JPH0231570Y2 - - Google Patents

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Publication number
JPH0231570Y2
JPH0231570Y2 JP1985034717U JP3471785U JPH0231570Y2 JP H0231570 Y2 JPH0231570 Y2 JP H0231570Y2 JP 1985034717 U JP1985034717 U JP 1985034717U JP 3471785 U JP3471785 U JP 3471785U JP H0231570 Y2 JPH0231570 Y2 JP H0231570Y2
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JP
Japan
Prior art keywords
fuel
injection
passages
passage
cross
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.)
Expired
Application number
JP1985034717U
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Japanese (ja)
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JPS61152765U (en
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Filing date
Publication date
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Priority to JP1985034717U priority Critical patent/JPH0231570Y2/ja
Priority to US06/838,290 priority patent/US4657189A/en
Publication of JPS61152765U publication Critical patent/JPS61152765U/ja
Application granted granted Critical
Publication of JPH0231570Y2 publication Critical patent/JPH0231570Y2/ja
Expired legal-status Critical Current

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Description

【考案の詳細な説明】 [産業上の利用分野] 本考案は、吸気バルブを複数個持つ多弁型エン
ジンで用いられる、噴射燃料通路を複数個持つ、
電磁制御式燃料噴射弁の構造に関する。
[Detailed Description of the Invention] [Industrial Field of Application] The present invention has a plurality of injection fuel passages, which is used in a multi-valve engine having a plurality of intake valves.
This invention relates to the structure of an electromagnetically controlled fuel injection valve.

[従来の技術] 1気筒に吸気弁を2個有し、吸気通路が吸気弁
近傍において隔壁により互いに仕切られている分
流吸気通路部分を有する複吸気弁エンジンにおい
て、電磁制御式の燃料噴射システムを採用する場
合、吸気通路を2系統に独立させて各々の系統の
燃料噴射弁を各分流吸気通路部分に取付けるなら
ば、燃料噴射弁の取付け数および噴射系統が通常
のエンジンにくらべて2倍になり、大幅なコスト
アツプは避けられない。
[Prior Art] An electromagnetically controlled fuel injection system is used in a dual intake valve engine that has two intake valves in one cylinder and has a branch intake passage section in which the intake passage is separated from each other by a partition wall near the intake valve. If adopted, if the intake passage is separated into two systems and the fuel injection valves of each system are installed in each branch intake passage, the number of installed fuel injectors and the injection system will be doubled compared to a normal engine. Therefore, a significant increase in costs is unavoidable.

これに対し、一つの燃料噴射弁に複数の燃料噴
孔を設けた構造が知られている(たとえば実開昭
52−170123号公報)。この装置においては、噴射
される燃料の計量を複数の燃料噴孔でそれぞれ行
つていたが、各々の燃料噴孔を、仕様の噴射量に
なるように精度良く加工する必要があり、燃料噴
孔が1つの従来弁に比べ、倍以上の加工時間がか
かる、加工方法が難しい等によるコストアツプに
なるという問題がある。
On the other hand, a structure in which a single fuel injection valve is provided with multiple fuel injection holes is known (for example,
52-170123). In this device, the amount of fuel to be injected was measured through multiple fuel injection holes, but each fuel injection hole had to be precisely machined to achieve the specified injection amount. Compared to conventional valves with one hole, there are problems in that the machining time is more than twice as long and the machining method is difficult, resulting in increased costs.

