Deprecated: The each() function is deprecated. This message will be suppressed on further calls in /home/zhenxiangba/zhenxiangba.com/public_html/phproxy-improved-master/index.php on line 456
JPH0337032B2 - - Google Patents
[go: Go Back, main page]

JPH0337032B2 - - Google Patents

Info

Publication number
JPH0337032B2
JPH0337032B2 JP19162382A JP19162382A JPH0337032B2 JP H0337032 B2 JPH0337032 B2 JP H0337032B2 JP 19162382 A JP19162382 A JP 19162382A JP 19162382 A JP19162382 A JP 19162382A JP H0337032 B2 JPH0337032 B2 JP H0337032B2
Authority
JP
Japan
Prior art keywords
inner circumferential
circumferential surface
cylinder
turbocharger
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.)
Expired - Lifetime
Application number
JP19162382A
Other languages
Japanese (ja)
Other versions
JPS5982569A (en
Inventor
Akira Kageyama
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 JP57191623A priority Critical patent/JPS5982569A/en
Publication of JPS5982569A publication Critical patent/JPS5982569A/en
Publication of JPH0337032B2 publication Critical patent/JPH0337032B2/ja
Granted legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M35/00Combustion-air cleaners, air intakes, intake silencers, or induction systems specially adapted for, or arranged on, internal-combustion engines
    • F02M35/10Air intakes; Induction systems
    • F02M35/104Intake manifolds
    • F02M35/112Intake manifolds for engines with cylinders all in one line
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M35/00Combustion-air cleaners, air intakes, intake silencers, or induction systems specially adapted for, or arranged on, internal-combustion engines
    • F02M35/10Air intakes; Induction systems
    • F02M35/10006Air intakes; Induction systems characterised by the position of elements of the air intake system in direction of the air intake flow, i.e. between ambient air inlet and supply to the combustion chamber
    • F02M35/10026Plenum chambers
    • F02M35/10052Plenum chambers special shapes or arrangements of plenum chambers; Constructional details
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M35/00Combustion-air cleaners, air intakes, intake silencers, or induction systems specially adapted for, or arranged on, internal-combustion engines
    • F02M35/10Air intakes; Induction systems
    • F02M35/1015Air intakes; Induction systems characterised by the engine type
    • F02M35/10157Supercharged engines
    • 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)
  • Physics & Mathematics (AREA)
  • Geometry (AREA)
  • Characterised By The Charging Evacuation (AREA)

Description

【発明の詳細な説明】 (産業上の利用分野) 本発明は、ターボ過給機付エンジンの吸気装置
の改良に関するものである。
DETAILED DESCRIPTION OF THE INVENTION (Field of Industrial Application) The present invention relates to an improvement in an intake system for a turbocharged engine.

(従来の技術) 従来より、吸気通路の途中に拡大室を設け、吸
入空気を貯留するようにした吸気装置がある(例
えば米国特許第4183332号明細書参照)。そして、
上記拡大室は燃料噴射方式のエンジン、特にデイ
ーゼルエンジンにおいては大容量のものが要求さ
れる。
(Prior Art) Conventionally, there has been an intake device in which an enlarged chamber is provided in the middle of an intake passage to store intake air (for example, see US Pat. No. 4,183,332). and,
The enlarged chamber is required to have a large capacity in a fuel injection type engine, especially a diesel engine.

(発明が解決しようとする課題) しかして、自動車等においては、エンジンの設
置スペースは制約される関係上、上記拡大室の形
成とともにターボ過給機を付設したものでは、吸
気装置が大きくなるので、そのコンパクト化を図
るために、吸気通路を屈曲して形成することにな
る。しかし、ターボ過給機からエンジンの気筒に
至る吸気通路が屈曲し角部が形成されると、充填
効率が低下して過給効果が減少する問題がある。
特にエンジンの一側面に吸気ポートと排気ポート
とが開口しているカウンタフロー型のエンジンに
おいては、吸気通路と排気通路とが接近している
ため、必要容積の拡大室を確保し、かつ、空気の
流れを阻害することなく良好な過給効果を得ると
ともに、コンパクトな配置構造を得ることは困難
であつた。
(Problem to be Solved by the Invention) However, in automobiles, etc., the installation space for the engine is limited, so if the enlarged chamber is formed and a turbo supercharger is attached, the intake system becomes large. In order to make it more compact, the intake passage is formed with a bend. However, when the intake passage from the turbocharger to the cylinder of the engine is bent and corners are formed, there is a problem in that the charging efficiency decreases and the supercharging effect decreases.
In particular, in a counterflow type engine where the intake port and exhaust port are opened on one side of the engine, the intake passage and exhaust passage are close to each other, so it is possible to secure an enlarged chamber with the required volume and to It has been difficult to obtain a good supercharging effect without obstructing the flow of fuel and to obtain a compact arrangement structure.

