JPS59213924A - Suction port for internal-combustion engine - Google Patents

Suction port for internal-combustion engine

Info

Publication number
JPS59213924A
JPS59213924A JP58088222A JP8822283A JPS59213924A JP S59213924 A JPS59213924 A JP S59213924A JP 58088222 A JP58088222 A JP 58088222A JP 8822283 A JP8822283 A JP 8822283A JP S59213924 A JPS59213924 A JP S59213924A
Authority
JP
Japan
Prior art keywords
intake
cylinder chamber
valve
peripheral surface
suction port
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.)
Pending
Application number
JP58088222A
Other languages
Japanese (ja)
Inventor
Katsuhiko Sugiyama
勝彦 杉山
Hiromitsu Kawazoe
川添 博光
Yoshinori Idota
芳典 井戸田
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 JP58088222A priority Critical patent/JPS59213924A/en
Publication of JPS59213924A publication Critical patent/JPS59213924A/en
Pending legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B31/00Modifying induction systems for imparting a rotation to the charge in the cylinder
    • 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

Landscapes

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

Abstract

PURPOSE:To increase a swirl ratio, by specifying a stepped portion formed between a peripheral surface of a vortex flow generating portion in a suction passage and an opening edge of a suction port. CONSTITUTION:A peripheral surface and an inlet of a vortex flow generating portion 16 are arcuately rounded. A radius of curvature R1 at an outlet of a stepped portion 21 formed near a peripheral surface of a cylinder chamber 11 is larger than a radius of curvature R2 at an inlet of the stepped portion 21 formed at a distant from the peripheral surface of the cylinder chamber 11, so that the stepped portion 21 may be smoothly shaped in such a manner that the outlet is less angulated than the inlet. A reduced amount of a height between an opening surface of a suction port 12 and a top wall of the vortex flow generating portion 16 is set to be within 0.18% of a diameter (d) of the suction port per one degree about a valve shaft 14. A suction air flow in a suction passage 15 is induced through an induction portion 19, the vortex flow generating portion 16 and the suction port 12 to the cylinder chamber 11. A main flow of the suction air is induced from an axial position of the induction portion 19 to an intermediate position between a peripheral surface of an outside part 17 of the vortex flow generating portion and a peripheral surface of the valve shaft 14. Then, it is induced through the suction port 12 to the cylinder chamber 11, where forming a vortex flow along the periphery of the cylinder chamber 11.

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むから偏芯した位
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 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 an intake passage is connected to the intake port. .

本発明者は、従前、Cの坤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溝成し、
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、シリンダ室局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、その平均減少鰍を弁軸の回りに7度当り吸気孔の径
の(2/J%以内に設定した内燃機関の吸気ポートを発
明した。
Previously, the inventor of the present invention has constructed an intake passage at the end of the passage that communicates with the intake hole and surrounds the intake valve in order to generate a moderately stable vortex flow without reducing the volumetric efficiency in the intake port of C. A groove is formed from the vortex generation part and the introduction part other than the end of this passage,
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 at the outer portion on the side facing the cylinder chamber than the inner portion on the center side of the cylinder chamber. and the height between the opening surface of the intake hole and the ceiling of the vortex generating section facing the same from the wide outer part to the narrow inner part around the valve stem, or Invented an intake port for an internal combustion engine in which the average reduction is set within 2/J% of the intake hole diameter per 7 degrees around the valve shaft.

本発明の目的は、上記の従前の発明を改良し、スワール
比の高い内燃機関の吸気ポートを提供するCとである。
An object of the present invention is to improve the above-mentioned previous invention and provide an intake port for an internal combustion engine with a high swirl ratio.

