text: fig1 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 . 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 . referring to fig2 , 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 . referring to fig3 a , 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 ( fig3 a ) is reduced as compared to the “ fin intensive ” deign of a conventional metallic intercooler / heat exchanger arrangement ( fig3 b ). the r values in fig3 a and 3b are notional ; however , the relative differences representationally distinguish between conventional intercooler designs ( fig3 b ) and the intercooler design according to the present invention ( fig3 a ). 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 . 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 . 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 referring to fig4 , 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 ( fig5 ; 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 . 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 ( fig6 ; fig7 ). 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 . 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 ( fig8 ). 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 . 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 ( fig7 ; fig9 ). that is , the end caps 42 , 44 are shaped to receive the respective intake and output header tanks 28 , 30 . 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 ( fig9 ). 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 ( fig9 ). referring to fig1 , 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 ( fig9 ). 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 . referring to fig1 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 . fig1 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 . fig1 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 . referring to fig1 - 15 , the multitude of non - metallic charge tubes 32 may be packed in particular arrangements ( fig1 ) and may alternatively or additionally be non - circular in cross - section . the multitude of non - metallic charge tubes 32 may be polygonal ( fig1 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 ( fig1 and 14 ) are filled to prevent airflow dead spaces within the header thanks 28 , 30 . 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 . 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 .