Heat exchanger for cooling a fluid of an internal combustion engine, assembly with at least one heat exchanger and method for manufacturing a heat exchanger

Abstract

A heat exchanger (10) cooling a fluid and a method for manufacturing, the heat exchanger (10) having an outer pipe section (12) in which a plurality of inner pipe sections (36) with channels for the fluid to be cooled are disposed. At least one cooling fluid channel (56) is disposed in the outer pipe section (12). The at least one cooling fluid channel (56) and the at least one channel for the fluid to be cooled are in heat contact and fluidically separated from each other. A plurality of inner pipe sections (36) open on both ends (38, 46) form of a pipe bundle (34) having ends fixed tightly in a corresponding lead-through opening (40) of an upstream end body (42) and fixed tightly with the other end (46) in a corresponding lead-through opening (48) of a downstream end body (50).

Claims

1. A heat exchanger cooling a charging fluid of a charged internal combustion engine, comprising: an outer pipe section including an inlet end; and an outlet end; a plurality of inner pipe sections arranged within said outer pipe section and extending between said inlet end and said outlet end and open at both opposing ends, said plurality of inner pipe sections defining a plurality of channels for the fluid to be cooled therein; at least one cooling fluid channel conducting a cooling fluid and arranged within said outer pipe section; wherein the at least one cooling fluid channel is in heat transfer contact with said one channel for the fluid to be cooled; wherein said at least one cooling fluid channel is separated fluid-tightly from said one channel for the fluid to be cooled; wherein said plurality of inner pipe sections, which are open each at both ends, are arranged together as a pipe bundle; wherein said plurality of inner pipe sections engage with and are sealably connected at a first end to a respective lead-through opening of an upstream end body; wherein said plurality of inner pipe sections engage with and are sealably connected at an opposing second end to a respective lead-through opening of a downstream end body; wherein said upstream end body separates fluid-tightly an inlet chamber of the outer pipe section from a coolant chamber arranged within said inner pipe sections; wherein said downstream end body separates fluid-tightly an outlet chamber of the outer pipe section from the coolant chamber arranged within said inner pipe sections; and wherein said inner pipe sections fluidically interconnects said inlet chamber to said outlet chamber; wherein adjacent inner pipe sections of said plurality of inner pipe sections are spaced apart from each other in the area of the end bodies and abut together in a longitudinal central section of said outer pipe section, the central section arranged between the end bodies; wherein the outer pipe section is tapered radially inwardly in the central section relative to the end bodies such that the central section has a smaller inner diameter than the end bodies.

2. The heat exchanger according to claim 1, wherein said plurality of inner pipe sections are spaced apart at a greater distance and in an area of said upstream end body and the downstream end body relative to spacing within the longitudinal central section of said outer pipe section; wherein said greater spacing at said area of outer pipe section includes in the area of the upstream end body and the downstream end body a fluid passage distributing cooling fluid to said cooling fluid channels.

3. The heat exchanger according to claim 1, wherein the outer pipe section is tapered radially inwardly from the end bodies to the central section; and wherein inner pipe sections of said plurality of inner pipe sections disposed at a radially outer circumference of said pipe bundle abut against a radially inner circumferential side of said longitudinal central section of the outer pipe section.

4. The heat exchanger according to claim 1, wherein said the inner pipe sections of said plurality of inner pipe sections which are not disposed at the radially outer circumference of the pipe bundle are tightly packed and abutting against each other, each of said inner pipe sections of said plurality of inner pipe sections which are not disposed at the radially outer circumference of the pipe bundle surrounded each by six abutting inner pipe sections within said central section.

5. The heat exchanger according to claim 1, wherein a radially outer circumferential side of said pipe bundle and a radially inner circumferential side of said outer pipe section each have a radially hexagonal profile in a radial direction relative to a longitudinal axial direction of said outer pipe section such that said pipe bundle is received within and abuts against said radially inner circumferential side of said outer pipe section.

6. The heat exchanger according to claim 1, wherein a radially inner circumferential side of the outer pipe section has a radial cross sectional profile that is at least partially complementary to a radial cross sectional profile of the radially outer circumferential side of said pipe bundle in accordance with said plurality of pipe sections therein.

