JPS6234928B2 - - Google Patents

Info

Publication number
JPS6234928B2
JPS6234928B2 JP55179935A JP17993580A JPS6234928B2 JP S6234928 B2 JPS6234928 B2 JP S6234928B2 JP 55179935 A JP55179935 A JP 55179935A JP 17993580 A JP17993580 A JP 17993580A JP S6234928 B2 JPS6234928 B2 JP S6234928B2
Authority
JP
Japan
Prior art keywords
exhaust
pressure
engine
supercharger
cam
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
JP55179935A
Other languages
Japanese (ja)
Other versions
JPS57102519A (en
Inventor
Kohei Yamada
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.)
Kawasaki Heavy Industries Ltd
Original Assignee
Kawasaki Heavy Industries Ltd
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 Kawasaki Heavy Industries Ltd filed Critical Kawasaki Heavy Industries Ltd
Priority to JP55179935A priority Critical patent/JPS57102519A/en
Publication of JPS57102519A publication Critical patent/JPS57102519A/en
Publication of JPS6234928B2 publication Critical patent/JPS6234928B2/ja
Granted legal-status Critical Current

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  • Automatic Cycles, And Cycles In General (AREA)
  • Supercharger (AREA)

Description

【発明の詳細な説明】 本発明は自動2輪車用2段過給機関に関するも
ので、前後輪間隔(ホイールベース)及び全幅を
増加させることなく2段過給を可能にするレイア
ウトの提供と、出力の向上を目的としている。
DETAILED DESCRIPTION OF THE INVENTION The present invention relates to a two-stage supercharged engine for two-wheeled motor vehicles, and provides a layout that enables two-stage supercharging without increasing the distance between front and rear wheels (wheelbase) or overall width. , aimed at improving output.

コンプレツサの翼車径が40mm前後の小型コンプ
レツサでは高圧力比(2程度)における断熱効率
が低く、又、過給機総合効率も極めて低い為小型
過給エンジンの全回転域における高トルク発生は
困難である。その為、この対策として2段過給方
式を自動2輪車に導入することが考えられるが、
その場合、高圧力比におけるコンプレツサの断熱
効率の向上、負荷変動に対する出力応答性の改
善、更に流量範囲の拡大、高圧タービンの排気バ
イパスコントロールによる低速トルク向上等のメ
リツトを有するが一方ではスペース的な余裕が少
ないため、2基の過給機や、インタークーラ、ア
フタークーラ等のコンパクトなレイアウトが困難
である。
Small compressors with compressor impeller diameters of around 40 mm have low adiabatic efficiency at high pressure ratios (about 2), and the overall supercharger efficiency is also extremely low, making it difficult for small supercharged engines to generate high torque over the entire rotation range. It is. Therefore, as a countermeasure to this problem, it is possible to introduce a two-stage supercharging system to motorcycles.
In this case, the benefits include improving the adiabatic efficiency of the compressor at high pressure ratios, improving the output response to load fluctuations, expanding the flow range, and improving low-speed torque by controlling the high-pressure turbine's exhaust bypass. Because there is little room, it is difficult to create a compact layout with two superchargers, an intercooler, an aftercooler, etc.

本発明は、自動2輪車用ダブルオーバーヘツド
カム(DOHC)直列型エンジンの前側の排気カム
と後側の吸気カムの間から、排気ポートを上向き
に開口させ、排気マニホールドを介し、エンジン
直上の高圧過給機の高圧タービン入口に接続する
ことにより、レイアウトのコンパクト化を可能に
したもので、直列型ダブルオーバーヘツドカムエ
ンジンを進行方向と直角横置きに、かつ排気カム
が前、吸気カムが後となるように配置し、吸排気
カムの間から排気ポートを上向きに開口させ、エ
ンジン直上の左右一側に高圧過給機を、他側にイ
ンタークーラを、前側に低圧過給機を、後側にア
フタークーラをそれぞれ配置し、各気筒の排気ポ
ートを排気マニホールドを介して高圧過給機の高
圧タービン入口に接続したことを特徴としてお
り、図面により説明すると次の通りである。
The present invention opens an exhaust port upward from between the front exhaust cam and the rear intake cam of a double overhead cam (DOHC) in-line engine for motorcycles, and connects the exhaust port directly above the engine via the exhaust manifold. By connecting to the high-pressure turbine inlet of the high-pressure supercharger, the layout can be made more compact.The in-line double overhead cam engine is placed horizontally at right angles to the direction of travel, with the exhaust cam at the front and the intake cam at the front. The exhaust port is opened upward from between the intake and exhaust cams, and the high-pressure supercharger is placed on one side directly above the engine, the intercooler is placed on the other side, and the low-pressure supercharger is placed on the front side. It is characterized by having an aftercooler arranged on the rear side, and the exhaust port of each cylinder is connected to the high-pressure turbine inlet of the high-pressure supercharger via an exhaust manifold.This will be explained with reference to the drawings as follows.