この問題を軽減するために、本出願人により、
先に第6図に示すような、噴射燃料をメータリン
グ(計量)する一つの燃料噴孔21と、該燃料噴
孔21の下流側に位置し、燃料噴孔21からの燃
料を分岐させて出口から噴射する複数の噴射燃料
通路22a,22bと、該噴射燃料通路と前記燃
料噴孔との間に位置する噴射燃料通路の合流部2
3とを有する電磁制御式燃料噴射弁において、前
記合流部23を、該合流部23からの燃料を各噴
射燃料通路22a,22bに分岐させる燃料分岐
部24の頂部25を通る各噴射燃料通路軸芯26
a,26bと直角の各噴射燃料通路断面の、各方
向の外周間距離と同等かそれ以上の内壁間寸法
D′(第7図参照)を有する任意断面形状の通路に
形成し、かつ合流部23の弁軸芯と直角方向の断
面積を、燃料噴孔21から燃料分岐部24の頂部
25までの間一定にした電磁制御式燃料噴射弁が
提案されている(実願昭59−183167号)。なお、
このような電磁制御式燃料噴射弁は実開昭58−
123660号公報にも開示されている。
In order to alleviate this problem, the applicant:
As shown in FIG. 6, there is one fuel injection hole 21 for metering the injected fuel, and a fuel injection hole 21 located downstream of the fuel injection hole 21 to branch the fuel from the fuel injection hole 21. A confluence section 2 of a plurality of injection fuel passages 22a and 22b injecting fuel from the outlet and an injection fuel passage located between the injection fuel passages and the fuel injection hole.
In the electromagnetically controlled fuel injection valve having the above-mentioned merging portion 23, each injected fuel passage axis passes through the top portion 25 of the fuel branching portion 24 that branches the fuel from the merging portion 23 into each injection fuel passage 22a, 22b. Core 26
A dimension between inner walls that is equal to or greater than the distance between the outer circumferences in each direction of each injection fuel passage cross section perpendicular to a and 26b.
D′ (see FIG. 7), and the cross-sectional area of the merging portion 23 in the direction perpendicular to the valve axis is set between the fuel injection hole 21 and the top 25 of the fuel branching portion 24. An electromagnetically controlled fuel injection valve with constant fuel pressure has been proposed (Utility Application No. 59-183167). In addition,
This type of electromagnetically controlled fuel injection valve was first developed in 1982.
It is also disclosed in Publication No. 123660.

上記提案の電磁制御式燃料噴射弁においては、
メータリングを行なう燃料噴孔21の下流側に位
置する、噴射燃料通路22a,22bの合流部2
3への開口断面が、第7図に示すように2つの楕
円を重ねたような形になり、交差部に突き出た部
分27ができるため、燃料付着を避けるため、突
き出た部分27を合流部23の形成時に削除して
いた。
In the electromagnetically controlled fuel injection valve proposed above,
Merging section 2 of injection fuel passages 22a and 22b located downstream of fuel injection hole 21 where metering is performed
As shown in Figure 7, the cross section of the opening to 3 is shaped like two ellipses overlapped, and a protruding part 27 is formed at the intersection, so to avoid fuel adhesion, the protruding part 27 is placed at the confluence. It was deleted when the 23rd was formed.

[考案が解決しようとする問題点] しかし、この場合つぎの問題があつた。すなわ
ち、既提案のものは合流部23の深さを規定して
いなかつたので、加工条件によつては、または加
工精度の誤差によつて、燃料分岐部24の頂部2
5が必ずしも尖つた頂角にならず、第8図に示す
ように平坦部28ができる場合があり、この場
合、燃料噴孔21から出た燃料が平坦部28では
じかれ、噴射方向性、左右噴射燃料通路22a,
22bへの燃料分配が悪化する。
[Problem that the invention aims to solve] However, in this case, the following problem occurred. That is, since the existing proposal did not specify the depth of the merging portion 23, depending on the machining conditions or due to errors in machining accuracy, the top 2 of the fuel branch portion 24 may
5 does not necessarily have a sharp apex angle, and a flat portion 28 may be formed as shown in FIG. Left and right injection fuel passages 22a,
Fuel distribution to 22b deteriorates.

本考案は、このような問題を解消するために、
燃料分岐部の頂部に必ず尖つたエツジ状の部分が
残るようにし、これによつて燃料噴射角、左右通
路への燃料分配を設定値通りにすることを目的と
する。
In order to solve these problems, this invention
The purpose is to ensure that a sharp edge-shaped portion remains at the top of the fuel branch, thereby adjusting the fuel injection angle and fuel distribution to the left and right passages as set values.

