JPS6022032A - Control apparatus for power generating means utilizing supercharged diesel engine - Google Patents

Control apparatus for power generating means utilizing supercharged diesel engine

Info

Publication number
JPS6022032A
JPS6022032A JP58130263A JP13026383A JPS6022032A JP S6022032 A JPS6022032 A JP S6022032A JP 58130263 A JP58130263 A JP 58130263A JP 13026383 A JP13026383 A JP 13026383A JP S6022032 A JPS6022032 A JP S6022032A
Authority
JP
Japan
Prior art keywords
fuel
diesel engine
supply rate
turbine nozzle
generator
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
JP58130263A
Other languages
Japanese (ja)
Inventor
Yuichi Nakamura
祐一 中村
Mikio Tanaka
幹夫 田中
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.)
Mitsubishi Heavy Industries Ltd
Original Assignee
Mitsubishi 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 Mitsubishi Heavy Industries Ltd filed Critical Mitsubishi Heavy Industries Ltd
Priority to JP58130263A priority Critical patent/JPS6022032A/en
Publication of JPS6022032A publication Critical patent/JPS6022032A/en
Pending legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02DCONTROLLING COMBUSTION ENGINES
    • F02D23/00Controlling engines characterised by their being supercharged
    • F02D23/02Controlling engines characterised by their being supercharged the engines being of fuel-injection type
    • 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
    • F02B37/24Control of the pumps by using pumps or turbines with adjustable guide vanes
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02DCONTROLLING COMBUSTION ENGINES
    • F02D29/00Controlling engines, such controlling being peculiar to the devices driven thereby, the devices being other than parts or accessories essential to engine operation, e.g. controlling of engines by signals external thereto
    • F02D29/06Controlling engines, such controlling being peculiar to the devices driven thereby, the devices being other than parts or accessories essential to engine operation, e.g. controlling of engines by signals external thereto peculiar to engines driving electric generators
    • 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)
  • Output Control And Ontrol Of Special Type Engine (AREA)
  • Control Of Vehicle Engines Or Engines For Specific Uses (AREA)
  • Electrical Control Of Air Or Fuel Supplied To Internal-Combustion Engine (AREA)

Abstract

PURPOSE:To improve characteristics of transient response to the rapid load change, by controlling increasing and decreasing of the fuel supply rate as well as a turbine nozzle of an exhaust turbocharger through detection of the load change. CONSTITUTION:An adjustable turbine nozzle 7 is provided in an exhaust turbine of an exhasut turbocharger which is attached to a highly supercharged diesel engine 1, and the nozzle 7 is controlled by a turbine nozzle controlling servo- unit 16. That is, the load change of a generator 2 is detected by a current transformer 11 and the output signal of the current transformer 11 is furnished to an arithmetic comparison circuit 12, in which the engine speed detected by an engine-speed detecting means 19 is compared with a deviation value, a differential value, a integral value, etc. to the initial set value. From the result of the above comparison, the required fuel supply rate and the required air supply rate are calculated by a circuit 13 for calculating the fuel supply rate and the air supply rate, and the servo-unit 16 as well as a fuel servo-unit 17 are controlled according to the result of the above calculation.

Description

【発明の詳細な説明】 つて発電機を駆動する過給ディー.ゼル発電装置の制御
装置に関する。
[Detailed Description of the Invention] A supercharging dee that drives a generator. The present invention relates to a control device for a ZEL power generator.

ディーゼル発電装置において、負荷変動による過渡時の
速度変動率を所定の値内に納めるため、従来は負荷変動
によって機関の回転速度が変動した事を、ガバナにより
機械的、電気的に検出してから、機関の燃料増減を行う
方法や、機関回転速度が変動する前に発電機側に取付け
たカレントトランスによって負荷の変動を検出して燃料
増減を行う方法などが取られており、後者の方が瞬時変
動率(は改善される。
In diesel power generators, in order to keep the speed fluctuation rate during transients due to load fluctuations within a predetermined value, conventionally, changes in engine speed due to load fluctuations are detected mechanically and electrically by a governor, and then , there are methods to increase or decrease the fuel in the engine, or methods to increase or decrease the fuel by detecting changes in load using a current transformer installed on the generator side before the engine rotational speed fluctuates.The latter method is better. Instantaneous fluctuation rate (will be improved.

