JPS5982569A - Suction device for turbosupercharged engine - Google Patents

Suction device for turbosupercharged engine

Info

Publication number
JPS5982569A
JPS5982569A JP57191623A JP19162382A JPS5982569A JP S5982569 A JPS5982569 A JP S5982569A JP 57191623 A JP57191623 A JP 57191623A JP 19162382 A JP19162382 A JP 19162382A JP S5982569 A JPS5982569 A JP S5982569A
Authority
JP
Japan
Prior art keywords
inner circumferential
circumferential surface
tangential direction
compressed air
cylinder
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
JP57191623A
Other languages
Japanese (ja)
Other versions
JPH0337032B2 (en
Inventor
Akira Kageyama
明 陰山
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

Abstract

PURPOSE:To make a device compact without reducing the supercharging effect by introducing compressed air from a turbosupercharger in the tangential direction through an expansion chamber midway on the suction passage and discharging it into a cylinder positioned in the tangential direction. CONSTITUTION:The compressed air generated by a turbosupercharger 9 flows into an expansion chamber 10, from its lower part on the opposite side to a cylinder head 6, through an introduction passage 11 and an inlet 10b, in the tangential direction of the first inner surface 10a and, after turning upward along the first inner surface 10a, the air is split into two at a splitting part 10c on the opposite side of the cylinder head 6. The air, then, is turned downward along the second inner surface 10d and discharged into each outlet introduction passage 12 through an outlet 10e which is opening in the tangential direction of the second inner surface 10d, and supplied to each cylinder from a suction port 3, after passing through an intake manifold 2a.

Description

【発明の詳細な説明】 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 The present invention relates to an improvement in an intake system for a turbocharged engine.

従来より、吸気通路の途中に拡大室を設け、吸入空気を
貯蓄するようにした吐気装館がある(例えば米国時ま1
−第グ、/g3,33.:z号明細書参照)。
Conventionally, there are exhaust vents that have an enlarged chamber in the middle of the intake passage to store intake air (for example, in the U.S.
-G, /g3,33. :Refer to No. z specification).

そして、上記拡大室は燃料噴射方式のエンジン、特にデ
ィーゼルエンジンにおいて大容量のものが要求される。
The enlarged chamber is required to have a large capacity in fuel injection type engines, especially diesel engines.

しかして、自動歪等においては、−エンジンの設置スペ
ースは制約され、上記拡大室の形成とともにターボ過給
機を付設したもσ)では、吸気装置が犬きくなるので、
そのコンパクト化を図るために、1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り、特に
エンジノの一側面に吸気ボー1・と排気ボートが開口し
ているカラ/タフロー型のエンジンにおいては、吸気1
0↓路と排気通路とが接近しており、必要賓債の拡大室
全確保し、かつ、空気の流れを阻害すZ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
ことけ困蛯である。
However, in automatic distortion, etc., the installation space for the engine is limited, and even if a turbo supercharger is attached along with the formation of the enlarged chamber, the intake system becomes stiff.
In order to make it more compact, one intake passage is formed by being bent. However, if the intake passage from the turbocharger to the engine cylinder is bent and corners are formed, there is a problem that the charging efficiency decreases and the supercharging effect is reduced. In a Kara/Taflow type engine with an open exhaust boat, the intake 1
The 0↓ passage and the exhaust passage are close to each other, ensuring all necessary expansion rooms, obtaining a good supercharging effect without obstructing air flow, and obtaining a compact arrangement structure. It's a shame.

