Susceptor for use in a fluid flow system
10470247 ยท 2019-11-05
Assignee
Inventors
- Mark D. EVERLY (St. Charles, MO, US)
- Richard T. Williams (Genoa City, WI, US)
- James N. PRADUN (Lake Geneva, WI, US)
Cpc classification
F02D41/22
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
G05D23/30
PHYSICS
F28F2200/00
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02D41/1446
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01N2560/07
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
H05B3/141
ELECTRICITY
F01N2610/102
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01N2560/20
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01N9/005
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01N2240/36
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01N2900/1602
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01N9/002
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01N2900/1404
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02D41/1447
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01N2240/16
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01N3/2006
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01N2900/1411
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01N2900/0416
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
G01M15/05
PHYSICS
F01N3/106
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Y02T10/12
GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
F01N3/103
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01N3/2066
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01N11/005
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01N2550/22
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01N2240/10
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01N2410/00
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02D2041/228
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01N3/2013
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01N3/023
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01N2410/04
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01N11/002
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01N2900/1406
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01N3/027
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Y02T10/40
GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
F01N2560/12
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01N9/00
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01N13/0097
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01N3/0814
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01N2560/06
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
H05B2203/022
ELECTRICITY
H05B2203/019
ELECTRICITY
F02D41/024
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02D2041/1433
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
H05B3/20
ELECTRICITY
G01F1/86
PHYSICS
F01N3/021
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02D41/222
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
F01N9/00
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
G05D23/30
PHYSICS
F02D41/02
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
H05B3/20
ELECTRICITY
G07C5/08
PHYSICS
G01M15/05
PHYSICS
F02D41/22
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
G05D23/24
PHYSICS
F01N13/00
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01N11/00
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01N3/023
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01N3/027
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
G01F1/86
PHYSICS
F01N3/20
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
H05B1/02
ELECTRICITY
Abstract
A susceptor for use in a heated fluid flow system is provided. In one form, a susceptor is arranged within a conduit and adapted to absorb radiant energy from at least one heating element and inhibit the radiant energy from being absorbed by the at least one wall of the conduit and/or other components. In another form, the susceptor absorbs and inhibits the radiant energy from being absorbed by the outer wall of the conduit.
Claims
1. A conduit for use in carrying a fluid flow, the conduit comprising: at least one wall defining an outer boundary of a flow pathway of the conduit and configured to allow for fluid to flow through the conduit along a longitudinal flow path about which the at least one wall is disposed; at least one heating element positioned within the flow pathway operable for heating the fluid flow flowing along the longitudinal flow path through the flow pathway; and a susceptor arranged relative to the longitudinal flow radially between the at least one heating element and the at least one wall and about a maiority of a perimeter of the flow pathway, the susceptor adapted to absorb radiant energy from the at least one heating element and inhibit the radiant energy from radiating radially outward relative to the longitudinal flow path and being absorbed by the at least one wall of the conduit.
2. The conduit according to claim 1, wherein the at least one heating element comprises a plurality of heating elements adapted to heat the fluid flow.
3. The conduit according to claim 2, wherein the plurality of heating elements includes a first heating element and a second heating element adjacent to the first heating element, wherein the susceptor is adapted to inhibit radiant energy that is emitted from the first heating element from being absorbed by the second heating element.
4. The conduit according to claim 1, wherein the susceptor provides a support structure to the at least one heating element.
5. The conduit according to claim 1, wherein the susceptor is supported by and spaced apart from the at least one wall of the conduit by a support member.
6. The conduit according to claim 1, wherein the susceptor comprises at least one susceptor wall disposed inside the at least one wall of the conduit, wherein the susceptor wall is thinner than a thickness of the at least one wall of the conduit.
7. The conduit according to claim 1, wherein the susceptor comprises a reflective material configured to reduce radiant heat from transferring away from the susceptor and into the at least one wall.
8. The conduit according to claim 1, wherein the susceptor is isolated from the at least one wall of the conduit.
9. The conduit according to claim 1, wherein the susceptor comprises a configuration selected from the group consisting of concentric louvres, radial blades, circumferential fins, a liner, a helical member, and combinations thereof.
10. The conduit according to claim 1, further comprising a second heating element positioned in the fluid flow and downstream of the at least one heating element.
