JP2021038701A - Exhaust passage - Google Patents

Exhaust passage Download PDF

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JP2021038701A
JP2021038701A JP2019160397A JP2019160397A JP2021038701A JP 2021038701 A JP2021038701 A JP 2021038701A JP 2019160397 A JP2019160397 A JP 2019160397A JP 2019160397 A JP2019160397 A JP 2019160397A JP 2021038701 A JP2021038701 A JP 2021038701A
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exhaust pipe
exhaust
tapered part
pressure loss
exhaust passage
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JP2021038701A5 (en
JP7351148B2 (en
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直芳 勝美
Naoyoshi Katsumi
直芳 勝美
健司 大橋
Kenji Ohashi
健司 大橋
建光 鈴木
Kenmitsu Suzuki
建光 鈴木
雄士 山口
Yuji Yamaguchi
雄士 山口
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Toyota Motor Corp
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Abstract

To provide an exhaust passage having a high agitation effect while suppressing pressure loss.SOLUTION: An exhaust passage 10 includes: an exhaust pipe 11; and a projection part 20 which is provided continuously to a partial range in a circumferential direction of the inner surface of the exhaust pipe 11 and has a tapered part inclined in the extending direction of the exhaust pipe 11, and the cross sectional area of which is decreased as it approaches the downstream side of the exhaust pipe. Exhaust gas passes through the tapered part of the projection part 20 when the gas flows from upstream to downstream, but gas inside the tapered part is pushed to the outside of the tapered part as it approaches downstream and thereby air flow is generated because the cross sectional area of the tapered part becomes smaller as it approaches the downstream side. The air flows are continuously generated in all the range of the tapered part to become a swirl flow, the agitation of the exhaust gas progresses further in the whole of the inside of the exhaust pipe 11, and thereby accuracy in measurement by a sensor is improved. Also, an opening part is relatively large even at the tapered part and the swirl flow spreads over the whole of the inside of the exhaust pipe 11, so that increase in pressure loss can be suppressed.SELECTED DRAWING: Figure 2

Description

本発明は、排気通路に関する。 The present invention relates to an exhaust passage.

内燃機関の排気管には、排ガス中の酸素濃度を検出するためのセンサが設けられている。内燃機関の運転制御では、例えば検出された酸素濃度に応じて吸入空気量や燃料噴射量が調整されて、空燃比が制御される。
各気筒から出る排ガスは、エキゾーストマニホールドを経て一つの排気管に流入する。排ガスの流れは下流方向への指向性が高く、排気管断面内で偏りが生じやすいため、センサに到達するまでに撹拌するための機構を設けることが検討されている。
The exhaust pipe of the internal combustion engine is provided with a sensor for detecting the oxygen concentration in the exhaust gas. In the operation control of the internal combustion engine, for example, the intake air amount and the fuel injection amount are adjusted according to the detected oxygen concentration, and the air-fuel ratio is controlled.
The exhaust gas emitted from each cylinder flows into one exhaust pipe via the exhaust manifold. Since the flow of exhaust gas has high directivity in the downstream direction and tends to be biased in the cross section of the exhaust pipe, it is being considered to provide a mechanism for stirring before reaching the sensor.

特許文献1には、排気流を分散する分散板として、2つのプレートを組み合わせた分散板が開示されている。
特許文献2には、排ガスセンサと排ガス浄化部との間に配設される排ガス撹拌部として、複数のブレードから構成された翼型形状のフィンが開示されている。
また特許文献3には、第1の排気管と第2の排気管との間に孔を備えた突起部を設けることが開示されている。特許文献3によれば、排気が当該突起部近傍を通過するときに乱流となって、排気が拡散されると記載されている。
Patent Document 1 discloses a dispersion plate in which two plates are combined as a dispersion plate for dispersing an exhaust flow.
Patent Document 2 discloses an airfoil-shaped fin composed of a plurality of blades as an exhaust gas stirring unit arranged between an exhaust gas sensor and an exhaust gas purification unit.
Further, Patent Document 3 discloses that a protrusion having a hole is provided between the first exhaust pipe and the second exhaust pipe. According to Patent Document 3, it is described that when the exhaust gas passes near the protrusion, it becomes a turbulent flow and the exhaust gas is diffused.

