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JPS6324133B2 - - Google Patents
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JPS6324133B2 - - Google Patents

Info

Publication number
JPS6324133B2
JPS6324133B2 JP57044131A JP4413182A JPS6324133B2 JP S6324133 B2 JPS6324133 B2 JP S6324133B2 JP 57044131 A JP57044131 A JP 57044131A JP 4413182 A JP4413182 A JP 4413182A JP S6324133 B2 JPS6324133 B2 JP S6324133B2
Authority
JP
Japan
Prior art keywords
port
intake port
intake
siamese
ports
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
Application number
JP57044131A
Other languages
Japanese (ja)
Other versions
JPS58160513A (en
Inventor
Kyoshi Nakanishi
Takeshi Okumura
Tokuta Inoe
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 Motor Corp
Original Assignee
Toyota 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 Toyota Motor Corp filed Critical Toyota Motor Corp
Priority to JP57044131A priority Critical patent/JPS58160513A/en
Publication of JPS58160513A publication Critical patent/JPS58160513A/en
Publication of JPS6324133B2 publication Critical patent/JPS6324133B2/ja
Granted 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
    • 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
    • F02B31/08Modifying induction systems for imparting a rotation to the charge in the cylinder having multiple air inlets
    • F02B31/085Modifying induction systems for imparting a rotation to the charge in the cylinder having multiple air inlets having two inlet valves
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02FCYLINDERS, PISTONS OR CASINGS, FOR COMBUSTION ENGINES; ARRANGEMENTS OF SEALINGS IN COMBUSTION ENGINES
    • F02F1/00Cylinders; Cylinder heads 
    • F02F1/24Cylinder heads
    • F02F1/42Shape or arrangement of intake or exhaust channels in cylinder heads
    • F02F1/4214Shape or arrangement of intake or exhaust channels in cylinder heads specially adapted for four or more valves per 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)
  • Cylinder Crankcases Of Internal Combustion Engines (AREA)

Description

【発明の詳細な説明】 本発明は、内燃機関の吸気系の構造に関し、と
くにデユアルポートでしかも二つのポートの分岐
点がシリンダヘツド内に位置する吸気系の両ポー
トを分離する隔壁の構造に関する。
DETAILED DESCRIPTION OF THE INVENTION The present invention relates to the structure of an intake system for an internal combustion engine, and more particularly to the structure of a partition wall that separates both ports of an intake system that has dual ports and the branching point of the two ports is located within the cylinder head. .

自動車用内燃機関において、低燃費化と高速負
荷時の高出力性能とを両立させるために、吸気ポ
ートを互いに独立のデユアルポートとし、一方を
ヘリカルポートにするとともに他方をストレート
ポートに構成した内燃機関は既に提案されてい
る。ところで、デユアル吸気ポート方式を採用す
るに際しては、通路壁面積を小にして壁面への燃
料付着を少なくし未燃炭化水素の放出量の低減お
よび運転性の向上をはかり、またシリンダヘツド
における吸気通路の占める空間を小にして燃焼室
の冷却を容易にする等のために、両ポートを、シ
リンダヘツド内において互いに分岐させる双子状
ポートいわゆるサイアミーズポートに構成するこ
とが望まれる。しかし、この場合は、独立二ポー
トに比べて、またはポートの少なくとも何れか一
方に絞り弁を設けた場合に比べて、二つのポート
の相互に及ぼし合う影響が非常に強く、二つのポ
ートを互いに如何に関連させて構成するか、また
は二つのポートをどのように互いにシリンダヘツ
ド内で分離させるかによつて、前記の低燃費化お
よび高出力性能に係る作用効果の得られる度合が
大きく異なつてくる。
In automotive internal combustion engines, in order to achieve both low fuel consumption and high output performance under high-speed loads, internal combustion engines have independent dual intake ports, one of which is a helical port and the other a straight port. has already been proposed. By the way, when adopting the dual intake port system, it is necessary to reduce the passage wall area to reduce fuel adhesion to the wall surface, reduce the amount of unburned hydrocarbons released, and improve driveability. In order to reduce the space occupied by the cylinder head and facilitate cooling of the combustion chamber, it is desirable to form both ports into twin ports, so-called Siamese ports, which are branched from each other within the cylinder head. However, in this case, compared to two independent ports, or compared to a case where a throttle valve is provided on at least one of the ports, the two ports have a much stronger influence on each other, and the two ports have a much stronger influence on each other. Depending on how the ports are connected or how the two ports are separated from each other within the cylinder head, the degree to which the aforementioned effects related to lower fuel consumption and higher output performance can be obtained varies greatly. come.