しかしながら、排気ターボ過給機を有する高過給ディー
ゼル機関においては、負荷の急増に対しては、前述の燃
料増減コントロールの応召性をいくら改善しても、排気
ターボ過給機の過渡応答特性が改善されていないので、
負荷急増時に機関に投入される大量の燃料を十分燃焼さ
せるだめの空気の供給が間に合わず、十分な出力が得ら
れない。
However, in a highly supercharged diesel engine with an exhaust turbo supercharger, no matter how much the responsiveness of the fuel increase/decrease control described above is improved, the transient response characteristics of the exhaust turbo supercharger will be affected in response to a sudden increase in load. Since it has not been improved,
When the load suddenly increases, sufficient air cannot be supplied in time to burn the large amount of fuel injected into the engine, making it impossible to obtain sufficient output.

このことが速度変動率の改善の支障となっていた。This has been an obstacle to improving the speed fluctuation rate.

本発明は上記のような事情にもとづきなされたもので、
その目的は、負荷変動を検出して、燃料の供給量の増減
を制御するとともに排気ターボ過給機のタービンノズル
をも制御することにより、過給機の過渡応答性を向上さ
せるととKある。
The present invention was made based on the above circumstances, and
The purpose is to improve the transient response of the supercharger by detecting load fluctuations, controlling increases and decreases in the amount of fuel supplied, and also controlling the turbine nozzle of the exhaust turbocharger. .

以下本発明の一実施例について図面を参照して詳細に説
明する。
An embodiment of the present invention will be described in detail below with reference to the drawings.

8i′!1図は本発明に係る過給ディーゼル発電装置の
制御装置の一実施例を示す系統図である。
8i′! FIG. 1 is a system diagram showing an embodiment of a control device for a supercharged diesel power generator according to the present invention.

先ず、過給ディーゼル発電装置について説明すると、1
は高過給ディーゼル機関であり、2はこの機関1に連結
された発電機である。高過給ディーゼル機関1への燃料
供給は、燃料噴射ポンプ3により、燃料噴射弁4を介し
て、シリンダ5へ投入されるようになっている。シリン
ダ5内で燃I焼して生じた排気ガスは、排気管6に集め
られ、排気ターボ過給機の可変タービンノズル7へ供給
すれ、ここでタービンホイール8を駆動する。タービン
ホイール8にはコンプレッサ9が直結されているので、
タービンホイール8の回転によってコンプレッサ9が回
転されて空気を圧縮する。そして、コンプレッサ9で出
棺された空気は、給気管10を通して高過給ディーゼル
機関】のシリンダ5へ過給される。
First, to explain the supercharged diesel generator, 1.
is a highly supercharged diesel engine, and 2 is a generator connected to this engine 1. Fuel is supplied to the highly supercharged diesel engine 1 by a fuel injection pump 3 through a fuel injection valve 4 and into a cylinder 5 . Exhaust gas produced by combustion in the cylinder 5 is collected in an exhaust pipe 6 and supplied to a variable turbine nozzle 7 of an exhaust turbo supercharger, where it drives a turbine wheel 8. Since the compressor 9 is directly connected to the turbine wheel 8,
The rotation of the turbine wheel 8 causes the compressor 9 to rotate and compress the air. The air discharged by the compressor 9 is supercharged through the air supply pipe 10 to the cylinder 5 of the highly supercharged diesel engine.

