JP2007198303A - Intake port of internal combustion engine - Google Patents

Intake port of internal combustion engine Download PDF

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Publication number
JP2007198303A
JP2007198303A JP2006019137A JP2006019137A JP2007198303A JP 2007198303 A JP2007198303 A JP 2007198303A JP 2006019137 A JP2006019137 A JP 2006019137A JP 2006019137 A JP2006019137 A JP 2006019137A JP 2007198303 A JP2007198303 A JP 2007198303A
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wall surface
intake
intake valve
layer flow
intake air
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Yasuo Sato
康夫 佐藤
Hisanori Itou
寿記 伊藤
Osamu Horikoshi
修 堀越
Yusuke Hoki
雄介 伯耆
Tomoyuki Takada
倫行 高田
Hirokazu Ito
弘和 伊藤
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Toyota Motor Corp
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Toyota Motor Corp
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    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00Road transport of goods or passengers
    • Y02T10/10Internal combustion engine [ICE] based vehicles
    • Y02T10/12Improving ICE efficiencies

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Abstract

<P>PROBLEM TO BE SOLVED: To concurrently secure both strong swirl and high charging efficiency. <P>SOLUTION: The upper wall surface 14 of an intake port 4 at the intake air inflow passage part 8 is formed of a first upper wall surface 14a and a second upper wall surface 14b lower than the first upper wall surface 14a. A lower layer flow passage X and an upper layer flow passage Y are formed on both sides of the top part of the second upper wall surface 14b. The side wall surface 9 of a spiral part 7 so extends as to close the downstream end of the lower layer flow passage X. A lower layer flow guide pipe 20 extending from the lower layer flow passage X to an intake valve opening area Z is installed. A lower layer flow flowing in the lower layer flow passage X produces swirl by flowing in the circumferential direction of a combustion chamber 3 after passing through the intake valve opening area Z when the intake valve 6 is opened. An upper layer flow flowing in the upper layer flow passage Y flows into the combustion chamber 3 after passing through the spiral part 7. <P>COPYRIGHT: (C)2007,JPO&INPIT

Description

本発明の内燃機関の吸気ポートに関する。   The present invention relates to an intake port of an internal combustion engine of the present invention.

吸気弁の軸線回りに形成された渦巻部と、渦巻部から接線状に延びる吸入空気流入通路部とにより構成され、吸入空気流入通路部が渦巻部の周壁面に接線状に接続される第1の側壁面と、吸気弁の弁軸に向けて渦巻部の周壁面まで延びる第2の側壁面とを有するヘリカル型吸気ポートにおいて、吸入空気流入通路部の上壁面が上述の第1の側壁面側に位置しかつ渦巻部の上壁面に滑らかに接続する第1の上壁面と、上述の第2の側壁面側に位置しかつ第1の上壁面よりも高さの低い第2の上壁面からなり、この第2の上壁面の高さ位置を境にして吸入空気流入通路部の底壁面に沿って流れる下層流と第1の上壁面に沿って流れる上層流とが発生し、この上層流によって燃焼室内にスワールが発生せしめられるヘリカル型吸気ポートが公知である(特許文献1を参照)。   A first portion is formed by a spiral portion formed around the axis of the intake valve and an intake air inflow passage portion extending tangentially from the spiral portion, and the intake air inflow passage portion is tangentially connected to the peripheral wall surface of the spiral portion. And a second side wall surface extending to the circumferential wall surface of the spiral portion toward the valve shaft of the intake valve, the upper wall surface of the intake air inflow passage portion is the first side wall surface described above. A first upper wall surface located on the side and smoothly connected to the upper wall surface of the spiral portion, and a second upper wall surface located on the second side wall surface side and having a height lower than that of the first upper wall surface A lower flow that flows along the bottom wall surface of the intake air inflow passage portion and an upper flow that flows along the first upper wall surface at the height position of the second upper wall surface. A helical intake port is known in which swirl is generated in the combustion chamber by the flow. (See Patent Document 1).

このヘリカル型吸気ポートでは吸入空気量が多いときに渦巻部内での上層流の旋回作用が下層流によって弱められ、それにより機関高回転域において過剰なスワールが発生するのが阻止される。
実開平2−147830号公報
In this helical type intake port, when the intake air amount is large, the swirling action of the upper layer flow in the spiral portion is weakened by the lower layer flow, thereby preventing the occurrence of excessive swirl in the high engine speed region.
Japanese Utility Model Publication No. 2-147830

ところでこのヘリカル型吸気ポートでは従来のヘリカル型吸気ポートと同様に吸入空気を渦巻部内で旋回させることにより燃焼室内にスワールを発生させるようにしている。この場合、スワールを強めるためには渦巻部内での旋回作用を強めなければならない。しかしながら渦巻部内での旋回作用を強めると吸入抵抗が増大するために充填効率が低下し、その結果最大負荷運転時の出力が低下することになる。   By the way, in this helical type intake port, swirl is generated in the combustion chamber by swirling the intake air in the spiral portion as in the conventional helical type intake port. In this case, in order to strengthen the swirl, the swirling action in the spiral portion must be strengthened. However, if the swirling action in the spiral portion is increased, the suction resistance increases, so that the charging efficiency is lowered, and as a result, the output during the maximum load operation is lowered.

