JPH0315622A - Port structure of engine - Google Patents

Port structure of engine

Info

Publication number
JPH0315622A
JPH0315622A JP1150779A JP15077989A JPH0315622A JP H0315622 A JPH0315622 A JP H0315622A JP 1150779 A JP1150779 A JP 1150779A JP 15077989 A JP15077989 A JP 15077989A JP H0315622 A JPH0315622 A JP H0315622A
Authority
JP
Japan
Prior art keywords
branch
port
radius
passage
intake
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.)
Granted
Application number
JP1150779A
Other languages
Japanese (ja)
Other versions
JP2765726B2 (en
Inventor
Masami Nishida
正美 西田
Masahiro Chiyoushi
調枝 昌博
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.)
Mazda Motor Corp
Original Assignee
Mazda Motor Corp
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 Mazda Motor Corp filed Critical Mazda Motor Corp
Priority to JP1150779A priority Critical patent/JP2765726B2/en
Publication of JPH0315622A publication Critical patent/JPH0315622A/en
Application granted granted Critical
Publication of JP2765726B2 publication Critical patent/JP2765726B2/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Abstract

PURPOSE:To improve distribution of fuel as well as to reduce flow resistance by forming a cross sectional shape of each of branch parts so that the radius of the inner circumferential part is larger than the radius of the outer circumferential part when a branch middle part of a port is cut in perpendicular to the flow direction. CONSTITUTION:At least an intake port 5 which opens in a combustion chamber 4 of an engine is formed by a common part 51, a branch middle part 54 and each of branch parts 52 and 53. Also, a tip end part of a fuel injection valve 3 is inserted into an escape groove 9 communicated with the intake port 5. In this case, when the intake port 5 is cut in perpendicular to the flow direction of intake air at least at the branch middle part 54, a cross sectional shape of each of the branch parts 52 and 53 is formed so that the radius Ra of the inner circumferential part is in the shape of a semicircle larger than the radius Rb of the outer circumferential part. And each of the branch parts 52 and 53 is formed so that the common part 51 in the shape of a circle is gradually separated in the half-cut state. By this, flow resistance f the intake air is reduced and distribution of fuel is improved.

Description

【発明の詳細な説明】 (産業上の利用分野) 本発明は、エンジンの吸気ポートあるいは排気ポートの
構造に関するものである。
DETAILED DESCRIPTION OF THE INVENTION (Field of Industrial Application) The present invention relates to the structure of an intake port or exhaust port of an engine.

(従来の技術) 従来より、エンジンの吸気ポート構造として、吸気ポー
トを1つの共通通路から2つの分岐通路に分岐して燃焼
室に開口するように構成するとともに、各分岐通路に吸
気弁を設けるようにして、1シリンダ当たりの吸気ポー
ト開口面積を増大し、高出力化を図ったものが知られて
いる(実開昭60−26284号公報参照)。
(Prior Art) Conventionally, the intake port structure of an engine has been configured such that the intake port is branched from one common passage into two branch passages that open into the combustion chamber, and an intake valve is provided in each branch passage. It is known that the intake port opening area per cylinder is increased in this manner to achieve high output (see Japanese Utility Model Publication No. 60-26284).

第11図ないし第16図に、この種の吸気ポート構造を
概略的に示す。これらの図において、4は燃焼室、5a
は吸気ポート、6は排気ポートである。吸気ポート5a
は、加工が容易になる等の観点から、吸気の流れ方向に
対して垂直に切った断面形状が略円形になった通路を組
み合せて構成ざれている。このため、円形の1つの共通
通路で構成される共通部51aと2つの分岐通路に分岐
した後の分岐部52a.53aとの間の、すなわち2つ
の分岐通路に分岐し始めてから完全に2つの分岐通路に
なる前の分岐途中部分54aでは、円形の2つの分岐通
路を横に繋ぎ合せた略ひようたん形の断面形状をなし、
しかも、下流側程、略ひようたん形を構成する2つの分
岐通路が徐々に離れるような形状となっている。
This type of intake port structure is schematically shown in FIGS. 11 to 16. In these figures, 4 is the combustion chamber, 5a
is an intake port, and 6 is an exhaust port. Intake port 5a
In view of ease of machining, the air passage is constructed by combining passages each having a substantially circular cross-sectional shape when taken perpendicularly to the flow direction of the intake air. For this reason, a common part 51a consisting of one circular common passage and a branch part 52a after branching into two branch passages. 53a, that is, at the mid-branching portion 54a between the beginning of the branching into two branching passages and before the two branching passages completely become two branching passages, there is a roughly gourd-shaped part 54a in which two circular branching passages are connected horizontally. Has a cross-sectional shape,
Moreover, the shape is such that the two branch passages constituting a substantially canopy shape become gradually separated from each other toward the downstream side.