次に、制御装置について説明する。高過給ディーゼル機
関1にはその回転数を検出するだめの回転検出器1aが
設けられている。また発電機2にはカレントトランス1
1が設けられていて、これにより負荷変動が検出される
。12はカレントトランス として、これらを予め設定されている回転数、定格出力
等に対する偏差値、微分値、積分値等と比較する比較演
算回路である。13は比較演算1旬1路12の出力にも
とづき、高過給ディーセル機関−・供給すべき燃料、空
気の量を計算する燃Fl及び空気量演算回路である。
Next, the control device will be explained. The highly supercharged diesel engine 1 is provided with a rotation detector 1a for detecting its rotation speed. In addition, the generator 2 has a current transformer 1
1 is provided to detect load fluctuations. Reference numeral 12 represents a current transformer, and a comparison calculation circuit that compares the current transformer with deviation values, differential values, integral values, etc. with respect to preset rotational speed, rated output, etc. Reference numeral 13 denotes a fuel Fl and air amount calculation circuit which calculates the amount of fuel and air to be supplied to the highly supercharged diesel engine based on the output of the comparison calculation 1st path 12.

燃料及び空気量演算回路13からの空気量信号はタービ
ンノズル制御回路14へ、寸だ燃料供給信号は燃料制御
回路15へ夫々分離して供給される。そして、タービン
ノズル制御回路14からは、空気量信号にもとづく信号
をタービンノズル調整サーボユニット16へ供給してサ
ーボユニットヲ駆動し、その制御量に応じて可変タービ
ンノズル7のノズルイ積を制御する。一方、燃料制御回
路15からは、燃料供給信号にもとづ<(8号を燃料サ
ーボユニット17へ供給してサーボユニットを、駆動し
、その制御量に応じて燃料ラック18を移動させること
により、燃料ポンプ3からの燃料の噴射量を制御する。
The air amount signal from the fuel and air amount calculating circuit 13 is separately supplied to the turbine nozzle control circuit 14, and the instant fuel supply signal is separately supplied to the fuel control circuit 15. Then, the turbine nozzle control circuit 14 supplies a signal based on the air amount signal to the turbine nozzle adjustment servo unit 16 to drive the servo unit, and controls the nozzle product of the variable turbine nozzle 7 according to the control amount. On the other hand, the fuel control circuit 15 supplies fuel to the fuel servo unit 17 based on the fuel supply signal to drive the servo unit, and moves the fuel rack 18 according to the controlled amount. , controls the amount of fuel injected from the fuel pump 3.

次に本発明装置の作用を説明する。Next, the operation of the device of the present invention will be explained.

本発明で(1′:l:、タービンノズルを可変翼(゛1
訂造のような可変タービンノズル7とし、これをタービ
ンノズル制御回路J4及びタービンノズル調整サーボユ
ニット16によって制御するようにしたので、無負荷状
態においてもタービンロータffi高速回転させること
ができる。すなわち、無負荷時でも、タービンノズル制
御回路14及びタービンノズル調整サーボユニット16
によって可変タービンノズル7のノズル面積を絞って、
ノズルにおける排気ガス流速を上昇させ、タービンロー
タの回転速度を定格時の70%程度に維持しておく。
In the present invention (1':l:, the turbine nozzle is
Since the variable turbine nozzle 7 is of a modified type and is controlled by the turbine nozzle control circuit J4 and the turbine nozzle adjustment servo unit 16, the turbine rotor ffi can be rotated at high speed even in a no-load state. That is, even when there is no load, the turbine nozzle control circuit 14 and the turbine nozzle adjustment servo unit 16
By narrowing down the nozzle area of the variable turbine nozzle 7,
The exhaust gas flow velocity in the nozzle is increased to maintain the rotational speed of the turbine rotor at approximately 70% of the rated speed.

