JP2009185653A - Intake device for internal combustion engine - Google Patents

Intake device for internal combustion engine Download PDF

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JP2009185653A
JP2009185653A JP2008024926A JP2008024926A JP2009185653A JP 2009185653 A JP2009185653 A JP 2009185653A JP 2008024926 A JP2008024926 A JP 2008024926A JP 2008024926 A JP2008024926 A JP 2008024926A JP 2009185653 A JP2009185653 A JP 2009185653A
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intake pipe
intake
passage area
flow passage
flow
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JP4951544B2 (en
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Takeshi Wakamatsu
健 若松
Takahiro Taira
貴浩 平
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Honda Motor Co Ltd
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Honda Motor Co Ltd
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  • Control Of Throttle Valves Provided In The Intake System Or In The Exhaust System (AREA)

Abstract

<P>PROBLEM TO BE SOLVED: To provide an intake device for an internal combustion engine capable of performing both the inhibition of air flow noise and the homogeneous dispersion of addition gas. <P>SOLUTION: An induction conduit 2 includes a first induction conduit 4 for supporting a valve stem 3a of a butterfly valve 3; a second induction conduit 5 having a flow passage area larger than that of the first induction conduit 4, and continuously arranged at the downstream side of the first induction conduit 4; and a third induction conduit 6 having a flow passage area smaller than that of the second induction conduit 5, and continuously arranged at the downstream side of the second induction conduit 5. The second induction conduit 5 includes a flow passage area enlarged portion 5a with the flow passage area on the one half 3b side of the butterfly valve 3 larger than the flow passage area on the other half 3c side, and a flow passage area gradually narrowed portion 5b continuously arranged at the downstream side of the flow passage area enlarged portion 5a, for making the flow passage area of the second induction conduit 5 gradually become closer to the flow passage area of the third induction conduit 6. An addition gas introducing port 8 is provided in the vicinity of the boundary of the second and third induction conduits 5, 6 for introducing the addition gas into the induction conduit 2. <P>COPYRIGHT: (C)2009,JPO&INPIT

Description

本発明は、内燃機関に空気を供給する吸気管内にバタフライバルブを配設してなる内燃機関の吸気装置に関する。   The present invention relates to an intake device for an internal combustion engine in which a butterfly valve is disposed in an intake pipe that supplies air to the internal combustion engine.

この種の吸気装置においては、全閉状態のバタフライバルブを急激に開くと、バタフライバルブの両端を通過した吸気流がバタフライバルブの下流側で合流し、耳障りな気流音が発生する。特に、吸気管が樹脂製であると、吸気管の反響により気流音が一層大きくなる。そこで、バタフライバルブの下流側の流路面積を拡大することで、吸気流が合流する際の圧力エネルギーを逃がし、気流音の発生を抑制している(特許文献1参照)。
特開平10−121994号公報(段落0029〜0031、図2)
In this type of intake device, when the fully closed butterfly valve is suddenly opened, the intake air flow that has passed through both ends of the butterfly valve merges on the downstream side of the butterfly valve, and an annoying airflow sound is generated. In particular, if the intake pipe is made of resin, the sound of the airflow is further increased due to the reflection of the intake pipe. Therefore, by expanding the flow path area on the downstream side of the butterfly valve, the pressure energy when the intake air flows join is released, and the generation of airflow noise is suppressed (see Patent Document 1).
Japanese Patent Laid-Open No. 10-121994 (paragraphs 0029 to 0031, FIG. 2)

ところで、内燃機関の吸気管にはEGRガスやブローバイガスなどの付加ガスを導入しているが、特許文献1に示すような流路面積拡大部を設けると、付加ガス導入口の設置箇所の選定が難しくなる。すなわち、流路面積拡大部が設けられていない場合、バタフライバルブの直ぐ下流側に吸気流の渦が生じるので、従来はそこに付加ガス導入口を設置して吸気管内に付加ガスを均一拡散させていた。しかし、特許文献1に示すような流路拡大部を設けると、吸気流の渦が生じにくくなるため、バタフライバルブの近くに付加ガス導入口を設けると、バタフライバルブの両端を通過した、速度の異なる吸気流のいずれか一方に付加ガスが乗って流れ、吸気管内に均一拡散しなくなる虞がある。一方、付加ガス導入口をバタフライバルブから離し過ぎると、その位置では吸気流が整流されているため、付加ガスが導入口側に偏って拡散し易くなる。要するに、特許文献1の技術を採用すると、気流音の発生は抑制できるが、吸気中への付加ガスの均一拡散が困難になる。特に、多気筒の内燃機関では、気筒毎に付加ガスの濃度が異なってしまい、燃焼のばらつきを生じるという問題を生じる。   By the way, additional gas such as EGR gas or blow-by gas is introduced into the intake pipe of the internal combustion engine. However, when a flow passage area enlarged portion as shown in Patent Document 1 is provided, selection of the installation location of the additional gas introduction port is selected. Becomes difficult. That is, when the flow passage area enlargement section is not provided, an vortex of the intake flow is generated immediately downstream of the butterfly valve. Conventionally, an additional gas introduction port is provided there to uniformly diffuse the additional gas in the intake pipe. It was. However, if the flow passage enlargement portion as shown in Patent Document 1 is provided, the vortex of the intake air flow is less likely to be generated. Therefore, if the additional gas inlet is provided near the butterfly valve, There is a possibility that the additional gas rides on one of the different intake flows and does not diffuse uniformly in the intake pipe. On the other hand, if the additional gas inlet is too far away from the butterfly valve, the intake flow is rectified at that position, so that the additional gas tends to be biased and diffused toward the inlet. In short, when the technique of Patent Document 1 is adopted, the generation of airflow noise can be suppressed, but it becomes difficult to uniformly diffuse additional gas into the intake air. In particular, in a multi-cylinder internal combustion engine, the concentration of the additional gas differs from cylinder to cylinder, causing a problem of variation in combustion.