(発明が解決しようとする課題) ところが、上記のように構成すると、次のような問題が
あった。すなわち、吸気ポート5aは、吸気量が上流測
と下流側とでほぼ均一になるようにするため、上流側の
共通部51aを大径にし、下流側の各分岐部52a.5
3aを小径として、共通部51aの断面積と2つの分岐
部52a.53aの合計断面積とがほぼ等しくなるよう
な形状にする必要がある。このようなことから、従来、
吸気ポート5aは、横から見て分岐途中部分54aで急
に絞られた形状となっていたとともに、分岐通路の中心
軸線のなす角〈分岐角〉βが大きく、かつ、分岐途中部
分54aの長さ之2が長く、しかも、分岐途中部分54
aの略ひようたん形断面の括れ部分(第14図および第
15図の斜fi1部分)57aの面積が大きくなってい
た。このため、従来の吸気ポート5aの構造では、気流
方向の角度変化や気流の干渉等により分岐途中部分54
aで流路抵抗が大きくなるという問題があった。また、
括れ部分57aの面積が大きかったため、上流側に設け
た燃料噴射弁3から噴制された燃料が括れ部分57aに
衝突して大量に付着するという問題があった。
(Problems to be Solved by the Invention) However, when configured as described above, there were the following problems. That is, the intake port 5a has a common portion 51a on the upstream side with a large diameter, and each downstream branch portion 52a . 5
3a as a small diameter, the cross-sectional area of the common part 51a and the two branch parts 52a. It is necessary to make the shape so that the total cross-sectional area of 53a is approximately equal. For this reason, conventionally,
When viewed from the side, the intake port 5a has a shape that is suddenly constricted at the mid-branch portion 54a, and the angle β formed by the central axis of the branch passage (branch angle) is large, and the length of the mid-branch portion 54a is large. The second part is long, and there is a part 54 in the middle of the branch.
The area of the constricted portion 57a (oblique fi1 portion in FIGS. 14 and 15) of the approximately gourd-shaped cross section of a was increased. For this reason, in the conventional structure of the intake port 5a, the mid-branch portion 54
There was a problem that the flow path resistance became large at a. Also,
Since the area of the constricted portion 57a was large, there was a problem in that a large amount of fuel injected from the fuel injection valve 3 provided on the upstream side collided with the constricted portion 57a and adhered thereto.

ところで、上記吸気ポート構造においては、各分岐部5
2a,53aの下流端開口部に向かって燃料を噴躬でき
るようにするために、一般に燃料噴射弁3として、先端
部に2個の11躬口を有する2噴口燃料噴射弁が使用さ
れている。そして、この2噴口燃料噴銅弁3の各噴射口
から噴射された燃料を各分岐部52a,53aに導入す
るために、2噴口燃料噴射弁3の先端部から吸気ポート
5aに向かって延びてその吸気ポート5aに開口する逃
がし溝9aが形成されている。
By the way, in the above intake port structure, each branch portion 5
In order to be able to inject fuel toward the downstream end openings of the fuel injection valves 2a and 53a, a two-hole fuel injection valve having two 11-hole ports at its tip is generally used as the fuel injection valve 3. . In order to introduce the fuel injected from each nozzle of the two-nozzle fuel injection valve 3 into each branch portion 52a, 53a, a pipe extends from the tip of the two-nozzle fuel injection valve 3 toward the intake port 5a. A relief groove 9a is formed which opens into the intake port 5a.

ところが、従来は、この逃がし溝98が分岐途中部分5
4aの途中までしか延びていなかったため、2つの分岐
部52a,53aの一方側にのみ偏って燃料が導入され
たりすることが起こり、燃料の分配性が悪いという問題
があった。
However, conventionally, this escape groove 98
4a, the fuel may be introduced only to one side of the two branch portions 52a and 53a, resulting in a problem of poor fuel distribution.

