| (19) |
 |
|
(11) |
EP 2 466 088 A1 |
| (12) |
EUROPEAN PATENT APPLICATION |
| (43) |
Date of publication: |
|
20.06.2012 Bulletin 2012/25 |
| (22) |
Date of filing: 14.12.2010 |
|
| (51) |
International Patent Classification (IPC):
|
|
| (84) |
Designated Contracting States: |
|
AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL
NO PL PT RO RS SE SI SK SM TR |
|
Designated Extension States: |
|
BA ME |
| (71) |
Applicant: Perkins Engines Company Limited |
|
Eastfield
Peterborough PE1 5NA (GB) |
|
| (72) |
Inventor: |
|
- De Almeida, Eduardo
Peoria, Illinois 61629-9510 (US)
|
| (74) |
Representative: Preuss, Udo |
|
Kramer - Barske - Schmidtchen
Landsberger Strasse 300 80687 München 80687 München (DE) |
|
| |
|
|
|
Remarks: |
|
Amended claims in accordance with Rule 137(2) EPC. |
|
(57) An exhaust system (12) for a combustion engine (14) comprising an exhaust passage
(16) having a first conduit port (23) and a first sensing portion (20a) configured
to determine a parameter related to a pressure of exhaust gas in the exhaust passage,
the first sensing portion (20a) being remote from the exhaust passage (16). A first
conduit (22) extends between the first sensing portion (20a) and the first conduit
port (23) for fluidly connecting the first sensing portion (20a) with the exhaust
passage (16). A first bleed passage (26) extends between the first conduit (22) and
a first bleed connection (27) for fluidly connecting the first bleed passage (26)
with another portion of the exhaust system (12) enabling a substantially continuous
flow of exhaust gas through at least a portion of the first conduit (22).
|

|
Technical Field
[0001] The present disclosure relates generally to an exhaust system.
Background
[0002] Exhaust gas systems for power units such as internal combustion engines nowadays
tend to be of increasingly complex arrangements involving multiple sub-systems and
components for emission control such as exhaust gas recirculation (EGR) arrangements
and aftertreatment arrangements. Exhaust gas is inherently dirty and potentially aggressive
as it contains many constituents, including water, that together and potentially with
other additional chemicals (such as for example urea) can form deposits in the systems
thereby reducing or halting proper operation of the various components and/or systems.
The current disclosure is aimed at alleviating some of such problems.
Summary
[0003] The present disclosure details an exhaust system for a combustion engine comprising
an exhaust passage having a first conduit port, a first sensing portion configured
to determine a parameter related to a pressure of exhaust gas in the exhaust passage,
the first sensing portion being remote from the exhaust passage. Furthermore, a first
conduit extends between the first sensing portion and the first conduit port for fluidly
connecting the first sensing portion with the exhaust passage and a first bleed passage
extends between the first conduit and a first bleed connection for fluidly connecting
the first bleed passage with another portion of the exhaust system enabling a substantially
continuous flow of exhaust gas through at least a portion of the first conduit.
Brief Description of the Drawings
[0004]
Fig. la is a schematic illustration of an exemplary exhaust system embodiment having
at least one sensing portion according to the present disclosure.
Fig. lb is a schematic illustration of a variant of the embodiment of Fig. la.
Fig. 2a is an schematic illustration of an expanded variant of the embodiment of Fig.
1 a.
Fig. 2b is a schematic illustration of a variant of the embodiment of Fig. 2a.
Fig. 3 is a schematic illustration of an exemplary exhaust system embodiment having
at least two sensing portions according to the present disclosure.
Fig. 4 is a schematic illustration of a variant of Fig. 3.
Fig. 5 is a schematic illustration of an exemplary exhaust system embodiment having
at least two sensing portions with a single bleed line.
Fig. 6 is a is a schematic illustration of an exemplary exhaust system embodiment
having two sensing portions as part of the same sensor.
Detailed Description
[0005] Figs. 1 to 6 are schematic illustrations of exemplary embodiments of a sensing arrangement
10 for an exhaust system 12 of a combustion engine 14 such as for example an internal
combustion engine. An exhaust passage 16 may be fluidly connected to the combustion
engine 14 to conduct exhaust gasses. In one embodiment the exhaust passage 16 may
for example be an exhaust gas recirculation (EGR) passage to conduct exhaust gasses
from an exhaust portion of the combustion engine 14 to an intake portion of the combustion
engine 14. In one embodiment the exhaust passage 16 may additionally or alternatively
be conducting exhaust gas from or to an aftertreatment arrangement and/or to the environment.