このように渦巻部内における旋回作用を強めることによってスワールを強めるようにしている限り、強力なスワールと高い充填効率を同時に確保することは困難であり、強力なスワールと高い充填効率を同時に確保するには発想の転換が必要である。
本発明者はこれまで長い期間に亘って吸入空気の流れ方について研究し、終いに強力なスワールと高い充填効率を同時に確保することのできる吸気ポートを見い出したのである。
As long as the swirl is strengthened by strengthening the swirling action in the spiral part, it is difficult to ensure a strong swirl and high filling efficiency at the same time. To ensure a strong swirl and high filling efficiency at the same time Needs a change of mindset.
The inventor has studied the flow of intake air over a long period of time, and finally found an intake port that can simultaneously ensure a strong swirl and high filling efficiency.

即ち、本発明によれば、吸気弁の軸線回りに形成された渦巻部と、渦巻部から接線状に延びる吸入空気流入通路部とにより構成され、渦巻部が吸気弁の軸線回りを延びる周壁面と、上壁面と、吸気弁により開閉される下端出口部とにより画定されており、吸入空気流入通路部が渦巻部の周壁面に接線状に接続される第1の側壁面と、吸気弁の弁軸に向けて渦巻部の周壁面まで延びる第2の側壁面と、上壁面と、底壁面とにより画定されている内燃機関の吸気ポートにおいて、渦巻部の下端出口部が燃焼室頂面の周縁部に配置されると共に、第1の側壁面が燃焼室の周縁部に対して接線状に延びるように吸入空気流入通路部が配置されており、吸気弁全開時に吸気弁と吸気弁の弁座間に形成される環状の吸気弁開口部のうちで、シリンダ軸線と吸気弁弁体の中心部とを含む平面に対し吸入空気流入通路部と反対側に形成される吸気弁開口部領域が存在しており、吸入空気流入通路部内に吸入空気流入通路部の下方を流れる下層流と吸入空気流入通路部の上方を流れる上層流が発生せしめられ、この下層流を吸気弁開口部領域に導くために吸入空気流入通路部から渦巻部内を横切って吸気弁開口部領域に向けて延びる下層流案内管を設け、吸気弁開弁時に下層流を下層流案内管により吸気弁開口部領域に導びいて吸気弁開口部領域から燃焼室内に燃焼室の周辺方向に向け流入させることにより燃焼室内にスワールを発生させ、上層流は吸気弁開弁時渦巻部内で旋回した後に吸気弁開口部全体から分散して燃焼室内に流入せしめられる。   That is, according to the present invention, the peripheral wall surface is configured by the spiral portion formed around the axis of the intake valve and the intake air inflow passage portion extending tangentially from the spiral portion, and the spiral portion extends around the axis of the intake valve. A first side wall surface tangentially connected to the peripheral wall surface of the spiral portion, and an intake valve In the intake port of the internal combustion engine defined by the second side wall surface extending toward the peripheral wall surface of the spiral portion toward the valve shaft, the upper wall surface, and the bottom wall surface, the lower end outlet portion of the spiral portion is the top surface of the combustion chamber. An intake air inflow passage portion is arranged at the peripheral portion so that the first side wall surface extends tangentially to the peripheral portion of the combustion chamber. Among the annular intake valve openings formed between the seats, the cylinder axis An intake valve opening region formed on the opposite side of the intake air inflow passage portion with respect to a plane including the central portion of the air valve body exists, and the intake air inflow passage portion is located below the intake air inflow passage portion. An upper layer flow that flows above the flowing lower layer flow and the intake air inflow passage portion is generated, and in order to guide the lower layer flow to the intake valve opening region, the intake air inflow passage portion crosses the inside of the spiral portion and enters the intake valve opening region. A lower flow guide pipe extending toward the engine is provided, and when the intake valve is opened, the lower flow is led to the intake valve opening area by the lower flow guide pipe and flows into the combustion chamber from the intake valve opening area toward the periphery of the combustion chamber. As a result, a swirl is generated in the combustion chamber, and the upper layer flow is swirled in the spiral portion when the intake valve is opened, and then dispersed from the entire intake valve opening and flows into the combustion chamber.

下層流案内管内を流れる下層流によってスワールが発生せしめられ、上層流路内を流れる上層流によって高い充填効率が確保される。   A swirl is generated by the lower flow flowing in the lower flow guide pipe, and high filling efficiency is ensured by the upper flow flowing in the upper flow path.

