JP2007297991A - Intake port for internal combustion engine - Google Patents

Intake port for internal combustion engine Download PDF

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Publication number
JP2007297991A
JP2007297991A JP2006127402A JP2006127402A JP2007297991A JP 2007297991 A JP2007297991 A JP 2007297991A JP 2006127402 A JP2006127402 A JP 2006127402A JP 2006127402 A JP2006127402 A JP 2006127402A JP 2007297991 A JP2007297991 A JP 2007297991A
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wall surface
intake valve
intake
combustion engine
internal combustion
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JP4650333B2 (en
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Yasuo Sato
康夫 佐藤
Hisanori Itou
寿記 伊藤
Osamu Horikoshi
修 堀越
Genshiro Endo
元志郎 遠藤
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 simultaneously secure a strong swirl and high filling efficiency. <P>SOLUTION: Inside an intake port 4, a lower flow flowing inside a lower flow passage X and an upper flow flowing inside an upper flow passage Y are generated. Streamlining walls 21, 22, 26 for streamlining the lower flow so as to make it flow toward an intake valve opening part region Z at the time of opening of an intake valve 6 are formed on an umbrella part back face 6b of the intake valve 6. The lower flow flows into the peripheral direction of a combustion chamber 3 from the intake valve opening part region Z at the time of opening of the intake valve 6 so as to generate a swirl, and the upper flow passes through a spiral part 7 and flows into the combustion chamber 3. <P>COPYRIGHT: (C)2008,JPO&INPIT

Description

本発明は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.

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、下層流は吸気弁開弁時に吸気弁開口部領域に向け流れた後に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して燃焼室内にスワールを発生させ、上層流は吸気弁開弁時に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し、吸気弁開弁時に下層流を吸気弁開口部領域に向かうよう整流させるために下層流の流れ方向に真直ぐに延びる整流壁を吸気弁のかさ部背面上に形成している。   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. A lower flow that flows and an upper flow that flows above the intake air inflow passage portion are generated, and the lower flow flows toward the intake valve opening region when the intake valve is opened, and then enters the combustion chamber from the intake valve opening region to the combustion chamber. Flowing in the peripheral direction to generate swirl in the combustion chamber, the upper layer flow swirls in the spiral when the intake valve is opened, then dispersed from the entire intake valve opening and flows into the combustion chamber, and the lower layer flow when the intake valve is opened In order to rectify the flow toward the intake valve opening region, a rectifying wall extending straight in the flow direction of the lower layer flow is formed on the back surface of the hood portion of the intake valve.

下層流路内を流れる下層流によって強力な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 strong swirl is generated by the lower flow flowing in the lower flow path, 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狭ばまりつつ下降し、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狭くなる。   As can be seen from FIGS. 3A to 3C and FIG. 5, the first upper wall surface 14a descends toward the spiral portion 7 with the width gradually narrowing, 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 becomes narrower gradually toward

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。図6(A)に図5の下層流路Xに関連する部分のみを取出した場合を示し、図6(B)に図5の上層流路Yに関連する部分のみを取出した場合を示す。   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. FIG. 6A shows a case where only a portion related to the lower layer flow path X of FIG. 5 is taken out, and FIG. 6B shows a case where only a portion related to the upper layer flow path Y of FIG. 5 is taken out.

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、図5および図6(A)においてZで示されている。
この吸気弁開口部領域Zは図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。本発明では図5および図6(A)からわかるように第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は下層流路Xが吸気弁開口部領域Zに向けてまっすぐに延びるように構成されている。
This intake valve opening region is indicated by Z in FIGS. 4, 5 and 6A.
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. In the present invention, as can be seen from FIG. 5 and FIG. 6A, the lower portion of the first side wall surface 12, the second side wall surface 13, the second upper wall surface 14b and the bottom wall surface 15 are provided by the lower flow path X. It is configured to extend straight toward the opening region Z.

このように下層流路Xが吸気弁開口部領域Zに向けてまっすぐに延びるように第2の上壁面10は図2に示される如く平面Kに対し第2の上壁面10と反対側に位置する吸気弁開口部19の上端縁に向けて延びている。このように下層流路Xを形成すると下層流路X内を流れる下層流は吸気弁6の開弁時に下層流路X内をまっすぐに進んで吸気弁開口部領域Zに進む。   In this way, the second upper wall surface 10 is positioned opposite to the second upper wall surface 10 with respect to the plane K as shown in FIG. 2 so that the lower layer flow path X extends straight toward the intake valve opening region Z. It extends toward the upper edge of the intake valve opening 19. When the lower layer flow path X is formed in this way, the lower layer flow flowing in the lower layer flow path X advances straight through the lower layer flow path X to the intake valve opening region Z when the intake valve 6 is opened.