11. A diesel engine exhaust system comprising: a conduit adapted to carry exhaust fluid flow, the conduit positioned upstream from a catalyst system of the diesel exhaust system, an outer wall of the conduit defining an outer boundary of a flow pathway of the conduit and configured to allow the exhaust fluid to flow through the conduit along a longitudinal flow path about which the outer wall of the conduit is disposed; at least one heating element disposed within the flow pathway; and a susceptor arranged relative to the longitudinal flow path radially between the at least one heating element and the outer wall of the conduit and about a maiority of a perimeter of the flow pathway, the susceptor being adapted to absorb radiant energy from the at least one heating element and inhibit the radiant energy from radiating radially outward relative to the longitudinal flow path and being absorbed by the outer wall of the conduit.
12. The diesel engine exhaust system according to claim 11, wherein the at least one heating element comprises a plurality of heating elements adapted to heat the fluid flow.
13. The diesel engine exhaust system according to claim 11, wherein the susceptor provides a support structure to the at least one heating element.
14. The diesel engine exhaust system according to claim 11, wherein the susceptor comprises a configuration selected from the group consisting of concentric louvres, radial blades, circumferential fins, a liner, a helical member, and combinations thereof.
15. The diesel engine exhaust system according to claim 11, wherein the susceptor is spaced apart from the outer wall by a support member.
16. The diesel engine exhaust system according to claim 11, wherein the susceptor comprises a reflective material configured to reduce radiant heat from transferring away from the susceptor and into the outer wall of the conduit.
17. The diesel engine exhaust system according to claim 11, wherein the susceptor comprises at least one susceptor wall disposed inside the outer wall of the conduit, wherein the at least one susceptor wall is thinner than a thickness of the outer wall of the conduit.
18. The diesel engine exhaust system according to claim 11, wherein the susceptor is isolated from the outer wall of the conduit.
19. The diesel engine exhaust system according to claim 11, further comprising insulation between the susceptor and the outer wall of the conduit.
20. The diesel engine exhaust system according to claim 11, wherein the susceptor is paired with an insulating blanket.
Description
DRAWINGS
(1) In order that the disclosure may be well understood, there will now be described various forms thereof, given by way of example, reference being made to the accompanying drawings, in which:
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(10) The drawings described herein are for illustration purposes only and are not intended to limit the scope of the present disclosure in any way.
DETAILED DESCRIPTION
(11) The following description is merely exemplary in nature and is not intended to limit the present disclosure, application, or uses. It should be understood that throughout the drawings, corresponding reference numerals indicate like or corresponding parts and features.
(12) Referring to
(13) It should be understood that the engine system 10 illustrated and described herein is merely exemplary, and thus other components such as a NO.sub.x adsorber or ammonia oxidation catalyst, among others, may be included, while other components such as the DOC, DPF, and SCR may not be employed. Although a diesel engine 12 is shown, it should be understood that the teachings of the present disclosure are also applicable to a gasoline engine and other fluid flow applications. Therefore, the diesel engine application should not be construed as limiting the scope of the present disclosure. Such variations should be construed as falling within the scope of the present disclosure.
(14) The heating system 20 includes a heater assembly 28 disposed upstream from the DOC 22, and a heater control module 30 for controlling operation of the heater assembly 28. The heater assembly 28 can include one or more heaters wherein each heater includes at least one resistive heating element. The heater assembly 28 is disposed within an exhaust fluid flow pathway in order to heat the fluid flow during operation. The heater control module 30 typically includes a control device adapted to receive input from the heater assembly 28. Examples of controlling the operation of heater assembly 28 can include turning the heater assembly on and off, modulating power to the heater assembly 28 as a single unit and/or modulating power to separate subcomponents, such as individual or groups of resistive heating elements, if available, and combinations thereof.
(15) In one form, the heater control module 30 includes a control device. The control device is in communication with at least one heater of the heater assembly 28. The control device is adapted to receive at least one input including but not limited to an exhaust fluid flow, mass velocity of an exhaust fluid flow, flow temperature upstream of the at least one electric heater, flow temperature downstream of the at least one electric heater, power input to the at least one electric heater, parameters derived from physical characteristics of the heating system, and combinations thereof. The heater can be any heater suitable to heat an exhaust fluid. Example heaters include but are not limited to a band heater, a bare wire resistive heating element, a cable heater, a cartridge heater, a layered heater, a strip heater, and a tubular heater.