7. An assembly with at least one heat exchanger according to claim 1, comprising: an outer pipe section in which is disposed said plurality of inner pipe sections with at least one channel for the fluid to be cooled; and in which is disposed at least one cooling channel for a cooling fluid; the at least one cooling channel and the at least one channel for the fluid to be cooled being sealed fluidically against each other and in heat transfer contact; wherein at least two heat exchangers are disposed in parallel or in series relative to a flow direction of the fluid to be cooled.

8. A method of manufacturing a heat exchanger for cooling a fluid of an internal combustion engine of claim 1, comprising: providing a plurality of inner pipe sections is made of synthetic material; forming said plurality of inner pipe sections in the form of a pipe bundle wherein longitudinally central portions of said inner pipe sections are tightly packed an abut against each other and longitudinally outer sections of said plurality of inner pipe sections are have a large radial spacing so as not to abut against adjacent inner pipe sections; providing two end bodies having a plurality of continuous openings extending there through; inserting a first end of pipe sections of said plurality of inner pipe sections through corresponding continuous openings of a first one of said end bodies; inserting a second end of pipe sections of said plurality of inner pipe sections through corresponding continuous openings of a second one of said end bodies; wherein said pipe bundle in an area of a central section is tapered radially inwardly between the first and second end bodies; seal tightly securing said first and second ends of said plurality of inner pipe sections into the continuous openings of respective ones of said first and second end bodies; and inserting said pipe bundle into an outer pipe section, so that the end bodies tightly abut against a radially inner circumferential side of said outer pipe section.

9. The method of manufacturing a heat exchanger according to claim 8, wherein said end of said plurality of inner pipe sections are firmly bonded and secured to the first end second end bodies, said bonding by welding and/or fixed by means of a tightly hardening material.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

(1) The accompanying Figs., where like reference numerals refer to identical or functionally similar elements throughout the separate views and which together with the detailed description below are incorporated in and form part of the specification, serve to further illustrate various embodiments and to explain various principles and advantages all in accordance with the present invention.

(2) Features of the present invention, which are believed to be novel, are set forth in the drawings and more particularly in the appended claims. The invention, together with the further objects and advantages thereof, may be best understood with reference to the following description, taken in conjunction with the accompanying drawings. The drawings show a form of the invention that is presently preferred; however, the invention is not limited to the precise arrangement shown in the drawings.

(3) FIG. 1 is an isometric representation of an intercooler of a charge air line of a charged internal combustion engine of a motor vehicle with a pipe bundle for guiding the charge air;

(4) FIG. 2 shows the intercooler of FIG. 1 which is open in longitudinal direction, the pipe bundle being represented in a longitudinal section;

(5) FIG. 3 is a detail view of the intercooler in FIG. 2 in the area of an upstream end plate for holding the pipe bundle;

(6) FIG. 4 is a detail view of a cross-section of the intercooler in FIGS. 1 to 3 in the area of a central section of the pipe bundle;

(7) FIG. 5 shows the intercooler of FIGS. 1 to 4 operated in counter-current process;

(8) FIG. 6 shows a detail view of a longitudinal section of the intercooler in FIG. 5;

(9) FIG. 7 shows the intercooler of FIGS. 1 to 4 operated in co-current process;

(10) FIG. 8 is a detail view of a longitudinal section of the intercooler in FIG. 7;

(11) FIGS. 9 to 14 depict a pipe bundle with one-piece end plates of an intercooler, which is similar to the pipe bundle of the intercooler in FIGS. 1 to 8 in different manufacturing steps;

(12) FIGS. 15 to 19 depict an alternative pipe bundle with two-piece end plates of an intercooler, which is similar to the pipe bundle of the intercooler in FIGS. 1 to 8 in different manufacturing steps;

(13) FIG. 20 a further example of an embodiment of an intercooler, which is similar to the intercooler in FIGS. 1 to 8, an outer pipe and the pipe bundle of the intercooler being bent in the central section;

(14) FIG. 21 depicts a parallel assembly of two intercoolers, which correspond to the intercooler in FIGS. 1 to 8;

(15) FIG. 22 depicts a serial assembly of two intercoolers, which correspond to the intercooler in FIGS. 1 to 8; and

(16) FIG. 23 is an assembly view of an intercooler according to the intercooler in FIGS. 1 to 8 as pre-cooler in front of a compact heat exchanger.

