Heat exchangers of various kinds are commonly used to transfer thermal energy from a first, hotter fluid to a second, cooler fluid. As one example well-known in the art, an internal combustion engine in an automobile or truck is kept operating at a desirable temperature with the use of a liquid coolant loop that removes waste heat from the engine and transfers it to a lower temperature air stream in a heat exchanger (i.e. a radiator). Such radiators typically include a plurality of fluid conduits to convey the coolant through the radiator, with ambient air directed over the outer surfaces of the tubes to convectively transfer heat away from the outer surfaces of the fluid conduits.
It should be readily apparent that the rate of heat transfer required in the radiator in order to maintain such a desirable engine temperature (sometimes referred to as the thermal load) increases proportionally with the power output of the engine. Consequently, large power-intensive machinery (such as, for example, agricultural, construction and mining equipment) require large radiators in order to provide adequate heat rejection surface area for these thermal loads. Producing radiators of such a large size can be problematic.
Compact and highly efficient radiators for automobiles and trucks are often produced in a cost-effective manner by metallurgical joining of at least certain portions of the radiator in a furnace brazing operation. However, as the size of the radiator is increased the physical limitations of the furnace can be reached, and alternate construction methods that are less cost-effective and/or result in less compact and less efficient heat exchangers may be employed out of necessity. As an example, in some large equipment the radiator is constructed using a large number of individual finned heat exchange tubes inserted through grommet seals.
According to some embodiments of the invention, a heat exchanger assembly includes a pair of core units in an end-to-end arrangement and a fluid tank arranged between the core units. Each core unit includes a plurality of air fins arranged in parallel with one another and spaced apart from one another in a core stacking direction. Each core unit additionally includes a plurality of parallel arranged fluid conveying tubes located between and bonded to adjacent ones of the plurality of air fins. First and second spaced apart header plates sealingly receive the first and second ends, respectively, of the tubes. First and second side plates are located adjacent outermost ones of the air fins to define an outermost boundary of the core unit in the core stacking direction. The fluid tank includes a first end and a second end opposite the first end, the first end being sealingly attached to one of the first and second header plates of one of the pair of core units and the second end being sealingly attached to one of the first and second header plates of the other of the pair of core units. The fluid tank is located entirely within the outermost boundary of at least one of the pair of core units in the core stacking direction.
In some embodiments the fluid tank is sealingly attached to at least one of the pair of core units by a crimp joint. In some embodiments a gasket is included between the fluid tank and a header plate of at least one of the core units.
A heat exchanger assembly according to some embodiments of the invention additionally includes at least one of an inlet tank and an outlet tank sealingly attached to the other of the first and second header plates of the one of the pair of core units.
In some embodiments the heat exchanger assembly includes a second pair of core units adjacent to the first pair in the core stacking direction of at least one core unit. Some such embodiments include a structural frame supporting the first and second pair of core units. In some embodiments the center tank and the fluid conveying tubes of the first pair of core units together define a first fluid flow path and the center tank and the fluid conveying tubes of the second pair of core units together define a second fluid flow path. The first and second fluid flow paths are arranged in parallel with one another with respect to a fluid passing therethrough.
According to some embodiments of the invention, a heat exchanger includes first and second core units. Each core unit has a set of substantially parallel tubes extending in a direction through the core unit. Each of the tubes has first and second ends opposite one another. A header is coupled to the first ends of the set of substantially parallel tubes to form a fluid-tight seal. A tank is located between the first and second core units and has opposite ends. A header of each of the first and second core units is crimped in fluid-tight engagement with a respective one of the opposite ends. The tank has at least one interior space in fluid communication with interior spaces of the substantially parallel tubes of the first and second core units.
According to another embodiment of the invention, a method of servicing a heat exchanger includes disconnecting a first pair of core units from a second pair of core units, the first and second pairs of core units being supported by a common frame. The method can include terminating fluid communication between tubes of the first pair of core units and tubes of the second pair of core units by disconnecting the first pair of core units from the second pair of core units. The method can further include removing the first pair of core units from the frame while keeping the second pair of core units in place in the frame.
Before any embodiments of the invention are explained in detail, it is to be understood that the invention is not limited in its application to the details of construction and the arrangement of components set forth in the following description or illustrated in the following drawings. The invention is capable of other embodiments and of being practiced or of being carried out in various ways. Also, it is to be understood that the phraseology and terminology used herein is for the purpose of description and should not be regarded as limiting. The use of “including,” “comprising,” or “having” and variations thereof herein is meant to encompass the items listed thereafter and equivalents thereof as well as additional items. Unless specified or limited otherwise, the terms “mounted,” “connected,” “supported,” and “coupled” and variations thereof are used broadly and encompass both direct and indirect mountings, connections, supports, and couplings. Further, “connected” and “coupled” are not restricted to physical or mechanical connections or couplings.
A heat exchanger assembly 1 according to an embodiment of the present invention is shown in
Each core unit 2 comprises a tube and fin matrix 3 (shown in greater detail in
The air fins 10 or tubes 11 or both can be constructed from metallic materials, including but not limited to aluminum, copper, steel, and the like. Alternatively, the air fins 10 or tubes 11 or both can be constructed from nonmetallic materials such as, for example, plastic. Although not shown in the exemplary embodiment, in some embodiments the fluid conveying tubes 11 can include internal webbing, inserts, or other features to increase turbulence and thereby enhance heat transfer in order to satisfy specific requirements of the application for which the heat exchanger assembly 1 is intended.