本発明はかかる点に鑑み、吸気直路にターボ過給機を備
え、このターボ過給機下流の吸気通路に拡大室を設けて
なり、該拡大室は、円弧状の第1内周面と、該第1内周
面の接線方向からターボ過給機による圧縮空気全導入す
る導入通路が開口する流入口と、該流入口から離れた6
γ置において一ヒ記第1内周面と滑らかに連続する円弧
状の第2内周面と、流入口から第1内周面および第3内
周面に沿って転向した圧縮空気を第3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ノ1.開
口する複斂の流出口とを備えてなるターボ過給(幾月エ
ンジンの吸気装置ff提供し、大容猜の拡大室を備え、
しかも過給効果を低減することなくコノバクト化を図っ
たものである。
In view of this point, the present invention includes a turbo supercharger in the direct intake path, and an enlarged chamber in the intake passage downstream of the turbo supercharger, the enlarged chamber having a first inner circumferential surface in the shape of an arc, an inlet in which an introduction passage through which all the compressed air from the turbocharger is introduced opens from the tangential direction of the first inner circumferential surface;
At the γ position, the arcuate second inner circumferential surface smoothly continues with the first inner circumferential surface, and the compressed air diverted from the inlet along the first inner circumferential surface and the third inner circumferential surface is transferred to the third inner circumferential surface. A lead-out passage is provided in the tangential direction of the inner circumferential surface and supplied to each cylinder. The turbocharger is equipped with an opening compound outlet, which provides an intake system for the engine, and is equipped with a large capacity expansion chamber.
Moreover, it is designed to be a conobacter without reducing the supercharging effect.

以下、本発明の実施例を図面に沿って説明する。Embodiments of the present invention will be described below with reference to the drawings.

第1図および第2図において、1はカウンタフロー型の
多気筒(q気筒)ディーゼルエノジン、2は該エンジン
1の各気筒の吸気ボート5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)からの排気ガス全
導出する排気通路である。なお、6はシリンダヘッド、
7はヘッドカバー、8はシリンダブロックである。
In FIGS. 1 and 2, 1 is a counterflow type multi-cylinder (q-cylinder) diesel engine; 2 is an intake passage that supplies air to the intake boat 5 of each cylinder of the engine 1;
Reference numeral 4 denotes an exhaust passage through which all exhaust gas is led out from exhaust ports (not shown) of each cylinder. In addition, 6 is the cylinder head,
7 is a head cover, and 8 is a cylinder block.

一方、9け吸気通路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
られた拡大室であり、上記ターボ過給機9は排気通路4
を流下する刊気ガスによって1駆動されるタービン9a
でブロア9 b ? 1M1転し、過給を行うものであ
る。
On the other hand, the turbocharger 9 is interposed in the middle of the intake passage 2, and 10 is an enlarged chamber provided in the intake passage 2 downstream of the turbocharger 9. aisle 4
A turbine 9a driven by air gas flowing down the
And blower 9b? It rotates 1M1 and performs supercharging.

排気通路4は、排気ポートから下方[湾曲してJu[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9dに接続され、このタービン9dの出
口には4升気管4bが4妾経、さ:t]、ている。
The exhaust passage 4 is connected to the turbine 9d of the turbocharger 9, and the exhaust manifold 4a that collects the gas is connected to the turbine 9d of the turbocharger 9, and the outlet of the turbine 9d is connected to the 4-gas pipe 4b. Concubine Sutra, sa:t], is.

吸気通路2は、吸気ポート5がら上方に湾曲した吸気マ
ニホールド2aが拡大室10に接わ“シきれ、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の入口にはエアクリーナ(図示せず)か
らの空気を供給する吸気W2bが接続されている。
In the intake passage 2, an intake manifold 2a curved upward from the intake port 5 is in contact with an enlarged chamber 10, and this enlarged chamber 10 is connected to the blower 9b of the turbo supercharger 9,
An intake W2b that supplies air from an air cleaner (not shown) is connected to the inlet of the blower 9b.

上記拡大室10I″i全体として略円筒形状に形成を7
]、中央部分はシリンダヘッド6側に屈曲しており、こ
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が接続てれる一
方、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f’している。
The enlarged chamber 10I''i is formed into a generally cylindrical shape as a whole.
], the central part is bent toward the cylinder head 6, and an introduction passage 11 for introducing compressed air from the outlet of the blower 9b of the turbocharger 9 is connected to the lower part of this central part. Two outlet passages 12 for supplying compressed air to each cylinder are connected f'.

