JPS63105233A - Turbo-compound engine - Google Patents

Turbo-compound engine

Info

Publication number
JPS63105233A
JPS63105233A JP61250662A JP25066286A JPS63105233A JP S63105233 A JPS63105233 A JP S63105233A JP 61250662 A JP61250662 A JP 61250662A JP 25066286 A JP25066286 A JP 25066286A JP S63105233 A JPS63105233 A JP S63105233A
Authority
JP
Japan
Prior art keywords
oil
bypass valve
engine
oil pressure
power turbine
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.)
Pending
Application number
JP61250662A
Other languages
Japanese (ja)
Inventor
Yoshio Sekiyama
惠夫 関山
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.)
Isuzu Motors Ltd
Original Assignee
Isuzu Motors 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 Isuzu Motors Ltd filed Critical Isuzu Motors Ltd
Priority to JP61250662A priority Critical patent/JPS63105233A/en
Publication of JPS63105233A publication Critical patent/JPS63105233A/en
Pending 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
    • F02B41/00Engines characterised by special means for improving conversion of heat or pressure energy into mechanical power
    • F02B41/02Engines with prolonged expansion
    • F02B41/10Engines with prolonged expansion in exhaust turbines
    • 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 avoid a loss from operating a power turbine within low-to-medium speed ranges by causing a by-pass valve to open and close in relation to the hydraulic pressure of the lubricating oil for an engine which is supplied to a liquid clutch. CONSTITUTION:The inlet oil-pressure of the hydraulic oil which is supplied from an oil gallery for an engine to the housing of a liquid clutch 16 is detected by an oil pressure sensor 37, while the outlet oil-pressure at the liquid clutch 16 by another oil pressure sensor 38. If the inlet oil-pressure is more than a fixed value (approx. 3kg/cm<2>), a by-pass valve 10 is caused to close. If the outlet oil-pressure is not more than a fixed value (approx. 0.5kg/cm<2>), the by- pass valve 10 is caused to open.

Description

【発明の詳細な説明】 [産業上の利用分野] 本発明はターボコンパウンド機関に関するものである。[Detailed description of the invention] [Industrial application field] The present invention relates to a turbo compound engine.

[従来の技術] ターボコンパウンド機関は内燃機関の排気管にターボ過
給機を接続して、これにより吸気過給を行うとともに、
ターボ過給機の後段に回収タービンを接続して、この吸
収動力を機関のクランク軸へ伝達するものである。とこ
ろで、ターボコンパウンド機関においてパワータービン
のエネルギ回収効果が発揮されるのは、機関の全負荷高
速域であり、第2図に破線で示すように機関の中・低速
域ではパワータービンによる背圧上昇のために逆に機関
の軸出力が低下する場合がある。
[Prior Art] In a turbo compound engine, a turbo supercharger is connected to the exhaust pipe of an internal combustion engine, and this performs intake supercharging.
A recovery turbine is connected to the rear stage of the turbocharger, and this absorbed power is transmitted to the engine crankshaft. By the way, in a turbo compound engine, the energy recovery effect of the power turbine is demonstrated in the engine's full load high speed range, and as shown by the broken line in Figure 2, the back pressure increases due to the power turbine in the middle and low speed range of the engine. Conversely, the shaft output of the engine may decrease due to this.

そこで、実開昭60−157941号公報に開示される
ものでは、ターボ過給機と回収タービンを接続する管の
途中に設けたバイパス弁を、アクセルペダルを踏み込ん
だ時にのみ閉じて回収タービンへ排気を供給し、アクセ
ルペダルを離した時にはバイパス弁を開いてターボ過給
機を出た排気を直接外部へ放出している。これにより、
排気エネルギが小さい無負荷運転で回収タービンを駆動
することの無駄が省れる。
Therefore, in the method disclosed in Japanese Utility Model Application Publication No. 60-157941, a bypass valve provided in the middle of the pipe connecting the turbo supercharger and the recovery turbine is closed only when the accelerator pedal is depressed to exhaust the air to the recovery turbine. When the accelerator pedal is released, the bypass valve opens to release the exhaust gas from the turbocharger directly to the outside. This results in
This eliminates the waste of driving the recovery turbine in no-load operation with low exhaust energy.