図1から図3を参照すると、1はシリンダブロック、2はシリンダヘッド、3は燃焼室を夫々示す。図1に示される実施例ではシリンダヘッド2内に一対の吸気ポート4,5が形成されており、また図1には示されていないがシリンダヘッド2内には一対の排気ポートが形成されている。本発明は一対の吸気ポート4,5のうちの図1において実線で示される片方の吸気ポート4に関するものであり、従って以下この吸気ポート4についてのみ説明する。   1 to 3, reference numeral 1 denotes a cylinder block, 2 denotes a cylinder head, and 3 denotes a combustion chamber. In the embodiment shown in FIG. 1, a pair of intake ports 4 and 5 are formed in the cylinder head 2, and a pair of exhaust ports are formed in the cylinder head 2 although not shown in FIG. Yes. The present invention relates to one intake port 4 indicated by a solid line in FIG. 1 of the pair of intake ports 4 and 5, and therefore only the intake port 4 will be described below.

図1から図3を参照すると、吸気ポート4は吸気弁6の軸線回りに形成された渦巻部7と、この渦巻部7から接線状に延びる吸入空気流入通路部8とにより構成される。図1、図2および図3(C)に示されるように渦巻部7は吸気弁6の軸線回りを延びる周壁面9と、上壁面10と、吸気弁6により開閉される下端出口部11とにより画定されており、図1および図2に示されるように吸入空気流入通路部8は渦巻部7の周壁面9に接線状に接続される第1の側壁面12と、吸気弁6の弁軸6aに向けて渦巻部7の周壁面9まで延びる第2の側壁面13と、上壁面14と、底壁面15とにより画定されている。   Referring to FIGS. 1 to 3, the intake port 4 is constituted by a spiral portion 7 formed around the axis of the intake valve 6 and an intake air inflow passage portion 8 extending tangentially from the spiral portion 7. As shown in FIGS. 1, 2, and 3 (C), the spiral portion 7 includes a peripheral wall surface 9 that extends around the axis of the intake valve 6, an upper wall surface 10, and a lower end outlet portion 11 that is opened and closed by the intake valve 6. 1 and 2, the intake air inflow passage portion 8 includes a first side wall surface 12 tangentially connected to the peripheral wall surface 9 of the spiral portion 7, and a valve of the intake valve 6. It is demarcated by the 2nd side wall surface 13 extended to the surrounding wall surface 9 of the spiral part 7 toward the axis | shaft 6a, the upper wall surface 14, and the bottom wall surface 15. FIG.

図1からわかるように渦巻部7の下端出口部11は燃焼室3の頂面16(図2)の周縁部に配置され、第1の側壁面12が燃焼室3の周縁部に対して接線状に延びるように吸入空気流入通路部8が配置されている。即ち、図1に示されるように吸入空気流入通路部8の下流側は燃焼室3の周縁部に対して接線状に延びており、吸入空気流入通路部8の上流側はレイアウト上の理由から吸入空気流入通路部8の下流側に対して燃焼室3から離れる方向に若干折曲せしめられている。   As can be seen from FIG. 1, the lower end outlet portion 11 of the spiral portion 7 is disposed at the peripheral portion of the top surface 16 (FIG. 2) of the combustion chamber 3, and the first side wall surface 12 is tangent to the peripheral portion of the combustion chamber 3. An intake air inflow passage portion 8 is arranged so as to extend in a shape. That is, as shown in FIG. 1, the downstream side of the intake air inflow passage portion 8 extends tangentially to the peripheral edge of the combustion chamber 3, and the upstream side of the intake air inflow passage portion 8 is for layout reasons. It is slightly bent in the direction away from the combustion chamber 3 with respect to the downstream side of the intake air inflow passage portion 8.

図5は吸気ポート4を図解的に表した斜視図を示している。図1から図3および図5を参照すると吸入空気流入通路部8の上壁面14は吸入空気流入通路部8の少くとも下流側において、第1の側壁面12側に位置しかつ渦巻部7の上壁面10に滑らかに接続する第1の上壁面14aと、第2の側壁面13側に位置しかつ第1の上壁面14aよりも底壁面15側に位置する第2の上壁面14bとにより構成される。第1の上壁面14aに対して低い位置に第2の上壁面14bが形成されている吸入空気流入通路部8部分の断面形状が図5においてハッチングで示されている。   FIG. 5 is a perspective view schematically showing the intake port 4. Referring to FIGS. 1 to 3 and FIG. 5, the upper wall surface 14 of the intake air inflow passage portion 8 is located on the first side wall surface 12 side at least downstream of the intake air inflow passage portion 8 and A first upper wall surface 14a that smoothly connects to the upper wall surface 10 and a second upper wall surface 14b that is located on the second side wall surface 13 side and located on the bottom wall surface 15 side with respect to the first upper wall surface 14a. Composed. The cross-sectional shape of the intake air inflow passage portion 8 where the second upper wall surface 14b is formed at a lower position than the first upper wall surface 14a is shown by hatching in FIG.

