Information
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Patent Grant
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6408833
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Patent Number
6,408,833
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Date Filed
Thursday, December 7, 200024 years ago
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Date Issued
Tuesday, June 25, 200222 years ago
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Inventors
-
Original Assignees
-
Examiners
Agents
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CPC
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US Classifications
Field of Search
US
- 123 56817
- 123 56818
- 060 6052
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International Classifications
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Abstract
An internal combustion engine is provided with a combustion air supply, an intake manifold, an exhaust manifold, and an exhaust gas recirculation system having a venturi assembly. The venturi assembly includes an outlet, a combustion air inlet connected and in communication with the combustion air supply, and an exhaust gas inlet connected and in communication with the exhaust manifold. A bypass fluid line and a bypass valve in the nature of a check valve are provided to bypass the venturi assembly. The check valve is responsive to changes in pressure drop across the venturi assembly, to open and close the bypass fluid line and limit the pressure drop across the venturi assembly.
Description
TECHNICAL FIELD
The present invention relates to exhaust gas recirculation systems in an internal combustion engine, and, more particularly, to a bypass system for an induction venturi assembly in such exhaust gas recirculation systems.
BACKGROUND ART
An exhaust gas recirculation (EGR) system is used for controlling the generation of undesirable pollutant gases and particulate matter in the operation of internal combustion engines. Such systems have proven particularly useful in internal combustion engines used in motor vehicles such as passenger cars, light duty trucks, and other on-road motor equipment. EGR systems primarily recirculate the exhaust gas by-products into the intake air supply of the internal combustion engine. The exhaust gas which is reintroduced to the engine cylinder reduces the concentration of oxygen therein, which in turn lowers the maximum combustion temperature within the cylinder, and slows the chemical reaction of the combustion process, decreasing the formation of nitrous oxides (NOx). Furthermore, the exhaust gases typically contain unburned hydrocarbons, which are burned upon reintroduction into the engine cylinder, further reducing the emission of exhaust gas by-products that otherwise would be emitted as undesirable pollutants from the internal combustion engine.
When utilizing EGR in a turbocharged diesel engine, the exhaust gas to be recirculated is preferably removed upstream of the exhaust gas driven turbine associated with the turbocharger. In many EGR applications, the exhaust gas is diverted directly from the exhaust manifold. Likewise, the recirculated exhaust gas is preferably reintroduced to the intake air stream downstream of the compressor and air-to-air aftercooler (ATAAC). Reintroducing the exhaust gas downstream of the compressor and ATAAC is preferred due to reliability and maintainability concerns that arise if the exhaust gas passes through the compressor and/or ATAAC. An example of such an EGR system is disclosed in U.S. Pat. No. 5,802,846 (Bailey), which is assigned to the assignee of the present invention.
With conventional EGR systems as described above, the charged and cooled combustion air transported from the ATAAC is at a relatively high pressure, as a result of the charging from the turbocharger. Since, typically, the exhaust gas is inducted into the combustion air flow downstream of the ATAAC, conventional EGR systems are configured to allow the lower pressure exhaust gas to mix with the higher pressure combustion air before the combined flow is introduced in to the intake manifold. Such EGR systems may include a venturi assembly, which induces the flow of exhaust gas into the flow of combustion air passing therethrough. An efficient venturi assembly is designed to “pump” exhaust gas from a lower pressure exhaust manifold to a higher pressure intake manifold. However, because varying EGR rates are required throughout the engine speed and load range, a variable orifice venturi assembly may be preferred. Such a variable orifice venturi assembly is physically difficult and complex to design and manufacture. Accordingly, venturi systems including a fixed orifice venturi assembly and a combustion air bypass circuit are favored. The bypass circuit consists of piping and a butterfly valve in a combustion air flow path. The butterfly valve is controllably actuated using an electronic controller which senses various parameters associated with operation of the engine. A bypass circuit can prevent excessive pressure losses in the combustion air circuit, which otherwise might occur during periods of high combustion air flow rates, such as at high engine speeds.
With a venturi assembly as described above, the maximum flow velocity and minimum pressure of the combustion air flowing through the venturi assembly occurs within the venturi throat disposed upstream from the expansion section. The butterfly valve is used to control the flow of combustion air to the venturi throat, which in turn affects the flow velocity and vacuum pressure created therein. By varying the vacuum pressure, the amount of exhaust gas induced into the venturi throat of the venturi assembly can be varied. However, the butterfly valve and electronic controller therefor can add complexity to the EGR system, increasing the chance for system failure and increasing the expense associated with repair.
The present invention is directed to overcoming one or more of the problems as set forth above.