本発明は、一方のポートがヘリカルポートでし
かも二つのポートの分岐点がシリンダヘツド内に
あるサイアミーズポートにおいて、低中速域にお
ける燃費の低減および高速域における高出力の性
能が効果的に達成されるようにした、二つのポー
ト間の相互の分離構造を提供することを目的とす
る。
The present invention effectively achieves reduced fuel consumption in the low to medium speed range and high output performance in the high speed range in a Siamese port where one port is a helical port and the branching point of the two ports is inside the cylinder head. The purpose of the present invention is to provide a mutual isolation structure between two ports.

この目的を達成するために、本発明の内燃機関
の吸気系においては、ヘリカルポートからなる主
吸気ポートとストレートポートからなる副吸気ポ
ートとが、両ポートの分岐点がシリンダヘツド内
にあるサイアミーズポートに構成されており、主
吸気ポートと副吸気ポートとは、サイアミーズポ
ートの下流側から上流側に向つて延びる隔壁によ
つて互いに隔離されるようになつており、しかも
サイアミーズポートの通路断面上部程隔壁は上流
側の位置まで長く延びており、通路断面下部程短
く延びて下流側の位置でとどまつている。この構
成をとることによつて、サイアミーズポートの上
壁面近傍の流れは隔壁によつて早くから分離さ
れ、ヘリカルポート内を充分な距離にわたつて案
内されるので、低中速域において燃焼室内に強力
なスワールを生成し、低燃費化をはかることがで
きる。また、下壁面近傍の流れは吸気弁近傍に至
るまで主、副吸気ポートを合せた大断面内を流れ
るので、壁面の絞り抵抗を受け難く、高体積効率
が確保できることになり、そしてこの高充填作用
は高速域に効果を強く発揮し、高速域における高
出力を保証することができる。
In order to achieve this object, in the intake system of the internal combustion engine of the present invention, the main intake port consisting of a helical port and the auxiliary intake port consisting of a straight port are connected to a Siamese port where the branching point of both ports is within the cylinder head. The main intake port and the sub-intake port are separated from each other by a partition wall extending from the downstream side to the upstream side of the Siamese port, and the upper part of the passage cross section of the Siamese port The partition wall extends for a long time to a position on the upstream side, and extends shorter toward the lower part of the passage cross section, and remains at a position on the downstream side. By adopting this configuration, the flow near the upper wall of the Siamese port is separated early by the partition wall and guided over a sufficient distance within the helical port, so that a strong flow is generated inside the combustion chamber in the low and medium speed range. It is possible to generate a swirl and reduce fuel consumption. In addition, the flow near the lower wall surface flows within a large cross section that includes the main and auxiliary intake ports up to the vicinity of the intake valve, so it is less susceptible to throttling resistance from the wall surface, and high volumetric efficiency can be ensured. The action is most effective in the high speed range, and can guarantee high output in the high speed range.