以上の事情に鑑みて、本発明は、吸気あるいは排気の流
れ抵抗を低減でき、また、2噴口燃料噴射弁を設けた吸
気ポートにおいて、燃料の分配性を向上することができ
るエンジンのポート構造を提供しようとするものである
In view of the above circumstances, the present invention provides an engine port structure that can reduce intake or exhaust flow resistance and improve fuel distribution in an intake port equipped with a two-injection fuel injection valve. This is what we are trying to provide.

〔課題を解決するための手段〕[Means to solve the problem]

本発明にかかるエンジンのポート構造は、1つの共通通
路から2つの分岐通路に分岐して燃焼室に開口するよう
にポートを形或したエンジンのポート構造において、少
なくとも、2つの分岐通路に分岐し始めてから完全に2
つの分岐通路になる前の分岐途中部分で、各分岐通路を
、流れの方向に対して垂直に切った断面の内側周部の半
径が外側同部の半径より大きくなるように構成するよう
にしたものである。
An engine port structure according to the present invention is an engine port structure in which a port is shaped so that one common passage branches into two branch passages and opens into a combustion chamber. Completely 2 since I started
In the middle of the branch before becoming two branch passages, each branch passage is configured so that the radius of the inner peripheral part of the cross section taken perpendicular to the flow direction is larger than the radius of the same outer part. It is something.

また、ポートが吸気ポートであって、このポートの同部
に、2個の噴射口を有し各噴射口から各分岐通路の下流
端開口部に向かってそれぞれ燃料を噴射する2噴口燃料
噴射弁が設けられている場合には、前記ポートの周部に
前記2噴口燃料噴射弁の各噴射口から分岐途中部分の下
流端まで延びる逃がし溝を形或することが好ましい。
Further, the port is an intake port, and a two-injector fuel injection valve has two injection ports in the same part of the port and injects fuel from each injection port toward the downstream end opening of each branch passage. is provided, it is preferable that a relief groove is formed in the circumference of the port, extending from each injection port of the two-injector fuel injection valve to the downstream end of the mid-branch portion.

(作用) 以上の構成によれば、分岐途中部分では、共通通路側か
ら分岐通路側に向かうに従って、円形の共通通路を徐々
に半割りに近い状態に切り離していくようにして2つの
分岐通路に分岐ざれることとなり、円形の共通通路を通
る吸気がその共通通路での気流方向に沿って2つの分岐
通路に分岐される、あるいは2つの分岐通路のそれぞれ
を通る排気がその分岐通路での気流方向に沿って円形の
共通通路に合流されることとなる。
(Function) According to the above configuration, in the middle of the branch, the circular common passage is gradually cut into half as it goes from the common passage side to the branch passage side, so that it becomes two branch passages. The intake air passing through the circular common passage is split into two branch passages along the airflow direction in the common passage, or the exhaust air passing through each of the two branch passages is divided into two branch passages. They merge into a circular common passage along the direction.

また、逃がし溝が分岐途中部分の下流端まで延びること
によって、2噴口燃料噴射弁の噴射口から噴射された燃
料が逃がし溝にガイドされて分岐途中部分の下流端まで
、すなわち2つの分岐通路に完全に分岐される位置まで
導かれることとなり、各分岐通路にその通路に向けて噴
射した燃料が確実に供給されることとなる。
Furthermore, since the relief groove extends to the downstream end of the mid-branch portion, the fuel injected from the injection port of the two-injector fuel injection valve is guided by the relief groove to the downstream end of the mid-branch portion, that is, into the two branch passages. The fuel is guided to a completely branched position, and the fuel injected toward each branch passage is reliably supplied to each branch passage.

〔実施例] 第1図ないし第10図は、本発明を吸気ポートの構造に
適用した場合の一実施例を示している。
[Embodiment] FIGS. 1 to 10 show an embodiment in which the present invention is applied to the structure of an intake port.

これらの図において、1はV型エンジンで、シリンダブ
ロック11と左右一対のシリンダヘッド12とシリンダ
力バー13とで@威されている。
In these figures, 1 is a V-type engine, which is comprised of a cylinder block 11, a pair of left and right cylinder heads 12, and a cylinder force bar 13.

各シリンダヘッド12には、吸気通路21を構成する吸
気マニホルド2が接続されている。吸気マニホルド2の
上流にはサージタンク22およびスロットル弁23が配
備され、サージタンク22内には吸気の固有振動数を変
更するバルブ24が設けられている。また、吸気マニホ
ルド2の下流端部には、燃料噴射弁3が装填されている
An intake manifold 2 forming an intake passage 21 is connected to each cylinder head 12 . A surge tank 22 and a throttle valve 23 are provided upstream of the intake manifold 2, and a valve 24 for changing the natural frequency of intake air is provided within the surge tank 22. Furthermore, a fuel injection valve 3 is installed at the downstream end of the intake manifold 2.