さて、本発明では吸気弁6の開弁時に下層流を吸気弁開口部領域Zに向かうよう整流させるために下層流の流れ方向に真直ぐに延びる整流壁を吸気弁6のかさ部背面6b上に形成するようにしている。例えば図1から図3に示される実施例では吸気弁6のかさ部背面6b上に凹溝20が形成されており、この凹溝20の壁面が上述の整流壁を形成している。   In the present invention, in order to rectify the lower flow toward the intake valve opening region Z when the intake valve 6 is opened, a rectifying wall that extends straight in the flow direction of the lower flow is formed on the back surface 6b of the intake valve 6. Try to form. For example, in the embodiment shown in FIGS. 1 to 3, a concave groove 20 is formed on the back surface 6 b of the intake valve 6, and the wall surface of the concave groove 20 forms the aforementioned rectifying wall.

即ち、もう少し具体的に言うと、この凹溝20はシリンダ軸線Oと反対側のかさ部背面6b上において平面K(図4)よりも吸入空気流入通路部8側から平面Kよりも吸気弁開口部領域Z側まで延びており、この凹溝20は吸気弁6の軸線方向に延びる垂直壁21とこの垂直壁21から直角方向に延びる底壁22とを有していて、これら垂直壁21および底壁22が上述の整流壁を形成している。   That is, more specifically, the concave groove 20 is formed on the bevel back surface 6b opposite to the cylinder axis O from the intake air inflow passage 8 side rather than the plane K (FIG. 4). The groove 20 has a vertical wall 21 extending in the axial direction of the intake valve 6 and a bottom wall 22 extending perpendicularly from the vertical wall 21, and the vertical wall 21 and The bottom wall 22 forms the aforementioned rectifying wall.

更にこの実施例ではこの垂直壁21は吸気弁6の弁軸6aの外周面に沿って延びており、底壁22は吸入空気流入通路部8から吸気弁開口部領域Zに向けて次第に下降するよう傾斜している。   Further, in this embodiment, the vertical wall 21 extends along the outer peripheral surface of the valve shaft 6 a of the intake valve 6, and the bottom wall 22 gradually descends from the intake air inflow passage portion 8 toward the intake valve opening region Z. It is so inclined.

これら垂直壁21および底壁22のような整流壁を吸気弁6のかさ部背面上に形成すると下層流路X内を流れる下層流は、吸気弁6の開弁時に下層流路X内をまっすぐに進んだ後、この整流壁によって吸気弁開口部領域Zに向かうよう整流される。その結果、下層流路X内を流れる下層流全体が吸気弁開口部領域Zに向けて流れる。次いでこの下層流は図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 the flow straightening walls such as the vertical wall 21 and the bottom wall 22 are formed on the back surface of the umbrella portion of the intake valve 6, the lower layer flow flowing in the lower layer flow path X is straight in the lower layer flow path X when the intake valve 6 is opened. Then, the air is rectified toward the intake valve opening region Z by the rectifying wall. As a result, the entire lower layer flow flowing in the lower layer flow path X flows toward the intake valve opening region Z. Next, this lower flow flows from the intake valve opening region Z into the combustion chamber 3 toward the periphery of the combustion chamber 3 as indicated by an arrow S in FIG. A powerful swirl is generated.

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、強力なスワールを発生させるためには本発明におけるように下層流全体が吸気弁開口部領域Zに向かうように下層流を整流壁により整流させて燃焼室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. In other words, in order to generate a strong swirl, as in the present invention, the lower flow is rectified by the rectifying wall so that the entire lower flow is directed to the intake valve opening region Z, and the strong suction toward the periphery of the combustion chamber 3 is performed. It is most effective to generate an air flow.

