JPH045469A - Fuel injection device - Google Patents

Fuel injection device

Info

Publication number
JPH045469A
JPH045469A JP10727790A JP10727790A JPH045469A JP H045469 A JPH045469 A JP H045469A JP 10727790 A JP10727790 A JP 10727790A JP 10727790 A JP10727790 A JP 10727790A JP H045469 A JPH045469 A JP H045469A
Authority
JP
Japan
Prior art keywords
fuel
fuel injection
nozzle hole
air
engine
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
JP10727790A
Other languages
Japanese (ja)
Inventor
Kiyoshi Yukishimo
雪下 清
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.)
Nissan Motor Co Ltd
Original Assignee
Nissan Motor 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 Nissan Motor Co Ltd filed Critical Nissan Motor Co Ltd
Priority to JP10727790A priority Critical patent/JPH045469A/en
Publication of JPH045469A publication Critical patent/JPH045469A/en
Pending legal-status Critical Current

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Abstract

PURPOSE:To provide satisfactory fuel mixed state in both low speed and high speed rotations of an engine by making the nozzle hole directing direction of a fuel injection valve variable in a fuel injection device for internal combustion engine for supplying a fuel by the fuel injection valve installed to an inlet pipe. CONSTITUTION:A nozzle hole part moving member 3 moves the directing direction of a nozzle hole 2 to, for example, a high speed rotation injection angle thetaof 60 deg. by bringing the oil pressure applied to a piston 6 into ON state at the time of engine high speed rotation. As the fuel is injected to the air main flow at a large angle, thus, the fuel is included into the air flow and satisfactorily mixed with the air. At the time of low speed rotation, the oil pressure applied to the piston 6 is brought into OFF state, the nozzle hole part moving member 3 is moved to the original position by a return spring 8 to make the directing direction of nozzle hole 2 to, for example, a low speed rotation injection angle alpha of 23 deg.. Hence, as the fuel is injected into the air main flow at a small angle, the fuel is carried on the air main flow and satisfactorily mixed with the air.

Description

【発明の詳細な説明】 産業上の利用分野 本発明は、燃料噴射装置に関する。[Detailed description of the invention] Industrial applications The present invention relates to a fuel injection device.

従来の技術 燃焼状態の制御に適している等の理由から、燃料噴射弁
を吸気管に装着し、所定量の燃料を噴射して、エンジン
に供給する、燃料噴射装置付のエンジンが知られている
(特開昭59−1417491号公報参照)。
Conventional Technology Engines equipped with a fuel injection device are known, in which a fuel injection valve is attached to the intake pipe and a predetermined amount of fuel is injected and supplied to the engine because it is suitable for controlling the combustion state. (Refer to Japanese Unexamined Patent Publication No. 1417491/1983).

発明か解決しようとする課題 しかしながら、このような従来の燃料噴射装置にあって
は、燃料噴射弁は吸気管に固定されており、燃料噴射弁
の噴孔指向方向は一定で燃料の噴射方向は不変となって
いる。
Problems to be Solved by the Invention However, in such conventional fuel injection devices, the fuel injection valve is fixed to the intake pipe, and the injection hole orientation direction of the fuel injection valve is constant, and the fuel injection direction is fixed. It remains unchanged.

このため、エンジンの低速回転と高速回転の燃料混合状
態を一定にすることがてきないという問題点があった。
For this reason, there is a problem in that it is not possible to maintain a constant fuel mixture state between low speed rotation and high speed rotation of the engine.

すなわち、エンジンの低速回転に合わせた空気の主流に
対して小さい燃料噴射角に燃料噴射弁を設置すると、高
速回転においては吸気管内の空気主流の流速が早いため
に、燃料は押し流されて空気主流中に混入できない。
In other words, if the fuel injection valve is installed at a small fuel injection angle relative to the main flow of air at low speed rotation of the engine, the flow velocity of the main flow of air in the intake pipe is fast at high speed rotation, so the fuel is swept away and becomes part of the main flow of air. It cannot be mixed inside.

このため、高速回転においては燃料と空気との混合状態
が悪くなり、燃焼が悪化して燃費悪化、排気ガス中のH
C排出量の増大等の弊害が起こる。
For this reason, at high speeds, the mixing state of fuel and air deteriorates, combustion worsens, fuel efficiency worsens, and H
Harmful effects such as an increase in C emissions occur.