シリンダブロック11内にはシリンダ毎にピストン14
が設けられ、また、シリンダヘッド12内にはシリンダ
毎に燃焼室4、吸気ポート5および排気ポート6が形成
されている。吸気および排気ポート5.6は、1つの共
通通路から2つの分岐通路に分岐して燃焼室4に開口し
ており、1つの共通通路で構成された共通部51.61
と、2つの分岐通路に分岐し始めてから完全に2つの分
岐通路になる前の分岐途中部分54.64と、完全に2
つの分岐通路に分岐した分岐部52,53.62.63
とからなっている。上記吸気ポート5の分岐部52.5
3および排気ポート6の分岐部62.63には、それぞ
れ図外の動弁機構によって開閉動作が行われる吸気弁7
および排気弁8が設けられている。
Inside the cylinder block 11, a piston 14 is provided for each cylinder.
A combustion chamber 4, an intake port 5, and an exhaust port 6 are formed in the cylinder head 12 for each cylinder. The intake and exhaust ports 5.6 branch from one common passage into two branch passages and open into the combustion chamber 4, and a common part 51.61 composed of one common passage
, the middle part of the branch after it starts to branch into two branch passages and before it completely becomes two branch passages, and the part 54.
Branch section 52, 53, 62, 63 branched into two branch passages
It consists of Branch portion 52.5 of the intake port 5
3 and the branch portions 62 and 63 of the exhaust port 6 are each provided with an intake valve 7 that is opened and closed by a valve mechanism (not shown).
and an exhaust valve 8 are provided.

燃料噴射弁3の先端部は、吸気ポート5に連通ずる逃が
し満9の一端部91に差し込まれている。
The tip of the fuel injection valve 3 is inserted into one end 91 of a relief valve 9 that communicates with the intake port 5.

上記燃料噴射弁3としては、第9図に示すように噴射口
33が先端部に2個形成された2噴口燃料噴射弁が用い
られている。この燃料噴射弁3の各噴射口33は、吸気
ポート5の各分岐部52.53の下流端開口部に向けら
れている。
As the fuel injection valve 3, a two-nozzle fuel injection valve is used in which two injection ports 33 are formed at the tip, as shown in FIG. 9. Each injection port 33 of this fuel injection valve 3 is directed toward the downstream end opening of each branch 52 , 53 of the intake port 5 .

上記吸気ポート5の共通部51を吸気の流れ方向に対し
て垂直に切ると、第3図に示すように、1つの大きな円
形の断面形状があらわれる。また、分岐途中部分54を
吸気の流れ方向に対して垂直に切ると、第4図ないし第
6図に示すように、2つの分岐通路の各断面形状を2つ
横に並べて重ね合せた断面形状があらわれ、各分岐通路
の断面形状は内側周部の半径Raが外側局部の半径Rb
より大きくなった略半円形となっている。さらに、分岐
部52.53を吸気の流れ方向に対して垂直に切ると、
第7図および第8図に示すように、完全に分岐した2つ
の分岐通路の断面形状があらわれ、各分岐通路の断面形
状は、上流側では内側周部の半径Raが外側周部の半径
Rbより大きくなった略半円形となっており、下流側程
、その内測周部の半径Raが徐々に小さくなり、最終的
に下流端開口部では内側周部の半径Raが外側同部の半
径Rbと等しくなって円形となっている。
When the common portion 51 of the intake port 5 is cut perpendicularly to the flow direction of the intake air, one large circular cross-sectional shape appears, as shown in FIG. Furthermore, when the mid-branch portion 54 is cut perpendicularly to the flow direction of the intake air, the cross-sectional shape is obtained by superimposing the cross-sectional shapes of the two branch passages side by side, as shown in FIGS. 4 to 6. appears, and the cross-sectional shape of each branch passage is such that the radius Ra of the inner peripheral part is the radius Rb of the outer local part.
It has a larger, almost semicircular shape. Furthermore, if the branch parts 52 and 53 are cut perpendicularly to the flow direction of the intake air,
As shown in FIG. 7 and FIG. 8, the cross-sectional shapes of two completely branched branch passages appear, and the cross-sectional shape of each branch passage is such that on the upstream side, the radius Ra of the inner circumference is the radius Rb of the outer circumference. It has a larger semicircular shape, and the radius Ra of the inner circumferential part gradually becomes smaller as it goes downstream, and finally, at the downstream end opening, the radius Ra of the inner circumferential part becomes the radius of the same outer part. It is equal to Rb and has a circular shape.

