Exhaust assembly temperature regulation

Patent metadata

Field	Value
Publication number	US-11105249-B2
Application number	US-201916556520-A
Country	US
Kind code	B2
Filing date	Aug 30, 2019
Priority date	Aug 30, 2019
Publication date	Aug 31, 2021
Grant date	Aug 31, 2021

Abstract

An exhaust assembly includes an exhaust tube and a coolant passage. The exhaust tube is oriented about an axis and an exhaust gas is configured to flow through the exhaust tube in a direction away from an end of the exhaust tube. The coolant passage is oriented about the axis radially outward of the exhaust tube, the coolant passage having an inner shell and an outer shell. The end of the exhaust tube includes one or more holes permitting exhaust gas to flow around the end of the exhaust tube between an outer wall of the exhaust tube and the inner shell of the coolant passage to regulate a temperature of the inner shell of the coolant passage.

First claim

What is claimed is:

1. An exhaust assembly comprising:
an exhaust tube oriented about an axis, wherein an exhaust gas is configured to flow through the exhaust tube in a direction away from an end wall of the exhaust tube; and
a coolant passage oriented about the axis radially outward of the exhaust tube, the coolant passage having an inner shell and an outer shell, wherein the inner shell comprises an inner wall axially adjacent the end wall of the exhaust tube;
wherein the end wall of the exhaust tube comprises one or more holes permitting exhaust gas to flow through the end wall and between an outer side of the end wall of the exhaust tube and the inner wall of the inner shell of the coolant passage around the end wall of the exhaust tube between an outer wall of the exhaust tube and the inner shell of the coolant passage to regulate a temperature of the inner shell of the coolant passage.

2. The exhaust assembly of claim 1 , further comprising:
a radiation shield oriented about the axis, radially outward of the outer wall of the exhaust tube and radially inward of the inner shell of the coolant passage, the radiation shield comprising an end adjacent the end wall of the exhaust tube;
wherein the end of the radiation shield includes one or more holes to permit the exhaust gas to flow between the radiation shield and the inner shell of the coolant passage to regulate the temperature of the inner shell of the coolant passage.

3. The exhaust assembly of claim 2 , wherein the one or more holes in the end of the radiation shield are axially aligned with the one or more holes in the end wall of the exhaust tube.

4. A gas engine comprising the exhaust assembly of claim 1 .

5. The exhaust assembly of claim 1 , wherein the exhaust tube comprises a plurality of exhaust inlets each positioned in a first axial direction with respect to the end wall of the exhaust tube and between the end wall and an outlet of the exhaust tube opposite the end wall of the exhaust tube, wherein no exhaust gas inlets are positioned in a second axial direction opposite the first axial direction with respect to the end wall of the exhaust tube and wherein the exhaust gas is received through the plurality of exhaust inlets and configured to flow out of the outlet of the exhaust tube.

6. The exhaust assembly of claim 5 , wherein the exhaust flowing between the outer wall of the exhaust tube and the coolant passage is configured to exit the passage between the outer wall of the exhaust tube and the inner shell of coolant passage at a gap in the outer wall of the exhaust tube adjacent the outlet of the exhaust tube.

7. The exhaust assembly of claim 1 , wherein the coolant passage is a coolant passage configured to receive water as the coolant.

8. A gas engine comprising:
an exhaust assembly configured to carry an exhaust gas, the exhaust assembly comprising:
an exhaust tube oriented about an axis, wherein the exhaust gas is configured to flow through the exhaust tube in a direction away from an end wall of the exhaust tube; and
a coolant passage oriented about the axis radially outward of the exhaust tube, the coolant passage having an inner shell, wherein the inner shell comprises an inner end wall axially adjacent the end wall of the exhaust tube;
wherein the end wall of the exhaust tube comprises one or more holes permitting exhaust gas to flow through the end wall and between an outer side of the end wall of the exhaust tube and the inner end wall and around the end wall of the exhaust tube between the exhaust tube and the inner shell of the coolant passage to regulate a temperature of the inner shell of the coolant passage.