本発明は、スワール比を高めるため、吸気通路の渦流生
起部の周面と@気孔の開口縁間に形成される段部につい
て工夫をしたものである。
In the present invention, in order to increase the swirl ratio, the step portion formed between the circumferential surface of the vortex generating portion of the intake passage and the opening edge of the pore is devised.

fillち、本発明は、上記の従前の発明において、吸
気通路の渦流生起部の周面と吸気孔の開口縁間の段部を
シリノダ室周面に近い部分では遠い部分より角立たぬよ
り円滑にしたことを特徴とする内燃機関の吸気ポートで
ある。
In the above-mentioned conventional invention, the present invention is such that the stepped portion between the circumferential surface of the vortex-generating portion of the intake passage and the opening edge of the intake hole is made smoother in a portion closer to the circumferential surface of the cylinder chamber than in a portion farther away. This is an intake port for an internal combustion engine that is characterized by a

こ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、スワール比のW′IIい渦流を生起させるこ
とができる、 次に、本発明の実施例について説明する1、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αυの円形端面にその中IL>から周辺111
11に偏芯した位置に円形の吸気孔(6)を開口し、吸
気孔@にポペット弁の吸気弁(喝を設けると共に吸気通
路a9を接続し、吸気通路(10を、吸気孔o乃に連通
して吸気弁0イを囲む通路端の渦流生起部Uttと00
通通路端外の導入部OX4から構成し、渦流生起部(田
の周面を吸気弁の弁軸0勺の周面に対面した1枚の円筒
面を滑うかに接続して形成し、弁軸0美の周面とこれに
対面した渦流生起部(埒の周面間の幅を、シリンダ室(
1υ周面側の外側部分0力ではシリンダ室中心側の内側
部分囮より広くして、弁tiIlll(141の回りに
外(III fa分Uカから内側部分(l印に至る間に
徐々に狭くし、渦流生起部(](itの幅広の外(1f
1部分Q7)にその接線方向に沿って導入部四を接続し
、吸気孔(功の開口面とこれに対16Jシた渦流生起M
ls (1(jの天井間の高さを、弁軸α匂の回りに幅
広の外側部分Q7)から幅狭の内11111部分θ〜に
至る間に同一とし又は徐々に減少させ、その減少景を弁
軸04)の回V&こ/#:当り吸気孔の径dの07g%
以内に、具体的には006%に設定し、第3図乃至第5
図に示すように、渦流生起部OQの周面と吸気孔u4の
開口縁間に形成された段部c2Dの出隅部と入隅部をそ
れぞれ円弧状に丸め、段部ンυの出隅部の曲率半径孔1
と大隅部の曲率半径R2をそれぞれシリンダ室Ov局面
に近い部分では遠い部分より大きくして、段部c2υを
シリンダ室0υ周而に近い部分では遠い部分より角立た
ぬよう円滑にしており、具体的には、上記の曲率半径孔
、と几、を、第4図の線図に実線で示すように、角度γ
に対して変化させている。
In this intake port, as is clear from the experimental results described later, it is possible to generate a vortex flow with a swirl ratio of W'II. As shown in FIGS. 1 and 2, the intake port is located on the circular end surface of the cylinder chamber αυ from the inside IL
Open a circular intake hole (6) at a position eccentric to 11, provide an intake valve (opener) of a poppet valve in the intake hole @ and connect the intake passage a9, and connect the intake passage (10 to the intake hole o). The vortex generating portion Utt and 00 at the end of the passage that communicate with each other and surround the intake valve 0i
It consists of an introductory part OX4 outside the end of the passageway, and a vortex generating part (formed by slidingly connecting the circumferential surface of the cylindrical surface to a cylindrical surface facing the circumferential surface of the valve shaft of the intake valve, The cylinder chamber (
At 0 force, the outer part on the circumferential side of 1υ is wider than the inner part on the center side of the cylinder chamber, and the inner part (from the outside (III fa) around the valve tiIllll (141) to the inner part (l mark) is gradually narrowed. and the wide outside (1f
1 part Q7) along its tangential direction, and connect the intake hole (the opening surface of the part Q7) and the vortex generation M
ls (1 (the height between the ceilings of j is kept the same or gradually decreased from the wide outer part Q7 around the valve axis α) to the narrow inner 11111 part θ~, and the decreasing pattern is The times of the valve stem 04) V&ko/#: 07g% of the intake hole diameter d
Specifically, set it to 006%, and
As shown in the figure, the outer and inner corners of the stepped portion c2D formed between the circumferential surface of the vortex generating portion OQ and the opening edge of the intake hole u4 are rounded into arc shapes, and the outer corner of the stepped portion nυ is rounded. radius of curvature of hole 1
and the radius of curvature R2 of the large corner are made larger in the part near the cylinder chamber Ov surface than in the part far away, and the stepped part c2υ is made smooth so that the part near the circumference of the cylinder chamber 0υ is less angular than the part far away. Specifically, the curvature radius of the hole, and the hole, as shown by the solid line in the diagram of
It is changing against.