図3(A)〜(C)および図5からわかるように第1の上壁面14aは渦巻部7に向けて次第に横巾が狹ばまりつつ下降し、次いで上述した如く渦巻部7の上壁面10に滑らかに接続される。この渦巻部7の上壁面10は渦巻部7の周縁部に沿って徐々に下降しつつ渦巻部7の全周のほぼ3/4に亘って延びる。一方、第2の上壁面14bの巾は吸入空気流入通路部8の下流側では底壁面15の巾のほぼ1/3程度であって一定であり、吸入空気流入通路部8の上流側では上流に向かうに従って次第に狹くなる。   As can be seen from FIGS. 3A to 3C and FIG. 5, the first upper wall surface 14a descends gradually toward the spiral portion 7 while the lateral width gradually decreases, and then the upper wall surface of the spiral portion 7 as described above. 10 is connected smoothly. The upper wall surface 10 of this spiral part 7 extends over almost ¾ of the entire circumference of the spiral part 7 while gradually descending along the peripheral part of the spiral part 7. On the other hand, the width of the second upper wall surface 14 b is approximately 1/3 of the width of the bottom wall surface 15 on the downstream side of the intake air inflow passage portion 8 and is constant, and on the upstream side of the intake air inflow passage portion 8. It gradually becomes ugly as you go to.

一方、図3(A)〜(C)および図5に示されるように第1の上壁面14aおよび第2の上壁面14bは吸入空気流入通路部8の横断面内においてはほぼ水平方向に延びており、これら第1の上壁面14aと第2の上壁面14bとの間に位置する壁面17は下向きの傾斜面からなる。この傾斜面17の巾は渦巻部7に向けて次第に広くなる。一方、図2に示されるように第2の上壁面14bも渦巻部7に向けて下降しており、この場合第2の上壁面14bの傾斜角は第1の上壁面14aの傾斜角よりも大きい。   On the other hand, as shown in FIGS. 3A to 3C and FIG. 5, the first upper wall surface 14 a and the second upper wall surface 14 b extend in a substantially horizontal direction within the cross section of the intake air inflow passage portion 8. The wall surface 17 located between the first upper wall surface 14a and the second upper wall surface 14b is a downward inclined surface. The width of the inclined surface 17 gradually increases toward the spiral portion 7. On the other hand, as shown in FIG. 2, the second upper wall surface 14b is also lowered toward the spiral portion 7. In this case, the inclination angle of the second upper wall surface 14b is larger than the inclination angle of the first upper wall surface 14a. large.

このように第1の上壁面14aと第2の上壁面14bとを階段状に形成すると吸入空気流入通路部8内には図5においてハッチングXで示される如く第1の側壁面12の下方部、第2の側壁面13、第2の上壁面14bおよび底壁面15によって画定された下層流路と、ハッチングYで示される如く下層流路の上方であって下層流路と第1の上壁面14a間に位置する上層流路とが形成される。即ち、吸入空気流入通路部8内には下層流路X内を流れる下層流と上層流路Y内を流れる上層流との2つの流れが発生する。   When the first upper wall surface 14a and the second upper wall surface 14b are formed stepwise in this way, the lower portion of the first side wall surface 12 is shown in the intake air inflow passage portion 8 as indicated by hatching X in FIG. A lower channel defined by the second side wall surface 13, the second upper wall surface 14b, and the bottom wall surface 15, and a lower channel and the first upper wall surface above the lower channel as indicated by hatching Y. The upper flow path located between 14a is formed. That is, in the intake air inflow passage portion 8, two flows are generated: a lower layer flow flowing in the lower layer flow path X and an upper layer flow flowing in the upper layer flow path Y.

図4は図1の拡大図を示す。図2および図3(C)に示されるように吸気弁6が開弁すると吸気弁6と吸気弁6の弁座18間には環状の吸気弁開口部19が形成される。この場合、吸気弁6全開時に吸気弁6と吸気弁6の弁座18間に形成される環状の吸気弁開口部19のうちで、図4においてシリンダ軸線Oと吸気弁6の弁体の中心部とを含む平面Kに対し吸入空気流入通路部8と反対側に形成される吸気弁開口部領域が存在する。   FIG. 4 shows an enlarged view of FIG. When the intake valve 6 is opened as shown in FIGS. 2 and 3C, an annular intake valve opening 19 is formed between the intake valve 6 and the valve seat 18 of the intake valve 6. In this case, in the annular intake valve opening 19 formed between the intake valve 6 and the valve seat 18 of the intake valve 6 when the intake valve 6 is fully opened, the cylinder axis O and the center of the valve body of the intake valve 6 in FIG. There is an intake valve opening region formed on the opposite side of the intake air inflow passage portion 8 with respect to the plane K including the portion.