し発明が解決しようとする問題点] 本発明の目的は流体クラッチの作動油である機関の潤滑
油の油圧がII藺の回転数にほぼ比例することに着目し
、パワータービンの作動油の入口油圧に関連してバイパ
ス弁を制御させるターボコンパウンド機関を提供するこ
とにある。
[Problems to be Solved by the Invention] The purpose of the present invention is to focus on the fact that the oil pressure of the engine's lubricating oil, which is the hydraulic oil of the fluid clutch, is approximately proportional to the rotational speed of the engine, and to An object of the present invention is to provide a turbo compound engine that controls a bypass valve in relation to oil pressure.

[問題を解決するための手段] 上記目的を達成するために、本発明の構成はターボ過給
機とこの下流側に接続されるパワータービンとの間に設
けたバイパス弁と、パワータービンの回転を機関のクラ
ンク軸へ伝達する流体クラッチへ供給される機関の潤滑
油の油圧に関連してバイパス弁を開閉する制御手段とを
備えるものである。
[Means for Solving the Problem] In order to achieve the above object, the configuration of the present invention includes a bypass valve provided between a turbocharger and a power turbine connected downstream of the turbocharger, and a and control means for opening and closing the bypass valve in relation to the oil pressure of the lubricating oil of the engine supplied to the fluid clutch that transmits the oil pressure to the crankshaft of the engine.

[作用] 機関のオイルギヤラリから流体クラッチへ送られる潤滑
油の入口油圧は機関回転数にほぼ比例するので、機関の
高速域では入口油圧が所定値以上になると、7クチユエ
ータによりバイパス弁が閉じられる。ターボ過給機から
排気がパワータービンへ導入され、パワータービンが駆
動される。
[Operation] Since the inlet oil pressure of the lubricating oil sent from the oil gear gallery of the engine to the fluid clutch is approximately proportional to the engine rotational speed, when the inlet oil pressure exceeds a predetermined value in the high speed range of the engine, the bypass valve is closed by the 7-cut unit. Exhaust gas is introduced from the turbocharger to the power turbine, and the power turbine is driven.

一方、機関の中・低速域では入口油圧が所定値以下にな
るので、バイパス弁が開かれる。ターボ過給機からの排
気は外部へ放出され、パワータービンは駆動されない。
On the other hand, in the middle and low speed range of the engine, the inlet oil pressure is below a predetermined value, so the bypass valve is opened. The exhaust gas from the turbocharger is discharged to the outside and the power turbine is not driven.

これにより、機関の中・低速域でパワータービンを駆動
することによる軸出力の低下が防止される。
This prevents the shaft output from decreasing due to driving the power turbine in the middle and low speed range of the engine.

機関の高速域でも、流体クラッチの出口油圧が異常に低
くなると、バイパス弁が開かれ、パワータービンの駆動
が停止され、流体クラッチの不具合によるパワータービ
ンのオーバーランニングが防止される。
Even in the high-speed range of the engine, if the outlet oil pressure of the fluid clutch becomes abnormally low, the bypass valve is opened and drive of the power turbine is stopped, thereby preventing overrunning of the power turbine due to malfunction of the fluid clutch.

[発明の実施例] 第1図に示すように、機関2の排気マニホールド3に連
なる排気管4は、ターボ過給機5のタービン8の入口に
接続され、この出口は接続管9を介してパワータービン
12の入口へ接続される。
[Embodiment of the Invention] As shown in FIG. 1, an exhaust pipe 4 connected to an exhaust manifold 3 of an engine 2 is connected to an inlet of a turbine 8 of a turbocharger 5, and this outlet is connected to an inlet of a turbine 8 of a turbocharger 5 through a connecting pipe 9. It is connected to the inlet of the power turbine 12.

このパワータービン12の出口は排気管26に接続され
、消音器を経て外部に開放される。ターボ過給機5は軸
7によりタービン8の翼車とプロア6の翼車とが結合さ
れ、このブOアロにより吸気が加圧されて機関2へ供給
される。
The outlet of this power turbine 12 is connected to an exhaust pipe 26 and opened to the outside through a muffler. In the turbocharger 5, the impeller of the turbine 8 and the impeller of the proar 6 are connected by a shaft 7, and intake air is pressurized by the proar and is supplied to the engine 2.