角度γは、第2図に示すように、吸気弁の弁軸α→の回
りにV−v線断面から吸気流の流れ方向に測った角度で
ある。
As shown in FIG. 2, the angle γ is an angle measured around the valve axis α→ of the intake valve from the V-V line cross section in the flow direction of the intake air flow.

この吸気ポートにおいては、吸気通路(旧を流れる吸気
流は、導入部01から渦流生起部(1(9に流入し、吸
気孔aのを経てシリンダ室Ql)に流入し、また、吸気
流の主流は、導入部OIO軸芯位置から渦流生起部の外
側部分α力の局面と弁軸(141の周面間の中間位置に
流入し、吸気孔04を経てシリンダ室01)にその局面
の吸気孔近接部分の接線方向に沿って流入し、シリンダ
室(lυの周面に沿って旋回する渦流となる。
In this intake port, the intake flow flowing through the intake passage (old) flows from the introduction part 01 into the vortex generation part (1 (9), passes through the intake hole a, and into the cylinder chamber Ql), and the intake flow The main flow flows from the introduction part OIO axis position to the intermediate position between the outer part of the vortex generating part α force and the circumferential surface of the valve shaft (141), and passes through the intake hole 04 to the cylinder chamber 01. It flows in along the tangential direction of the portion near the hole and becomes a vortex flow that swirls along the circumferential surface of the cylinder chamber (lυ).

本例の吸気ポートにおいては、吸気通路碩9を流通する
吸気流の流量Qを6値に設足し、その6値についてそれ
ぞれシリンダ室aυに生起する渦流の強さ即ちスワール
比SRを求めてみたところ、第7図の線図に実線で示す
ような実験結果を得た。
In the intake port of this example, the flow rate Q of the intake air flowing through the intake passage 9 was set to 6 values, and the strength of the vortex generated in the cylinder chamber aυ, that is, the swirl ratio SR, was determined for each of the 6 values. However, we obtained experimental results as shown by the solid line in the diagram of FIG.

また、比較のため、段部(21)の出隅部の曲率半径用
と入隅部の曲率半径ル2′f:、第6図の線図に破線で
示すように変化させた従来の場合についても同様に吸気
通路(1Gの流量Qに対するスワール比Sliを求めて
みたところ、第7図の線図に破線で示すよりな実験結果
を得た。
Also, for comparison, the radius of curvature of the protruding corner of the stepped portion (21) and the radius of curvature of the inlet corner 2'f: are changed as shown by broken lines in the diagram of FIG. 6 in the conventional case. When we similarly determined the swirl ratio Sli for the flow rate Q of the intake passage (1G), we obtained experimental results shown by the broken line in the diagram of FIG.

これらの実験結果から明らかなように、本例の吸気ポー
トにおいては、スワール比の高い渦流を生起させること
ができる。
As is clear from these experimental results, the intake port of this example can generate a vortex flow with a high swirl ratio.