なお本発明では凹溝20を常に図1に示す位置に維持しておかなければならず、そのために吸気弁6に対して軸線回りの回転止めが施こされている。図1に示される実施例では図3(C)に示されるように吸気弁6の弁軸6aの摺動孔23内に軸線方向に延びるスリット24が形成されており、弁軸6a内に圧入された回止めピン25がスリット24内に遊嵌せしめられている。   In the present invention, the concave groove 20 must always be maintained at the position shown in FIG. 1, and for this purpose, the intake valve 6 is prevented from rotating about its axis. In the embodiment shown in FIG. 1, as shown in FIG. 3C, a slit 24 extending in the axial direction is formed in the sliding hole 23 of the valve shaft 6a of the intake valve 6, and press-fitted into the valve shaft 6a. The anti-rotation pin 25 is loosely fitted in the slit 24.

図7および図8に別の実施例を示す。
この実施例では吸気弁6のかさ部背面6b上に突出部26が形成されており、この突出部26の壁面が前述した整流壁を形成している。もう少し具体的に言うと、この実施例では突出壁26が吸気弁6のかさ部背面6b上から吸気弁6の軸線方向に延びる薄肉垂直平板からなり、更にこの突出壁26は吸気弁6の軸線に関して吸気弁開口部領域Z側のかさ部背面6b上に形成されている。
7 and 8 show another embodiment.
In this embodiment, a protrusion 26 is formed on the back surface 6b of the intake valve 6 and the wall surface of the protrusion 26 forms the aforementioned rectifying wall. More specifically, in this embodiment, the projecting wall 26 is formed of a thin vertical plate extending in the axial direction of the intake valve 6 from the back surface 6b of the intake valve 6, and the projecting wall 26 further includes the axis of the intake valve 6. Is formed on the back portion 6b of the umbrella portion on the intake valve opening region Z side.

この実施例でも下層流路X内を流れる下層流は、吸気弁6の開弁時に下層流路X内をまっすぐに進んだ後、この突出壁26によって吸気弁開口部領域Zに向かうよう整流される。その結果、下層流路X内を流れる下層流全体が吸気弁開口部領域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、斯くして燃焼室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。   In this embodiment as well, the lower layer flow flowing in the lower layer flow path X straightens through the lower layer flow path X when the intake valve 6 is opened, and is then rectified by the protruding wall 26 toward the intake valve opening region Z. The As a result, the entire lower-layer flow flowing in the lower-layer flow path X flows from the intake valve opening region Z into the combustion chamber 3 toward the periphery of the combustion chamber 3. A powerful swirl around is generated.

このように本発明では吸気ポート4内から燃焼室3内に燃焼室3の周辺方向に向けてまっすぐに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よって吸入空気量が増大せしめられる。斯くして高い充填効率を図りつつ強力なスワールを発生させることができる。   As described above, in the present invention, a strong swirl is generated in the combustion chamber 3 by the lower flow that flows straight into the combustion chamber 3 from the intake port 4 toward the periphery of the combustion chamber 3, and the swirl 7 The amount of intake air is increased by the upper layer flow that flows into the combustion chamber 3 after turning. Thus, 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. 下層流路Xおよび上層流路Yを示す図である。It is a figure which shows the lower layer flow path X and the upper layer flow path Y. 別の実施例を示す吸気ポートの平面図である。It is a top view of the intake port which shows another Example. 図7に示される吸気弁の斜視図である。FIG. 8 is a perspective view of the intake valve shown in FIG. 7.

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 凹溝
21 垂直壁
22 底壁
26 突出壁
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 concave groove 21 vertical wall 22 bottom wall 26 protruding wall X upper layer flow path Y lower flow path Z intake valve opening area

Claims (13)

