JPS63277841A - Fuel injection control device for internal combustion engine - Google Patents

Fuel injection control device for internal combustion engine

Info

Publication number
JPS63277841A
JPS63277841A JP10929587A JP10929587A JPS63277841A JP S63277841 A JPS63277841 A JP S63277841A JP 10929587 A JP10929587 A JP 10929587A JP 10929587 A JP10929587 A JP 10929587A JP S63277841 A JPS63277841 A JP S63277841A
Authority
JP
Japan
Prior art keywords
injection
solenoid valve
pilot injection
pilot
nozzle
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
JP10929587A
Other languages
Japanese (ja)
Inventor
Keiichi Yamada
恵一 山田
Nobukazu Takagi
伸和 高木
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.)
Bosch Corp
Original Assignee
Diesel Kiki 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 Diesel Kiki Co Ltd filed Critical Diesel Kiki Co Ltd
Priority to JP10929587A priority Critical patent/JPS63277841A/en
Publication of JPS63277841A publication Critical patent/JPS63277841A/en
Pending legal-status Critical Current

Links

Abstract

PURPOSE:To reduce the mechanical noise by adjusting a pulse width of a driving pulse for controlling the operation of a fuel pumping solenoid valve and starting main injection before ending of pilot injection. CONSTITUTION:When an engine is in an operational condition where pilot injection should be executed, a control circuit 5 reads an output signal from a nozzle lift sensor and determines whether or not the output signal has fallen twice in one injection stroke. If NO, stop control of a solenoid valve 20 is increased by a predetermined value, and if YES, the stop control is decreased by a predetermined value. In an actual operation of the solenoid valve 20, a pilot injection time and a main injection time are continuously established under a separate condition. Accordingly, an injection nozzle 10 is seated only once in one injection stroke to thereby reduce a seating noise. Accordingly, a mechanical noise may be reduced as maintaining the effectiveness of the pilot injection.

Description

【発明の詳細な説明】 (産業上の利用分野) 本発明は内燃機関、例えばディーゼルエンジン用の燃料
噴射制御装置において主燃料噴射に先立って行われるパ
イロット噴射が可能な燃料噴射制御装置の改良に関する
ものである。
DETAILED DESCRIPTION OF THE INVENTION (Field of Industrial Application) The present invention relates to an improvement in a fuel injection control device for an internal combustion engine, such as a diesel engine, which is capable of pilot injection performed prior to main fuel injection. It is something.

(従来技術及びその問題点) −・股にディーゼルエンジンは燃料の着火遅れに起因す
る燃焼騒音が発生し、特に低速、低負荷運転状態の時に
前記燃焼騒音の発生が顕著である。
(Prior Art and its Problems) - Diesel engines generate combustion noise due to a delay in ignition of fuel, and the combustion noise is particularly noticeable when operating at low speeds and low loads.

従来パイロット噴射機能を備えた燃料噴射ポンプが、例
えば特開昭60−125754号公報にて公知である。
A conventional fuel injection pump having a pilot injection function is known, for example, from Japanese Patent Laid-Open No. 125754/1983.

この従来の燃料噴射ポンプは燃料の加圧及び噴射ノズル
への圧送が行われる高圧室と低圧室との間を開閉する燃
料溢流用の電磁弁をエンジン運転状態に応じて燃料の加
圧圧送中に駆動パルス(第5図(a))にて開閉制御す
ることにより(同1:11(b))、パイロット噴射と
主噴射とを行わせるものである(同図(C))。この場
合、噴射ノズルの各噴射時のリフト期間(A、B)はノ
ズルリフトセンサにより検知される(同図(d))。
This conventional fuel injection pump uses a solenoid valve for fuel overflow, which opens and closes between a high pressure chamber and a low pressure chamber, where fuel is pressurized and pumped to the injection nozzle, depending on the engine operating state. Pilot injection and main injection are performed (FIG. 5(C)) by controlling opening and closing using drive pulses (FIG. 5(a)) (FIG. 5(a)) (FIG. 5(c)). In this case, the lift period (A, B) during each injection of the injection nozzle is detected by the nozzle lift sensor (FIG. 4(d)).