[問題点を解決するための手段] この目的は、本考案によれば、次の電磁制御式
燃料噴射弁によつて、達成される。すなわち、 燃料を計量する燃料噴孔が、弁軸芯と同芯状
に、1つだけ設けられており; 前記燃料噴孔より下流側に、通路断面積が通路
長手方向に一定とされた噴射燃料通路が、該噴射
燃料通路の上流側部分が下流側部分よりも前記弁
軸芯に近づく傾きをもつて前記弁軸芯に対して傾
けられて、複数個、設けられており; 前記燃料噴孔と前記噴射燃料通路との間には、
合流部が、複数の前記噴射燃料通路の前記合流部
への開口断面を包絡する形状かそれより大の断面
形状状をもつて該断面形状を前記弁軸芯に沿う方
向に一定にして、設けられており、; 複数の前記噴射燃料通路の間には、燃料が前記
燃料噴孔から噴射されて前記合流部を飛行してき
たときに該燃料を複数の前記噴射燃料通路に分配
する燃料分岐部が形成されている; 電磁制御式燃料噴射弁において; 複数の前記噴射燃料通路は、前記弁軸芯に対す
る傾きを、複数の噴射燃料通路の間に形成される
前記燃料分岐部がその頂部に、複数の前記噴射燃
料通路の壁面の重複する交わりによつて形成され
る上方に向つて尖つたエツジ部を有するように、
定められており; 前記合流部は、前記燃料分岐部頂部の前記弁軸
芯上で前記燃料噴孔に対向する部位から、上流側
に隔てられて形成されており、この隔てた形成に
よつて前記燃料分岐部頂部に、前記合流部の形成
において削りとられないエツジ部が前記燃料噴孔
に対向する部位に残されている、 ことを特塚徴とする電磁制御式燃料噴射弁。
[Means for Solving the Problems] According to the present invention, this object is achieved by the following electromagnetically controlled fuel injection valve. That is, only one fuel nozzle hole for metering fuel is provided concentrically with the valve shaft; downstream of the fuel nozzle hole, there is an injection hole whose passage cross-sectional area is constant in the longitudinal direction of the passage. A plurality of fuel passages are provided and are inclined with respect to the valve axis such that an upstream portion of the injection fuel passage is closer to the valve axis than a downstream portion; Between the hole and the injection fuel passage,
The merging portion has a cross-sectional shape that envelops the opening cross section of the plurality of injected fuel passages to the merging portion, or has a larger cross-sectional shape, and is provided so that the cross-sectional shape is constant in the direction along the valve axis. a fuel branching section between the plurality of injection fuel passages that distributes the fuel to the plurality of injection fuel passages when the fuel is injected from the fuel injection hole and flies through the merging section; In the electromagnetically controlled fuel injection valve, the plurality of injected fuel passages are inclined with respect to the valve axis, and the fuel branch portion formed between the plurality of injected fuel passages is formed at the top thereof; having an upwardly pointed edge portion formed by overlapping intersections of the wall surfaces of the plurality of injection fuel passages;
The merging portion is formed so as to be separated upstream from a portion facing the fuel injection hole on the valve axis at the top of the fuel branching portion, and due to this separated formation. An electromagnetically controlled fuel injection valve characterized in that an edge portion that is not cut away in forming the merging portion is left at a top portion of the fuel branching portion at a portion facing the fuel injection hole.

[作用] 上記構成の燃料噴射弁においては、合流部が、
噴射燃料通路の壁面の重複する交わりによつて形
成される頂部のエツジ部の燃料噴孔対向部位より
上流側に隔てて形成されているので、燃料分岐部
の頂部の燃料噴孔対向部には必ずエツジ部が残
り、燃料分岐部頂部に平坦部は形成されない。
[Operation] In the fuel injection valve having the above configuration, the merging portion is
Since it is formed upstream from the fuel nozzle hole facing portion of the top edge portion formed by the overlapping intersection of the wall surfaces of the injection fuel passage, the fuel nozzle hole facing portion of the top of the fuel branch portion is An edge portion always remains and no flat portion is formed at the top of the fuel branch.