本発明はかかる点に鑑みてなされたもので、カ
ウンタフロー型のターボ過給機付エンジンにおい
て、大容積の拡大室を備え、しかも過給効果を低
減することなくコンパクト化を図ることを目的と
する。
The present invention has been made in view of the above, and an object of the present invention is to provide a counterflow type turbocharged engine with a large-volume expansion chamber and to make it more compact without reducing the supercharging effect. do.

(課題を解決するための手段) 上記の目的を達成するため、本発明の解決手段
は、吸気通路にターボ過給機を備えるとともに、
吸気ポートと排気ポートとが同一側面に開口した
カウンタフロー型の多気筒エンジンを前提とす
る。上記ターボ過給機下流の吸気通路には略円筒
状の拡大室が設けられ、該拡大室とターボ過給機
とは上下位置に配置されているとともに、該拡大
室はその円筒軸線方向が気筒列方向とほぼ平行に
なるように配置されている。上記拡大室は、円弧
状の第1内周面と、該第1内周面の接線方向にタ
ーボ過給機からの圧縮空気を導入する導入通路が
開口する流入口と、該流入口より円筒軸線方向に
離れた位置において上記第1内周面と滑らかに連
続する円弧状の第2内周面と、上記流入口から第
1内周面及び第2内周面に沿つて転向した圧縮空
気を第2内周面の接続方向に排出して各気筒に供
給する導出通路がそれぞれ開口する複数の流出口
とを備えてなるものとする。
(Means for Solving the Problems) In order to achieve the above object, the solving means of the present invention includes a turbo supercharger in the intake passage, and
The assumption is that the engine is a counterflow type multi-cylinder engine in which the intake port and exhaust port are open on the same side. A substantially cylindrical enlarged chamber is provided in the intake passage downstream of the turbocharger, and the enlarged chamber and the turbocharger are arranged vertically, and the direction of the cylindrical axis of the enlarged chamber is aligned with the cylinder. They are arranged almost parallel to the column direction. The enlarged chamber has a first inner circumferential surface having a circular arc shape, an inlet in which an introduction passage for introducing compressed air from the turbocharger opens in a tangential direction of the first inner circumferential surface, and a cylindrical shape extending from the inlet. an arcuate second inner circumferential surface that smoothly continues with the first inner circumferential surface at a position separated from the axial direction; and compressed air diverted from the inlet along the first inner circumferential surface and the second inner circumferential surface. A plurality of outlet ports are provided, each of which has a derivation passage opening in the connection direction of the second inner circumferential surface and supplies the gas to each cylinder.

(作用) これにより、本発明では、ターボ過給機からの
圧縮空気は、拡大室に対し導入通路より流入口を
経て第1内周面の接続方向に流入し、この第1内
周面及びこれに滑らかに連続する第2内周面に沿
つて転向した後、この第2内周面の接線方向に開
口している流出口から各導出通路に排出され、吸
気マニホールドを経て吸気ポートから各気筒に供
給される。したがつて、圧縮空気の流れに乱れや
縮流を生じさせることなく圧縮空気を各気筒に過
給することができる。
(Function) Accordingly, in the present invention, compressed air from the turbocharger flows into the expansion chamber from the introduction passage through the inlet in the direction in which the first inner circumferential surface and the first inner circumferential surface are connected. After turning along the second inner circumferential surface that is smoothly continuous with this, it is discharged from the outlet opening in the tangential direction of this second inner circumferential surface to each outlet passage, passes through the intake manifold, and exits each intake port from the intake port. supplied to the cylinder. Therefore, compressed air can be supercharged to each cylinder without causing turbulence or contraction in the flow of compressed air.

