JPH0347465A - Fuel supply device for engine - Google Patents

Fuel supply device for engine

Info

Publication number
JPH0347465A
JPH0347465A JP1181420A JP18142089A JPH0347465A JP H0347465 A JPH0347465 A JP H0347465A JP 1181420 A JP1181420 A JP 1181420A JP 18142089 A JP18142089 A JP 18142089A JP H0347465 A JPH0347465 A JP H0347465A
Authority
JP
Japan
Prior art keywords
fuel
intake
combustion chamber
engine
suction
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
JP1181420A
Other languages
Japanese (ja)
Other versions
JP2756834B2 (en
Inventor
Masaaki Yoshikawa
雅明 吉川
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.)
Yamaha Motor Co Ltd
Original Assignee
Yamaha 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 Yamaha Motor Co Ltd filed Critical Yamaha Motor Co Ltd
Priority to JP1181420A priority Critical patent/JP2756834B2/en
Publication of JPH0347465A publication Critical patent/JPH0347465A/en
Application granted granted Critical
Publication of JP2756834B2 publication Critical patent/JP2756834B2/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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Abstract

PURPOSE:To enhance the performance of an engine by allowing a fuel injection valve to make two injections under the suction stroke intermittently, mixing the fuel with the air thoroughly in each divergent passage, and making uniform the mixing of fuel with the suction air in the combustion chamber. CONSTITUTION:Exhaust valves 24 and suction valves 12, 12' make opening/ closing motions one after another in the exhaust and suction strokes of an engine 1. In a short period centering on the suction valves 12, 12' making simultaneous valve opening motions, a fuel injection valve 19 injects the fuel as the first injecting run in the timing immediately before a piston 6 reaches the upper fulcrum, like the arrow A. With a small pause inserted, the injection valve 19 injects the fuel as the second injecting run before or after the piston 6 has reached the upper dead point, like the arrow B. Under low speed operation, on the other hand, a single mode injection is conducted as shown by the arrow C. This manner of two runs of injecting prevents the fuel from being injected concentratedly to the suction air which has unsatisfactory flow speed, and thus the engine performance is kept good.

Description

【発明の詳細な説明】 (産業上の利用分野) この発明は、複数の分岐通路を有する吸気通路に、燃料
を噴射する燃料噴射弁を備^たエンジンの燃料供給装置
に関する。
DETAILED DESCRIPTION OF THE INVENTION (Field of Industrial Application) The present invention relates to a fuel supply device for an engine that is equipped with a fuel injection valve that injects fuel into an intake passage having a plurality of branch passages.

(従来の技術) エンジンの吸気系には、吸入効率を高めるため、次のよ
うに構成されたものがある。
(Prior Art) Some engine intake systems are configured as follows in order to increase intake efficiency.

即ち、シリンダ内の燃焼室に連なる吸気通路がその中途
部から上記燃焼室に至る間で複数の分岐通路に分岐され
ている。また、上記燃焼室に開口する上記各分岐通路を
それぞれ開閉する吸気弁が設けられ、これら各吸気弁の
弁体が吸気カム軸に直交する方向で互いに偏位しており
、かつ、上記吸気通路に燃料を噴射する燃料噴射弁が設
けられている。
That is, an intake passage connected to a combustion chamber in the cylinder is branched into a plurality of branch passages from an intermediate portion thereof to the combustion chamber. Further, an intake valve is provided to open and close each of the branch passages opening into the combustion chamber, and the valve bodies of each of these intake valves are offset from each other in a direction perpendicular to the intake camshaft, and the intake passage A fuel injection valve is provided to inject fuel into the engine.

そして、上記各吸気弁が開弁じ、空気が吸気通路を通っ
て燃焼室に勢いよく吸入されるとき、燃料噴射弁により
噴射された燃料が上記吸入空気により撹乱、混合されて
混合気となり、これが燃焼室内に供給されて、ここで燃
焼させられるようになっている。
When each of the intake valves opens and air is forcefully sucked into the combustion chamber through the intake passage, the fuel injected by the fuel injection valve is disturbed and mixed by the intake air to form an air-fuel mixture. It is supplied into the combustion chamber and burned there.

