This invention relates to concentric tube heat exchangers, and more particularly to seals for closing an annular passageway between the inner and outer tubes of such heat exchangers.
Concentric tube heat exchangers are commonly employed as transmission and transaxle oil coolers and are mounted in the coolant tank or manifold of a vehicle radiator. These heat exchangers include a cylindrical outer tube, a cylindrical inner tube and a turbulizer placed in an annular passageway between the inner and outer tubes. Oil is admitted to the annular passageway via an inlet port located at one end of the tube for passage through the turbulizer. The oil is cooled and exits via an outlet port located near the other end of the outer tube.
Numerous arrangements are known in the prior art for sealing the ends of the annular passageway. These include deformation of the inner and/or outer tubes, for example as shown in U.S. Pat. No. 3,001,767 (Straubing), U.S. Pat. No. 5,732,769 (Staffa) and U.S. Pat. No. 5,950,716 (Appelquist et al.); or by use of annular seals as described in U.S. Pat. Nos. 3,323,586 and 3,339,260 (Burne et al.)
The suitability of prior art end sealing methods can be affected by the type of material from which the heat exchanger is made. For example, in aluminum concentric tube heat exchangers, it has proven difficult to seal the annular passageway by deformation of the tubes. This has led some manufacturers to seal the annular passageway with machined aluminum end blocks, which significantly increase the weight and cost of the heat exchanger.
Accordingly, there is a need for improved methods for sealing the annular passageway in a concentric tube heat exchanger which will provide economical and reliable sealing in a variety of materials.
In one aspect, the present invention provides a concentric tube heat exchanger having a first end and a second end. The heat exchanger comprises an outer tube and an inner tube. The inner tube is received inside the outer tube and concentric therewith, wherein an annular passageway is formed between the inner and outer tubes. The heat exchanger further comprises first and second annular sealing members received inside the annular passageway between the inner and outer tubes. The first sealing member is positioned proximate the first end of the heat exchanger and the second sealing member is positioned proximate the second end of the heat exchanger. Each of the sealing members comprises an outer wall and an inner wall which are connected to one another, each of the walls having first and second axially-spaced ends, the outer wall being sealed to the outer tube and the inner wall being sealed to the inner tube, thereby sealing the ends of the tubes.
The concentric tube heat exchanger according to the invention further comprises a turbulizer received in the annular passageway between the tubes. The turbulizer comprises a plurality of corrugations defining a plurality of axially extending flow passages extending parallel to the tubes. Each of the corrugations comprises a top land, a bottom land and a pair of side surfaces connecting the top and bottom lands, the top land being in heat exchange contact with the outer tube and the bottom land being in heat exchange contact with the inner tube. The convolutions are arranged in axially extending rows with the convolutions in each row being connected to one another and with an offset being provided between adjacent convolutions in each row. The offset has a width which is from about 30 percent to about 40 percent of a width of the top land or the bottom land.
In another aspect, the present invention provides a sealing member for sealing opposite ends of an annular passageway extending along an axis between inner and outer tubes of a concentric tube heat exchanger. The sealing member comprises an outer wall and an inner wall. The outer wall has first and second axially-spaced ends and a generally axially-extending portion between its ends for sealing to the outer tube. The inner wall has first and second axially-spaced ends, is connected to the outer wall and is spaced radially inwardly of the outer wall. The inner wall has a generally axially-extending portion between its ends for sealing to the inner tube. The generally axially-extending portions of the walls diverge from one another along said axis.
The invention will now be described, by way of example only, with reference to the accompanying drawings, in which:
Heat exchanger 10 further comprises an inlet port 18 located adjacent its first end 20 and an outlet port 22 (
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Lastly, the heat exchanger 10 comprises a pair of annular sealing members 32 for sealing the ends of the annular passageway 16. In
As shown in
The preferred sealing members 32 shown in the drawings each comprise an outer wall 42 and an inner wall 48, with the inner wall 48 being spaced radially inwardly of the outer wall 42, and preferably concentric therewith. The outer wall 42 has a first end 46 and a second end 44, the ends 44, 46 being axially spaced from one another, with at least a portion of the outer wall extending generally along the axis. Similarly, the inner wall has a first end 52 and a second end 50, the ends 50, 52 being axially spaced from one another, with at least a portion of the outer wall extending generally along the axis. In the sealing members 32 shown in the drawings, the entire outer and inner walls 42 and 46 extend along the axis, with the inner wall 48 abutting the outer surface of inner tube 14 and sealed thereto, and with the outer wall 42 abutting the inner surface of outer tube 12 and sealed thereto. However, it will be appreciated that this is not necessary that the entire outer and inner walls 42, 48 extend generally axially. Rather, it will be appreciated that only portions of walls 42, 46 are required to extend axially, sufficient to form seals with the outer and inner tubes 12, 14, respectively.