拡大室10の中央部分のシリンダヘッド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1
1が開口する流入口iobが開設芒れている。また、上
記中央部分のシリンダヘッド6と反対側内面は内方に突
出し、第1内周而10aを沿っ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10
cの左右には、流入口10bから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、両側部
分におけるシリンダヘッド6 +1tllの下方には、
圧縮空気を第2内周面10dの接線方向に排出する導出
通路12がそれぞれ開口するグつの流出口10eが開設
きれ、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 arcuate first inner circumferential surface 10a is formed on the inner surface of the cylinder head 6 side in the central portion of the enlarged chamber 10, and a first inner circumferential surface 10a is formed below the central portion. Introduction passage 1 introduced from the tangential direction of the inner peripheral surface 10a
The inflow port IOB 1 is opened. Further, the inner surface of the central portion opposite to the cylinder head 6 protrudes inward and is formed into a flow dividing portion 10c that divides the compressed air flowing along the first inner circumference 10a to the left and right.
On the left and right sides of c, arcuate second inner circumferential surfaces 10d that smoothly continue with the first inner circumferential surface 10a are formed at positions away from the inlet 10b. Furthermore, below the cylinder head 6+1tll on both sides,
Two outlet ports 10e are opened, each having a lead-out passage 12 for discharging compressed air in the tangential direction of the second inner circumferential surface 10d, and the periphery 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に対しシリンダヘッド6
の反対側下方より、導入通路11からγiiu人口10
bTh経て第1内周1(ir 10 aの接、11ス方
向に流入12、この框/内周1fii10aVC沿って
上方に転向した後、シリンダヘッド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10dK
沿って下方に転向し、この第2内周面10dの接線方向
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?経て吸気ポート6から各
気筒に供給される。
To explain the operation of the above embodiment, the turbo supercharger 9
The compressed air is sent to the cylinder head 6 to the expansion chamber 10.
γiiiu population 10 from the introduction passage 11 from the lower side opposite to
After bTh, the first inner periphery 1 (ir 10 a, 11th inflow 12, turns upward along this stile/inner periphery 1 fii 10 a VC, and then splits to the left and right at the dividing part 10 c on the opposite side from the cylinder head 6. Also, the second inner peripheral surface 10dK
The air is discharged from the outlet 10e opening in the tangential direction of the second inner circumferential surface 10d into each outlet passage 12, and is discharged from the intake manifold 2a? The air is then supplied to each cylinder from the intake port 6.

本発明は上記実施例の構造に限定さるものでは、なく紳
々の変形例全包含している。すなわち、上記実施例では
、拡大室10の中央部分ケシリンダヘッド6側に近付け
て形成し、圧ゐ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ッド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 all modifications thereof. That is, in the embodiment described above, the center portion of the enlarged chamber 10 is formed close to the cylinder head 6 side, and the pressure air is divided to the left and right side well, and the turbo supercharger 9 is arranged close to the cylinder head side. 6, but the center portion may be formed in the same way as the left and right portions, and the enlarged chamber 10 may be formed into a complete cylinder.
The connection position of the turbocharger 9 is also 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1
0を上方に配設しているのに対し、この配置は上下反対
にもよいが、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もとづくレイアウト上
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 placed downward in the enlarged chamber 1.
0 is placed above, this arrangement may be reversed vertically, but it is better to place the expansion chamber 10 above as in the above embodiment because of the layout based on the relationship with other auxiliary equipment. It is preferable. Furthermore, the expansion chamber 10 and the intake manifold 2a
In addition to being formed integrally, it may be formed by being divided vertically or horizontally depending on the manufacturing process.