[0006] In one embodiment the sensing arrangement 10 may include a first sensing portion
20a. In another embodiment the sensing arrangement may include at least a first sensing
portion 20a and a second sensing portion 20b. The sensing arrangement 10 may be configured
to determine parameters relating to an exhaust gas pressure. The first and second
sensing portions 20a and 20b may for example be individual pressure sensors such as
absolute pressure sensors. Alternatively, the first and second sensing portions 20a
and 20b may actually be portions of a single sensor such as a Δp ("delta-pressure")
sensor.
[0007] First sensing portion 20a may be remote from the exhaust passage 16 and may be fluidly
connected to the exhaust passage 16 via a first conduit 22. The fluid connection of
the first conduit 22 with the exhaust passage 16 will from hereon be referred to as
first conduit port 23. Similarly, second sensing portion 20b may be remote from the
exhaust passage 16 and may be fluidly connected to the exhaust passage 16 via a second
conduit 24. The fluid connection of the second conduit 24 with the exhaust passage
16 will from hereon be referred to as second conduit port 25.
[0008] A first bleed passage 26 may extend from the first conduit 22 to a portion of the
exhaust system 12 to fluidly connect them together. The fluid connection of the first
bleed passage 26 with the portion of the exhaust system 12 it fluidly connects to
will from hereon be referred to as the first bleed connection 27. In one embodiment
the first bleed passage 26 may extend from the first conduit 22 to the exhaust passage
16 and the first bleed connection 27 is then the fluid connection between the first
bleed passage 26 and the exhaust passage 16.
[0009] Similarly, a second bleed passage 28 may extend from the second conduit 24 to a portion
of the exhaust system 12 to fluidly connect them together. The fluid connection of
the second bleed passage 28 with the portion of the exhaust system 12 it fluidly connects
to will from hereon be referred to as the second bleed connection 29. In one embodiment
the second bleed passage 28 may extend from the second conduit 24 to the exhaust passage
16 and the second bleed connection 29 is then the fluid connection between the second
bleed passage 28 and the exhaust passage 16.
[0010] It is to be understood that the first and/or second bleed passages 26 and 28 may
have cross-sectional diameters, or orifices with such a cross-sectional diameter,
which are small compared to the exhaust passage 16 such that the flow through the
first and/or second bleed passages 26 and 28 may be little or even insignificant compared
to the flow flowing through the exhaust passage 16.
[0011] The exhaust passage 16 may have a restriction 18 therein, dividing the exhaust passage
16 in an upstream portion 16a and a downstream portion 16b. In one embodiment the
restriction 18 may be a restrictor having a fixed cross-sectional opening such as
for example a fixed venturi. In another embodiment the restriction 18 may have a variable
cross-sectional opening therethrough such as for example a valve arrangement including
a moveable valve member.
[0012] The location of the first bleed connection 27 and/or the second bleed connection
29 in the exhaust system may be chosen as suitable. For example the first bleed connection
27 may be located on upstream portion 16a, on downstream portion 16b, on a portion
of the exhaust passage 16 upstream of the first conduit port 23 or on a portion of
the exhaust passage 16 downstream of the first conduit port 23. The second bleed connection
29 may be located on upstream portion 16a, on downstream portion 16b, on a portion
of the exhaust passage 16 upstream of the second conduit port 25 or on a portion of
the exhaust passage 16 downstream of the second conduit port 25.
[0013] Figs. 3 and 4 show exemplary embodiments in which an additional restricting element
30 may be present in the exhaust passage. The restricting element 30 may be anything
that provides resistance to the gas flow and may for example include a components
such as a turbocharger or a valve, but may also be a just a bend or narrowing in the
conduit for example. The characteristic of the restricting element 30 is that the
gas flow therethrough is restricted such that there is a gas pressure differential
across the restricting element 30.
[0014] As best seen in Fig. 3 in one embodiment the first bleed connection 27 may be located
in a portion of the exhaust passage 16 upstream of the restricting element 30 whilst
the first conduit port 23 is located in a portion of the exhaust passage 16 downstream
of the restricting element 30. The second bleed connection 29 may be located in a
portion of the exhaust system upstream of the restriction 18 whilst the second conduit
port 25 is located in a portion of the exhaust passage 16 downstream of the restriction
18. It is to be understood that the restricting element 30 may be omitted.
[0015] As best seen in Fig. 4, in one embodiment the first bleed connection 27 may be located
in a portion of the exhaust passage 16 downstream of the restriction 18 whilst the
first conduit port 23 maybe located in a portion of the exhaust passage 16 upstream
of the restriction 18. The second bleed connection 29 may be located in a portion
of the exhaust system downstream of the restricting element 30 whilst the second conduit
port 25 may be located in a portion of the exhaust passage 16 upstream of the restricting
element 30. It is to be understood that the restricting element 30 may be omitted.