特開2016−79962号公報Japanese Unexamined Patent Publication No. 2016-79962 特開2015−55227号公報JP-A-2015-55227 特開2014−126009号公報Japanese Unexamined Patent Publication No. 2014-12609

上記特許文献1〜3の分散板等はいずれも開口率が小さいため、圧力損失が大きくなりやすいという問題があった。また特許文献1〜2の分散板等は、複数のプレートを使用するため、製造コストや信頼性の点で不利なものであった。また、特許文献3の突起部は、孔とセンサの配置によっては、センサへのガス当たり流量が低下してセンサの応答性が悪化する場合があった。 Since the dispersion plates and the like of Patent Documents 1 to 3 have a small aperture ratio, there is a problem that the pressure loss tends to be large. Further, since the dispersion plates and the like of Patent Documents 1 and 2 use a plurality of plates, they are disadvantageous in terms of manufacturing cost and reliability. Further, in the protrusion of Patent Document 3, depending on the arrangement of the hole and the sensor, the flow rate per gas to the sensor may decrease and the responsiveness of the sensor may deteriorate.

本発明はこのような問題を解決するものであり、圧力損失を抑制しながら、高い撹拌効果を有する排気通路を提供するものである。 The present invention solves such a problem and provides an exhaust passage having a high stirring effect while suppressing a pressure loss.

本実施形態にかかる排気通路は、
排気管と、
前記排気管の内面と円周方向の一部の範囲で連続して設けられ、排気管の延在方向に傾き排気管の下流側ほど断面積が小さくなるテーパ部を有する突出部と、を備えることを特徴とする。
The exhaust passage according to this embodiment is
Exhaust pipe and
It is provided with a protruding portion that is continuously provided on the inner surface of the exhaust pipe and a part of the circumferential direction, and has a tapered portion that is inclined in the extending direction of the exhaust pipe and the cross-sectional area becomes smaller toward the downstream side of the exhaust pipe. It is characterized by that.

本発明により、圧力損失を抑制しながら、高い撹拌効果を有する、排気通路を提供できる。 INDUSTRIAL APPLICABILITY According to the present invention, it is possible to provide an exhaust passage having a high stirring effect while suppressing a pressure loss.

本実施形態に係る排気通路の一例を示す模式的な斜視図である。It is a schematic perspective view which shows an example of the exhaust passage which concerns on this embodiment. 突出部により排気が撹拌される機構を説明するための模式的な斜視図である。It is a schematic perspective view for demonstrating the mechanism that the exhaust gas is agitated by the protrusion. 排ガス流量の分布を示す図である。It is a figure which shows the distribution of the exhaust gas flow rate. 突出部の中心角の違いによる圧力損失とミキシング効果との関係を示すグラフである。It is a graph which shows the relationship between the pressure loss due to the difference in the central angle of the protrusion, and the mixing effect. 突出部の一例を示す模式的な、(A)正面図、(B)上面図、(C)側面図である。It is (A) front view, (B) top view, (C) side view which shows an example of the protrusion. 図5の例に示す突出部の模式的な斜視図である。It is a schematic perspective view of the protrusion shown in the example of FIG. 突出部の別の一例を示す斜視図である。It is a perspective view which shows another example of the protrusion. 突出部の別の一例を示す斜視図である。It is a perspective view which shows another example of the protrusion. 排気通路の別の一例を示す模式的な斜視図である。It is a schematic perspective view which shows another example of an exhaust passage.

以下、実施の形態を通じて本発明を説明するが、特許請求の範囲に係る発明を以下の実施形態に限定するものではない。また、説明を明確にするため、以下の記載及び図面は、適宜、簡略化されている。なお、本明細書においては、排気管の軸方向(延在方向)の下流向きにX軸をとり、X軸に垂直な面をYZ面(単に断面ともいう)とする。 Hereinafter, the present invention will be described through the embodiments, but the invention according to the claims is not limited to the following embodiments. Further, in order to clarify the explanation, the following description and drawings have been simplified as appropriate. In the present specification, the X-axis is taken in the downstream direction in the axial direction (extending direction) of the exhaust pipe, and the plane perpendicular to the X-axis is referred to as the YZ plane (also simply referred to as a cross section).

