BRIEF DESCRIPTION OF THE DRAWINGS
FIG. 1 is a front elevation of a radiator embodying the present invention;
FIG. 2 is a front perspective view of the radiator of FIG. 1;
FIG. 3 is an enlarged front elevation of a PTO section of the heat exchanger of FIG. 1;
FIG. 4 is an enlarged front perspective view of the PTO section of FIG. 3;
FIG. 5 is a perspective view from above of a tank/transfer tube assembly of the heat exchanger of FIG. 1;
FIG. 6 is a perspective from below of the tank/transfer tube assembly of FIG. 5;
FIG. 7 is a perspective view of a internal side piece of the heat exchanger of FIG. 1;
FIG. 8 is an enlarged view of a portion of the side piece of FIG. 7;
FIG. 9 is a perspective view showing selected components of FIGS. 1-8 in an assembled state; and
FIG. 10 is an enlarged front view of a portion of FIG. 9;
FIGS. 11 and 12 are perspective views of a pair of core subassemblies prior to assembly into the heat exchanger of FIG. 1; and
FIG. 13 is a front elevation of an alternate embodiment of a radiator embodying the present invention.
DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS
With reference to FIGS. 1 and 2, a heat exchanger 10 is shown as an air cooled radiator for the coolant of an engine, and includes a so-called “PTO” section in the form of an opening 12 extending through a fin and tube core 14 of the heat exchanger 10. The heat exchanger 10 also includes a pair of primary tube plates or headers 16 and 18 connected to opposite ends 20 and 22 of the core 14. Although not shown, tanks of any suitable form can be connected to the headers 16 and 18 in order to distribute and/or collect the coolant from the core 14. It should be appreciated that while the heat exchanger 10 is described herein in connection with the illustrated radiator, the invention may find use with other types of heat exchangers and accordingly is not limited to radiators unless expressly recited in the claims.
While any suitable fin and/or tube constructions can be used, in a preferred form, the core 14 includes a plurality of spaced, parallel flattened tubes 24 (only six shown in FIG. 1 for purposes of illustration) with corrugated fins 26 (again only three partially shown for purposes of illustration) extending between adjacent pairs of the tubes 24 in a so-called parallel flow type construction. The core 14 is divided into a first core section 30, a second core section 32, a third core section 34, and a fourth core section 36, again with each of the sections 30, 32, 34 and 36 being formed from the flattened tubes 24 and corrugated fins 26.
As best seen in FIG. 3, the opening 12 is bounded on a first side 40 by a header/tank assembly 42 connected to an end 44 of the first section 30, on a second side 46 opposite from the first side 40 by another header/tank assembly 48 connected to an end 50 of the second section 32, on a third side 52 extending between the first and second sides 40 and 46 by a portion 54 of the third section 34, and on a fourth side 56 opposite from the third side 52 by a portion 58 of the fourth section 36. In this regard, the portion 54 is preferably defined by a side piece 60 of the third section 34 and the portion 58 is preferably defined by a side piece 62 of the fourth section 36, with each of the side pieces 60 and 62 extending from one of the headers 16 to the other header 18. The header/tank assembly 42 includes a tube plate or header 64 that receives tube ends 66 of the tubes 24 of the first section 30, and a tank 68 connected to the header 64 to collect and/or distribute coolant to and from the tubes 24 (only two shown in FIG. 3 for purposes of illustration) of the first section 30. Similarly, the second header/tank assembly 48 includes a tube plate or header 70 receiving the tube ends 72 of the tubes 24 (again, only two shown) of the second section 32 and a tank 74 connected to the header 70 to collect and/or distribute coolant to and from the tubes 24 of the section 32. A pair of fluid conduits in the form of cylindrical tubes 80 and 82 extend between the tanks 68 and 74 in order to direct coolant from one of the tanks 68,74 to the other of the tanks 68,74. In this regard, as best seen in FIGS. 5 and 6, each of the tanks 68,74 include a pair of spaced conduit receiving openings 84 and 86 that receive one of the opposite ends 88 and 90 of each of the tubes 80 and 82. In a highly preferred form, the tanks 68 and 74 and the tubes 80 and 82 are provided as a subassembly 92 during construction of the heat exchanger 10 with the ends 88 of each of the tubes 80 and 82 having a deformed mechanical connection to the tank 68 so as to fix the tanks 68 with respect to the tubes 80 and 82, and the other end 90 of each of the tubes 80 and 82 being allowed to slide freely through its respective opening 84,86 so as to allow the tanks 74 to slide freely relative to the tubes 80 and 82. Preferably, the deformed mechanical connection is provided by swedging the end 84 or by staking the end 84 and the corresponding opening 88 or 90, with a hose connection type bead 93 being provided on each of the tubes 80 and 82 to prevent movement of the tank 68 down the length of the tubes 80 and 82. It should be appreciated that the deformed mechanical connection could just as easily be provided between the tank 74 and the ends 90, with the tank 68 being allowed to slide freely relative to the tubes 80 and 82.
