JPS5865963A - Method for obtaining a desired injection rate pattern in fuel injector for internal-combustion engine - Google Patents

Method for obtaining a desired injection rate pattern in fuel injector for internal-combustion engine

Info

Publication number
JPS5865963A
JPS5865963A JP16231481A JP16231481A JPS5865963A JP S5865963 A JPS5865963 A JP S5865963A JP 16231481 A JP16231481 A JP 16231481A JP 16231481 A JP16231481 A JP 16231481A JP S5865963 A JPS5865963 A JP S5865963A
Authority
JP
Japan
Prior art keywords
fuel
spool
pressure
injection rate
rate pattern
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.)
Granted
Application number
JP16231481A
Other languages
Japanese (ja)
Other versions
JPH0233870B2 (en
Inventor
Yoshihisa Yamamoto
義久 山本
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.)
Denso Corp
Original Assignee
NipponDenso 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 NipponDenso Co Ltd filed Critical NipponDenso Co Ltd
Priority to JP16231481A priority Critical patent/JPS5865963A/en
Publication of JPS5865963A publication Critical patent/JPS5865963A/en
Publication of JPH0233870B2 publication Critical patent/JPH0233870B2/ja
Granted legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M59/00Pumps specially adapted for fuel-injection and not provided for in groups F02M39/00 -F02M57/00, e.g. rotary cylinder-block type of pumps
    • F02M59/02Pumps specially adapted for fuel-injection and not provided for in groups F02M39/00 -F02M57/00, e.g. rotary cylinder-block type of pumps of reciprocating-piston or reciprocating-cylinder type
    • F02M59/10Pumps specially adapted for fuel-injection and not provided for in groups F02M39/00 -F02M57/00, e.g. rotary cylinder-block type of pumps of reciprocating-piston or reciprocating-cylinder type characterised by the piston-drive
    • F02M59/105Pumps specially adapted for fuel-injection and not provided for in groups F02M39/00 -F02M57/00, e.g. rotary cylinder-block type of pumps of reciprocating-piston or reciprocating-cylinder type characterised by the piston-drive hydraulic drive

Abstract

PURPOSE:To obtain a desired injection rate pattern by keeping in the partially opened state for a certain time, the supply port of the spool valve for switching and introducing the pressure from a pressure source into the pressure supply system for driving a plunger, in the case of an injection pump. CONSTITUTION:After the first solenoid valve 24 is set in an opened state through current flow at time A, the spool 3 of a spool valve shifts rightward, and a supply port a is partially opened at time G, and then the current flow in the first solenoid valve 24 is suspended, and the closed state is formed. At this time, the fuel in the hydraulic oil chamber 15 of the spool valve is sealed, and the spool 3 is set in recess, so the flow rate of the pressurized fuel which passes- through the supply port (a) and is supplied into the hydraulic oil chamber 21 of a fuel compressing apparatus is reduced, and the lowering speed of the plunger 7 in the fuel compressing apparatus reduces, and the fuel injection rate is reduced. Thus, the initial rise of the injection rate pattern is made gentle, and the engine noise is reduced.

Description

【発明の詳細な説明】 本発明は内燃機関、特にディーセ゛ルエンジン用燃料噴
躬装置において所望の噴射率パターンを得る方法に関す
る。
DETAILED DESCRIPTION OF THE INVENTION The present invention relates to a method for obtaining a desired injection rate pattern in a fuel injection system for an internal combustion engine, particularly a diesel engine.

近年、エンジン排気ガスの清浄化および省エネルギの観
点から、燃料噴射装置における高圧化−高噴射率化や抜
雑なタイミング制御が必要になり。
In recent years, from the viewpoint of cleaning engine exhaust gas and saving energy, it has become necessary to increase the pressure and injection rate of fuel injection devices and to perform sophisticated timing control.