本発明は、このような事情に鑑み、気流音の発生抑制と付加ガスの均一拡散の両立が可能な内燃機関の吸気装置を提供することを目的とする。   In view of such circumstances, an object of the present invention is to provide an intake device for an internal combustion engine capable of both suppressing generation of airflow noise and uniform diffusion of additional gas.

前記課題を解決するための本発明は、内燃機関に空気を供給する吸気管内にバタフライバルブを配設してなる内燃機関の吸気装置において、前記バタフライバルブの弁軸を支持する第1吸気管部と、該第1吸気管部の流路面積よりも大きな流路面積を有し、前記第1吸気管部の下流に連設した第2吸気管部と、該第2吸気管部の流路面積よりも小さな流路面積を有し、前記第2吸気管部の下流に連設した第3吸気管部とで前記吸気管を構成するとともに、前記第2吸気管部には、前記バタフライバルブの一方の半体側の流路面積を他方の半体側の流路面積よりも大きくする流路面積拡大部分と、前記第2吸気管部の流路面積を前記第3吸気管部の流路面積に徐々に近づけるべく前記流路面積拡大部分の下流に連設した流路面積漸減部分とを設け、さらに、前記第2及び第3吸気管部の境界近傍には、前記吸気管内に付加ガスを導入する付加ガス導入口を設けたことを特徴とする。   In order to solve the above-mentioned problems, the present invention provides an intake device for an internal combustion engine in which a butterfly valve is disposed in an intake pipe that supplies air to the internal combustion engine, and a first intake pipe portion that supports a valve shaft of the butterfly valve. A second intake pipe portion having a flow passage area larger than the flow passage area of the first intake pipe portion and continuously provided downstream of the first intake pipe portion, and a flow path of the second intake pipe portion The intake pipe is configured with a third intake pipe portion having a flow path area smaller than the area and continuously provided downstream of the second intake pipe portion, and the second intake pipe portion includes the butterfly valve A channel area enlarged portion in which the channel area on one half side is larger than the channel area on the other half side, and the channel area of the second intake pipe section is the channel area of the third intake pipe section. In order to gradually approach the channel area, a channel area gradually decreasing portion connected downstream of the channel area expanding portion is provided. Further, wherein the vicinity of the boundary between the second and third suction pipe portion, characterized in that a additional gas inlet for introducing an additional gas into the intake pipe.

かかる構成によれば、バタフライバルブの一方の半体側の通路を通過した吸気は、第2吸気管部の流路面積拡大部分に流入して流速を低下させる一方、他方の半体側の通路を通過した吸気は、第2吸気管部の内面に沿って流れるので、前者の吸気流は後者の吸気流に較べて流速が小さくなる。このため、2つの吸気流が吸気管内の軸方向にオフセットした位置で合流するので、吸気流の直接衝突が回避され、気流音の発生が抑制される。一方、第2及び第3吸気管部の境界近傍では、流速の異なる吸気流が合流して強い乱流を形成しているので、付加ガスは強い乱流に乗って吸気管内に拡散する。   According to this configuration, the intake air that has passed through the passage on one half side of the butterfly valve flows into the flow passage area enlarged portion of the second intake pipe portion to reduce the flow velocity, while passing through the other half side passage. Since the intake air flows along the inner surface of the second intake pipe portion, the flow rate of the former intake flow is smaller than that of the latter intake flow. For this reason, since two intake air flows merge at a position offset in the axial direction in the intake pipe, a direct collision of the intake air flow is avoided and generation of airflow noise is suppressed. On the other hand, in the vicinity of the boundary between the second and third intake pipe portions, the intake flows having different flow velocities merge to form a strong turbulent flow, so that the additional gas rides on the strong turbulent flow and diffuses into the intake pipe.

前記流路面積漸減部分と同一の吸気管周上にある領域または該領域の下流で前記第2及び第3吸気管部の境界近傍にある領域に前記付加ガス導入口を配置することが好ましい。   It is preferable that the additional gas inlet is arranged in a region on the same intake pipe circumference as the flow path area gradually decreasing portion or in a region near the boundary between the second and third intake pipe portions downstream of the region.

かかる構成によれば、流路面積拡大部分を通過することで流速が小さくなった吸気流は、流路面積漸減部分に案内されるため、第2吸気管部と第3吸気管部との境界よりも上流側で第2吸気管部の軸芯に向かう流れを形成する。一方、流路面積拡大部分を通過しなかった吸気流は、該流路面積拡大部分を通過した吸気流よりも流速が大であるため、該流路面積拡大部分を通過した吸気流よりも下流側、換言すれば、第2吸気管部と第3吸気管部との境界よりも下流側で、第3吸気管部の軸芯に向かう流れを形成するようになる。このため、2つの吸気流が第2吸気管部と第3吸気管部との境界付近において合流することとなり、流路面積漸減部分と同一の吸気管周上にある領域で強い乱流が生じるので、この領域若しくはそのやや下流側に付加ガス導入口を配置することで、付加ガスをより均一に拡散させることができる。   According to such a configuration, since the intake flow whose flow velocity has been reduced by passing through the flow passage area enlarged portion is guided to the flow passage area gradually decreasing portion, the boundary between the second intake pipe portion and the third intake pipe portion. A flow toward the axial center of the second intake pipe portion is formed on the upstream side. On the other hand, the flow rate of the intake air flow that has not passed through the enlarged flow channel area is higher than the flow rate of the intake air flow that has passed through the enlarged flow channel area portion. On the other hand, in other words, a flow toward the axial center of the third intake pipe portion is formed on the downstream side of the boundary between the second intake pipe portion and the third intake pipe portion. For this reason, the two intake flows merge near the boundary between the second intake pipe portion and the third intake pipe portion, and a strong turbulent flow is generated in a region on the same intake pipe circumference as the flow passage area gradually decreasing portion. Therefore, the additional gas can be diffused more uniformly by arranging the additional gas introduction port in this region or slightly downstream thereof.