第1図は本発明による3気筒直列型ダブルオー
バーヘツドカムエンジン1をクランク軸と直角な
断面で示す縦断左側面図で、このエンジン1は矢
印Fで示す進行方向に対し直角横置きに配置され
ている。シリンダブロツク2の上端面に複数個の
ボルトで締着されたシリンダヘツド3内には各気
筒ごとに排気弁4、吸気弁5が支持され、排気弁
4は燃焼室6と排気ポート7を区画し、吸気弁5
は燃焼室6と吸気ポート8を区画している。9は
ピストン、10は連接杆である。排気弁4と吸気
弁5の各上端はタペツト11,12を介して排気
カム13と吸気カム14に弁ばねの弾力により弾
性的に当接している。15,16はカムカバーで
ある。
FIG. 1 is a vertical left side view showing a three-cylinder in-line double overhead cam engine 1 according to the present invention in a cross section perpendicular to the crankshaft. ing. An exhaust valve 4 and an intake valve 5 are supported for each cylinder in a cylinder head 3 that is fastened to the upper end surface of the cylinder block 2 with a plurality of bolts, and the exhaust valve 4 partitions a combustion chamber 6 and an exhaust port 7. and intake valve 5
partitions the combustion chamber 6 and the intake port 8. 9 is a piston, and 10 is a connecting rod. The upper ends of the exhaust valve 4 and the intake valve 5 are in elastic contact with the exhaust cam 13 and the intake cam 14 via tappets 11 and 12 due to the elasticity of the valve springs. 15 and 16 are cam covers.

排気ポート7は従来のものが排気弁4より前方
(第1図左方)に延長しているのに対して、排気
カム13と吸気カム14の間においてシリンダヘ
ツド3内を上方へ延び、上向きに開口して排気マ
ニホールド18に接続している。排気マニホール
ド18は図示の実施例においては3気筒の各排気
ポート7に下端が接続し、上端は高圧過給機T1
の高圧タービン20の入口21に接続している。
高圧タービン20の排気ガス出口22は低圧過給
機T2の低圧タービン23の入口24に接続し、
低圧タービン23の排気ガス出口25は第3図に
示すように下向きの排気管26、後向きマフラー
27を経て大気に開放している。
Whereas the conventional exhaust port 7 extends forward from the exhaust valve 4 (to the left in Figure 1), the exhaust port 7 extends upward within the cylinder head 3 between the exhaust cam 13 and the intake cam 14, and extends upward from the exhaust cam 13 and the intake cam 14. The exhaust manifold 18 is connected to the exhaust manifold 18. In the illustrated embodiment, the exhaust manifold 18 has a lower end connected to each exhaust port 7 of the three cylinders, and an upper end connected to the high pressure supercharger T1.
The high pressure turbine 20 is connected to the inlet 21 of the high pressure turbine 20 .
The exhaust gas outlet 22 of the high-pressure turbine 20 is connected to the inlet 24 of the low-pressure turbine 23 of the low-pressure supercharger T2 ,
As shown in FIG. 3, the exhaust gas outlet 25 of the low pressure turbine 23 is exposed to the atmosphere via a downward exhaust pipe 26 and a rearward muffler 27.