以下に、本発明の内燃機関の吸気系の望ましい
実施例を図面を参照しながら説明する。第1図な
いし第8図は本発明の第1実施例に係る吸気通路
を示している。まず、第1図および第2図はシリ
ンダヘツド近傍の構造を示しており、図中、1は
シリンダヘツド、2はシリンダボア、シリンダボ
ア2は想像線でその位置のみを示してある。シリ
ンダボア2の領域内には、二つの吸気ポート3,
4と一つの排気ポート5(排気ポートは二つあつ
てもよい)とが設けられており、各ポート3,
4,5はそれぞれの吸気弁6,7および排気弁に
よつて開閉されるようになつている。
Preferred embodiments of the intake system for an internal combustion engine according to the present invention will be described below with reference to the drawings. 1 to 8 show an intake passage according to a first embodiment of the present invention. First, FIGS. 1 and 2 show the structure in the vicinity of the cylinder head. In the figures, 1 is the cylinder head, 2 is the cylinder bore, and the cylinder bore 2 is shown only its position by an imaginary line. In the area of the cylinder bore 2 there are two intake ports 3,
4 and one exhaust port 5 (there may be two exhaust ports), and each port 3,
4 and 5 are opened and closed by respective intake valves 6 and 7 and exhaust valves.

二つの吸気ポートのうち一方の吸気ポート、す
なわち主吸気ポート3は、他方の吸気ポートすな
わち副吸気ポート4より長く、通路断面積が大
で、かつヘリカル形状に形成されている。副吸気
ポート4はほゞ真直に延びている。副吸気ポート
4は主吸気ポートのヘリカル形状の内周側から分
岐しているが、その分岐点8はシリンダヘツド1
内に位置している。分岐点8と吸気弁6,7との
間において、両ポート3,4は特別な絞り弁は有
していない。
One of the two intake ports, that is, the main intake port 3, is longer than the other intake port, that is, the auxiliary intake port 4, has a larger passage cross-sectional area, and is formed in a helical shape. The sub-intake port 4 extends substantially straight. The auxiliary intake port 4 branches from the inner peripheral side of the helical shape of the main intake port, and its branching point 8 is located at the cylinder head 1.
Located within. Between the branch point 8 and the intake valves 6, 7, the two ports 3, 4 have no special throttle valves.

主吸気ポート3は、第3図に示すように、ほゞ
真直に延びる導入部3aとそれに連なつて下流側
に延びる渦巻部3bとからなつており、渦巻部3
bはその出口側の端部で下方に向つて折れ曲り、
断面円形の円筒部を介してシリンダヘツド燃焼室
リセス9に開口している。主吸気ポート3のヘリ
カル形状の内周側壁面10は、主吸気ポート3の
通路断面の上部程したがつて上壁面11に近づく
程、また下流にいく程、ヘリカル形状の外周側壁
面12に向つて傾斜し膨出しており、このためヘ
リカル形状の主吸気ポート3は、通路断面上部
程、また下流側程その流路が狭まつている。ま
た、主吸気ポート3の上壁面11は、下流にいく
程、徐々に下降している。
As shown in FIG. 3, the main intake port 3 consists of an introduction section 3a that extends almost straight and a spiral section 3b that extends downstream in series with the introduction section 3a.
b is bent downward at the end on the exit side,
The cylinder head opens into the combustion chamber recess 9 through a cylindrical portion having a circular cross section. The helical inner wall surface 10 of the main intake port 3 is directed toward the helical outer wall surface 12 as it approaches the upper wall surface 11 of the passage cross section of the main intake port 3 and as it goes downstream. The helical main intake port 3 has a flow path that narrows toward the upper part of the passage cross section and toward the downstream side. Further, the upper wall surface 11 of the main intake port 3 gradually descends as it goes downstream.

一方、ストレートポートである副吸気ポート4
は、第3図に示すように、主吸気ポート3の導入
部3aから分岐し、ほゞ真直に延びてその終端で
下方に折れ曲り断面円形の円筒部を介して、点火
プラグ13対向側の大きなスキツシユエリアの上
面を形成するシリンダヘツド下部平坦面14に開
口している。ストレートポート4の上壁面15は
下流にいく程徐々に下降している。
On the other hand, auxiliary intake port 4, which is a straight port,
As shown in FIG. 3, it branches from the introduction part 3a of the main intake port 3, extends almost straight, bends downward at the end, and connects to the opposite side of the spark plug 13 via a cylindrical part with a circular cross section. It opens into a lower flat surface 14 of the cylinder head which forms the upper surface of a large skid area. The upper wall surface 15 of the straight port 4 gradually descends toward the downstream.

