JPH0612070B2 - Turbo Compound Organization - Google Patents
Turbo Compound OrganizationInfo
- Publication number
- JPH0612070B2 JPH0612070B2 JP61255870A JP25587086A JPH0612070B2 JP H0612070 B2 JPH0612070 B2 JP H0612070B2 JP 61255870 A JP61255870 A JP 61255870A JP 25587086 A JP25587086 A JP 25587086A JP H0612070 B2 JPH0612070 B2 JP H0612070B2
- Authority
- JP
- Japan
- Prior art keywords
- engine
- bypass valve
- power turbine
- turbocharger
- fluctuation rate
- 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
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B41/00—Engines characterised by special means for improving conversion of heat or pressure energy into mechanical power
- F02B41/02—Engines with prolonged expansion
- F02B41/10—Engines with prolonged expansion in exhaust turbines
-
- Y—GENERAL 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
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T10/00—Road transport of goods or passengers
- Y02T10/10—Internal combustion engine [ICE] based vehicles
- Y02T10/12—Improving ICE efficiencies
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Supercharger (AREA)
Description
【発明の詳細な説明】 [産業上の利用分野] 本発明はターボコンパウンド機関に関するものである。DETAILED DESCRIPTION OF THE INVENTION [Industrial application] The present invention relates to a turbo compound engine.
[従来の技術] 実開昭60-157941号公報に開示されるターボコンパウン
ド機関では、ターボ過給機とパワー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パワー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。[Prior Art] In the turbo compound engine disclosed in Japanese Utility Model Laid-Open No. 60-157941, the bypass valve provided in the middle of the pipe connecting the turbocharger and the power turbine is closed only when the accelerator pedal is depressed. Supply the exhaust to the power turbine,
When the accelerator pedal is released, the bypass valve is opened and the exhaust gas from the turbocharger is discharged directly to the outside.
上述のターボコンパウンド機関によれば、部分負荷運転
および全負荷運転でパワータービンを有効に駆動し、排
気エネルギを動力として吸収することができる。また、
排気エネルギが小さい無負荷運転ではパワータービンを
駆動することの無駄が省れる。According to the turbo compound engine described above, the power turbine can be effectively driven in partial load operation and full load operation, and exhaust energy can be absorbed as power. Also,
In no-load operation with small exhaust energy, it is possible to avoid waste of driving the power turbine.
[発明が解決しようとする問題点] しかし、車両に搭載されるターボコンパウンド機関の場
合に、急加速運転ではターボ過給機の応答遅れだけでな
く、パワータービンの応答遅れも重なり、第3図に破線
で示すように軸出力の損失が生じる。[Problems to be Solved by the Invention] However, in the case of a turbo compound engine mounted on a vehicle, not only the response delay of the turbocharger but also the response delay of the power turbine are overlapped during the rapid acceleration operation. A shaft output loss occurs as shown by the broken line.
逆に、急減速運転ではパワータービンの出力が引続き発
生する一方、機関のクランク軸は回転数が低下するの
で、パワータービンの出力に過大な逆トルクが作用し、
流体クラツチや変速機を損傷する恐れがある。On the other hand, in the rapid deceleration operation, the output of the power turbine continues to be generated, while the crankshaft of the engine decreases in rotation speed, so excessive reverse torque acts on the output of the power turbine,
It may damage the fluid clutch or transmission.
本発明の目的は上述の問題を解消するために、急加・減
速時、パワータービンの駆動を停止する、ターボコンパ
ウンド機関を提供することにある。An object of the present invention is to provide a turbo compound engine that stops driving of a power turbine at the time of sudden acceleration / deceleration in order to solve the above problems.
[問題を解決するための手段] 上記目的を達成するために、本発明の構成は機関の排気
管にターボ過給機とパワータービンを順に接続し、ター
ボ過給機とパワータービンとを接続する管の途中に、開
弁時ターボ過給機からの排気を外部へ放出するバイパス
弁を配設し、機関のクランク軸に配設した機関回転数セ
ンサの信号に基づき機関の回転変動率を求める電子制御
装置を備え、機関の回転変動率が所定値よりも小さい時
電子制御装置に出力によりバイパス弁を閉じ、機関の回
転変動率が所定値よりも大きい時電子制御装置に出力に
よりバイパス弁を開くようにしたものである。[Means for Solving the Problem] In order to achieve the above object, the structure of the present invention connects a turbocharger and a power turbine in sequence to an exhaust pipe of an engine, and connects the turbocharger and a power turbine. A bypass valve that discharges exhaust gas from the turbocharger when the valve is open is installed in the middle of the pipe, and the rotational fluctuation rate of the engine is calculated based on the signal from the engine speed sensor that is installed on the crankshaft of the engine. Equipped with an electronic control unit, the bypass valve is closed by output to the electronic control unit when the engine rotation fluctuation rate is smaller than a predetermined value, and the bypass valve is output by output to the electronic control unit when the engine rotation fluctuation rate is larger than the predetermined value. It was opened.
