EXHAUST GAS RECIRCULATION COOLING ELEMENT FOR AN INTERNAL COMBUSTION ENGINE

• US 20110185714A1
• Filed: 12/12/2008
• Published: 08/04/2011
• Est. Priority Date: 12/12/2007
• Status: Active Grant

• Current Assignee: GEA Maschinenkuehltechnik GmbH
• Original Assignee: GEA Maschinenkuhltechnik GmbH (Kelvion Holding GmbH)
• Inventors: Krauss, Dietmar, Lohbreyer, Martin, Abendroth, Dietmar
• Granted Patent: US 8,978,629 B2
• Time in Patent Office: Days
• US Class Current: 60/320
• CPC Class Codes: F28D 21/0003 the heat being recuperated from exhaust gases F28D21/0014 takes precedence
• CPC Class Codes: F28D 7/1623 with particular pattern of flow of the heat exchange media, e.g. change of flow direction
• CPC Class Codes: F28D 7/163 with conduit assemblies having a particular shape, e.g. square or annular; with assemblies of conduits having different geometrical features; with multiple groups of conduits connected in series or parallel and arranged inside common casing F28D7/1615 takes precedence
• CPC Class Codes: F28F 1/32 the means having portions engaging further tubular elements
• CPC Class Codes: F28F 9/26 Arrangements for connecting different sections of heat-exchange elements, e.g. of radiators connecting different sections in water heaters F24H9/14 , connecting headers with inlet or outlet fittings F28F9/0246
• CPC Class Codes: Y02T 10/12 Improving ICE efficiencies

Abstract

The invention relates to an exhaust gas recirculation cooling element (1) comprising a heat exchanger (2) having several heat exchange units (11, 12, 13) that are introduced between the inflow region (3) and the outflow region (7) of the exhaust gas (AG). Said units comprise cooling tubes with cooling ribs. The heat exchanger (2) is surrounded by a housing (16), the lateral walls thereof (19) being arranged at a distance in relation to the perforated lateral walls (10). Guide channels (28) are arranged between the closed lateral walls (9) of the heat exchanger (2) and the adjacent lateral walls (20) of the housing (16), said guide channels extending in a diagonal manner and being provided to direct the coolant (KM) from a coolant inlet to the coolant outflow through the individual heat exchange units (11, 12, 13).

Claims

1-22. -22. (canceled)

23. An exhaust gas recirculation cooling element for an internal combustion engine, comprising:

a housing having coolant fittings,

a heat exchange unit arranged in the housing and including a plurality of cooling pipes having external cooling fins and configured for flow-through of a coolant,

a heat exchanger insert having two closed sidewalls and two perforated sidewalls, with the plurality of cooling pipes secured to the perforated sidewalls;

guide channels for transporting the coolant from and to the plurality of cooling pipes, said guide channels configured as a gap disposed between the heat exchanger insert and the housing; and

a plurality of ribs for delimiting the guide channels, wherein the ribs are formed on the housing and oriented inwardly or are formed on the heat exchanger and oriented outwardly,

wherein the ribs are oriented diagonally in the region of the closed sidewalls, so that diagonal guide channels are formed for transferring the coolant to a coolant inlet side and from a coolant outlet side of a heat exchange unit along the closed sidewalls.

24. The exhaust gas recirculation cooling element of claim 23, wherein the heat exchanger insert is exchangeable.

25. The exhaust gas recirculation cooling element of claim 23, wherein the heat exchanger insert comprises plurality of sequentially connected heat exchange units.

26. The exhaust gas recirculation cooling element of claim 25, wherein coolant flowing out of a first of the plurality of heat exchange unit enters a second heat exchange unit located downstream of the first heat exchange unit by way of the guide channels.

27. The exhaust gas recirculation cooling element of claim 25, wherein the cooling pipes of the plurality of heat exchange units have coolant flow in an identical direction.

28. The exhaust gas recirculation cooling element of claim 25, wherein the cooling pipes of the plurality of heat exchange units have coolant flow in a counterflow direction.

29. The exhaust gas recirculation cooling element of claim 23, wherein the heat exchanger insert has at a first end an inflow region for hot exhaust gas and at a second end an outflow region for cooled exhaust gas.

30. The exhaust gas recirculation cooling element of claim 29, wherein the inflow and outflow regions of the heat exchanger insert have a conical shape.

31. The exhaust gas recirculation cooling element of claim 30, wherein the coolant inlet is provided in the outflow region and the coolant outlet is provided in the inflow region.

32. The exhaust gas recirculation cooling element of claim 23, wherein the cooling fins are made of sheet metal and extend across an entire cross-section of a heat exchange unit.

33. The exhaust gas recirculation cooling element of claim 32, wherein the cooling fins comprise an opening through with the cooling pipes pass and trough-shaped turbulators disposed along the periphery of the opening, with the turbulators formed as depressions in the cooling fins.

34. The exhaust gas recirculation cooling element of claim 33, wherein the depressions are oriented in an identical direction normal to a surface of the cooling fins.

35. The exhaust gas recirculation cooling element of claim 33, wherein the turbulators are kidney-shaped.

36. The exhaust gas recirculation cooling element of claim 35, wherein a cooling fin has four turbulators distributed along the periphery of an opening.

37. The exhaust gas recirculation cooling element of claim 33, wherein the turbulators have first and second ends, with a first end of the turbulators located adjacent to a longitudinal plane extending through axes defined by consecutively arranged openings in a flow direction having a smaller radius than the second end.

38. The exhaust gas recirculation cooling element of claim 37, wherein a first angle enclosed between, on one hand, a plane bisecting the axis of an opening and the first end of a turbulator located adjacent to the longitudinal plane and, on the other hand, the longitudinal plane is about 15°

.

39. The exhaust gas recirculation cooling element of claim 33, wherein the turbulators extend over a second angle of about 50°

to 60°

along the periphery of an opening.

40. The exhaust gas recirculation cooling element of claim 23, wherein the heat exchanger insert is made of stainless steel.