JPH0520564B2 - - Google Patents

Info

Publication number
JPH0520564B2
JPH0520564B2 JP58075430A JP7543083A JPH0520564B2 JP H0520564 B2 JPH0520564 B2 JP H0520564B2 JP 58075430 A JP58075430 A JP 58075430A JP 7543083 A JP7543083 A JP 7543083A JP H0520564 B2 JPH0520564 B2 JP H0520564B2
Authority
JP
Japan
Prior art keywords
intake
cylinder chamber
circumferential surface
valve
vortex
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
JP58075430A
Other languages
Japanese (ja)
Other versions
JPS59201929A (en
Inventor
Katsuhiko Sugyama
Hiromitsu Kawazoe
Yoshinori Idota
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Toyota Central R&D Labs Inc
Original Assignee
Toyota Central R&D Labs Inc
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Toyota Central R&D Labs Inc filed Critical Toyota Central R&D Labs Inc
Priority to JP58075430A priority Critical patent/JPS59201929A/en
Publication of JPS59201929A publication Critical patent/JPS59201929A/en
Publication of JPH0520564B2 publication Critical patent/JPH0520564B2/ja
Granted legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B31/00—Modifying induction systems for imparting a rotation to the charge in the cylinder
    • Y—GENERAL 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
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00—Road transport of goods or passengers
    • Y02T10/10—Internal combustion engine [ICE] based vehicles
    • Y02T10/12—Improving ICE efficiencies

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Cylinder Crankcases Of Internal Combustion Engines (AREA)

Description

【発明の詳細な説明】 本発明は、シリンダ室の端面にその中心から偏
芯した位置に吸気孔を開口し、吸気孔に吸気弁を
設けると共に吸気通路を接続した内燃機関の吸気
ポートに関する。
DETAILED DESCRIPTION OF THE INVENTION The present invention relates to an intake port for an internal combustion engine in which an intake hole is opened at a position eccentric from the center of an end face of a cylinder chamber, an intake valve is provided in the intake hole, and an intake passage is connected to the intake port.

本発明者は、特開昭59−180027号公報に開示さ
れているように、従前、この種の吸気ポートにお
いて、適度の安定した渦流を体積効率を低下させ
ずに生起させる目的で、吸気通路を、吸気孔に連
通して吸気弁を囲む通路端の渦流生起部とこの通
路端以外の導入部から構成し、吸気弁の弁軸周面
とこれに対面した渦流生起部の周面間の幅を、シ
リンダ室周面側の外側部分ではシリンダ室中心側
の内側部分より広くし、渦流生起部の幅広の外側
部分に導入部を接続し、吸気孔の開口面とこれに
対面した渦流生起部の天井間の高さを、弁軸の回
りに幅広の外側部分から幅狭の内側部分に至る間
に同一とし又は減少させ、その平均減少量を弁軸
の回りに1度当り吸気孔の径の0.18%以内に設定
した内燃機関の吸気ポートを発明した。
As disclosed in Japanese Unexamined Patent Publication No. 59-180027, the present inventor has previously developed an intake passage in this type of intake port for the purpose of generating a moderately stable vortex flow without reducing the volumetric efficiency. consists of a vortex generating part at the end of the passage that communicates with the intake hole and surrounds the intake valve, and an introduction part other than the end of the passage, and between the peripheral surface of the valve shaft of the intake valve and the peripheral surface of the vortex generating part facing it The width is made wider at the outer part on the cylinder chamber circumferential side than the inner part on the center side of the cylinder chamber, and the introduction part is connected to the wide outer part of the vortex generating part, and the vortex generating part facing the opening surface of the intake hole is made wider. The height between the ceilings of the parts is the same or decreases from the wide outer part to the narrow inner part around the valve stem, and the average decrease is equal to the height of the intake hole per degree around the valve stem. Invented an internal combustion engine intake port that is set within 0.18% of the diameter.

この従来の吸気ポートは、適度の安定した渦流
を体積効率を低下させずに生起させることができ
るが、生起する渦流のスワール比が十分に高いと
は言い難い。
Although this conventional intake port can generate a moderately stable vortex without reducing volumetric efficiency, it cannot be said that the swirl ratio of the vortex generated is sufficiently high.

本発明の目的は、上記のような従来の課題を解
決することである。
An object of the present invention is to solve the conventional problems as described above.

