JPS5982526A - Supercharger for internal-combustion engine - Google Patents
Supercharger for internal-combustion engineInfo
- Publication number
- JPS5982526A JPS5982526A JP57191423A JP19142382A JPS5982526A JP S5982526 A JPS5982526 A JP S5982526A JP 57191423 A JP57191423 A JP 57191423A JP 19142382 A JP19142382 A JP 19142382A JP S5982526 A JPS5982526 A JP S5982526A
- Authority
- JP
- Japan
- Prior art keywords
- turbine
- bypass
- engine
- pressure stage
- exhaust
- 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
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
- F02B37/00—Engines characterised by provision of pumps driven at least for part of the time by exhaust
- F02B37/013—Engines characterised by provision of pumps driven at least for part of the time by exhaust with exhaust-driven pumps arranged in series
-
- 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
- F02B37/00—Engines characterised by provision of pumps driven at least for part of the time by exhaust
- F02B37/004—Engines characterised by provision of pumps driven at least for part of the time by exhaust with exhaust drives arranged in series
-
- 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)
Abstract
Description
【発明の詳細な説明】
本発明は、自動車用機関等として使用される内燃機関の
過給装置に関するものである。DETAILED DESCRIPTION OF THE INVENTION The present invention relates to a supercharging device for an internal combustion engine used as an automobile engine or the like.
自動車用48関のように小型軽量化、高出力及び低燃費
等が要求される内燃機関では、排気タボ過給機を付設し
て燃焼条件を改善することが有効である。For internal combustion engines such as the 48 engine for automobiles, which are required to be compact and lightweight, high output, and low fuel consumption, it is effective to improve the combustion conditions by adding an exhaust turbo supercharger.
ところが、自動車用機関のように運転回転域及び負荷領
域の広い内?一機関に単に排気ターホ過給機を組み合わ
せただけでは、必ずしも機関の運転性が良(ならない。However, within a wide operating rotation range and load range like an automobile engine? Simply combining an exhaust turbocharger with an engine does not necessarily result in good engine operability.
即ち、機1猫の最高出力を重視して過給機を高速域でマ
ツチングさせると、タービン効率が低下する中低速域で
のトルク及び加速性が低下して運転性が悪化する。That is, if the supercharger is matched in the high speed range with emphasis on the maximum output of machine 1, the torque and acceleration performance in the medium and low speed range where turbine efficiency decreases will decrease, resulting in deterioration of drivability.
又、逆に、中低速域でのトルク及び加速性を重視して過
給機を中低速域でマツチングさせると、高速域での給気
圧が過大となって機関の耐久性及び騒音に悪影響を及は
すと同時に、私情室内での余剰空気が過度に多くなって
機関のボンピングロスが増大するために燃料消費率が悪
化するという不都合があった。On the other hand, if the turbocharger is matched in the mid-to-low speed range with emphasis on torque and acceleration in the mid-to-low speed range, the boost pressure in the high-speed range will become excessive, which will have a negative impact on engine durability and noise. At the same time, there was an inconvenience in that excess air in the private room became excessively large, increasing the engine's pumping loss and deteriorating the fuel consumption rate.
一方、機関の排気エネルギの回収率を向上させるために
2基の排気ターボ過給機を直列に接続した2段過給装置
もあるが、この2段過給装置の場合にも前記の場合と同
様の特性が見られるという欠点があった。On the other hand, there is also a two-stage supercharging system in which two exhaust turbo superchargers are connected in series in order to improve the recovery rate of exhaust energy of the engine, but this two-stage supercharging system is also similar to the above case. The drawback was that similar characteristics were observed.
本発明は、このような実状に鑑みてなされたもので、2
基の排気ターボ過給機を直列に接続していわゆる2段過
給を行なわせるようにし、置1圧段(FIl+の過給機
のタービン及びコンプレッサにそhぞれ排気バイパス路
及び給気バイパス路を設けると共に、前記タービン、コ
ンプレッサ及び両バイパス路の流量を可変制御するバイ
パス弁を設けることにより、機関の運転状態に応じて過
給機の運転パターンを変え、以って、機関の運転状態に
応答して給気圧を最適制御して機関の出力性能、加速性
能及び燃料消費率等を改善しようとするものである。The present invention has been made in view of the above-mentioned circumstances.