The sealing members 32 illustrated in the drawings are of generally U-shaped cross section, with the first end 46 of the outer wall 42 being connected to the first end 52 of the inner wall 48 by a radially extending connecting portion 54 which seals the radial space between the walls 42, 48. The second ends 44, 50 of the walls 42, 48 are distal to the connecting portion. Preferably, the connecting portion 54 is integrally formed with the walls 42, 48.
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In a particularly preferred embodiment of the present invention, all the components of heat exchanger 10 are formed from aluminum or alloys thereof, and are preferably formed from brazeable aluminum alloys. In particular, the tubes 12, 14 are preferably of welded and drawn construction and comprise an aluminum alloy core layer clad on at least one side with an aluminum brazing alloy. More preferably, the inner surface of the outer tube 12 and the outer surface of the inner tube 14, i.e. the “oil-side” surfaces, are clad with a brazing alloy, while the opposite surfaces of these tubes, i.e. the “water-side” surfaces, are clad with an alloy containing an amount of zinc for sacrificial corrosion protection. Where the oil-side surfaces of tubes 12, 14 are clad with a brazing alloy, it will be appreciated that neither the turbulizer 30 nor the sealing members 32 require a cladding of brazing alloy. It will be appreciated that alternate arrangements are possible, for example, the turbulizer 30 and sealing members 32 may be clad with brazing alloy, and the tubes 12, 14 may be unclad. Alternatively, all these components may be clad with a brazing alloy. In yet another alternative, the heat exchanger 10 may be comprised of non-clad aluminum members, and the filler metal for brazing may be provided by means of a brazing paste or preform, and brazing can be accomplished by either flux or fluxless brazing by suitable selection of the braze system and materials. Similarly, a brazing paste or preform can be used to join the fittings 26, 28 to the corrosion resistant clad water-side surface of the outer tube 12.
It will be appreciated that the sealing members 32 may be installed with the second ends 44, 50 of walls 42, 48 facing the inlet or outlet port 18, 22. However, for manufacturing purposes, it is preferred that the sealing members 32 are received in the annular passageway with the second ends 44, 50 of walls 42, 48 facing the ends 20, 24 of heat exchanger 10, as shown in the drawings.
The heat exchanger 10 is preferably by assembled by inserting the inner tube 14 and the turbulizer 30 into the outer tube 12, inserting the sealing members 32 into the opposite ends 20 and 22, expanding the inner tube so that both the outer and inner tubes 12, 14 are in intimate heat exchange contact with the turbulizer 30, applying the fittings to the outer tube, and then brazing the assembly in a brazing oven.
A preferred form of turbulizer 30 is now described below with reference to
The top lands 76 of the convolutions 74 are arranged in axially extending rows, as seen in
The features of turbulizer 30 described above are also present in the turbulizer described in the above-mentioned So patent. The turbulizer 30 according to the invention differs from the So turbulizer in several important respects, which are now discussed below.
Firstly, the turbulizer 30 according to the invention has a preferred offset WO which is significantly less than that of the So turbulizer, thereby maximizing the width of the area 84 along which the convolutions 84 are connected with one another. In the So turbulizer, the width of offset is about 50 percent of the width of the top and bottom lands, whereas the offset in the turbulizer 30 according to the invention is about 30 to 40 percent (i.e. WO/WT or WB=0.30-0.40), preferably about 31 to about 36 percent. The inventors have found that decreasing the offset of the convolutions 74 helps to ensure formability of the turbulizer 30 from metals such as aluminum, while providing high heat transfer and low pressure drop.
Secondly, the turbulizer 30 according to the invention is formed with the top land width WT which is greater than the bottom land with WB, and with the side surfaces 80 of each convolution 74 sloping away from one another from the top land 76 to the bottom land 78. Thus, when the turbulizer sheet 30 is rolled up and inserted into the annular passageway 16 with the bottom lands 78 in heat exchange contact with the inner tube 14 and the top lands 76 in heat exchange contact with the outer tube 12, the side surfaces 80 are extend substantially radially between the outer tube 12 and inner tube 14, producing axial flow passages of substantially constant cross-sectional area. This helps to maximize heat transfer and minimize pressure drop.
In a particularly preferred embodiment of the invention, the side surfaces are sloped at about 5° from vertical, the top land width WT is about 1.1 mm, the bottom land width WB is about 1.0 mm, the centers of rows 82 are spaced about 2.1 mm apart, and the offset with WO is about 0.35 mm. In a turbulizer having these dimensions, the offset expressed as a percentage of the top land width is about 31 percent and the offset expressed as a percentage of the bottom land width is about 36 percent.
The above-mentioned features of the turbulizer according to the invention, for example the top and bottom lands of different width, the radially extending side surfaces, and the decreased offset, ensure optimum fit-up of the turbulizer during assembly, thereby maximizing metal-to-metal contact between the turbulizer and the tubes, which ensures brazeability and optimum heat transfer.
Although the invention has been described in connection with certain preferred embodiments, it is not intended to be limited thereto. Rather, the invention includes all embodiments which may fall within the scope of the following claims.
Number | Date | Country | |
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Parent | 10652768 | Aug 2003 | US |
Child | 11080902 | Mar 2005 | US |