[0016] As best seen in Figs. 5 and 6, the first and second bleed connections 27 and 29 may
actually be fluidly connected together such that the first and the second bleed passages
26 and 28 are merged.
[0017] It is to be understood that the aforementioned embodiments are exemplary only and
not intended to be limiting. Individually, or as part of a combination, any of the
first conduit port 23, the second conduit port 25, the fist bleed connection 27 and
the second bleed connection 29 may be located as suitable. For example, it may be
desirable to have exhaust gas flow predominantly from the first bleed passage 26 to
the first bleed connection 27 or vice versa. Similarly, it may be desirable to have
exhaust gas flow predominantly from the second bleed passage 28 to the second bleed
connection 29 or vice versa.
Industrial Applicability
[0018] For exemplary purposes only the system will be described as being operational as
an EGR loop with the exhaust passage 16 being fluidly connectable to an intake portion
of the engine. During operation of the EGR loop exhaust gas produced by combustion
engine 14 may flow through the exhaust passage 16 and through restriction 18, which
in this case may be regarded as an EGR valve. The restriction 18 may be controlled
to regulate the amount of EGR and may even be closed fully. In the example of the
exhaust system 12 being a portion of an EGR loop it may be desirable to determine
various gas pressure related parameters upstream and downstream of the restriction
18 to aid in determining or estimating the EGR mass flow. However, it may be undesirable
or just not practical to have the first and/or second sensing portions 20a and 20b
in immediate proximity of the main exhaust flow in the exhaust passage 16 and therefore
the first and second conduits 22 and 24 may enable the first and second sensing portions
20a and 20b to be located remotely from the exhaust passage 16. Gas flowing through
the exhaust passage 16 will act on the remote first and second sensing portions 20a
and 20b. As without the first and/or second bleed passages 26, 28 the first and second
conduits 22 and 24 are basically dead ends, the flow of gas may stagnate to an extent
in the first and second conduits 22 and 24. By providing a first bleed passage 26
extending between the first conduit 22 and a first bleed connection 27 for fluidly
connecting the first bleed passage 26 with another portion of the exhaust system 12
enables a substantially continuous flow of exhaust gas through at least a portion
of the first conduit 22. Similarly, providing a second bleed passage 28 extending
between the second conduit 24 and a second bleed connection 29 for fluidly connecting
the second bleed passage 28 with another portion of the exhaust system 12 enables
a substantially continuous flow of exhaust gas through at least a portion of the second
conduit 24.
[0019] By changing the flow characteristics through at least portions of the first and second
conduits 22 and 24, build up of deposits or the forming of condensation in the first
and second conduits 22 and 24 and especially near the first and second conduit ports
23 and 25 may be reduced. By using existing pressure differentials upstream and downstream
of the first and second conduit ports 23 and 25 predominant flow directions can be
achieved. For example, by fluidly connecting the first bleed passage 26 to a portion
of the exhaust system 12 where a relatively higher exhaust gas pressure exists than
in the first conduit 22, any gas flow will then predominantly take place from the
first bleed connection 27, through the first bleed passage 26, through at least a
portion of the first conduit 22 and subsequently through the first conduit port 23.
Of course the reverse order applies when the exhaust gas pressure in the first conduit
22 is relatively higher than the exhaust gas pressure at the first bleed connection
27. It may for example be preferred to have the flow directed in such a manner to
move any deposits away from the first sensing portion 20a rather than towards it.
Of course this equally applies to the portion of the system including the second sensing
portion 20b, the second bleed connection 29 and its associated second bleed passage
28.
[0020] In situations where fouling and/or condensation issues tend to mainly concentrate
near the first conduit port 23, the fluid connection between first conduit 22 and
the first bleed passage 26 may be located relatively close to the first conduit port
23, e.g. within 50 or even within 25 millimeters from the first conduit port 23. This
of course applies equally to the second conduit 24, the second conduit port 25 and
the second bleed passage 28.
[0021] In one embodiment at least one of the fluid connections between the first conduit
22 and the first bleed passage 26, and between the second conduit 24 and the second
bleed passage 28 may be located adjacent the associated sensing portion 20a and 20b
respectively.