The air fins 10 depicted in
The first and second header plates 5 of each heat exchange core 2 are spaced apart from one another in the tube-axial direction of the tubes 11 of said core unit 2. Each of the header plates 5 includes a plurality of tube slots 12 (
The first and second side pieces 6 of each core unit 2 are arranged adjacent outermost ones of the air fins 10 of the core unit 2 in order to bound the tube and fin matrix 3 in the core stacking direction A. In other words, the first and second side pieces 6 of a core unit 2 can define the outermost boundaries of the core unit 2 in the core stacking direction A. The side pieces 6 can be used during the joining of the tube and fin matrix 3 to apply a compressive load in the core stacking direction A in order to ensure that contact between adjacent ones of the air fins 10 and tubes 11 is maintained. In some embodiments, it can be advantageous for the side plates 6 to be joined to the outermost air fins 10. By way of example only, in some embodiments the air fins 10, fluid conveying tubes 11, header plates 5 and side pieces 6 can all be constructed of aluminum or an aluminum alloy, and can be joined together in one or more brazing operations to form a core unit 2.
The embodiment of
In order to prevent undesirable leakage of fluid from the heat exchanger assembly during operation, a fluid-tight seal can be provided between the tanks 7 and the corresponding header plates 5. In the exemplary embodiment of
The heat exchanger assembly 1 further includes an intermediate fluid tank 4 located between the first and second core units 2. One embodiment of such an intermediate tank 4 is shown in greater detail in
Ribs 17 can be included within the intermediate tank 4. These ribs 17 can be used to strengthen the intermediate tank 4 with respect to loads exerted by fluid pressure acting on the tank walls, and can also provide structural support for the heat exchanger assembly 1 (e.g., against forces tending to rotate or tilt one core unit 2 with respect to another). Additionally or alternatively, the ribs 17 can be used to prevent at least some re-mixing of the fluid within the intermediate tank 4. The ribs 17 shown in
The exemplary intermediate tank 4 of the illustrated embodiment includes first and second flanges 16 extending around each of the two open faces 15, similar to the flange 16 of the tank 7 in
In so joining the intermediate tank 4 to a core unit 2, the intermediate tank 4 can be advantageously located within the previously described core stacking direction outermost boundaries of the core unit 2. By having the intermediate tank 4 so located, multiple heat exchanger assemblies 1 can be placed immediately adjacent one another in the core stacking direction A. Also, the use of crimp joints between the intermediate tank 4 and the adjacent core units 2 (as described above) enables a maintenance-free compressed joint requiring no screws, bolts, or other separate fasteners, in one embodiment, while still providing a strong and stable connection between the core units 2.
In an alternative embodiment 101 of a heat exchanger assembly according to the present invention (shown in
The illustrated structural frame 107 includes a center rail 104 spanning between the side channels 103 to strengthen the heat exchanger assembly 101. Also with reference to the illustrated embodiment by way of example, fasteners 106 are used to secure the center rail 104 to the side rails 103, as well as to secure the intermediate tanks to the center rail 104 and to secure the inlet tanks and the outlet tanks to the end channels 102. The fasteners 106 used in the exemplary embodiment of
By utilizing a heat exchanger assembly 1, 101 as described above (having at least two core units 2 joined in end-to-end fashion via one or more intermediate tanks 4 as also described above), the overall heat exchanger assembly 1, 101 can be modular in nature. In particular, a user in some embodiments can partially disassemble the system to remove, service, repair, and/or replace one or more of the pairs of core units 2 and intermediate tank 4 as desired. In some embodiments, this action can be performed without disassembly or removal of the other core units 2 in the system.
With continued reference to the heat exchanger assembly 101 of
A heat exchanger assembly as described above can find utility as an engine coolant radiator for use in large machinery, such as construction, agricultural, and mining equipment, among others. In some embodiments, such a radiator is used to reject heat from a flow of coolant passing through the tubes of the core units to an air flow directed over the air fins and the outer surfaces of the tubes. It should be understood, however, that a heat exchanger assembly according to the present invention can find utility in other applications as well.
Several advantages can be realized through the use of a heat exchanger assembly as described. As one example, a highly effective brazed tube and fin core construction can be used to create a heat exchanger assembly that is larger in face area than can be accommodated within an available brazing furnace. The heat exchanger assembly can thus be constructed of compact core units that are compactly packaged together with minimal air blockage or bypass. As another example, individual core sections of the heat exchanger assembly can be replaced when damaged without needing to replace the entire heat exchanger assembly, thus decreasing the repair and replacement cost.
Various alternatives to certain features and elements of the present invention are described herein with reference to specific embodiments of the present invention. With the exception of features, elements, and manners of operation that are mutually exclusive of or are inconsistent with each embodiment described above, it should be noted that the alternative features, elements, and manners of operation described with reference to one particular embodiment are applicable to the other embodiments.
The embodiments described above and illustrated in the figures are presented by way of example only and are not intended as a limitation upon the concepts and principles of the present invention. As such, it will be appreciated by one having ordinary skill in the art that various changes in the elements and their configuration and arrangement are possible without departing from the spirit and scope of the present invention.
Various features and advantages of the invention are set forth in the following claims.
This application claims priority to U.S. Provisional Patent Application No. 61/415,588, filed Nov. 19, 2010, the entire contents of which are incorporated by reference herein.
Filing Document | Filing Date | Country | Kind | 371c Date |
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PCT/US11/60911 | 11/16/2011 | WO | 00 | 3/14/2013 |
Number | Date | Country | |
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61415588 | Nov 2010 | US |