Exhaust passage

Abstract

An exhaust passage including a protrusion which is less likely to receive heat from a gas and hence has high heat-resistance reliability is provided. An exhaust passage includes an exhaust pipe, and a protrusion continuously formed over a range of a part of an inner surface of the exhaust pipe in a circumferential direction thereof, the protrusion being inclined toward a direction in which the exhaust pipe extends, and being configured in such a manner that a cross-sectional area of the exhaust pipe becomes smaller toward a downstream side thereof, in which the exhaust passage further includes a convex part on an inner surface of the protrusion.

Claims

1. An exhaust passage comprising: an exhaust pipe; and a protrusion continuously formed over a range of a part of an inner surface of the exhaust pipe in a circumferential direction thereof, the protrusion being inclined toward a direction in which the exhaust pipe extends, and the protrusion configured in such a manner that a cross-sectional area of the exhaust pipe becomes smaller toward a downstream side thereof, wherein the exhaust passage further comprises a convex part on an inner surface of the protrusion.

2. The exhaust passage according to claim 1, wherein the convex part is a linear convex part, and a plurality of convex parts are arranged with an interval therebetween in the direction in which the exhaust pipe extends.

3. The exhaust passage according to claim 1, wherein the convex part is provided in a part of the protrusion where a thermal stress is exerted on the protrusion.

4. The exhaust passage according to claim 1, wherein a plurality of convex parts are arranged in a staggered pattern.

Description

BRIEF DESCRIPTION OF DRAWINGS

(1) FIG. 1 is a schematic diagram showing an example of an exhaust passage according to the present disclosure;

(2) FIG. 2 is a schematic diagram of an example of a protrusion;

(3) FIG. 3 is a schematic diagram for explaining a flow of gas;

(4) FIG. 4 is a schematic top view and a schematic side view showing an example of a protrusion of an exhaust passage according to a first embodiment;

(5) FIG. 5 is a schematic diagram for explaining a flow of gas in the first embodiment;

(6) FIG. 6 is a schematic bottom view showing an example of a protrusion of an exhaust passage according to a second embodiment;

(7) FIG. 7 is a cross-sectional view taken along a line A-A in FIG. 6;

(8) FIG. 8 is a schematic top view and a schematic side view showing an example of a protrusion of an exhaust passage according to a third embodiment;

(9) FIG. 9 shows temperatures of a protrusion according to related art; and

(10) FIG. 10 shows magnitudes of thermal stresses exerted on a protrusion according to related art.

DESCRIPTION OF EMBODIMENTS

(11) The present disclosure will be explained hereinafter through embodiments according to the present disclosure. However, the below-shown embodiments are not intended to limit the scope of the present disclosure specified in the claims. Further, for clarifying the explanation, the following description and drawings are simplified as appropriate. Note that, in this specification, an X-axis is defined in the downstream direction in the axial direction of the exhaust pipe (the direction in which the exhaust pipe extends, hereinafter also referred to as the extending direction of the exhaust pipe), and a plane perpendicular to the X-axis is referred to as (i.e., defined as) a YZ-plane (also referred to simply as a cross section).

(12) An exhaust passage 10 shown in the example shown in FIG. 1 is an exhaust passage that is suitably used in an internal combustion engine, and includes an exhaust pipe 11 (exhaust pipes 11A and 11B), and a protrusion 20, and also includes convex parts 21 on the inner surface of the protrusion 20.

(13) As shown in FIG. 2, the protrusion 20 is inclined toward the central-axis direction of the exhaust pipe, and has a tapered shape from a base end 23 of the protrusion 20 toward a tip 22 thereof. The base end 23 of the protrusion is connected to the exhaust pipe 11A. The protrusion 20 and the exhaust pipe 11A may be connected by welding, or they may be integrally molded. Note that the illustration of the convex parts 21 is omitted in FIG. 2.

(14) The exhaust pipe 11A shown in FIG. 1 may be connected to another pipe (not shown) on the upstream side thereof. Further, an air-fuel ratio sensor (not shown) is disposed on the downstream side of the exhaust pipe 11B.

(15) In FIG. 1, a gas 31 flows in the X-axis direction. Note that, in the exhaust passage including the protrusion 20, a part of the exhaust gas 32 hits the protrusion 20 and flows 33 along the protrusion 20. Because the protrusion 20 has the tapered shape, a part of the gas 34 comes off the protrusion as it flows downstream, so that an airflow indicted by a dashed-line arrow is formed. This airflow is continuously formed over the entire area of the protrusion 20 and becomes a swirling flow, and the gas is further stirred throughout the inside of the pipe even after the airflow has passed through the protrusion 20. As a result, the surface uniformity of the gas is improved, and therefore the accuracy of the measurement by the sensor is improved. Further, the exhaust passage according to this embodiment has a relatively large opening (i.e., a large mouth) even at the place thereon where the protrusion 20 is provided. Further, the above-described swirling flow spreads throughout the inside of the pipe, so it is possible to prevent or reduce an increase in the pressure loss.

(16) There are cases in which the temperature of the exhaust gas 31 exceeds 800° C. FIG. 9 shows temperatures of a protrusion 51 not including any convex part 21 when a gas having a temperature of 800° C. flows around the protrusion 51. The base end 53 of the protrusion 51 is close to the exhaust pipe 11 and heat tends to be dissipated therefrom, whereas heat cannot be dissipated from the tip 52. Therefore, the tip 52 has a higher temperature than that of the base end 53, and a large temperature gradient occurs between the tip 52 and the base end 53. As a result, thermal stresses occur as shown in FIG. 10, and a maximum thermal stress area 54 is formed near the base end 53, causing a thermal deformation and/or a thermal creep rupture.