The main exhaust turbo superchargers are connected in series to perform so-called two-stage supercharging, and the turbine and compressor of the first pressure stage (FIl+ supercharger are connected to an exhaust bypass passage and an air intake bypass passage, respectively). By providing a bypass valve that variably controls the flow rates of the turbine, compressor, and both bypass paths, the operating pattern of the supercharger can be changed according to the operating state of the engine. The aim is to optimally control the boost pressure in response to the engine's engine output performance, acceleration performance, fuel consumption rate, etc.
以下に本発明を図示された一実施例に基づいて詳細に説
明する。The present invention will be explained in detail below based on an illustrated embodiment.
図示しない自動車に搭載された機関1の吸気通路には、
図示しないエアクリーナを介して吸入した空気を加圧す
る低圧段排気ターボ過給機2 (7) コア フレツサ
2 a (!: 、’Zのコンプレッサ2aから吐出さ
れた加圧空気を更に加圧して機関1に送シ込む高圧段排
気ターボ過給機3のコンプレッサ3aとを介装しており
、低圧段排気ターボ過給機2のタービン2bと機関1の
排気マニフオールドとの間に高圧段排気ターボ過給機3
のタービン3bを介装することにより、いわゆる2段過
給装置を構成している。In the intake passage of the engine 1 mounted on a car (not shown),
A low-pressure stage exhaust turbo supercharger 2 that pressurizes air taken in through an air cleaner (not shown). The compressor 3a of the high pressure stage exhaust turbo supercharger 3 is interposed between the turbine 2b of the low pressure stage exhaust turbo supercharger 2 and the exhaust manifold of the engine 1. Feeder 3
By interposing the turbine 3b, a so-called two-stage supercharging device is constructed.
又、高圧段排気ターボ過給機3のコンプレッサ3a及び
タービン3bの入口と出口とをそれぞれ鞘気バイパス路
4と排気バイパス路5とを介して接続している。そして
、この両バイパス路4,5の上下両端部にそれぞれバイ
パス路4゜5の開度を拡狭調整してバイパス流量を可変
制御するバイパス弁6,7を設けると共に、給気通路及
び排気通路における両バイパス路4,5との分岐点より
下流の部分及び両バイパス路4゜5との合流点より上流
の部分、す1」ち、コンプレッサ3a及びタービン3b
の入口及び出口部分にそれぞt1バイパス弁8.9を設
けることにより、これらのバイパス弁8.9の開度を調
整してコンプレッサ3a及びタービン3bの流量を調整
できるようにもしている。10は高圧段排気ターボ過給
機3のコンプレッサ入口に設けたインタクーラ、11(
l−1給気通路の下流端部分、例えば、給気通路と給気
マニフオールドとの接続部等に介装したアフタクーラで
あり、前記各バイパス弁6,7,8.9は、機関1の運
転情報(回転数、負荷等)が入力されるコントローラで
開JM NL’111整さiするようになっている。Further, the inlet and outlet of the compressor 3a and turbine 3b of the high-pressure exhaust turbocharger 3 are connected via a sheath air bypass passage 4 and an exhaust bypass passage 5, respectively. Bypass valves 6 and 7 are provided at the upper and lower ends of the bypass passages 4 and 5, respectively, for variably controlling the bypass flow rate by adjusting the opening degree of the bypass passages 4 and 5, respectively. The part downstream from the branching point with both bypass passages 4 and 5 and the part upstream from the junction with both bypass passages 4 and 5, i.e., the compressor 3a and the turbine 3b.
By providing t1 bypass valves 8.9 at the inlet and outlet portions of the t1 bypass valves 8.9, the opening degrees of these bypass valves 8.9 can be adjusted to adjust the flow rates of the compressor 3a and the turbine 3b. 10 is an intercooler installed at the compressor inlet of the high-pressure stage exhaust turbo supercharger 3; 11 (
1-1 is an aftercooler installed at the downstream end of the air supply passage, for example, at the connection between the air supply passage and the air supply manifold, and each of the bypass valves 6, 7, 8.9 The controller to which operating information (rotational speed, load, etc.) is input is configured to perform the Open JM NL'111 adjustment.
