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JPS63183225A - How to operate a diesel engine with a power turbine - Google Patents

How to operate a diesel engine with a power turbine

Info

Publication number
JPS63183225A
JPS63183225A JP62011379A JP1137987A JPS63183225A JP S63183225 A JPS63183225 A JP S63183225A JP 62011379 A JP62011379 A JP 62011379A JP 1137987 A JP1137987 A JP 1137987A JP S63183225 A JPS63183225 A JP S63183225A
Authority
JP
Japan
Prior art keywords
diesel engine
power turbine
exhaust gas
superchargers
bypass
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
JP62011379A
Other languages
Japanese (ja)
Inventor
Hiroyuki Sugihara
啓之 杉原
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.)
IHI Corp
Original Assignee
Ishikawajima Harima Heavy Industries Co 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 Ishikawajima Harima Heavy Industries Co Ltd filed Critical Ishikawajima Harima Heavy Industries Co Ltd
Priority to JP62011379A priority Critical patent/JPS63183225A/en
Publication of JPS63183225A publication Critical patent/JPS63183225A/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
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B37/00Engines characterised by provision of pumps driven at least for part of the time by exhaust
    • F02B37/001Engines characterised by provision of pumps driven at least for part of the time by exhaust using exhaust drives arranged in parallel
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B37/00Engines characterised by provision of pumps driven at least for part of the time by exhaust
    • F02B37/007Engines characterised by provision of pumps driven at least for part of the time by exhaust with exhaust-driven pumps arranged in parallel, e.g. at least one pump supplying alternatively
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B37/00Engines characterised by provision of pumps driven at least for part of the time by exhaust
    • F02B37/12Control of the pumps
    • F02B37/18Control of the pumps by bypassing exhaust from the inlet to the outlet of turbine or to the atmosphere
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B3/00Engines characterised by air compression and subsequent fuel addition
    • F02B3/06Engines characterised by air compression and subsequent fuel addition with compression ignition
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Supercharger (AREA)

Abstract

(57)【要約】本公報は電子出願前の出願データであるた
め要約のデータは記録されません。
(57) [Summary] This bulletin contains application data before electronic filing, so abstract data is not recorded.

Description

【発明の詳細な説明】 [産業上の利用分野] 本発明は2台以上の過給機を装着したパワータービン付
ディーゼル機関において、適数の過給機をカット運転す
るときの運転方法に関するものである。
[Detailed Description of the Invention] [Industrial Application Field] The present invention relates to an operating method for cut-off operation of an appropriate number of superchargers in a power turbine-equipped diesel engine equipped with two or more superchargers. It is.

[従来の技術] 2台以上の過給機を装着したパワータービン付ディーゼ
ル機関は、これが船に使用されている場合において船の
速度を余り必要としない場合とか、1台の過給機が故障
したような場合等では過給機の使用台数を減らして運転
されている。−例として、2台の過給機を装着したパワ
ータービン付ディーゼル機関について説明すると、従来
では、第3図に示す如く、排気ガスによりタービン翼車
を回転させるタービンTと、タービン翼車の回転により
翼車を回転して吸気を圧縮するコンプレッサCを備えた
2台の過給機1と2をパワータービン4付きのディーゼ
ル機関3に装着し、ディーゼル機関3の負荷が50%以
上のときディーゼル機関から各過給機1,2のタービン
Tへ送られる排気ガスの一部をバイパスさせてパワータ
ービン4を運転し、該パワータービン4で動力として回
収してディーゼル機関の主軸に戻したりするようにしで
ある。5はパワータービン4の入口側バイパスラインに
設けられたバルブである。
[Prior art] A diesel engine with a power turbine equipped with two or more superchargers is used on a ship when the speed of the ship is not required or when one supercharger breaks down. In such cases, the number of turbochargers used is reduced. - As an example, to explain a diesel engine with a power turbine equipped with two superchargers, as shown in FIG. Two superchargers 1 and 2 equipped with a compressor C that compresses intake air by rotating a blade wheel are attached to a diesel engine 3 equipped with a power turbine 4, and when the load of the diesel engine 3 is 50% or more, the diesel A part of the exhaust gas sent from the engine to the turbine T of each supercharger 1, 2 is bypassed to operate the power turbine 4, and the power turbine 4 recovers it as power and returns it to the main shaft of the diesel engine. It's Nishide. Reference numeral 5 denotes a valve provided in the bypass line on the inlet side of the power turbine 4.