(17) Please note that identical components in the Figs. have the same reference numerals. Skilled artisans will appreciate that elements in the Figs. are illustrated for simplicity and clarity and have not necessarily been drawn to scale. For example, the dimensions of some of the elements in the Figs. may be exaggerated relative to other elements to help to improve understanding of embodiments of the present invention.

DETAILED DESCRIPTION

(18) Before In FIGS. 1 to 8, an intercooler 10 for charge air of a charged internal combustion engine of a motor vehicle is shown in different perspectives and operating modes.

(19) The intercooler 10 comprises an outer pipe 12 featuring an inlet pipe section 14, an outlet pipe section 16 and an intermediate center pipe section 18. A flow direction of the charge air to be cooled is shown by arrows 11 in FIGS. 1 to 3. The outer pipe 12 is split in longitudinal direction and composed of two half shells 20. In FIG. 2, the outer pipe 12 open in longitudinal direction is shown with one of the half shells 20. The center pipe section 18 is tapered relative to the inlet pipe section 14 and the outlet pipe section 16. The radially outer circumferential side and the radially inner circumferential side of the center pipe section 18 have a hexagonal cross-section. The radially inner circumferential side of the center pipe section 18 merges into the radially inner circumferential side of the inlet pipe section 14 and of the outlet pipe section 16, which also have a hexagonal cross-section.

(20) The radially outer circumferential sides of the inlet pipe section 14 and of the outlet pipe section 16 each have a circular cross-section. On the side facing the center pipe section 18, the inlet pipe section 14 features a circumferential receiving groove 22. Accordingly, the outlet pipe section 16 features a circumferential receiving groove 24. The radially outer circumferences of the receiving grooves 22 and 24 have a circular cross-section. Their radially inner edges have a hexagonal profile in accordance with the hexagonal profile of the radially inner circumferential side of the outlet pipe section 16 and the inlet pipe section 14.

(21) Seen from the inlet pipe section 14 directly behind the receiving groove 22 is provided in the outer pipe 12 an upstream passage 26 relative to the charge air flow for coolant of the intercooler 10. Preferably, liquid coolant is used. As an alternative, gaseous coolant may also be used. The upstream passage 26 leads into a coolant chamber 27 inside of the outer pipe 12. As will be explained in detail below, the passage 26 may, according to the operating mode, be used as inlet or as outlet for the coolant. The upstream passage 26 is located in a conical transition area 28 between the inlet pipe section 14 and the center pipe section 18.

(22) Seen from the center pipe section 18 in front of the downstream receiving groove 24, the outer pipe 12 features a downstream passage 30 for the coolant to the coolant chamber 27. The downstream passage 30 is located on the circumferential side of the outer pipe 12 opposite the upstream passage 26. The downstream passage 30 is located in a conical transition area 32 between the center pipe section 18 and the outlet pipe section 16.

(23) The passages 26 and 30 are each connected with a line section of a coolant line of a coolant circuit not shown.

(24) A pipe bundle 34 is disposed in the outer pipe 12 with a plurality of inner pipes 36 in such a way that the inner pipes 36 extend in longitudinal direction of the outer pipe 12. In FIG. 2, the pipe bundle 34 is shown in a longitudinal section. The inner pipes 36 have the same profile with the same external diameter and internal diameter. Their upstream free ends 38 are secured tightly in respective continuous inlet openings 40 in an upstream end plate 42. The end plate 42 is round. It is made of synthetic material. The inner pipes 36 lead through the upstream end plate 42. The upstream ends 38 of the inner pipes 36 are each welded in the inlet openings 40 with the end plate 42. The inlet openings 40 are uniformly distributed in the upstream end plate 42, so that also the upstream ends 38 of the inner pipes 36 seen in profile are uniformly distributed.