本発明は、シリンダ室の端面にその中心から偏
芯した位置に吸気孔を開口し、吸気孔に吸気弁を
設けると共に吸気通路を接続した内燃機関の吸気
ポートにおいて、 吸気通路を、吸気孔に連通して吸気弁を囲む通
路端の渦流生起部とこの通路端以外の導入部から
構成し、 渦流生起部の周面を吸気弁の弁軸の周面に対面
したほぼ円筒面状に形成し、 吸気弁の弁軸の周面とこれに対面した渦流生起
部の周面間の幅を、シリンダ室周面側の外側部分
ではシリンダ室中心側の内側部分より広くして、
弁軸の周りに外側部分から内側部分に至る間に
徐々に狭くし、 渦流生起部の外側部分の周面をシリンダ室の周
面にほぼ沿つて配置し、 渦流生起部の幅広の外側部分にその接線方向に
沿つてほぼ直線状の導入部を接続し、 吸気孔の開口面とこれに対面した渦流生起部の
天井間の高さを、弁軸の周りに幅広の外側部分か
ら幅狭の内側部分に至る間に同一とし又は減少さ
せ、その平均減少量を弁軸の回りに1度当り吸気
孔の径の0.18%以内に設定し、 シリンダ室の端面の中心と吸気孔の中心を結ぶ
線が複数個の直列に配置したシリンダ室の端面の
中心を結ぶ線に対してなす角度を70度以内に設定
し、 吸気通路を流れる吸気流の主流が導入部から渦
流生起部の外側部分の周面と吸気弁の弁軸の周面
の間に流入し、吸気孔を経てシリンダ室にその周
面の吸気孔近接部分の接線方向に沿つて流入し、
シリンダ室の周面に沿つて旋回する渦流となる構
成にしたことを特徴とする内燃機関の吸気ポート
である。
The present invention provides an intake port for an internal combustion engine in which an intake hole is opened at a position eccentric from the center of the end face of a cylinder chamber, an intake valve is provided in the intake hole, and the intake passage is connected to the intake port. It is composed of a vortex generation part at the end of the passage that communicates with the intake valve and an introduction part other than the end of the passage, and the circumferential surface of the vortex generation part is formed into a substantially cylindrical surface facing the circumference of the valve shaft of the intake valve. , the width between the circumferential surface of the valve shaft of the intake valve and the circumferential surface of the vortex generating portion facing the same is made wider at the outer part on the cylinder chamber circumferential side than in the inner part on the cylinder chamber center side,
It gradually narrows from the outer part to the inner part around the valve stem, and the circumferential surface of the outer part of the vortex generating part is arranged almost along the circumferential surface of the cylinder chamber, and the outer part of the vortex generating part is wide. Connect the almost linear introduction part along the tangential direction, and adjust the height between the opening surface of the intake hole and the ceiling of the vortex generation part facing this by connecting the wide outer part to the narrow part around the valve stem. It is the same or decreases while reaching the inner part, and the average decrease amount is set within 0.18% of the diameter of the intake hole per degree around the valve stem, and the center of the end face of the cylinder chamber and the center of the intake hole are connected. The angle that the line makes with the line connecting the centers of the end faces of multiple cylinder chambers arranged in series is set within 70 degrees, so that the main flow of the intake air flowing through the intake passage is directed from the introduction part to the outer part of the vortex generation part. Flows between the circumferential surface and the circumferential surface of the valve shaft of the intake valve, passes through the intake hole, and flows into the cylinder chamber along the tangential direction of the portion of the circumferential surface adjacent to the intake hole,
This is an intake port for an internal combustion engine, characterized by having a configuration in which a vortex flow swirls along the circumferential surface of a cylinder chamber.

本発明の内燃機関の吸気ポートにおいては、吸
気通路を流れる吸気流の主流が導入部から渦流生
起部の外側部分の周面と吸気弁の弁軸の周面の間
に流入し、吸気孔を経てシリンダ室にその周面の
吸気孔近接部分の接線方向に沿つて流入し、シリ
ンダ室の周面に沿つて旋回する渦流となる。
In the intake port of the internal combustion engine of the present invention, the main flow of the intake air flowing through the intake passage flows from the introduction part between the peripheral surface of the outer part of the vortex generating part and the peripheral surface of the valve shaft of the intake valve, and flows through the intake hole. The fluid then flows into the cylinder chamber along the tangential direction of the portion of the circumferential surface of the cylinder chamber adjacent to the intake hole, forming a vortex flow that swirls along the circumferential surface of the cylinder chamber.