さらに、この場合、カウンタフロー型のエンジ
ンであつても、拡大室とターボ過給機とを上下に
配置したこと、及び拡大室の円筒軸線方向が気筒
列方向と略平行であることによつて、拡大室及び
ターボ過給機をレイアウト上無理なくコンパクト
に配置することができる。
Furthermore, in this case, even if it is a counterflow type engine, the expansion chamber and the turbocharger are arranged vertically, and the cylindrical axis direction of the expansion chamber is approximately parallel to the cylinder row direction. , the expansion chamber and the turbocharger can be arranged compactly and without difficulty in terms of layout.

(実施例) 以下、本発明の実施例を図面に沿つて説明す
る。第1図及び第2図において、1はカウンタフ
ロー型の多気筒(4気筒)デイーゼルエンジン、
2は該エンジン1の各気筒の吸気ポート3に空気
を供給する吸気通路、4は各気筒の排気ポート
(図示せず)からの排気ガスを導出する排気通路
である。なお、6はシリンダヘツド、7はヘツド
カバー、8はシリンダブロツクである。
(Example) Examples of the present invention will be described below with reference to the drawings. In FIGS. 1 and 2, 1 is a counterflow type multi-cylinder (4-cylinder) diesel engine;
2 is an intake passage that supplies air to the intake port 3 of each cylinder of the engine 1, and 4 is an exhaust passage that leads out exhaust gas from an exhaust port (not shown) of each cylinder. Note that 6 is a cylinder head, 7 is a head cover, and 8 is a cylinder block.

一方、9は吸気通路2の途中に介装されたター
ボ過給機、10は該ターボ過給機9より下流の吸
気通路2に設けられかつターボ過給機9の上方位
置に配置された拡大室である。上記ターボ過給機
9は排気通路4を流下する排気ガスによつて駆動
されるタービン9aでブロア9bを回転し、過給
を行うものである。
On the other hand, 9 is a turbo supercharger installed in the middle of the intake passage 2, and 10 is an enlarged turbo supercharger installed in the intake passage 2 downstream of the turbo supercharger 9 and located above the turbo supercharger 9. It is a room. The turbo supercharger 9 uses a turbine 9a driven by exhaust gas flowing down the exhaust passage 4 to rotate a blower 9b to perform supercharging.

排気通路4は、排気ポートから下方に湾曲して
排気ガスを集合する排気マニホールド4aが上記
ターボ過給機9のタービン9aに接続され、この
タービン9aの出口に排気管4bが接続されて構
成されている。
The exhaust passage 4 includes an exhaust manifold 4a that curves downward from an exhaust port and collects exhaust gas, and is connected to a turbine 9a of the turbocharger 9, and an exhaust pipe 4b is connected to the outlet of the turbine 9a. ing.

吸気通路2は、吸気ポート3から上方に湾曲し
た吸気マニホールド2aが拡大室10に接続さ
れ、この拡大室10が上記ターボ過給機9のブロ
ア9bに接続され、このブロア9bの入口にエア
クリーナ(図示せず)からの空気を供給する吸気
管2bが接続されて構成されている。
In the intake passage 2, an intake manifold 2a curved upward from the intake port 3 is connected to an enlarged chamber 10, this enlarged chamber 10 is connected to the blower 9b of the turbo supercharger 9, and an air cleaner ( An intake pipe 2b that supplies air from a pipe (not shown) is connected thereto.

上記拡大室10は全体として略円筒状に形成さ
れ、その円筒軸線方向が気筒列方向と略平行にな
るように配置されており、拡大室10の中央部分
はシリンダヘツド6側に屈曲している。この拡大
室10の中央部分の下方にターボ過給機9のブロ
ア9bの出口からの圧縮空気を導入する導入通路
11が接続される一方、拡大室10の左右にそれ
ぞれ圧縮空気を各気筒に供給する2つずつの導出
通路12が接続されている。
The enlarged chamber 10 is formed into a generally cylindrical shape as a whole, and is arranged so that the cylindrical axis direction is substantially parallel to the cylinder row direction, and the central portion of the enlarged chamber 10 is bent toward the cylinder head 6 side. . An introduction passage 11 that introduces compressed air from the outlet of the blower 9b of the turbocharger 9 is connected to the lower part of the center of the expansion chamber 10, while compressed air is supplied to each cylinder on the left and right sides of the expansion chamber 10, respectively. Two outlet passages 12 are connected to each other.