そこで、高速回転に合わせて、燃料が空気主流内に混入
できるように、空気の主流に対して大きな燃料噴射角に
燃料噴射弁を設置すると、高速回転における燃料の混合
状態は改善されて燃焼状態は良くなるが、低速回転にお
いては空気流量が少ないので、燃料は空気の流れに乗れ
ず噴射された燃料のほとんどが壁流となってしまうため
、燃焼は悪化して、トルク低下、燃費悪化、HC排出量
の増大、レスポンス悪化等の弊害か起こるという問題点
があった。
Therefore, if the fuel injection valve is installed at a large fuel injection angle relative to the main stream of air so that the fuel can mix into the main stream of air at high speed rotation, the fuel mixing state at high speed rotation will be improved and the combustion condition will be improved. However, since the air flow rate is small at low speeds, the fuel cannot ride the air flow and most of the injected fuel ends up in a wall flow, which worsens combustion, resulting in lower torque, worse fuel efficiency, and There have been problems in that adverse effects such as an increase in HC emissions and a deterioration in response occur.

本発明は、このような従来の問題点に着目してなされた
ものであり、その目的とするところは、エンジンの低速
回転と高速回転との燃料混合状態を共に良好とした燃料
噴射装置を提供しようとするものである。
The present invention has been made in view of these conventional problems, and an object of the present invention is to provide a fuel injection device that improves the fuel mixture state at both low speed rotation and high speed rotation of an engine. This is what I am trying to do.

課題を解決するための手段 このため本発明は、吸気管に装着した燃料噴射弁により
燃料を供給する内燃機関の燃料噴射装置において、燃料
噴射弁の噴孔指向方向を可変とした。
Means for Solving the Problems Accordingly, the present invention provides a fuel injection device for an internal combustion engine that supplies fuel with a fuel injection valve attached to an intake pipe, in which the direction of injection hole orientation of the fuel injection valve is made variable.

作用 エンジンの低速回転域においては、燃料噴射弁の噴孔指
向方向を、吸入空気の主流に対し、小さい角度に設定す
る。燃料は空気の主流に略平行となる如く噴射されるの
で、空気と良く混合する。
In the low-speed rotation range of the engine, the injection hole orientation direction of the fuel injection valve is set at a small angle with respect to the mainstream of intake air. Since the fuel is injected approximately parallel to the mainstream of air, it mixes well with the air.

また、高速回転域においては、燃料噴射弁の噴射指向方
向を空気の主流に対し大きい角度に設定する。燃料は空
気の主流に対向する如く噴射され空気と良(混合する。
Further, in a high speed rotation range, the injection direction of the fuel injection valve is set at a large angle with respect to the mainstream of air. The fuel is injected facing the mainstream of air and mixes well with the air.

実施例 以下、本発明を図面に基づいて説明する。第1図は、本
発明の第1実施例を示す図である。
EXAMPLES Hereinafter, the present invention will be explained based on the drawings. FIG. 1 is a diagram showing a first embodiment of the present invention.

まず構成を説明する。燃料噴射弁1の先端部に、燃料の
噴孔2を有する円筒形状の噴孔部移動部材3が移動可能
に取り付けられ、該噴孔部移動部材3は、ピン4を介し
て油圧によって移動する口。
First, the configuration will be explained. A cylindrical nozzle hole moving member 3 having a fuel nozzle hole 2 is movably attached to the tip of the fuel injection valve 1, and the nozzle hole moving member 3 is moved by hydraulic pressure via a pin 4. mouth.

ド5及びピストン6に結合されている。ピストン6には
、油のシールのためOリング7が設けられており、また
油かドレンされたときにピストン6を戻すリターンスプ
リング8が配設されている。
5 and a piston 6. The piston 6 is provided with an O-ring 7 for oil sealing, and is also provided with a return spring 8 that returns the piston 6 when the oil is drained.

なお、9はシール部材である。Note that 9 is a sealing member.

第2図に、燃料噴射弁噴孔2の指向方向を切換える油圧
制御のブロック図を示す。
FIG. 2 shows a block diagram of hydraulic control for switching the orientation direction of the fuel injection valve nozzle hole 2. As shown in FIG.

エンジン回転数、エンジン負荷、エアフローメータ出力
、水温等の特性値を基にフントロールユニット10によ
って、エンジンの運転状態を検知し、ソレノイドバルブ
11へ信号を送り、オイルポンプ12から送られて来る
オイルの油路を切換え、スプールバルブを作動させて油
路を形成することによりピストン6に掛る油圧を制御す
る。
The engine operating condition is detected by the engine control unit 10 based on characteristic values such as engine speed, engine load, air flow meter output, water temperature, etc., and a signal is sent to the solenoid valve 11 to send the oil sent from the oil pump 12. The oil pressure applied to the piston 6 is controlled by switching the oil passage and forming the oil passage by operating the spool valve.

