Method and systems for an EGR cooler including cooling tubes with a compliant region

Patent metadata

Field	Value
Publication number	US-10697404-B2
Application number	US-201916375623-A
Country	US
Kind code	B2
Filing date	Apr 4, 2019
Priority date	Mar 22, 2016
Publication date	Jun 30, 2020
Grant date	Jun 30, 2020

Abstract

Various methods and systems are provided for an exhaust gas recirculation cooler including a plurality of cooling tubes. In one example, an exhaust gas recirculation (EGR) cooler includes a plurality of cooling tubes positioned within a housing of the EGR cooler, each cooling tube of the plurality of cooling tubes extending between and directly coupled to tube sheets of the EGR cooler at ends of each cooling tube, where at least one end of one or more cooling tubes of a first portion of the plurality of cooling tubes, inward of a tube sheet coupled to the at least one end, includes a compliant region, where the first portion is positioned proximate to an exhaust inlet of the EGR cooler.

First claim

The invention claimed is:

1. A method of expanding cooling tubes within a cooler, comprising:
positioning a cooling tube within the cooler between, but spaced a distance away from, adjacent rows of fins of the cooler;
directly coupling a first end of the cooling tube to a first tube sheet, where the cooling tube includes a first compliant region arranged inward of where the first end is coupled to the first tube sheet; and
passing a mandrel through the cooling tube and past the first compliant region and then expanding the mandrel to expand an outer diameter of the cooling tube and couple an outer surface of the cooling tube to the adjacent rows of fins.

2. The method of claim 1 , further comprising directly coupling a second end of the cooling tube, opposite the first end, to a second tube sheet, where the cooling tube includes a second compliant region inward of where the second end is coupled to the second tube sheet.

3. The method of claim 2 , wherein expanding the mandrel includes increasing an outer diameter of the mandrel in a central region of the cooling tube, between the first compliant region and the second compliant region.

4. The method of claim 2 , further comprising, after passing the mandrel through the cooling tube to the second compliant region, collapsing the mandrel and passing the collapsed mandrel through the second compliant region.

5. The method of claim 2 , further comprising, after passing the mandrel through the cooling tube to the second compliant region, collapsing the mandrel, and re-passing the mandrel through the cooling tube and out past the first compliant region to remove the mandrel from the cooling tube.

6. The method of claim 1 , wherein the mandrel includes an expansion section configured to expand outward from a body of the mandrel, relative to a central axis of the mandrel.

7. The method of claim 6 , wherein passing the mandrel through the cooling tube and past the first compliant region includes passing the mandrel, with the expansion section retracted, through the cooling tube and past the first compliant region and wherein expanding the mandrel to expand the outer diameter of the cooling tube and couple the outer surface of the cooling tube to the adjacent rows of fins includes actuating the expansion section of the mandrel to expand outward from the central axis to the adjacent rows of fins.

8. The method of claim 1 , wherein upon expanding the mandrel to expand the outer diameter of the cooling tube and couple the outer surface of the cooling tube to the adjacent rows of fins, the outer surface of the cooling tube is in direct contact with the adjacent rows of fins with there no longer being a gap between the cooling tube and the adjacent rows of fins.

9. The method of claim 1 , wherein the first compliant region includes a plurality of corrugations.

10. The method of claim 9 , wherein each corrugation of the plurality of corrugations extends outward from the outer surface of the cooling tube, the first compliant region having a larger diameter than the outer diameter of the cooling tube prior to expanding the mandrel to expand the outer diameter of the cooling tube.

11. The method of claim 1 , wherein the first compliant region includes a plurality of bellows.

12. The method of claim 1 , further comprising positioning the cooling tube proximate to an exhaust inlet of the cooler.

13. The method of claim 1 , wherein the first compliant region is continuous and formed as one piece with a remainder of the cooling tube.

14. The method of claim 1 , wherein a second end of the cooling tube does not include a compliant region and further comprising directly coupling the second end of the cooling tube, opposite the first end, to a second tube sheet.

15. A method of expanding cooling tubes within a cooler, comprising:
positioning a cooling tube within the cooler between, but spaced a distance away from, adjacent rows of fins of the cooler so that a gap exists between an outer surface of the cooling tube and fins surrounding the cooling tube;
directly coupling a first end of the cooling tube to a first tube sheet, where the cooling tube includes a first compliant region arranged inward of where the first end is coupled to the first tube sheet and a central region not including the first compliant region; and
expanding only an outer diameter of the central region of the cooling tube and coupling an outer surface of the cooling tube, in the central region, to the adjacent rows of fins without expanding the first compliant region of the cooling tube.

16. The method of claim 15 , wherein expanding only the outer diameter of the central region of the cooling tube includes passing a mandrel through the cooling tube and past the first compliant region and then expanding an expansion section of the mandrel, outward from a body of the mandrel, relative to a central axis of the mandrel.

17. The method of claim 15 , further comprising directly coupling a second end of the cooling tube, opposite the first end, to a second tube sheet, where the cooling tube includes a second compliant region inward of where the second end is coupled to the second tube sheet, the central region arranged between the first compliant region and the second compliant region.

18. The method of claim 17 , wherein the first compliant region and the second compliant region each include a plurality of corrugations extending outward from the outer surface of the cooling tube.

19. The method of claim 15 , wherein the cooling tube is a first cooling tube, further comprising positioning the first cooling tube proximate to an exhaust inlet of the cooler, and further comprising positioning a second cooling tube not including a compliant region downstream of the first cooling tube within the cooler.

20. A method of expanding cooling tubes within a cooler, comprising
positioning a cooling tube within the cooler between, but spaced a distance away from, adjacent rows of fins of the cooler;
directly coupling a first end of the cooling tube to a first tube sheet, where the cooling tube includes a first compliant region arranged inward of where the first end is coupled to the first tube sheet;
passing a mandrel through the cooling tube and past the first compliant region and then expanding an expansion section of the mandrel to expand an outer diameter of the cooling tube and couple an outer surface of the cooling tube to the adjacent rows of fins, in a region of the cooling tube not including the first compliant region;
directly coupling a second end of the cooling tube, opposite the first end, to a second tube sheet, where the cooling tube includes a second compliant region inward of where the second end is coupled to the second tube sheet; and
after passing the mandrel through the cooling tube to the second compliant region, collapsing the mandrel and then passing the collapsed mandrel through the second compliant region or re-passing the mandrel through the cooling tube and out past the first compliant region to remove the mandrel from the cooling tube.

Assignees

• Transp Ip Holdings Llp
• Transp Ip Holdings Llc

Inventors

• Sheth Pushkar Haresh
• Dowell John Patrick
• Jain Jayesh
• Peters Eric David

Classifications

• F28D1/05316

  Assemblies of conduits connected to common headers, e.g. core type radiators (F28D1/05366 takes precedence) · CPC title

• F02M26/28

  with liquid-cooled heat exchangers · CPC title

• F02M26/02

  EGR systems specially adapted for supercharged engines · CPC title

• F02M26/32

  Liquid-cooled heat exchangers · CPC title

• F02M26/11

  Manufacture or assembly of EGR systems; Materials or coatings specially adapted for EGR systems · CPC title