上記の構成において、図示しない各センサからの111
力信号(機関の運転情報)に基ついて機関が中低速領域
で運転されていると判断した時は、給気バイパス路4及
び排気バイパス路5に設けた各バイパス弁6,7が全閉
状態に保持されると共に、高圧段排気ターボ過給機3の
コンプレッサ3a及びタービン3bの出入口部分に設け
た各バイパス弁8,9がそれぞれ全開状態に保持される
。従って、この時は、機関lの排気が高圧段排気ターボ
過給機3のタービン3bを駆動した後に低圧段排気ター
ボ過給機2のクービン2bを駆動するので、従来公知の
2段過給が行なわれる。In the above configuration, 111 from each sensor (not shown)
When it is determined that the engine is operating in a medium-low speed range based on the engine power signal (engine operating information), the bypass valves 6 and 7 provided in the air supply bypass path 4 and the exhaust bypass path 5 are fully closed. At the same time, the bypass valves 8 and 9 provided at the inlet and outlet portions of the compressor 3a and turbine 3b of the high-pressure stage exhaust turbo supercharger 3 are respectively kept fully open. Therefore, at this time, the exhaust gas of the engine l drives the turbine 3b of the high-pressure stage exhaust turbo supercharger 3 and then the turbine 2b of the low-pressure stage exhaust turbo supercharger 2, so that the conventionally known two-stage supercharging is performed. It is done.
又、前記した運転状報に基づいて機関1が高速運転され
ていると判断した時は、コントローラからの指令で各バ
イパス路4.511411のバイパス弁6,7が全開保
持されると同時に、高速段a1気ターボ:+1φ給機3
のコンプレッサ3a及びタービン3bの出入口部分に設
けたバイパス方8゜9が全閉保持される。すると、+1
シ関1から排出さiした排気が高速段排気ターボ過給機
3のタービン3bをバイパスして低圧段排気ターボ過給
機2のタービン2bに直接供給さノLるので、低圧段排
気ターボ過給機2のみが駆動さi′Lる。このために、
機関1の高速運転領域で排気エネルギが上昇し7ようと
も、給気圧の過大及び温度上昇が抑制され、余剰空気漏
の少ない状態で機関1を効率よく運転できる。Also, when it is determined that the engine 1 is being operated at high speed based on the above-mentioned operating status information, the bypass valves 6 and 7 of each bypass path 4.511411 are held fully open by a command from the controller, and at the same time Stage a1 air turbo: +1φ feeder 3
Bypasses 8.9 provided at the inlet and outlet portions of the compressor 3a and turbine 3b are kept fully closed. Then +1
The exhaust gas discharged from the engine 1 bypasses the turbine 3b of the high-pressure exhaust turbocharger 3 and is directly supplied to the turbine 2b of the low-pressure exhaust turbocharger 2. Only feeder 2 is driven i'L. For this,
Even if the exhaust energy increases in the high-speed operating range of the engine 1, excessive boost pressure and temperature rise are suppressed, and the engine 1 can be operated efficiently with little surplus air leakage.
一方、排気ブレーキの作動時のように給排気路をともに
閉塞する必吸がある時は、すべてのバイパス弁6,7,
8.9を全開作動させる。On the other hand, when there is a necessary intake that blocks both the supply and exhaust passages, such as when the exhaust brake is activated, all the bypass valves 6, 7,
8. Operate 9 fully.
すると、1f71圧段排気ターボ過給機3のコンプレッ
サ3a、タービン3b及び両バイパス路4゜5がともに
閉塞されて給排気を遮断するので、従来のように独立し
た排気ブレーキ弁、ノイズザプレツザ等を設ける必要性
がなくなる。Then, the compressor 3a, turbine 3b, and both bypass passages 4.5 of the 1f71 pressure stage exhaust turbo supercharger 3 are blocked, cutting off the supply and exhaust, so an independent exhaust brake valve, noise suppressor, etc. are provided as in the past. The need disappears.
尚、上記実施例では、バイパス弁を全開か全開に切替作
動させるようにしているのみであるが、と1しらの開度
を多段階又は無段階に調整してバイパス路4,5、コン
プレッサ3a、タービン3 b等の流星をきめ細かく可
変制御して給気圧力等を最適制御するようにしても良く
、かつ、機関の運転状態を回転数、負荷に加えて、給気
圧力、給気温度、排気圧力、排気温度、回転峨及び負荷
等の変動状態、機関温度、過給機の回転数等から総合的
に判断することが望寸しい。Incidentally, in the above embodiment, the bypass valve is only operated by switching between fully open and completely open, but the opening degree of the bypass valve is adjusted in multiple stages or steplessly to control the bypass passages 4, 5 and the compressor 3a. , turbine 3b, etc. may be finely and variably controlled to optimally control the supply air pressure, etc., and the operating state of the engine may be controlled in addition to the rotation speed and load to determine the supply air pressure, supply air temperature, It is desirable to make a comprehensive judgment based on exhaust pressure, exhaust temperature, fluctuations in rotational peak and load, engine temperature, supercharger rotation speed, etc.