14は、ピストン6に掛る油圧を受けてONする油圧ス
イッチで、正常な作動状態を確認する油圧スイッチであ
る。
Reference numeral 14 denotes an oil pressure switch that is turned on in response to oil pressure applied to the piston 6, and is used to confirm a normal operating state.

次に作用を説明する。噴孔部移動部材3は、エンジン高
速回転時には、ピストン6に掛る油圧をON状態とする
ことによって、噴孔2の指向方向を、第3図に図示した
ように、例えば60’の高速回転用噴射角度θとなるよ
うに移動する。これにより燃料は空気主流に大きな角度
で噴射されるので、空気流に混入しよく混合する。
Next, the effect will be explained. When the engine rotates at high speed, the nozzle hole moving member 3 turns on the hydraulic pressure applied to the piston 6, thereby changing the orientation direction of the nozzle hole 2, for example, for a high speed rotation of 60' as shown in FIG. Move so that the injection angle is θ. As a result, the fuel is injected into the main stream of air at a large angle, so that it mixes well with the air stream.

また、低速回転時には、ピストン6に掛る油圧をOFF
状態とし、リターンスプリング8によって、噴孔部移動
部材3を元の位置に移動させ、噴孔2の指向方向を、例
えば23°の低速回転噴射角αとする。これにより、燃
料は空気主流に小さい角度で噴射されるので、空気主流
に乗り流れて空気と良(混合する。
Also, during low speed rotation, the hydraulic pressure applied to the piston 6 is turned off.
state, the nozzle hole portion moving member 3 is moved to the original position by the return spring 8, and the orientation direction of the nozzle hole 2 is set to a low-speed rotation injection angle α of, for example, 23°. As a result, the fuel is injected into the mainstream air at a small angle, so it flows along the mainstream air and mixes well with the air.

なお、噴孔2指向方向の低速回転用燃料噴射角度から、
高速回転用燃料噴射角度への切換えは、パワーショック
をドライバーに感じさせないように同一出力ポイントて
行われるようにする。
In addition, from the fuel injection angle for low speed rotation in the direction of injection hole 2,
Switching to the fuel injection angle for high-speed rotation is made at the same output point so that the driver does not feel a power shock.

第4図に切換ポイントを示す。切換ポイントは、エンジ
ン回転速度、車速、水温、エンジン負荷なとを判断の特
性値として行われ、高負荷はど低いエンジン回転速度で
切換えられる。
Figure 4 shows the switching points. The switching point is determined using characteristic values such as engine rotation speed, vehicle speed, water temperature, and engine load, and high load is switched at a low engine rotation speed.

なおまた、この切換に連動してエンジン制御装置の空燃
比制御と点火時期制御もそれぞれ低速及び高速の特性に
合った制御特性に切換えられ、最高制御が行われる。
Additionally, in conjunction with this switching, the air-fuel ratio control and ignition timing control of the engine control device are also switched to control characteristics that match the low-speed and high-speed characteristics, respectively, and maximum control is performed.

第5図には、エンジン高速回転域における噴孔指向方向
を、空気主流に対し燃料噴射角が23゜及び60°に設
定した場合の、エンジン回転数と出力(PS)およびH
C排出量(%)との関係を示す。
Figure 5 shows the engine speed, output (PS), and H
The relationship with C emissions (%) is shown.

噴孔2の指向方向を空気主流に対して燃料噴射角(60
°)が大きくなるように設定することによって、出力は
増加し、HC排出量は減少しておリ、本発明装置がエン
ジン性能向上に効果があることが分かる。
The orientation direction of the nozzle hole 2 is set at a fuel injection angle (60
It can be seen that by setting the angle (°) to be large, the output increases and the amount of HC emissions decreases, indicating that the device of the present invention is effective in improving engine performance.

また、エンジン回転速度9800 rpm一定の高速回
転において、噴孔2の指向方向を空気主流に対して燃料
噴射角が23°及び60°となるように設定し、吸気ボ
ート内の燃料混合状態を実験により調べたところ、燃料
噴射角23°の場合は、燃料が混合している個所は、吸
気ポート上部の一部に限られ、他の部分は空気が主で燃
料は混合されていない。これに対し燃料噴射角60’の
場合には燃料の混合領域はポート内全体に広がり、混合
状態が極めて良いことを確認した。
In addition, at a constant high-speed engine rotation speed of 9800 rpm, the orientation direction of the injection hole 2 was set so that the fuel injection angle was 23° and 60° with respect to the mainstream air, and the fuel mixing state in the intake boat was tested. According to research, when the fuel injection angle is 23 degrees, the area where fuel is mixed is limited to a part of the upper part of the intake port, and the other area is mainly air and no fuel is mixed. On the other hand, when the fuel injection angle was 60', the fuel mixing area spread throughout the port, and it was confirmed that the mixing state was extremely good.