この吸気弁開口部領域が図4および図5においてZで示されている。
この吸気弁開口部領域Zが図4において平面Kと燃焼室3周縁部側の吸気弁開口部19との交差部から渦巻部7内における吸入空気流の旋回方向にほぼ90度の範囲Mである。
This intake valve opening region is indicated by Z in FIGS.
This intake valve opening region Z is in a range M of approximately 90 degrees in the swirling direction of the intake air flow in the spiral portion 7 from the intersection of the plane K and the intake valve opening 19 on the peripheral edge side of the combustion chamber 3 in FIG. is there.

一方、図1、図2および図4に示されるように渦巻部7の側壁面9は下層流路Xの下流端を閉塞するように延びている。もう少し具体的に言うと下層流路Xの下流端を閉塞するこの渦巻部7の側壁面部分9aは図2に示されるように第2の上壁面14bの下流端から下方に向けて底壁面15の近傍まで延びており、また、この側壁面部分9aは図1に示されるように第2の側壁面13から第1の側壁面12に向けて第2の上壁面14bの全横巾に亘って延びている。   On the other hand, as shown in FIGS. 1, 2, and 4, the side wall surface 9 of the spiral portion 7 extends so as to close the downstream end of the lower layer flow path X. More specifically, the side wall surface portion 9a of the spiral portion 7 that closes the downstream end of the lower layer flow path X has a bottom wall surface 15 facing downward from the downstream end of the second upper wall surface 14b as shown in FIG. The side wall surface portion 9a extends over the entire width of the second upper wall surface 14b from the second side wall surface 13 toward the first side wall surface 12, as shown in FIG. It extends.

吸気ポート4内には下層流を吸気弁開口部領域Zに導くために吸入空気流入通路部8から渦巻部7内を横切って吸気弁開口部領域Zに向けて延びる下層流案内管20が設けられている。この下層流案内管20は下層流路Xの下流端を閉塞する渦巻部7の側壁面部分9a内を貫通し、下層流路X内から渦巻部7内を横切って吸気弁開口部領域Zに向けて延びている。図1から図5に示す実施例ではこの下層流案内管20は中空円筒からなる。   In the intake port 4, a lower flow guide pipe 20 extending from the intake air inflow passage portion 8 across the spiral portion 7 toward the intake valve opening region Z is provided in order to guide the lower flow to the intake valve opening region Z. It has been. The lower flow guide tube 20 passes through the side wall surface portion 9a of the spiral portion 7 that closes the downstream end of the lower flow passage X, and crosses the spiral portion 7 from the lower flow passage X to the intake valve opening region Z. It extends toward. In the embodiment shown in FIGS. 1 to 5, the lower flow guide tube 20 is formed of a hollow cylinder.

このような下層流案内管20を設けると第2の上壁面14b下方の下層流路X内を流れる下層流は吸気弁6の開弁時に、下層流案内管20内を進んだ後、図4において矢印Sで示すように吸気弁開口部領域Zから燃焼室3内に燃焼室3の周辺方向に向けて流入し、それによって燃焼室3内にはシリンダ軸線O回りの強力なスワールが発生せしめられる。   When such a lower flow guide pipe 20 is provided, the lower flow flowing in the lower flow path X below the second upper wall surface 14b advances through the lower flow guide pipe 20 when the intake valve 6 is opened, As shown by an arrow S, the air flows from the intake valve opening region Z into the combustion chamber 3 toward the periphery of the combustion chamber 3, thereby generating a strong swirl around the cylinder axis O in the combustion chamber 3. It is done.

一方、上層流路Y内を流れる上層流は吸気弁6の開弁時に上層流路Y内を進んだ後、渦巻部7内で旋回し、図4において矢印Tで示されるように吸気弁開口部19の全体から分散して燃焼室3内に流入する。このように吸入空気が吸気弁開口部19の全体から流入させることによって吸入空気量を増大させることができる。即ち、上層流を旋回させないで燃焼室3内に流入させようとすると大部分の上層流は吸入空気流入通路部8とは反対側の吸気弁開口部のみから燃焼室3内に流入することになる。このことは実質的に吸気弁開口部の流路面積が小さくなっていることと同じであり、従って吸入空気量の増大は期待できない。   On the other hand, the upper layer flow flowing in the upper layer flow path Y advances in the upper layer flow path Y when the intake valve 6 is opened, and then swirls in the spiral portion 7 to open the intake valve opening as shown by an arrow T in FIG. Dispersed from the entire portion 19 and flows into the combustion chamber 3. Thus, the amount of intake air can be increased by allowing the intake air to flow from the entire intake valve opening 19. That is, if the upper layer flow is caused to flow into the combustion chamber 3 without swirling, most of the upper layer flow flows into the combustion chamber 3 only from the intake valve opening on the side opposite to the intake air inflow passage portion 8. Become. This is substantially the same as the flow passage area of the intake valve opening being reduced, and therefore an increase in the intake air amount cannot be expected.

