Patent Document

BACKGROUND OF THE INVENTION  
       [0001]     The present application claims priority to U.S. Provisional Patent Application Ser. No. 60/565,372, filed Apr. 26, 2004.  
         [0002]     The present invention relates to an intercooler, and more particularly to a tube intensive intercooler assembly.  
         [0003]     A multitude of systems for increasing the amount of air, and, concomitantly, fuel to an engine are well known. The concept of boosting charge, either with a turbocharger or supercharger, is well known. Moreover, the concept of using intercooling between a booster device, such as the turbocharger or supercharger, and the engine is also well known.  
         [0004]     Intercooler or charge air cooler assemblies are relatively intricate systems which are typically manufactured from aluminum. Conventional intercooler assemblies utilize a multitude of flow passages which are cooled by air flowing over a multitude of fins which extend from external surfaces of the passages. Conventional intercoolers are “fin intensive” deigns in which a majority of the radiant cooling occurs through the metallic fins. Although effective, such conventional metallic intercooler assemblies are relatively heavy in weight and are also typically limited to rectilinear constructions.  
         [0005]     Accordingly, it is desirable to provide a lightweight, thermally effective intercooler assembly which may be manufactured in a multitude of configurations.  
       SUMMARY OF THE INVENTION  
       [0006]     A non-metallic intercooler assembly according to the present invention includes an intake header tank, an outlet header tank, and a multitude of non-metallic charge tubes which communicate airflow from the intake header tank to the outlet header tank. A multitude of non-metallic fins primarily provide structural support rather than thermal transfer as generally understood with a conventional aluminum radiator/intercooler system.  
         [0007]     The intake header tank and the outlet header tank are manufactured from non-metallic or metallic materials. The multitude of non-metallic charge tubes and support side plates are manufactured of laser opaque material while the multitude of non-metallic fins are manufactured of laser transparent materials. The laser opaque and laser transparent materials are arranged and assembled to achieve an effective laser welding assembly process. The multitude of non-metallic charge tubes pass through the non-metallic fins and are laser welded thereto. As the multitude of non-metallic fins are laser transparent while the multitude of non-metallic charge tubes are laser opaque, the laser is readily directed to the desired location to assure a secure bond. Each of the non-metallic fins include an end section which is passed through a slot in the side plate and bent toward the side plate to provide a planar engagement surface to receive a laser weld. As the multitude of non-metallic fins are laser transparent while the side plates are laser opaque, the laser is readily directed from an external location to the planar engagement surface to assure a secure bond. The side plates are laser welded to an end cap which direct or collect the airflow to/from the multitude of non-metallic charge tubes and communicate airflow to/from the header tanks.  
         [0008]     In another embodiment, the intercooler assembly is contoured to provide various shapes to facilitate installation in heretofore unavailable locations. In yet another embodiment, the multitude of non-metallic charge tubes are non-circular in cross-section to increase the packing density of the charge tubes and specifically tailor the size and shape of the intercooler assembly.  
         [0009]     The present invention therefore provides a lightweight, thermally effective intercooler assembly which may be manufactured in a multitude of configurations.  
     
    
     BRIEF DESCRIPTION OF THE DRAWINGS  
       [0010]     The various features and advantages of this invention will become apparent to those skilled in the art from the following detailed description of the currently preferred embodiment. The drawings that accompany the detailed description can be briefly described as follows:  
         [0011]      FIG. 1  is a general schematic view of an exemplary boosted engine system embodiment for use with the present invention;  
         [0012]      FIG. 2  is a perspective view of an air cooler assembly according to the present invention;  
         [0013]      FIG. 3A  is a block diagram of the air cooler assembly according to the present invention;  
         [0014]      FIG. 3B  is a block diagram of a PRIOR ART air cooler assembly utilizing thermal resistance values for comparison to the present invention utilized in  FIG. 3A ;  
         [0015]      FIG. 4  is an exploded view of an air cooler assembly according to the present invention;  
         [0016]      FIG. 5  is an expanded view of a charge tube to fin laser interface according to the present invention;  
         [0017]      FIG. 6  is an expanded view of a fin to side wall laser interface illustrating the fin planar engagement surface according to the present invention;  
         [0018]      FIG. 7  is a front of an air cooler assembly according to the present invention;  
         [0019]      FIG. 8  is an expanded view of a fin to end cap laser interface according to the present invention;  
         [0020]      FIG. 9  is an expanded view of an end cap to header tank laser interface according to the present invention;  
         [0021]      FIG. 10  is an expanded view of a conduit to header tank laser interface according to the present invention;  
         [0022]      FIG. 11  is a front of another embodiment of an air cooler assembly according to the present invention;  
         [0023]      FIG. 12  is a front of another embodiment of an air cooler assembly according to the present invention;  
         [0024]      FIG. 13  is a top view of a charge tube packing arrangement as provided to a header tank;  
         [0025]      FIG. 14  is a top view of a charge tube packing arrangement as provided to a header tank; and  
         [0026]      FIG. 15  is a top view of another charge tube packing arrangement as provided to a header tank. 