高圧タービン20内のタービン翼車(図示せ
ず)は高圧過給機T1内の高圧コンプレツサ29
内のコンプレツサ翼車(図示せず)に直結してお
り、一方、低圧タービン23内のタービン翼車
(図示せず)は低圧過給機T2内の低圧コンプレツ
サ30内のコンプレツサ翼車(図示せず)に直結
している。低圧コンプレツサ30の空気入口31
(第2図)はその上流側のエアフローメータ、エ
アフイルタを介して大気と連通している。低圧コ
ンプレツサ30の加圧空気出口32はインターク
ーラ33を経て高圧コンプレツサ29の入口34
に接続し、高圧コンプレツサ29の加圧空気出口
35はアフタークーラとエコライザーチユーブ3
7を経て吸気管38の部分から各気筒の吸気ポー
ト8に接続している。第2図において40は前
輪、41は後輪であり、細い矢印は排気ガスの流
れ、太い矢印は吸入空気の流れを示している。又
第1図において42はスロツトル弁である。
A turbine wheel (not shown) in the high-pressure turbine 20 is a high-pressure compressor 29 in the high-pressure supercharger T1 .
The turbine wheel (not shown) in the low-pressure turbine 23 is directly connected to the compressor wheel (not shown) in the low-pressure supercharger T2 . (not shown). Air inlet 31 of low pressure compressor 30
(Fig. 2) communicates with the atmosphere via an air flow meter and an air filter on its upstream side. The pressurized air outlet 32 of the low pressure compressor 30 is connected to the inlet 34 of the high pressure compressor 29 via an intercooler 33.
The pressurized air outlet 35 of the high pressure compressor 29 is connected to the aftercooler and equalizer tube 3.
7, the intake pipe 38 is connected to the intake port 8 of each cylinder. In FIG. 2, 40 is a front wheel, 41 is a rear wheel, thin arrows indicate the flow of exhaust gas, and thick arrows indicate the flow of intake air. Further, in FIG. 1, 42 is a throttle valve.

第1図、第2図で明らかなように、本発明にお
いては、エンジン1の特にシリンダヘツド3の直
上空間の左側(第2図)に高圧過給機T1が、又
右側空間にインタークーラ33が配置され、それ
らの直前に低圧過給機T2が配置され、又直後に
アフタークーラ36が配置されている。そしてこ
のような過給エンジンを自動2輪車に搭載した場
合の左側面レイアウトは第3図のようになり、
高、低圧過給機T1,T2及びアフタークーラ36
は従来燃料タンクが配置されていた位置を占め、
概ね燃料タンクと同じ外形のカバー(図示せず)
により覆われる。45はハンドル、46はフロン
トフオーク、47はスイングアームである。
As is clear from FIGS. 1 and 2, in the present invention, the high-pressure supercharger T1 is located on the left side (FIG. 2) of the space directly above the cylinder head 3 of the engine 1, and the intercooler T1 is located on the right side of the space. 33, a low-pressure supercharger T2 is placed immediately before them, and an aftercooler 36 is placed immediately after. When such a supercharged engine is installed in a motorcycle, the left side layout is as shown in Figure 3.
High and low pressure superchargers T 1 , T 2 and aftercooler 36
occupies the position where the fuel tank was previously located,
A cover with approximately the same external shape as the fuel tank (not shown)
covered by. 45 is a handle, 46 is a front fork, and 47 is a swing arm.

次に作動を説明する。第1図において燃焼室6
で発生した排気ガスは、排気弁4を経て排気ポー
ト7に排出され、排気マニホールド18を経て高
圧過給機T1の高圧タービン20に入り、内部の
タービン翼車を駆動した後出口22から低圧過給
機T2の低圧タービン23に入り、内部のタービ
ン翼車を駆動した後出口25から排気管26(第
3図)、マフラー27を経て大気中へ排出され
る。一方、第2図において、エアフイルタ、エア
フローメータを通過した後の空気は入口31から
低圧過給機T2の低圧コンプレツサ30に入り、
内部の翼車により加圧された後インタークーラ3
3を通過し、そこで冷却された後高圧過給機T1
の高圧コンプレツサ29に入り、内部の翼車によ
り更に加圧され、出口35からアフタークーラ3
6へ入り、そこで冷却された後エコライザーチユ
ーブ37、吸気管38、吸気ポート8、吸気弁5
を経て各気筒の燃焼室6へ供給される。高圧ター
ビン20、低圧タービン23の熱はそれらの外面
に被覆された断熱板17(第1図、第2図中に太
い破線で示す)により放熱が阻止されており、イ
ンタークーラ33とエンジン排気系との間の断熱
板19(第2図)はエンジン排気系の熱のインタ
ークーラ33への伝達を阻止している。
Next, the operation will be explained. In Fig. 1, the combustion chamber 6
Exhaust gas generated in After entering the low pressure turbine 23 of the supercharger T 2 and driving the internal turbine wheel, it is discharged from the outlet 25 through the exhaust pipe 26 (FIG. 3) and the muffler 27 into the atmosphere. On the other hand, in FIG. 2, the air after passing through the air filter and air flow meter enters the low pressure compressor 30 of the low pressure supercharger T2 from the inlet 31.
After being pressurized by the internal impeller, intercooler 3
3 and after being cooled there, the high pressure supercharger T 1
The high-pressure compressor 29 is further pressurized by the internal impeller, and the aftercooler 3 is sent from the outlet 35.
6, and after being cooled there, the equalizer tube 37, intake pipe 38, intake port 8, intake valve 5
The fuel is then supplied to the combustion chamber 6 of each cylinder. Heat from the high-pressure turbine 20 and low-pressure turbine 23 is prevented from being radiated by a heat insulating plate 17 (indicated by thick broken lines in FIGS. 1 and 2) coated on their outer surfaces, and the intercooler 33 and engine exhaust system A heat insulating plate 19 (FIG. 2) between the intercooler 33 and the intercooler 33 prevents heat from the engine exhaust system from being transferred to the intercooler 33.

