JPS6234935B2 - - Google Patents

Info

Publication number
JPS6234935B2
JPS6234935B2 JP59167969A JP16796984A JPS6234935B2 JP S6234935 B2 JPS6234935 B2 JP S6234935B2 JP 59167969 A JP59167969 A JP 59167969A JP 16796984 A JP16796984 A JP 16796984A JP S6234935 B2 JPS6234935 B2 JP S6234935B2
Authority
JP
Japan
Prior art keywords
section
passage
helical
channel
cross
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
JP59167969A
Other languages
Japanese (ja)
Other versions
JPS60101246A (en
Inventor
Erusubetsuto Ruudoihi
Erusubetsuto Gyuntaa
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Publication of JPS60101246A publication Critical patent/JPS60101246A/en
Publication of JPS6234935B2 publication Critical patent/JPS6234935B2/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
    • F02B27/00Use of kinetic or wave energy of charge in induction systems, or of combustion residues in exhaust systems, for improving quantity of charge or for increasing removal of combustion residues
    • F02B27/02Use of kinetic or wave energy of charge in induction systems, or of combustion residues in exhaust systems, for improving quantity of charge or for increasing removal of combustion residues the systems having variable, i.e. adjustable, cross-sectional areas, chambers of variable volume, or like variable means
    • 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
    • F02F1/4228Helically-shaped channels 
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B3/00Engines characterised by air compression and subsequent fuel addition
    • F02B3/06Engines characterised by air compression and subsequent fuel addition with compression ignition
    • 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)
  • Exhaust Silencers (AREA)

Description

【発明の詳細な説明】 本発明は往復動ピストン式内燃機関の吸気系に
おける渦流形成通路であつて、この渦流形成通路
内を通過せしめられるガス状の媒体に回転運動を
与えるために、渦流形成通路が所望の渦流形成方
向に曲げられており、シリンダヘツドに位置する
吸気弁を有していて、渦流形成通路が螺旋形に曲
げられた通路区分とこれに接続するS字形に湾曲
させられた案内通路区分とを有しており、螺旋形
の通路区分がS字形に湾曲させられた案内通路区
分とシリンダ室との間に設けられていて、S字形
に湾曲させられた案内通路区分の一方の端点がシ
リンダ軸線と弁軸線とを通る通路横断面の上に位
置しかつ他方の端点を吸気管に対する案内通路区
分の開口が位置する、前記通路横断面に対して平
行に延びる通路横断面の上に位置しており、螺旋
形の通路区分の螺旋軸線がシリンダ軸線と弁軸線
とを通る通路横断面の上に、弁軸線にたいして偏
心的に配置されていて、螺旋形の通路区分がほぼ
一定の勾配と少なくとも220℃の螺旋形成角とを
有する螺線に沿つて配置されていてかつ螺旋軸線
とこれに向き合つている通路側壁との間にほぼ一
定の間隔を有していて、螺旋形の通路区分のシリ
ンダ室に向いた端部が円筒状の弁開口通路区分を
介してシリンダ室に開口している形式のものに関
する。
DETAILED DESCRIPTION OF THE INVENTION The present invention relates to a vortex forming passage in an intake system of a reciprocating piston type internal combustion engine. the passageway is bent in the desired swirl-forming direction and has an intake valve located in the cylinder head, the swirl-forming passageway being curved into an S-shape connected to a helically bent passageway section; a guide passage section, the helical passage section being provided between the S-shaped curved guide passage section and the cylinder chamber, one of the S-shaped curved guide passage sections; of a passage cross-section extending parallel to the passage cross-section, the end point of which lies on the passage cross-section passing through the cylinder axis and the valve axis, and the other end point of which lies the opening of the guide passage section to the intake pipe; The spiral axis of the helical passage section is located above the passage cross section passing through the cylinder axis and the valve axis, and is eccentrically arranged with respect to the valve axis, so that the helical passage section is approximately constant. and a helical formation angle of at least 220° C. and a substantially constant spacing between the helical axis and the opposing passageway side wall; The end of the passage section facing the cylinder chamber opens into the cylinder chamber via a cylindrical valve-opening passage section.