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

第1図は本発明の実施例の吸気ポートの略示斜視図、第
2図は同吸気ポートの横断平面図、第3図は第2図のト
」線断面の一部省略図、第グ図は第2図のIV−IV線
断面の一部省略図、第5図は第2図の■−v線断面の一
部省略図、第6図は同吸気ポートにおける段部の出隅部
と大隅部の各曲率半径の変化の様子を示す線図、第7図
は同吸気ポートにおけるスワール比と吸気流尿の関係を
示す線図である。 11ニジリンダ室    12:吸気子113:吸気弁
      14:弁 軸15:吸気曲路     1
6:渦流生起部17:外fi11 f41i分    
 18:内側部分19:祷入部      21:段 
部第2図 ■ 第3図 第4図
1 is a schematic perspective view of an intake port according to an embodiment of the present invention, FIG. 2 is a cross-sectional plan view of the same intake port, and FIG. 3 is a partially omitted cross-sectional view taken along the line T in FIG. The figure is a partially omitted view of the cross section taken along the line IV-IV in Fig. 2, Fig. 5 is a partially omitted view of the cross section taken along the ■-v line of Fig. 2, and Fig. 6 is the protruding corner of the stepped portion of the same intake port. FIG. 7 is a diagram showing the relationship between the swirl ratio and the intake air flow at the same intake port. 11 Niji cylinder chamber 12: Intake element 113: Intake valve 14: Valve shaft 15: Intake curved path 1
6: Eddy current generating part 17: Outside fi11 f41i
18: Inner part 19: Praying part 21: Step
Figure 2 ■ Figure 3 Figure 4

Claims (1)

【特許請求の範囲】[Claims] 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、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+L>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(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
鍛を弁軸の回りに7度当り吸気孔の径のO/ざ%以内に
設定し、渦流生起部の周面と吸気孔の開口縁間の段部を
、シリンダ室局面に近い部分では遠い部分より角立たぬ
よう円滑にしたことを特徴とする内燃機関の吸気ポート
In the intake port of an internal combustion engine, in which an intake hole is opened at a position eccentric from the center of the end face of the cylinder chamber, an intake valve is provided in the intake hole, and the intake passage is connected, the intake passage is communicated with the intake hole to intake air. It consists of a vortex generating part at the end of the passage surrounding the valve and an introduction part at the other end of the passage, and the width between the circumferential surface of the valve shaft of the intake valve and the circumferential surface of the vortex generating part facing it is equal to the width on the circumferential side of the cylinder chamber. The outer part is made wider than the inner part on the +L> side of the cylinder chamber, and the introduction part is connected to the wide outer part of the vortex generating part, and the height between the opening surface of the hole and the ceiling of the vortex generating part facing it is The width is the same or decreases from the wide outer part to the narrow inner part around the valve stem, and the average reduction is equal to O/Z% of the intake hole diameter per 7 degrees around the valve stem. An intake port for an internal combustion engine, characterized in that the step between the circumferential surface of the vortex generating part and the opening edge of the intake hole is made smooth so that the part closer to the cylinder chamber surface is less angular than the part farther away. .
JP58088222A 1983-05-18 1983-05-18 Suction port for internal-combustion engine Pending JPS59213924A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP58088222A JPS59213924A (en) 1983-05-18 1983-05-18 Suction port for internal-combustion engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP58088222A JPS59213924A (en) 1983-05-18 1983-05-18 Suction port for internal-combustion engine

Publications (1)

Publication Number Publication Date
JPS59213924A true JPS59213924A (en) 1984-12-03

Family

ID=13936846

Family Applications (1)

Application Number Title Priority Date Filing Date
JP58088222A Pending JPS59213924A (en) 1983-05-18 1983-05-18 Suction port for internal-combustion engine

Country Status (1)

Country Link
JP (1) JPS59213924A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0619424A2 (en) * 1993-04-05 1994-10-12 Isuzu Motors Limited Multi-intake valve engine

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS543515B1 (en) * 1971-02-17 1979-02-23

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS543515B1 (en) * 1971-02-17 1979-02-23

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0619424A2 (en) * 1993-04-05 1994-10-12 Isuzu Motors Limited Multi-intake valve engine
EP0619424A3 (en) * 1993-04-05 1994-11-02 Isuzu Motors Limited Multi-intake valve engine

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