拡大室10の中央部分のシリンダヘツド6側の
内面には円弧状の第1内周面10aが形成され、
さらに、この中央部分の下方には、上記ターボ過
給機9による圧縮空気を第1内周面10aの接線
方向から導入する導入通路11が開口する流入口
10bが開設されている。また、上記中央部分の
シリンダヘツド6と反対側内面は内方に突出し、
第1内周面10aを沿つて流れる圧縮空気を左右
に分流させる分流部10cに形成され、この分流
部10cの左右には、流入口10bから円筒軸線
方向に離れた位置において上記第1内周面10a
と滑らかに連続する円弧状の第2内周面10dが
それぞれ形成されている。さらに、拡大室10の
両側部分におけるシリンダヘツド側の下方には、
圧縮空気を第2内周面10dの接続方向に排出す
る導出通路12がそれぞれ開口する4つの流出口
10eが開設され、この流出口10eの周縁は
徐々に絞られるような曲面に形成されている。
An arc-shaped first inner circumferential surface 10a is formed on the inner surface of the central portion of the enlarged chamber 10 on the cylinder head 6 side.
Furthermore, an inlet 10b is provided below this central portion, through which an introduction passage 11 opens, through which compressed air from the turbocharger 9 is introduced from the tangential direction of the first inner circumferential surface 10a. Further, the inner surface of the central portion opposite to the cylinder head 6 protrudes inward,
A dividing portion 10c is formed to divide the compressed air flowing along the first inner circumferential surface 10a to the left and right, and on the left and right sides of the dividing portion 10c, the first inner circumferential Surface 10a
A second inner circumferential surface 10d having a circular arc shape and smoothly continuous with each other is formed. Further, below the cylinder head side on both sides of the enlarged chamber 10,
Four outlet ports 10e are provided, each having an outlet passage 12 for discharging the compressed air in the connection direction of the second inner circumferential surface 10d, and the peripheral edge of the outlet port 10e is formed into a curved surface that gradually narrows. .

上記実施例の作用について説明すれば、ターボ
過給機9による圧縮空気は、拡大室10に対して
シリンダヘツド6の反対側下方より、導入通路1
1から流入口10bを経て第1内周面10aの接
続方向に流入し、この第1内周面10aに沿つて
上方に転向した後、シリンダヘツド6と反対側の
分流部10cで左右に分流するとともに、第2内
周面10dに沿つて下方に転向し、この第2内周
面10dの接続方向に開口している流出口10e
から各導出通路12に排出され、吸気マニホール
ド2aを経て吸気ポート3から各気筒に供給され
る。
To explain the operation of the above embodiment, compressed air from the turbocharger 9 is introduced into the introduction passage 1 from below on the opposite side of the cylinder head 6 to the expansion chamber 10.
1 flows in the connection direction of the first inner circumferential surface 10a through the inlet 10b, turns upward along the first inner circumferential surface 10a, and then is divided to the left and right at the flow dividing portion 10c on the opposite side from the cylinder head 6. At the same time, the outlet 10e turns downward along the second inner circumferential surface 10d and opens in the connection direction of the second inner circumferential surface 10d.
The air is discharged from the air into each outlet passage 12, and is supplied to each cylinder from the intake port 3 via the intake manifold 2a.

本発明は上記実施例の構造に限定されるもので
はなく、種々の変形例に包含している。すなわ
ち、上記実施例では、拡大室10の中央部分をシ
リンダヘツド6側に近付けて形成し、圧縮空気の
左右への分流を良好に行うとともに、ターボ過給
機9の配設位置をシリンダヘツド6に近付けるよ
うにしているが、この中央部分を左右部分と同様
に形成し、拡大室10を完全な円筒状としてもよ
く、ターボ過給機9の接続位置も中央部分に限定
されない。
The present invention is not limited to the structure of the above embodiment, but includes various modifications. That is, in the embodiment described above, the central portion of the enlarged chamber 10 is formed close to the cylinder head 6 side, so that the compressed air can be divided to the left and right well, and the turbocharger 9 is disposed close to the cylinder head 6 side. However, the central portion may be formed in the same manner as the left and right portions, and the enlarged chamber 10 may have a completely cylindrical shape, and the connection position of the turbocharger 9 is not limited to the central portion.