このような形式の渦流形成通路はほぼ3つの通
路区分から成つており、これらの通路区分は内燃
機関のシリンダから出発して、第1の通路区分は
円筒状の弁開口通路区分として、この弁開口通路
区分に接続された通路区分は螺旋形に巻かれた通
路区分として、この通路区分に接続された通路区
分はS字形に湾曲せしめられた案内通路区分とし
て構成されている。このような通路構成によつて
いわゆる偏向点からいわゆる螺旋点まで達する案
内通路区分は、有利にはその全長にわたつて変化
しない通路横断面を有しておりかつ同じ横断面で
螺旋形の通路区分に移行している。案内通路区分
から弁開口通路区分の入口開口への接続区分を形
成する螺旋形の通路区分も、変化しない横断面を
有している。このばあい各側壁から螺旋点までの
間隔は同じであるかあるいはほぼ同じである。一
方では螺旋点が弁案内を通る通路横断面に位置す
るように、他方では案内通路が流体力学的に申分
なく螺旋点に近づけられるように、弁案内と案内
通路の弁案内に隣接する壁との間には案内羽根が
設けられている。この案内羽根は根本で案内通路
の壁に、先端で弁案内に接続されている。この案
内羽根によつて螺旋形の通路区分の入口から弁開
口通路への長さが制限される。したがつて通路を
通つて流れる空気は案内羽根によつて一方では螺
旋形の通路内に、他方では弁開口通路内に強制さ
れて流入する。
A swirl-forming channel of this type consists essentially of three channel sections, starting from the cylinder of the internal combustion engine, the first channel section being a cylindrical valve opening channel section, which The channel section connected to the open channel section is designed as a helically wound channel section, and the channel section connected to this channel section is designed as an S-curved guide channel section. The guide channel section leading from the so-called deflection point to the so-called spiral point with such a channel configuration advantageously has a channel cross section that does not change over its entire length and has a helical channel section with the same cross section. is moving to. The helical channel section forming the connection section from the guide channel section to the inlet opening of the valve opening channel section also has an unchanged cross section. In this case the spacing from each side wall to the spiral point is the same or approximately the same. The valve guide and the walls of the guide passage adjacent to the valve guide are arranged so that, on the one hand, the helix point is located in the passage cross-section through the valve guide, and on the other hand, the guide passage can be brought hydrodynamically satisfactorily close to the helix point. A guide vane is provided between the two. This guide vane is connected at its root to the wall of the guide channel and at its tip to the valve guide. This guide vane limits the length of the helical passage section from the inlet to the valve opening passage. The air flowing through the channel is therefore forced by the guide vanes into the helical channel on the one hand and into the valve opening channel on the other hand.

本発明の課題はこのような通路か出発して、特
に螺旋形の通路区分を、空気が特に強く螺旋形の
通路区分の一方の壁、つまり弁開口通路の開口と
反対側の壁に押しつけられるように改良し、これ
によつて空気が目標を定めてかつ高速度で、しか
も強い渦流が与えられた状態で内燃機関のシリン
ダ内に達するようにすることである。
The object of the invention is to start from such a passage, in particular a helical passage section, in which the air is particularly strongly pressed against one wall of the helical passage section, that is to say on the wall opposite to the opening of the valve opening passage. The object of the present invention is to improve the air flow so that the air reaches the cylinders of an internal combustion engine in a targeted manner and at a high velocity and with a strong turbulence.

この課題は本発明によれば螺旋形の通路区分の
横断面が入口から弁開口通路まで台形に構成され
ていることによつて解決された。
This object is achieved according to the invention in that the cross section of the helical channel section is trapezoidal from the inlet to the valve opening channel.