(発明が解決しようとする問題点) ところで、上記各分岐通路は長さや形状が互いに異なる
ものであり、このため、これら分岐通路における吸入空
気の流動抵抗は互いに相違することとなっている。よっ
て、吸気弁が開弁じたときを基準時として、この基準時
から、分岐通路における吸入空気の流速が所定の速度に
到達するまでの時間(以下、これを単に到達時間という
)は各分岐通路で互いに相違することとなっている。
(Problems to be Solved by the Invention) Incidentally, each of the above-mentioned branch passages has a different length and shape, and therefore the flow resistance of the intake air in these branch passages is different from each other. Therefore, with the time when the intake valve opens as the reference time, the time from this reference time until the flow velocity of the intake air in the branch passage reaches a predetermined velocity (hereinafter simply referred to as arrival time) is the time for each branch passage. They are different from each other.

そして、この場合に、吸入空気に対し燃料を噴射すると
、上記到達時間が長い分岐通路においては、吸入空気の
流速が所定の速度に達する前に、この吸入空気と共に燃
料が燃焼室に供給されてしまうことがあり、この場合に
は、吸入空気と燃料との混合が不十分となって、エンジ
ン性能の向上が阻害されるおそれを生じる。
In this case, when fuel is injected into the intake air, the fuel is supplied to the combustion chamber together with the intake air before the flow velocity of the intake air reaches a predetermined speed in the branch passage where the arrival time is long. In this case, the intake air and fuel may not be sufficiently mixed, which may impede improvement in engine performance.

そこで、到達時間が長い分岐通路において、吸入空気の
流速が所定の速度に達したのを見計らってから燃料を噴
射させ、いずれの分岐通路においても、吸入空気に燃料
を十分に混合させることが考えられる。
Therefore, one idea is to inject fuel after the flow velocity of intake air reaches a predetermined speed in the branch passages where the arrival time is long, so that the fuel is sufficiently mixed with the intake air in both branch passages. It will be done.

しかし、このようにすると、燃焼室に吸入される当初の
吸入空気には燃料が混合されないことから、燃焼室にお
ける吸入空気と燃料との混合が不均一となって好ましく
ない。
However, if this is done, the fuel is not mixed with the initial intake air taken into the combustion chamber, which is undesirable because the mixture of the intake air and fuel in the combustion chamber becomes non-uniform.

(発明の目的) この発明は、上記のような事情に注目してなされたもの
で、各分岐通路における吸入空気に対し、燃料ができる
だけ十分に混合されるようにし、しかも、燃焼室におい
て吸入空気と燃料の混合が均一になされるようにして、
エンジン性能を向上させることを目的とする。
(Object of the Invention) This invention has been made with attention to the above-mentioned circumstances, and it is possible to mix fuel as thoroughly as possible with the intake air in each branch passage, and to prevent the intake air from entering the combustion chamber. and fuel are evenly mixed,
The purpose is to improve engine performance.

(発明の構成) 上記目的を達成するためのこの発明の特徴とするところ
は、吸入行程で、上記燃料噴射弁が断続的に皿回噴射す
るようにした点にある。
(Structure of the Invention) A feature of the present invention for achieving the above object is that the fuel injection valve intermittently performs counter-injection during the intake stroke.

(作 用) 上記構成による作用は次の如くである。(for production) The effects of the above configuration are as follows.

吸入行程で、燃料噴射弁19が断続的に皿回噴射するよ
うにしたため、到達時間の短い分岐通路11では、第一
回目の噴射で吸入空気に噴射された燃料は、この吸入空
気に十分に混合されて燃焼室7に供給される。また、こ
の際、到達時間の長い分岐通路11′では、吸入空気の
速度が不十分のために、吸入空気への燃料の混合は十分
とはいえ・ないおそれがある、しかし、この第一回目の
噴射によって、燃焼室7に吸入される当初の吸入空気に
も所定量の燃料が混合されることとなり、このため、そ
の後の第二回目の噴射とにより、燃焼室7において吸入
空気と燃料との混合が不均一になることは防止される。
In the intake stroke, the fuel injection valve 19 intermittently injects counterclockwise, so in the branch passage 11 where the arrival time is short, the fuel injected into the intake air in the first injection is sufficiently absorbed into the intake air. The mixture is mixed and supplied to the combustion chamber 7. In addition, at this time, in the branch passage 11' where the arrival time is long, the velocity of the intake air is insufficient, so the mixing of fuel into the intake air may not be sufficient. Due to this injection, a predetermined amount of fuel is mixed with the initial intake air taken into the combustion chamber 7, and therefore, with the subsequent second injection, the intake air and fuel are mixed in the combustion chamber 7. Non-uniform mixing is prevented.

