The present invention relates to an exhaust gas recirculation valve for recirculating exhaust gas to an inlet system.
An exhaust gas recirculation (EGR) valve controls the opening of a valve body arranged at a branching point between an exhaust passage and an exhaust gas recirculation passage to thereby regulate the amount of recirculated exhaust gas that is recirculated to an intake passage via the exhaust gas recirculation passage.
For example, in a valve device of Patent Document 1, a butterfly valve is provided within a housing formed at a section where an inlet tube into which exhaust gas flows from an internal combustion engine, a first outlet tube leading to the outside, and a second outlet tube leading to a recirculation device intersect one another. The butterfly valve is located downstream of the connecting portion of those tubes at a position to hinder the flow of the fluid thereto, and has a three-way valve structure configured to control the flow of the fluid by being rotated with a motor and to control the amount of exhaust gas flowing to the recirculation device.
For other examples of the three-way valve structure, there are Patent Documents 2 and 3, for instance. An exhaust gas processing device of Patent Document 2 is constructed of, within a valve chamber having one inlet and two outlets, an arm turning about a spindle as a fulcrum, a support rod provided at a valve guard of this arm, and flap valves supported on the opposite sides of the arm with the support rod to have a degree of freedom in inclination, and has a three-way valve structure configured to alternately collect contaminants in the exhaust gas by alternately opening/closing the two outlets with the front and back surfaces of the flap valve.
Also, an exhaust gas recirculation device of Patent Document 3 has a butterfly valve provided at a merging portion between a cooler passage and a bypass passage extending in parallel, and has a three-way valve structure for controlling a mixing ratio of exhaust gases flowing into the merging portion from the passages.
In the three-way valve structure of Patent Document 1, the butterfly valve is located at the position to hinder the flow of the exhaust gas, which poses a problem leading to losses of the flow rate and pressure. In addition, since the inlet and outlet tubes for the exhaust gas are not aligned on a straight line, an exhaust gas pipe connected to the outlet tube has to be bent to draw back to the position of a muffler, which may pose problems such as increased size of the housing, and decreased degree of freedom in piping in an engine layout.
The three-way valve structures of Patent Document 2 and 3 have no configurations to be intended for exhaust gas recirculation valves, they cannot be simply applied to the recirculation ones. In addition, like Patent Document 1, the valve is located at the position to hinder the flow of the fluid, and the inlet and outlets are not arranged linearly, which may also cause the aforementioned problem.
The present invention is made to solve the above-described problems, and an object of the invention is to provide an exhaust gas recirculation valve in which an exhaust passage is formed linearly to reduce the loss of a flow rate thereof, and in which, for example, no occurrence of bends of an exhaust pipe due to an arrangement of the exhaust gas recirculation valve is implemented to thus improve a degree of freedom in piping in an engine layout.
An exhaust gas recirculation valve according to the present invention includes: a linear exhaust passage for passing exhaust gas therethrough; an exhaust gas recirculation passage, branched from the exhaust passage, for conducting the exhaust gas to an intake passage; a shaft rotatably located on an inner wall of a passage that is branched to the exhaust passage and the exhaust gas recirculation passage; and a butterfly valve having two wings rotating about the shaft, and configured such that when a first wing thereof opens the exhaust passage, a second wing thereof closes the exhaust gas recirculation passage, and that when the first wing narrows the exhaust passage, the second wing opens the exhaust gas recirculation passage.
According to the invention, when the exhaust passage is formed linearly, the pressure loss of the exhaust gas can be suppressed to thereby reduce the loss of the flow rate, and also, for example, no occurrence of bends of an exhaust gas pipe due to an arrangement of the exhaust gas recirculation valve is implemented to thus improve a degree of freedom in piping in an engine layout, which may achieve compactness thereof.
In the following, in order to describe the present invention in more detail, embodiments for carrying out the invention will now be described in detail with reference to the accompanying drawings.
As shown in
In
In the exhaust gas recirculation valve shown in
Bearing sections 10a, 10b are formed at the branching point in the housing 1 where the EGR passage 7 and the exhaust passage 4 are branched. When these bearing sections 10a, 10b rotatably support a shaft 8 at its opposite ends in an axial direction thereof, the shaft 8 is pivotally supported at a certain position on the inner wall of the passages at the branching point. An elliptical butterfly valve 9 is attached to this shaft 8. A valve seat 5a to be seated by a second wing 9b of the butterfly valve 9 is formed in the remaining part of the opening of the branch opening 5 except the part where the shaft 8 is disposed.
Incidentally, although in the illustrated example, the shaft 8 is supported at the opposite ends by the bearing sections 10a, 10b, it may be cantilever supported by the bearing section provided at either of the ends.
When the shaft 8 is rotation driven by an actuator (not shown), the butterfly valve 9 attached to this shaft 8 is also rotated integrally. The rotation of the butterfly valve 9 in one direction causes a first wing 9a to gradually move in a direction to close the exhaust passage 4, narrowing an opening area thereof, and at the same time the second wing 9b gradually opens the EGR passage 7. When the butterfly valve 9 is rotated in the opposite direction thereof, the first wing 9a gradually opens the exhaust passage 4, and at the same time the second wing 9b gradually closes the EGR passage 7.
Hereupon, a description will be given of a relationship between shapes of the exhaust passage 4 and losses in flow rate and pressure.