[0022] It will be apparent to those skilled in the art that various modifications and variations
can be made in the disclosed linkage arrangement. Other embodiments will be apparent
to those skilled in the art from consideration of the specification and practice of
the disclosed embodiments herein. It is intended that the specification and examples
be considered as exemplary only, with a true scope of the disclosure being indicated
by the following claims.
1. An exhaust system (12) for a combustion engine (14) comprising:
an exhaust passage (16) having a first conduit port (23);
a first sensing portion (20a) configured to determine a parameter related to a pressure
of exhaust gas in the exhaust passage, the first sensing portion (20a) being remote
from the exhaust passage (16);
a first conduit (22) extending between the first sensing portion (20a) and the first
conduit port (23) for fluidly connecting the first sensing portion (20a) with the
exhaust passage (16);
a first bleed passage (26) extending between the first conduit (22) and a first bleed
connection (27) for fluidly connecting the first bleed passage (26) with another portion
of the exhaust system (12) enabling a substantially continuous flow of exhaust gas
through at least a portion of the first conduit (22).
2. An exhaust system (12) according to claim 1, further including
a restriction (18) in the exhaust passage (16);
a second conduit port (25) in the exhaust passage (16);
a second sensing portion (20b) configured to determine a parameter related to a pressure
of exhaust gas in the exhaust passage (16), the second sensing portion (20b) being
remote from the exhaust passage (16);
a second conduit (24) extending between the second sensing portion (20b) and the second
conduit port (25) for fluidly connecting the second sensing portion (20b) with the
exhaust passage (16);
a second bleed passage (28) extending between the second conduit (24) and a second
bleed connection (29) for fluidly connecting the second bleed passage (28) with another
portion of the exhaust system (12) enabling a substantially continuous flow of exhaust
gas through at least a portion of the second conduit (24) wherein the first conduit
port (23) is located in a portion of the exhaust passage ( 16a) upstream of the restriction
(18) and the second conduit port (25) is located in a portion of the exhaust passage
(16b) downstream of the restriction (18).
3. An exhaust system (12) according to claim 2 wherein said first and second sensing
portions (20a, 20b) are portions of a single Δp sensor.
4. An exhaust system (12) according to claim 2 wherein the first sensing portion (20a)
is a first pressure sensor and the second sensing portion (20b) is a second pressure
sensor.
5. An exhaust system (12) according to any of the preceding claims wherein the restriction
(18) is a venturi.
6. An exhaust system (12) according to any of claims 1 to 4, wherein the restriction
(18) is an EGR valve.
7. An exhaust system (12) according to any of claims 2 to 6, wherein the first and second
bleed connections (27, 29) are fluidly connected to each other.
8. An exhaust system (12) according to any of the preceding claims, wherein at least
one of the first and second bleed connections (27, 29) is located in the exhaust system
(12) such that exhaust gas tends to flow predominantly from the bleed passage (26,
28) to the associated bleed connection (27,29).
9. An exhaust system (12) according to any of the preceding claims, wherein at least
one of the first and second bleed connections (27, 29) is located in the exhaust system
(12) such that exhaust gas tends to flow predominantly from the bleed connection (27,
29) to the associated bleed passage (26, 28).
10. An exhaust system (12) according to any of claims 2 to 6 wherein both the first and
second bleed connections (27, 29) are located in a portion of the exhaust passage
( 16a) upstream of the restriction (18).
11. An exhaust system (12) according to any of claims2 to 6 wherein both the first and
second bleed connections (27, 29) are located in a portion of the exhaust passage
(16b) downstream of the restriction (18).
12. An exhaust system (12) according to any of the preceding claims, wherein at least
one of the fluid connections a) between the first conduit (22) and the first bleed
passage (26) and b) between the second conduit (24) and the second bleed passage (28)
is located within 50 millimeters from the first conduit port (23).
13. An exhaust system (12) according to any of the preceding claims, wherein at least
one of the fluid connections between a) between the first conduit (22) and the first
bleed passage (26) and b) between the second conduit (24) and the second bleed passage
(28) is located within 25 millimeters from the first conduit port (23).
14. An exhaust system (12) according to any of claims 1 to 11, wherein at least one of
the fluid connections a) between the first conduit (22) and the first bleed passage
(26) and b) between the second conduit (24) and the second bleed passage (28) is located
adjacent the associated sensing portion (20a, 20b)
15. An exhaust system (12) according to any of the preceding claims wherein at least one
of the first and second bleed passages (26, 28) includes a portion having a small
cross-sectional diameter relative to the exhaust passage (16) such that any flow through
the at least one of the first and second bleed passages (26, 28) is little or insignificant
compared through the flow flowing through the exhaust passage (16).