主吸気ポート3と副吸気ポート4とは、隔壁1
6によつて互いに隔てられる。隔壁16は第1図
に示すように、サイアミーズポートの下流側から
上流側に向つて延びているが、サイアミーズポー
トの通路断面の上部側程サイアミーズポート入口
部17に近い位置まですなわち上流側の位置まで
長く延びており、通路断面の下部側程短く延びて
下流側の位置でとどまつている。第4図ないし第
6図は主吸気ポート3と副吸気ポート4間の隔壁
16の延び方をサイアミーズポートの上流側から
下流側にかけての断面の推移において示してい
る。図に示すように上流側では隔壁16は上壁面
11に近い部位のみ存在し、下流側に移る程下壁
面18に近い位置まで存在し、さらに下流側では
両ポート3,4は隔壁16によつて完全に隔離さ
れる。したがつて、両ポート3,4を水平な仮想
面で切断して見ると第7図および第8図に示すよ
うになり、通路断面上部の水平面に沿つて見ると
第7図のように、主吸気ポート3と副吸気ポート
とは上流側の位置から早くから隔離され、通路断
面下部の水平面に沿つて見ると第8図のように、
ポート通路は吸気バルブ7近傍まで主、副の両ポ
ート3,4を合せた大断面となつている。なお、
第1の実施例においては主吸気ポート3の上壁面
11と副吸気ポート4の上壁面15とは、分離位
置において、互いにほゞ同じ高さに位置してい
る。
The main intake port 3 and the sub-intake port 4 are connected to the partition wall 1
separated from each other by 6. As shown in FIG. 1, the partition wall 16 extends from the downstream side to the upstream side of the Siamese port, and the closer to the upper side of the passage cross section of the Siamese port, the closer to the Siamese port inlet 17, that is, the upstream position. It extends for a long time until the bottom of the cross section of the passage, and it extends for a shorter length toward the lower side of the passage cross section, and stays at a position on the downstream side. 4 to 6 show the extension of the partition wall 16 between the main intake port 3 and the sub-intake port 4 in the progression of the cross section from the upstream side to the downstream side of the Siamese port. As shown in the figure, on the upstream side, the partition wall 16 exists only at a portion close to the upper wall surface 11, and as it moves downstream, it exists at a position closer to the lower wall surface 18, and further downstream, both ports 3 and 4 are completely isolated. Therefore, when both ports 3 and 4 are viewed along a horizontal imaginary plane, they are as shown in FIGS. 7 and 8, and when viewed along the horizontal plane at the top of the cross section of the passage, as shown in FIG. The main intake port 3 and the auxiliary intake port are separated from each other from an upstream position, and when viewed along the horizontal plane at the bottom of the passage cross section, as shown in Figure 8,
The port passage has a large cross section including both the main and sub ports 3 and 4 up to the vicinity of the intake valve 7. In addition,
In the first embodiment, the upper wall surface 11 of the main intake port 3 and the upper wall surface 15 of the auxiliary intake port 4 are located at substantially the same height as each other in the separated position.

第9図ないし第13図は本発明の第2実施例に
係る吸気通路を示している。本実施例において
は、副吸気ポート4の上壁面15は主吸気ポート
3の上壁面11より低い位置に設けられており、
副吸気ポート4が隔壁16を介して主吸気ポート
3の通路断面の低い位置と連通するようになつて
いる。その他の構成は第1実施例と同じであり、
対応する部位に第1実施例と同一の符号を付して
構成に係る説明を省略する。
9 to 13 show an intake passage according to a second embodiment of the present invention. In this embodiment, the upper wall surface 15 of the sub-intake port 4 is provided at a lower position than the upper wall surface 11 of the main intake port 3,
The auxiliary intake port 4 communicates with a lower position in the passage cross section of the main intake port 3 via the partition wall 16. The other configurations are the same as the first embodiment,
Corresponding parts are given the same reference numerals as those in the first embodiment, and explanations regarding the configuration will be omitted.