     
    
     DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENT  
       [0027]      FIG. 1  illustrates a schematic view of a boosted engine system  10 . Generally, airflow from an intake  12  is communicated through an air cleaner  14  prior to communication to a compressor  16  of a booster such as a turbocharger  18  or supercharger. It should be understood that other systems may also be utilized to boost charge air. From the turbocharger  18 , compressed, heated, airflow (“charge airflow”) is communicated through an air-to-air intercooler assembly  20  to reduce the temperature thereof. From the intercooler assembly  20 , the cooler airflow is communicated to an engine  22  for combustion therein to provide a motive force. Exhaust from the engine  22  is communicated to a turbine  24  of the turbocharger  18  and exhausted through an exhaust system  26 .  
         [0028]     It should be understood that although a particular component arrangement is disclosed in the illustrated embodiment, other components arrangements as well as various systems which will benefit from cooled air are also be usable with the present instant invention. The intercooler assembly  20  operates as an air-to-air heat exchanger to cool the charge air as generally understood. The cooled charge air decrease combustion temperature and increases the density of the charge air to increase the air packed into the combustion chambers. It should be further understood that systems which utilize an air-to-air heat exchanger other than motive source systems such as an air conditioning or thermal management system will also benefit from the present invention.  
         [0029]     Referring to  FIG. 2 , the intercooler assembly  20  includes an intake header tank  28 , an outlet header tank  30  and a multitude of non-metallic charge tubes  32  which communicate airflow from the intake header tank  28  to the outlet header tank  30 . A multitude of non-metallic fins  34  extend transverse to the longitudinal axis of the multitude of non-metallic charge tubes  32 . The multitude of non-metallic charge tubes  32  pass through the fins  34 . Notably, relatively few fins  34  are utilized as the fins  34  primarily provide structural support rather than thermal transfer as generally understood with a conventional metal radiator/intercooler system. The fins  34  are mounted to non-metallic side plates  36  which interconnect the intake header tank  28  and the outlet header tank  30  to provide a relatively rigid structure.  
         [0030]     Referring to  FIGS. 3A, 3B , the non-metallic intercooler assembly  20  designed according to the present invention is a “tube intensive” design. That is, the heat flow resistance on the greater volume provided by the tubes ( FIG. 3A ) is reduced as compared to the “fin intensive” deign of a conventional metallic intercooler/heat exchanger arrangement ( FIG. 3B ). The R values in  FIGS. 3A and 3B  are notional; however, the relative differences representationally distinguish between conventional intercooler designs ( FIG. 3B ) and the intercooler design according to the present invention ( FIG. 3A ). It should be understood that the tubes need not only be each individually larger than conventional designs, but will provide a larger volume of airflow due to a larger individual tube size, more numerous tubes, or a combination thereof as schematically illustrated. Most preferably, the multitude of non-metallic charge tubes  32  each provide a length to diameter aspect ratio of between 80:1 and 160:1. Furthermore, as the fins  34  are non-metallic, the fins provide almost no thermal dissipation properties, as non-metallic material are approximately one thousand times less useful than aluminum for thermal transfer properties.  
         [0031]     The intake header tank  28 , an outlet header tank  30  may be manufactured from non-metallic or metallic materials. The multitude of non-metallic charge tubes  32  and the side plates  36  are preferably manufactured of laser opaque material while the multitude of non-metallic fins  34  are preferably manufactured of laser transparent materials. It should be understood that various combinations and arrangements of laser opaque and laser transparent materials may be utilized to achieve the desired laser welding assembly process disclosed herein. Laser welding is well known and the laser welder will only be schematically described as such laser welders themselves are commonly understood and form no part of the present invention.  
         [0032]     Preferably, the non-metallic materials utilized in the present invention are thermal plastics. Most preferably, the non-metallic materials utilized herein are nylon 6, nylon 12, nylon 46, nylon 66, PPA, PPS, ABS, polycarbonate, PEEK, polypropylene, and PET. Laser opaque non-metallic materials are manufactured by injecting a carbon black dye into the non-metallic material, while the laser transparent material is manufactured by injecting an organic dye into the non-metallic material. The material may therefore be of generally the same appearance yet provide the necessary difference in laser welding properties. It should be understood that various textures may be utilize to identify the laser opaque from the laser transparent materials as well as provide various aesthetic effects  
         [0033]     Referring to  FIG. 4 , the intercooler assembly  20  is illustrated in an exploded view. The multitude of non-metallic fins  34  are located transverse to the longitudinal axis L of the multitude of non-metallic charge tubes  32 . The multitude of non-metallic charge tubes  32  pass through the non-metallic fins  34  and are laser welded thereto ( FIG. 5 ; only one tube shown). As the multitude of non-metallic fins  34  are preferably, laser transparent while the multitude of non-metallic charge tubes  32  are laser opaque, the laser is readily directed to the desired location to assure a secure bond.  