しかしながら、」1記パイロット噴射を主噴射に先行し
て行う場合、n;1記噴射ノズルが1回の噴射行程で、
パイロット噴射時と主噴射時において、それぞれ開閉弁
動作が行われるため、当該弁体の着座時における機械騒
音が大きく、パイロット噴射による燃焼騒音の低減効果
を半減するという問題があった。
However, when performing the pilot injection in 1. prior to the main injection, the injection nozzle in 1.
Since opening and closing valve operations are performed during pilot injection and main injection, there is a problem in that mechanical noise is large when the valve body is seated, and the combustion noise reduction effect of pilot injection is halved.

(発明の目的) 本発明は上記問題点を解決するためになされたものであ
り、燃料溢流用の電磁弁により制御される燃料噴射装置
において、パイロット噴射による燃焼騒音の低減と同時
に機械騒音も低減し、更には排気ガス規制を図り得る内
燃機関用燃事゛1噴射制御装置を提供することを目的と
する。
(Object of the Invention) The present invention has been made to solve the above-mentioned problems, and is intended to reduce combustion noise due to pilot injection and at the same time reduce mechanical noise in a fuel injection device controlled by a solenoid valve for fuel overflow. Furthermore, it is an object of the present invention to provide a fuel injection control device for an internal combustion engine that is capable of regulating exhaust gas.

(発明の構成) −1,記目的を達成するために本発明によれば、燃t’
)の加)1:、圧送用の電磁弁を、機関の運転状態に応
じて開閉制御することにより、主噴射に先立ってパイロ
ット噴射を行わせるようにした燃料噴射制御装置におい
て、01i記電磁弁を開閉制御する駆動パルスのパルス
幅を調整することによりnIj記パイロット噴射の終了
前に前記主噴射を開始させるようにしたことを特徴とす
る内燃機関用燃料噴射制御装置が提供される。
(Structure of the Invention) -1. According to the present invention, in order to achieve the above objects, the fuel t'
) addition) 1: In a fuel injection control device that performs pilot injection prior to main injection by controlling opening and closing of a pressure-feeding solenoid valve according to the operating state of the engine, the solenoid valve 01i There is provided a fuel injection control device for an internal combustion engine, characterized in that the main injection is started before the end of the nIj pilot injection by adjusting the pulse width of a drive pulse that controls opening and closing of the main injection.

(実施例) 以下、本発明の実施例を図面を参照しながら説明する。(Example) Embodiments of the present invention will be described below with reference to the drawings.

第1図は本発明の装置を実施する噴射ノズル及びこれに
連結される分配型燃料噴射ポンプの要部を示す断面図で
ある。図中10は噴射ノズルであり、この噴射ノズルl
Oは、基本的には、シート而10a、1111記シート
而10aと当接可能なブr座I 01)から成り、この
噴射ノズル10のリフト期間(ノズルリフト期間)はノ
ズルリフトセンサ(図示省略)により検知される。本実
施例においては、ノズルリフトセンサは、単にシート而
10aと弁座10 bとの当接状態を検知するだけで十
分であり、従って、シート而10aと弁座10bとをス
イッチとして用いたセンサ(SOIセンサ)が適用され
、該Solセンサからのリフト信号(Sol信号)は制
御回路5に供給される。尚、Sol信号がハイレベルの
ときは噴射ノズル10の開成を、ローレベルのときは噴
射ノズルlOの閉成(竹片状@)を夫々表わす。
FIG. 1 is a cross-sectional view showing the main parts of an injection nozzle and a distribution type fuel injection pump connected thereto, implementing the apparatus of the present invention. 10 in the figure is an injection nozzle, and this injection nozzle l
O basically consists of a seat I01) which can come into contact with the seat 10a, 1111 and the seat 10a, and during the lift period of the injection nozzle 10 (nozzle lift period), a nozzle lift sensor (not shown) is used. ) is detected. In this embodiment, it is sufficient for the nozzle lift sensor to simply detect the contact state between the seat 10a and the valve seat 10b, and therefore the nozzle lift sensor uses the seat 10a and the valve seat 10b as a switch. (SOI sensor) is applied, and a lift signal (Sol signal) from the Sol sensor is supplied to the control circuit 5. Note that when the Sol signal is at a high level, it indicates that the injection nozzle 10 is opened, and when it is at a low level, it indicates that the injection nozzle IO is closed (bamboo-shaped @).