(25) The upstream end plate 42 is disposed tightly in the receiving groove 22. An annular sealing 44 is disposed in a sealing groove 174 in the radially outer circumferential side of the upstream end plate 42. The upstream end plate 42 separates an inlet chamber 43 in the inlet pipe section 14 tightly from the coolant chamber 27.

(26) Downstream ends 46 of the inner pipes 36 are attached in outlet openings 48 of a circular downstream end plate 50 in analogy to the upstream ends 38. The end plate 50 is made of synthetic material. The downstream ends 46 of the inner pipes 36 are each welded in the outlet openings 48 with the end plate 50. The downstream end plate 50 is disposed in the downstream receiving groove 24. The downstream end plate 50 separates an outlet chamber 51 in the outlet pipe section 16 tightly from the coolant chamber 27. An annular sealing 52 is disposed in a sealing groove of the downstream end plate 50. The outlet openings 48 are uniformly distributed across the downstream end plate 50, so that the downstream ends 46 of the inner pipes 36 are uniformly distributed across the cross-section of the outlet pipe section 16.

(27) In the area of the center pipe section 18 of the outer pipe 12, the pipe bundle 34 is tapered into a bundle central section 54. There are inner pipes 36 loosely adjacent to each other. The inner pipes 36 are disposed is such a way that the inner pipes 36, which are not located at the radially outer circumferential side of the pipe bundle 34, each have six adjacent inner pipes 36. In the area of the bundle central section 54, each of these inner pipes 36 contacts each of the six adjacent inner pipes 36. Thus, the inner pipes 36 are tightly packed in the bundle central section 54. Gaps between the inner pipes 36 form coolant channels 56 for the coolant. As can be seen in FIG. 4, the coolant channels 56 have an approximately triangular profile with inwardly bent sides in the bundle central section 54. The profile of the gaps and thus of the coolant channels 56 is identical.

(28) The radially outer circumferential side of the pipe bundle 34 has according to the radially inner circumferential side of the outer pipe 12 a hexagonal base profile. The inner pipes 36, which are located on the radially outer circumferential side of the pipe bundle 34, are loosely adjacent to the radially inner circumferential side of the center pipe section 18 of the outer pipe 12. The radially inner circumferential side of the center pipe section 18 features a profiling 58, which is complementary to a profiling of the radially outer circumferential side of the pipe bundle 34. In this way, the profile of the coolant channels 56 defined each by two adjacent inner pipes 36 and an intermediate area of the radially inner circumferential side of the center pipe section 18 is identical with the coolant channels 56 inside of the pipe bundle 34. In this way, a uniform flow through the pipe bundle 34 with coolant can be realized also in the area of the radially outer circumferential side.

(29) In the transition areas 28 and 32 of the outer pipe 12, the inner pipes 36 are spaced, so that a distributor chamber section 60 and 62 each of the coolant chamber 27 is formed, in which the coolant can be uniformly distributed before entering the coolant channels 56 and after leaving the coolant channels 56. In this way, a uniform distribution of the coolant to the coolant channels 56 and a uniform outflow from the coolant channels 56 will be realized. The passages 26 and 30 lead each into the corresponding distributor chamber section 60 and 62.

(30) As shown in FIGS. 5 and 6 and FIGS. 7 and 8, during operation of the intercooler, the charge air to be cooled flows in the flow direction 11 from the corresponding line section of the charge air line to the inlet chamber 43 of the intercooler 10. There, the charge air to be cooled is uniformly distributed to the upstream ends 38 of the inner pipes 36. The charge air to be cooled flows through the inner pipes 36, as indicated in FIGS. 6 and 8 by arrows 84. When flowing through the inner pipes 36, the charge air is cooled. The cooled charge air passes through the downstream ends 46 into the outlet chamber 51. There, it is collected and leaves the intercooler 10.

(31) The intercooler 10 may be operated according to a counter-current process, shown in FIGS. 5 and 6, or according to a co-current process, shown in FIGS. 7 and 8.