9. The gas engine of claim 8 , wherein the exhaust assembly further comprises:
a radiation shield oriented about the axis, radially outward of the exhaust tube and radially inward of the inner shell of the coolant passage, the radiation shield comprising an end adjacent the end wall of the exhaust tube;
wherein the end of the radiation shield includes one or more holes to permit the exhaust gas to flow between the radiation shield and the inner shell of the coolant passage to regulate the temperature of the inner shell of the coolant passage.

10. The gas engine of claim 9 , wherein the one or more holes in the end of the radiation shield are axially aligned with the one or more holes in the end wall of the exhaust tube.

11. The gas engine of claim 8 , wherein the exhaust tube comprises a plurality of exhaust inlets each positioned in a first axial direction with respect to the end wall of the exhaust tube and between the end wall and an outlet of the exhaust tube opposite the end wall of the exhaust tube, wherein no exhaust gas inlets are positioned in a second axial direction opposite the first axial direction with respect to the end wall of the exhaust tube, and wherein the exhaust gas is received through the plurality of exhaust inlets and configured to flow out of the outlet of the exhaust tube.

12. The gas engine of claim 11 , wherein the exhaust flowing between the exhaust tube and the inner shell is configured to exit at a gap in exhaust tube adjacent the outlet of the exhaust tube.

13. The gas engine of claim 8 , wherein the coolant passage is configured to receive water as the coolant.

14. A method of preventing condensation of exhaust gases within an exhaust assembly, the method comprising:
receiving the exhaust gases in an exhaust tube oriented about an axis, the exhaust gases configured to flow through the exhaust tube in a direction away from an end wall of the exhaust tube;
receiving a coolant in a coolant passage oriented about the axis radially outward of the exhaust tube, the coolant passage having an inner shell, wherein the inner shell comprises an inner end wall axially adjacent the end wall of the exhaust tube; and
directing a portion of the exhaust gases, using one or more holes in the end wall of the exhaust tube, to flow through the end wall and between an outer side of the end wall of the exhaust tube and the inner end wall and around the end wall of the exhaust tube between an outer wall of the exhaust tube and the inner shell of the coolant passage to regulate a temperature of the inner shell of the coolant passage.

15. The method of claim 14 , wherein the exhaust assembly further comprises a radiation shield oriented about the axis, radially outward of the outer wall of the exhaust tube and radially inward of the inner shell of the coolant passage, the radiation shield comprising an end adjacent the end wall of the exhaust tube, and wherein directing the portion of the exhaust gases comprises:
directing the portion of the exhaust gases , using one or more holes in the end of the radiation shied, to flow between the radiation shield and the inner shell of the coolant passage to regulate the temperature of the inner shell of the coolant passage.

16. The method of claim 15 , wherein the one or more holes in the end of the radiation shield are axially aligned with the one or more holes in the end wall of the exhaust tube.

17. The metho of c aim 14 , wherein the exhaust assembly is included in a gas engine.

18. The method of claim 14 , wherein receiving the exhaust gases in the exhaust tube comprises receiving the exhaust gases through a plurality of exhaust inlets each positioned in a first axial direction with respect to the end wall of the exhaust tube and between the end wall and an outlet of the exhaust tube opposite the end wall of the exhaust tube, wherein no exhaust gas inlets are positioned in a second axial direction opposite th

Assignees

• Caterpillar Inc

Inventors

• Kennedy Joseph L
• Hodges Bradley W
• Palmer Andrew D

Classifications

• F01N13/14

  having thermal insulation {(exhaust manifolds F01N13/102)} · CPC title

• F01N13/102

  having thermal insulation · CPC title

• F28D7/1669

  the conduit assemblies having an annular shape; the conduits being assembled around a central distribution tube · CPC title

• F01N2260/20

  for heat or sound protection, e.g. using a shield or specially shaped outer surface of exhaust device · CPC title

• F28F9/20

  Arrangements of heat reflectors, e.g. separately-insertible reflecting walls · CPC title