本発明の内燃機関の吸気ポートにおいては、後
記の実験結果から明らかなように、従来の吸気ポ
ートに比較して、スワール比の高い渦流を体積効
率を低下させずに生起させることができる。
As is clear from the experimental results described later, in the intake port of the internal combustion engine of the present invention, a vortex flow with a higher swirl ratio can be generated without reducing the volumetric efficiency compared to the conventional intake port.

次に、本発明の実施例について説明する。 Next, examples of the present invention will be described.

本例の内燃機関の吸気ポートは、第1図と第2
図に示すように、シリンダ室11の円形端面にそ
の中心から周辺側に偏芯した位置に円形の吸気孔
12を開口し、吸気孔12にポペツト弁の吸気弁
13を設けると共に吸気通路15を接続し、吸気
通路15を、吸気孔12に連通して吸気弁13を
囲む通路端の渦流生起部16とこの通路端以外の
導入部19から構成し、渦流生起部16の周面を
吸気弁の弁軸14の周面に対面した2枚の円筒面
を滑らかに接続してほぼ円筒面状に形成し、弁軸
14の周面とこれに対面した渦流生起部16の周
面間の幅を、シリンダ室11周面側の外側部分1
7ではシリンダ室中心側の内側部分18より広く
して、弁軸14の回りに外側部分17から内側部
分18に至る間に徐々に狭くし、外側部分17の
周面をシリンダ室11の周面にほぼ沿つて配置
し、渦流生起部16の幅広の外側部分17にその
接線方向に沿つてほぼ直線状の導入部19を接続
し、吸気孔12の開口面とこれに対面した渦流生
起部16の天井間の高さを、弁軸14の回りに幅
広の外側部分17から幅狭の内側部分18に至る
間に同一とし又は徐々に減少させ、その減少量を
弁軸14の回りに1度当り吸気孔の径dの0.18%
以内に、具体的には0.06%に設定し、第3図に示
すように、吸気孔12の中心とシリンダ室11の
端面の中心を結ぶ線が複数個の直列に配置したシ
リンダ室の端面の中心を結ぶ線に対してなす角度
θを70度以内に、具体的には6度に設定し、ま
た、第2図に示すように、吸気孔12の中心とシ
リンダ室11の端面の中心間の距離rをシリンダ
室11の径Dの%以内に、具体的には25%に設定
している。
The intake ports of the internal combustion engine in this example are shown in Figures 1 and 2.
As shown in the figure, a circular intake hole 12 is opened in the circular end face of the cylinder chamber 11 at a position eccentric from the center to the peripheral side, and an intake valve 13 of a poppet valve is provided in the intake hole 12, and an intake passage 15 is provided. The intake passage 15 is composed of a vortex generation part 16 at the end of the passage that communicates with the intake hole 12 and surrounds the intake valve 13, and an introduction part 19 at the other end of the passage, and the peripheral surface of the vortex generation part 16 is connected to the intake valve 13. Two cylindrical surfaces facing the circumferential surface of the valve stem 14 are smoothly connected to form a substantially cylindrical surface, and the width between the circumferential surface of the valve stem 14 and the circumferential surface of the vortex generating portion 16 facing this is determined. , the outer part 1 on the circumferential side of the cylinder chamber 11
7, it is wider than the inner part 18 on the center side of the cylinder chamber, and gradually narrows from the outer part 17 to the inner part 18 around the valve shaft 14, so that the circumferential surface of the outer part 17 is the same as the circumferential surface of the cylinder chamber 11. A substantially straight introduction part 19 is connected to the wide outer part 17 of the vortex generating part 16 along the tangential direction thereof, and the vortex generating part 16 facing the opening surface of the intake hole 12 is connected to the wide outer part 17 of the vortex generating part 16. The height between the ceilings is the same or gradually decreases around the valve stem 14 from the wide outer part 17 to the narrow inner part 18, and the amount of decrease is made once around the valve stem 14. 0.18% of the intake hole diameter d
As shown in FIG. 3, the line connecting the center of the intake hole 12 and the center of the end surface of the cylinder chamber 11 is set within The angle θ with respect to the line connecting the centers is set within 70 degrees, specifically 6 degrees, and as shown in FIG. The distance r is set within a percentage of the diameter D of the cylinder chamber 11, specifically, 25%.