それに応じて神々の提案がなされてきた。その一つとし
て、電子制御油圧駆動式ユニットインジェクタが開発さ
れている。ところが、この型式のユニットインジェクタ
において、高圧化および普鳴耐重化を行うと、噴射率が
急上昇するため、エンジンの騒音が大きくなるきらいが
ある。また、噴射率カー急上昇、′fなわち立上りが急
激であると、騒音ばかりでな(NOxの濃度増大が生じ
ることが判明している。したがって、前記型式のユニッ
トインジェクタにおいて、高圧化を達成すると共に一噴
耐重の立上りを緩慢にすることが望まれている。
Proposals from the gods have been made accordingly. As one of these, an electronically controlled hydraulically driven unit injector has been developed. However, in this type of unit injector, when the pressure is increased and the injection rate is increased, the injection rate increases rapidly, which tends to increase engine noise. In addition, it has been found that if the injection rate suddenly rises rapidly, it not only causes noise but also increases the concentration of NOx. Therefore, in the unit injector of the above type, it is difficult At the same time, it is desired to slow the rise in single-spout load resistance.

しかしながら、噴射率パターンの変更は従来の通常の燃
料噴射装置においても、また前記型式のユニットインジ
ェクタにおいても極めて困難であった。
However, it has been extremely difficult to change the injection rate pattern both in conventional conventional fuel injection devices and in the above-mentioned type of unit injector.

本発明の目的は−プランジャを駆動する圧送系に圧力源
圧力を切換え導入するスプール弁の供給ボートを部分的
に開の状態に一定時間保持することにより一導入圧力の
初期立上りをゆる<シーシたがって噴射率の立上りをゆ
るくして、所望の噴射率パターンを得る方法を提供する
ことである。
The object of the present invention is to reduce the initial rise of the introduced pressure by keeping the supply boat of the spool valve partially open for a certain period of time, which switches and introduces the pressure source pressure into the pressure feeding system that drives the plunger. It is an object of the present invention to provide a method for obtaining a desired injection rate pattern by slowing down the rise of the injection rate.

以下に5本発明の方法の実施に用いる装置により添付図
面を参照して本発明の詳細な説明する。
The present invention will now be described in detail with reference to the accompanying drawings, with reference to the apparatus used to carry out the method of the present invention.

第1図を参照すると一本発明の方法の実施に用いる燃料
噴射装置10が示され、この装置はインジェクタ1 +
 fli制御装置60および燃料供給圧力源14を含む
。インジェクタ1はスプール弁、燃料圧縮装置、1丸射
ノズル装置および電磁弁装置を有する。スプール弁はス
プール3.該スプール弁を一方向に押圧するばね3a−
該スプールを収容している孔2を含む。孔2は供給ボー
) (a)および戻しボート(b)を形成され−また前
記スプール3の左端面との間に作動油室15を画成して
いる。インジェクタ1の燃料圧縮装置は大径ピストン6
、これを収容する孔4.プランジャ7、これを収容する
孔5.該大径ピストンと該孔4との間に画成されろ作動
油室21−および該プランジャ7と該孔5との間に画成
される燃料室12を含む。インジェクタ1の噴射ノズル
装置は燃料噴射ノズル8と。
Referring to FIG. 1, there is shown a fuel injection device 10 for use in carrying out the method of the present invention, which device includes an injector 1 +
fli controller 60 and fuel supply pressure source 14. The injector 1 has a spool valve, a fuel compression device, a single injection nozzle device, and a solenoid valve device. The spool valve is spool 3. A spring 3a- that presses the spool valve in one direction.
It includes a hole 2 accommodating the spool. The hole 2 is formed with a supply boat (a) and a return boat (b), and defines a hydraulic oil chamber 15 between the hole 2 and the left end surface of the spool 3. The fuel compression device of the injector 1 is a large diameter piston 6
, a hole 4 for accommodating this. A plunger 7, a hole 5 for housing it. It includes a hydraulic oil chamber 21 defined between the large diameter piston and the hole 4, and a fuel chamber 12 defined between the plunger 7 and the hole 5. The injection nozzle device of the injector 1 is a fuel injection nozzle 8.