[作用] 機関の回転変動率は、機関回転数センサの信号から電子
制御装置により演算される。機関の回転変動率が所定値
(流体クラツチ、変速機などの強度から勘案して決定さ
れる)よりも小さい場合は、電子制御装置の出力により
バイパス弁が閉じられる。ターボ過給機のタービンから
出た排気は、バイパス弁を経てパワータービンへ導入さ
れ、排気エネルギが動力として機関へ回収される。[Operation] The engine speed fluctuation rate is calculated by the electronic control unit from the signal from the engine speed sensor. When the rotational fluctuation rate of the engine is smaller than a predetermined value (determined in consideration of the strength of the fluid clutch, transmission, etc.), the bypass valve is closed by the output of the electronic control unit. Exhaust gas from the turbocharger turbine is introduced into the power turbine through a bypass valve, and the exhaust energy is recovered as power by the engine.
機関の回転変動率が所定値よりも大きい場合は、電子制
御装置の出力によりバイパス弁が開かれる。ターボ過給
機のタービンから出た排気は接続管、バイパス弁を経て
外部へ放出され、パワータービンは排気を導入されな
い。パワータービンは駆動されず、流体クラツチや変速
機の損傷を回避する。When the rotational fluctuation rate of the engine is larger than the predetermined value, the bypass valve is opened by the output of the electronic control unit. Exhaust gas emitted from the turbine of the turbocharger is discharged to the outside through the connecting pipe and the bypass valve, and the power turbine does not introduce the exhaust gas. The power turbine is not driven, avoiding damage to the fluid clutch and transmission.
[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、タービン8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。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
車とブロア6の翼車とが結合され、ブロア6により吸気
が加圧されて機関2へ供給される。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 an outlet of the turbine 8 is connected to a connecting pipe 9. Connected to the inlet of the power turbine 12. Power turbine 12
Is connected to the exhaust pipe 26 and is opened to the outside through a silencer. In the turbocharger 5, an impeller of a turbine 8 and an impeller of a blower 6 are connected by a shaft 7, and intake air is pressurized by the blower 6 and 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は流体ク
ラツチ16の入力側に結合される。流体クラツチ16の
出力側は軸17を介して減速機18の入力歯車21に結
合され、減速機18の出力歯車24は機関2のクランク
軸19に結合される。The shaft 13 of the power turbine 12 is connected to the sun gear of the planetary gear reducer 14, while the shaft 15 of the ring gear is connected to the input side of the fluid clutch 16. The output side of the fluid clutch 16 is connected to the input gear 21 of the speed reducer 18 via the shaft 17, and the output gear 24 of the speed reducer 18 is connected to the crankshaft 19 of the engine 2.
なお、流体クラツチ16には作動油として機関2を潤滑
する潤滑油が供給され、逆止弁39を経てオイルパン4
0へ戻される。Note that the fluid clutch 16 is supplied with lubricating oil that lubricates the engine 2 as operating oil, and passes through the check valve 39 to the oil pan 4
Returned to 0.
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の入口との接続管の途中に、バイパス弁10が設けら
れ、バイパス弁10を開くとタービン8の出口側がバイ
パス管20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。バイパス弁10は機
関の急加速運転および急減速運転では開かれ、通常の運
転では閉じられる。つまり、機関の回転変動率が所定値
よりも小さい時は、電子制御装置に出力によりバイパス
弁10は閉じられ、機関の回転変動率が所定値よりも大
きい時は、電子制御装置に出力によりバイパス弁10は
開かれる。Outlet of turbine 8 of turbocharger 5 and power turbine 1
A bypass valve 10 is provided in the middle of the connection pipe with the inlet of the second valve 2. When the bypass valve 10 is opened, the outlet side of the turbine 8 is communicated with the bypass pipe 20, and the exhaust gas is directly discharged to the outside and sent to the power turbine 12. I can't. The bypass valve 10 is opened during the sudden acceleration operation and the sudden deceleration operation of the engine, and is closed during the normal operation. That is, when the engine speed fluctuation rate is smaller than the predetermined value, the bypass valve 10 is closed by the output to the electronic control device, and when the engine speed fluctuation rate is larger than the predetermined value, the bypass valve 10 is bypassed by the output to the electronic control device. The valve 10 is opened.