したがつて、従来のように平坦な頂部によつて
燃料がはじかれるようなこともなく、本考案では
尖つた頂部によつて燃料は複数の噴射燃料通路に
本質的に均等に分配される。
Therefore, instead of the fuel being repelled by the flat top as in the prior art, the pointed top essentially distributes the fuel evenly among the plurality of injection fuel passages.

[実施例] 以下に本考案に係る電磁制御式燃料噴射弁の望
ましい実施例を図面を参照して説明する。
[Embodiments] Preferred embodiments of the electromagnetically controlled fuel injection valve according to the present invention will be described below with reference to the drawings.

第1図ないし第5図は、本考案に係る電磁制御
式燃料噴射弁を示している。
1 to 5 show an electromagnetically controlled fuel injection valve according to the present invention.

まず、第5図は、電磁制御式燃料噴射弁1全体
を示している。電磁制御式燃料噴射弁1の先端部
には、燃料供給通路2からの燃料を計量する1つ
の燃料噴孔3が弁軸芯と同芯状に設けられてお
り、燃料噴孔3への燃料を制御するために、第1
図に示すように、ボール4と曲面状の内壁面5に
よりシート部6が構成されている。
First, FIG. 5 shows the entire electromagnetically controlled fuel injection valve 1. As shown in FIG. At the tip of the electromagnetically controlled fuel injection valve 1, one fuel injection hole 3 for metering the fuel from the fuel supply passage 2 is provided concentrically with the valve axis. In order to control
As shown in the figure, a seat portion 6 is constituted by a ball 4 and a curved inner wall surface 5.

燃料噴孔3の下流側に対応させて、アダプダ7
が取付けられており、アダプダ7には、第1図に
示すように、燃料噴孔3からの燃料を分流させて
出口から噴射する、複数の(図示例では2つの)
任意形状断面の、ただし通路長手方向には断面形
状を一定とされた、噴射燃料通路8a,8bと、
該噴射燃料通路8a,8bと燃料噴孔3との間に
位置する噴射燃料通路の合流部9が設けられてい
る。噴射燃料通路8a,8bは、本実施例では断
面円状に形成されている。噴射燃料通路8a,8
bは、その上流部分が下流部分より弁軸芯に近づ
くような傾きをもつて弁軸芯に対して傾けられて
おり、合流部9より下流側において、噴射燃料通
路8a,8bの間に形成された断面逆V字状の燃
料分岐部10によつて、その軸芯11a,11b
が所定の開き角αになるように、分岐されてい
る。噴射燃料通路8a,8bの弁軸芯に対する傾
き(噴射燃料通路8a,8bが2個の場合は傾き
角はα/2)は、燃料分岐部10の頂部12に、
噴射燃料通路8a,8bの壁面の重複する交わり
によつて形成される(したがつて、少なくとも、
ある長さの陵線を有するように形成される)、上
方に向つて尖つたエツジ部が形成されるように、
定められている。
The adapter 7 corresponds to the downstream side of the fuel injection hole 3.
As shown in FIG. 1, the adapter 7 is equipped with a plurality of (two in the illustrated example) which divides the fuel from the fuel nozzle hole 3 and injects it from the outlet.
injection fuel passages 8a and 8b having arbitrary cross-sectional shapes, but having a constant cross-sectional shape in the longitudinal direction of the passages;
A confluence portion 9 of the injection fuel passages is provided between the injection fuel passages 8a, 8b and the fuel injection holes 3. In this embodiment, the injection fuel passages 8a and 8b are formed to have a circular cross section. Injection fuel passages 8a, 8
b is inclined with respect to the valve shaft center such that the upstream portion thereof is closer to the valve shaft center than the downstream portion, and is formed between the injection fuel passages 8a and 8b on the downstream side of the confluence portion 9. The fuel branch part 10, which has an inverted V-shaped cross section, allows its axes 11a and 11b to be
is branched so that it has a predetermined opening angle α. The inclination of the injected fuel passages 8a, 8b with respect to the valve axis (if there are two injected fuel passages 8a, 8b, the inclination angle is α/2) is determined by
formed by the overlapping intersection of the walls of the injection fuel passages 8a, 8b (therefore, at least
(formed to have a ridge line of a certain length), with an upwardly pointed edge formed;
It is determined.