これを押圧するはね8aを含む。インジェクタ1の電磁
弁装置は6個の2ボ一ト2位置電磁弁24゜25−26
を含み、第1の電磁弁24は管路30を介してスプール
弁の作動油室15と燃料供給圧力源14とにそれぞれ接
続されている。第2の電磁弁25は管路40を介してス
プール弁の作動油室15と低圧の燃料タンク16とにそ
れぞれ接続されている。また、第6の電磁弁2Gは管路
50および絞り22を介してスプール弁の戻しボート(
b)に接続され、さらに管路50を介して低圧の燃料タ
ンク16に接続されている。スプール弁の供給ボー) 
(a)は管路30’、30を介して燃料供給圧力源14
に連通している。燃料圧縮装置の燃料室12は逆止め弁
13および管路30’を介して燃料供給圧力源14に連
通し、また通路8bを介してノズル8に連通している。
It includes a spring 8a that presses it. The solenoid valve device of injector 1 consists of 6 2-bot 2-position solenoid valves 24°25-26
The first electromagnetic valve 24 is connected to the hydraulic oil chamber 15 of the spool valve and the fuel supply pressure source 14 via a conduit 30, respectively. The second electromagnetic valve 25 is connected to the hydraulic oil chamber 15 of the spool valve and the low-pressure fuel tank 16 via a conduit 40, respectively. Further, the sixth solenoid valve 2G is connected to the spool valve return boat (
b) and further connected via a line 50 to a low-pressure fuel tank 16. Spool valve supply bow)
(a) shows the fuel supply pressure source 14 via the pipes 30', 30;
is connected to. The fuel chamber 12 of the fuel compression device communicates with a fuel supply pressure source 14 via a check valve 13 and a line 30' and with the nozzle 8 via a passage 8b.

燃料圧縮装置の作動油室21はスプール弁の孔2におけ
るスプール3の位置に応じてスプール弁の供給ボート(
a)または戻しポ+ −) (b)のいずれか一方に連
通するようにされている。
The hydraulic oil chamber 21 of the fuel compression device is connected to the spool valve supply boat (
a) or the return port +-) (b).

燃料供給圧力源14は燃料タンク16′、フィにタ17
−ポンプ18−該ポンプのバイパス管路に設けられた調
圧弁19および蓄圧器2 ’0を含む。
The fuel supply pressure source 14 includes a fuel tank 16' and a fuel tank 17'.
- Pump 18 - includes a pressure regulating valve 19 and a pressure accumulator 2'0 provided in the bypass line of the pump.

第2図を参照すると、制御装置60はコントローラ23
およびセンサ(Sよ〜s6)を含む。センサ(Sよ)は
エンジンの回転速度、センサ(s2)はアクセルペダル
の踏込み量、センサ(S3)はエンジンの温度、センサ
(84)はエンジンの気筒マー久センサ(S5)は配管
からの燃料洩れやエンジンオーバランなどの緊急状態、
センサ(s6)は燃料圧力供給源14の圧力をそれぞれ
検出する。コントローラ23は噴射量設定回路(PI)
 、 ”J=を射開始時期設定回路(P2) +噴射量
を決定する第1の計算回路(A、、) +哨躬開始時期
を決定する第2の計装回路(Aρおよび出力増幅回路(
A、)を含む。第1の計算回路(A1)はセンサ(Sl
−82)からの信号に基いて第6の電磁弁26に対する
通電時間を計算1−る。第2の計算回路(A、)はセン
サ(S工、52−83)からの信号に基いて気筒マーク
に対する第1の電磁弁24への通電開始時刻偏差を計算
する。
Referring to FIG. 2, the control device 60 includes the controller 23
and sensors (Syo~s6). The sensor (S) is the engine rotation speed, the sensor (S2) is the amount of accelerator pedal depression, the sensor (S3) is the engine temperature, and the sensor (84) is the engine cylinder mark sensor (S5) is the fuel from the pipe. Emergency situations such as leaks or engine overruns,
The sensors (s6) each detect the pressure of the fuel pressure supply source 14. The controller 23 is an injection amount setting circuit (PI)
, ``J = injection start timing setting circuit (P2) + first calculation circuit that determines the injection amount (A,,) + second instrumentation circuit that determines the control start timing (Aρ and output amplification circuit (
A,). The first calculation circuit (A1) is a sensor (Sl
Calculate the energization time for the sixth solenoid valve 26 based on the signal from -82). The second calculation circuit (A) calculates the deviation of the time when energization to the first electromagnetic valve 24 starts to be energized with respect to the cylinder mark based on the signal from the sensor (S, 52-83).