これに対して上層流に渦巻部7内で旋回流を与えると上層流は上述したように吸気弁開口部19の全体から分散して燃焼室3内に流入する。このことは吸気弁開口部19の流路面積が大きくなったことと同じであり、従って吸入空気量が増大するために充填効率が向上することになる。このように本発明において渦巻部7内で旋回流を生じさせるのは充填効率の向上のためであり、従来のようにスワールの発生のためではない。   On the other hand, when a swirl flow is given to the upper layer flow in the spiral portion 7, the upper layer flow is dispersed from the entire intake valve opening 19 and flows into the combustion chamber 3 as described above. This is the same as the flow passage area of the intake valve opening 19 is increased, and therefore the intake air amount is increased, so that the charging efficiency is improved. In this way, in the present invention, the swirl flow is generated in the spiral portion 7 for the purpose of improving the filling efficiency and not for the generation of swirl as in the prior art.

一方、吸入空気を渦巻部7内で旋回させつつ燃焼室3内に流入させると旋回している吸入空気流全体がそのままスワール流に移行していくかのように思える。しかしながらスワールの発生に寄与するのは旋回する吸入空気流のうちの燃焼室3の周辺方向に向かう一部の吸入空気流であり、従って吸入空気を旋回しつつ燃焼室3内に流入させても実際には吸入空気の一部しかスワールの発生に寄与しない。即ち、スワールを発生させるためには本発明におけるように燃焼室3の周辺方向に向かう強力な吸入空気流を発生させることが最も効果的である。   On the other hand, when the intake air is swirled in the spiral portion 7 and flows into the combustion chamber 3, it seems as if the swirled intake air flow is shifted to the swirl flow as it is. However, it is a part of the swirling intake air flow that is directed toward the periphery of the combustion chamber 3 that contributes to the generation of swirl. Therefore, even if the intake air is swirled and flows into the combustion chamber 3 Actually, only a part of the intake air contributes to the generation of the swirl. That is, in order to generate a swirl, it is most effective to generate a strong intake air flow toward the periphery of the combustion chamber 3 as in the present invention.

渦巻部7の側壁面部分9aを設けないと第2の上壁面14bの下方を通って吸気弁開口部領域Zに向かう下層流と、渦巻部7内で旋回しはじめた上層流とが互いに干渉し、その結果強力なスワールが得られなくなる。これに対し、渦巻部7の側壁面部分9aを設けるとこのような下層流と上層流との干渉がなくなるために強力なスワールを得ることができるようになる。   If the side wall surface portion 9a of the spiral portion 7 is not provided, the lower layer flow toward the intake valve opening region Z passing under the second upper wall surface 14b and the upper layer flow that starts to swirl in the spiral portion 7 interfere with each other. As a result, a strong swirl cannot be obtained. On the other hand, when the side wall surface portion 9a of the spiral portion 7 is provided, since such interference between the lower layer flow and the upper layer flow is eliminated, a strong swirl can be obtained.

図6および図7に夫々別の実施例を示す。図6に示す実施例では下層流案内管20の下流端が燃焼室3の頂面16とほぼ平行をなすように斜めに切除されている。このようにすると下層流案内管20の下流端を吸気弁開口部領域Zに近づけることができるので燃焼室3の周辺方向に向かう強力な空気流を発生することができる。また、図7に示す実施例では図8に示されるように吸入空気流入通路部8の第1の側壁面12側に位置する下層流案内管20の壁面上に下層流案内管20の全長に亘って延びるスリット21が形成されている。   6 and 7 show different embodiments. In the embodiment shown in FIG. 6, the downstream end of the lower flow guide tube 20 is cut obliquely so as to be substantially parallel to the top surface 16 of the combustion chamber 3. In this way, the downstream end of the lower flow guide tube 20 can be brought close to the intake valve opening region Z, so that a strong air flow toward the periphery of the combustion chamber 3 can be generated. In the embodiment shown in FIG. 7, as shown in FIG. 8, the entire length of the lower flow guide tube 20 is formed on the wall surface of the lower flow guide tube 20 located on the first side wall surface 12 side of the intake air inflow passage portion 8. A slit 21 is formed to extend over.

このように本発明では下層流案内管20内から燃焼室3内に燃焼室3の周辺方向に向けて流入する下層流によって燃焼室3内に強力なスワールが発生せしめられ、渦巻部7内で旋回した後に燃焼室3内に流入する上層流において吸入空気量が増大せしめられ、それにより高い充填効率を図りつつ強力なスワールを発生しうるようにしている。   As described above, in the present invention, a strong swirl is generated in the combustion chamber 3 by the lower flow that flows from the lower flow guide tube 20 into the combustion chamber 3 toward the periphery of the combustion chamber 3, and the swirl 7 The amount of intake air is increased in the upper layer flow that flows into the combustion chamber 3 after turning, so that a strong swirl can be generated while achieving high filling efficiency.