また、上記実施例ではターボ過給機9を下方
に、拡大室10を上方に配設しているのに対し、
この配置は上下反対にしてもよいが、上記実施例
のように拡大室10を上方に配置する方が、他の
補機との関係に基づくレイアウト上好ましい。さ
らに、拡大室10と吸気マニホールド2aとの形
成は、一体的に形成するほか、その製作に応じて
上下もしくは左右に適宜分割形成される。
Further, in the above embodiment, the turbocharger 9 is arranged below and the expansion chamber 10 is arranged above, whereas
Although this arrangement may be reversed, it is preferable to arrange the enlargement chamber 10 upward as in the above embodiment from the standpoint of layout based on the relationship with other auxiliary machines. Further, the enlarged chamber 10 and the intake manifold 2a may be formed integrally or may be divided vertically or horizontally depending on the manufacturing thereof.

(発明の効果) 以上説明したように、本発明によれば、カウン
タフロー型のターボ過給機付エンジンにおいて、
ターボ過給機の下流側の吸気通路に設けられる円
筒状拡大室は、滑らかに連続した第1内周面と第
2内周面とを有し、流入口から第1内周面の接線
方向に圧縮空気を導入し、第1及び第2内周面に
沿つて転向させて、流出口から第2内周面の接線
方向に排出して各気筒に供給するようにしたこと
により、圧縮空気の流れに乱れおよび縮流を発生
させることなく、その吸入空気量の低下を阻止し
て過給効果を十分に発揮させることができる。し
かも、拡大室とターボ過給機との上下配置及び拡
大室の円筒軸線の気筒列方向と平行な配置によ
り、拡大室及びターボ過給機をコンパクトに配置
でき、良好なレイアウトのエンジンを得ることが
できる利点を有する。
(Effects of the Invention) As explained above, according to the present invention, in a counterflow type turbocharged engine,
The cylindrical enlarged chamber provided in the intake passage on the downstream side of the turbocharger has a first inner circumferential surface and a second inner circumferential surface that are smoothly continuous, and has a tangential direction from the inlet to the first inner circumferential surface. Compressed air is introduced into the cylinder, diverted along the first and second inner circumferential surfaces, and discharged from the outlet in the tangential direction of the second inner circumferential surface to be supplied to each cylinder. It is possible to prevent the intake air amount from decreasing and to fully exhibit the supercharging effect without causing turbulence or contraction in the flow of air. Furthermore, by vertically arranging the expansion chamber and the turbocharger and arranging the cylindrical axis of the expansion chamber parallel to the cylinder row direction, the expansion chamber and the turbocharger can be arranged compactly, and an engine with a good layout can be obtained. It has the advantage of being able to

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

図面は本発明の一実施例を図示し、第1図は平
面図、第2図は第1図の−線に沿う断面図で
ある。 1……デイーゼルエンジン、2……吸気通路、
3……吸気ポート、4……排気通路、9……ター
ボ過給機、10……拡大室、10a……第1内周
面、10b……流入口、10c……分流部、10
d……第2内周面、10e……流出口、11……
導入通路、12……導出通路。
The drawings illustrate one embodiment of the present invention, with FIG. 1 being a plan view and FIG. 2 being a sectional view taken along the line - in FIG. 1. 1... Diesel engine, 2... Intake passage,
3... Intake port, 4... Exhaust passage, 9... Turbo supercharger, 10... Expansion chamber, 10a... First inner peripheral surface, 10b... Inflow port, 10c... Diversion section, 10
d... Second inner peripheral surface, 10e... Outlet, 11...
Introductory passageway, 12... Leading-out passageway.

Claims (1)