出力増幅回路(A3)はクランク位置を判別して、関連
の気筒の電磁弁24−25−26に所定のタイミングで
通電する。この出力増幅回路(A3)は通常は第1と第
6の電磁弁24.26に対しては一定時間だけ通電する
が、センサ(s5)からの緊急信号またはセンサ(S6
)からの圧力源圧力信号に応じて通電を停止したり、ま
たは通電したままにすることも可能である。
The output amplification circuit (A3) determines the crank position and energizes the solenoid valves 24-25-26 of the related cylinders at a predetermined timing. This output amplification circuit (A3) normally energizes the first and sixth solenoid valves 24, 26 for a certain period of time, but when an emergency signal from the sensor (s5) or an emergency signal from the sensor (S6
) It is also possible to de-energize or keep energized in response to a pressure signal from the pressure source.

第1図に示す燃料噴射装置10の従来の作動を第6図を
参照して説明する。第1図の状態において、第1の電磁
弁24が時刻Aで通電されて、その2個のボートが連通
状態(以下、「開」という)に置かれると、燃料が燃料
供給圧力源14からスプール弁の作動油室15へ導入さ
れ、スプール3をはね3aの力に抗して右方へ動かす。
The conventional operation of the fuel injection device 10 shown in FIG. 1 will be explained with reference to FIG. 6. In the state shown in FIG. 1, when the first solenoid valve 24 is energized at time A and the two boats are placed in communication (hereinafter referred to as "open"), fuel is supplied from the fuel supply pressure source 14. It is introduced into the hydraulic oil chamber 15 of the spool valve, and moves the spool 3 to the right against the force of the spring 3a.

この間、第2の電磁弁2502個のボートは非連通状態
(以下、閉という)に置かれている。スプール弁のスプ
ール3が孔2内で右方へ動くにつれて、戻しボート(b
)が閉じられ5次に供給ボー) (a)が開かれる。こ
れにより、燃料圧縮装置の作動油室21がスプール弁の
供給ポー) (a)を介して燃料供給圧力源14と連通
して加圧燃料を受は取り、大径ピストン6とプランジャ
7との受圧面積の差によりプランジャ7が下方へ駆動さ
れて燃料室12内の燃料を通路8bおよびノズル8を介
して噴射する。
During this time, the boats of 2502 second solenoid valves are placed in a non-communicating state (hereinafter referred to as closed). As the spool 3 of the spool valve moves to the right in the hole 2, the return boat (b
) is closed and 5th supply bow) (a) is opened. As a result, the hydraulic oil chamber 21 of the fuel compression device communicates with the fuel supply pressure source 14 via the supply port (a) of the spool valve to receive pressurized fuel and connect the large diameter piston 6 and plunger 7. The plunger 7 is driven downward by the difference in pressure receiving area, and the fuel in the fuel chamber 12 is injected through the passage 8b and the nozzle 8.

この際、燃料室12内の燃料は逆止め弁13により管路
30”を経て燃料供給圧力源14へ逆流″1−るのを阻
Iトされる。
At this time, the fuel in the fuel chamber 12 is prevented from flowing back to the fuel supply pressure source 14 through the conduit 30'' by the check valve 13.