(16) The system of
(17) When urea water solution is used as the reductant in the SCR 26, NOx is reduced into N.sub.2, H.sub.2O and CO.sub.2.
(18) Referring to
(19) As further shown, at least one heating element 210 is positioned proximate the conduit 202 to heat the fluid flow. It should be understood that any form of heater may be employed with the teachings of the present disclosure. The susceptor 200 is a relatively thin-walled element as shown, as compared with the conduit 202, such that it can absorb radiant energy that would otherwise be absorbed by the cone walls 204, the can walls 208, and the pipe walls 206. In this exemplary form, the various walls 204, 206, and 208 have a higher thermal mass and would not transfer as much heat to the flow since some of its heat would be lost to the outside environment, for example, through convection or conduction through an insulating jacket. The susceptor 200 can be supported by and spaced apart from the cone walls 204, the can wall 208, and the pipe walls 206 according to application requirements by structural supports 212. In another form, the susceptor 200 includes a reflective material (not shown) adapted to reduce heat transfer away from the susceptor. In yet another form, the susceptor 200 can be isolated from one or all of the walls 204, 206, 208 of the conduit 202.
(20) In another form, a diesel engine exhaust system includes a conduit 202 adapted to carry exhaust fluid flow positioned upstream from a catalyst system of the diesel exhaust system. At least one heating element 210 is disposed proximate an outer wall defining at least a portion of the conduit 202. In this form, the susceptor 200 is arranged within the conduit 202 and is adapted to absorb radiant energy from being absorbed by the outer wall of the conduit 202.
(21) In one form as shown in
(22) In another form, a support member 212 is disposed between at least one heating element 210 and another structural member that is exposed to the fluid flow. For example, the susceptor 200 may serve as the support structure for the heating elements 210. In addition, the susceptor 200 serves the purpose of inhibiting or preventing radiant energy from being absorbed by a wall of a conduit that houses controls and switching hardware or other components that would absorb radiant energy in the absence of susceptor 200.
(23) The advantage of such a susceptor 200 is generally faster and thus more efficient heating of the fluid and any downstream components. In one exemplary application of an exhaust heating system, the time to heat an exhaust gas after-treatment catalyst to temperature can be desired. Typically, upon a cold start-up of the system, current catalysts are not effective until they reach a threshold temperature. Until this temperature is reached, the after-treatment system is not as effective in treating the exhaust (for example, to remove NOx with an SCR Catalyst). By increasing the rate of temperature rise of the catalyst, the time of operation of an engine without an optimally functioning exhaust gas after-treatment system can be decreased and the total amount of pollution emitted by the engine and after-treatment system can likewise be reduced with the use of a susceptor in accordance with the teachings of the present disclosure.
(24) Alternate forms of the susceptor are shown in
(25) Additional variations of a susceptor may include, by way of example, improving susceptor efficiency by making its side facing the can or pipe wall out of a reflecting material or by insulating the face from the walls of the conduit. This would help limit heat from transferring from the susceptor and into the ambient air through the can wall and instead transfer it back into the exhaust gas. To reduce heat loss to surrounding components/air, the susceptor should be appropriately isolated from the can wall and/or heating elements.
(26) Additionally, a susceptor could be placed between the can wall and the elements to allow a thicker sheet metal can for better mechanical durability (if the trade-off between thermal performance and structural robustness is an issue).
(27) Further, a susceptor with an insulating material between it and the can wall could reduce the need for another insulating device on the outside of the heater. Alternately, the susceptor could be paired with an insulating blanket (not shown) for extra thermal insulation, especially in very cold conditions.
(28) Accordingly, a variety of different forms of heaters, sensors, control systems, and related devices and methods have been disclosed herein for use in fluid flow systems. Many of the different forms can be combined with each other and may also include additional features specific to the data, equations, and configurations as set forth herein. Such variations should be construed as falling within the scope of the present disclosure.
(29) The description of the disclosure is merely exemplary in nature and, thus, variations that do not depart from the substance of the disclosure are intended to be within the scope of the disclosure. Such variations are not to be regarded as a departure from the spirit and scope of the disclosure.