前記流路面積拡大部分は、前記バタフライバルブの上流側に傾倒する半体側の流路面積を拡大させるように配置してあることが好ましい。   It is preferable that the flow path area enlarged portion is arranged so as to increase the flow area on the half body side that is inclined to the upstream side of the butterfly valve.

かかる構成によれば、バタフライバルブによる流量調整が徐々に行え、低流量の吸気制御が可能になる。   According to such a configuration, the flow rate can be gradually adjusted by the butterfly valve, and the intake control with a low flow rate can be performed.

前記バタフライバルブの一方の半体側にある流路と、他方の半体側にある流路との境界近傍に前記付加ガス導入口を配置し、該付加ガス導入口から前記バタフライバルブの弁軸と略平行な方向に前記付加ガスを吸気管内に導入することが好ましい。   The additional gas introduction port is disposed in the vicinity of the boundary between the flow path on one half side of the butterfly valve and the flow path on the other half side, and the valve shaft of the butterfly valve substantially extends from the additional gas introduction port. It is preferable to introduce the additional gas into the intake pipe in a parallel direction.

かかる構成によれば、バタフライバルブの一方の半体側にある流路と、他方の半体側にある流路のいずれか一方に偏って付加ガスが拡散する虞がなくなり、拡散効果がさらに良くなる。   According to such a configuration, there is no possibility that the additional gas is diffused by being biased to one of the flow path on one half side of the butterfly valve and the flow path on the other half side, and the diffusion effect is further improved.

前記第1吸気管部をスロットルボディで構成するとともに、前記第2及び第3吸気管部を吸気マニホールドで構成し、該吸気マニホールドの前記スロットルボディに対する接合面に前記流路面積拡大部分を隣接させて形成することが好ましい。   The first intake pipe portion is formed of a throttle body, the second and third intake pipe portions are formed of an intake manifold, and the flow passage area enlarged portion is adjacent to a joint surface of the intake manifold to the throttle body. It is preferable to form them.

かかる構成によれば、第2及び第3吸気管部の成形に際し、離型方向の制約が生じなくなり、成形コストの上昇抑制が可能になるばかりでなく、流路面積拡大部分の容積拡大が容易になり、気流音の低減にも役立つ。   According to such a configuration, when the second and third intake pipe portions are molded, there is no restriction in the mold release direction, and it is possible not only to suppress an increase in molding cost, but also to easily increase the volume of the channel area expansion portion. And helps reduce airflow noise.

前記流路面積拡大部分には、その内部に収まって吸気管軸芯に沿って延びるリブを設けてあることが好ましい。   It is preferable that the flow passage area enlarged portion is provided with a rib that extends inside the intake pipe shaft core.

かかる構成によれば、吸気管の剛性が向上するので、気流音が吸気管内で反響しにくくなり、気流音をさらに小さくできる。さらに、リブは流路面積拡大部分内に収容されるので、第1吸気管部または第3吸気管部の流路に対してリブが突出することがなく、第1吸気管部及び第3吸気管部の流路面積低下(換言すれば内燃機関の体積効率低下)を回避する。しかも、リブは吸気管軸芯に沿って延びているので、吸気抵抗の増大を抑制できる。   According to this configuration, since the rigidity of the intake pipe is improved, the airflow sound is less likely to be reflected in the intake pipe, and the airflow sound can be further reduced. Further, since the rib is accommodated in the flow path area enlarged portion, the rib does not protrude from the flow path of the first intake pipe portion or the third intake pipe portion, and the first intake pipe portion and the third intake air are not projected. A reduction in the flow area of the pipe portion (in other words, a reduction in volumetric efficiency of the internal combustion engine) is avoided. Moreover, since the rib extends along the intake pipe axis, an increase in intake resistance can be suppressed.

前記リブは、その高さと幅のうちの少なくとも1つが下流側に向かって大きくなるように形成してあることが好ましい。   The rib is preferably formed such that at least one of its height and width increases toward the downstream side.

かかる構成によれば、第2吸気管部の流路面積が吸気管軸芯方向に対して緩やかに変化し、第2吸気管部の流路面積が第3吸気管部の流路面積に徐々に近づくので、吸気抵抗の抑制効果がさらに高くなる。   According to this configuration, the flow passage area of the second intake pipe portion changes gradually with respect to the intake pipe axial center direction, and the flow passage area of the second intake pipe portion gradually increases to the flow passage area of the third intake pipe portion. Therefore, the effect of suppressing the intake resistance is further increased.

本発明によれば、バタフライバルブの両方の半体を通過した吸気が吸気管内の軸方向にオフセットした位置で合流するので、吸気の直接衝突による気流音の発生を抑制することができる。また、第2及び第3吸気管部の境界近傍では、流速の異なる吸気流が合流し、強い乱流が形成されているので、この乱流に付加ガスを乗せて吸気管内に均一拡散させることができる。   According to the present invention, since the intake air that has passed through both halves of the butterfly valve merges at a position offset in the axial direction in the intake pipe, the generation of airflow noise due to the direct collision of the intake air can be suppressed. Further, in the vicinity of the boundary between the second and third intake pipe portions, intake flows having different flow velocities merge to form a strong turbulent flow, so that additional gas is placed on the turbulent flow and uniformly diffused in the intake pipe. Can do.

以下、本発明の実施形態を添付図面を参照しながら詳細に説明する。
図1は本発明の内燃機関の吸気装置を示す図で、図2のA−A線断面図である。図2は図1の吸気マニホールドを開口端から見た図である。
Hereinafter, embodiments of the present invention will be described in detail with reference to the accompanying drawings.
1 is a view showing an intake device for an internal combustion engine according to the present invention, and is a cross-sectional view taken along line AA of FIG. FIG. 2 is a view of the intake manifold of FIG. 1 as viewed from the open end.