パワータービン12の軸13は遊星歯車減速機14の太
陽歯車と結合される一方、リング歯車の軸15が流体ク
ラッチ16の入力側に結合される。
The shaft 13 of the power turbine 12 is coupled to the sun gear of the planetary gear reducer 14, while the shaft 15 of the ring gear is coupled to the input side of the fluid clutch 16.

流体クラッチ16の出力側は軸17を介して減速機18
の入力歯¥l121に結合され、この出力歯車24が機
関2のクランク軸19に結合される。
The output side of the fluid clutch 16 is connected to a reducer 18 via a shaft 17.
The output gear 24 is connected to the crankshaft 19 of the engine 2.

ターボ過給機5のタービン8の出口とパワータービン1
2の入口との接続管9の途中に、バイパス弁10が設け
られ、これを開くとタービン8の出口側がバイパス管2
0に連通され、排気が直接外部へ排出され、パワーター
ビン12へは送られない。
The outlet of the turbine 8 of the turbocharger 5 and the power turbine 1
A bypass valve 10 is provided in the middle of the connecting pipe 9 to the inlet of the turbine 2, and when this valve is opened, the outlet side of the turbine 8 is connected to the bypass pipe 2.
0, the exhaust gas is directly discharged to the outside, and is not sent to the power turbine 12.

バイパス弁10は流体クツラチ16の作動油の入口油圧
が所定値よりも高いと閉じられる。また、好ましくは流
体クラッチ16の作動油の出口油圧が異常に低下した場
合にバイパス弁10が間かれる。
The bypass valve 10 is closed when the inlet oil pressure of the hydraulic oil of the fluid clutch 16 is higher than a predetermined value. Preferably, the bypass valve 10 is opened when the outlet oil pressure of the hydraulic oil of the fluid clutch 16 is abnormally reduced.

図示の実施例ではパワータービン12へ作動油として機
関のオイルギヤラリから潤滑油が供給される。流体クラ
ッチ16の作動油は逆止弁39を経て機関のオイルパン
40へ戻される。流体クラッチ16のハウジングの入口
側に油圧センサ37が、また出口側に油圧センサ38が
設けられる。
In the illustrated embodiment, lubricating oil is supplied to the power turbine 12 as hydraulic oil from an oil gear gallery of the engine. The hydraulic oil of the fluid clutch 16 is returned to the oil pan 40 of the engine via the check valve 39. An oil pressure sensor 37 is provided on the inlet side of the housing of the fluid clutch 16, and an oil pressure sensor 38 is provided on the outlet side.

そして、油圧センサ37.38の信号がマイクロコンピ
ュータを含む電子IT)III装置36へ入力され、こ
の入力信号に基づく出力信号によりアクチュエータ(例
えばN磁アクチュエータ)が作動され、バイパス弁10
が開閉される。
Then, the signals from the oil pressure sensors 37 and 38 are input to the electronic IT (IT) III device 36 including a microcomputer, and an output signal based on this input signal operates an actuator (for example, an N-magnetic actuator).
is opened and closed.

しかし、第3図に示すように、油圧センサ37゜38の
代りに、圧力スイッチ37a、38aを直列に接続し、
かつバイパス弁10としての電磁弁の通電回路に挿入接
続してもよい。
However, as shown in FIG. 3, instead of the oil pressure sensors 37 and 38, pressure switches 37a and 38a are connected in series,
In addition, it may be inserted and connected to the energizing circuit of a solenoid valve as the bypass valve 10.

次に、本発明によるターボコンパウンド機関の作動につ
いて説明する。機関2を潤滑する油ポンプの吐出圧は第
2図に示すように機関の回転数にほぼ比例するので、機
関のオイルギヤラリから流体クラッチ16のハウジング
へ供給される作動油の入口油圧は油圧センサ37により
、また流体クラッチ16の出口油圧は油圧センサ38に
よりそれぞれ検出され、それぞれ電子111tll装置
36へ入力される。そして、入口油圧が所定値pH第3
図、例えば3kO1012)を超えると、電子制t[l
装WI36からの信号によりバイパス弁10が閉じられ
る。
Next, the operation of the turbo compound engine according to the present invention will be explained. The discharge pressure of the oil pump that lubricates the engine 2 is approximately proportional to the engine rotational speed as shown in FIG. Accordingly, the outlet oil pressure of the fluid clutch 16 is detected by the oil pressure sensor 38 and input to the electronic 111tll device 36, respectively. Then, the inlet oil pressure reaches a predetermined value pH 3.
(e.g., 3kO1012), the electronic control t[l
Bypass valve 10 is closed by a signal from WI 36.