1);j記燃料溢流用の電磁弁20は具体的には前記戻
り通路21が穿設されたバルブハウジング22と、コイ
ル23が巻回された鉄心24とを備えている。
1);J The electromagnetic valve 20 for fuel overflow specifically includes a valve housing 22 in which the return passage 21 is bored, and an iron core 24 around which a coil 23 is wound.

気筒数と同数の燃料分配通路7,8は、プランジャ6が
嵌装されるプランジャバレル4及びブロック:3に夫々
設けられており、更に通路8の出[1はパイプ9a、9
bを介して各気筒毎に配されている前記噴射ノズル10
に接続されている。
The same number of fuel distribution passages 7 and 8 as the number of cylinders are provided in the plunger barrel 4 and the block 3 in which the plunger 6 is fitted, respectively, and the outlet of the passage 8 [1 is the pipe 9a, 9
The injection nozzle 10 is arranged for each cylinder via b.
It is connected to the.

尚、同図中1はポンプハウジングで、該ポンプハウジン
グ1には機関(図示省略)の出力軸に連結される駆動軸
(図示省略)によって駆動されるフィードポンプ(図示
省略)が装着されている。
In the figure, 1 is a pump housing, and a feed pump (not shown) is mounted on the pump housing 1, which is driven by a drive shaft (not shown) connected to the output shaft of an engine (not shown). .

前記制御回路5は、中央演算処理装置(CPU)、後述
する噴射制御プログラム等が予め記憶されているリード
オンリメモリ(ROM)及びランダムアクセスメモリ(
r<ΔM)等から構成され、該制御回路5にはエンジン
回転数を表わす回転数信号、クランク軸基準位置信号、
アクセル開度信号、吸気圧信け、吸気温信号及びエンジ
ン冷却水温信号が夫々人力される。制御回路5はこれら
各入力信号に基づきり;ノ記燃料溢流用の電磁弁20に
制御信号(駆動パルス信号)を出力することにより噴射
T11、噴射時間その他の制御が行われる。
The control circuit 5 includes a central processing unit (CPU), a read-only memory (ROM) and a random access memory (ROM) in which an injection control program, which will be described later, is stored in advance.
r<ΔM), etc., and the control circuit 5 includes a rotational speed signal representing the engine rotational speed, a crankshaft reference position signal,
The accelerator opening signal, intake pressure signal, intake temperature signal, and engine coolant temperature signal are each manually input. Based on these input signals, the control circuit 5 outputs a control signal (drive pulse signal) to the electromagnetic valve 20 for fuel overflow to control the injection T11, injection time, and other matters.

次に本発明に係る燃料溢流用の電磁弁20の開閉制御に
よる噴射制御を第2図のプログラムフローチャートに従
って説明する。
Next, injection control by opening/closing control of the electromagnetic valve 20 for fuel overflow according to the present invention will be explained according to the program flowchart shown in FIG.

先ず、イグニッションスイッチ(図示省略)がオンにな
って電源が投下されると、ステップlにおいて制御回路
の初期化が行われ、続くステップ2でエンジン運転状態
を表す前記各種センサがらの夫々の運転パラメータ信号
の読込みが行われる。
First, when the ignition switch (not shown) is turned on and the power is turned on, the control circuit is initialized in step 1, and in step 2, the operating parameters of the various sensors representing the engine operating state are determined. Signals are read.