DISCLOSURE OF THE INVENTION
In one aspect of the invention, an internal combustion engine comprises a combustion air supply, an exhaust manifold and an intake manifold. A venturi assembly includes an outlet connected and in communication with the intake manifold, a combustion air inlet connected and in communication with the combustion air supply, and an exhaust gas inlet connected and in communication with the exhaust manifold. A bypass fluid line is connected and in communication with the combustion air supply, and connected and in communication with the intake manifold, bypassing the venturi assembly. A bypass valve, controls flow through the bypass fluid line, the bypass valve being responsive to pressure differential on opposite sides of the venturi assembly.
In another aspect of the present invention, a venturi bypass system for recirculating exhaust gas in an internal combustion engine, comprises a venturi assembly having an outlet, a combustion air inlet and an exhaust gas inlet; a bypass line conducting combustion air around the venturi assembly; and a bypass valve positioned in the bypass line to open and close the bypass line in response to pressure drop across the venturi assembly.
In still another aspect of the present invention, a method of recirculating exhaust gas in an internal combustion engine, comprises providing an exhaust gas recirculation system including a venturi assembly having a combustion air inlet, an exhaust gas inlet and an outlet; transporting combustion air to the combustion air inlet; transporting exhaust gas to the exhaust gas inlet; and selectively controlling flow through the bypass line in response to pressure drop across the venturi assembly, thereby controlling the pressure drop across the venturi assembly.
BRIEF DESCRIPTION OF THE DRAWINGS
The sole drawing,
FIG. 1
, illustrates an internal combustion engine including an embodiment of a venturi bypass exhaust gas re-circulation system of the present invention.
BEST MODE FOR CARRYING OUT THE INVENTION
Referring now to the drawing, there is shown an embodiment of an internal combustion engine
10
, including an embodiment of a venturi bypass system
12
of the present invention. Internal combustion engine
10
also includes a combustion air supply
14
, intake manifold
16
, exhaust manifolds
18
and
20
and a plurality of combustion cylinders
22
. In the embodiment shown, engine
10
includes six combustion cylinders
22
, but may include more or fewer combustion cylinders
22
, as those skilled in the art will recognize readily.
Intake manifold
16
and exhaust manifolds
18
,
20
are each fluidly coupled with a plurality of combustion cylinders
22
, as indicated schematically by intake and exhaust fluid lines
24
and
26
, respectively. In the embodiment shown, a single intake manifold
16
is fluidly coupled with each combustion cylinder
22
. However, it is also possible to configure intake manifold
16
as a split or multiple-piece manifold, each associated with a different group of combustion cylinders. Each exhaust manifold
18
and exhaust manifold
20
is coupled to a plurality of combustion cylinders
22
, and, as shown, each is connected to three different combustion cylinders
22
. However, it is also possible to configure engine
10
with a single exhaust manifold, or with more exhaust manifolds and with more or fewer combustion cylinders.
Combustion air supply
14
provides a source of pressurized combustion air to venturi bypass system
12
, and ultimately to intake manifold
16
. Combustion air supply
14
includes a turbocharger
28
and an ATAAC
30
, each of which is shown schematically for simplicity. Turbocharger
28
includes a turbine
32
and a compressor
34
therein. The turbine, in known manner, is driven by exhaust gas received from exhaust manifolds
18
and
20
via fluid lines
36
and
38
, respectively. Turbine
32
is mechanically coupled with compressor
34
, such as by a shaft
40
, to drive compressor
34
. Compressor
34
receives ambient combustion air, as indicated by arrow
42
. Compressor
34
compresses the ambient combustion air, and outputs compressed combustion air via fluid line
44
. The compressed combustion air is at an elevated temperature as a result of the work performed thereon during the compression process within turbocharger
28
. The hot combustion air is then cooled within ATAAC
30
. Spent exhaust gas from turbine
32
is passed from turbocharger
28
, as indicated by arrow
46
, to subsequent exhaust gas processing, which may include a muffler, not shown, an is ultimately discharged to the ambient environment.
An exhaust gas re-circulation (EGR) system
50
includes fluid lines
52
and
54
from, respectively, exhaust manifolds
18
and
20
. EGR valves
56
and
58
are provided in fluid lines
52
and
54
, respectively, to control the flow of exhaust gases from exhaust manifolds
18
and
20
. Flows from EGR valves
56
and
58
are combined in a single EGR fluid line
60
having an EGR cooler
62
therein.
Venturi bypass system
12
receives cooled and compressed combustion air via line
44
, and also receives exhaust gas via EGR fluid line
60
. Venturi bypass system
12
controllably mixes a selected amount of exhaust gas with the cooled and compressed combustion air, and outputs the air/exhaust gas mixture to a combustion fluid line
70
fluidly connected to intake manifold
16
. More particularly, venturi bypass system
12
includes a venturi assembly
72
having an outlet
74
, a combustion air inlet
76
and an exhaust gas inlet
78
. Combustion air inlet
76
is connected to, and in communication with, combustion air supply
14
, via fluid line
44
. Exhaust gas inlet
78
is connected to, and in communication with, exhaust manifolds
18
and
20
via EGR fluid line
60
. Outlet
74
is connected to, and in communication with, intake manifold
16
via combustion fluid line
70
.