以上のように吸気ポート5は、分岐途中部分54で、各
分岐通路が、流れの方向に対して垂直に切った断面の内
側周部の半径Raが外側同部の半径Rbより大きくなる
ように構成されている。このため、分岐角αが従来の分
岐角βと比べて小さくなる。すなわち、従来の構成では
、各分岐通路の断面形状が円形であったため、2つの分
岐通路の中心軸線間が各分岐通路の半径Rcの2倍の距
離だけ離れたときに、2つの分岐通路が完全に分岐し終
わるようになる。これに対し、本発明の構成によれば、
各分岐通路の断面形状が略半円形であるため、2つの分
岐通路の中心軸線間を僅かに離しただけで、2つの分岐
通路が完全に分岐し終わるようになる。したがって、従
来と比べて分岐角αを小さくすることができ、分岐し始
めてから分岐し終わるまでが短くてよくなるため、分岐
途中部分54の艮さ(1を短くすることができる。
As described above, the intake port 5 is configured so that the radius Ra of the inner peripheral part of the cross section taken perpendicularly to the flow direction is larger than the radius Rb of the outer peripheral part of each branch passage at the intermediate branching part 54. It is configured. Therefore, the branching angle α becomes smaller than the conventional branching angle β. That is, in the conventional configuration, since the cross-sectional shape of each branch passage was circular, when the center axes of the two branch passages were separated by a distance twice the radius Rc of each branch passage, the two branch passages It will be completely branched out. On the other hand, according to the configuration of the present invention,
Since the cross-sectional shape of each branch passage is approximately semicircular, the two branch passages can be completely branched by just slightly separating the center axes of the two branch passages. Therefore, the branching angle α can be made smaller than in the past, and the time from the start of branching to the end of branching can be shortened, so that the length (1) of the part 54 in the middle of branching can be shortened.

しかも、分岐途中部分54では、共通通路側から分岐通
路側に向かうに従って、円形の共通通路を徐々に半割り
に近い状態に切り離していくようにして2つの分岐通路
に分岐されるため、共通通路の高さ日と分岐通路の高さ
hとがほほ等しくなる。このため、吸気ポート5が、横
から見て、分岐途中部分54で急に絞られるということ
がなくなる。また、分岐途中部分54では、内側局部の
半径Raが大きくなっているため、略ひょうたん形断面
の括れ部分く第5図および第6図の斜線部〉57か細く
なる。すなわち、括れ部分57の面積が、従来と比べて
小さくなる。
Moreover, in the intermediate branching section 54, the circular common passage is gradually cut into two branch passages as it goes from the common passage side to the branch passage side, so that the common passage is divided into two branch passages. The height h and the height h of the branch passage are almost equal. Therefore, the intake port 5 is not suddenly constricted at the mid-branch portion 54 when viewed from the side. Further, in the intermediate branching portion 54, since the radius Ra of the inner local portion is large, the constricted portion of the approximately gourd-shaped cross section (shaded portion 57 in FIGS. 5 and 6) becomes narrower. That is, the area of the constricted portion 57 is smaller than that of the conventional case.

このように本発明の構成によれば、分岐角αを小さくす
ることができるとともに、分岐途中部分54で急に絞ら
れるということを防止でき、かつ、分岐途中部分54の
長さ乏1を短くすることができる。このため、共通通路
を通ってきた吸気が、気流方向をほとんど変えられるこ
となく、かつ、分岐途中部分54で互いに干渉し合うこ
となく、スムーズに2つの分岐通路に導入されるように
なる。
As described above, according to the configuration of the present invention, it is possible to reduce the branch angle α, prevent sudden narrowing at the mid-branch portion 54, and shorten the length of the mid-branch portion 54. can do. Therefore, the intake air that has passed through the common passage is smoothly introduced into the two branch passages without changing the air flow direction and without interfering with each other at the intermediate branch portion 54.