この吸気装置1は、吸気管2の内部にバタフライバルブ3を配設し、その開度を調節して内燃機関に供給する空気量を制御するものである。吸気管2は、バタフライバルブ3を内蔵したスロットルボディで形成した第1吸気管部4と、第1吸気管部4と連通する樹脂製の吸気マニホールドで形成した第2及び第3吸気管部5,6とで構成してある。各吸気管部4,5,6は断面円形の流路を備え、その軸芯CLを一致させて連設してある。第1吸気管部4の流路面積は第3吸気管部6の流路面積と略等しくしてある。ただし、第2吸気管部5の流路面積は、流路面積拡大部分5aと流路面積漸減部分5bを設けた分だけ、第1及び第3吸気管部4,6の流路面積よりも大きくなっている。第1吸気管部4にはバタフライバルブ3の弁軸3aを回動自在に支持してある。バタフライバルブ3は、その先端部が開弁時に第2吸気管部5内に進入するように配置してある。なお、閉弁状態のバタフライバルブ3は図1に2点鎖線で示してある。   This intake device 1 is provided with a butterfly valve 3 inside an intake pipe 2 and controls the amount of air supplied to the internal combustion engine by adjusting the opening degree. The intake pipe 2 includes a first intake pipe portion 4 formed of a throttle body incorporating a butterfly valve 3 and second and third intake pipe portions 5 formed of a resin intake manifold communicating with the first intake pipe portion 4. , 6. Each of the intake pipe portions 4, 5, and 6 has a flow path having a circular cross section, and the axial centers CL thereof are aligned to be connected. The flow passage area of the first intake pipe portion 4 is substantially equal to the flow passage area of the third intake pipe portion 6. However, the flow passage area of the second intake pipe portion 5 is larger than the flow passage areas of the first and third intake pipe portions 4 and 6 by the provision of the flow passage area enlarged portion 5a and the flow passage area gradually decreasing portion 5b. It is getting bigger. A valve shaft 3a of the butterfly valve 3 is rotatably supported on the first intake pipe portion 4. The butterfly valve 3 is arranged so that its tip end enters the second intake pipe 5 when the valve is opened. Note that the butterfly valve 3 in the closed state is indicated by a two-dot chain line in FIG.

第2吸気管部5は、バタフライバルブ3を構成する2つの半体3b,3cのうち、上流側に傾倒する第1半体3b側の流路20の面積を、下流側に傾倒する第2半体3c側の流路30の面積よりも大きくする流路面積拡大部分5aを備えている。なお、第1及び第2半体3b,3c側の流路20,30とは、バタフライバルブ3の弁軸3aを吸気管軸芯CLに沿って延長した面で区画される吸気管2の内部空間をいう。流路面積拡大部分5aは、図1に示す断面(バタフライバルブ3の弁軸3aと直交する吸気管軸芯CLを含む断面)において、第2吸気管部5の周壁の一部を半径方向外方へ膨出させて形成してある。なお、流路面積拡大部分5aは、第2吸気管部5の開口端から見て略半円形に形成してある(図2参照)。   The second intake pipe unit 5 tilts the area of the flow path 20 on the first half 3b side that tilts upstream of the two halves 3b and 3c constituting the butterfly valve 3 to the downstream side. A channel area enlarged portion 5a that is larger than the area of the channel 30 on the half body 3c side is provided. The flow paths 20 and 30 on the first and second half bodies 3b and 3c side are the insides of the intake pipe 2 defined by the surface extending the valve shaft 3a of the butterfly valve 3 along the intake pipe axis CL. Space. In the cross section shown in FIG. 1 (the cross section including the intake pipe axis CL that is orthogonal to the valve shaft 3a of the butterfly valve 3), the flow passage area enlarged portion 5a is a part of the peripheral wall of the second intake pipe portion 5 outside the radial direction. It is formed to bulge out. The channel area enlarged portion 5a is formed in a substantially semicircular shape when viewed from the opening end of the second intake pipe portion 5 (see FIG. 2).

流路面積拡大部分5aの下流側には、第2吸気管部5の流路面積を第3吸気管部6の流路面積と等しくする流路面積漸減部分5bを連設してある。つまり、この流路面積漸減部分5bは、その流路面積が下流側へ向かって徐々に小さくなるように形成してある。さらに、流路面積拡大部分5aと流路面積漸減部分5bには、吸気管軸芯CLに沿って延びるリブ7を一対設けてある。これらのリブ7,7は、その上面を第1及び第3吸気管部4,6の内面4a,6aと面一にしてある。なお、本実施形態では、リブ7,7は図2のA−A線に関して対称に配置してある。   A flow passage area gradually decreasing portion 5 b is provided downstream from the flow passage area enlarged portion 5 a so that the flow passage area of the second intake pipe portion 5 is equal to the flow passage area of the third intake pipe portion 6. That is, the channel area gradually decreasing portion 5b is formed such that the channel area gradually decreases toward the downstream side. Further, a pair of ribs 7 extending along the intake pipe axis CL are provided in the flow channel area enlarged portion 5a and the flow channel area gradually decreasing portion 5b. The upper surfaces of the ribs 7 and 7 are flush with the inner surfaces 4 a and 6 a of the first and third intake pipe portions 4 and 6. In the present embodiment, the ribs 7 are arranged symmetrically with respect to the line AA in FIG.