Venturi assembly
72
, in known manner, not shown in detail herein, includes a venturi nozzle in communication with combustion air inlet
76
. The venturi nozzle defines and terminates at a venturi throat. Venturi assembly
72
further defines an exhaust gas venturi section, which tapers to and terminates at an induction area at which exhaust gas from exhaust gas inlet
78
is inducted into the passing flow of compressed combustion air traveling at an increased velocity and decreased pressure through the induction area. Dependent upon the pressure and velocity of the compressed combustion air, the amount of exhaust gas inducted into the flow may be controllably varied. Venturi assembly
72
also may define a receiver section positioned immediately downstream from the induction area. The receiver section typically has a cross sectional area that remains substantially constant for a predetermined distance in the direction of fluid flow, to assist in uniformly mixing the inducted exhaust gas into the flow of combustion air.
In accordance with the present invention, a bypass fluid line
80
extends between fluid line
44
and combustion fluid line
70
, and defines a bypass path for combustion air around venturi assembly
72
. A valve
82
is positioned within bypass fluid line
80
, and controls the flow of fluid bypassing venturi assembly
72
from fluid line
44
to combustion fluid line
70
. Valve
82
is controllably actuated to open and close bypass fluid line
80
in response to pressure drop across venturi assembly
72
. In accordance with the present invention, bypass valve
82
is in the form of a check valve that is spring loaded and responsive to the pressure drop across venturi assembly
72
. Bypass valve
82
has an inlet
84
on the turbocharger side of valve
82
, inlet
82
being in communication with fluid line
44
through bypass line
80
. By pass valve
82
has an outlet
86
on the intake manifold side of valve
82
, outlet
86
being in communication with combustion fluid line
70
through bypass fluid line
80
. Bypass valve
82
is responsive to the pressure differential from inlet
84
to outlet
86
, to selectively open after a preset differential is reached. Valve
82
thereby is controllably actuated in response to the pressure drop to selectively open and close, to control an amount of combustion air that flows through bypass fluid line
80
, thereby bypassing venturi assembly
72
.
INDUSTRIAL APPLICABILITY
During use, combustion occurs within combustion cylinders
22
, which produces exhaust gas received within exhaust manifolds
18
and
20
. Exhaust gas is transported to turbocharger
28
via fluid lines
36
and
38
, for rotatably driving turbine
32
of turbocharger
28
. Turbine
32
rotatably drives shaft
40
, and thereby compressor
34
, which in turn compresses combustion air and outputs compressed combustion air via fluid line
44
. The hot, compressed combustion air is cooled within ATAAC
30
, and is transported via line
44
to combustion air inlet
76
of venturi assembly
72
. The fluid pressure in fluid line
44
is also experienced in bypass line
80
, on the turbocharger side of bypass valve
82
.
As the combustion air flows through venturi assembly
72
, the velocity thereof increases and the pressure decreases. Exhaust gas from exhaust manifolds
18
and
20
, cooled in EGR cooler
62
is received at exhaust gas inlet
78
via fluid line
60
. Dependent upon the pressure and velocity of the combustion air which flows through venturi assembly
72
, the amount of exhaust gas inducted into the passing flow of combustion air is varied. The combustion air/exhaust gas mixture flows from venturi assembly
72
, through combustion fluid line
70
, to intake manifold
16
. The fluid pressure in combustion fluid line
70
is also experienced in bypass line
80
, on the intake manifold side of bypass valve
82
. By varying the degree to which bypass valve
82
is opened, the amount of compressed air from turbocharger
28
which is allowed to bypass venturi assembly
72
and flow directly to intake manifold
16
, may likewise be varied. Bypass valve
82
is provided with a preset spring load to allow a given amount of pressure drop across venturi assembly
72
. As the pressure drop across venturi assembly
72
exceeds the pre-established acceptable limit, spring loaded check bypass valve
72
begins to open, allowing bypass flow from fluid line
44
to combustion fluid line
70
, through bypass fluid line
80
. Combustion air flow from fluid line
44
to combustion fluid line
70
, via bypass fluid line
80
, limits the pressure drop across venturi assembly
72
to the pre-established acceptable limit for efficient operation of EGR system
50
and venturi assembly
72
thereof.