次に、第1の電磁弁24が時刻Bで通電を停止されて、
その2個のボートが閉の状態に酋かれた後、第2の電磁
弁25が時刻Cで通電されて、その2個のボートが1開
の状態にされ、スプール弁の作動油室15内の燃料を低
圧の燃料タンク16へ導き、それによりスプール弁のス
プール3がはね3aの力により孔2内を左方へ動く。ス
プール3が孔2内を左方へ動くてつれて、供給ボー) 
(a)が閉じられ1次に戻しボート(b)が開かれる。
Next, the first solenoid valve 24 is de-energized at time B, and
After the two boats are in the closed state, the second solenoid valve 25 is energized at time C, the two boats are in the open state, and the inside of the hydraulic oil chamber 15 of the spool valve is turned on. of fuel is led to the low-pressure fuel tank 16, whereby the spool 3 of the spool valve moves to the left in the hole 2 by the force of the spring 3a. As the spool 3 moves to the left inside the hole 2, the supply bow)
(a) is closed and the primary return boat (b) is opened.

スプール3が孔2の左端に達した後、第2の電磁弁25
が通電を停止される(時刻D)。
After the spool 3 reaches the left end of the hole 2, the second solenoid valve 25
is de-energized (time D).

この状態において、第6の電磁弁26が時刻Eで通電さ
れて、その2個のボートが開の状態に1紅かれると、燃
料圧縮装置の作動油室21内の燃料はスプール弁の尿し
ポー)(bL第6の電磁弁26および管路50を経て低
圧の燃料タンク16へ排出される。このように、第、3
の電磁弁26が通電されている間、燃料が燃料圧縮装置
の作動油室21から排出されるにつれて、燃料圧力供給
源14からの燃料が管路30“および逆止め弁13を経
て燃料圧縮装置の燃料室12内へ流入して。
In this state, when the sixth solenoid valve 26 is energized at time E and the two boats are opened, the fuel in the hydraulic oil chamber 21 of the fuel compression device is drained from the spool valve. (bL) is discharged to the low pressure fuel tank 16 via the sixth electromagnetic valve 26 and the pipe 50. In this way, the third
While solenoid valve 26 is energized, fuel from fuel pressure source 14 passes through line 30'' and check valve 13 to the fuel compression device as fuel is discharged from hydraulic fluid chamber 21 of the fuel compression device. into the fuel chamber 12.

大径ピストン6およびプランジャ7を押し上げる。Push up the large diameter piston 6 and plunger 7.

したがって、燃料室12からノズル8を経て噴射される
燃料噴射量は第6の電磁弁260通電時間により決定さ
れる。第3の電磁弁26が通電を時刻Fで停止されて閉
の状態にされると、燃料圧縮装置の作動油室21と燃料
室12のそれぞれの圧力が大径ピストン6とプランジャ
7の面積比に応じてつりあうように、大径ピストン6と
プランジャ7が停止する。絞り22は燃料圧縮装置の燃
料室12内における燃料の調量時間を延長させる作用を
し、正確な調量を可能にする。
Therefore, the amount of fuel injected from the fuel chamber 12 through the nozzle 8 is determined by the energization time of the sixth electromagnetic valve 260. When the third electromagnetic valve 26 is turned off at time F and placed in a closed state, the respective pressures in the hydraulic oil chamber 21 and the fuel chamber 12 of the fuel compression device are adjusted to the area ratio of the large-diameter piston 6 and the plunger 7. The large-diameter piston 6 and the plunger 7 stop in a balanced manner according to. The throttle 22 serves to extend the metering time of the fuel in the fuel chamber 12 of the fuel compression device, allowing accurate metering.

以上の工程が繰り返されて、燃料がエンジンに供給され
る。ここで、第1の′電磁弁24がA%iされて開の状
態てなる時刻AはセンサS工等がらの信号に基いて可変
制御されて噴射タイミングを最適にするようにされる。
The above steps are repeated to supply fuel to the engine. Here, the time A when the first electromagnetic valve 24 is in the open state is variably controlled based on signals from the sensor S, etc. to optimize the injection timing.