図1の例に示す排気通路10は、内燃機関用に好適に用いられる排気通路であって、排気管11(11A,11B)と、突出部20とを備えている。図5及び図6に示されるように、突出部20は、少なくとも排気管の延在方向に傾くテーパ部22を有し、排気管11と内接する内接部21を有していてもよい。前記テーパ部22は、排気管11の下流側ほど断面積が小さくなる形状を有している。ここでテーパ部の断面とは、排気管の軸に対して垂直な円弧状の断面をいい、テーパ部の断面積とは、円弧と、円弧の端点と排気管の中心とを結んだ線により構成される扇形の面積をいう。また当該扇形の中心角をθ(図5(A)参照)とする。本実施形態の排気通路は、圧力損失を抑制しながら、高い撹拌効果を有する。このことについて図2を参照して説明する。 The exhaust passage 10 shown in the example of FIG. 1 is an exhaust passage preferably used for an internal combustion engine, and includes an exhaust pipe 11 (11A, 11B) and a protruding portion 20. As shown in FIGS. 5 and 6, the protruding portion 20 may have at least a tapered portion 22 inclined in the extending direction of the exhaust pipe, and may have an inscribed portion 21 inscribed in the exhaust pipe 11. The tapered portion 22 has a shape in which the cross-sectional area becomes smaller toward the downstream side of the exhaust pipe 11. Here, the cross section of the tapered portion means an arc-shaped cross section perpendicular to the axis of the exhaust pipe, and the cross-sectional area of the tapered portion is a line connecting the arc, the end point of the arc, and the center of the exhaust pipe. The area of the fan shape that is composed. Further, the central angle of the sector is θ (see FIG. 5 (A)). The exhaust passage of the present embodiment has a high stirring effect while suppressing pressure loss. This will be described with reference to FIG.

図2は突出部により排ガスが撹拌される機構を説明するための模式的な斜視図である。図2中の(A)及び(B)は各々排気通路を通過する排ガスのXY断面を模式的に示すものである。
図2の例に示すように、排ガスは上流から下流に流れる際に、突出部20のテーパ部22を通過する(図2(A))。テーパ部22は下流側ほど断面積が小さくなる構造を有しているため、下流に進むにしたがってテーパ部22の気体がテーパ部外に押し出されて矢印に示す気流が発生する。この気流はテーパ部22全域で連続的に生じて旋回流となり、突出部通過後においても管内全体で排ガスの撹拌が進む(図2(B))。その結果、排ガスの面均一性向上し、センサによる測定精度が向上する。また、本実施形態の排気通路は、テーパ部においても比較的開口部が大きくまた、前述する旋回流が管内全体に広がるため、圧力損失の増加を抑制することができる。
図3は、突出部の有無による排ガス流量の分布の違いを示す図である。図3に示す通り、突出部有する本実施形態の排気通路では、排ガス流量の面均一性が向上している。特に、圧力損失の抑制効果に優れる点から、突出部の断面積を排気管の断面積の50%以下とすることが好ましい。
FIG. 2 is a schematic perspective view for explaining a mechanism in which the exhaust gas is agitated by the protruding portion. (A) and (B) in FIG. 2 schematically show an XY cross section of the exhaust gas passing through the exhaust passage, respectively.
As shown in the example of FIG. 2, the exhaust gas passes through the tapered portion 22 of the protruding portion 20 when flowing from the upstream to the downstream (FIG. 2 (A)). Since the tapered portion 22 has a structure in which the cross-sectional area becomes smaller toward the downstream side, the gas in the tapered portion 22 is pushed out of the tapered portion as it goes downstream, and the air flow indicated by the arrow is generated. This airflow is continuously generated over the entire tapered portion 22 to form a swirling flow, and the exhaust gas is agitated throughout the pipe even after passing through the protruding portion (FIG. 2B). As a result, the surface uniformity of the exhaust gas is improved, and the measurement accuracy by the sensor is improved. Further, the exhaust passage of the present embodiment has a relatively large opening even in the tapered portion, and the swirling flow described above spreads throughout the pipe, so that an increase in pressure loss can be suppressed.
FIG. 3 is a diagram showing the difference in the distribution of the exhaust gas flow rate depending on the presence or absence of the protrusion. As shown in FIG. 3, in the exhaust passage of the present embodiment having a protruding portion, the surface uniformity of the exhaust gas flow rate is improved. In particular, it is preferable that the cross-sectional area of the protruding portion is 50% or less of the cross-sectional area of the exhaust pipe from the viewpoint of excellent effect of suppressing pressure loss.