         [0034]     Each of the non-metallic fins  34  include an end section  38  which is assembled through a slot  40  formed in the side plate  36 . The end section  38  is then bent toward the side plate  36  to provide a planar engagement surface to receive a laser weld ( FIG. 6 ;  FIG. 7 ). As the multitude of non-metallic fins  34  are preferably, laser transparent while the side plates  36  are laser opaque, the laser is readily directed from an external location to the desired location to assure a secure bond.  
         [0035]     The side plates  36  are laser welded to an end cap  42 ,  44 . Each end cap  42 ,  44  is essentially of a rectilinear trough shape to direct or collect the airflow to/from the multitude of non-metallic charge tubes  32  and communicate the airflow with the header tanks  28 , 30 . The end caps  42 ,  44  include a U-shaped receipt portion  46  which receives the side plate  36  therein ( FIG. 8 ). Preferably, the end cap  42 ,  44  is laser transparent and the side plates  36  are laser opaque. The laser is readily directed from an external location to the desired location to assure a secure bond.  
         [0036]     The shape of the end cap  42 ,  44  need not be rectilinear but may be of any shape to receive the multitude of non-metallic charge tubes  32  and provide an interface for the respective intake and outlet header tanks  28 ,  30  ( FIG. 7 ;  FIG. 9 ). That is, the end caps  42 ,  44  are shaped to receive the respective intake and output header tanks  28 ,  30 .  
         [0037]     The intake and output header tanks  28 ,  30  may be attached to the end caps  42 ,  44  through fasteners F for intake and output header tanks  28 ,  30  manufactured of a metallic material ( FIG. 9 ). Alternatively, the header tanks  28 ,  30  may be manufactured of a non-metallic material and attached to the end caps  42 ,  44  through laser welding ( FIG. 9 ).  
         [0038]     Referring to  FIG. 10 , a flexible laser transparent communication conduit  46  is laser welded directly to the laser opaque header tanks  28 ,  30 . Laser opaque header tanks  28 ,  30  provide laser welding to the laser transparent end caps  42 ,  44  ( FIG. 9 ). By directly attaching the communication conduit  46  through laser welding, components such as hose clamps and tube barbs are eliminated which thereby increases reliability while minimizing expense, complexity and part count.  
         [0039]     Referring to  FIGS. 11 and 12 , additional embodiments of an intercooler assembly  20 ′  20 ″ are illustrated. The intercooler assembly  20 ′,  20 ″ are contoured to provide various shapes by preferably adjusting the shape and/or length of the multitude of non-metallic charge tubes  32 ′,  32 ″. It should be further understood that the header tanks  28 ′,  28 ″,  30 ′, and  30 ″ although illustrated as generally rectilinear, may be shaped to further conform to a desired mounting location.  
         [0040]      FIG. 11  illustrates curved non-metallic charge tubes  32 ′ which facilitate installation, for example, adjacent a wheel well. The intercooler assembly  20 ′ includes fins  34 ′ with a corrugated portion  35  such that the length of the fin is longitudinally variable in length during assembly. That is, the corrugated portions  35  permit the length of a single fin  34 ′ to be adjusted to fit various areas and provide some degree of flex to the intercooler assembly  20 ′ within a predetermined plane.  
         [0041]      FIG. 12  illustrates a mechanically symmetrical intercooler assembly  20 ″ with header tanks offset for a predetermined installation such as in a raked front facia; chassis mounted; in front of engine cooling radiator; in front of air conditioning condenser; sandwiched between air conditioner and coolant radiator; under a headlight; under a bumper; and/or within a fog light opening. It should be understood that various installations will benefit from the present invention.  
         [0042]     Referring to  FIGS. 13-15 , the multitude of non-metallic charge tubes  32  may be packed in particular arrangements ( FIG. 13 ) and may alternatively or additionally be non-circular in cross-section. The multitude of non-metallic charge tubes  32  may be polygonal ( FIGS. 14 and 15 ) to increase the density of the tubes and may include various shape combinations so as to specifically tailor the size and shape of the intercooler assembly. Most preferably, the areas A between the non-metallic charge tubes  32  ( FIGS. 13 and 14 ) are filled to prevent airflow dead spaces within the header thanks  28 ,  30 .  
         [0043]     Although particular step sequences are shown, described, and claimed, it should be understood that steps may be performed in any order, separated or combined unless otherwise indicated and will still benefit from the present invention.  
         [0044]     The foregoing description is exemplary rather than defined by the limitations within. Many modifications and variations of the present invention are possible in light of the above teachings. The preferred embodiments of this invention have been disclosed, however, one of ordinary skill in the art would recognize that certain modifications would come within the scope of this invention. It is, therefore, to be understood that within the scope of the appended claims, the invention may be practiced otherwise than as specifically described. For that reason the following claims should be studied to determine the true scope and content of this invention.

Technology Category: 7