しかも、第二回目の噴射時には、到達時間の長い分岐通
路11’でも吸入空気が所定の速度に達するため、この
ときには、いずれの分岐通路11.11’においても、
吸入空気に燃料が十分に混合され、この状態で燃焼室7
に供給されることとなる。
Moreover, at the time of the second injection, the intake air reaches a predetermined speed even in the branch passage 11' which takes a long time to reach, so at this time, in either branch passage 11.11',
The fuel is sufficiently mixed with the intake air, and in this state the combustion chamber 7
It will be supplied to

(実施例) 以下、この発明の実施例を図面により説明する。(Example) Embodiments of the present invention will be described below with reference to the drawings.

第1図と第2図において、1は自動車に搭載される4サ
イクルエンジンで、このエンジン1のシリンダ2が並設
されてシリンダブロック3が構成され、このシリンダブ
ロック3上にシリンダヘッド4が取り付けられ、上記シ
リンダ2にはクランク軸に連結されるピストン6が上下
摺動自在に嵌入されている。そして、上記シリンダブロ
ック3、シリンダヘッド4.およびピストン6で囲まれ
た空間が燃焼室7となっており、この燃焼室7のほぼ中
心に臨む点火プラグ7aが設けられている。
In FIGS. 1 and 2, 1 is a four-stroke engine installed in a car, cylinders 2 of this engine 1 are arranged side by side to form a cylinder block 3, and a cylinder head 4 is mounted on this cylinder block 3. A piston 6 connected to a crankshaft is fitted into the cylinder 2 so as to be vertically slidable. Then, the cylinder block 3, cylinder head 4. A space surrounded by the piston 6 is a combustion chamber 7, and an ignition plug 7a facing approximately the center of the combustion chamber 7 is provided.

上記シリンダヘッド4の左側(第1図に向っての方向を
いい、以下同じとする)には、サージタンク8から上記
燃焼室7に連なる吸気通路9が形成されている。この吸
気通路9はサージタンク8に連なる主通路10と、この
主通路10から燃焼室7に向って分岐する三本の分岐通
路11.11′とで形成され、これら分岐通路11.1
1’のうち中間の分岐通路11は平面視(第2図)で主
通路lOの延長線上に位置し、燃焼室7の中心に向って
延びている。また、両側の分岐通路11.11’は中間
の分岐通路11を挟んでほぼ対称形をなし、いずれも燃
焼室7の側部に向って延びている。
An intake passage 9 is formed on the left side of the cylinder head 4 (referring to the direction as viewed in FIG. 1, hereinafter referred to as the same), which extends from the surge tank 8 to the combustion chamber 7. This intake passage 9 is formed of a main passage 10 connected to the surge tank 8, and three branch passages 11.11' branching from this main passage 10 toward the combustion chamber 7.
The middle branch passage 11 of the combustion chamber 1' is located on an extension of the main passage 1O in plan view (FIG. 2) and extends toward the center of the combustion chamber 7. Further, the branch passages 11 and 11' on both sides are substantially symmetrical with the intermediate branch passage 11 in between, and both extend toward the side of the combustion chamber 7.

上記分岐通路11.11’が燃焼室7に開口する分岐ボ
ート11a、11a’は互いに同径であり、これらは、
燃焼室7の左側上面でシリンダ2軸心のほぼ周方向に並
設されている。このため、中間の分岐通路11よりも両
側の分岐通路11’、11’は長さが長くなっている。
The branch boats 11a and 11a' in which the branch passages 11 and 11' open into the combustion chamber 7 have the same diameter, and these
They are arranged in parallel on the left upper surface of the combustion chamber 7 in the substantially circumferential direction of the two cylinder axes. For this reason, the branch passages 11', 11' on both sides are longer in length than the branch passage 11 in the middle.

また、上記各分岐ボート11a、11a  を開閉する
吸気弁12.12’が設けられ、かつ、同上各分岐ポー
ト11a、11a’を閉じるように吸気弁12.12’
を付勢するばね14が設けられている。
Further, an intake valve 12.12' is provided to open and close each branch port 11a, 11a, and an intake valve 12.12' is provided to open and close each branch port 11a, 11a'.
A spring 14 is provided to bias the .

上記シリンダヘッド4の上部に形成されたカム室15に
は前記クランク軸に連動する吸気カム軸16が設けられ
ている。この吸気カム軸16は上記吸気弁12,1.2
’の上端側とカム係合し、クランク軸に同期してこれら
吸気弁12.12’をばね14に抗し適宜開弁させる。
A cam chamber 15 formed in the upper part of the cylinder head 4 is provided with an intake camshaft 16 that interlocks with the crankshaft. This intake camshaft 16 is connected to the intake valves 12, 1.2.
The cam engages with the upper end side of the intake valve 12, 12', and opens the intake valves 12, 12' appropriately against the spring 14 in synchronization with the crankshaft.