一方、本考案は実施例のようなカウンタフロー型エンジ
ンに我見てクロスフロー型エンジンにも適用可能である
On the other hand, the present invention can be applied not only to a counterflow type engine as in the embodiment but also to a crossflow type engine.

以上説明したように、本発明によれば、ターボ過給機の
下流側の吸気通路に形成する拡大室は、滑らかに連続し
た第1内周面と第!内周面と全有し、流入口から第1内
周而の接線、方向に圧縮空気全導入し、第1および第2
内周而に沿って転向σせて、流出L1から第2内周面の
接線方向に排出して各気前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烙せるこ
となく、その吸入空気量の低下を阻止して過給効果を十
分に発揮させるとともに、拡大室およびターボ過給機を
コンパクトに配置し、良好なレイアウトのエンジン¥得
ることができる利点ケ有する。
As explained above, according to the present invention, the enlarged chamber formed in the intake passage on the downstream side of the turbocharger has a smoothly continuous first inner peripheral surface and a first! The compressed air is fully introduced from the inlet in the direction tangent to the first inner circumference, and the first and second
By turning the compressed air along the inner circumference and discharging it from the outflow L1 in the tangential direction of the second inner circumferential surface and supplying it to each airflow, turbulence and contraction may occur in the flow of compressed air. The engine has the advantage of being able to fully demonstrate the supercharging effect by preventing a decrease in the amount of intake air without causing any problems, and by arranging the enlarged chamber and turbocharger in a compact manner, the engine can have a good layout. .

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

図面σ本発明の一実施例を例示し、第1図は平面図、第
2図U第1図のl−H線に沿う1所面図である。 1  ・ディーゼルエンジン、2  吸気通路、6・ 
吸気ポート、4 ・・・排気細路、9・・ ターボ過給
機、10 ・・拡大室、10a・・・・第1内周面、1
0b・・・・・流入口、10c・・ 分流部、10d・
・・第3内周面、10e   ・流出口、11 ・・・
導入通路、12・・−・・・導出通路
Drawings σ Illustrate one embodiment of the present invention; FIG. 1 is a plan view, and FIG. 2 is a plan view taken along line 1-H in FIG. 1. Diesel engine, 2. Intake passage, 6.
Intake port, 4... Exhaust narrow passage, 9... Turbo supercharger, 10... Expansion chamber, 10a... First inner peripheral surface, 1
0b...Inlet, 10c... Diversion part, 10d...
...Third inner peripheral surface, 10e - Outlet, 11...
Inlet passage, 12... Outlet passage

Claims (1)

【特許請求の範囲】[Claims] (1)吸気通路にターボ過給機を備えたエンジンにおい
て、上記ターボ過給機下流の吸気通路に拡大室を設けて
なり、該拡大室は、円弧状の第1内周面と、該第1内周
面の接線方向からターボ過給(幾による圧縮空気を導入
する導入通路が開1」する流入口と、該流入口から離れ
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、流入口から第1内周面および第!内
周面に沿って転向した圧縮空気?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1iiiえてなること(r−特徴と
するターボ過給機付エンジンの吸気装置。
(1) In an engine equipped with a turbo supercharger in the intake passage, an enlarged chamber is provided in the intake passage downstream of the turbo supercharger, and the enlarged chamber has an arcuate first inner circumferential surface and the first inner circumferential surface. 1. An inlet in which an introduction passage for introducing compressed air for turbocharging opens from the tangential direction of the inner circumferential surface, and a circle that smoothly continues with the first inner circumferential surface at a position away from the inlet. An arcuate second inner circumferential surface, compressed air diverted from the inlet along the first inner circumferential surface and the second inner circumferential surface, and a derivation passageway that discharges compressed air in the tangential direction of the second inner circumferential surface and supplies it to each cylinder. An intake system for a turbocharged engine characterized by having a plurality of outlet ports each having an opening.
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 true JPS5982569A (en) 1984-05-12
JPH0337032B2 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)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
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

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
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
JPH0337032B2 (en) 1991-06-04

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