そこで、仮に発電機2の負荷が急増したとすると、負荷
の変化はカレントトランス11によって即座に検出され
て、比較演算回路12へ入力される。比較演算回路12
には回転検出器19に」:って検出されたディーゼル機
関1の回転数も入力されており、これらと初期設定値に
対する偏差値、微分値、積分値等が比較され、その結果
にもとづき燃料及び空気量演訊1回路13にて所要の燃
料供給量、空気量が計算される。そして、燃料制御回路
15及び燃料サーボユニット17によって、燃1i」ラ
ック18f:燃料増加方向へ移動させ、シリンダ5内へ
噴射させる燃料を増大さぜる。一方、燃焼に必要となる
空気は、タービンホイール8によって駆動されるコンプ
レッサ9によってシリンダ5へ送り込まれるが、無負荷
時にすでに定格時の70%程度の回転数に維持されてい
るため、klめて媛時間に所望の回転数へ上昇し、供給
空気量を増加させることができる。従って、燃料の増加
に合せて空気骨も増加させることができるのて、出力応
答遅れが極めて矧縮され、その結果速度変動+41;が
題名に改善される。
Therefore, if the load on the generator 2 suddenly increases, the change in load is immediately detected by the current transformer 11 and input to the comparison calculation circuit 12. Comparison calculation circuit 12
The rotation speed of the diesel engine 1 detected by the rotation detector 19 is also input, and these are compared with the deviation value, differential value, integral value, etc. with respect to the initial setting value, and based on the results, the fuel The required fuel supply amount and air amount are calculated in the air amount calculation circuit 13. Then, the fuel control circuit 15 and the fuel servo unit 17 move the fuel rack 18f in the fuel increasing direction to increase the amount of fuel injected into the cylinder 5. On the other hand, the air required for combustion is sent into the cylinder 5 by a compressor 9 driven by a turbine wheel 8, but since the rotation speed is already maintained at about 70% of the rated speed when no load is applied, It is possible to increase the rotation speed to a desired speed and increase the amount of air supplied. Therefore, since the air mass can be increased in accordance with the increase in fuel, the output response delay is extremely reduced, and as a result, the speed fluctuation is improved by +41.

第2図及び第3図は、従来の過給ディーゼル発電装置(
第2図)と、本発明による?tilJ御装置を備えた過
給ディーゼル発電装置(第3図)との運転状態を夫々比
較して示した特性図であり、aは負荷変動、1〕は過給
機回転数及びタービンノズル面積、Cは燃料供給量、d
はディーゼル機関の回転数を夫々時間に対して示したも
のである。これらの図から、負荷の変動に対し、本発明
によれば過給機の加速時間が半減し、それに伴なって機
関回転数の変動が大幅に改善されることが明らかである
Figures 2 and 3 show a conventional supercharged diesel generator (
Figure 2) and according to the present invention? It is a characteristic diagram showing a comparison of the operating conditions with a supercharged diesel generator equipped with a tilJ control device (Fig. 3), where a is load fluctuation, 1] is supercharger rotation speed and turbine nozzle area, C is the fuel supply amount, d
are the rotational speeds of the diesel engine versus time. From these figures, it is clear that according to the present invention, the acceleration time of the supercharger is halved in response to load fluctuations, and accordingly, fluctuations in engine speed are significantly improved.

なお本発明の制御装置では次のような制御も可能である
Note that the control device of the present invention also allows the following control.

(1) 運転時の排気ターボ過給機の最低回転数は、同
発電装置運転時のターボの最高回転数の約70%以上に
なるようにターボの可変ノズル開度を制御して、無負荷
、低負荷から急激な負荷投入しても機関出力が短時間で
追縦するように出来る。
(1) The variable nozzle opening of the turbo is controlled so that the minimum rotation speed of the exhaust turbo supercharger during operation is approximately 70% or more of the maximum rotation speed of the turbo during operation of the generator, and the Even if the load is suddenly turned on from a low load, the engine output can be made to catch up in a short time.

(2) 発電機の負荷パターンが予め一足に決められて
いる場合は発電機負荷制御シグナルジェネレータと機関
側制御プロクラムを同期させる琳によって自動的に燃料
噴射と排気ターボ過給イアにの可変ノズルの制御劣性い
機関出力応答遅れを短縮できる。
(2) If the generator load pattern is predetermined, Rin, which synchronizes the generator load control signal generator and the engine control program, automatically controls the fuel injection and the variable nozzle on the exhaust turbo supercharging ear. Engine output response delay, which is inferior to control, can be reduced.

超 以上詳述したように本説明によれば、急速負荷変動に対
する過渡応答特性が大幅に改善される。
As described in detail above, according to the present description, the transient response characteristics to rapid load fluctuations are significantly improved.