以上説明したように本発明によれば、低圧段シ1.気タ
ーボ過給機とともに2段過給装置を構成する高圧段排気
ターボ】!蹟給機のコンプレッサとタービンとにそれぞ
れバイパス路を設け、前記コンプレッサ、タービン及び
両バイパス路の流量(開度)を可変制御するバイパス弁
を設けているので、機関の運転状態に応じてバイパス弁
を開閉制御して給気圧を最適制御して機関の出力制能、
加速性能及び燃料消費率等を向上できる。As explained above, according to the present invention, the low pressure stage 1. A high-pressure stage exhaust turbo that constitutes a two-stage supercharging device together with a gas turbo supercharger]! A bypass passage is provided for each of the compressor and turbine of the feeder, and a bypass valve is provided to variably control the flow rate (opening degree) of the compressor, turbine, and both bypass passages. Controls engine output by controlling opening and closing to optimally control supply pressure.
Acceleration performance, fuel consumption rate, etc. can be improved.
図は本発明の一実施例の開示(1り成図である。
1・・・機関 2・・・低圧段排気〃−ボ過給機2a
・・・コンプレッサ 2b・・・タービン3・・・高
圧段排気ターボ過給機
3a・・・コンプレッサ 3b中タービン4・・・給
気バイパス路 5・・・排気バイパス路6、7.8.
9・・・バイパス弁。
特許出願人
日野自動車工業株式会社
149The figure shows an embodiment of the present invention. 1. Engine 2. Low-pressure stage exhaust turbocharger 2a
...Compressor 2b...Turbine 3...High pressure stage exhaust turbo supercharger 3a...Compressor 3b middle turbine 4...Air supply bypass path 5...Exhaust bypass path 6, 7.8.
9...Bypass valve. Patent applicant Hino Motors Co., Ltd. 149
Claims (1)
気ターボ過給機と、該過給機で加圧した空気を更に加圧
して機関に送り込む高圧段排気ターボ過給機とを備えて
なシ、機関の排気マニフォールドと低圧段排気ターボ過
給機のタービン入口との間に高圧段排気ターボ過給機の
タービンを介装し、高圧段排気ターボ過給機のコンプレ
ッサ及びタービンの入口と出口とをそれぞれ給気バイパ
ス路及び排気バイパス路を介して接続すると共に、高圧
段排気ターボ過給機のコンプレッサ、タービン及び前記
両バイパス路の流量を可変制御するバイパス弁を設けた
ことを特徴とする内燃機関の過給@置。A low pressure stage exhaust turbo supercharger that pressurizes air taken in through an air cleaner, and a high pressure stage exhaust turbo supercharger that further pressurizes the air pressurized by the supercharger and sends it to the engine, The turbine of the high pressure stage exhaust turbo supercharger is interposed between the exhaust manifold of the engine and the turbine inlet of the low pressure stage exhaust turbo supercharger, and the inlet and outlet of the compressor and turbine of the high pressure stage exhaust turbo supercharger are connected. An internal combustion engine characterized by being provided with a bypass valve that is connected to each other via an air supply bypass passage and an exhaust bypass passage, and that variably controls the compressor and turbine of a high-pressure stage exhaust turbo supercharger, and the flow rates of both of the bypass passages. Supercharging@place.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP57191423A JPS5982526A (en) | 1982-10-29 | 1982-10-29 | Supercharger for internal-combustion engine |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP57191423A JPS5982526A (en) | 1982-10-29 | 1982-10-29 | Supercharger for internal-combustion engine |
Publications (1)
Publication Number | Publication Date |
---|---|
JPS5982526A true JPS5982526A (en) | 1984-05-12 |
Family
ID=16274362
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP57191423A Pending JPS5982526A (en) | 1982-10-29 | 1982-10-29 | Supercharger for internal-combustion engine |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPS5982526A (en) |
Cited By (18)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS62214230A (en) * | 1986-03-08 | 1987-09-21 | エムテ−ウ−・モ−トレン−ウント・ツルビネン−ウニオン・フリ−ドリツヒスハ−フエン・ゲゼルシヤフト・ミツト・ベシユレンクタ−・ハフツング | Piston internal combustion engine having two-step charger |
JPS62197729U (en) * | 1986-06-09 | 1987-12-16 | ||