合流部9は、第1図および第4図に示すよう
に、噴射燃料通路8a,8bの壁面が交わる陵線
によつて特定されるエツジ部の燃料分岐部頂部1
2の、弁軸芯上で燃料噴孔3に対向する部位より
上流側に隔たつた位置において形成される。第1
図においてはlはこの隔たり量を示す。合流部9
は、各噴射燃料通路8a,8bの軸芯11a,1
1bと直角面内の各噴射燃料通路8a,8bの合
流部9への開口断面Aの、外径ピツチHと同等か
それ以上の径(第2図の場合)Dまたは内壁面間
寸法(第3図の場合)Dを有する断面形状、すな
わち開口断面Aを包絡する形状かそれより大の断
面形形状に形成されている。そして、合流部9の
通路断面積は、合流部9の外周壁面において、弁
軸芯に沿う方向に一定とされている。合流部9の
噴射弁軸芯と直交する面内の断面は、各噴射燃料
通路8a,8bの延長の断面を含む。
As shown in FIGS. 1 and 4, the merging section 9 is a fuel branching section top 1 at an edge section specified by a ridge line where the wall surfaces of the injection fuel passages 8a and 8b intersect.
2, it is formed at a position spaced apart upstream from the part facing the fuel injection hole 3 on the valve axis. 1st
In the figure, l indicates this distance. Confluence part 9
are the axes 11a, 1 of each injection fuel passage 8a, 8b.
The opening cross section A of each injected fuel passage 8a, 8b to the confluence part 9 in a plane perpendicular to In the case of Fig. 3), it is formed to have a cross-sectional shape D, that is, a cross-sectional shape that envelopes the opening cross-section A or is larger than that. The passage cross-sectional area of the merging portion 9 is constant in the direction along the valve axis on the outer peripheral wall surface of the merging portion 9. A cross section of the merging portion 9 in a plane perpendicular to the injection valve axis includes a cross section of an extension of each of the injected fuel passages 8a and 8b.

このように形成された合流部9と燃料分岐部1
0にあつては、噴射燃料通路8a,8bが2個の
場合、燃料分岐部10の頂部12が、第4図に示
すように弁軸芯上で燃料噴孔3に対向する部位か
ら両側に向つて湾曲しながら徐々に上方に延び、
両端は合流部9の底面13で終つている。そし
て、燃料分岐部10の頂部12には、合流部9が
頂部12の燃料噴孔対向部より上流側に隔てられ
て形成されることによつて、合流部9の座ぐり形
成において合流部9と干渉しないために残され
る、上方に向つて尖つたエツジ部が残されてい
る。
The confluence section 9 and fuel branch section 1 formed in this way
0, when there are two injection fuel passages 8a and 8b, the top part 12 of the fuel branch part 10 extends from the part facing the fuel nozzle hole 3 on the valve shaft center to both sides as shown in FIG. It gradually extends upward while curving towards the
Both ends terminate at the bottom surface 13 of the confluence section 9. The merging portion 9 is formed in the top portion 12 of the fuel branching portion 10 so as to be spaced upstream from the fuel injection hole opposing portion of the top portion 12. There is a sharp edge facing upwards that is left in place to avoid interference with the surface.

この合流部9の通路断面形状状は、上記の条件
を満たす限り任意の形状でよい。その例を第2
図、第3図に第1図の−断面でみた形状を示
す。
The cross-sectional shape of the passage of the merging portion 9 may be any shape as long as the above conditions are satisfied. The second example is
Figures 3 and 3 show the shape taken along the - cross section in Figure 1.