図5及び図6は、突出部の一例を示す模式的である。突出部20は、図5及び図6の例に示すように、下流側ほど断面積が小さくなるテーパ部22を有している。テーパ部22の形状は、下流側ほど断面積が小さくなる形状であれば特に限定されず、例えば、図6及び図7の例のように直線型であってもよく、図8のように曲線(半円型や、放物線型)であってもよい。また、テーパ部の先端は、図7の例のように先端まで直線的な形状であってもよく、図6のように先端を切断して閉じたたような台形状の形状であってもよく、図8の例のように開口していてもよい。いずれの形状であっても圧力損失を抑制しながら、高い撹拌効果を有する。突出部20は、排気管11と接続するための内接部21を有していてもよい。 5 and 6 are schematic showing an example of a protruding portion. As shown in the examples of FIGS. 5 and 6, the protruding portion 20 has a tapered portion 22 whose cross-sectional area becomes smaller toward the downstream side. The shape of the tapered portion 22 is not particularly limited as long as the cross-sectional area becomes smaller toward the downstream side. For example, it may be a linear shape as in the examples of FIGS. 6 and 7, and a curved line as shown in FIG. It may be (semi-circular type or parabolic type). Further, the tip of the tapered portion may have a linear shape up to the tip as shown in the example of FIG. 7, or may have a trapezoidal shape such that the tip is cut and closed as shown in FIG. Often, it may be open as in the example of FIG. Any shape has a high stirring effect while suppressing pressure loss. The protruding portion 20 may have an inscribed portion 21 for connecting to the exhaust pipe 11.

次に、突出部をX軸方向に見た時の正面図(図5(A))の中心角θと撹拌効果の関係を説明する。図4は、突出部の中心角の違いによる圧力損失とミキシング効果との関係を示すグラフである。
図4に示されるように、中心角θが大きくなるほどミキシング効果が向上する一方、圧力損失が増大する傾向がみられる。中心角θが180度を超えると、ミキシング効果の向上に対して圧力損失の上昇が顕著になっている。一方、中心角が90度未満の範囲では、十分なミキシング効果が得られない場合がある。本実施形態においては、ミキシング効果と圧力損失の抑制とのバランスの観点から、中心角θが90〜180度の範囲内であることが特に好ましい。
Next, the relationship between the central angle θ and the stirring effect in the front view (FIG. 5 (A)) when the protruding portion is viewed in the X-axis direction will be described. FIG. 4 is a graph showing the relationship between the pressure loss due to the difference in the central angle of the protruding portion and the mixing effect.
As shown in FIG. 4, as the central angle θ becomes larger, the mixing effect is improved, but the pressure loss tends to increase. When the central angle θ exceeds 180 degrees, the increase in pressure loss becomes remarkable with respect to the improvement of the mixing effect. On the other hand, if the central angle is less than 90 degrees, a sufficient mixing effect may not be obtained. In the present embodiment, it is particularly preferable that the central angle θ is in the range of 90 to 180 degrees from the viewpoint of the balance between the mixing effect and the suppression of the pressure loss.

本実施形態において、排気管11内に突出部20を設ける方法は特に限定されない。例えば図1の例のように、上流側の排気管11Aと下流側の排気管11Bとの間に、突出部20が設けられた接続具23を用いて突出部20が設けられていてもよい。また、排気管11に突出部20を溶接してもよい。 In the present embodiment, the method of providing the protruding portion 20 in the exhaust pipe 11 is not particularly limited. For example, as in the example of FIG. 1, the protruding portion 20 may be provided between the exhaust pipe 11A on the upstream side and the exhaust pipe 11B on the downstream side by using a connector 23 provided with the protruding portion 20. .. Further, the protruding portion 20 may be welded to the exhaust pipe 11.