この運転パラメータ信号の読込みが終了すると、続くス
テップ3でエンジンがパイロット噴射をすべき運転状態
(例えばアイドル運転状@)にあるか否かの判別を前記
読込んだ運転パラメータ信号(回転数信号、アクセル開
度信号、水温信号)に基づいて行なう。このステップ3
の判別結果が否定(No)のときは、ステップ4に進ん
で通常の噴射制御による燃t1噴射、即ち、エンジン運
転状1厳に応じた所要喰の燃料量を主噴射のみにより一
時に1ノ(給する公知の手法による燃料噴射が実行され
る。
When the reading of this operating parameter signal is completed, in the following step 3, it is determined whether or not the engine is in an operating state in which pilot injection should be performed (for example, idling operating state @). This is done based on the accelerator opening signal and water temperature signal). This step 3
If the determination result is negative (No), proceed to step 4 and inject fuel t1 under normal injection control, that is, inject the required amount of fuel according to the engine operating condition 1 at a time by main injection only. (Fuel injection is performed using a known method.

一方、前記ステップ3の判別結果が肯定(Yes)のと
き、即ち、エンジンがパイロット噴射を実行すべき運転
状態にあるときは、当該パイロット噴射の実行に伴う噴
射ノズルIOの着座時の機械騒音を低減すべく、以下の
制御(ステップ5乃至ステップ9の制御)が実行される
On the other hand, when the determination result in step 3 is affirmative (Yes), that is, when the engine is in an operating state in which pilot injection should be performed, the mechanical noise when the injection nozzle IO is seated due to the execution of the pilot injection is reduced. In order to reduce this, the following control (control in steps 5 to 9) is executed.

先ず、ステップ5においては、前記運転パラメータに基
づいて1);i記制御弁20の駆動パルス(目C:′!
駆動パルス、第3図(a))の波形、即ちパイロット噴
射制御の開始時点から終了時点までの制御期間(ローレ
ベル期間)Δ叶、パイロット噴射制御と主噴射制御との
間の休止制御期間(ハイレベル期間) i”DPMが決
定され、これらの値に基づいて更に主噴射制御期間AD
Hが決定される。
First, in step 5, based on the operating parameters, 1); drive pulse (item C:'!) of control valve 20 is determined;
The drive pulse, the waveform of Fig. 3 (a), that is, the control period (low level period) from the start point to the end point of pilot injection control, Δ, the rest control period (between pilot injection control and main injection control) High level period) i” DPM is determined, and based on these values, the main injection control period AD is further determined.
H is determined.

ステップ6では、ノズルリフトセンサの出力値t;(S
ol信号)の状態を読込み、次のステップ7で+”+”
+i記読込んだSol信号が1回の噴射行程で2度\′
l下がったか否か、即ち噴射ノズル10が実際にパイロ
ット噴射を開始する時点(Sol信号の最初の立]ユリ
)から主噴射を終了する時点(SO1信はの最後の立下
り)までのΔi期間中にS01信シ)がローレベルにな
ったか否かを判別する。
In step 6, the nozzle lift sensor output value t;(S
ol signal), and in the next step 7, +”+”
+ i The read Sol signal is 2 times\' in one injection stroke
Δi period from the time when the injection nozzle 10 actually starts pilot injection (the first rising of the Sol signal) to the time when the main injection ends (the last falling of the SO1 signal) During this time, it is determined whether or not the S01 signal (S01 signal) has become low level.

この、ステップ7の判別結果が否定(No)、即ち噴射
ノズルの着座が1回の噴射行程で1度しか生じなかった
ときには、ステップ9に進んで体11−制御1’orM
を所定値だけ増加させて、その後ステップ2に戻る。
If the determination result in step 7 is negative (No), that is, the injection nozzle is seated only once in one injection stroke, the process proceeds to step 9, and the body 11-control 1'orM
is increased by a predetermined value, and then the process returns to step 2.

一方、このステップ7の判別結果が肯定(Yes)のと
きは、即ち噴射ノズルが1回の噴射行程で2度着座した
と判断したときには次のステップ8に進み、前記制御期
間1”llPMを所定値だけ減少させ、その後ステップ
2に戻る。
On the other hand, when the determination result in step 7 is affirmative (Yes), that is, when it is determined that the injection nozzle has been seated twice in one injection stroke, the process proceeds to the next step 8, and the control period 1''llPM is set to a predetermined value. Decrement by the value and then return to step 2.