通路、特に螺旋形の通路区分を台形に構成する
ことによつて、空気は傾斜した両方の面あるいは
壁を擦過するときに台形横断面の頂面側から台形
横断面の底面に押しつけられる。このばあいこの
押しつけ力は同様に台形に合わせられた案内羽根
の傾斜した案内面によつて強められる。このよう
な形式で空気は螺施面、つまり台形の底面に導か
れ、これによつて内燃機関のシリンダに円筒状に
開口する弁開口通路内に導かれる。実験が示すよ
うに、このように構成された螺旋形の通路区分に
よつてはきわめて良好な渦流が得られる。したが
つてこの渦流によつては燃料と燃焼空気との間に
きわめて良好な混合が得られる。
Due to the trapezoidal configuration of the channel, in particular the helical channel section, the air is forced from the top side of the trapezoidal cross section to the bottom side of the trapezoidal cross section as it passes over both inclined surfaces or walls. In this case, this pressing force is likewise increased by the inclined guide surfaces of the trapezoidal guide vanes. In this way, the air is guided through the threaded surface, ie the trapezoidal base, and thereby into the valve opening channel which opens cylindrically into the cylinder of the internal combustion engine. Experiments have shown that a helical channel section configured in this way provides a very good swirling flow. This vortex therefore results in very good mixing between the fuel and the combustion air.

さらに本発明の別の実施例によれば台形の横断
面の底面は弁開口通路の開口と反対側に位置して
いる。
According to a further embodiment of the invention, the bottom surface of the trapezoidal cross section is located opposite the opening of the valve opening channel.

通路の螺旋形の区分における隘路を避けるため
には、台形に構成された螺旋形の通路区分の、弁
開口通路に向かつて傾斜した側壁の中央範囲は、
側壁から螺旋軸線までに同じであるかほぼ同じで
ある間隔を有している。
In order to avoid bottlenecks in the helical section of the passage, the central region of the side wall of the trapezoidally configured helical passage section is inclined towards the valve opening passage.
They have the same or approximately the same spacing from the sidewalls to the helical axis.

次に図面について本発明を説明する: 本発明による通路はほぼ3つの通路区分から形
成されている。これらの3つの通路区分の内1つ
の通路区分は内燃機関のシリンダに接続されてお
りかつ弁開口通路区分3として構成されている。
この弁開口通路区分3に接続された螺旋形の通路
区分4は、弁開口通路区分3と螺旋形の通路区分
に接続された案内通路区分5との間に配置されて
いる。この案内通路区分5の、螺旋形の通路区分
とは反対側の端部は吸気管15に開口している。
シリンダ軸線Xと弁軸線Vとを通る通路横断面K
と、吸気管15に案内通路区分5が開口してい
る、通路横断面Kに対して平行な通路横断面
K′との間に位置している案内通路区分5は有利
にはS字形に湾曲せしめられておりかつ円形ある
いは方形の横断面から螺旋形の通路区分4の台形
の横断面に移行している。螺旋形の通路区分4は
その入口から弁開口通路区分3まで台形に構成さ
れており、このばあい台形の底面16は弁開口通
路区分3の開口と反対側に位置している。側壁1
8と19ならびに底面16とこの底面と向きあつ
ている頂面17とから成る台形の通路区分4は一
定の勾配を有する螺線に沿つて弁開口に向かつて
傾斜して配置されておりかつ弁案内9を案内通路
区分5の壁と結合する案内羽根7も同様に弁開口
通路区分3に向かつて傾斜した案内面を備えてい
る。螺旋形の通路区分4の螺旋軸線Yは間隔aだ
け弁の縦中心軸線から、つまり弁軸線Vからずら
されている。したがつて螺旋形の通路区分はこの
軸線を中心として弁開口通路区分3に向かつて巻
かれている。螺旋形の通路区分の側壁18,19
を一層判りやすくするためにこれは第2図におい
てはハツチングで示されている。螺旋形の通路区
分4がこのように構成されていることによつてこ
れを通過する空気20は側方に傾斜せしめられた
壁18,19により台形状の通路横断面の底面1
6にたいして押しつけられる。これによつて空気
にはきわめて強い渦流が与えられる。通路1の偏
向点はこの実施例のばあいにも直線E上に位置し
て通路1内を通る空気20は螺旋形の通路区分4
に与えられている形状によつて弁開口通路区分3
内に導入される。この弁開口通路内で空気は渦流
状態を維持したままでシリンダ壁によつて引続き
案内される。側壁18から螺旋軸線Yまでの間隔
b間隔は側壁18の傾斜位置を考慮すれば同じで
あるかあるいはほぼ同じである。このばあいこの
間隔は有利には側壁18の適当な中央範囲21で
測定される。
The invention will now be explained with reference to the drawings: The passage according to the invention is formed from approximately three passage sections. One of these three passage sections is connected to the cylinder of the internal combustion engine and is designed as a valve opening passage section 3.
A helical passage section 4 connected to this valve opening passage section 3 is arranged between the valve opening passage section 3 and a guide passage section 5 connected to the helical passage section. The end of this guide channel section 5 opposite to the helical channel section opens into the intake pipe 15 .
Passage cross section K passing through cylinder axis X and valve axis V
and a passage cross-section parallel to the passage cross-section K, in which the guide passage section 5 opens into the intake pipe 15.
The guide channel section 5 located between K' is preferably curved in an S-shape and passes from a circular or square cross section to a trapezoidal cross section of the helical channel section 4. . The helical passage section 4 is trapezoidally configured from its inlet to the valve opening passage section 3, the bottom surface 16 of the trapezoid being located opposite the opening of the valve opening passage section 3. side wall 1
8 and 19 as well as a bottom surface 16 and a top surface 17 facing this bottom surface, the trapezoidal passage section 4 is arranged inclined toward the valve opening along a spiral with a constant slope and is arranged inclined towards the valve opening. The guide vane 7, which connects the guide 9 with the wall of the guide channel section 5, likewise has a guide surface that is inclined towards the valve opening channel section 3. The helical axis Y of the helical passage section 4 is offset from the central longitudinal axis of the valve, ie from the valve axis V, by a distance a. The helical channel section is therefore wound around this axis towards the valve opening channel section 3. Side walls 18, 19 of the helical passage section
In order to make it easier to understand, this is indicated by hatching in FIG. Due to this embodiment of the helical channel section 4, the air 20 passing through it is influenced by the laterally inclined walls 18, 19 to the bottom surface 1 of the trapezoidal channel cross section.
It is forced against 6. This gives the air an extremely strong vortex. The point of deflection of the channel 1 is also located on the straight line E in this embodiment, so that the air 20 passing through the channel 1 is guided by the helical channel section 4.
By the shape given to the valve opening passage section 3
be introduced within. In this valve opening channel, the air continues to be guided by the cylinder wall in a swirling state. The distance b from the side wall 18 to the helical axis Y is the same or approximately the same if the inclined position of the side wall 18 is considered. In this case, this distance is preferably measured in a suitable central region 21 of the side wall 18.