(32) In the counter-current process, the coolant is supplied from the coolant circuit through the downstream passage 30 to the downstream distributor chamber section 62 of the coolant chamber 27. The distances of the inner pipes 36 allow the coolant to be distributed uniformly across the cross-section of the distributor chamber section 62. The coolant flows uniformly to the coolant channels 56 between the inner pipes 36. The coolant flows against the flow direction 64 of the charge air, indicated in FIG. 6 by arrows 66, through the coolant channels 56. Heat is transferred from the charge air to be cooled through the inner pipes 36 to the coolant, so that the charge air in the inner pipes 36 is cooled. The coolant flows from the coolant channels 56 into the upstream distributor chamber section 60 where it is collected. It passes through the upstream passage 26 from the coolant chamber 27 back into the coolant circuit.

(33) During operation of the co-current process, shown in FIGS. 7 and 8, and unlike the counter-current process, the coolant is supplied through the upstream passage 26 to the upstream distributor chamber section 60. It flows in the direction of the charge air flow 64 through the coolant channels 56, indicated in FIG. 8 by arrows 166, thus cooling the charge air. The coolant leaves the coolant channels 56 and reaches the downstream distributor section 62. The coolant exits the intercooler 10 through the downstream passage 30.

(34) In FIGS. 9 to 14 some process steps of a method for manufacturing a pipe bundle 134 with end plates 142 and 150 are shown by way of an example, which may be used for the intercooler 10 in FIGS. 1 to 8. Those elements that are similar to those of the example of an embodiment of the intercooler 10 in FIGS. 1 to 8, have the same reference numerals. Unlike the pipe bundle 34, the pipe bundle 134 features a smaller number of inner pipes 36.

(35) The inner pipes 36 are extruded with the aid of a matrix 168 made of synthetic material. The matrix 168 is a hexagonal disc. The matrix 168 features a plurality of guide holes 170, which are disposed according to the later assemblies of the inner pipes 36 in the pipe bundle 134, and through which the extruded inner pipes 36, as indicated in FIG. 9, are inserted in the direction of an arrow 172.

(36) An upstream end plate 142 and a downstream end plate 150 are, as shown in FIG. 10, placed onto the pipe bundle 134. The end plates 142 and 150 are each made in one piece. The upstream end plate 142 features inlet openings 40 and the downstream end plate 150 features outlet openings 48 for the inner pipes 36. The arrangement of the inlet openings 40 and the outlet openings 48 corresponds to the arrangement of the guide holes 170. The end plates 142 and 150 are placed next to each other in such a way that an inlet opening 40 each of the upstream end plate 142, an outlet opening 48 of the downstream end plate 150 and one of the guide holes 170 of the matrix 168 are aligned.

(37) Once the inner pipes 36 have the desired length, they are, as shown in FIG. 11, cut to length with a knife 176 along the surface of the matrix 168 facing the end plates 142 and 150.

(38) Subsequently, as shown in FIG. 12, the upstream end plate 142 on the inner pipes 36 is pushed away from the downstream end plate 150 to the upstream ends 38 of the inner pipes 36. The downstream end plate 150 is moved to the downstream ends 46. The pushing directions are indicated in FIG. 11 by arrows 178. In this phase of the manufacturing process, the upstream ends 38 are disposed loosely in the inlet openings 40 and the downstream ends 46 are disposed loosely in the outlet openings 48, so that they can be moved in the longitudinal direction in the end plates 142 and 150.

(39) In another process step, as shown in FIG. 13, the pipe bundle 134 is tapered in the bundle central section 54. In this case, the eccentric inner pipes 36 are bent toward the center of the pipe bundle 134. The closer the radially inner pipes 36 are located at the center of the pipe bundle 134, the lower is the required amount of bending. As a result of the ends 38 and 46 still being held loosely in the end plates 142 and 150, a mechanically stress-free bending can occur. The pipe bundle 134 is tapered until the inner pipes 36 in the area of the bundle central section 54 are close to each other.

(40) Subsequently, as shown in FIG. 14, the downstream ends 46 in the respective outlet openings 48 are welded to the downstream end plate 150. For this purpose, a mandrel plate 180 with hot mandrels 182, which are disposed according to the outlet openings 48, is fitted into the open ends 46. Due to the heat, the ends 46 are firmly bonded to and sealed to the downstream end plate 150. Accordingly, the upstream ends 38 are sealingly connected with the upstream end plate 142. As an alternative, the upstream ends 38 can first be connected with the upstream end plate 142, and then the downstream ends 46 with the downstream end plate 150. The connection of the ends 38 and 46 with the corresponding end plates 142 and 150 can also be done in one step, for example using two mandrel plates 180.