また、出口油圧は逆止弁39の作用により大気圧よりも
高くなっているが、所定値(例えば0.5k(J/Cl
112 )以下になると、電子制御1111t36から
の信号によりバイパス弁10が開かれる。
Furthermore, although the outlet oil pressure is higher than atmospheric pressure due to the action of the check valve 39, it is kept at a predetermined value (for example, 0.5k (J/Cl).
112), the bypass valve 10 is opened by a signal from the electronic control 1111t36.

逆止弁39の故障、機関のオイルギヤラリから流体クラ
ッチ16の入口につながる油圧回路の閉塞や流体クラッ
チ16のケーシングからの油洩れなどが生じた場合、流
体クラッチ16の内部の油圧が低下し、トルクが出力軸
へ伝達されなくなる。
If the check valve 39 malfunctions, the hydraulic circuit connecting from the engine's oil gear to the inlet of the fluid clutch 16 is blocked, or oil leaks from the casing of the fluid clutch 16, the oil pressure inside the fluid clutch 16 will drop and the torque will decrease. is no longer transmitted to the output shaft.

この時パワータービン12は煕負荷運転状態になり、排
気)fflffiに従って回転数が上昇し、オーバーラ
ンニングを起こす。
At this time, the power turbine 12 enters a low load operating state, and the rotational speed increases according to the exhaust gas)ffffi, causing overrunning.

このような場合は、流体クラッチ16の出口油圧(逆止
弁39よりも上流側)が所定値以下になるので、バイパ
ス弁10が開かれ、パワータービン12へ排気が導入さ
れなくなり、パワータービン12のオーバーランニング
が防止される。
In such a case, the outlet oil pressure of the fluid clutch 16 (upstream of the check valve 39) becomes less than a predetermined value, so the bypass valve 10 is opened and exhaust gas is no longer introduced into the power turbine 12. overrunning is prevented.

第4図は上述の1lltllプログラムの流れ図を示し
、同図において911〜p14は各ステップを示す。p
llで流体クラッチ16の入口油圧が所定値p1よりも
大きいか否かを判別し、入口油圧が所定1plよりも小
ざい場合にはp14でバイパス弁10を開いてパワータ
ービン12の駆動を停止する。
FIG. 4 shows a flowchart of the above-mentioned 1lltll program, in which 911 to p14 indicate each step. p
At ll, it is determined whether the inlet oil pressure of the fluid clutch 16 is larger than a predetermined value p1, and if the inlet oil pressure is smaller than the predetermined value p1, the bypass valve 10 is opened at p14 to stop driving the power turbine 12. .

一方、pllで入口油圧が所定値p1よりも大きい場合
には、p12で流体クラッチ16の出口油圧が所定値p
2よりも小さいか否かを判別する。出口油圧が所定(i
ap2よりも大きい場合には、p14でバイパス弁10
を開く。一方、出口油圧が所定fiip2よりも小さい
場合には、p13でバイパス弁10を閉じ、パワーター
ビン12を駆動する。
On the other hand, if the inlet oil pressure at pll is greater than the predetermined value p1, the outlet oil pressure of the fluid clutch 16 is set to the predetermined value p12 at p12.
It is determined whether the value is smaller than 2 or not. The outlet oil pressure is specified (i
If it is larger than ap2, the bypass valve 10 is activated at p14.
open. On the other hand, if the outlet oil pressure is smaller than the predetermined value fiip2, the bypass valve 10 is closed at p13 and the power turbine 12 is driven.