本発明の通路を用いた十分な実験の結果、台形
の通路区分4の横断面は所望の渦流状態を得るた
めには行程容積リツトルあたりほぼ10cm2であると
有利であることが判つた。もちろんこの値は機関
の大きさと出力に相応してこれらの値に比例して
変えることができる。
After considerable experimentation with the passage of the invention, it has been found that it is advantageous for the cross-section of the trapezoidal passage section 4 to be approximately 10 cm 2 per liter of stroke volume in order to obtain the desired swirling conditions. Of course, this value can be varied proportionally to these values, depending on the size and power of the engine.

第2図に示された通路の1実施例においては、
S字形に湾曲された案内通路区分5は螺旋形の通
路区分4に面した端部において同様に台形に構成
されている。このばあい横断面の底面16は、S
字形に湾曲された案内通路区分5と螺旋形の通路
区分4との移行部において既に傾斜しはじめる。
この傾斜は第2図に示されているようにαに瓦つ
ている。この螺旋形成角αはシリンダ2に供給さ
れる空気に十分な渦流状態を与えるためには少な
くとも220°でなければならない。
In one embodiment of the passageway shown in FIG.
At its end facing the helical channel section 4, the S-shaped guide channel section 5 is likewise trapezoidally designed. In this case, the bottom surface 16 of the cross section is S
Already at the transition between the curved guide channel section 5 and the helical channel section 4 it begins to slope.
This slope is skewed to α as shown in FIG. This helix formation angle α must be at least 220° in order to provide the air supplied to the cylinder 2 with a sufficient swirling state.