第2図に示した例では、合流部9aは円形断面
の通路に形成され、通路径Dは、噴射燃料通路8
a,8bの合流部9aへの開口断面の外径ピツチ
H以上、すなわちD≧Hに形成されている。
In the example shown in FIG.
The outer diameter pitch of the cross section of the opening of a, 8b to the merging portion 9a is greater than or equal to H, that is, D≧H.

第3図に示した例では、合流部9bはトラツク
状断面の通路に形成され、長径側の寸法Dが前述
と同様D≧Hに、短径側の巾Wは、噴射燃料通路
8a,8bの各径と同等かそれ以上の寸法に形成
されている。この合流部9a,9bの形成は、ア
ダプタ7の上部からの座ぐり加工によつて行なわ
れる。
In the example shown in FIG. 3, the merging portion 9b is formed as a passage with a track-shaped cross section, the dimension D on the major axis side is D≧H as described above, and the width W on the minor axis side is the injected fuel passage 8a, 8b. It is formed to have dimensions equal to or larger than each diameter of the The merging portions 9a and 9b are formed by counterboring from the top of the adapter 7.

つぎに、上記のように構成された電磁制御式燃
料噴射弁における作用について説明する。
Next, the operation of the electromagnetically controlled fuel injection valve configured as described above will be explained.

燃料供給通路2からシート部6を通して送られ
てきた燃料は、まず、一つの燃料噴孔3によつて
設定流量になるようメータリング(計量)され
る。メータリングされた燃料は、合流部9を飛行
して、燃料分岐部10の頂部12の位置で各噴射
燃料通路8a,8bに分配される。分配された燃
料は噴射燃料通路8a,8bの出口から、それぞ
れ燃料噴霧として噴射される。
The fuel sent from the fuel supply passage 2 through the seat portion 6 is first metered by one fuel injection hole 3 to a set flow rate. The metered fuel travels through the junction 9 and is distributed to each injection fuel passage 8a, 8b at the top 12 of the fuel branch 10. The distributed fuel is injected as fuel spray from the exits of the injection fuel passages 8a and 8b, respectively.

合流部9の、通路断面積は、各噴射燃料通路8
a,8bの合流部9への開口断面の包絡形状かそ
れよりも大であり、しかもその通路断面積が流れ
方向に一定であるため、合流部9の容積は十分に
大に確保される。そのため、合流部9での燃料の
壁面付着は生じず、合流部9での燃料の飛行は安
定したものとなる。また断面積一定の合流部9を
飛行するときに燃料は、流れに大きな変動を受け
ず、燃料分岐部10に至る。燃料分岐部10の頂
部12の燃料噴孔対向部にはエツジ状部が残され
ているので、平坦な面にあたつてはじかれること
はなく、円滑にかつ均等にかつ狙い通りの設定
量、設定方向に、各噴射燃料通路8a,8bに分
配される。
The passage cross-sectional area of the merging portion 9 is the same as that of each injection fuel passage 8.
Since the cross-sections of the openings of a and 8b to the merging portion 9 are envelope-shaped or larger, and the passage cross-sectional area is constant in the flow direction, the volume of the merging portion 9 is ensured to be sufficiently large. Therefore, the fuel does not adhere to the wall surface at the merging section 9, and the flight of the fuel at the merging section 9 becomes stable. Further, when the fuel flies through the confluence section 9 having a constant cross-sectional area, the fuel reaches the fuel branch section 10 without being subject to large fluctuations in flow. Since an edge-shaped portion is left on the top portion 12 of the fuel branch portion 10 facing the fuel nozzle hole, it will not be repelled by hitting a flat surface, and will smoothly and evenly achieve the desired set amount. It is distributed to each injection fuel passage 8a, 8b in a set direction.

また、合流部9での流れが安定すると、合流部
9から上流側、すなわち燃料噴孔3へ悪影響を及
ぼすことはなくなり、燃料噴孔3における計量精
度が向上される。
Furthermore, when the flow at the merging portion 9 becomes stable, there will be no adverse effect on the upstream side from the merging portion 9, that is, the fuel injection hole 3, and the metering accuracy in the fuel injection hole 3 will be improved.