吸気ポートの平面図である。It is a top view of an intake port. 図1のII−II線に沿ってみた吸気ポートの断面図である。It is sectional drawing of the intake port seen along the II-II line of FIG. 図1に示される吸気ポートの断面図であって、(A),(B),(C)は夫々図1のA−A線、B−B線、C−C線に沿ってみた断面図である。FIG. 2 is a cross-sectional view of the intake port shown in FIG. 1, wherein (A), (B), and (C) are cross-sectional views taken along lines AA, BB, and CC, respectively, in FIG. It is. 図1の拡大図である。It is an enlarged view of FIG. 図解的に表した吸気ポートの斜視図である。It is a perspective view of the intake port represented graphically. 別の実施例を示す吸気ポートの側面断面図である。It is side surface sectional drawing of the intake port which shows another Example. 更に別の実施例を示す吸気ポートの側面断面図である。It is side surface sectional drawing of the intake port which shows another Example. 下層流案内管の斜視図である。It is a perspective view of a lower layer flow guide pipe.

符号の説明Explanation of symbols

3 燃焼室
4,5 吸気ポート
6 吸気弁
7 渦巻部
8 吸入空気流入通路部
9 周壁面
10 上壁面
11 下端出口部
12 第1の側壁面
13 第2の側壁面
14a 第1の上壁面
14b 第2の上壁面
15 底壁面
18 弁座
19 吸気弁開口部
20 下層流案内管
X 上層流路
Y 下層流路
Z 吸気弁開口部領域
DESCRIPTION OF SYMBOLS 3 Combustion chamber 4,5 Intake port 6 Intake valve 7 Spiral part 8 Intake air inflow passage part 9 Peripheral wall surface 10 Upper wall surface 11 Lower end outlet part 12 1st side wall surface 13 2nd side wall surface 14a 1st upper wall surface 14b 1st 2 Upper wall surface 15 Bottom wall surface 18 Valve seat 19 Intake valve opening 20 Lower layer flow guide tube X Upper layer flow channel Y Lower flow channel Z Intake valve opening region

Claims (6)