この吸気ポートにおいては、吸気通路15を流
れる吸気流は、導入部19から渦流生起部16に
流入し、吸気孔12を経てシリンダ室11に流入
し、また、吸気流の主流は、導入部19の軸芯位
置から渦流生起部の外側部分17の周面と弁軸1
4の周面間の中間位置に流入し、吸気孔12を経
てシリンダ室11にその周面の吸気孔近接部分の
接線方向に沿つて流入し、シリンダ室11の周面
に沿つて旋回する渦流となる。
In this intake port, the intake air flowing through the intake passage 15 flows from the introduction part 19 into the vortex generating part 16 and flows into the cylinder chamber 11 via the intake hole 12. from the axial center position to the peripheral surface of the outer portion 17 of the vortex generating portion
4, flows into the cylinder chamber 11 through the intake hole 12 along the tangential direction of the portion of the circumference near the intake hole, and swirls along the circumferential surface of the cylinder chamber 11. becomes.

本例の吸気ポートにおいて、吸気孔12の中心
とシリンダ室11の端面の中心を結ぶ線が複数個
の直列に配置したシリンダ室11の端面の中心を
結ぶ線に対してなす角度θを各値に設定し、その
各値についてそれぞれシリンダ室11に生起する
渦流の強さ即ちスワール比SRとシリンダ室11
の体積効率VEを求めてみたところ、第4図の線
図に示すような実験結果を得た。なお、同線図に
おいては、上記の配置角度θの符号は、吸気孔1
2の中心が複数個の直列に配置したシリンダ室1
1の端面の中心を結ぶ線に対し吸気通路の導入部
19側に位置するときにプラスとし、導入部19
と反対側に位置するときにマイナスとしている。
同線図の上部から明らかなように、スワール比
SRは、配置角度θが70度を越すと、急激に減少
し、45度以内において非常に高い値となる。体積
効率VEは、同線図の下部から明らかなように、
配置角度θの大小によつて大きく変化しない。従
つて、配置角度θを70度以内に設定すると、体積
効率を低下させずに、スワール比を高くすること
ができ、配置角度θを45度以内に設定すると、体
積効率を低下させずにスワール比を非常に高くす
ることができる。
In the intake port of this example, each value is the angle θ that a line connecting the center of the intake hole 12 and the center of the end surface of the cylinder chamber 11 makes with a line connecting the centers of the end surfaces of a plurality of cylinder chambers 11 arranged in series. and for each value, the strength of the vortex generated in the cylinder chamber 11, that is, the swirl ratio SR and the cylinder chamber 11.
When we calculated the volumetric efficiency VE, we obtained experimental results as shown in the diagram in Figure 4. In addition, in the same diagram, the sign of the above arrangement angle θ is the same as that of the intake hole 1.
The center of 2 is a cylinder chamber 1 in which a plurality of cylinder chambers are arranged in series.
1 is positive when it is located on the introduction part 19 side of the intake passage with respect to the line connecting the centers of the end faces of
It is considered negative when it is located on the opposite side.
As is clear from the top of the diagram, the swirl ratio
SR decreases rapidly when the arrangement angle θ exceeds 70 degrees, and reaches a very high value within 45 degrees. As is clear from the bottom of the diagram, the volumetric efficiency VE is
It does not change greatly depending on the size of the arrangement angle θ. Therefore, if the arrangement angle θ is set within 70 degrees, the swirl ratio can be increased without reducing the volumetric efficiency, and if the arrangement angle θ is set within 45 degrees, the swirl ratio can be increased without reducing the volumetric efficiency. The ratio can be very high.