(17) The exhaust passage according to the embodiment solves the above-described problem by providing the convex parts 21 on the inner surface of the protrusion 20. As shown in the example shown in FIG. 3, the gas 35 tends to flow in a straight line, so it does not flow as indicated by a dashed-line arrow 36 even though the convex part 21 is present, but instead flows straight along near the central axis of the exhaust pipe. Therefore, in the protrusion 20 including the convex parts 21, an area which the high-temperature gas is unlikely to enter is formed, so that a boundary insulation layer 40 is formed. As a result, the high-temperature gas is less likely to come into contact with the base material of the protrusion 20. Due to the above-described features, the exhaust passage according to the embodiment becomes an exhaust passage including a protrusion which is less likely to receive heat from a gas and hence has high heat-resistance reliability.

(18) Preferred embodiments will be described hereinafter.

First Embodiment

(19) An exhaust passage according to a first embodiment will be described with reference to FIG. 4. The exhaust passage 10 according to the first embodiment includes an exhaust pipe 11, a protrusion 20, and also includes convex parts 21 on the inner surface of the protrusion 20. Further, the convex parts 21 are linear convex parts (21A, 21B and 21C), and these convex parts are arranged with intervals therebetween in the extending direction of the exhaust pipe.

(20) By providing a plurality of convex parts 21 as shown in FIG. 5, the gas 35 flows straight through an area that is closer to the central axis than the apexes of the convex parts are (i.e., an area between the apexes of the convex parts and the central axis), so that the protrusion is even less likely to receive heat.

(21) The intervals L between adjacent ones of the plurality of convex parts 21 may be constant, or may vary from one interval to another. The intervals L between adjacent convex parts are preferably 10 mm or shorter in order to improve the effect of preventing the gas from coming into direct contact with the base material of the protrusion 20. Meanwhile, the lower limit of each of the intervals L between adjacent convex parts is not limited to any particular value, but as an example, it is 1 mm or longer.

(22) Further, the height H of the convex part 21 is preferably 2 mm or larger in order to prevent the peeling of the boundary insulation layer which would otherwise be caused by the Karman vortex. By preventing the peeling of the boundary insulation layer which would otherwise be caused by the Karman vortex, the boundary insulation layer 40 is stabilized. The upper limit of the height H of the convex part 21 is not limited to any particular values, but as an example, it is 10 mm or smaller.

(23) The method for forming linear convex parts is not limited to any particular methods, but they can be easily formed, for example, by welding.

Second Embodiment

(24) An exhaust passage according to a second embodiment will be described with reference to FIG. 6. The exhaust passage 10 according to the second embodiment includes an exhaust pipe 11, a protrusion 20, and also includes convex parts 21 on the inner surface of the protrusion 20. Further, the convex parts 21 are disposed in parts where thermal stresses are exerted on the protrusion.

(25) By providing the convex parts 21 in the parts where thermal stresses are exerted as shown in FIG. 7, it is possible to prevent a gas 36 having a high temperature from hitting the (maximum) thermal stress area 54.

(26) The method for forming convex parts according to the second embodiment is not limited to any particular methods, but they can be easily formed, for example, by bending.

Third Embodiment

(27) An exhaust passage according to a third embodiment will be described with reference to FIG. 8. The exhaust passage 10 according to the third embodiment includes an exhaust pipe 11, a protrusion 20, and also includes convex parts 21D to 211 on the inner surface of the protrusion 20. Further, these convex parts are arranged in a staggered pattern.

(28) By providing the convex parts in a staggered pattern, a plurality of convex parts, e.g., the convex parts 21D and 21H, are arranged in a gas flow direction 37. By providing a plurality of convex parts, e.g., the convex parts 21D and 21H, in the gas flow direction, similarly to the first embodiment, the gas flows straight through an area that is closer to the central axis than the apexes of the convex parts are (i.e., an area between the apexes of the convex parts and the central axis), so that the protrusion is less likely to receive heat.

(29) The interval L between convex parts (e.g., the interval between the convex parts 21D and 21H) in the gas flow direction is preferably 10 mm or shorter. Meanwhile, the lower limit of the interval L between convex parts is not limited to any particular values, but as an example, it is 1 mm or longer.

(30) Further, the height H of the convex part 21 is preferably 2 mm or larger in order to prevent the peeling of the boundary insulation layer which would otherwise be caused by the Karman vortex. By preventing the peeling of the boundary insulation layer which would otherwise be caused by the Karman vortex, the boundary insulation layer is stabilized. The upper limit of the height H of the convex part 21 is not limited to any particular values, but as an example, it is 10 mm or smaller.

(31) The method for forming convex parts in a staggered pattern is not limited to any particular methods, but they can be formed, for example, by punching out the base material so that parts on the base end side are left, and then performing bending and shaping.

(32) Each of the exhaust passages according to the above-described first to third embodiments includes a protrusion which provides a high stirring effect while preventing or reducing the pressure loss as described above, is less likely to receive heat from a gas, and has high heat-resistance reliability. Therefore, the exhaust passage according to the embodiment can be suitably used, for example, as an exhaust passage of an internal combustion engine. Further, the protrusion used in the exhaust passage according to the embodiment is formed as a single piece and has a relatively simple structure, so it is highly reliable and can be manufactured at a low cost.

(33) From the disclosure thus described, it will be obvious that the embodiments of the disclosure may be varied in many ways. Such variations are not to be regarded as a departure from the spirit and scope of the disclosure, and all such modifications as would be obvious to one skilled in the art are intended for inclusion within the scope of the following claims.