吸気弁の軸線回りに形成された渦巻部と、該渦巻部から接線状に延びる吸入空気流入通路部とにより構成され、該渦巻部が吸気弁の軸線回りを延びる周壁面と、上壁面と、吸気弁により開閉される下端出口部とにより画定されており、該吸入空気流入通路部が渦巻部の周壁面に接線状に接続される第1の側壁面と、吸気弁の弁軸に向けて渦巻部の周壁面まで延びる第2の側壁面と、上壁面と、底壁面とにより画定されている内燃機関の吸気ポートにおいて、上記渦巻部の下端出口部が燃焼室頂面の周縁部に配置されると共に、上記第1の側壁面が燃焼室の周縁部に対して接線状に延びるように吸入空気流入通路部が配置されており、吸気弁全開時に吸気弁と吸気弁の弁座間に形成される環状の吸気弁開口部のうちで、シリンダ軸線と吸気弁弁体の中心部とを含む平面に対し吸入空気流入通路部と反対側に形成される吸気弁開口部領域が存在しており、上記吸入空気流入通路部内に吸入空気流入通路部の下方を流れる下層流と吸入空気流入通路部の上方を流れる上層流が発生せしめられ、該下層流を吸気弁開口部領域に導くために該吸入空気流入通路部から渦巻部内を横切って吸気弁開口部領域に向けて延びる下層流案内管を設け、吸気弁開弁時に該下層流を該下層流案内管により吸気弁開口部領域に導びいて該吸気弁開口部領域から燃焼室内に燃焼室の周辺方向に向け流入させることにより燃焼室内にスワールを発生させ、上記上層流は吸気弁開弁時渦巻部内で旋回した後に吸気弁開口部全体から分散して燃焼室内に流入する内燃機関の吸気ポート。   A spiral portion formed around the axis of the intake valve, an intake air inflow passage portion extending tangentially from the spiral portion, a peripheral wall surface extending around the axis of the intake valve, an upper wall surface, A first side wall surface that is defined by a lower end outlet portion that is opened and closed by an intake valve, and the intake air inflow passage portion is tangentially connected to the peripheral wall surface of the spiral portion, and toward the valve shaft of the intake valve In the intake port of the internal combustion engine defined by the second side wall surface extending to the peripheral wall surface of the spiral portion, the upper wall surface, and the bottom wall surface, the lower end outlet portion of the spiral portion is disposed at the peripheral edge portion of the combustion chamber top surface In addition, an intake air inflow passage is disposed so that the first side wall surface extends tangentially to the peripheral edge of the combustion chamber, and is formed between the intake valve and the valve seat of the intake valve when the intake valve is fully open. Of the annular intake valve opening, the cylinder axis and the intake valve valve An intake valve opening region formed on the opposite side of the intake air inflow passage portion with respect to a plane including the central portion of the intake air flow passage exists, and the lower layer flow that flows below the intake air inflow passage portion in the intake air inflow passage portion And an upper layer flow that flows above the intake air inflow passage portion is generated, and in order to guide the lower layer flow to the intake valve opening region, from the intake air inflow passage portion across the spiral portion toward the intake valve opening region. An extended lower flow guide pipe is provided, and when the intake valve is opened, the lower flow is guided to the intake valve opening area by the lower flow guide pipe and flows from the intake valve opening area into the combustion chamber toward the periphery of the combustion chamber. An intake port of the internal combustion engine in which a swirl is generated in the combustion chamber and the upper layer flow is swirled in the spiral portion when the intake valve is opened and then dispersed from the entire intake valve opening and flows into the combustion chamber. 上記吸入空気流入通路部の上壁面を吸入空気流入通路部の少くとも下流側において、上記第1の側壁面側に位置しかつ渦巻部の上壁面に滑らかに接続する第1の上壁面と、上記第2の側壁面側に位置しかつ該第1の上壁面よりも上記底壁面側に位置する第2の上壁面とにより構成し、上記下層流が流れる下層流路が上記第1の側壁面の下方部、上記第2の側壁面、上記第2の上壁面および上記底壁面によって画定され、上記上層流が流れる上層流路が、下層流路の上方であって下層流路と上記第1の上壁面間に形成され、上記下層流案内管が該下層流路内から渦巻部内を横切って吸気弁開口部領域に向けて延びている請求項1に記載の内燃機関の吸気ポート。   A first upper wall surface that is located on the first side wall surface side at least downstream of the intake air inflow passage portion and smoothly connected to the upper wall surface of the spiral portion; And a second upper wall surface positioned on the second side wall surface side and positioned on the bottom wall surface side with respect to the first upper wall surface, and the lower layer flow path through which the lower layer flow flows is the first side The upper layer flow path defined by the lower part of the wall surface, the second side wall surface, the second upper wall surface and the bottom wall surface and through which the upper layer flow flows is above the lower layer flow path and the lower layer flow path and the first wall surface. 2. The intake port of the internal combustion engine according to claim 1, wherein the intake port is formed between upper wall surfaces of the internal combustion engine and extends from the lower flow path to the intake valve opening region across the spiral portion. 上記渦巻部の側壁面が上記下層流路の下流端を閉塞するように延びており、上記下層流案内管が上記下層流路の下流端を閉塞する渦巻部の側壁面部分内を貫通している請求項2に記載の内燃機関の吸気ポート。   The side wall surface of the spiral portion extends so as to close the downstream end of the lower layer flow path, and the lower layer flow guide tube passes through the side wall surface portion of the spiral portion blocking the downstream end of the lower layer flow path. The intake port of the internal combustion engine according to claim 2. 上記吸気弁開口部領域は上記平面と燃焼室周縁部側の吸気弁開口部との交差部から渦巻部内における吸入空気流の旋回方向にほぼ90度の範囲である請求項1に記載の内燃機関の吸気ポート。   2. The internal combustion engine according to claim 1, wherein the intake valve opening region is in a range of approximately 90 degrees in a swirling direction of the intake air flow in the spiral portion from an intersection of the flat surface and the intake valve opening on the peripheral side of the combustion chamber. Intake port. 上記下層流案内管の下流端が燃焼室頂面とほぼ平行をなすように斜めに切除されている請求項1に記載の内燃機関の吸気ポート。   The intake port of an internal combustion engine according to claim 1, wherein the downstream end of the lower flow guide pipe is cut obliquely so as to be substantially parallel to the top surface of the combustion chamber. 吸入空気流入通路部の上記第1の側壁面側に位置する下層流案内管の壁面上に下層流案内管の全長に亘って延びるスリットが形成されている請求項1に記載の内燃機関の吸気ポート。   The intake of the internal combustion engine according to claim 1, wherein a slit extending over the entire length of the lower flow guide tube is formed on a wall surface of the lower flow guide tube located on the first side wall surface side of the intake air inflow passage portion. port.
JP2006019137A 2006-01-27 2006-01-27 Intake port of internal combustion engine Pending JP2007198303A (en)

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Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113976834A (en) * 2021-11-04 2022-01-28 中国重汽集团济南动力有限公司 Engine air flue sand core device
KR20220020021A (en) 2020-08-11 2022-02-18 한화정밀기계 주식회사 Adjusting device for lead of component

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR20220020021A (en) 2020-08-11 2022-02-18 한화정밀기계 주식회사 Adjusting device for lead of component
CN113976834A (en) * 2021-11-04 2022-01-28 中国重汽集团济南动力有限公司 Engine air flue sand core device
CN113976834B (en) * 2021-11-04 2023-10-27 中国重汽集团济南动力有限公司 Engine air flue sand core device

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