また、括れ部分57の面積を小さくできるため、燃料噴
射弁3から噴射された燃料が括れ部分57に断突して大
量に付着するということを防止することができる。
Further, since the area of the constricted portion 57 can be made small, it is possible to prevent a large amount of fuel injected from the fuel injection valve 3 from breaking into the constricted portion 57 and adhering to the constricted portion 57.

しかも、この実膚例の構成では、完全に2つの分岐通路
に分岐した後の分岐部52.53が、各分岐通路の内側
周部の半径Raが下流側程徐々に大きくなり、最終的に
下流端開口部で外側周部の半径Rbと等しくなるように
構成されている。このため、分岐部52.53において
も、吸気が抵抗なくスムーズに流されるようになる。
Moreover, in the configuration of this example, the radius Ra of the inner circumferential portion of each branch passage becomes gradually larger toward the downstream side of the branch part 52, 53 after completely branching into two branch passages, and finally The downstream end opening is configured to have a radius Rb equal to the outer peripheral portion. Therefore, the intake air can flow smoothly without resistance even at the branch portions 52 and 53.

前述した逃がし溝9は、吸気マニホルド2の下流端部を
貫通し、他端部92が吸気ポート5の分岐途中部分54
の下流端まで延びている。このため、燃料噴射弁3の噴
射口33から吸気ポート5の各分岐部52.53に向か
って噴射された燃料は、確実に目的とする分岐部52.
53に導入される。すなわち、一方の分岐部52に向か
って噴射された燃料は他方の分岐部53に入り込むこと
なく確実に一方の分岐部52に導入され、また、他方の
分岐部53に向かって噴射された燃料は一方の分岐部5
2に入り込むことなく確実に他方の分岐部53に導入さ
れる。
The above-mentioned relief groove 9 passes through the downstream end of the intake manifold 2, and the other end 92 is connected to the mid-branch portion 54 of the intake port 5.
extends to the downstream end of the Therefore, the fuel injected from the injection port 33 of the fuel injection valve 3 toward each branch portion 52.53 of the intake port 5 is reliably directed to the target branch portion 52.53.
Introduced in 53. That is, the fuel injected toward one branch 52 is reliably introduced into one branch 52 without entering the other branch 53, and the fuel injected toward the other branch 53 is One branch 5
2, and is reliably introduced into the other branch 53.

なお、排気ポート6に本発明のポート構造を適用しても
よい。また、分岐通路のうちで流れの方向に対して垂直
に切った断面の内側周部の半径が外側周部の半径より大
きくなるように構成する部分は、分岐途中部分のみであ
ってもよい。
Note that the port structure of the present invention may be applied to the exhaust port 6. In addition, the portion of the branch passage where the radius of the inner circumferential portion of a cross section taken perpendicularly to the flow direction is larger than the radius of the outer circumferential portion may be only the intermediate portion of the branch.

(発明の効果) 本発明にかかるエンジンのポート構造は、少なくとも分
岐途中部分で、各分岐通路が、流れの方向に対して垂直
に切った断面の内側周部の半径が外側周部の半径より大
きくなるように構成されている。このため、分岐途中部
分では、共通通路側から分岐通路側に向かうに従って、
円形の共通通路を徐々に半割りに近い状態に切り離して
いくようにして2つの分岐通路に分岐されることとなり
、円形の共通通路を通る吸気がその共通通路での気流方
向に沿って2つの分岐通路にスムーズに分岐される、あ
るいは2つの分岐通路のそれぞれを通る排気がその分岐
通路での気流方向に沿って円形の共通通路にスムーズに
合流されることとなる。
(Effects of the Invention) In the engine port structure according to the present invention, at least in the middle of the branch, the radius of the inner circumference of each branch passage in a cross section cut perpendicular to the flow direction is greater than the radius of the outer circumference. It is designed to be large. Therefore, in the middle of the branch, as you go from the common passage side to the branch passage side,
The circular common passage is gradually separated into two branch passages, and the intake air passing through the circular common passage is divided into two branches along the airflow direction in the common passage. The exhaust gases are smoothly branched into the branch passage, or the exhaust gas passing through each of the two branch passages is smoothly merged into the circular common passage along the airflow direction in the branch passage.

したがって、吸気および排気の流れ抵抗を低減すること
ができる。
Therefore, the flow resistance of intake and exhaust air can be reduced.