By way of example, and not limitation, a typical fixed venturi EGR system, at low engine speed may experience a pressure drop across venturi assembly
72
of 8 kPa, which allows adequate EGR induction. At higher engine speeds, the pressure drop across venturi assembly
72
may increase to 28 kPa. Control of the EGR flow to desired levels may require the adjustment of EGR valves
56
and
58
. However, with a venturi bypass system
12
of the present invention, bypass check valve
82
may be set to limit pressure drop across venturi assembly
72
to, for example, 15 kPa. If the pressure drop exceeds 15 kPa, valve
82
opens sufficiently to allow flow through bypass fluid line
80
, and limit the pressure drop to 15 kPa.
Venturi bypass system
12
of the present invention allows exhaust gas to be effectively and controllably inducted into a pressurized flow of combustion air, over a wide range of engine operating speeds and conditions, using a fixed venturi assembly. The simplicity of the system minimizes the risk of failure and the expense of repair. Thus, the venturi bypass system provides a compact design with simple and efficient operation.
Other aspects, objects and advantages of this invention can be obtained from a study of the drawings, the disclosure and the appended claims.
Claims
- 1. An internal combustion engine, comprising:a combustion air supply; an exhaust manifold; an intake manifold; a venturi assembly including an outlet connected and in communication with said intake manifold, a combustion air inlet connected and in communication with said combustion air supply, and an exhaust gas inlet connected and in communication with said exhaust manifold; a bypass fluid line connected and in communication with,said combustion air supply, and connected and in communication with said intake manifold and bypassing said venturi assembly; and a bypass valve, controlling flow through said bypass fluid line, said bypass control valve being responsive to pressure differential on opposite sides of said venturi assembly.
- 2. The internal combustion engine of claim 1, said bypass valve being a spring loaded check valve.
- 3. The internal combustion engine of claim 2, said spring loaded check valve arranged to open in response to increased pressure drop across said venturi assembly.
- 4. The internal combustion engine of claim 3, said combustion air supply including an exhaust gas turbocharger.
- 5. The internal combustion engine of claim 1, said combustion air supply including an exhaust gas turbocharger.
- 6. The internal combustion engine of claim 1, said combustion air supply including a turbocharger having a turbine in communication with and operated by exhaust gas flow from said exhaust manifold and a compressor operated by said turbine, said compressor providing combustion air to said intake manifold.
- 7. The internal combustion engine of claim 6, including a fluid line from said compressor to said venturi assembly, and said bypass fluid line connected to and in communication with said fluid line from said compressor.
- 8. The internal combustion engine of claim 7, including a combustion fluid line from said venturi assembly to said intake manifold, and said bypass fluid line connected to and in communication with said combustion fluid line.
- 9. The internal combustion engine of claim 8, including an aftercooler in said fluid line from said compressor.
- 10. The internal combustion engine of claim 1, including a combustion fluid line from said venturi assembly to said intake manifold, and said bypass fluid line connected to and in communication with said combustion fluid line.
- 11. A venturi bypass system for recirculating exhaust gas in an internal combustion engine, comprising:a venturi assembly having an outlet, a combustion air inlet and an exhaust gas inlet; a bypass fluid line conducting combustion air around said venturi assembly; and a bypass valve positioned in said bypass fluid line to open and close said bypass fluid line in response to pressure drop across said venturi assembly.
- 12. The venturi bypass system of claim 11, said bypass valve being a spring loaded check valve.
- 13. The venturi bypass system of claim 11, including a combustion air supply, a fluid line connected to and in flow communication with said combustion air inlet and said combustion air supply, a combustion fluid line connected to and in communication with said outlet, and said bypass fluid line connected to and in flow communication with said fluid line and said combustion fluid line.
- 14. The venturi bypass system of claim 13, said bypass valve being a spring loaded check valve.
- 15. The venturi bypass system of claim 14, said check valve being responsive to differential pressure on opposite sides thereof.
- 16. A method of recirculating exhaust gas in an internal combustion engine, comprising the steps of:providing an exhaust gas recirculation system including a venturi assembly having a combustion air inlet, an exhaust gas inlet and an outlet; transporting combustion air to said combustion air inlet; transporting exhaust gas to said exhaust gas inlet; providing a bypass fluid line for transporting combustion air around said venturi assembly; and selectively controlling flow through said bypass fluid line in response to pressure drop across said venturi assembly, and thereby controlling a pressure drop across said venturi assembly.
- 17. The method of claim 16, including selectively operating a bypass valve in response to pressure drop across said venturi assembly.
- 18. The method of claim 17, including operating said bypass valve to open and close said bypass fluid line in response to the differential pressure on opposite sides of said bypass valve.
- 19. The method of claim 17, including providing a spring operated check valve in said bypass fluid line, and operating said check valve to open and close said bypass fluid line in response to the differential pressure on opposite sides of said check valve.
- 20. The method of claim 16, including providing a spring loaded check valve in said bypass fluid line, and operating said spring loaded check valve in response to pressure drop across said venturi assembly.
US Referenced Citations (21)