また、第6の電磁弁26が通電されて開の状態に置かれ
る時間間隔EFはセンサ5l−82等からの信号に基い
て燃料の所定の;iI7!I量を可能に1−る。各電磁
弁の開閉の時刻A〜Fの設定はおる程度の自由度を有し
−これらの時刻のいくつかは同時としてもよい場合がお
る。
Further, the time interval EF during which the sixth electromagnetic valve 26 is energized and placed in an open state is determined based on the signals from the sensor 5l-82, etc., at a predetermined time interval EF of the fuel; iI7! The amount of I can be reduced to 1-. There is a certain degree of freedom in setting the opening and closing times A to F of each electromagnetic valve - some of these times may be simultaneous.

第1図に示す燃料噴射装置10の本発明による作動は第
4図を参照して説明される。第1図の状態において、第
1の電磁弁24が時刻Aで通電されて開の状態にされた
後、スプール弁のスプール3が右方へ移動して供給ボー
) (a)を部分的に開放した時刻Gで第1の電磁弁2
4の通電が停止されて閉の状態にされる。この時、スプ
ール弁の作動油室15内の燃料は密封され、スプール3
が休止するので、供給ボート(a)を通って燃料圧縮装
置の作動油室21へ供給されろ加圧燃料の流量が小さく
、シたがって燃料圧縮装置のプランジャ7の下降速度し
ま小さく、燃料噴射率が小さい。次に1時刻Hで再び第
1の電磁弁24に通電されて開の状態にされると、スプ
ール3がさらに右方へ移動して供給ボー) (a)を完
全に開口させた後、孔2の右端に達する。この間、供給
ボー) (a)は完全に開口しているから、プランジャ
7の下降速度は大きくなり−したがって燃料鳴耐重も高
い。燃料の噴射が終了し、スプール3が孔2の右端で停
止した後。
The operation of the fuel injection system 10 shown in FIG. 1 according to the invention will be explained with reference to FIG. In the state shown in FIG. 1, after the first electromagnetic valve 24 is energized at time A and placed in the open state, the spool 3 of the spool valve moves to the right to partially control the supply bow (a). At the time G when the first solenoid valve 2 is opened.
4 is stopped and brought into a closed state. At this time, the fuel in the hydraulic oil chamber 15 of the spool valve is sealed, and the spool 3
is at rest, the flow rate of the pressurized fuel supplied to the hydraulic oil chamber 21 of the fuel compression device through the supply boat (a) is small, and therefore the descending speed of the plunger 7 of the fuel compression device is small, causing fuel injection. rate is small. Next, at 1 time H, when the first solenoid valve 24 is energized again and opened, the spool 3 moves further to the right, completely opening the supply bow (a), and then opening the spool 3. Reach the right end of 2. During this time, since the supply bow (a) is completely opened, the descending speed of the plunger 7 is high - and therefore the fuel noise resistance is also high. After the fuel injection is finished and the spool 3 stops at the right end of the hole 2.

第1の電磁弁24が時刻Bで通電を停止され閉の状態に
される。この時点以後は、第2および第6の電磁弁は紀
ろ図の従来のものと同様に開閉される。
The first electromagnetic valve 24 is de-energized at time B and is placed in a closed state. From this point on, the second and sixth solenoid valves are opened and closed in the same manner as the conventional one in the Kiro diagram.

第5図において、実線で示す本発明による噴射率パター
ンが鎖線で示す従来のものに比較すると。
In FIG. 5, the injection rate pattern according to the present invention shown by the solid line is compared with the conventional injection rate pattern shown by the chain line.