吸気管2には、付加ガス(EGRガスやブローバイガス、蒸発燃料など)を内部に導入するための付加ガス導入口8がバタフライバルブ3の下流側に設けてある。この付加ガス導入口8は、流路面積漸減部分5bと同一の吸気管周上にある領域であって、第1及び第2半体3b,3c側の流路20,30の境界に配置してある。詳しくは、付加ガス導入口8を第2及び第3吸気管部5,6の境界からやや上流側に寄せて配置してある。さらに、付加ガス導入口8からバタフライバルブ3の弁軸3aと略平行な方向に付加ガスを吸気管2内に導入している。なお、吸気マニホールド9には、付加ガス導入口8に連なるホース接続管10を設けてある(図2参照)。   The intake pipe 2 is provided with an additional gas introduction port 8 for introducing additional gas (EGR gas, blow-by gas, evaporated fuel, etc.) into the downstream side of the butterfly valve 3. This additional gas inlet 8 is a region on the same intake pipe circumference as the flow passage area gradually decreasing portion 5b, and is disposed at the boundary between the flow passages 20 and 30 on the first and second half bodies 3b and 3c side. It is. Specifically, the additional gas introduction port 8 is disposed slightly upstream from the boundary between the second and third intake pipe portions 5 and 6. Further, additional gas is introduced into the intake pipe 2 from the additional gas introduction port 8 in a direction substantially parallel to the valve shaft 3 a of the butterfly valve 3. The intake manifold 9 is provided with a hose connection pipe 10 connected to the additional gas introduction port 8 (see FIG. 2).

第1及び第2吸気管部4,5の開口端にはフランジ11,12が設けてあり、これらフランジ11,12の間にシール材13を介装して第1及び第2吸気管部4,5を互いに連結してある。これにより、第2吸気管部5の流路面積拡大部分5aが第1吸気管部4のフランジ11を隣接して不連続な段差を形成している。   Flange 11, 12 is provided at the open ends of the first and second intake pipe portions 4, 5, and the first and second intake pipe portions 4 are interposed between the flanges 11, 12 with a sealing material 13 interposed therebetween. , 5 are connected to each other. Thereby, the flow passage area enlarged portion 5 a of the second intake pipe portion 5 forms a discontinuous step adjacent to the flange 11 of the first intake pipe portion 4.

この吸気装置1では、バタフライバルブ3の上流側に傾倒する第1半体3b側の通路aを通過した吸気は、第2吸気管部5の流路面積拡大部分5aに流入して流速を低下させる一方、他方の半体3c側の通路bを通過した吸気は、第2吸気管部の内面に沿って流れるので、前者の吸気流Aは後者の吸気流Bに較べて流速が小さくなる。その後、2つの吸気流A,Bは第2吸気管部5の中央に向かって湾曲するが、流速の小さい吸気流Aは、流速の大きい吸気流Bに較べて湾曲度が大きくなるので、2つの吸気流A,Bが吸気管2内の軸方向にオフセットした位置で合流する。つまり、2つの吸気流A,Bの直接衝突が回避され、吸気A,Bの直接衝突による気流音の発生が抑制される。この結果、全閉状態のバタフライバルブ3を急激に開いても、従来のように大きな気流音は生じなくなる。   In the intake device 1, the intake air that has passed through the passage a on the first half 3 b side that is inclined to the upstream side of the butterfly valve 3 flows into the flow passage area enlarged portion 5 a of the second intake pipe portion 5 to reduce the flow velocity. On the other hand, since the intake air that has passed through the passage b on the other half 3c side flows along the inner surface of the second intake pipe section, the flow rate of the former intake air flow A is smaller than that of the latter intake air flow B. Thereafter, the two intake flows A and B are curved toward the center of the second intake pipe section 5, but the intake flow A having a low flow velocity has a higher degree of curvature than the intake flow B having a high flow velocity. The two intake flows A and B merge at a position offset in the axial direction in the intake pipe 2. That is, the direct collision of the two intake air flows A and B is avoided, and the generation of airflow noise due to the direct collision of the intake air A and B is suppressed. As a result, even if the butterfly valve 3 in the fully closed state is suddenly opened, no loud airflow noise is generated as in the conventional case.

ところで、流路面積拡大部分5aを通過することで流速が小さくなった吸気流Aは、流路面積漸減部分5bに案内されるため、第2吸気管部5と第3吸気管部6との境界よりも上流側で第2吸気管部5の軸芯CLに向かう流れを形成する。一方、流路面積拡大部分5aを通過しなかった吸気流Bは、流路面積拡大部分5aを通過した吸気流Aよりも流速が大であるため、流路面積拡大部分5aを通過した吸気流よりも下流側、換言すれば、第2吸気管部5と第3吸気管部6との境界よりも下流側で、第3吸気管部6の軸芯CLに向かう流れを形成するようになる。このため、2つの吸気流A,Bが第2吸気管部5と第3吸気管部6との境界付近において合流することとなり、流路面積漸減部分5bと同一の吸気管周上にある領域で強い乱流が生じるので、この領域若しくはそのやや下流側に付加ガス導入口8を配置することで、付加ガスを均一に拡散させることができる。要するに、吸気管2内に付加ガスを均一拡散させるためには、付加ガス導入口8をこのように配置するのが最も好ましい。ただし、付加ガスは乱流に乗って吸気管2内に拡散するので、第2及び第3吸気管部5,6の境界から上下流側にある程度離れた位置に付加ガス導入口8を配置しても、十分な拡散効果は期待できる。   By the way, the intake air flow A whose flow velocity has been reduced by passing through the flow passage area enlarged portion 5a is guided to the flow passage area gradually decreasing portion 5b, so that the second intake pipe portion 5 and the third intake pipe portion 6 A flow toward the axis CL of the second intake pipe portion 5 is formed upstream of the boundary. On the other hand, since the intake air flow B that has not passed through the flow passage area enlarged portion 5a has a flow velocity larger than that of the intake air flow A that has passed through the flow passage area enlarged portion 5a, the intake air flow that has passed through the flow passage area enlarged portion 5a. The flow toward the axial center CL of the third intake pipe portion 6 is formed further downstream than the boundary between the second intake pipe portion 5 and the third intake pipe portion 6. . For this reason, the two intake flows A and B are merged in the vicinity of the boundary between the second intake pipe portion 5 and the third intake pipe portion 6, and the region on the same intake pipe circumference as the flow passage area gradually decreasing portion 5b. Since a strong turbulent flow is generated at this point, the additional gas can be uniformly diffused by arranging the additional gas inlet 8 in this region or slightly downstream thereof. In short, in order to uniformly diffuse the additional gas into the intake pipe 2, it is most preferable to arrange the additional gas inlet 8 in this way. However, since the additional gas rides on the turbulent flow and diffuses into the intake pipe 2, the additional gas inlet 8 is arranged at a certain distance from the boundary between the second and third intake pipe portions 5 and 6 to the upstream and downstream sides. However, a sufficient diffusion effect can be expected.