【特許請求の範囲】 1 吸気通路にターボ過給機を備えるとともに、
吸気ポートと排気ポートとが同一側面に開口した
カウンタフロー型の多気筒エンジンにおいて、 上記ターボ過給機下流の吸気通路には略円筒状
の拡大室が設けられ、該拡大室とターボ過給機と
は上下位置に配置されているとともに、該拡大室
はその円筒軸線方向が気筒列方向とほぼ平行にな
るように配置されており、 上記拡大室は、円弧状の第1内周面と、該第1
内周面の接線方向にターボ過給機からの圧縮空気
を導入する導入通路が開口する流入口と、該流入
口より円筒軸線方向に離れた位置において上記第
1内周面と滑らかに連続する円弧状の第2内周面
と、上記流入口から第1内周面及び第2内周面に
沿つて転向した圧縮空気を第2内周面の接線方向
に排出して各気筒に供給する導出通路がそれぞれ
開口する複数の流出口とを備えてなることを特徴
とするターボ過給機付エンジンの吸気装置。
[Claims] 1. A turbo supercharger is provided in the intake passage, and
In a counterflow type multi-cylinder engine in which an intake port and an exhaust port open on the same side, a substantially cylindrical enlarged chamber is provided in the intake passage downstream of the turbocharger, and the enlarged chamber and the turbocharger are connected to each other. are arranged above and below, and the enlarged chamber is arranged so that its cylinder axis direction is substantially parallel to the direction of the cylinder row, and the enlarged chamber has an arcuate first inner circumferential surface; The first
an inlet in which an introduction passage for introducing compressed air from the turbocharger opens in a tangential direction of the inner circumferential surface; and an inlet that is smoothly continuous with the first inner circumferential surface at a position distant from the inlet in the cylinder axis direction. An arc-shaped second inner circumferential surface and compressed air diverted from the inlet to the first inner circumferential surface and the second inner circumferential surface are discharged in a tangential direction of the second inner circumferential surface and supplied to each cylinder. An intake system for a turbocharged engine, characterized in that each outlet passage has a plurality of outlet openings.
JP57191623A 1982-10-30 1982-10-30 Suction device for turbosupercharged engine Granted JPS5982569A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP57191623A JPS5982569A (en) 1982-10-30 1982-10-30 Suction device for turbosupercharged engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP57191623A JPS5982569A (en) 1982-10-30 1982-10-30 Suction device for turbosupercharged engine

Publications (2)

Publication Number Publication Date
JPS5982569A JPS5982569A (en) 1984-05-12
JPH0337032B2 true JPH0337032B2 (en) 1991-06-04

Family

ID=16277715

Family Applications (1)

Application Number Title Priority Date Filing Date
JP57191623A Granted JPS5982569A (en) 1982-10-30 1982-10-30 Suction device for turbosupercharged engine

Country Status (1)

Country Link
JP (1) JPS5982569A (en)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH0736091Y2 (en) * 1987-11-05 1995-08-16 マツダ株式会社 Engine intake system
JPH01271613A (en) * 1988-04-20 1989-10-30 Yanmar Diesel Engine Co Ltd Air supply device of diesel engine of exhaust turbine supercharging type jointly used in inertial air supply supercharge
JPH04107444U (en) * 1991-02-28 1992-09-17 ダイハツ工業株式会社 Inertial supercharging intake manifold in internal combustion engines

Also Published As

Publication number Publication date
JPS5982569A (en) 1984-05-12

Similar Documents

Publication Publication Date Title
CN101137835B (en) Supercharged engine with EGR device
EP3438429B1 (en) Engine with turbo supercharger
JP2005337117A (en) Engine intake system
JPH03151519A (en) Multiple cylinder engine with turbo charger
US5572965A (en) Intake pipe for internal combustion engine
JPH0337032B2 (en)
JP2001506341A (en) Internal combustion engine supercharged by a turbocharger
JP2676300B2 (en) Exhaust gas recirculation system for turbocharged engine
JPH01244154A (en) Exhauster for engine with pressure wave supercharger
US10316738B2 (en) Turbocharger engine
US10760477B2 (en) Turbocharger engine
JP3267165B2 (en) Exhaust manifold structure for 4-cylinder engine
JPH0350256Y2 (en)
JP3104381B2 (en) Turbocharger turbine housing
JPS61187520A (en) Intake device of engine
JPH1193788A (en) Intake device for internal combustion engine
JP6399028B2 (en) Turbocharged engine
JP3387193B2 (en) Exhaust gas recirculation device
JPH0614052Y2 (en) Exhaust gas recirculation system for internal combustion engine
JPH059460Y2 (en)
JPS6321326A (en) Exhaust manifold for turbo supercharged engine
JPH0979043A (en) Exhaust gas purification device for internal combustion engine with supercharger
JP6460028B2 (en) Turbocharged engine
JPS5930179Y2 (en) supercharger
JPH04183930A (en) Exhaust device of turbo-supercharging type multiple cylinder engine