CR明の効果j 本発明は上述のように、パワータービンの動力を機関の
クランク軸へ伝達する流体クラッチの作動油の入口油圧
に関連して、ターボ過Ia機とタワータービンとの間に
配設したバイパス弁を制御するようにしたので、入口油
圧が機関の回転数にほぼ比例して変化することから、機
関の高速域ではバイパス弁が閉じられてパワータービン
が墾勤され、排気エネルギが有効に回収される一方、機
関の中・低速域ではバイパス弁が開かれてパワータービ
ンが駆動されないから、パワータービンを中・低速域で
駆動することによる損失が回避される。
Effects of CR Light As described above, the present invention is directed to a system that is arranged between a turbo Ia machine and a tower turbine in relation to the inlet hydraulic pressure of the hydraulic oil of the fluid clutch that transmits the power of the power turbine to the crankshaft of the engine. Since the inlet oil pressure changes almost in proportion to the engine speed, the bypass valve is closed in the high-speed range of the engine and the power turbine is activated, reducing exhaust energy. While the power is effectively recovered, the bypass valve is opened in the middle and low speed range of the engine and the power turbine is not driven, thereby avoiding losses caused by driving the power turbine in the middle and low speed range.

さらに、流体クラッチの入口油圧と出口油圧に関連して
バイパス弁を作動させるようにすれば、流体クラッチの
故障によるパワータービンのオーバランニングを防止す
ることができる。
Furthermore, by activating the bypass valve in relation to the inlet oil pressure and outlet oil pressure of the fluid clutch, it is possible to prevent overrunning of the power turbine due to failure of the fluid clutch.

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

第1図は本発明に係るターボコンパウンドRrjAの概
略構成図、第2図は機関回転数と流体クラッチの入口油
圧と関係を表す縮図、第3図は本発明のターボコンパウ
ンド機関におけるバイパス弁11tl+御手段の一部変
更例を示す電気回路図、第4図は同制御手段をマイクロ
コンピュータで作動させるプログラムの流れ図、第5図
は一般的なターボコンパウンド機関の特性を表す線図で
ある。 2:内燃機関 4:排気管 5:ターボ過給機8:ター
ビン 9:接続管 10:バイパス弁12:パワーター
ビン 14:遊星歯巾減速機16:流体クラッチ 18
:減速n 1つ:クランク軸 25ニ一方向クラツチ 
36:電子tIIItla装置 36.37:油圧セン
サ 特許出願人 いすず自動車株式会社 代理人   弁理士  山本俊夫 旗聞回帖畢χ        攬聞0輛1欠第 5 図
        第 2FIA第3図 第 4 図
Fig. 1 is a schematic configuration diagram of the turbo compound RrjA according to the present invention, Fig. 2 is a miniature diagram showing the relationship between the engine speed and the inlet oil pressure of the fluid clutch, and Fig. 3 is a diagram showing the bypass valve 11tl + control in the turbo compound engine of the present invention. FIG. 4 is a flowchart of a program for operating the control means by a microcomputer, and FIG. 5 is a diagram showing the characteristics of a general turbo compound engine. 2: Internal combustion engine 4: Exhaust pipe 5: Turbo supercharger 8: Turbine 9: Connection pipe 10: Bypass valve 12: Power turbine 14: Planetary tooth width reducer 16: Fluid clutch 18
: Reduction n 1: Crankshaft 25-way one-way clutch
36: Electronic tIIItla device 36. 37: Oil pressure sensor patent applicant Isuzu Motors Co., Ltd. Agent Patent attorney Toshio Yamamoto Flag circular book review χ 攬萬 0 輛 1 5 Figure 2 FIA Figure 3 Figure 4

Claims (3)