立上りがゆるやかであることが示されている。発明者が
行った実験によると、ノズル8を押圧てるばね8aは弱
い方が1本発明による効果が顕著であることが判ってい
る。第4図に示す本発明の実施例においては、第1の電
磁弁24の作動を操作することにより第5図の実線で示
す噴射率パターンが得られたが、代替的に第2の電磁弁
25の作動を操作(例えは1時間間隔GHで開の状態に
1−る)¥ることによっても第5図の実線の噴射率パタ
ーンが得られる。さらに、スプール弁がソレノイド駆動
の場合、スプール弁のソレノイドに流す電流を一時的に
一定に保ってスプールを停止させるか、またはソレノイ
ドに流″1″電流を制御し゛Cスゾールをゆっくり動か
すようにしても第5図の実線で示”!噴射率パターンが
得られろ。このように。
It is shown that the rise is gradual. According to experiments conducted by the inventor, it has been found that the effect of the present invention is more pronounced when the spring 8a pressing the nozzle 8 is weaker. In the embodiment of the present invention shown in FIG. 4, the injection rate pattern shown by the solid line in FIG. 5 was obtained by manipulating the operation of the first solenoid valve 24; The injection rate pattern shown by the solid line in FIG. 5 can also be obtained by operating the valve 25 (for example, by turning it into the open state at 1-hour intervals). Furthermore, if the spool valve is driven by a solenoid, the current flowing through the spool valve solenoid can be temporarily kept constant to stop the spool, or the current flowing through the solenoid can be controlled to slowly move the spool. The injection rate pattern is also shown by the solid line in Figure 5. You can obtain the injection rate pattern like this.

本発明は第1図に示j構成の燃料噴射装置ばかりでな(
、圧力源の数、作動油のaI類、配管、電磁弁の型式や
個数、スプールの型式、ノズルの型式や調量方法などが
異なっても、またコントローラもアナログ回路でなくデ
ィジタルあるいは両者の複合とすることも−センサの数
1種類が異なっても同様に適用可能であることは明らか
である。
The present invention is applicable not only to a fuel injection device having the configuration shown in FIG.
, the number of pressure sources, the type and number of hydraulic oil, piping, the type and number of solenoid valves, the spool type, the nozzle type and metering method, etc., and the controller is not an analog circuit but a digital one or a combination of both. It is clear that the present invention is equally applicable even if the number of types of sensors is different.

以上の辿り1本発明によると、スプール弁の作動油の供
給ボートが部分的に開口した時点でスプールを一時的に
停止させるか、または減速させ。
According to the present invention, the spool is temporarily stopped or decelerated when the hydraulic oil supply boat of the spool valve is partially opened.

その後スプールを一定速度で移動させることにより、噴
射率パターンの初期立上りをゆるやかにする。これによ
り、内燃機関の騒音が低減され、また排気ガスが清浄化
されるなどの効果が有られる。
Thereafter, by moving the spool at a constant speed, the initial rise of the injection rate pattern is made gradual. This has the effect of reducing the noise of the internal combustion engine and purifying the exhaust gas.

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

鉋1図は本発明の方法の実施に用いる燃料噴射装置の概
略図。 一2図は第1図の装置の制御装置のブロック図。 第6図は従来の方法による各要素の制御タイミングを示
す図、 第4図は本発明の方法による各要素の制御タイミングを
部分的に示す図、および 第5区は従来技術および本発明により得られる噴射率パ
ターンを示す図である。 図において。 1・・・・・・・・・インジェクタ 3・・・・・・・・・スプール 6・・・・・・・・・大径ピストン 7・・・・・・・・・プランジャ 8・・・・・・・・・ノズル 10・・・・・・・・・燃料噴射装置 14・・・・・・・・・燃料圧力供給跡15−21・・
・・・・・・・作動油室23・・・・・・・・・コント
ローラ 24−25−26・・・・・・・・・第1.第2および
第6の′電磁弁 代理人 浅 村   皓 外4名
Figure 1 is a schematic diagram of a fuel injection device used to carry out the method of the present invention. FIG. 12 is a block diagram of the control device of the apparatus shown in FIG. FIG. 6 is a diagram showing the control timing of each element according to the conventional method, FIG. FIG. 2 is a diagram showing an injection rate pattern. In fig. 1...Injector 3...Spool 6...Large diameter piston 7...Plunger 8... ...Nozzle 10...Fuel injection device 14...Fuel pressure supply trace 15-21...
..... Hydraulic oil chamber 23 ..... Controller 24-25-26 ..... 1st. 2nd and 6th Solenoid Valve Agents: 4 people, Akira Asamura

