36 through the one or more flexible jumper tubes 38 illustrated in
Thus, heat exchanger 10 defines two heat exchanging sections which have different fluids flowing through the sections. In the lower section, a first fluid is introduced into first inlet 42 into first header tank 30. The first fluid flows from first header tank 30 through a portion of the first plurality of tubes 12 to second header tank 32 where the first fluid makes a turn and returns to first header tank 30 through the other portion of the first plurality of tubes 12 and leaves first header tank 30 through first outlet 44. In the upper section, a second fluid, different from the first fluid, is introduced into second inlet 48 into second header tank 32. The second fluid flows from second header tank 32 through the second plurality of tubes 14 and into first intermediate tank 34, through the one or more flexible jumper tubes 38 into second intermediate tank 36. The second fluid flows from second intermediate tank 36 through the third plurality of tubes 16 and into first header tank 30 and leaves first header tank 30 through second outlet 46.
If the temperature of the second fluid is higher than the temperature of the first fluid the differences in the thermal expansion of the plurality of tubes 12, 14, 16 is compensated for by open gap 56 which reduces and/or eliminates the thermal strain which could occur due to the differences in thermal expansion of the plurality of tubes 12, 14, 16. The one or more flexible jumper tubes 38 permit the movement between first intermediate tank 34 and second intermediate tank 36.
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Each of the first, second and third plurality of tubes 12, 14, 16 are arranged in parallel to each other and each tube is flat so that the direction of the air flow (perpendicular to the page in
First and second header tanks 130 and 132 extend in the stacking direction of the plurality of tubes 12, 14, 16 and the plurality of fins 18, 20, 22 perpendicular to the length of the plurality of tubes 12, 14, 16. First header tank 130 includes first inlet 42; first outlet 44, second outlet 46, and second inlet 48. A first internal baffle (not shown) separates first inlet 42 from first outlet 44, a second baffle (not shown) separates first inlet 42 from second outlet 46 and a third internal baffle separates second outlet 46 from second inlet 48. Second header tank 132 includes a third inlet 50 and a third outlet 52. An internal baffle (not shown) separates third inlet 50 from third outlet 52. First and second intermediate tanks 34 and 36 are disposed adjacent each other as shown in
First side plate 24 extends along the lower end of the first plurality of fins 18. Second side plate 26 extends along the upper end of the second plurality of fins 20. Third side plate 28 extends along the upper end of the third plurality of fins 22. First, second and third side plates 24, 26 and 28 provide support for core portion 40.
The first plurality of tubes 12 are in fluid communication with first and second header tanks 130 and 132. The second plurality of tubes 14 are in fluid communication with first header tank 130 and first intermediate tank 34. The third plurality of tubes 16 are in fluid communication with the second intermediate tank 36 and the second header tank 132. As discussed above, first intermediate tank 34 is not in fluid communication with second intermediate tank 36.
Thus, heat exchanger 10 defines three heat exchanging sections which have different fluids flowing through the sections. In the lower section, a first fluid is introduced into first inlet 42 into first header tank 130. The first fluid flows from first header tank 130 through a portion of the first plurality of tubes 12 to second header tank 132 where the first fluid makes a U-turn and returns to first header tank 130 through the other portion of the first plurality of tubes 12 and leaves first header tank 130 through first outlet 44. In one of the upper sections, a second fluid, different from the first fluid, is introduced into second inlet 48 into first header tank 130. The second fluid flows from first header tank 130 through a portion of the second plurality of tubes 14 and into first intermediate tank 34 where the second fluid makes a U-turn and returns to first header tank 130 through the other portion of the second plurality of tubes 14 and leaves first header tank 130 through second outlet 46. In the other of the upper sections, a third fluid, different than the first and second fluids, is introduced into third inlet 50 into second header tank 132. The third fluid flows from second header tank 132 through a portion of the third plurality of tubes 16 and into second intermediate tank 36 where the third fluid makes a U-turn and returns to the second header tank 132 through the other portion of the third plurality of tubes 16 and leaves second header tank 132 through third outlet 52.
If the temperature of the second fluid and/or the third fluid is higher than the temperature of the first fluid the differences in the thermal expansion of the plurality of tubes 12, 14, 16 is compensated for by open gap 56 which reduces and/or eliminates the thermal strain which could occur due to the differences in thermal expansion of the plurality of tubes 12, 14, 16.
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The foregoing description of the embodiments has been provided for purposes of illustration and description. It is not intended to be exhaustive or to limit the invention. Individual elements or features of a particular embodiment are generally not limited to that particular embodiment, but, where applicable, are interchangeable and can be used in a selected embodiment, even if not specifically shown or described. The same may also be varied in many ways. Such variations are not to be regarded as a departure from the invention, and all such modifications are intended to be included within the scope of the invention.
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Number | Date | Country | |
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20110240275 A1 | Oct 2011 | US |