From the graphs in
Since the exhaust passage 4 is formed linearly in Embodiment 1, the losses in the flow rate and pressure of the exhaust gas are lowered. In addition, since the shaft 8 is arranged at the branching point between the exhaust passage 4 and the EGR passage 7, the shaft 8 does not interfere with the flow of the exhaust gas, which enables to suppress the loss in the flow rate. Meanwhile, when the exhaust passage 4 is opened, the first wing 9a of the butterfly valve 9 conforms to the inner wall surface of the exhaust passage 4, and at the same time the second wing 9b closes the branch opening 5, and therefore the two (first and second) wings 9a, 9b do not interfere with the flow of the exhaust gas within the exhaust passage 4, and the loss in the flow rate can be suppressed.
Further, since the exhaust gas inlet 2 and the exhaust gas outlet 3 are located on the same straight line, in the case where the exhaust gas recirculation valve is arranged midway of the exhaust passage 25 shown in
In an example shown in
Also, since the butterfly valve 9 has an elliptical shape with the arc sections conforming to a circular cross section of the cylindrical exhaust passage 4, an extended diameter of a valve orbit passing portion 11 in the housing 1 that is a portion where the butterfly valve 9 passes during opening/closing operations thereof can be suppressed to a minimum. Thus, compactness and weight reduction of the housing 1 can be achieved.
In contrast,
Furthermore, when the valve is opened at the exhaust passage 4 as shown in
On the other hand, when the valve is closed at the exhaust passage 4 as shown in
In the butterfly valve 9 described so far, it is configured that since as shown in
Since the length d1 of the wing 9a can be adjusted easily by forming the butterfly valve 9 in an asymmetrical shape about the shaft 8, any amount of clearance d3, that is, the maximum EGR amount can be adjusted according to the conditions of an engine combustion chamber 23.
Further, when the valve is closed at the exhaust passage 4, the pressures applied to the two wings 9a and 9b are adjusted such that an area ratio between the wings 9a and 9b is changed; thus, an adjustment of the torque can be done easily. Therefore, it becomes possible to further reduce the torque produced in the butterfly valve 9.
As described above, according to Embodiment 1, the exhaust gas recirculation valve is configured to include: the linear exhaust passage 4 for causing the exhaust gas to pass therethrough; the EGR passage 7, branched from the exhaust passage 4, for conducting the exhaust gas to the intake passage 20 (or the intake passage 22); the rotatable shaft 8 rotatably located on the inner wall of the passage that is branched to the exhaust passage 4 and the EGR passage 7; and the butterfly valve 9 having the two wings 9a, 9b rotating about the shaft 8, and configured such that when the first wing 9a opens the exhaust passage 4, the second wing 9b closes the exhaust gas recirculation passage 7, and that when the first wing 9a narrows the exhaust passage 4, the second wing 9b opens the EGR passage 7. For this reason, the pressure loss of the exhaust gas flowing through the exhaust passage 4 is suppressed to thereby reduce the loss in the flow rate. In addition, the degree of freedom in piping in an engine layout can be improved by, for instance, no occurrence of bends of the exhaust pipe due to the arrangement of the exhaust gas recirculation valve, and consequently the engine can be made compact. Further, since the valve body is formed in a butterfly shape, the torque can be reduced.
Also, according to Embodiment 1, it is configured that the butterfly valve 9 has an elliptical shape including the linear section in a direction orthogonal to the axial direction of the shaft 8, and the arc sections at the opposite ends thereof, and therefore the enlargement of the diameter in the valve orbit passing portion 11 can be suppressed to a minimum to thereby perform the downsizing and weight reduction of the housing 1. Further, the valve can be simplified in the shape, and fabricated easily and at low cost.
Also, according to Embodiment 1, the butterfly valve 9 can be easily formed in an asymmetrical shape when the linear section in the elliptical shape of the butterfly valve 9 is only changed in the dimension. Then, it is configured that the butterfly valve 9 has the two wings 9a, 9b having an elliptical shape to be asymmetrical about the shaft 8 to form a clearance between the first wing 9a and the internal wall of the exhaust passage 4, when the first wing 9a closes the exhaust passage 4, and therefore the amount of throttling the exhaust in the exhaust passage 4 can be adjusted and the torque can be further reduced.
However, according to the present invention, within the scope of the invention, a modification of arbitrary components in the embodiments or an omission of arbitrary components in the embodiments is possible.
As described above, the exhaust gas recirculation valve of the present invention may be used as the exhaust gas recirculation valve 27 for low-pressure EGR or as the exhaust gas recirculation valve 29 for high-pressure EGR as shown in
1 housing, 2 exhaust gas inlet, 3 exhaust gas outlet, 4 exhaust passage, 5 branch opening, 5a valve seat, 6 EGR gas outlet, 7 EGR passage, 8 shaft, 9 butterfly valve, 9a, 9b wing, 10a, 10b bearing section, 11 valve orbit passing portion, 20, 22 intake passage, 21 compressor, 23 engine combustion chamber, 24 turbine, 25 exhaust passage, 26 low-pressure EGR passage, 27, 29 exhaust gas recirculation valve, 28 high-pressure EGR passage
Filing Document | Filing Date | Country | Kind | 371c Date |
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PCT/JP2010/007221 | 12/13/2010 | WO | 00 | 2/28/2013 |