また、図9の例に示されるように、排気管11は、突出部20の下流側にセンサ30を取り付けるためのセンサ取付部31を有していてもよい。センサ取付部31の形状は、センサ30に応じて適宜調整すればよい。センサ30は、排気管内の酸素濃度を測定可能なセンサが好ましく、例えば、A/Fセンサ、Oセンサなどが挙げられる。 Further, as shown in the example of FIG. 9, the exhaust pipe 11 may have a sensor mounting portion 31 for mounting the sensor 30 on the downstream side of the protruding portion 20. The shape of the sensor mounting portion 31 may be appropriately adjusted according to the sensor 30. The sensor 30 is preferably a sensor capable of measuring the oxygen concentration in the exhaust pipe, and examples thereof include an A / F sensor and an O 2 sensor.

上記本実施形態の排気通路は、上述のとおり圧力損失を抑制しながら高い撹拌効果を有するものであり、例えば内燃機関の排気通路として好適に用いることができる。本実施形態で用いる突出部は、1ピースで比較的単純な構造であるため、信頼性が高く、また製造コストを抑えることもできる。 As described above, the exhaust passage of the present embodiment has a high stirring effect while suppressing pressure loss, and can be suitably used as, for example, an exhaust passage of an internal combustion engine. Since the protruding portion used in the present embodiment has a relatively simple structure with one piece, it is highly reliable and the manufacturing cost can be suppressed.

10 排気通路、 11(11A,11B) 排気管、 20 突出部、 21 内接部、 22 テーパ部、 23 接続具、 30 センサ、 31 センサ取付部。 10 Exhaust passage, 11 (11A, 11B) Exhaust pipe, 20 Protruding part, 21 Inscribed part, 22 Tapered part, 23 Connector, 30 Sensor, 31 Sensor mounting part.

Claims (1)

排気管と、
前記排気管の内面と円周方向の一部の範囲で連続して設けられ、排気管の延在方向に傾き排気管の下流側ほど断面積が小さくなるテーパ部を有する突出部と、を備える、
排気通路。
Exhaust pipe and
It is provided with a protruding portion that is continuously provided on the inner surface of the exhaust pipe and a part of the circumferential direction, and has a tapered portion that is inclined in the extending direction of the exhaust pipe and the cross-sectional area becomes smaller toward the downstream side of the exhaust pipe. ,
Exhaust passage.
JP2019160397A 2019-09-03 2019-09-03 exhaust passage Active JP7351148B2 (en)

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US11585240B2 (en) 2021-01-19 2023-02-21 Toyota Jidosha Kabushiki Kaisha Exhaust passage

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2003507688A (en) * 1999-08-17 2003-02-25 エミテック ゲゼルシヤフト フユア エミツシオンス テクノロギー ミツト ベシユレンクテル ハフツング Mixing element for fluid flowing in pipe
JP2006144576A (en) * 2004-11-16 2006-06-08 Denso Corp Nitrogen oxide cleaning device
JP2006307718A (en) * 2005-04-27 2006-11-09 Calsonic Kansei Corp Drainage structure of muffler
JP2014531554A (en) * 2011-09-08 2014-11-27 テンネコ・オートモティブ・オペレーティング・カンパニー・インコーポレイテッド Pre-injection exhaust gas flow changer
JP2015010508A (en) * 2013-06-27 2015-01-19 株式会社日本自動車部品総合研究所 Exhaust purification device for internal combustion engine
JP2018087504A (en) * 2016-11-28 2018-06-07 トヨタ自動車株式会社 Muffler

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2003507688A (en) * 1999-08-17 2003-02-25 エミテック ゲゼルシヤフト フユア エミツシオンス テクノロギー ミツト ベシユレンクテル ハフツング Mixing element for fluid flowing in pipe
JP2006144576A (en) * 2004-11-16 2006-06-08 Denso Corp Nitrogen oxide cleaning device
JP2006307718A (en) * 2005-04-27 2006-11-09 Calsonic Kansei Corp Drainage structure of muffler
JP2014531554A (en) * 2011-09-08 2014-11-27 テンネコ・オートモティブ・オペレーティング・カンパニー・インコーポレイテッド Pre-injection exhaust gas flow changer
JP2015010508A (en) * 2013-06-27 2015-01-19 株式会社日本自動車部品総合研究所 Exhaust purification device for internal combustion engine
JP2018087504A (en) * 2016-11-28 2018-06-07 トヨタ自動車株式会社 Muffler

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US11585240B2 (en) 2021-01-19 2023-02-21 Toyota Jidosha Kabushiki Kaisha Exhaust passage

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