以上説明したように本発明においては、直列型
ダブルオーバーヘツドカムエンジン1を進行方向
(矢印F)と直角横向きに、かつ排気カム13が
前、吸気カム14が後になるように配置し、吸排
気カム14,13の間から排気ポート7を上向き
に開口させ、エンジン直上の左右一側に高圧過給
機T1を、他側にインタークーラ33を、前側に
低圧過給機T2を、後側にアフタークーラ36を
それぞれ配置し、各気筒の排気ポート7を排気マ
ニホールド18を介して第1段過給機T1の高圧
タービン入口21に接続したので、レイアウトが
コンパクト化し、自動2輪車に2段過給方式の採
用が可能となる。従つてバイパスバルブ48,4
9を適当に作動させ、高圧、低圧タービン回転数
を制御し、高圧、低圧コンプレツサを最適作動範
囲内で作動させる事により、低速から高速に至る
まで、小型エンジンにて高トルクを得る事が可能
となる。又、合計1.5〜2Kg/cm2程度の比較的高
い給気圧力を単段の場合よりも低温の状態で得ら
れる為、過給ガソリン機関の異常燃焼による出力
限界を高める事も可能となる。排気ポート7を排
気弁4の前側に配置すると、第1段過給機T1
エンジンの前方に大幅に張り出し、ホイールベー
スが増加して実用困難になるが、排気ポート7が
前後の吸排気カム14,13の間で上向きに開口
しているため、高圧過給機T1がエンジンの直上
を占め、その前方の低圧過給機T2を排気カムカ
バー15の上側で前方への突出量を少なく保持し
て配置することができ、全体がコンパクトにまと
まる。
As explained above, in the present invention, the in-line double overhead cam engine 1 is arranged horizontally at right angles to the traveling direction (arrow F), with the exhaust cam 13 at the front and the intake cam 14 at the rear. The exhaust port 7 is opened upward from between the cams 14 and 13, and the high-pressure supercharger T1 is placed on one side of the left and right directly above the engine, the intercooler 33 is placed on the other side, the low-pressure supercharger T2 is placed on the front side, and the low-pressure supercharger T2 is placed on the rear side. Aftercoolers 36 are placed on each side, and the exhaust port 7 of each cylinder is connected to the high-pressure turbine inlet 21 of the first stage supercharger T 1 via the exhaust manifold 18, making the layout more compact and making it easier for motorcycles. It becomes possible to adopt a two-stage supercharging system. Therefore, the bypass valve 48,4
By operating 9 appropriately, controlling the high-pressure and low-pressure turbine rotation speeds, and operating the high-pressure and low-pressure compressors within the optimum operating range, it is possible to obtain high torque with a small engine from low speed to high speed. becomes. In addition, since a relatively high air supply pressure of about 1.5 to 2 kg/cm 2 in total can be obtained at a lower temperature than in the case of a single stage, it is also possible to increase the output limit due to abnormal combustion of the supercharged gasoline engine. If the exhaust port 7 is placed in front of the exhaust valve 4, the first stage supercharger T1 will protrude significantly in front of the engine, increasing the wheelbase and making it difficult to put it into practice. Since it opens upward between the cams 14 and 13, the high-pressure supercharger T 1 occupies the position directly above the engine, and the low-pressure supercharger T 2 in front of it is placed above the exhaust cam cover 15 to prevent it from protruding forward. It can be held and placed in small quantities, making the whole thing compact.