Amended claims in accordance with Rule 137(2) EPC.
1. An exhaust system (12) for a combustion engine (14) comprising:
an exhaust passage (16) having a first conduit port (23) and a second conduit port
(25) in the exhaust passage (16);
a restriction (18) in the exhaust passage (16);
a first sensing portion (20a) configured to determine a parameter related to a pressure
of exhaust gas in the exhaust passage, the first sensing portion (20a) being remote
from the exhaust passage (16);
a second sensing portion (20b) configured to determine a parameter related to a pressure
of exhaust gas in the exhaust passage (16), the second sensing portion (20b) being
remote from the exhaust passage (16);
a first conduit (22) extending between the first sensing portion (20a) and the first
conduit port (23) for fluidly connecting the first sensing portion (20a) with the
exhaust passage (16);
a second conduit (24) extending between the second sensing portion (20b) and the second
conduit port (25) for fluidly connecting the second sensing portion (20b) with the
exhaust passage (16);
a first bleed passage (26) extending between the first conduit (22) and a first bleed
connection (27) for fluidly connecting the first bleed passage (26) with another portion
of the exhaust system (12) enabling a substantially continuous flow of exhaust gas
through at least a portion of the first conduit (22); and
a second bleed passage (28) extending between the second conduit (24) and a second
bleed connection (29) for fluidly connecting the second bleed passage (28) with another
portion of the exhaust system (12) enabling a substantially continuous flow of exhaust
gas through at least a portion of the second conduit (24) wherein the first conduit
port (23) is located in a portion of the exhaust passage (16a) upstream of the restriction
(18) and the second conduit port (25) is located in a portion of the exhaust passage
(16b) downstream of the restriction (18).
2. An exhaust system (12) according to claim 1, wherein said first and second sensing
portions (20a, 20b) are portions of a single Δp sensor.
3. An exhaust system (12) according to claim 1, wherein the first sensing portion (20a)
is a first pressure sensor and the second sensing portion (20b) is a second pressure
sensor.
4. An exhaust system (12) according to any of the preceding claims wherein the restriction
(18) is a venturi.
5. An exhaust system (12) according to any of claims 1 to 3, wherein the restriction
(18) is an EGR valve.
6. An exhaust system (12) according to any of claims 1 to 5, wherein the first and second
bleed connections (27, 29) are fluidly connected to each other.
7. An exhaust system (12) according to any of the preceding claims, wherein at least
one of the first and second bleed connections (27, 29) is located in the exhaust system
(12) such that exhaust gas tends to flow predominantly from the bleed passage (26,
28) to the associated bleed connection (27, 29).
8. An exhaust system (12) according to any of the preceding claims, wherein at least
one of the first and second bleed connections (27, 29) is located in the exhaust system
(12) such that exhaust gas tends to flow predominantly from the bleed connection (27,
29) to the associated bleed passage (26, 28).
9. An exhaust system (12) according to any of claims 1 to 5, wherein both the first
and second bleed connections (27, 29) are located in a portion of the exhaust passage
(16a) upstream of the restriction (18).
10. An exhaust system (12) according to any of claims 1 to 5, wherein both the first
and second bleed connections (27, 29) are located in a portion of the exhaust passage
(16b) downstream of the restriction (18).
11. An exhaust system (12) according to any of the preceding claims, wherein at least
one of the fluid connections a) between the first conduit (22) and the first bleed
passage (26) and b) between the second conduit (24) and the second bleed passage (28)
is located within 50 millimeters from the first conduit port (23).
12. An exhaust system (12) according to any of the preceding claims, wherein at least
one of the fluid connections between a) between the first conduit (22) and the first
bleed passage (26) and b) between the second conduit (24) and the second bleed passage
(28) is located within 25 millimeters from the first conduit port (23).
13. An exhaust system (12) according to any of claims 1 to 10, wherein at least one of
the fluid connections a) between the first conduit (22) and the first bleed passage
(26) and b) between the second conduit (24) and the second bleed passage (28) is located
adjacent the associated sensing portion (20a, 20b)
14. An exhaust system (12) according to any of the preceding claims wherein at least
one of the first and second bleed passages (26, 28) includes a portion having a small
cross-sectional diameter relative to the exhaust passage (16) such that any flow through
the at least one of the first and second bleed passages (26, 28) is little or insignificant
compared through the flow flowing through the exhaust passage (16).