Claims (1)

【特許請求の範囲】 (1)圧力源からの圧力を切り換えるスプール弁を有す
る切換制御弁機構、前記圧力により作動されるピストン
およびプランジャを有する圧送機構。 および圧送された燃料を噴射するノズルを含む油圧駆動
方式の燃料噴射装置において所望の噴射率パターンを得
る方法において、前記圧送&桐のtストン作動油室を前
記圧力源に連通させる前記切換制御弁機構の制御ボート
が部分的に開口した後に前記切換制御弁機構の切換速度
を減速、または一時的に零にすることを特徴とする燃料
噴射装置において所望の噴射率パターンを得る方法。 (2、特許請求の範囲第1項に記載の方法において一前
記スプール弁を作動させる前記切換制御弁機構の2個の
開閉弁の中の少なくとも一方を噴射初期に開閉すること
により前記スプール弁の切換速度を減速、または一時的
に零にすることを特徴とする燃料噴射装置において所望
の噴射率パターンを得る方法。 (3)特許請求の範囲第1項に記載の方法において、電
磁力により作動する前記スプール弁の電流値を噴射初期
に変えることにより、前記スプール弁の切換速度を減速
または一時的に零にすることを特徴とする燃料噴射装置
において所望の噴射率パターンを得る方法。
Claims: (1) A switching control valve mechanism having a spool valve that switches pressure from a pressure source, and a pressure feeding mechanism having a piston and plunger operated by the pressure. and a method for obtaining a desired injection rate pattern in a hydraulically driven fuel injection device including a nozzle that injects pressure-fed fuel, wherein the switching control valve communicates the pressure-fed & paulownia t-stone hydraulic oil chamber with the pressure source. A method for obtaining a desired injection rate pattern in a fuel injection device, characterized in that the switching speed of the switching control valve mechanism is reduced or temporarily reduced to zero after a control boat of the mechanism is partially opened. (2. In the method according to claim 1, one of the two on-off valves of the switching control valve mechanism that operates the spool valve is opened and closed at the initial stage of injection. A method for obtaining a desired injection rate pattern in a fuel injection device characterized by decelerating or temporarily reducing the switching speed to zero. (3) In the method according to claim 1, the switching speed is actuated by electromagnetic force. A method for obtaining a desired injection rate pattern in a fuel injection device, characterized in that the switching speed of the spool valve is reduced or temporarily reduced to zero by changing the current value of the spool valve at an early stage of injection.
JP16231481A 1981-10-12 1981-10-12 Method for obtaining a desired injection rate pattern in fuel injector for internal-combustion engine Granted JPS5865963A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP16231481A JPS5865963A (en) 1981-10-12 1981-10-12 Method for obtaining a desired injection rate pattern in fuel injector for internal-combustion engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP16231481A JPS5865963A (en) 1981-10-12 1981-10-12 Method for obtaining a desired injection rate pattern in fuel injector for internal-combustion engine

Publications (2)

Publication Number Publication Date
JPS5865963A true JPS5865963A (en) 1983-04-19
JPH0233870B2 JPH0233870B2 (en) 1990-07-31

Family

ID=15752160

Family Applications (1)

Application Number Title Priority Date Filing Date
JP16231481A Granted JPS5865963A (en) 1981-10-12 1981-10-12 Method for obtaining a desired injection rate pattern in fuel injector for internal-combustion engine

Country Status (1)

Country Link
JP (1) JPS5865963A (en)

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS56127359U (en) * 1980-02-25 1981-09-28

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS56127359U (en) * 1980-02-25 1981-09-28

Also Published As

Publication number Publication date
JPH0233870B2 (en) 1990-07-31

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