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

第1図は本発明による2段過給機関の縦断左側
面図、第2図は平面図、第3図は自動2輪車に搭
載した状態を示す左側面図である。1…エンジ
ン、7…排気ポート、11…排気カム、12…吸
気カム、18…排気マニホールド、21…高圧タ
ービン入口、33…インタークーラ、36…アフ
タークーラ、T1…高圧過給機、T2…低圧過給
機。
FIG. 1 is a vertical left side view of a two-stage supercharged engine according to the present invention, FIG. 2 is a plan view, and FIG. 3 is a left side view showing a state in which the two-stage supercharged engine is mounted on a motorcycle. 1...Engine, 7...Exhaust port, 11...Exhaust cam, 12...Intake cam, 18...Exhaust manifold, 21...High pressure turbine inlet, 33...Intercooler, 36...Aftercooler, T1 ...High pressure supercharger, T2 ...Low pressure supercharger.

Claims (1)

【特許請求の範囲】[Claims] 1 直列型ダブルオーバーヘツドカムエンジンを
進行方向と直角横置きに、かつ排気カムが前、吸
気カムが後となるように配置し、吸排気カムの間
から排気ポートを上向きに開口させ、エンジン直
上の左右一側に高圧過給機を、他側にインターク
ーラを、前側に低圧過給機を、後側にアフターク
ーラをそれぞれ配置し、各気筒の排気ポートを排
気マニホールドを介して第1段過給機の高圧ター
ビン入口に接続したことを特徴とする自動2輪車
用2段過給機関。
1. An in-line double overhead cam engine is placed horizontally at right angles to the direction of travel, with the exhaust cam at the front and the intake cam at the rear.The exhaust port is opened upward from between the intake and exhaust cams, and is placed directly above the engine. A high-pressure supercharger is placed on one side of the left and right side, an intercooler is placed on the other side, a low-pressure supercharger is placed on the front side, and an aftercooler is placed on the rear side.The exhaust port of each cylinder is connected to the first stage via an exhaust manifold. A two-stage supercharged engine for a motorcycle, characterized in that it is connected to a high-pressure turbine inlet of a supercharger.
JP55179935A 1980-12-18 1980-12-18 Two-stage-supercharged engine for motorcycle Granted JPS57102519A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP55179935A JPS57102519A (en) 1980-12-18 1980-12-18 Two-stage-supercharged engine for motorcycle

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP55179935A JPS57102519A (en) 1980-12-18 1980-12-18 Two-stage-supercharged engine for motorcycle

Publications (2)

Publication Number Publication Date
JPS57102519A JPS57102519A (en) 1982-06-25
JPS6234928B2 true JPS6234928B2 (en) 1987-07-29

Family

ID=16074502

Family Applications (1)

Application Number Title Priority Date Filing Date
JP55179935A Granted JPS57102519A (en) 1980-12-18 1980-12-18 Two-stage-supercharged engine for motorcycle

Country Status (1)

Country Link
JP (1) JPS57102519A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2010065681A (en) * 2008-09-10 2010-03-25 Borgwarner Inc Coupling turbochargers for passive pre-swirl counter-rotation

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS60185032U (en) * 1984-05-17 1985-12-07 スズキ株式会社 Motorcycle with supercharger
US7270110B2 (en) 2000-04-24 2007-09-18 Frank Keoppel Four stroke internal combustion engine with inlet air compression chamber
US6536384B1 (en) 2000-04-24 2003-03-25 Frank Keoppel Two-stroke internal combustion engine with isolated crankcase
US7549493B1 (en) 2006-02-28 2009-06-23 Jones Daniel W Wet belt supercharger drive for a motorcycle
JP5426134B2 (en) * 2007-12-26 2014-02-26 ヤマハ発動機株式会社 Saddle riding vehicle
DE102012203701A1 (en) * 2012-03-08 2013-09-12 Man Diesel & Turbo Se Exhaust gas turbocharger module and thus equipped internal combustion engine

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2010065681A (en) * 2008-09-10 2010-03-25 Borgwarner Inc Coupling turbochargers for passive pre-swirl counter-rotation

Also Published As

Publication number Publication date
JPS57102519A (en) 1982-06-25

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