上記ディーゼル機関3から過給@1,2に送られる排気
ガスの一部をパワータービン4に導いてバイパスさせる
量は、ディーゼル機関3から過給機1.2へ送られる排
気ガスのトータル量の約10〜20%位が最良とされて
いる。バイパス量が少なすぎると、パワータービン4の
翼車を充分に回転できないため充分な動力回収が図れず
、又、バイパス量が多いと、パワータービン4の性能は
向上するが、過給機への排気ガス量が減少して充分な出
力が得られず、これがディーゼル機関の性能を悪化させ
ることになるからである。
The amount of part of the exhaust gas sent from the diesel engine 3 to the superchargers 1 and 2 to the power turbine 4 and bypassed is the total amount of exhaust gas sent from the diesel engine 3 to the supercharger 1.2. Approximately 10 to 20% is said to be the best. If the amount of bypass is too small, the impeller of the power turbine 4 cannot be rotated sufficiently, making it impossible to recover sufficient power. If the amount of bypass is too large, the performance of the power turbine 4 improves, but the power to the supercharger is This is because the amount of exhaust gas decreases and sufficient output cannot be obtained, which deteriorates the performance of the diesel engine.

[発明が解決しようとする問題点] ところが、前記した従来のパワータービン付ディーゼル
機関では、パワータービン4の排気ガス入口ケーシング
が1つ目構造であるため、2台の過給機1,2のうち、
1台の過給機2をカッ1〜運転する場合、トータルの排
気ガス間に対し、パワータービンへバイパスされる排気
ガス最の比が増加し、過給機に供給される排気ガス量が
相対的に減少してしまう。そのため、トータルの排気ガ
スaに対してバイパスする排気ガス岳を前記の如り10
〜20%とするのが最良であるとするとき、従来方式で
は過給機カット運転時にバイパス比率が大きくなって上
記の10〜20%に保持できず、過給機1への排気ガス
足が減少して出力が得られず、ディーゼル機関3の性能
を悪化さけるおそれがめった。
[Problems to be Solved by the Invention] However, in the conventional diesel engine with a power turbine described above, since the exhaust gas inlet casing of the power turbine 4 has a first structure, the two superchargers 1 and 2 home,
When one turbocharger 2 is operated from 1 to 1, the ratio of the exhaust gas bypassed to the power turbine to the total exhaust gas increases, and the amount of exhaust gas supplied to the turbocharger becomes relative. will decrease. Therefore, the amount of exhaust gas to be bypassed for the total exhaust gas a is set to 10 as described above.
When it is assumed that the best value is ~20%, in the conventional method, the bypass ratio increases during turbocharger cut operation and cannot be maintained at the above 10 to 20%, resulting in the exhaust gas flow to the turbocharger 1. There is a danger that the performance of the diesel engine 3 will be deteriorated due to the decrease in output and the output cannot be obtained.

そこで、本発明は、2台以上の過給機を装着したパワー
タービン付ディーゼル機関で過給機のカット運転を行う
とき、ディービル機関からの排気ガスのうちバイパスさ
れる排気カスの比率を変えないようにして過給はへの排
気カス但を減少させることなくディーゼル機関の性能悪
化を未然に防止しようとするものである。
Therefore, the present invention aims to change the ratio of exhaust gas that is bypassed in the exhaust gas from the diesel engine when performing supercharger cut operation in a diesel engine with a power turbine equipped with two or more superchargers. Supercharging is an attempt to prevent deterioration of diesel engine performance without reducing exhaust gas emissions.