また、本例の吸気ポートにおいて、吸気孔12
の中心とシリンダ室11の端面の中心間の距離r
をシリンダ室11の径Dに対して各値に設定し、
その各値r/Dについてそれぞれスワール比SR
と体積効率VEを求めてみたところ、第5図の線
図に示すような実験結果を得た。同線図の上部か
ら明らかなように、スワール比SRは、上記の値
即ち無次元配置距離r/Dが0.3を越すと、急激
に減少し、0.15以上で0.26以下において非常に高
い値となる。体積効率VEは、同線図の下部から
明らかなように、無次元配置距離r/Dの大小に
よつて大きく変化しない。従つて、無次元配置距
離r/Dを30%以内に設定すると、体積効率を低
下させずに、スワール比を高くすることができ、
無次元配置距離r/Dを15%以上で26%以下に設
定すると、体積効率を低下させずに、スワール比
を非常に高くすることができる。
Further, in the intake port of this example, the intake hole 12
The distance r between the center of and the center of the end face of the cylinder chamber 11
is set to each value for the diameter D of the cylinder chamber 11,
Swirl ratio SR for each value r/D
When we calculated the volumetric efficiency VE, we obtained experimental results as shown in the diagram in Figure 5. As is clear from the upper part of the diagram, the swirl ratio SR decreases rapidly when the above value, that is, the dimensionless arrangement distance r/D exceeds 0.3, and becomes a very high value when it is 0.15 or more and 0.26 or less. . As is clear from the lower part of the diagram, the volumetric efficiency VE does not change significantly depending on the dimensionless arrangement distance r/D. Therefore, if the dimensionless arrangement distance r/D is set within 30%, the swirl ratio can be increased without reducing the volumetric efficiency.
When the dimensionless arrangement distance r/D is set to 15% or more and 26% or less, the swirl ratio can be made very high without reducing the volumetric efficiency.

【図面の簡単な説明】[Brief explanation of the drawing]

第1図は本発明の実施例の吸気ポートの略示斜
斜図、第2図は同吸気ポートの平面図、第3図は
同吸気ポートの配列状態を示す略示平面図であ
り、第4図は同吸気ポートにおける吸気孔の配置
角度とスワール比又は体積効率の関係を示す線
図、第5図は同吸気ポートにおける吸気孔の配置
距離とスワール比又は体積効率の関係を示す線図
である。 11……シリンダ室、12……吸気孔、13…
…吸気弁、14……弁軸、15……吸気通路、1
6……渦流生起部、17……外側部分、18……
内側部分、19……導入部、θ……吸気孔の配置
角度、r……吸気孔の配置距離、D……シリンダ
室の径。
FIG. 1 is a schematic perspective view of an intake port according to an embodiment of the present invention, FIG. 2 is a plan view of the intake port, and FIG. 3 is a schematic plan view showing the arrangement of the intake ports. Figure 4 is a diagram showing the relationship between the intake hole arrangement angle and swirl ratio or volumetric efficiency at the same intake port, and Figure 5 is a diagram showing the relationship between the intake hole arrangement distance and the swirl ratio or volumetric efficiency at the same intake port. It is. 11...Cylinder chamber, 12...Intake hole, 13...
...Intake valve, 14...Valve stem, 15...Intake passage, 1
6... Vortex generating part, 17... Outer part, 18...
Inner part, 19...Introduction part, θ...Arrangement angle of intake hole, r...Arrangement distance of intake hole, D...Diameter of cylinder chamber.

Claims (1)