つぎに、第1実施例および第2実施例の作用に
ついて説明する。
Next, the effects of the first embodiment and the second embodiment will be explained.

まず、サイアミーズポートの通路断面上部を流
れる流れは、隔壁16が上部では上流側に延びて
いるので早くから主吸気ポート3側と副吸気ポー
ト4側とに分離する。そして、主吸気ポート3側
に流入した吸気は、隔壁16がヘリカルポートの
外周側壁面12に向つて膨出しているため外周側
壁面12に近づくように偏流し、長い距離にわた
つて通路上部の絞りと上壁面11の下降によつ
て、増速されつつ旋回および下降の力を与えら
れ、渦巻部3bに入つてそこで強力な旋回流を生
じた後、吸気弁6と弁座間の間隙を通つて燃焼室
に入り、強力な渦流、いわゆるスワールを発生さ
せる。また、副吸気ポート4側に流入した空気は
直線状に流れポート4終端で下方に折れ曲つて燃
焼室内に吸入されて流れ込む。このように、通路
断面上部のとくにヘリカルポート3側の流れは、
スワールの発生に効くが、機関の低中速域におい
ては、ヘリカル形状による流れ抵抗は余り大きく
ないので、主吸気ポート3側に多量の混合気が流
れ、スワールの生成による燃焼の安定性がはから
れ、混合比のリーンリミツトをさらにリーン側に
向上でき、低燃費化をはかることができる。
First, the flow flowing in the upper part of the passage cross section of the Siamese port is early separated into the main intake port 3 side and the sub intake port 4 side because the partition wall 16 extends upstream at the upper part. Since the partition wall 16 bulges toward the outer circumferential wall surface 12 of the helical port, the intake air flowing into the main intake port 3 side is diverted toward the outer circumferential wall surface 12, and flows over a long distance toward the outer circumferential wall surface 12 of the helical port. Due to the throttle and the lowering of the upper wall surface 11, a swirling and descending force is applied while increasing the speed, and after entering the spiral portion 3b and generating a strong swirling flow there, it passes through the gap between the intake valve 6 and the valve seat. The gas then enters the combustion chamber, creating a powerful eddy current, so-called swirl. Further, the air flowing into the sub-intake port 4 side flows in a straight line, bends downward at the terminal end of the port 4, and is sucked into the combustion chamber. In this way, the flow in the upper part of the passage cross section, especially on the helical port 3 side, is
It is effective in generating swirl, but in the low and medium speed range of the engine, the flow resistance due to the helical shape is not so large, so a large amount of air-fuel mixture flows to the main intake port 3 side, which reduces the stability of combustion due to the generation of swirl. As a result, the lean limit of the mixture ratio can be further improved to the lean side, and fuel efficiency can be improved.

一方、サイアミーズポートの通路断面下部を流
れる流れは、隔壁16が下流側に後退しているの
で、副吸気ポート4の吸気弁7近傍に至るまで主
副合せた大断面内を流れて、吸気弁7近傍に至つ
て始めて分離し、燃焼室内に流入する。しかも、
主吸気ポート3側も通路断面下部は上部程絞られ
ていないので、増速およびヘリカル外周面に沿う
流れは緩和され、上部程の強い旋回流は生じな
い。したがつて旋回流による流れ抵抗、絞り抵抗
も少なく、かつ隔壁壁面の粘性抵抗も小であるの
で、吸気流量の確保、高充填に効くことになる。
したがつて、機関の高速域においては、吸入空気
量が増大し、それにつれてサイアミーズポート上
端部、とくにヘリカルポート側上端部を流れる流
れは流れ抵抗が増して、通過流量割合が低下する
が、通路下部が前記の如く吸気流量を確保するの
で、高速域においても高出力性能を得ることがで
きる。
On the other hand, since the partition wall 16 has retreated downstream, the flow flowing in the lower part of the passage cross section of the Siamese port flows within the large cross section of the main and sub intake ports until it reaches the vicinity of the intake valve 7 of the sub intake port 4. It is not until it reaches around 7 that it separates and flows into the combustion chamber. Moreover,
On the main intake port 3 side, the lower part of the passage cross section is not as constricted as the upper part, so the speed increase and the flow along the helical outer peripheral surface are relaxed, and the swirling flow as strong as the upper part does not occur. Therefore, the flow resistance and restriction resistance due to the swirling flow are small, and the viscous resistance of the partition wall surface is also small, which is effective in securing the intake air flow rate and achieving high filling.
Therefore, in the high-speed range of the engine, the amount of intake air increases, and as a result, the flow resistance of the flow flowing through the upper end of the Siamese port, especially the upper end on the helical port side, increases and the rate of flow passing through the passage decreases. Since the lower portion secures the intake flow rate as described above, high output performance can be obtained even in the high speed range.