以l−の如く決定された駆動パルス(目標駆動パルス)
に基づいた電磁弁20の実際の作動においては(第:3
1り1(1))) 、基本的には電磁弁20が閉成され
たときにのみ1)η述のプランジャ6による燃料の加1
1ミが可能であるが、電磁弁20を閉成させるための駆
動パルス中に於て所定期間”I’DPMだけ電磁弁20
を開成させるように制御することによって一時的に燃料
の加圧が低減し、パイロット噴射期間Δ′と主噴射期間
B′とが分離された状態で連続的に行なわれる(第3図
(c))、尚、この時SO[信号は第3図(d)に示さ
れるように変化し、1度の噴射行程において噴射ノズル
は1度の着座を行なうに過ぎず着座音が低減する。
Drive pulse (target drive pulse) determined as follows:
In the actual operation of the solenoid valve 20 based on (No. 3)
1(1))) Basically, the addition of fuel by the plunger 6 described in η is performed only when the solenoid valve 20 is closed.
However, during the drive pulse for closing the solenoid valve 20, the solenoid valve 20 is
By controlling the valve to open, the pressurization of the fuel is temporarily reduced, and the pilot injection period Δ' and the main injection period B' are performed continuously in a separated state (Fig. 3(c)). ), at this time, the SO signal changes as shown in FIG. 3(d), and the injection nozzle is only seated once in one injection stroke, and the seating noise is reduced.

従って、本実施例のパイロット噴射制御装置によれば、
通常噴射に対しては従来のようなパイロット噴射特有の
燃焼騒音の低減が図られる一方機械騒音も低減され、更
に従前と同様な排気ガス規;I11を有効になし得る。
Therefore, according to the pilot injection control device of this embodiment,
For normal injection, combustion noise peculiar to pilot injection as in the prior art is reduced, while mechanical noise is also reduced, and the same exhaust gas regulation I11 as before can be effectively met.

ここで第4図は本実施例によるエンジン騒音の低減効果
を示すものであり、パイロット噴射を行なわない通常噴
射の場合(符号P)、従来のパイロット噴射を行なう場
合(符号R)の2つの場合に比べ本実施例の場合(符号
Q)は最も騒音レベ ・ルが低いことがわかる。
Here, FIG. 4 shows the engine noise reduction effect according to this embodiment, and shows two cases: normal injection without pilot injection (symbol P) and conventional pilot injection (symbol R). It can be seen that the noise level is the lowest in the case of this example (marked Q) compared to the above.

尚、パイロット噴射と主噴射との間で噴射ノズルが着座
することがなく、当該着座時の噴射ノズルの弁体の第1
図中」二方向の跳上がりを防止することができるので噴
射ノズルのリフト(第3図(C))は電磁弁20の駆動
パルスに対して精度良く応答する。
Note that the injection nozzle is not seated between pilot injection and main injection, and the first valve body of the injection nozzle when seated is
Since jumps in two directions can be prevented, the lift of the injection nozzle (FIG. 3(C)) responds accurately to the drive pulse of the electromagnetic valve 20.

(発明の効果) 以1〕il′l!述したように本発明に依れば、燃料の
加j(ミ圧送用の電磁弁を、機関の運転状態に応じて開
閉;Ix制御することにより、主噴射に先立ってパイロ
ット噴射を行わせるようにした燃料噴射制御装置におい
て、前記電磁弁を開閉制御する駆動パルスのパルス幅を
調整することにより0;i記パイロット噴射の終了1)
;jに前記主噴射を開始させるようにしたので、従前の
パイロット噴射の有効性を維持しつつ機械騒音の低減が
図られ、勿論排気ガス規制をも図り得ることとなり、特
にアイドル時の噴射制御時に有用である。
(Effect of the invention) 1]il'l! As described above, according to the present invention, the pilot injection is performed prior to the main injection by controlling the solenoid valve for fuel injection (opening/closing depending on the operating state of the engine). By adjusting the pulse width of the drive pulse that controls the opening and closing of the electromagnetic valve,
Since the main injection is started at j, it is possible to reduce mechanical noise while maintaining the effectiveness of the conventional pilot injection, and of course it is also possible to achieve exhaust gas regulation. Sometimes useful.