[問題点を解決するための手段] 本発明は、上記目的を達成するために、2台以上の過給
機のうら適数台をカット運転するときに、ディーゼル機
関からの排気ガスの一部をバイパスさせてパワータービ
ンで動力として回収させる際、上記バイパスさせる排気
ガスの量をカットされる過給機の数に応じて少なくする
ように変え、バイパス比率を変化させないように運転す
る方法とする。
[Means for Solving the Problems] In order to achieve the above object, the present invention provides that when an appropriate number of superchargers of two or more turbochargers are cut-off, a portion of exhaust gas from a diesel engine is When the exhaust gas is bypassed and recovered as motive power by a power turbine, the amount of the bypassed exhaust gas is changed to be reduced according to the number of superchargers to be cut, and the operation is performed without changing the bypass ratio. .

[作  用] 過給機を1台若しくは適数台カットして過給機の運転台
数を減少してディーゼル機関を運転するときは、パワー
タービンへ送られるバイパス排気ガス量を少なくすると
、バイパス比率はすべての過給機が運転するときの適正
なバイパス比率若しくはこれに近いものとすることがで
き、運転中の過給機から充分な出力が得られ、ディーゼ
ル機関の性能を悪化させることはなくなる。
[Function] When operating a diesel engine by cutting one or a suitable number of superchargers to reduce the number of superchargers in operation, reducing the amount of bypass exhaust gas sent to the power turbine will reduce the bypass ratio. can be set at or close to the appropriate bypass ratio when all superchargers are in operation, and sufficient output can be obtained from the operating supercharger without degrading the performance of the diesel engine. .

[実 施 例] 以下、本発明の実施例を図面を参照して説明する。[Example] Embodiments of the present invention will be described below with reference to the drawings.

第1図は本発明の実施例を示すもので、−例として2台
の過給機1,2を装着したパワータービン付ディービル
機関を示している。
FIG. 1 shows an embodiment of the present invention, and shows, as an example, a diesel engine with a power turbine equipped with two superchargers 1 and 2.

2台の過給機1と2とディーゼル機関3とを、ディービ
ル機関3から排出される排気ガスを各タービンTに導き
、且つ各コンプレッサCから吐出された空気がディーゼ
ル機関3に送入されるように接続し、更に、上記ディー
ゼル機関3から過給機1,2へ導かれる排気ガスの一部
をバイパスさせるバイパスライン6を設け、該バイパス
ライン6にパワータービン4を組み込んでなる構成にお
いて、上記パワータービン4のガス入口ケーシングを、
たとえば、第2図の如き構成とする。すなわち、パワー
タービン4のガス入ロケーシングアに、過給機1,2の
数に対応させて所要の断面積をもつガス人口8と9を設
けると共に、ケーシング7の内部も仕切壁10にて2つ
に分割し、各ガス人口8,9から入ったガスが独白にケ
ーシング7内を通ってタービンn車(図示せず)を回転
させるようにする。上記の如き構成としたパワータービ
ン4のガス入ロケーシングアにおける各ガス人口8,9
を、各々排気ガスのバイパス管11.12を介して排気
ガス管13に接続し、各バイパス管11.12の途中に
バルブ14と15を設置し、過給機のカット運転時にバ
ルブ14と15を適宜開閉して排気ガスのバイパス量を
変化させられるようにし、一方のバルブ14又は15を
閉じると、半分の排気ガスしかパワータービン4に作用
しないようにする。
The two superchargers 1 and 2 and the diesel engine 3 are arranged so that the exhaust gas discharged from the diesel engine 3 is guided to each turbine T, and the air discharged from each compressor C is sent to the diesel engine 3. A bypass line 6 is provided for bypassing part of the exhaust gas led from the diesel engine 3 to the superchargers 1 and 2, and a power turbine 4 is installed in the bypass line 6. , the gas inlet casing of the power turbine 4,
For example, the configuration is as shown in FIG. That is, gas ports 8 and 9 having a required cross-sectional area are provided in the gas-filled casing of the power turbine 4 in correspondence with the number of superchargers 1 and 2, and two gas ports 8 and 9 are provided inside the casing 7 with a partition wall 10. The gas entering from each gas population 8 and 9 passes through the casing 7 and rotates a turbine wheel (not shown). Each gas population 8, 9 in the gas-filled location casing of the power turbine 4 configured as described above
are connected to the exhaust gas pipe 13 via exhaust gas bypass pipes 11.12, respectively, and valves 14 and 15 are installed in the middle of each bypass pipe 11.12. The exhaust gas bypass amount can be changed by appropriately opening and closing the valves, and when one valve 14 or 15 is closed, only half of the exhaust gas acts on the power turbine 4.