以上の通りであるから、本発明の内燃機関の吸
気系によるときは、隔壁の構造によつてサイアミ
ーズポートの通路断面上部と下部の流れの作用を
効果的に異ならしめたので、低中速域において上
層部の流れにより強力なスワールの生成を確保で
き、リーンリミツトの向上を通して燃費の改善を
はかることができ、高速域において下層部の流れ
により高体積効率を得ることができ、高出力性能
を維持することができる。
As described above, when using the intake system of the internal combustion engine of the present invention, the structure of the partition wall effectively makes the flow action different between the upper and lower passage cross sections of the Siamese port. The flow in the upper part of the engine ensures the generation of a strong swirl, and by improving the lean limit, it is possible to improve fuel efficiency, and in the high-speed range, the flow in the lower part of the engine allows high volumetric efficiency to be obtained, maintaining high output performance. can do.

また、シリンダヘツド内サイアミーズポート構
成としたことによる他の一般的効果も当然得られ
る。たとえば、独立二ポートに比べて仕切壁が減
少し、壁面への燃料付着を少なくし、未燃炭化水
素の放出の低減、運転性の向上をはかることがで
きる。また、独立二ポートに比べて燃焼室壁上面
でのウオータジヤケツトの占める空間を大にで
き、冷却効果の向上とそれに伴なうノツク限界の
向上を通して低燃費化をはかることができる。さ
らにサイアミーズ化によつて製作時に一体中子を
使用でき、燃焼室内ポート配置の製作精度を向上
でき、量産エンジンの性能のばらつきを抑えるこ
ともできる。
In addition, other general effects can naturally be obtained by using the Siamese port structure within the cylinder head. For example, compared to two independent ports, there are fewer partition walls, which reduces fuel adhesion to the wall surface, reduces the release of unburned hydrocarbons, and improves drivability. Furthermore, compared to two independent ports, the space occupied by the water jacket on the upper surface of the combustion chamber wall can be increased, and fuel efficiency can be achieved by improving the cooling effect and the concomitant knock limit. Furthermore, by using Siamese, an integral core can be used during manufacturing, improving the manufacturing accuracy of the combustion chamber port arrangement and suppressing variations in performance of mass-produced engines.