As best seen in FIGS. 7 and 8, each of the side pieces 60 and 62 are formed from a metal strip and include a pair of spaced stops 94 and 96, preferably provided in the form of an elongate, transverse embossed louvers 100 and 102 that are formed from the material of the side piece 60,62 and provide a stop surface 106 and 108 in the form an edge of the louver. As best seen in FIGS. 9 and 10, each of the headers 64,70 abuts one set of the stops 94 and 96 to locate the header 64,70 with respect to the tube ends 66 received therein. While not required, it is preferred that each of the side pieces 60 and 62 also include one or more elongate, embossed stiffening beads 110 and 112 in order to enhance the structural strength of the opening 12.
While any suitable material may be used, it is preferred that all of the components of the heat exchanger (with the possible exception of the unshown tanks for the primary headers 16 and 18) be made from aluminum, with braze cladding provided where appropriate. In this regard, it is also preferred that the tanks 68 and 74 be drawn aluminum tanks.
During assembly of the heat exchanger 10, the tubes 24 and fins 26 of the third or fourth core section 34 or 36 are assembled into the core 14, with the corresponding side piece 60 or 62 located on an inboard side of the corresponding section 34,36 and an additional channel shaped side piece 118 located on an outboard side of the core section 34, 36. The tubes 24 and fins 26 of each of the core sections 30 and 32 are assembled separately as subassemblies, and then assembled into the core 14. The tubes 24 and fins 26 of the other of the third or fourth core section 34 or 36 are next assembled into the core 14, with the corresponding side piece 60 or 62 located on an inboard side of the corresponding section 34,36 and an additional channel shaped side piece 120 located on an outboard side of the other core section 34, 36. Once the core stack is completed, a headering fixture will be used to insert the ends 114 and 116 of the tubes 24 into the respective headers 16 and 18, and the ends 66 and 72 into their respective headers 64 and 70, with the headers 64 and 70 abutting the stops 94 and 96. Next, the subassembly 92 is inserted into the core 14, with the tanks 74 slid along the tubes 80 and 82 towards the tank 68 so that the subassembly 92 can be inserted between the headers 64,70, of the core section 30,32. The tank 74 is then slid in an opposite direction so that the tanks 68 and 74 can be connected to their respective header 64 and 70. While clad brazing material may be used for all of the components of the heat exchanger 10, it may be desirable to add a brazing wire or collar at the interface between each of the tubes 80 and 82 and one or both of the openings 88 and 90 in each of the tanks 68 and 74. A brazing fixture is then provided to support the core both longitudinally and laterally while the fins 24 and tubes 26 of the core 14, the primary headers 16 and 18, the secondary header/tank assemblies 42 and 48, and the tubes 80 and 82 are placed in a braze oven and brazed at the same time to form suitable braze joints at all of the respective interfaces and provide a leak-free design.
FIG. 13 shows an alternate embodiment of the heat exchanger 10 wherein the second core section 32 is eliminated and the opening 12 is bounded on the second side 46 by the primary header 18, rather than by the header/tank assembly 48 as in the embodiment of FIGS. 1-12. This embodiment can be assembled similar to the prior embodiment except that, obviously, there will be no assembly of the core section 32, and the tank 68 with the tubes 80 and 82 fixed thereto by the previously described deformed mechanical connection is assembled into the core 14, with the tubes 80 and 82 being allowed to slide freely through respective openings 120 and 122 in the header 18 so as to allow the tank 68 to be slid towards the header 118 for assembly of the core section 30 and associated header 64 into the core 14. After the core section 30 and the header 64 are assembled into the core 14, the tank 68 is slid together with the tubes 80 and 82 towards the header 64 to be connected therewith.
It should be appreciated that by brazing the components of the heat exchanger 10, including the components of the opening 12, the heat exchanger 10 can be manufactured in a simplified and more cost effective manner in comparison to constructions that require brazing and multiple weld steps. It should also be appreciated that the sliding tank structure of the subassembly 92 allows for the core sections 30, 32, 34 and 36 to be assembled in essentially conventional fashion, with the tanks 68,74 and tubes 80, 82 being added after. In this regard, it should be appreciated that by providing the stops 94 and 96, the headers 64 and 70 can be easily located with respect to the tubes 24 during assembly, which further allows the tanks 68 and 74 to be connected to the headers 64 and 70 while reacting the engagement force through the stops 94 and 96 to the side pieces 62 and 64.
Patent Application
20080006388