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

図面は本発明の1実施例を示すものであつて、
第1図は本発明の通路の螺旋形の通路区分の第2
図の―線に沿つた横断面図、第2図は第1図
の―線に沿つた断面図である。 1…通路、2…シリンダ、3に…弁開口通路区
分、4…螺旋形の通路区分、5…案内通路区分、
7…案内羽根、9…弁案内、14…偏向点、15
…吸気導管、16…底面、17…頂面、18,1
9…側壁、20…空気、21…中央範囲。
The drawings show one embodiment of the invention,
FIG. 1 shows the second helical passage section of the passage of the present invention.
FIG. 2 is a cross-sectional view taken along line - in FIG. 1, and FIG. 2 is a cross-sectional view taken along line - in FIG. 1... passage, 2... cylinder, 3... valve opening passage section, 4... spiral passage section, 5... guide passage section,
7... Guide vane, 9... Valve guide, 14... Deflection point, 15
...Intake conduit, 16...Bottom surface, 17...Top surface, 18,1
9...Side wall, 20...Air, 21...Central range.

Claims (1)

【特許請求の範囲】 1 往復動ピストン式内燃機関の吸気系における
渦流形成通路であつて、この渦流形成通路内を通
過せしめられるガス状の媒体に回転運動を与える
ために、渦流形成通路が所望の渦流形成方向に曲
げられており、シリンダヘツドに位置する吸気弁
を有していて、渦流形成通路が螺旋形に曲げられ
た通路区分4とこれに接続するS字形に湾曲させ
られた案内通路区分5とを有しており、螺旋形の
通路区分4がS字形に湾曲させられた案内通路区
分5とシリンダ室との間に設けられていて、S字
形に湾曲させられた案内通路区分5の一方の端点
がシリンダ軸線Xと弁軸線Vとを通る通路横断面
Kの上に位置しかつ他方の端点が吸気管に対する
案内通路区分5の開口15が位置する、前記通路
横断面Kに対して平行に延びる通路横断面K′の
上に位置しており、螺旋形の通路区分4の螺旋軸
線Yがシリンダ軸線Xと弁軸線Vとを通る通路横
断面Kの上に、弁軸線Vにたいして偏心的に配置
されていて、螺旋形の通路区分4がほぼ一定の勾
配と少なくとも220℃の螺旋形成角αとを有する
螺線に沿つて配置されていてかつ螺旋軸線Yとこ
れに向き合つている通路側壁18との間にほぼ一
定の間隔bを有していて、螺旋形の通路区分4の
シリンダ室に向いた端部が円筒状の弁開口通路区
分3を介してシリンダ室に開口している形式のも
のにおいて、螺旋形の通路区分4の横断面が入口
から弁開口通路区分3まで台形に構成されている
ことを特徴とする、渦流形成通路。 2 台形の横断面の底辺が弁開口通路区分3の開
口とは反対側に位置している、特許請求の範囲第
1項記載の渦流形成通路。
[Scope of Claims] 1. A vortex forming passage in the intake system of a reciprocating piston internal combustion engine, where the vortex forming passage is desired in order to impart rotational motion to a gaseous medium passed through the vortex forming passage. a passage section 4 which is bent in the direction of vortex formation and has an intake valve located in the cylinder head, the vortex formation passage being helically bent, and a guide passage connected thereto which is curved in an S-shape; a helical passage section 4 is provided between the S-shaped curved guide passage section 5 and the cylinder chamber; for said passage cross-section K, one end point of which lies on said passage cross-section K passing through the cylinder axis X and the valve axis V, and the other end point of which lies the opening 15 of the guide passage section 5 for the intake pipe. The spiral axis Y of the helical passage section 4 lies on a passage cross section K, which runs parallel to the cylinder axis eccentrically arranged, the helical channel section 4 is arranged along a helix having a substantially constant slope and a helix forming angle α of at least 220° C. and facing the helical axis Y; The end of the helical passage section 4 facing the cylinder chamber opens into the cylinder chamber via the cylindrical valve opening passage section 3. Swirl-forming channel of the type characterized in that the cross-section of the helical channel section 4 from the inlet to the valve opening channel section 3 is trapezoidally configured. 2. Swirl-forming channel according to claim 1, wherein the base of the trapezoidal cross section is located on the opposite side of the opening of the valve opening channel section 3.
JP59167969A 1972-08-29 1984-08-13 Vortex stream forming passage Granted JPS60101246A (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE2242383.2 1972-08-29
DE2242383A DE2242383A1 (en) 1972-08-29 1972-08-29 SPIRAL CHANNEL, ESPECIALLY IN THE INTAKE SYSTEM OF RECIPROCATING PISTON INTERNAL ENGINEERING MACHINES