なお、この際、これら吸気弁12.12’は互いに同時
に開、閉弁するようになっている。
At this time, these intake valves 12 and 12' are opened and closed at the same time.

ところで、上記したように各吸気弁12.12′は同時
に開、閉弁するが、前記したように中間の分岐通路11
よりも両側の分岐通路11’11′の方が長さが長いこ
とから、中間の分岐通路11では前記到達時間は短く、
これに比べて両側の各分岐通路11’では到達時間が長
くなっている。
By the way, as mentioned above, each intake valve 12, 12' opens and closes at the same time, but as mentioned above, the intermediate branch passage 11
Since the branch passages 11' and 11' on both sides are longer in length, the arrival time is shorter in the intermediate branch passage 11.
In comparison, the arrival time is longer in each of the branch passages 11' on both sides.

上記吸気通路9に燃料を噴出する燃料噴射弁19が設け
られる。この燃料噴射弁19は三つの噴射孔を有し、中
間の燃料噴射方向19aは側面視(第1図)で、燃焼室
7の上面において、中間の分岐ボートl laの孔心と
、両側の分岐ボートlla’の孔心との間を通り、かつ
、平面視(第2図)で、中間の分岐ボートl laの孔
心と交差している。また、両側の燃料噴射方向19a、
19a は側面視(第1図)では、上記中間の燃料噴射
方向19aと同じ方向に向っているが、平面視(第2図
)では、両側の分岐ボートlla’の孔心と交差してい
る。
A fuel injection valve 19 is provided to inject fuel into the intake passage 9. This fuel injection valve 19 has three injection holes, and the middle fuel injection direction 19a is located at the hole center of the middle branch boat lla and on both sides on the upper surface of the combustion chamber 7, as seen from the side view (Fig. 1). It passes between the hole center of the branch boat lla' and intersects with the hole center of the intermediate branch boat lla in plan view (FIG. 2). Further, fuel injection directions 19a on both sides,
19a is oriented in the same direction as the intermediate fuel injection direction 19a in side view (Fig. 1), but in plan view (Fig. 2), it intersects with the hole center of the branch boat lla' on both sides. .

一方、前記シリンダヘッド4の右側には燃焼室7を外部
に連通させる一対の排気ボート23.23が形成される
。これら各排気ポート23を開閉する排気弁24.24
が設けられ、上記各排気ポート23を閉じる排気弁24
を付勢するばね25が設けられている。また、前記カム
室15には前記クランク軸に連動する排気カム軸26が
設けられている。この排気カム軸26は上記各排気弁2
4の上端側とカム係合し、クランク軸に同期してこれら
排気弁24をばね25に抗し適宜開弁させる。
Meanwhile, a pair of exhaust boats 23 and 23 are formed on the right side of the cylinder head 4 to communicate the combustion chamber 7 with the outside. Exhaust valves 24 and 24 that open and close each of these exhaust ports 23
An exhaust valve 24 is provided to close each exhaust port 23.
A spring 25 is provided to bias the . Further, the cam chamber 15 is provided with an exhaust camshaft 26 that is interlocked with the crankshaft. This exhaust camshaft 26 is connected to each exhaust valve 2 mentioned above.
4, and opens these exhaust valves 24 appropriately against a spring 25 in synchronization with the crankshaft.

第3図において、エンジンlの排気、吸入行程では各排
気弁24と、各吸気弁12.12’とが、順次、開閉弁
動作を行う、そして、各吸気弁12.12’が同時に開
弁動作する直前から直後にかけ、かつ、ピストン6が上
死点に達する直前で、図中矢印Aで示すように、燃料噴
射弁19が第一回の噴射として燃料を噴射する。そして
、これかられずかの休止期間tをおき、かつ、ピストン
6が上死点に達した前後で、図中矢印Bで示すように同
上燃料噴射弁19が第二回の噴射として燃料を噴射する
In FIG. 3, during the exhaust and intake strokes of the engine I, each exhaust valve 24 and each intake valve 12.12' sequentially open and close, and each intake valve 12.12' simultaneously opens. From immediately before to immediately after the operation, and immediately before the piston 6 reaches the top dead center, the fuel injection valve 19 injects fuel as a first injection, as shown by arrow A in the figure. Then, after some rest period t, and before and after the piston 6 reaches the top dead center, the fuel injection valve 19 injects fuel as a second injection as shown by arrow B in the figure. .