また、ポートが吸気ポートであって、このポートの周部
に、2fI1の噴射口を有し各哨躬口から各分岐通路の
下流端開口部に向かってそれぞれ燃料を噴射する2噴口
燃料噴射弁が設けられている場合、ポートの周部に2噴
口燃料噴射弁の各噴射口から分岐途中部分の下流端まで
延びる逃がし溝を形成すれば、2噴口燃料噴射弁の噴射
口から噴銅された燃料が逃がし溝にガイドされて分岐途
中部分の下流端まで、すなわち完全に2つの分岐通路に
分岐される位置まで導かれるため、各分岐通路にその通
路に向けて噴射した燃料が確実に供給されることとなり
、燃料の分配性が向上する。
Further, the port is an intake port, and the two-injector fuel injection valve has an injection port of 2fI1 around the port and injects fuel from each control port toward the downstream end opening of each branch passage. If a relief groove is formed around the port that extends from each nozzle of the two-nozzle fuel injection valve to the downstream end of the mid-branching part, it will be possible to prevent the injection of copper from the nozzle of the two-nozzle fuel injector. Since the fuel is guided by the relief groove to the downstream end of the intermediate part of the branch, that is, to the position where it completely branches into two branch passages, the fuel injected toward that passage is reliably supplied to each branch passage. This improves fuel distribution.

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

第1図は本発明にかかるエンジンのポート構造の一実施
例を示す縦断面図、第2図はその概略平面図、第3図は
第1図のトl線断面図、第4図は第1図のIV − r
V線断面図、第5図は第1図のVV線断面図、第6図は
第1図のVl−Vl線断面図、第7図は第1図の■−■
線断面図、第8図は第1図の■−■線断面図、第9図は
燃料噴射弁の先端部の断面図、第10図はその実施例を
適用したV型エンジンの全体正面図、第11図は従来の
エンジンのポート構造の概略平面図、第12図はその概
略縦断面図、第13図は第12図の刈一刈線断面図、第
14図は第12図のU−XIi線断面図、第1 5[[
12図のXv−Xv線断面図、第16図は第12図のX
VI−XVI線断面図である。 3・・・2噴口燃料噴射弁、4・・・燃焼室、5・・・
吸気ポート、6・・・排気ポート、9・・・逃がし溝、
33・・・2噴口燃料噴射弁の噴射口、54・・・分岐
途中部分、Ra・・・内側同部の半径、Rb・・・外側
周部の半径。
FIG. 1 is a longitudinal sectional view showing one embodiment of the engine port structure according to the present invention, FIG. 2 is a schematic plan view thereof, FIG. 3 is a sectional view taken along the line T in FIG. 1, and FIG. IV-r in Figure 1
5 is a sectional view taken along the VV line in Fig. 1, Fig. 6 is a sectional view taken along the Vl-Vl line in Fig. 1, and Fig. 7 is a sectional view taken from ■-■ in Fig. 1.
8 is a sectional view taken along the line ■-■ in FIG. 1, FIG. 9 is a sectional view of the tip of the fuel injection valve, and FIG. 10 is an overall front view of a V-type engine to which this embodiment is applied. , FIG. 11 is a schematic plan view of a conventional engine port structure, FIG. 12 is a schematic vertical sectional view thereof, FIG. 13 is a sectional view along the cutting line of FIG. -XIi line sectional view, 1st 5[[
12 is a sectional view taken along the line Xv-Xv, and FIG. 16 is a sectional view taken along the line Xv-Xv in
It is a sectional view taken along the line VI-XVI. 3...2-nozzle fuel injection valve, 4...combustion chamber, 5...
Intake port, 6... Exhaust port, 9... Relief groove,
33... Injection port of a two-nozzle fuel injection valve, 54... Branch midway portion, Ra... Radius of the inner same part, Rb... Radius of the outer peripheral part.

Claims (1)