Publications (2)

Publication Number Publication Date
JPS60101246A JPS60101246A (en) 1985-06-05
JPS6234935B2 true JPS6234935B2 (en) 1987-07-29

Family

ID=5854841

Family Applications (2)

Application Number Title Priority Date Filing Date
JP48096549A Pending JPS4951409A (en) 1972-08-29 1973-08-28
JP59167969A Granted JPS60101246A (en) 1972-08-29 1984-08-13 Vortex stream forming passage

Family Applications Before (1)

Application Number Title Priority Date Filing Date
JP48096549A Pending JPS4951409A (en) 1972-08-29 1973-08-28

Country Status (10)

Country Link
JP (2) JPS4951409A (en)
KR (1) KR780000181B1 (en)
DD (1) DD114295A6 (en)
DE (1) DE2242383A1 (en)
FR (1) FR2198059B2 (en)
GB (1) GB1442605A (en)
HU (1) HU169184B (en)
IT (1) IT1045375B (en)
RO (1) RO68683A (en)
SE (1) SE403817B (en)

Families Citing this family (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5924851Y2 (en) * 1977-01-14 1984-07-23 ヤンマーディーゼル株式会社 Air supply path for internal combustion engines
JPS5849382Y2 (en) * 1978-09-19 1983-11-11 トヨタ自動車株式会社 Internal combustion engine helical intake port
JPS5932647B2 (en) * 1978-09-25 1984-08-10 トヨタ自動車株式会社 Helical intake port for internal combustion engines
JPS5920850B2 (en) * 1978-09-25 1984-05-16 トヨタ自動車株式会社 Helical intake port for internal combustion engines
JPS5840647B2 (en) * 1978-10-19 1983-09-07 トヨタ自動車株式会社 Internal combustion engine intake system
JPS6124670Y2 (en) * 1981-02-27 1986-07-24
BR8203421A (en) * 1981-06-15 1983-06-07 Deere & Co HELICOIDAL ADMISSION OPENING
JPS5912125A (en) * 1982-07-12 1984-01-21 Toyota Central Res & Dev Lab Inc Inlet port of internal combustion engine
JPS5951129A (en) * 1982-09-18 1984-03-24 Toyota Central Res & Dev Lab Inc Intake port of internal-combustion engine
EP0257646B1 (en) * 1986-08-28 1992-01-29 Bando Chemical Industries, Ltd. V belt with blocks
IT1305199B1 (en) * 1998-11-23 2001-04-10 Fiat Auto Spa INTERNAL COMBUSTION ALTERNATIVE ENGINE, PARTICULARLY OF THE DIRECT ADINJECTION TYPE, AND ITS ASPIRATION FILLING OF ONE OF ITS
FR2871523B1 (en) * 2004-06-10 2009-02-13 Renault Sas INTAKE DUCT WITH OPTIMIZED PASSAGE SECTION FOR INTERNAL COMBUSTION ENGINE
US10337449B2 (en) * 2017-01-02 2019-07-02 Ford Global Technologies, Llc Internal combustion engine with cylinder head
SE540850C2 (en) * 2017-02-03 2018-11-27 Scania Cv Ab A compression ignited combustion engine
CN115324764A (en) * 2022-10-14 2022-11-11 潍柴动力股份有限公司 Air inlet channel structure of cylinder cover and gas engine

Also Published As

Publication number Publication date
FR2198059A2 (en) 1974-03-29
JPS4951409A (en) 1974-05-18
HU169184B (en) 1976-10-28
JPS60101246A (en) 1985-06-05
SE403817B (en) 1978-09-04
DE2242383A1 (en) 1974-03-14
RO68683A (en) 1980-10-30
IT1045375B (en) 1980-05-10
FR2198059B2 (en) 1977-05-13
GB1442605A (en) 1976-07-14
KR780000181B1 (en) 1978-05-13
DD114295A6 (en) 1975-07-20

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