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

第1図は本発明の装置を実施する噴射ノズル及びこれに
連結される分配型燃料噴射ポンプの要部を示す断面図、
第2図は第1図の電磁弁の開閉制御による噴射制御を示
すプログラムフローチャー1・、第3図は本発明の+r
t射制御装置による噴射ノズルの作動を説明するタイミ
ングチャート、第4図は本発明の制御装置によるエンジ
ン騒音の低減効果の実験例を示すグラフ、第5図は従来
の噴射制御装置を説明する第3図と同様の図である。 5・・・制御回路、10・・・噴射ノズル、20・・・
加圧圧送用電磁弁。
FIG. 1 is a sectional view showing the main parts of an injection nozzle implementing the device of the present invention and a distribution type fuel injection pump connected thereto;
FIG. 2 is a program flowchart 1 showing injection control by opening/closing control of the solenoid valve shown in FIG. 1, and FIG. 3 is a program flowchart 1.
FIG. 4 is a timing chart illustrating the operation of the injection nozzle by the injection control device, FIG. 4 is a graph showing an experimental example of the effect of reducing engine noise by the control device of the present invention, and FIG. It is a figure similar to figure 3. 5... Control circuit, 10... Injection nozzle, 20...
Solenoid valve for pressurized pressure feeding.

Claims (1)

【特許請求の範囲】[Claims] 1. 燃料の加圧圧送用の電磁弁を、機関の運転状態に
応じて開閉制御することにより、主噴射に先立ってパイ
ロット噴射を行わせるようにした燃料噴射制御装置にお
いて、前記電磁弁を開閉制御する駆動パルスのパルス幅
を調整することにより前記パイロット噴射の終了前に前
記主噴射を開始させるようにしたことを特徴とする内燃
機関用燃料噴射制御装置。
1. In a fuel injection control device that performs pilot injection prior to main injection by controlling opening and closing of an electromagnetic valve for pressurized fuel feeding according to the operating state of the engine, the electromagnetic valve is controlled to open and close. A fuel injection control device for an internal combustion engine, characterized in that the main injection is started before the end of the pilot injection by adjusting the pulse width of the drive pulse.
JP10929587A 1987-05-01 1987-05-01 Fuel injection control device for internal combustion engine Pending JPS63277841A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP10929587A JPS63277841A (en) 1987-05-01 1987-05-01 Fuel injection control device for internal combustion engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP10929587A JPS63277841A (en) 1987-05-01 1987-05-01 Fuel injection control device for internal combustion engine

Publications (1)

Publication Number Publication Date
JPS63277841A true JPS63277841A (en) 1988-11-15

Family

ID=14506555

Family Applications (1)

Application Number Title Priority Date Filing Date
JP10929587A Pending JPS63277841A (en) 1987-05-01 1987-05-01 Fuel injection control device for internal combustion engine

Country Status (1)

Country Link
JP (1) JPS63277841A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR100730687B1 (en) * 2000-02-05 2007-06-20 로베르트 보쉬 게엠베하 Method and device for controlling an electromagnetic flow rate control valve
USRE44544E1 (en) 2004-11-12 2013-10-22 C. R. F. Societa Consortile Per Azioni Electroinjector for controlling fuel injection in an internal-combustion engine

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR100730687B1 (en) * 2000-02-05 2007-06-20 로베르트 보쉬 게엠베하 Method and device for controlling an electromagnetic flow rate control valve
USRE44544E1 (en) 2004-11-12 2013-10-22 C. R. F. Societa Consortile Per Azioni Electroinjector for controlling fuel injection in an internal-combustion engine

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