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、該下層流は吸気弁開弁時に上記吸気弁開口部領域に向け流れた後に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して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し、吸気弁開弁時に該下層流を上記吸気弁開口部領域に向かうよう整流させるために該下層流の流れ方向に真直ぐに延びる整流壁を吸気弁のかさ部背面上に形成した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 the lower layer flow flows toward the intake valve opening region when the intake valve is opened and then enters the combustion chamber from the intake valve opening region to the periphery of the combustion chamber. The upper layer flow swirls in the vortex when the intake valve is opened and then dispersed from the entire intake valve opening and flows into the combustion chamber. An intake port of an internal combustion engine in which a rectifying wall extending straight in the flow direction of the lower flow is formed on the back surface of the hood portion of the intake valve in order to rectify the lower flow toward the intake valve opening region. 吸気弁のかさ部背面上に凹溝が形成されており、該凹溝の壁面が上記整流壁を形成している請求項1に記載の内燃機関の吸気ポート。   2. An intake port for an internal combustion engine according to claim 1, wherein a concave groove is formed on the back surface of the umbrella portion of the intake valve, and a wall surface of the concave groove forms the rectifying wall. 上記凹溝がシリンダ軸線と反対側の上記かさ部背面上において上記平面よりも吸入空気流入通路部側から上記平面よりも吸気弁開口部領域側まで延びている請求項2に記載の内燃機関の吸気ポート。   3. The internal combustion engine according to claim 2, wherein the concave groove extends from the intake air inflow passage portion side to the intake valve opening region side from the plane on the back surface of the bulk portion opposite to the cylinder axis. Intake port. 上記凹溝が吸気弁の軸線方向に延びる垂直壁と該垂直壁から直角方向に延びる底壁とを有し、これら垂直壁および底壁が上記整流壁を形成している請求項2に記載の内燃機関の吸気ポート。   The said recessed groove has the vertical wall extended in the axial direction of an intake valve, and the bottom wall extended at right angles from this vertical wall, These vertical wall and bottom wall form the said baffle wall. The intake port of the internal combustion engine. 上記垂直壁が吸気弁の弁軸の外周面に沿って延びている請求項4に記載の内燃機関の吸気ポート。   The intake port of the internal combustion engine according to claim 4, wherein the vertical wall extends along an outer peripheral surface of a valve shaft of the intake valve. 上記底壁が吸入空気流入通路部から吸気弁開口部領域に向けて次第に下降するよう傾斜している請求項4に記載の内燃機関の吸気ポート。   The intake port of the internal combustion engine according to claim 4, wherein the bottom wall is inclined so as to gradually descend from the intake air inflow passage portion toward the intake valve opening region. 吸気弁のかさ部背面上に突出部が形成されており、該突出部の壁面が上記整流壁を形成している請求項1に記載の内燃機関の吸気ポート。   2. An intake port for an internal combustion engine according to claim 1, wherein a protrusion is formed on the rear surface of the umbrella portion of the intake valve, and a wall surface of the protrusion forms the rectifying wall. 上記突出壁が吸気弁のかさ部背面上から吸気弁の軸線方向に延びる薄肉垂直平板からなる請求項7に記載の内燃機関の吸気ポート。   8. The intake port of an internal combustion engine according to claim 7, wherein the protruding wall is a thin vertical plate extending in the axial direction of the intake valve from above the back surface of the intake valve. 上記突出壁が吸気弁の軸線に関して吸気弁開口部領域側のかさ部背面上に形成されている請求項7に記載の内燃機関の吸気ポート。   The intake port of the internal combustion engine according to claim 7, wherein the protruding wall is formed on a back surface of the bevel portion on the intake valve opening region side with respect to the axis of the intake valve. 吸気弁に対して軸線回りの回転止めが施こされている請求項1に記載の内燃機関の吸気ポート。   The intake port of the internal combustion engine according to claim 1, wherein a rotation stop around an axis is provided to the intake valve. 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を該下層流路が上記吸気弁開口部領域に向けてまっすぐに延びるように構成した請求項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. 1 formed between the upper wall surfaces of the first side wall surface, the lower side wall surface, the second side wall surface, the second upper wall surface and the bottom wall surface of the lower channel toward the intake valve opening region. The intake port of the internal combustion engine according to claim 1, wherein the intake port is configured to extend straight. 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. 上記第2の上壁面は上記平面に対し該第2の上壁面と反対側に位置する吸気弁開口部の上端縁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。   2. The intake port of the internal combustion engine according to claim 1, wherein the second upper wall surface extends toward an upper end edge of an intake valve opening located on the opposite side to the second upper wall surface with respect to the plane.
JP2006127402A 2006-05-01 2006-05-01 Intake port of internal combustion engine Expired - Fee Related JP4650333B2 (en)

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Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS50153123A (en) * 1974-05-31 1975-12-09
JPS56142228U (en) * 1980-03-26 1981-10-27
JPS60128908U (en) * 1984-02-09 1985-08-29 中村 孝夫 fuel saving intake valve
JPH0252934U (en) * 1988-10-08 1990-04-17

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS50153123A (en) * 1974-05-31 1975-12-09
JPS56142228U (en) * 1980-03-26 1981-10-27
JPS60128908U (en) * 1984-02-09 1985-08-29 中村 孝夫 fuel saving intake valve
JPH0252934U (en) * 1988-10-08 1990-04-17

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