さらに、第1及び第2半体3b,3c側の流路20,30の境界に付加ガス導入口8を配置してあるので、第1及び第2半体3b,3c側の流路20,30のいずれか一方に偏って付加ガスが拡散する虞がなくなり、拡散効果が良くなる。また、付加ガス導入口8からバタフライバルブ3の弁軸3aと略平行な方向に付加ガスを吸気管2内に導入しているので、つまり、付加ガス導入口8から付加ガスを吸気管2の中心に向かって流出させているので、付加ガスの偏りがなくなり、拡散効果がさらに良くなる。なお、付加ガス導入口8は流路20,30の境界近傍に配置してあれば、その境界から多少離れていても差し支えない。   Further, since the additional gas introduction port 8 is arranged at the boundary between the flow paths 20 and 30 on the first and second half bodies 3b and 3c, the flow paths 20 and 30 on the first and second half bodies 3b and 3c side are arranged. There is no risk of the additional gas diffusing to be biased to any one of 30 and the diffusion effect is improved. Further, since the additional gas is introduced into the intake pipe 2 from the additional gas introduction port 8 in a direction substantially parallel to the valve shaft 3 a of the butterfly valve 3, that is, the additional gas is introduced into the intake pipe 2 from the additional gas introduction port 8. Since it is made to flow toward the center, the bias of the additional gas is eliminated and the diffusion effect is further improved. As long as the additional gas inlet 8 is disposed in the vicinity of the boundary between the flow paths 20 and 30, it may be slightly separated from the boundary.

ところで、バタフライバルブ3の上流側に傾倒する半体3b側の流路20の面積を拡大させるように流路面積拡大部分5aを配置してあるので、バタフライバルブ3による流量調整が徐々に行え、低流量の吸気制御(アイドル制御など)が可能になる。仮に、バタフライバルブ3の下流側に傾倒する半体3c側の流路30の面積を拡大させるように流路面積拡大部分5aを配置した場合には、バタフライバルブ3の開度を大きくした際、半体3cの先端部が流路面積拡大部分5aに面する位置まで達すると、流路面積が急激に増加してしまい、低流量の吸気制御が困難になる。   By the way, since the flow passage area enlarged portion 5a is arranged so as to enlarge the area of the flow passage 20 on the half body 3b side inclined to the upstream side of the butterfly valve 3, the flow rate adjustment by the butterfly valve 3 can be gradually performed. Low flow rate intake control (such as idle control) is possible. If the flow path area enlarged portion 5a is arranged so as to increase the area of the flow path 30 on the half 3c side that is inclined to the downstream side of the butterfly valve 3, when the opening of the butterfly valve 3 is increased, When the tip of the half 3c reaches a position facing the flow passage area enlarged portion 5a, the flow passage area increases rapidly, and intake control at a low flow rate becomes difficult.

この吸気装置1では、第1吸気管部4をスロットルボディで形成するとともに、第2及び第3吸気管部5,6を樹脂製の吸気マニホールドで形成し、第2吸気管部5の流路面積拡大部分5aに第1吸気管部4のフランジ11を隣接して不連続な段差を形成しているので、第2及び第3吸気管部5,6の成形に際し、離型方向の制約が生じなくなり、成形コストの上昇抑制が可能になる。また、流路面積拡大部分5aの容積拡大が容易になり、気流音の低減にも役立つ。   In the intake device 1, the first intake pipe portion 4 is formed of a throttle body, and the second and third intake pipe portions 5 and 6 are formed of a resin intake manifold, and the flow path of the second intake pipe portion 5 Since the discontinuous step is formed adjacent to the flange 11 of the first intake pipe portion 4 in the area enlarged portion 5a, there is a restriction in the mold release direction when the second and third intake pipe portions 5 and 6 are formed. It does not occur, and the rise in molding cost can be suppressed. Moreover, the volume expansion of the flow path area enlarged portion 5a is facilitated, which helps to reduce the air flow noise.

さらに、流路面積拡大部分5aと流路面積漸減部分5bにリブ7を一対設けて剛性を高めているので、気流音が吸気管2内で反響しにくくなり、気流音をさらに小さくできる。また、リブ7,7は、吸気管軸芯CLに沿って延び、その先端を第1及び第3吸気管部4,6の内面4a,6aと面一にして流路面積拡大部分5aと流路面積漸減部分5b内に収容してあるので、吸気抵抗の増大を抑制できる。つまり、吸気抵抗の増加を抑えつつ気流音を小さくできる。   Further, since the rigidity is enhanced by providing a pair of ribs 7 on the flow channel area enlarged portion 5a and the flow channel area gradually decreasing portion 5b, the air flow noise is less likely to reverberate in the intake pipe 2, and the air flow noise can be further reduced. The ribs 7 and 7 extend along the intake pipe axis CL, and their tips are flush with the inner surfaces 4a and 6a of the first and third intake pipe portions 4 and 6, and the flow passage area enlarged portion 5a and the flow are increased. Since it is accommodated in the road area gradually decreasing portion 5b, an increase in intake resistance can be suppressed. That is, airflow noise can be reduced while suppressing an increase in intake resistance.