【特許請求の範囲】 1、1つの共通通路から2つの分岐通路に分岐して燃焼
室に開口するようにポートを形成した土ンジンのポート
構造において、少なくとも、2つの分岐通路に分岐し始
めてから完全に2つの分岐通路になる前の分岐途中部分
で、各分岐通路が、流れの方向に対して垂直に切つた断
面の内側周部の半径が外側周部の半径より大きくなるよ
うに構成されていることを特徴とするエンジンのポート
構造。 2、ポートが吸気ポートであつて、このポートの周部に
は、2個の噴射口を有し各噴射口から各分岐通路の下流
端開口部に向かつてそれぞれ燃料を噴射する2噴口燃料
噴射弁が設けられているとともに、この2噴口燃料噴射
弁の各噴射口から分岐途中部分の下流端まで延びる逃が
し溝が形成されていることを特徴とする請求項1記載の
エンジンのポート構造。
[Claims] 1. In the port structure of a soil engine in which a port is formed so that one common passage branches into two branch passages and opens into the combustion chamber, at least after the port starts to branch into two branch passages. In the intermediate part of the branch before completely becoming two branch passages, each branch passage is configured such that the radius of the inner periphery of the cross section cut perpendicular to the flow direction is larger than the radius of the outer periphery. The engine port structure is characterized by: 2. A two-injector fuel injection system in which the port is an intake port, and the port has two injection ports around the port, and fuel is injected from each injection port toward the downstream end opening of each branch passage. 2. The port structure for an engine according to claim 1, further comprising a valve and a relief groove extending from each injection port of the two-injector fuel injection valve to a downstream end of the mid-branch portion.
JP1150779A 1989-06-13 1989-06-13 Engine port structure Expired - Fee Related JP2765726B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP1150779A JP2765726B2 (en) 1989-06-13 1989-06-13 Engine port structure

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP1150779A JP2765726B2 (en) 1989-06-13 1989-06-13 Engine port structure

Publications (2)

Publication Number Publication Date
JPH0315622A true JPH0315622A (en) 1991-01-24
JP2765726B2 JP2765726B2 (en) 1998-06-18

Family

ID=15504249

Family Applications (1)

Application Number Title Priority Date Filing Date
JP1150779A Expired - Fee Related JP2765726B2 (en) 1989-06-13 1989-06-13 Engine port structure

Country Status (1)

Country Link
JP (1) JP2765726B2 (en)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2006100849A1 (en) * 2005-03-18 2006-09-28 Toyota Jidosha Kabushiki Kaisha Dual-system fuel injection engine
US7216627B2 (en) 2005-03-18 2007-05-15 Toyota Jidosha Kabushiki Kaisha Internal combustion engine provided with double system of fuel injection
US7281517B2 (en) 2005-03-18 2007-10-16 Yamaha Hatsudoki Kabushiki Kaisha Internal combustion engine provided with double system of fuel injection
US7299784B2 (en) 2005-03-18 2007-11-27 Toyota Jidosha Kabushiki Kaisha Internal combustion engine
FR2931207A1 (en) * 2008-05-14 2009-11-20 Renault Sas Gas e.g. intake gas, transferring device for internal combustion engine, has separated ducts joined in main duct opening in gas manifold, where overall sectional surface of ducts is constant during passage from main duct to separated ducts
US7637242B2 (en) 2004-03-22 2009-12-29 Yamaha Motor Co., Ltd. Fuel supply system and vehicle

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS6261957U (en) * 1985-10-07 1987-04-17

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS6261957U (en) * 1985-10-07 1987-04-17

Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7637242B2 (en) 2004-03-22 2009-12-29 Yamaha Motor Co., Ltd. Fuel supply system and vehicle
WO2006100849A1 (en) * 2005-03-18 2006-09-28 Toyota Jidosha Kabushiki Kaisha Dual-system fuel injection engine
US7216627B2 (en) 2005-03-18 2007-05-15 Toyota Jidosha Kabushiki Kaisha Internal combustion engine provided with double system of fuel injection
US7281517B2 (en) 2005-03-18 2007-10-16 Yamaha Hatsudoki Kabushiki Kaisha Internal combustion engine provided with double system of fuel injection
US7296558B2 (en) 2005-03-18 2007-11-20 Yamaha Hatsudoki Kabushiki Kaisha Dual-injector fuel injection engine
US7299784B2 (en) 2005-03-18 2007-11-27 Toyota Jidosha Kabushiki Kaisha Internal combustion engine
JPWO2006100849A1 (en) * 2005-03-18 2008-08-28 トヨタ自動車株式会社 Dual fuel injection engine
AU2006225905B2 (en) * 2005-03-18 2009-10-29 Toyota Jidosha Kabushiki Kaisha Dual-system fuel injection engine
JP4495211B2 (en) * 2005-03-18 2010-06-30 トヨタ自動車株式会社 Dual fuel injection engine
FR2931207A1 (en) * 2008-05-14 2009-11-20 Renault Sas Gas e.g. intake gas, transferring device for internal combustion engine, has separated ducts joined in main duct opening in gas manifold, where overall sectional surface of ducts is constant during passage from main duct to separated ducts

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