一方、低速回転時には、図中矢印Cで示すように単一の
噴射のみが行われるようになっており、この噴射時期や
期間は上記第一回の噴射とほぼ一致している。なお、こ
の低速回転時にも、高速回転時と同じく、燃料を皿回噴
射させてもよい。
On the other hand, during low-speed rotation, only a single injection is performed as shown by arrow C in the figure, and the timing and period of this injection almost coincide with the first injection. Note that during this low-speed rotation, the fuel may be injected counterclockwise as well as during high-speed rotation.

また、上記の場合、高、低速回転時にかかわらず、燃料
噴射弁19の噴射時期や噴射期間、および休止期間tは
クランク軸に連動する電子制御装置で任意に調整される
ようになっている。
Further, in the above case, regardless of whether the engine is rotating at high or low speed, the injection timing, injection period, and rest period t of the fuel injection valve 19 are arbitrarily adjusted by an electronic control device linked to the crankshaft.

上記実施例によれば、次の効果がある。即ち、高速回転
時には、各分岐通路11.11’における吸入空気の流
速は大きく変動し易いものである。しかし、上記実施例
によれば、皿回噴射のため、流速が不十分な吸入空気に
対し集中的に燃料を噴射してしまうことは防止される。
According to the above embodiment, there are the following effects. That is, during high-speed rotation, the flow velocity of the intake air in each branch passage 11, 11' tends to fluctuate greatly. However, according to the above-mentioned embodiment, because of the countersunk injection, it is possible to prevent the fuel from being intensively injected into the intake air whose flow velocity is insufficient.

つまり、吸入空気の流速が変動していても、吸入空気と
燃料との混合は平均化され、この混合が不十分になって
しまうことは防止され、よって、エンジン性能は良好に
保たれる。
In other words, even if the flow velocity of the intake air fluctuates, the mixture of the intake air and fuel is averaged, and insufficient mixing is prevented, thereby maintaining good engine performance.

第4図は、他の実施例を示している。FIG. 4 shows another embodiment.

これによれば、中間の吸気弁12よりも両側の吸気弁1
2’、12’の方が開、閉弁時期が早められている。
According to this, the intake valves 1 on both sides are
2' and 12' have earlier opening and closing timings.

また、低速回転時における噴射は第一回の噴射の中途部
から始り、第二回の噴射の中途部で終了するようになっ
ている。
Furthermore, injection during low-speed rotation starts in the middle of the first injection and ends in the middle of the second injection.

他の構成や作用は、前記実施例と同様である。Other configurations and operations are similar to those of the previous embodiment.

なお、以上は図示の例によるが、分岐ポート11a、1
1a’は二つでも、四つであってもよい。
Note that although the above is based on the illustrated example, the branch ports 11a, 1
1a' may be two or four.

(発明の効果) この発明によれば、シリンダ内の燃焼室に連なる吸気通
路を、その中途部から上記燃焼室に至る間で複数の分岐
通路に分岐し、燃焼室に開口する上記各分岐通路の分岐
ボートをそれぞれ開閉する吸気弁を設け、これら各吸気
弁の弁体を吸気カム軸に直交する方向で互いに偏位させ
、上記吸気通路に燃料を噴射する燃料噴射弁を設けたエ
ンジンにおいて、吸入行程で、上記燃料噴射弁が断続的
に皿回噴射するようにしたため、到達時間の短い分岐通
路では、第一回目の噴射で吸入空気に噴射された燃料は
、この吸入空気に十分に混合されて燃焼室に供給される
。また、この際、到達時間の長い分岐通路では、吸入空
気の速度が不十分のために、吸入空気への燃料の混合は
十分とはいえないおそれがある。しかし、この第一回目
の噴射によって、燃焼室に吸入される当初の吸入空気に
も所定量の燃料が混合されることとなり、このため、そ
の後の第二回目の噴射とにより、燃焼室において吸入空
気と燃料との混合が不均一になることは防止される。
(Effects of the Invention) According to the present invention, the intake passage connected to the combustion chamber in the cylinder is branched into a plurality of branch passages from its midpoint to the combustion chamber, and each of the branch passages opens into the combustion chamber. In an engine that is provided with intake valves that open and close branch boats, the valve bodies of these intake valves are offset from each other in a direction perpendicular to the intake camshaft, and a fuel injection valve that injects fuel into the intake passage, During the intake stroke, the fuel injection valve injects intermittently in countersunk injections, so in the branch passage where the arrival time is short, the fuel injected into the intake air during the first injection is sufficiently mixed with this intake air. and supplied to the combustion chamber. Further, in this case, in the branch passage where the arrival time is long, the velocity of the intake air is insufficient, so there is a possibility that the mixing of fuel into the intake air is not sufficient. However, due to this first injection, a predetermined amount of fuel is mixed with the initial intake air that is drawn into the combustion chamber, and therefore, due to the subsequent second injection, the intake air is injected into the combustion chamber. Non-uniform mixing of air and fuel is prevented.