〔変形例〕
図3は図1の第2及び第3吸気管部の変形例を示す図で、図2のA−A線に対応する断面図である。図4は図3のB−B線断面図である。
流路面積拡大部分5aと流路面積漸減部分5bには、吸気管軸芯CLに沿って延びるリブ70が一対設けてある。これらリブ70,70は下流側に向かって幅を徐々に大きくしてある(図4参照)。さらに、各リブ70の上面には、リブ70の高さが下流側に向かって徐々に大きくなるように形成した傾斜面70aと、傾斜面70aの下流側に連設されて第3吸気管部6の内面6aと面一に連なる平行面70bとが形成されている(図3参照)。
[Modification]
3 is a view showing a modification of the second and third intake pipe portions of FIG. 1, and is a cross-sectional view corresponding to the line AA of FIG. 4 is a cross-sectional view taken along line BB in FIG.
A pair of ribs 70 extending along the intake pipe axis CL are provided in the flow channel area enlarged portion 5a and the flow channel area gradually decreasing portion 5b. These ribs 70 and 70 are gradually increased in width toward the downstream side (see FIG. 4). Further, on the upper surface of each rib 70, an inclined surface 70a formed so that the height of the rib 70 gradually increases toward the downstream side, and a third intake pipe portion connected to the downstream side of the inclined surface 70a. 6 and the parallel surface 70b that is flush with the inner surface 6a are formed (see FIG. 3).

このようにリブ70を形成すると、第2吸気管部5の流路面積が吸気管軸芯CL方向に対して緩やかに変化し、第2吸気管部5の流路面積が第3吸気管部6の流路面積に徐々に近づくので、吸気抵抗の抑制効果がさらに高くなる。   When the rib 70 is formed in this way, the flow passage area of the second intake pipe portion 5 changes gently with respect to the intake pipe axis CL direction, and the flow passage area of the second intake pipe portion 5 changes to the third intake pipe portion. 6 is gradually approached, so that the effect of suppressing the intake resistance is further increased.

なお、この変形例ではリブ70の高さと幅を変化させているが、高さと幅のいずれか一方を変化させるだけでも、吸気抵抗の増加はある程度抑制できる。   In this modification, the height and width of the rib 70 are changed. However, the increase in the intake resistance can be suppressed to some extent only by changing either the height or the width.

ところで、2種類の付加ガスを吸気管2内に導入する場合には、2つの付加ガス導入口8をバタフライバルブ3の弁軸3aと平行になるように配置することが最も好ましい。
さらに、多くの付加ガスを吸気管2内に導入する場合には、図3に示すように、1つの付加ガス導入口8を上述の位置に配置し、残りの付加ガス導入口80は、付加ガス導入口8の上流側または下流側に隣接配置するか、あるいは、同一の吸気管周上に隣接配置すればよい。その際、ブローバイガス中のタールが隣接する付加ガス導入口80に付着するのを防止するため、ブローバイガスの導入口は下流側に配置しておくことが望ましい。
By the way, when two types of additional gas are introduced into the intake pipe 2, it is most preferable to arrange the two additional gas introduction ports 8 in parallel with the valve shaft 3 a of the butterfly valve 3.
Further, when a large amount of additional gas is introduced into the intake pipe 2, as shown in FIG. 3, one additional gas introduction port 8 is disposed at the above-mentioned position, and the remaining additional gas introduction ports 80 are added. It may be arranged adjacent to the upstream side or downstream side of the gas inlet 8 or may be arranged adjacently on the same intake pipe circumference. At that time, in order to prevent tar in the blow-by gas from adhering to the adjacent additional gas introduction port 80, it is desirable that the blow-by gas introduction port be disposed downstream.

本発明の内燃機関の吸気装置を示す図で、図2のA−A線断面図である。It is a figure which shows the intake device of the internal combustion engine of this invention, and is the sectional view on the AA line of FIG. 図1の吸気マニホールドを開口端から見た図である。FIG. 2 is a view of the intake manifold of FIG. 1 as viewed from an open end. 図1の第2及び第3吸気管部の変形例を示す図で、図2のA−A線に対応する断面図である。It is a figure which shows the modification of the 2nd and 3rd intake pipe part of FIG. 1, and is sectional drawing corresponding to the AA line of FIG. 図3のB−B線断面図である。FIG. 4 is a sectional view taken along line BB in FIG. 3.

符号の説明Explanation of symbols

1 吸気装置
2 吸気管
3 バタフライバルブ
3a 弁軸
3b 第1半体
3c 第2半体
4 第1吸気管部
5 第2吸気管部
5a 流路面積拡大部分
5b 流路面積漸減部分
6 第3給気管部
7 リブ
8 付加ガス導入口
9 吸気マニホールド
10 ホース接続管
11 フランジ
12 フランジ
13 シール材
20 第1半体側流路
30 第2半体側流路
A 吸気流
B 吸気流
a 通路
b 通路
CL 吸気管軸芯
DESCRIPTION OF SYMBOLS 1 Intake device 2 Intake pipe 3 Butterfly valve 3a Valve shaft 3b 1st half 3c 2nd half 4 1st intake pipe part 5 2nd intake pipe part 5a Flow path area enlarged part 5b Flow path area gradually reduced part 6 3rd supply Trachea part 7 Rib 8 Additional gas inlet 9 Intake manifold 10 Hose connection pipe 11 Flange 12 Flange 13 Sealing material 20 First half side flow path 30 Second half side flow path A Intake flow B Intake flow a Passage b Passage CL CL Intake pipe Shaft core

Claims (7)