【特許請求の範囲】[Claims] (1)ターボ過給機とこの下流側に接続されるパワータ
ービンとの間に設けたバイパス弁と、パワータービンの
回転を機関のクランク軸へ伝達する流体クラッチへ供給
される機関の潤滑油の油圧に関連してバイパス弁を開閉
する制御手段とを備えることを特徴とするターボコンパ
ウンド機関。
(1) Engine lubricating oil supplied to the bypass valve installed between the turbocharger and the power turbine connected downstream, and the fluid clutch that transmits the rotation of the power turbine to the engine crankshaft. A turbo compound engine comprising: control means for opening and closing a bypass valve in relation to hydraulic pressure.
(2)前記制御手段がパワータービンの油入口側の油圧
センサと、バイパス弁を駆動するアクチュエータと、入
口油圧が所定値以上になると前記アクチュエータを作動
させてバイパス弁を閉じる電子制御装置とからなる、特
許請求の範囲(1)に記載のターボコンパウンド機関。
(2) The control means includes an oil pressure sensor on the oil inlet side of the power turbine, an actuator that drives the bypass valve, and an electronic control device that operates the actuator and closes the bypass valve when the inlet oil pressure exceeds a predetermined value. , a turbo compound engine according to claim (1).
(3)前記制御手段がパワータービンの油入口側の油圧
センサと、抽出口側の油圧センサと、バイパス弁を駆動
するアクチュエータと、入口油圧が所定値以上になると
前記アクチュエータによりバイパス弁を閉じ、出口油圧
が所定値以下になると前記アクチュエータによりバイパ
ス弁を開く電子制御装置とからなる、特許請求の範囲(
1)に記載のターボコンパウンド機関。
(3) The control means includes an oil pressure sensor on the oil inlet side of the power turbine, an oil pressure sensor on the extraction port side, and an actuator that drives a bypass valve, and when the inlet oil pressure becomes a predetermined value or more, the actuator closes the bypass valve, and an electronic control device that causes the actuator to open the bypass valve when the outlet oil pressure falls below a predetermined value.
The turbo compound engine described in 1).
JP61250662A 1986-10-23 1986-10-23 Turbo-compound engine Pending JPS63105233A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP61250662A JPS63105233A (en) 1986-10-23 1986-10-23 Turbo-compound engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP61250662A JPS63105233A (en) 1986-10-23 1986-10-23 Turbo-compound engine

Publications (1)

Publication Number Publication Date
JPS63105233A true JPS63105233A (en) 1988-05-10

Family

ID=17211180

Family Applications (1)

Application Number Title Priority Date Filing Date
JP61250662A Pending JPS63105233A (en) 1986-10-23 1986-10-23 Turbo-compound engine

Country Status (1)

Country Link
JP (1) JPS63105233A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1990014509A1 (en) * 1989-05-24 1990-11-29 Kabushiki Kaisha Komatsu Seisakusho Power transmission of turbocompound engine
US5119633A (en) * 1990-09-25 1992-06-09 Cummins Engine Company, Inc. Power turbine bypass for improved compression braking
JP2006299908A (en) * 2005-04-20 2006-11-02 Hino Motors Ltd Turbo compound engine

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1990014509A1 (en) * 1989-05-24 1990-11-29 Kabushiki Kaisha Komatsu Seisakusho Power transmission of turbocompound engine
US5119633A (en) * 1990-09-25 1992-06-09 Cummins Engine Company, Inc. Power turbine bypass for improved compression braking
JP2006299908A (en) * 2005-04-20 2006-11-02 Hino Motors Ltd Turbo compound engine
JP4551810B2 (en) * 2005-04-20 2010-09-29 日野自動車株式会社 Turbo compound engine

Similar Documents

Publication Publication Date Title
EP0301547A2 (en) Turbo compound engine
JPH0361616A (en) Supercharger for engine
JPS63105233A (en) Turbo-compound engine
JP2534338B2 (en) Turbo compound engine
JP3137802B2 (en) Engine supercharger
JPH08177507A (en) Supercharger of internal combustion engine and its operation method
JPH0526265Y2 (en)
JPS62103422A (en) Turbo-compound engine
JPS63111239A (en) Turbo compound engine
CN211975156U (en) Exhaust treatment system of engine
JPS63100225A (en) Turbo-compound engine
JPH07208187A (en) Turbo-supercharged engine
JPH0255829A (en) Internal combustion engine with supercharger
JPS63109236A (en) Turbo-compound engine
JPH041308Y2 (en)
JPS6332913Y2 (en)
JPH0512630U (en) Centrifugal mechanical turbocharger
JPH0454221A (en) Supercharging device for engine
JPH02140432A (en) Fuel injection amount controlling device for internal combustion engine with supercharger
JPH03233135A (en) Control method of engine with supercharger
JP2001115847A (en) Supercharging system
JPH0810654Y2 (en) Auxiliary air supply for engine
JPH041422A (en) Composite supercharging system in marine engine
JPH0579811B2 (en)
JP2000204957A (en) Internal combustion engine with supercharger