そのだめ発電装置として必要な特性である714度変動
率が顕著に改善される。
As a result, the 714 degree fluctuation rate, which is a necessary characteristic for a power generation device, is significantly improved.

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

第1図は本発明に係る過給ディーゼル発電装置の制御装
置の一実施例を示す系統図、第2図U従来の過給ティー
セル発電装置の運転状態を示す特性図、第3図は本発明
により制御された過給ティーセル発電装置の運転状態を
示す特性図である。 1・・高過給ディーゼル(幾関、2・・発電’IV’;
 13−・燃料噴射ポンプ、7・Il′ili′J変タ
ービンノスル、9・・コンプレッサ、1III11カレ
ントトランス、]2・・比較演算回路、】3・・燃判及
草気量演算回路、14・・タービンノズル制御回路、1
5・・燃料制御回路、16・・タービンノズルWJ J
l サーボユニット、17・・燃料サーボユニット、1
8・・燃料ラック、19・・回転検出器第1図 −糠央 馳回≦ml
Fig. 1 is a system diagram showing an embodiment of a control device for a supercharged diesel power generation device according to the present invention, Fig. 2 is a characteristic diagram showing the operating state of a conventional supercharged tea cell power generation device, and Fig. 3 is a diagram showing an embodiment of a control device for a supercharged diesel power generation device according to the present invention. It is a characteristic diagram showing the operating state of the supercharged tea cell power generation device controlled by. 1. Highly supercharged diesel (Ikuseki, 2. Power generation 'IV';
13-・Fuel injection pump, 7・Il′ili′J variable turbine nostle, 9・・Compressor, 1III11 current transformer, ]2・・Comparison calculation circuit, ]3・・Fuel level and air flow calculation circuit, 14・・・Turbine nozzle control circuit, 1
5... Fuel control circuit, 16... Turbine nozzle WJ J
l Servo unit, 17...Fuel servo unit, 1
8...Fuel rack, 19...Rotation detector Fig. 1 - Nukao Hase times≦ml

Claims (1)

【特許請求の範囲】[Claims] 排気ターボ過給ディーゼル機関によって発電機を駆動す
る過給ディーゼル発電装置の制御装置において、ディー
ゼル機関の回転数および発電機の負荷が入力され設定値
との偏差値を出力する比較演算装置と、この比11咬演
算装置の出力にもとづき所要の燃料及び空気の供給量を
演算する燃料及び空気量演算装置と、この装置からの燃
料信号にもとづき前記排気ターボ過給ディーゼル機関へ
の燃料供給量を制御する燃料制御装置と、前記燃料及び
空気量6it算装置からの空気量信号にもとづき前記排
気ターボ過給ディーゼル機関の可変タービンノズルを制
御することにより空気供給量を制御するタービンノズル
制御装置とを具備することを特徴とする過給ディーセル
発電装置の制御装置。
A control device for a supercharged diesel generator that drives a generator by an exhaust turbocharged diesel engine includes a comparison calculation device that inputs the rotation speed of the diesel engine and the load of the generator and outputs a deviation value from a set value; A fuel and air amount calculation device that calculates the required amount of fuel and air to be supplied based on the output of the ratio calculation device, and a fuel supply amount to the exhaust turbocharged diesel engine based on the fuel signal from this device. and a turbine nozzle control device that controls the amount of air supplied by controlling the variable turbine nozzle of the exhaust turbocharged diesel engine based on the air amount signal from the fuel and air amount 6IT calculating device. A control device for a supercharged diesel power generation device.
JP58130263A 1983-07-19 1983-07-19 Control apparatus for power generating means utilizing supercharged diesel engine Pending JPS6022032A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP58130263A JPS6022032A (en) 1983-07-19 1983-07-19 Control apparatus for power generating means utilizing supercharged diesel engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP58130263A JPS6022032A (en) 1983-07-19 1983-07-19 Control apparatus for power generating means utilizing supercharged diesel engine

Publications (1)

Publication Number Publication Date
JPS6022032A true JPS6022032A (en) 1985-02-04

Family

ID=15030088

Family Applications (1)