図示の実施例では、機関2のクランク軸19に機関回転
数センサ35が配設され、機関回転数センサ35の信号
がマイクロコンピユータからなる電子制御装置36へ入
力され、機関回転数の経時的変化から回転変動率が演算
される。回転変動率に基づく電子制御装置36の出力に
よりバイパス弁10が開閉される。バイパス弁10は電
磁弁として構成され、例えば電磁コイルないし電磁アク
チユエータが通電されると、バイパス弁10が開き、逆
に非通電されると、バイパス弁10が閉じるように構成
される。In the illustrated embodiment, an engine speed sensor 35 is arranged on the crankshaft 19 of the engine 2, and a signal from the engine speed sensor 35 is input to an electronic control unit 36 composed of a microcomputer to change the engine speed with time. From this, the rotation fluctuation rate is calculated. The bypass valve 10 is opened and closed by the output of the electronic control unit 36 based on the rotation fluctuation rate. The bypass valve 10 is configured as an electromagnetic valve. For example, when the electromagnetic coil or the electromagnetic actuator is energized, the bypass valve 10 is opened, and conversely, when it is de-energized, the bypass valve 10 is closed.
第2図は上述の制御プログラムの流れ図であり、p11〜
p15は各ステツプで示す。p11で回転数センサ35の信
号に基づく機関回転数を逐次入力し、p12で所定時間毎
に入力される機関回転数から回転変動率を算出する。p
13で回転変動率が所定値αよりも大きいか否かを判別す
る。回転変動率が所定値αよりも小さい場合は、p15で
バイパス弁10を閉じる。一方、回転変動率が所定値α
よりも大きい場合は、p14でバイパス弁10を開く。FIG. 2 is a flow chart of the control program described above.
p15 is shown at each step. At p11, the engine speed based on the signal from the speed sensor 35 is sequentially input, and at p12, the rotational fluctuation rate is calculated from the engine speed input at every predetermined time. p
At 13, it is determined whether or not the rotation fluctuation rate is larger than the predetermined value α. When the rotation fluctuation rate is smaller than the predetermined value α, the bypass valve 10 is closed at p15. On the other hand, the rotation fluctuation rate is a predetermined value α
If it is larger than that, the bypass valve 10 is opened at p14.
[発明の効果] 本発明は上述のように、ターボ過給機とパワータービン
との間に配設したバイパス弁の開閉を、回転変動率に関
連して制御するように構成したので、機関の急加速運転
では、バイパス弁が開かれ、ターボ過給機だけが作動
し、パワータービンは停止しているので、パワータービ
ンを駆動することによる一時的な軸出力の損失・低下
と、加速性能の低下とが回避される。[Advantages of the Invention] As described above, the present invention is configured to control the opening / closing of the bypass valve arranged between the turbocharger and the power turbine in relation to the rotational fluctuation rate. In rapid acceleration operation, the bypass valve is opened, only the turbocharger is operating, and the power turbine is stopped.Therefore, temporary loss / decrease in shaft output due to driving the power turbine and acceleration performance Deterioration is avoided.
また、機関の急減速運転でも、バイパス弁が開かれ、パ
ワータービンが駆動されないので、機関のクランク軸か
ら変速機および流体クラツチを経てパワータービンの出
力軸へ伝達される過大な逆トルクによる流体クラツチの
損傷や歯車変速機における歯車の損傷などが回避され
る。In addition, even when the engine suddenly decelerates, the bypass valve is opened and the power turbine is not driven.Therefore, the fluid clutch due to the excessive reverse torque transmitted from the crankshaft of the engine to the output shaft of the power turbine through the transmission and the fluid clutch. And damage to gears in the gear transmission are avoided.