【特許請求の範囲】 1 シリンダ室の端面にその中心から偏芯した位
置に吸気孔を開口し、吸気孔に吸気弁を設けると
共に吸気通路を接続した内燃機関の吸気ポートに
おいて、 吸気通路を、吸気孔に連通して吸気弁を囲む通
路端の渦流生起部とこの通路端以外の導入部から
構成し、 渦流生起部の周面を吸気弁の弁軸の周面に対面
したほぼ円筒面状に形成し、 吸気弁の弁軸の周面とこれに対面した渦流生起
部の周面間の幅を、シリンダ室周面側の外側部分
ではシリンダ室中心側の内側部分より広くして、
弁軸の回りに外側部分から内側部分に至る間に
徐々に狭くし、 渦流生起部の外側部分の周面をシリンダ室の周
面にほぼ沿つて配置し、 渦流生起部の幅広の外側部分にその接線方向に
沿つてほぼ直線状の導入部を接続し、 吸気孔の開口面とこれに対面した渦流生起部の
天井間の高さを、弁軸の回りに幅広の外側部分か
ら幅狭の内側部分に至る間に同一とし又は減少さ
せ、その平均減少量を弁軸の回りに1度当り吸気
孔の径の0.18%以内に設定し、 シリンダ室の端面の中心と吸気孔の中心を結ぶ
線が複数個の直列に配置したシリンダ室の端面の
中心を結ぶ線に対してなす角度を70度以内に設定
し、 吸気通路を流れる吸気流の主流が導入部から渦
流生起部の外側部分の周面と吸気弁の弁軸の周面
の間に流入し、吸気孔を経てシリンダ室にその周
面の吸気孔近接部分の接線方向に沿つて流入し、
シリンダ室の周面に沿つて旋回する渦流となる構
成にしたことを特徴とする内燃機関の吸気ポー
ト。 2 前記の角度を45度以内に設定したことを特徴
とする特許請求の範囲第1項記載の内燃機関の吸
気ポート。 3 シリンダ室の端面の中心と吸気孔の中心間の
距離をシリンダ室の径の30%以内に設定したこと
を特徴とする特許請求の範囲第1項又は第2項記
載の内燃機関の吸気ポート。
[Scope of Claims] 1. In an intake port of an internal combustion engine in which an intake hole is opened in an end face of a cylinder chamber at a position eccentric from the center thereof, an intake valve is provided in the intake hole, and the intake passage is connected to the intake port, the intake passage is connected to the intake port. It consists of a vortex-generating part at the end of the passage that communicates with the intake hole and surrounds the intake valve, and an introduction part other than the end of the passage, and the circumferential surface of the vortex-generating part is a substantially cylindrical surface facing the circumferential surface of the valve shaft of the intake valve. The width between the circumferential surface of the valve shaft of the intake valve and the circumferential surface of the vortex generating portion facing the intake valve is made wider in the outer portion on the cylinder chamber circumferential side than in the inner portion on the cylinder chamber center side,
It gradually narrows from the outer part to the inner part around the valve shaft, and the circumferential surface of the outer part of the vortex generating part is arranged almost along the circumferential surface of the cylinder chamber, and the outer part of the vortex generating part is wide. Connect the almost linear introduction part along the tangential direction, and adjust the height between the opening surface of the intake hole and the ceiling of the vortex generation part facing this by connecting the wide outer part to the narrow part around the valve stem. It is the same or decreases while reaching the inner part, and the average decrease amount is set within 0.18% of the diameter of the intake hole per degree around the valve stem, and the center of the end face of the cylinder chamber and the center of the intake hole are connected. The angle that the line makes with the line connecting the centers of the end faces of multiple cylinder chambers arranged in series is set within 70 degrees, so that the main flow of the intake air flowing through the intake passage is directed from the introduction part to the outer part of the vortex generation part. Flows between the circumferential surface and the circumferential surface of the valve shaft of the intake valve, passes through the intake hole, and flows into the cylinder chamber along the tangential direction of the portion of the circumferential surface adjacent to the intake hole,
An intake port for an internal combustion engine, characterized in that the intake port is configured to form a vortex flow that swirls along the circumferential surface of a cylinder chamber. 2. An intake port for an internal combustion engine according to claim 1, wherein the angle is set within 45 degrees. 3. The intake port of an internal combustion engine according to claim 1 or 2, characterized in that the distance between the center of the end face of the cylinder chamber and the center of the intake hole is set within 30% of the diameter of the cylinder chamber. .
JP58075430A 1983-04-28 1983-04-28 internal combustion engine intake port Granted JPS59201929A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP58075430A JPS59201929A (en) 1983-04-28 1983-04-28 internal combustion engine intake port

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP58075430A JPS59201929A (en) 1983-04-28 1983-04-28 internal combustion engine intake port

Publications (2)

Publication Number Publication Date
JPS59201929A JPS59201929A (en) 1984-11-15
JPH0520564B2 true JPH0520564B2 (en) 1993-03-19

Family

ID=13575991

Family Applications (1)

Application Number Title Priority Date Filing Date
JP58075430A Granted JPS59201929A (en) 1983-04-28 1983-04-28 internal combustion engine intake port

Country Status (1)

Country Link
JP (1) JPS59201929A (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2558621Y2 (en) * 1993-03-10 1997-12-24 株式会社椿本チエイン Article unloading device for first-in first-out article storage shelf device

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS6030423Y2 (en) * 1977-06-10 1985-09-12 ヤンマーディーゼル株式会社 internal combustion engine intake port

Also Published As

Publication number Publication date
JPS59201929A (en) 1984-11-15

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