本発明の運転方法を、上述の如き構成をもつパワーター
ビン付ディーゼル機関で実施する場合には、次のように
して行う。先ず、2台の過給機1,2をともに運転し、
且つ排気ガスのエネルギーをパワータービン4で動力と
して回収しようとするときは、バルブ14.15をとも
に開く。
When the operating method of the present invention is implemented in a diesel engine with a power turbine having the above-described configuration, it is carried out as follows. First, operate the two superchargers 1 and 2 together,
Further, when the energy of the exhaust gas is to be recovered as motive power by the power turbine 4, the valves 14 and 15 are both opened.

2台の過給機1.2で圧縮された空気はディーゼル機関
3へ送られ、該ディーゼル機関3からの排気ガスの一部
はバイパスされるが、バイパス量はバイパス比が適正と
なるようにガス入口8゜9で規制されているので、所定
母がパワータービン4に送られる。パワータービン4で
は、排気ガスによりタービン翼車を回転させる運動に変
えられ、動力と−して回収される。
The air compressed by the two superchargers 1.2 is sent to the diesel engine 3, and part of the exhaust gas from the diesel engine 3 is bypassed, but the amount of bypass is adjusted so that the bypass ratio is appropriate. Since the gas inlet is regulated at 8°9, a predetermined amount is sent to the power turbine 4. In the power turbine 4, the exhaust gas is converted into a motion that rotates a turbine wheel, and is recovered as motive power.

次に、1台の過給機2を使用しないカット運転時にパワ
ータービン4を使用するときは、バルブ14.15のい
ずれか一方、たとえば、バルブ15を閉にし、バルブ1
4のみ間にして運転する。
Next, when using the power turbine 4 during a cut operation in which one supercharger 2 is not used, either one of the valves 14 or 15, for example, the valve 15, is closed, and the valve 1 is closed.
Drive with only 4 in between.

これにより過給機カット運転時のバイパス量を半分に変
えることができて、排気ガスのバイパス比を適正に保つ
ことができ、パワータービン4の性能を維持しつつ、デ
ィーゼル機関3の性能も悪化させることがない。
As a result, the amount of bypass during supercharger cut operation can be changed to half, and the bypass ratio of exhaust gas can be maintained appropriately, and while the performance of the power turbine 4 is maintained, the performance of the diesel engine 3 is also deteriorated. I have nothing to do.

なお、本発明の運転方法は、上記した実施例のみに限定
されるものではなく、たとえば、パワータービン4のガ
ス入ロケーシングアには2つのガス人口8,9を設けて
バイパス管11.12も2本にした場合を示したが、過
給機の装着台数に応じて上記ガス入口及びバイパス管の
数が増減することは当然であり、又、上記ガス入ロケー
シングアに複数個のガス入口を分割して設けることに代
え、可変容量型のノズルを使用し、過給機カット運転時
に該可変容量型ノズルにて排気ガスのバイパス量を調整
して運転させるようにしてもよい。
Note that the operating method of the present invention is not limited to the above-described embodiments; for example, two gas ports 8 and 9 are provided in the gas-filled casing of the power turbine 4, and the bypass pipes 11 and 12 are also provided with two gas ports 8 and 9. Although we have shown the case in this book, it is natural that the number of gas inlets and bypass pipes will increase or decrease depending on the number of turbochargers installed, and it is also possible to divide multiple gas inlets into the gas-filled casing a. Instead of providing a variable displacement nozzle, a variable displacement nozzle may be used to adjust the bypass amount of exhaust gas during supercharger cut operation.

[発明の効果] 以上述べた如く、本発明のパワータービン付ディーゼル
機関の運転方法によれば、2台以上の過給機のうち、い
ずれかの過給機をカットした運転を行うときにディービ
ル機関からの排気ガスをパワータービンを経てバイパス
させるとき、排気ガスのバイパス量を変化させて最適な
バイパス比率に保持させるようにするので、パワーター
ビンの性能を良好に維持しつつ過給殿の充分なる出力が
得られてディーゼル機関の性能をも良好に維持させるこ
とができる、という優れた効果を奏し得る。
[Effects of the Invention] As described above, according to the method of operating a diesel engine with a power turbine of the present invention, when operating with one of two or more superchargers cut, the diesel engine When the exhaust gas from the building engine is bypassed through the power turbine, the bypass amount of the exhaust gas is changed to maintain the optimal bypass ratio, so the performance of the power turbine is maintained well and the supercharging An excellent effect can be achieved in that sufficient output can be obtained and the performance of the diesel engine can be maintained well.