しかも、第二回目の噴射時には、到達時間の長い分岐通
路でも吸入空気が所定の速度に達するため、このときに
は、いずれの分岐通路においても、吸入空気に燃料が十
分に混合され、この状態で、燃焼室に供給されることと
なる。
Moreover, during the second injection, the intake air reaches a predetermined speed even in the branch passages that take a long time to reach, so at this time, fuel is sufficiently mixed with the intake air in any of the branch passages, and in this state, It will be supplied to the combustion chamber.

よって、上記燃焼室における吸入空気と燃料との混合は
全体として、十分、かつ、均一になされることとなり、
エンジン性能の向上が達成される。
Therefore, the intake air and fuel are mixed sufficiently and uniformly in the combustion chamber as a whole.
Improved engine performance is achieved.

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

図はこの発明の実施例を示し、第1図は全体側面断面図
、第2図は簡略平面図、第3図はグラフ図、第4図は他
の実施例で、第3図に相当する図である。 ■・・エンジン、2・・シリンダ、7・・燃焼室、9・
・吸気通路、11.11’  ・・分岐通路、12.1
2’  ・・吸気弁、19・・燃料噴射弁。
The figures show an embodiment of the invention, in which Fig. 1 is an overall side sectional view, Fig. 2 is a simplified plan view, Fig. 3 is a graph, and Fig. 4 is another embodiment, which corresponds to Fig. 3. It is a diagram. ■...Engine, 2...Cylinder, 7...Combustion chamber, 9...
・Intake passage, 11.11' ・Branch passage, 12.1
2'...Intake valve, 19...Fuel injection valve.

Claims (1)

【特許請求の範囲】[Claims] 1、シリンダ内の燃焼室に連なる吸気通路を、その中途
部から上記燃焼室に至る間で複数の分岐通路に分岐し、
燃焼室に開口する上記各分岐通路をそれぞれ開閉する吸
気弁を設け、これら各吸気弁の弁体を吸気カム軸に直交
する方向で互いに偏位させ、上記吸気通路に燃料を噴射
する燃料噴射弁を設けたエンジンにおいて、吸入行程で
、上記燃料噴射弁が断続的に二回噴射するようにしたエ
ンジンの燃料供給装置。
1. An intake passage connected to a combustion chamber in a cylinder is branched into a plurality of branch passages from an intermediate part thereof to the combustion chamber,
A fuel injection valve that includes intake valves that open and close the branch passages that open into the combustion chamber, and that injects fuel into the intake passage by deviating the valve bodies of the intake valves from each other in a direction perpendicular to the intake camshaft. A fuel supply device for an engine, wherein the fuel injection valve intermittently injects twice during the intake stroke.
JP1181420A 1989-07-12 1989-07-12 Engine fuel supply Expired - Fee Related JP2756834B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP1181420A JP2756834B2 (en) 1989-07-12 1989-07-12 Engine fuel supply

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP1181420A JP2756834B2 (en) 1989-07-12 1989-07-12 Engine fuel supply

Publications (2)

Publication Number Publication Date
JPH0347465A true JPH0347465A (en) 1991-02-28
JP2756834B2 JP2756834B2 (en) 1998-05-25

Family

ID=16100458

Family Applications (1)

Application Number Title Priority Date Filing Date
JP1181420A Expired - Fee Related JP2756834B2 (en) 1989-07-12 1989-07-12 Engine fuel supply

Country Status (1)

Country Link
JP (1) JP2756834B2 (en)

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS6290937U (en) * 1985-11-26 1987-06-10
JPS6411367U (en) * 1987-07-11 1989-01-20

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS6290937U (en) * 1985-11-26 1987-06-10
JPS6411367U (en) * 1987-07-11 1989-01-20

Also Published As

Publication number Publication date
JP2756834B2 (en) 1998-05-25

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