(41) Annular sealings, which are not shown, are inserted into the corresponding sealing grooves 174 of the end plates 142 and 150. The pipe bundle 134 is inserted into one of the half shells of the outer pipe, the end plates 142 and 150 being inserted into the respective holding fixtures in the radially inner circumferential side of the outer pipe. Subsequently, the second half shell of the outer pipe is mounted, and both half shells are sealingly connected with each other. In this case, the connection can, for example, be realized by means of a welded connection or a glued connection. A different type of connection, such as a screwed connection or a snap-in connection, may also be provided.

(42) In FIGS. 15 to 19, some process steps of an alternative manufacturing method for a pipe bundle 134 with end plates 242 and 250 are shown as an example. Those elements that are similar to those of the example of an embodiment of the method in FIGS. 9 to 14, have the same reference numerals. As in the method according to the first example of an embodiment, the inner pipes 36 are first, according to the second example of an embodiment, extruded with the aid of the matrix 168 according to FIG. 9.

(43) Unlike the example of an embodiment in FIGS. 9 to 14, the upstream end plate 242 and the downstream end plate 250 seen in longitudinal direction are each made in two parts, as shown in FIGS. 15 to 19. The end plates 242 and 250 feature each a first end plate part 243 and a second end plate part 245. The end plate parts 243 and 245 of the upstream end plate 242 feature the inlet openings 40 for the inner pipes 36. The inlet openings 40 extend each through the end plate part 242 and the end plate part 245. The end plate parts 243 and 245 of the downstream end plate 250 feature the outlet openings 48 for the inner pipes 36. The outlet openings 48 extend each through the end plate part 243 and the end plate part 245. The arrangement of the inlet openings 40 and the outlet openings 48 corresponds to the arrangement of the guide holes 170 in the matrix 168.

(44) After the extrusion of the inner pipes 36, the end plates 242 and 250 are, as shown in FIG. 15, placed onto the inner pipes 36, so that the respective first end plate parts 243 face each other and abut against each other.

(45) The respective second end plate parts 245 features each a casting chamber 284 that surrounds the inner pipes 36 leading therethrough and connects their gaps with each other. The casting chambers 284 feature each a filling port 286 on the radially outer circumferential side of the respective second end plate part 245. Furthermore, the first end plate parts 243 feature each a lug 288 which engages in a corresponding holding fixture 290 of the respective second end plate part 245.

(46) Once the inner pipes 36 have the desired length, they will be, as shown in FIG. 16, similar to the first example of an embodiment cut with the knife 176 along the surface of the matrix 168 facing the end plates 242 and 250.

(47) Subsequently, similarly to the first example of an embodiment, the end plates 242 and 250 are drawn apart and placed at the respective ends 38 and 46 of the inner pipes 36. This is shown in FIG. 17.

(48) Then, the pipe bundle 134 is tapered according to the first example of an embodiment in the bundle central section 54, so that the inner pipes 36 there are close to each other. In this phase of the manufacturing process, the ends 38 and 46 are still supported movably in the axial direction in the end plates 242 and 250.

(49) Subsequently, as shown in FIG. 19, a hopper 292 is inserted into the filling port 286 of the second end plate part 245 of the downstream end plate 250. A tightly hardening material in the form of a liquid adhesive is filled through the hopper 292 and the filling port 286. The adhesive is distributed in the casting chamber 284 and sealingly embeds therein the downstream ends 46 of the inner pipes 36 in the second end plate part 245. Once the adhesive is hardened, the downstream ends 46 are held tightly in the corresponding outlet openings 48 of the second end plate part 245. Accordingly, adhesive is filled into the second end plate part 245 of the upstream end plate 242 so that the upstream ends 38 of the inner pipes 36 are sealingly embedded in the second end plate part 245 of the upstream end plate 242. The hopper 292 is now removed. As an alternative, the upstream ends 38 of the inner pipes 36 in the upstream end plate 242 can be embedded first and then the downstream ends 46 in the downstream end plate 250. The embedding of the upstream ends 38 and the downstream ends 46 may also be done in one operation.