第6図には、本発明の第2実施例を示す。この実施例は
、燃料噴射弁1の先端部に貫通孔16を穿設した球形の
噴孔部移動部材(可変ノズル)15を回転可能に取付け
、該噴孔部移動部材15にピン17を介してロッド18
とピストン19とを装着し、更に、油圧が印加されない
とき又は油圧がドレンされたときにピストン19を元の
位置に戻すリターンスプリング20を設けたものである
FIG. 6 shows a second embodiment of the invention. In this embodiment, a spherical nozzle hole moving member (variable nozzle) 15 having a through hole 16 is rotatably attached to the tip of a fuel injection valve 1, and a pin 17 is connected to the nozzle hole moving member 15. Te rod 18
and a piston 19, and is further provided with a return spring 20 that returns the piston 19 to its original position when oil pressure is not applied or when oil pressure is drained.

高速回転時には、油圧をピストン19に掛け、噴孔部移
動部材15を回転させて、噴孔(貫通孔)16の指向方
向を高速側に切換える。低速回転時には油圧をOFF状
態としてリターンスプリング20によって噴孔部移動部
材15を元の位置に戻し、噴孔16の指向方向を低速側
に切換えることによって、高速及び低速相方の燃料と空
気との混合状態を良くする。
During high speed rotation, hydraulic pressure is applied to the piston 19 to rotate the nozzle hole moving member 15 and switch the direction of the nozzle hole (through hole) 16 to the high speed side. During low speed rotation, the oil pressure is turned off, the nozzle hole moving member 15 is returned to its original position by the return spring 20, and the orientation direction of the nozzle hole 16 is switched to the low speed side, thereby mixing the high speed and low speed partner fuel and air. improve the condition.

本実施例によれば、噴孔部移動部材15を球形に形成し
たので、噴孔指向方向の切換がよりスムースにできると
いう効果がある。
According to this embodiment, since the nozzle hole moving member 15 is formed into a spherical shape, there is an effect that the nozzle hole pointing direction can be switched more smoothly.

第7図には、本発明の第3実施例を示す。この実施例は
、燃料噴射弁1の先端部に低回転側燃料噴孔21と高回
転側燃料噴孔22と、これらの噴射穴21.22を開閉
する弁23と油圧がピストン24に掛らないときは、ピ
ストン24を元の位置に戻すリターンスプリング25と
を設けたもので、高速回転のときは油圧を両ピストン2
4,24に掛は低回転側燃料噴射穴21を弁23て閉じ
、高回転側燃料噴射穴22を開いて、燃料を高回転側燃
料噴射穴22から噴射する。低速回転のときは油圧をド
レインさせて高回転側燃料噴射穴22を閉じ低回転側燃
料噴射穴21を開いて燃料を低回転側燃料噴射穴21か
ら噴射する。本実施例によっても、前記各実施例と同様
の効果が得られる。
FIG. 7 shows a third embodiment of the invention. In this embodiment, a low rotation side fuel injection hole 21 and a high rotation side fuel injection hole 22 are provided at the tip of a fuel injection valve 1, a valve 23 opens and closes these injection holes 21 and 22, and hydraulic pressure is applied to a piston 24. A return spring 25 is provided to return the piston 24 to its original position when the piston 24 is not in use.
4 and 24, the low rotation side fuel injection hole 21 is closed by the valve 23, the high rotation side fuel injection hole 22 is opened, and fuel is injected from the high rotation side fuel injection hole 22. During low speed rotation, the oil pressure is drained to close the high rotation side fuel injection hole 22, open the low rotation side fuel injection hole 21, and inject fuel from the low rotation side fuel injection hole 21. This embodiment also provides the same effects as those of the embodiments described above.

発明の効果 本発明は以上説明したように構成されているので、以下
に記載する効果を奏する。
Effects of the Invention Since the present invention is configured as described above, it produces the effects described below.

エンジン回転速度に関係なく常に良好な燃料混合状態を
得ることができ、エンジン性能を大幅に向上させること
ができる。
A good fuel mixture condition can always be obtained regardless of the engine rotation speed, and engine performance can be greatly improved.