一方、通常の運転では、バイパス弁は閉じられ、パワー
タービンが駆動されるので、排気エネルギが動力として
有効に回収され、安定した走行が得られ、軸出力の増大
と走行燃費の向上が得られる。On the other hand, in normal operation, the bypass valve is closed and the power turbine is driven, so exhaust energy is effectively recovered as power, stable running is obtained, and shaft output and running fuel consumption are improved. .
第1図は本発明に係るターボコンパウンド機関の概略構
成図、第2図はターボコンパウンド機関におけるバイパ
ス弁をマイクロコンピユータで作動させる制御プログラ
ムの流れ図、第3図はターボコンパウンド機関の急加速
時の過渡特性を表す線図である。 2:内燃機関、5:ターボ過給機、9:接続管、10:
バイパス弁、12:パワータービン、14:遊星歯車減
速機、16:流体クラツチ、18:減速機、19:クラ
ンク軸、20:バイパス管、35:機関回転数センサ、
36:電子制御装置FIG. 1 is a schematic configuration diagram of a turbo compound engine according to the present invention, FIG. 2 is a flow chart of a control program for operating a bypass valve in the turbo compound engine by a micro computer, and FIG. 3 is a transient during rapid acceleration of the turbo compound engine. It is a diagram showing characteristics. 2: internal combustion engine, 5: turbocharger, 9: connecting pipe, 10:
Bypass valve, 12: power turbine, 14: planetary gear reducer, 16: fluid clutch, 18: reducer, 19: crankshaft, 20: bypass pipe, 35: engine speed sensor,
36: Electronic control unit
Claims (1)
ビンを順に接続し、ターボ過給機とパワータービンとを
接続する管の途中に、開弁時ターボ過給機からの排気を
外部へ放出するバイパス弁を配設し、機関のクランク軸
に配設した機関回転数センサの信号に基づき機関の回転
変動率を求める電子制御装置を備え、機関の回転変動率
が所定値よりも小さい時電子制御装置に出力によりバイ
パス弁を閉じ、機関の回転変動率が所定値よりも大きい
時電子制御装置に出力によりバイパス弁を開くことを特
徴とする、ターボコンパウンド機関。1. A turbocharger and a power turbine are sequentially connected to an exhaust pipe of an engine, and the exhaust gas from the turbocharger at the time of opening the valve is externally provided in the middle of a pipe connecting the turbocharger and the power turbine. Equipped with a bypass valve that discharges to the engine, equipped with an electronic control unit that obtains the engine speed fluctuation rate based on the signal from the engine speed sensor installed on the engine crankshaft, and the engine speed fluctuation rate is smaller than a specified value. A turbo compound engine, characterized in that the bypass valve is closed by output to the electronic control unit, and the bypass valve is opened by output to the electronic control unit when the rotational fluctuation rate of the engine is larger than a predetermined value.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP61255870A JPH0612070B2 (en) | 1986-10-29 | 1986-10-29 | Turbo Compound Organization |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP61255870A JPH0612070B2 (en) | 1986-10-29 | 1986-10-29 | Turbo Compound Organization |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS63111239A JPS63111239A (en) | 1988-05-16 |
| JPH0612070B2 true JPH0612070B2 (en) | 1994-02-16 |
Family
ID=17284719
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP61255870A Expired - Lifetime JPH0612070B2 (en) | 1986-10-29 | 1986-10-29 | Turbo Compound Organization |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPH0612070B2 (en) |
Families Citing this family (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE102006004092B3 (en) * | 2006-01-28 | 2007-08-16 | Man B & W Diesel A/S | Two-stroke large-diesel engine, has hydraulic power unit driven by drive unit that is operable with exhaust gas in upper output region, where hydraulic power unit composes pump and is assigned to common rail |
| DE102008064521B4 (en) * | 2008-12-18 | 2021-05-20 | Dr. Ing. H.C. F. Porsche Aktiengesellschaft | Internal combustion engine with exhaust gas turbocharger |
| CN115034020A (en) * | 2022-06-30 | 2022-09-09 | 李惠彬 | Electromechanical coupling power generation device based on engine exhaust turbine kinetic energy and design method |
-
1986
- 1986-10-29 JP JP61255870A patent/JPH0612070B2/en not_active Expired - Lifetime
Also Published As
| Publication number | Publication date |
|---|---|
| JPS63111239A (en) | 1988-05-16 |
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