DE3933518A1 (en) * | 1988-10-06 | 1990-04-12 | Toyota Motor Co Ltd | INTERNAL COMBUSTION ENGINE WITH A SEQUENTIAL TURBOCHARGER SYSTEM |
JPH0280730U (en) * | 1988-12-13 | 1990-06-21 | ||
US5142866A (en) * | 1990-06-20 | 1992-09-01 | Toyota Jidosha Kabushiki Kaisha | Sequential turbocharger system for an internal combustion engine |
US5199261A (en) * | 1990-08-10 | 1993-04-06 | Cummins Engine Company, Inc. | Internal combustion engine with turbocharger system |
EP0864737A1 (en) * | 1997-03-11 | 1998-09-16 | Man Nutzfahrzeuge Ag | Control device for a pressure-charged internal combustion engine |
US6112523A (en) * | 1998-04-30 | 2000-09-05 | Fuji Jukogyo Kabushiki Kaisha | Multistage supercharging system for a reciprocating engine |
EP1375868A1 (en) * | 2002-06-26 | 2004-01-02 | Borg Warner Inc. | Engine brake apparatus for a turbocharged IC engine |
WO2004046519A1 (en) * | 2002-11-20 | 2004-06-03 | Honeywell International Inc. | Sequential turbocharging system and a method for sequential turbocharging of an internal combustion engine |
EP1519017A1 (en) * | 2003-09-26 | 2005-03-30 | Toyota Jidosha Kabushiki Kaisha | Turbocharging system |
DE102006011188A1 (en) | 2006-03-10 | 2007-09-13 | Bayerische Motoren Werke Ag | Two-stage exhaust gas turbocharger arrangement for internal combustion engine, has high and low pressure turbochargers, where turbine of one high pressure turbocharger and turbine of low pressure turbocharger are connected with each other |
WO2008018577A1 (en) | 2006-08-10 | 2008-02-14 | Mitsubishi Heavy Industries, Ltd. | Method of manufacturing multi-stage supercharging exhaust turbosupercharger |
WO2008018574A1 (en) | 2006-08-10 | 2008-02-14 | Mitsubishi Heavy Industries, Ltd. | Multi-stage supercharging exhaust turbosupercharger |
US20100089342A1 (en) * | 2007-02-28 | 2010-04-15 | Behr Gmbh & Co. Kg | Charge-air cooling device, system for turbocharging and/or charge-air cooling, method for charge-air cooling |
US20110041497A1 (en) * | 2009-08-20 | 2011-02-24 | Gm Global Technology Operations, Inc. | Two-stage turbocharged engine system |
CN102434283A (en) * | 2011-11-09 | 2012-05-02 | 无锡康明斯涡轮增压技术有限公司 | Integrated low-pressure stage turbine shell structure for two-stage supercharging exhaust gas turbocharger |
CN104533599A (en) * | 2014-12-29 | 2015-04-22 | 中国船舶重工集团公司第七一一研究所 | Two-stage adjustable pressurization system of internal combustion engine |
Citations (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS5584816A (en) * | 1978-12-18 | 1980-06-26 | Hino Motors Ltd | Apparatus for raising low-speed torque of internal combustion engine |
-
1982
- 1982-10-29 JP JP57191423A patent/JPS5982526A/en active Pending
Patent Citations (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS5584816A (en) * | 1978-12-18 | 1980-06-26 | Hino Motors Ltd | Apparatus for raising low-speed torque of internal combustion engine |
Cited By (25)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS62214230A (en) * | 1986-03-08 | 1987-09-21 | エムテ−ウ−・モ−トレン−ウント・ツルビネン−ウニオン・フリ−ドリツヒスハ−フエン・ゲゼルシヤフト・ミツト・ベシユレンクタ−・ハフツング | Piston internal combustion engine having two-step charger |
US4753076A (en) * | 1986-03-08 | 1988-06-28 | Mtu Friedrichshafen Gmbh | Piston internal combustion engine with two-stage supercharging |
JPS62197729U (en) * | 1986-06-09 | 1987-12-16 | ||
DE3933518A1 (en) * | 1988-10-06 | 1990-04-12 | Toyota Motor Co Ltd | INTERNAL COMBUSTION ENGINE WITH A SEQUENTIAL TURBOCHARGER SYSTEM |
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