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

第1図は本発明の運転方法を実施する一例を示す概略図
、第2図はパワータービンのガス入口ケーシングの一例
を示す斜視図、第3図は従来の例を示す概略図である。 1.2・・・過給機、3・・・ディーゼル機関、4・・
・パワータービン、7・・・ガス入口ケーシング、11
゜12・・・バイパス管。
FIG. 1 is a schematic view showing an example of implementing the operating method of the present invention, FIG. 2 is a perspective view showing an example of a gas inlet casing of a power turbine, and FIG. 3 is a schematic view showing a conventional example. 1.2...Supercharger, 3...Diesel engine, 4...
- Power turbine, 7... Gas inlet casing, 11
゜12...Bypass pipe.

Claims (1)

【特許請求の範囲】[Claims] 1)2台以上の過給機を装着したパワータービン付ディ
ーゼル機関で適数の過給機をカット運転するときにディ
ーゼル機関からの排気ガスの一部をバイパスさせてパワ
ータービンで動力として回収させる際、上記バイパスさ
せる排気ガスの量をカットされる過給機の数に応じて少
なくするよう変え、バイパス比率を変化させないように
運転することを特徴とするパワータービン付ディーゼル
機関の運転方法。
1) In a diesel engine equipped with a power turbine equipped with two or more superchargers, when an appropriate number of superchargers are cut-off, a portion of the exhaust gas from the diesel engine is bypassed and recovered as power by the power turbine. A method of operating a diesel engine with a power turbine, characterized in that the amount of exhaust gas to be bypassed is reduced in accordance with the number of superchargers to be cut, and the operation is performed without changing the bypass ratio.
JP62011379A 1987-01-22 1987-01-22 How to operate a diesel engine with a power turbine Pending JPS63183225A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP62011379A JPS63183225A (en) 1987-01-22 1987-01-22 How to operate a diesel engine with a power turbine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP62011379A JPS63183225A (en) 1987-01-22 1987-01-22 How to operate a diesel engine with a power turbine

Publications (1)

Publication Number Publication Date
JPS63183225A true JPS63183225A (en) 1988-07-28

Family

ID=11776377

Family Applications (1)

Application Number Title Priority Date Filing Date
JP62011379A Pending JPS63183225A (en) 1987-01-22 1987-01-22 How to operate a diesel engine with a power turbine

Country Status (1)

Country Link
JP (1) JPS63183225A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2011049183A1 (en) * 2009-10-23 2011-04-28 三菱重工業株式会社 Turbo compound system and method for operating same
US20130055711A1 (en) * 2011-09-07 2013-03-07 Douglas C. Hofer Method and system for a turbocharged engine
CN103590891A (en) * 2009-06-25 2014-02-19 三菱重工业株式会社 Engine exhaust energy recovery device
CN104314649A (en) * 2014-09-30 2015-01-28 东风商用车有限公司 Waste gas bypass power turbine system

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103590891A (en) * 2009-06-25 2014-02-19 三菱重工业株式会社 Engine exhaust energy recovery device
WO2011049183A1 (en) * 2009-10-23 2011-04-28 三菱重工業株式会社 Turbo compound system and method for operating same
JP2011089488A (en) * 2009-10-23 2011-05-06 Mitsubishi Heavy Ind Ltd Turbo compound system and operating method thereof
US20130055711A1 (en) * 2011-09-07 2013-03-07 Douglas C. Hofer Method and system for a turbocharged engine
US8813494B2 (en) * 2011-09-07 2014-08-26 General Electric Company Method and system for a turbocharged engine
CN104314649A (en) * 2014-09-30 2015-01-28 东风商用车有限公司 Waste gas bypass power turbine system

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