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

第1図は本発明の第1実施例に係る内燃機関の
吸気系の縦断面図、第2図は第1図の吸気系の平
面図、第3図は第1図および第2図においてサイ
アミーズポートのみを取出して示した斜視図、第
4図は第1図の−線に沿うサイアミーズポー
トの縦断面図、第5図は第1図の−線に沿う
サイアミーズポートの縦断面図、第6図は第1図
の−線に沿うサイアミーズポートの縦断面
図、第7図は通路断面上部におけるサイアミーズ
ポートの横断面図、第8図は通路断面下部におけ
るサイアミーズポートの横断面図、第9図は本発
明の第2実施例に係る内燃機関の吸気系の縦断面
図、第10図は第9図においてサイアミーズポー
トのみを取出して示した斜視図、第11図は第9
図のXI−XI線に沿うサイアミーズポートの縦断面
図、第12図は第9図のXII−XII線に沿うサイアミ
ーズポートの縦断面図、第13図は第9図の
−線に沿うサイアミーズポートの縦断面図、
である。 1……シリンダヘツド、3……主吸気ポート、
3a……導入部、3b……渦巻部、4……副吸気
ポート、6……吸気弁、7……吸気弁、8……分
岐点、10……主吸気ポート内周側壁面、11…
…主吸気ポート上壁面、12……主吸気ポート外
周側壁面、15……副吸気ポート上壁面、16…
…隔壁、17……サイアミーズポート入口部。
1 is a longitudinal sectional view of an intake system of an internal combustion engine according to a first embodiment of the present invention, FIG. 2 is a plan view of the intake system of FIG. 1, and FIG. FIG. 4 is a vertical sectional view of the Siamese port taken along the - line in FIG. 1, FIG. 5 is a longitudinal sectional view of the Siamese port taken along the - line in FIG. 1, and FIG. The figures are a longitudinal sectional view of the Siamese port taken along the - line in Fig. 1, Fig. 7 is a cross-sectional view of the Siamese port at the upper part of the passage cross-section, Fig. 8 is a cross-sectional view of the Siamese port at the lower part of the passage cross-section, and Fig. 9 10 is a longitudinal cross-sectional view of an intake system of an internal combustion engine according to a second embodiment of the present invention, FIG. 10 is a perspective view showing only the Siamese port in FIG. 9, and FIG.
Fig. 12 is a vertical cross-sectional view of the Siamese port along the line XI-XI in Fig. 9, Fig. 13 is a longitudinal cross-sectional view of the Siamese port along the - line in Fig. 9. Longitudinal cross-sectional view of
It is. 1... Cylinder head, 3... Main intake port,
3a... Introduction part, 3b... Spiral part, 4... Sub-intake port, 6... Intake valve, 7... Intake valve, 8... Branch point, 10... Main intake port inner peripheral side wall surface, 11...
...Main intake port top wall surface, 12...Main intake port outer peripheral side wall surface, 15...Sub-intake port top wall surface, 16...
...Bulkhead, 17...Siamese Port entrance.

Claims (1)

【特許請求の範囲】[Claims] 1 ヘリカルポートからなる主吸気ポートとスト
レートポートからなる副吸気ポートとを両ポート
の分岐点がシリンダヘツド内にあるサイアミーズ
ポートに構成し、主吸気ポートと副吸気ポートを
隔てるサイアミーズポート内を下流から上流に向
つて延びる隔壁を、サイアミーズポートの通路断
面上部程上流側まで長く延ばし、通路断面下部程
短く延ばしたことを特徴とする内燃機関の吸気
系。
1 A main intake port consisting of a helical port and a sub-intake port consisting of a straight port are configured into a Siamese port where the branch point of both ports is inside the cylinder head, and the inside of the Siamese port that separates the main intake port and sub-intake port is connected from downstream. An intake system for an internal combustion engine, characterized in that a partition wall extending upstream is extended upstream toward the upper part of the passage cross section of a Siamese port, and is extended shorter toward the lower part of the passage cross section.
JP57044131A 1982-03-19 1982-03-19 Internal combustion engine intake system Granted JPS58160513A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP57044131A JPS58160513A (en) 1982-03-19 1982-03-19 Internal combustion engine intake system

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP57044131A JPS58160513A (en) 1982-03-19 1982-03-19 Internal combustion engine intake system

Publications (2)

Publication Number Publication Date
JPS58160513A JPS58160513A (en) 1983-09-24
JPS6324133B2 true JPS6324133B2 (en) 1988-05-19

Family

ID=12683058

Family Applications (1)

Application Number Title Priority Date Filing Date
JP57044131A Granted JPS58160513A (en) 1982-03-19 1982-03-19 Internal combustion engine intake system

Country Status (1)

Country Link
JP (1) JPS58160513A (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2006342746A (en) * 2005-06-09 2006-12-21 Toyota Motor Corp Intake structure of internal combustion engine

Also Published As

Publication number Publication date
JPS58160513A (en) 1983-09-24

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