Application Number Title Priority Date Filing Date
JP58130263A Pending JPS6022032A (en) 1983-07-19 1983-07-19 Control apparatus for power generating means utilizing supercharged diesel engine

Country Status (1)

Country Link
JP (1) JPS6022032A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS61162554U (en) * 1985-03-29 1986-10-08
EP0870915A1 (en) * 1997-04-12 1998-10-14 Daimler-Benz Aktiengesellschaft Method to control/regulate the charged air mass flow of an internal combustion engine with an exhaust gas turbocharger comprising a variable geometry turbine
EP1106806A2 (en) * 1999-12-10 2001-06-13 Caterpillar Inc. Method and apparatus for controlling the speed of an engine
EP1830049A1 (en) * 2006-03-03 2007-09-05 Dr.Ing. h.c.F. Porsche Aktiengesellschaft Method and control unit for adjusting in a turbocharger a turbine flow cross section

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5079622A (en) * 1973-11-16 1975-06-28
JPS5550175A (en) * 1978-10-05 1980-04-11 Nec Corp Received signal processor

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5079622A (en) * 1973-11-16 1975-06-28
JPS5550175A (en) * 1978-10-05 1980-04-11 Nec Corp Received signal processor

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS61162554U (en) * 1985-03-29 1986-10-08
EP0870915A1 (en) * 1997-04-12 1998-10-14 Daimler-Benz Aktiengesellschaft Method to control/regulate the charged air mass flow of an internal combustion engine with an exhaust gas turbocharger comprising a variable geometry turbine
US6058707A (en) * 1997-04-12 2000-05-09 Daimler Chrysler Ag Method of controlling the charge air mass flows of an internal combustion engine including an exhaust gas turbocharger with adjustable turbine geometry
EP1106806A2 (en) * 1999-12-10 2001-06-13 Caterpillar Inc. Method and apparatus for controlling the speed of an engine
EP1106806A3 (en) * 1999-12-10 2002-12-11 Caterpillar Inc. Method and apparatus for controlling the speed of an engine
EP1830049A1 (en) * 2006-03-03 2007-09-05 Dr.Ing. h.c.F. Porsche Aktiengesellschaft Method and control unit for adjusting in a turbocharger a turbine flow cross section
US7954319B2 (en) 2006-03-03 2011-06-07 Dr. Ing. H.C. F. Porsche Aktiengesellschaft Method and control unit for setting a turbine flow cross-section

Similar Documents

Publication Publication Date Title
EP1801384B1 (en) Methods and systems for variable geometry turbocharger control
US6272859B1 (en) Device for controlling a variable geometry turbocharger
CN1054902C (en) Gas turbine apparatus and method of operating same
EP0136541A2 (en) System controlling variable capacity turbine of automotive turbocharger
EP1474597A1 (en) Control method for variable geometry turbocharger and related system
US4299088A (en) Cyclic load duty control for gas turbine
US4104876A (en) Fan R. P. M. control loop stabilization using high rotor speed
JPH0228697B2 (en)
JPS6022032A (en) Control apparatus for power generating means utilizing supercharged diesel engine
US6314733B1 (en) Control method
US4813226A (en) Demand control of variable geometry gas turbine power plant
EP1302644B1 (en) Method for controlling an exhaust-gas turbocharger with a variable turbine geometry
KR100871763B1 (en) Method and device for controlling an internal combustion engine
JPS6244095Y2 (en)
JPS6183460A (en) Throttle valve controller for supercharged engine
JPS57328A (en) Turbosupercharge spark ignition engine
JPS627933A (en) Supercharger control device
US20220074354A1 (en) Turbogenerator method and apparatus
JP2605053B2 (en) Engine boost pressure control device
JP2600833Y2 (en) Boost compensator pressure regulator
JPH06213005A (en) Fan stall preventing device
JPS6213731A (en) Control method for supercharger with varying nozzle
JPH0515541Y2 (en)
JPS626256Y2 (en)
JPS62261638A (en) Fuel-ratio controller for internal combustion engine