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

第1図は本発明の第1実施例を示す断面図、第2図は噴
孔の指向方向を切換える油圧制御のブロック図、第3図
は噴孔指向方向の切換による燃料噴射角の変化を示す説
明図、第4図は噴孔指向方向の切換ポイントを示す図、
第5図は燃料噴射角度をパラメータとしたエンジン回転
速度と出力、及びエンジン回転速度とHC排出量の関係
を示す図、第6図は本発明の第2実施例を示す断面図、
第7図は本発明の第3実施例を示す図である。 1・・燃料噴射弁、2・・・噴孔、3・・・噴孔部移動
部材、4・・・ピン、5・・・ロット、6・・・ピスト
ン、8・・リターンスプリング、10・・・コントロー
ルユニ。 ト、11・・ソレノイドバルブ、12・・・スプールバ
ルブ、15・・・噴孔部移動部材、16・−・貫通孔、
17−・−ピン、18・・・ロット、19・・・ピスト
ン、20・−リターンスプリング、21・・低回転側燃
料噴孔、22・・・高回転側燃料噴孔、23・・弁、2
4・・ピストン、25・・リターンスプリング。 第3図 第4図 エンレン回転数 6軒鳴引情な昧0関係 ■載J11
Fig. 1 is a cross-sectional view showing the first embodiment of the present invention, Fig. 2 is a block diagram of hydraulic control for switching the nozzle orifice orientation direction, and Fig. 3 shows the change in fuel injection angle due to the nozzle orifice orientation direction switching. FIG. 4 is a diagram showing the switching point of the nozzle orifice direction,
FIG. 5 is a diagram showing the relationship between engine speed and output using the fuel injection angle as a parameter, and the relationship between engine speed and HC emissions, FIG. 6 is a sectional view showing the second embodiment of the present invention,
FIG. 7 is a diagram showing a third embodiment of the present invention. DESCRIPTION OF SYMBOLS 1... Fuel injection valve, 2... Nozzle hole, 3... Nozzle hole part moving member, 4... Pin, 5... Lot, 6... Piston, 8... Return spring, 10... ...Control Uni. 11... Solenoid valve, 12... Spool valve, 15... Nozzle hole portion moving member, 16... Through hole,
17--Pin, 18--Rot, 19--Piston, 20--Return spring, 21--Low rotation side fuel nozzle hole, 22--High rotation side fuel nozzle hole, 23--Valve, 2
4. Piston, 25. Return spring. Fig. 3 Fig. 4 Enren rotational speed 6 ejaculate 0 relation ■ J11

Claims (1)

【特許請求の範囲】[Claims] (1)吸気管に装着した燃料噴射弁により燃料を供給す
る内燃機関の燃料噴射装置において、燃料噴射弁の噴孔
指向方向を可変としたことを特徴とする燃料噴射装置。
(1) A fuel injection device for an internal combustion engine that supplies fuel with a fuel injection valve attached to an intake pipe, characterized in that the orientation direction of the injection hole of the fuel injection valve is variable.
JP10727790A 1990-04-23 1990-04-23 Fuel injection device Pending JPH045469A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP10727790A JPH045469A (en) 1990-04-23 1990-04-23 Fuel injection device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP10727790A JPH045469A (en) 1990-04-23 1990-04-23 Fuel injection device

Publications (1)

Publication Number Publication Date
JPH045469A true JPH045469A (en) 1992-01-09

Family

ID=14454991

Family Applications (1)

Application Number Title Priority Date Filing Date
JP10727790A Pending JPH045469A (en) 1990-04-23 1990-04-23 Fuel injection device

Country Status (1)

Country Link
JP (1) JPH045469A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1997011270A1 (en) * 1995-09-21 1997-03-27 Robert Bosch Gmbh Fuel injection valve
US5785024A (en) * 1996-08-22 1998-07-28 Mitsubishi Jidosha Kogyo Kabushiki Kaisha Cylinder head device for internal combustion engine
US6206304B1 (en) 1999-01-13 2001-03-27 Toyota Jidosha Kabushiki Kaisha Injector
CN112253348A (en) * 2020-09-15 2021-01-22 东风汽车集团有限公司 Liquid fuel internal combustion engine and liquid fuel injection device thereof

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1997011270A1 (en) * 1995-09-21 1997-03-27 Robert Bosch Gmbh Fuel injection valve
US5819707A (en) * 1995-09-21 1998-10-13 Robert Bosch Gmbh Fuel injection valve
US5785024A (en) * 1996-08-22 1998-07-28 Mitsubishi Jidosha Kogyo Kabushiki Kaisha Cylinder head device for internal combustion engine
US6206304B1 (en) 1999-01-13 2001-03-27 Toyota Jidosha Kabushiki Kaisha Injector
CN112253348A (en) * 2020-09-15 2021-01-22 东风汽车集团有限公司 Liquid fuel internal combustion engine and liquid fuel injection device thereof

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