(50) The annular sealings are inserted into the sealing grooves 174 in the second end plate part 245. Subsequently, the pipe bundle 134 is inserted similarly to the first example of an embodiment into the first of the half shells of the outer pipe 12. The outer pipe is closed by the second half shell. The two half-shells are tightly connected with each other, they are in particular welded or glued.

(51) FIG. 20 shows another example of an embodiment of an intercooler 310. Those elements that are similar to those of the example of an embodiment of the intercooler 10 in FIGS. 1 to 9, have the same reference numerals. Unlike the intercooler 10 of the first example of an embodiment, the two half shells 320 of the outer pipe 312 and the pipe bundle 334 therein are bent in the area of the central pipe section 318 and the bundle central section, respectively, in the second example of an embodiment.

(52) FIG. 21 shows an example of an embodiment of a parallel assembly of two intercoolers 10 according to the intercooler 10 in FIGS. 1 to 9. The inlet pipe sections 14 and the outlet pipe sections 16 of the two intercoolers 10 are each connected with each other by means of a manifold 94 and connected with the corresponding line section of the charge air line, which is not shown.

(53) FIG. 22 shows an example of an embodiment of a serial assembly of two intercoolers 10 according to the intercooler 10 in FIGS. 1 to 9. In this connection, the two intercoolers 10 are connected in series one after the other, the outlet pipe section 16 of the upstream intercooler 10 being connected with the inlet pipe section 14 of the downstream intercooler 10.

(54) As an example, FIG. 23 shows a use of the intercooler 10 in FIGS. 1 to 9 as pre-cooler in front of a compact heat exchanger 96.

(55) In all above described examples of an embodiment of an intercooler 10; 310, an assembly of intercoolers 10 and a method for manufacturing an intercooler 10, the following modifications are among others possible:

(56) The invention is not limited to an intercooler 10; 310 of a charged internal combustion engine of a motor vehicle. Rather, it can also be used with different internal combustion engines, for example with industrial engines. It can also be used in other types of heat exchangers for cooling a fluid of an internal combustion engine such as a gas or a liquid.

(57) The inner pipes 36 may also have different inner diameters and/or outer diameters.

(58) Instead of being loosely held together, the inner pipes 36 may also be connected with each other in the area of the bundle central section 54. They may, for example, be glued or welded.

(59) Instead of being loosely held at the radially inner circumferential side of the center pipe section 18; 318, the inner pipes 36 may also be connected with it in the area of the bundle central section 54. They may, for example, be glued or welded with it.

(60) Instead of being welded with the one-piece end plates 42; 142 and 50; 150, the ends 38 and 46 of the inner pipes 36 in the examples of an embodiment in FIGS. 1 to 14 may also be connected tightly therewith in different ways. They may, for example, also be connected tightly by means of a different type of bonded connection, for example by means of a glued connection, with the corresponding end plates 42; 142 and 50; 150. Accordingly, when using multi-part end plates 242 and 250, as shown in the example of an embodiment in FIGS. 15 to 19, the ends 38 and 46 may be welded with the end plates 242 and 250.

(61) Instead of being made of synthetic material, the end plates 42; 142; 242 and 50; 150; 250 and/or the inner pipes 36 and/or the outer pipe 12; 312 may also be made of a different material, for example a metal, for example aluminum or an aluminum alloy.

(62) In the foregoing specification, specific embodiments of the present invention have been described. However, one of ordinary skill in the art appreciates that various modifications and changes can be made without departing from the scope of the present invention as set forth in the claims below. Accordingly, the specification and Figs. are to be regarded in an illustrative rather than a restrictive sense, and all such modifications are intended to be included within the scope of the present invention. The benefits, advantages, solutions to problems, and any element(s) that may cause any benefit, advantage, or solution to occur or become more pronounced are not to be construed as a critical, required, or essential features or elements of any or all the claims The invention is defined solely by the appended claims including any amendments made during the pendency of this application and all equivalents of those claims as issued.