内燃機関に空気を供給する吸気管内にバタフライバルブを配設してなる内燃機関の吸気装置において、前記バタフライバルブの弁軸を支持する第1吸気管部と、該第1吸気管部の流路面積よりも大きな流路面積を有し、前記第1吸気管部の下流に連設した第2吸気管部と、該第2吸気管部の流路面積よりも小さな流路面積を有し、前記第2吸気管部の下流に連設した第3吸気管部とで前記吸気管を構成するとともに、前記第2吸気管部には、前記バタフライバルブの一方の半体側の流路面積を他方の半体側の流路面積よりも大きくする流路面積拡大部分と、前記第2吸気管部の流路面積を前記第3吸気管部の流路面積に徐々に近づけるべく前記流路面積拡大部分の下流に連設した流路面積漸減部分とを設け、さらに、前記第2及び第3吸気管部の境界近傍には、前記吸気管内に付加ガスを導入する付加ガス導入口を設けたことを特徴とする内燃機関の吸気装置。   In an intake device for an internal combustion engine in which a butterfly valve is disposed in an intake pipe that supplies air to the internal combustion engine, a first intake pipe portion that supports a valve shaft of the butterfly valve, and a flow path of the first intake pipe portion A flow passage area larger than the area, a second intake pipe portion provided downstream of the first intake pipe portion, and a flow passage area smaller than the flow passage area of the second intake pipe portion, The third intake pipe portion connected downstream of the second intake pipe portion constitutes the intake pipe, and the second intake pipe portion has a flow area on one half side of the butterfly valve on the other side. A flow passage area enlarged portion that is larger than a flow passage area on the half body side, and the flow passage area enlarged portion that gradually brings the flow passage area of the second intake pipe portion closer to the flow passage area of the third intake pipe portion. A flow passage area gradually decreasing portion provided downstream of the second and third intake pipes; The vicinity of the boundary, an intake system for an internal combustion engine, characterized by comprising an additional gas inlet for introducing an additional gas into the intake pipe. 前記流路面積漸減部分と同一の吸気管周上にある領域または該領域の下流で前記第2及び第3吸気管部の境界近傍にある領域に前記付加ガス導入口を配置したことを特徴とする請求項1に記載の内燃機関の吸気装置。   The additional gas introduction port is disposed in a region on the same intake pipe circumference as the flow path area gradually decreasing portion or in a region near the boundary between the second and third intake pipe portions downstream of the region. The intake device for an internal combustion engine according to claim 1. 前記流路面積拡大部分は、前記バタフライバルブの上流側に傾倒する半体側の流路面積を拡大させるように配置してあることを特徴とする請求項1または請求項2に記載の内燃機関の吸気装置。   3. The internal combustion engine according to claim 1, wherein the flow passage area enlarged portion is arranged so as to enlarge a flow passage area on a half body side that is inclined to the upstream side of the butterfly valve. 4. Intake device. 前記バタフライバルブの一方の半体側にある流路と、他方の半体側にある流路との境界近傍に前記付加ガス導入口を配置し、該付加ガス導入口から前記バタフライバルブの弁軸と略平行な方向に前記付加ガスを吸気管内に導入することを特徴とする請求項1ないし請求項3に記載の内燃機関の吸気装置。   The additional gas introduction port is disposed in the vicinity of the boundary between the flow path on one half side of the butterfly valve and the flow path on the other half side, and the valve shaft of the butterfly valve substantially extends from the additional gas introduction port. 4. The intake system for an internal combustion engine according to claim 1, wherein the additional gas is introduced into the intake pipe in a parallel direction. 前記第1吸気管部をスロットルボディで構成するとともに、前記第2及び第3吸気管部を吸気マニホールドで構成し、該吸気マニホールドの前記スロットルボディに対する接合面に前記流路面積拡大部分を隣接させて形成したことを特徴とする請求項1ないし請求項4に記載の内燃機関の吸気装置。   The first intake pipe portion is formed of a throttle body, the second and third intake pipe portions are formed of an intake manifold, and the flow passage area enlarged portion is adjacent to a joint surface of the intake manifold to the throttle body. 5. The intake device for an internal combustion engine according to claim 1, wherein the intake device is formed as described above. 前記流路面積拡大部分には、その内部に収まって吸気管軸芯に沿って延びるリブを設けてあることを特徴とする請求項1ないし請求項5に記載の内燃機関の吸気装置。   6. The intake device for an internal combustion engine according to claim 1, wherein a rib that is accommodated in the flow passage area enlarged portion and extends along an intake pipe axis is provided in the passage area enlarged portion. 前記リブは、その高さと幅のうちの少なくとも1つが下流側に向かって大きくなるように形成してあることを特徴とする請求項1に記載の内燃機関の吸気装置。   2. The intake device for an internal combustion engine according to claim 1, wherein the rib is formed so that at least one of its height and width increases toward the downstream side.
JP2008024926A 2008-02-05 2008-02-05 Intake device for internal combustion engine Expired - Fee Related JP4951544B2 (en)

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Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2013087730A (en) * 2011-10-20 2013-05-13 Honda Motor Co Ltd Air intake device for internal combustion engine
CN104160128A (en) * 2012-02-29 2014-11-19 西门子公司 Turbocompressor

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2002004961A (en) * 2000-06-27 2002-01-09 Toyota Motor Corp Gas mixture system
JP2004100653A (en) * 2002-09-12 2004-04-02 Aichi Mach Ind Co Ltd Intake manifold
JP2007138745A (en) * 2005-11-15 2007-06-07 Nissan Motor Co Ltd Intake device of internal combustion engine

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2002004961A (en) * 2000-06-27 2002-01-09 Toyota Motor Corp Gas mixture system
JP2004100653A (en) * 2002-09-12 2004-04-02 Aichi Mach Ind Co Ltd Intake manifold
JP2007138745A (en) * 2005-11-15 2007-06-07 Nissan Motor Co Ltd Intake device of internal combustion engine

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2013087730A (en) * 2011-10-20 2013-05-13 Honda Motor Co Ltd Air intake device for internal combustion engine
CN104160128A (en) * 2012-02-29 2014-11-19 西门子公司 Turbocompressor

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