[考案の効果] したがつて、本考案によるときは、噴射燃料通
路を弁軸芯に対して、噴射燃料通路壁面の重複す
る交わりによつて燃料分岐部頂部に上流側に向つ
て尖つたエツジ部が形成されるように傾けて形成
するとともに、合流部を燃料分岐部頂部の燃料噴
孔対向部より上流側に隔てて形成したので、分岐
部頂部の燃料噴孔対向部位に必ずエツジ部を残す
ことができ、合流部から各噴射燃料通路への燃料
の分配を均一化、安定化することができるととも
に燃料分岐方向を安定化することができ、これに
よつて、各噴射燃料通路からエンジン吸気通路に
向けて噴射される燃料の量、方向の精度を向上す
ることができるという効果が得られる。
[Effect of the invention] Therefore, according to the invention, the injection fuel passage is formed with a pointed edge toward the upstream side at the top of the fuel branch part by the overlapping intersection of the injection fuel passage wall surfaces with respect to the valve shaft core. Since the merging part is formed at an angle upstream from the part facing the fuel nozzle hole at the top of the fuel branch part, the edge part is always formed at the part facing the fuel nozzle hole at the top of the branch part. This makes it possible to equalize and stabilize the distribution of fuel from the merging section to each injection fuel passage, and also to stabilize the direction of fuel branching. The effect is that the accuracy of the amount and direction of fuel injected toward the intake passage can be improved.

また、燃料の合流部における飛行の安定化によ
り、燃料噴孔における計量の精度も向上すること
ができるという効果も得られる。
Furthermore, by stabilizing the flight at the fuel merging section, the accuracy of metering at the fuel injection hole can also be improved.

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

第1図は本考案の一実施例に係る電磁制御式燃
料噴射弁の先端部の断面図、第2図は第1図の
−線に沿う横断面図、第3図は本考案のもう一
つの実施例に係る電磁制御式燃料噴射弁の合流部
近傍の、第1図の−線に対応する部位の横断
面図、第4図は第1図の電磁制御式燃料噴射弁の
合流部近傍の斜視図、第5図イは第1図の電磁制
御式燃料噴射弁全体の断面図、第5図ロは第5図
イの電磁制御式燃料噴射弁の先端部の正面図、第
6図は既提案の燃料噴射弁の光端部の断面図、第
7図は第6図の−線に沿う断面図、第8図は
第6図の燃料噴射弁の合流部の斜視図、である。 1……電磁制御式燃料噴射弁、2……燃料供給
通路、3……燃料噴孔、6……シート部、7……
アダプタ、8a,8b……噴射燃料通路、9,9
a,9b……合流部、10……燃料分岐部、11
a,11b……軸芯(噴射燃料通路8a,8b
の)、12……燃料分岐部の頂部、13……合流
部底面、H……噴射燃料通路8a,8bの合流部
9への開口断面の外径ピツチ、D……合流部の通
路径、W……合流部の通路幅。
FIG. 1 is a sectional view of the tip of an electromagnetically controlled fuel injection valve according to an embodiment of the present invention, FIG. 2 is a cross-sectional view taken along the - line of FIG. FIG. 4 is a cross-sectional view of a portion corresponding to the - line in FIG. 1 near the merging portion of an electromagnetically controlled fuel injection valve according to two embodiments; FIG. 5A is a sectional view of the entire electromagnetically controlled fuel injection valve in FIG. 1, FIG. 5B is a front view of the tip of the electromagnetically controlled fuel injection valve in FIG. 5A, and FIG. 6 is a sectional view of the light end of the previously proposed fuel injection valve, FIG. 7 is a sectional view taken along the - line in FIG. 6, and FIG. . DESCRIPTION OF SYMBOLS 1...Electromagnetically controlled fuel injection valve, 2...Fuel supply passage, 3...Fuel injection hole, 6...Seat portion, 7...
Adapter, 8a, 8b... Injection fuel passage, 9, 9
a, 9b... Merging section, 10... Fuel branching section, 11
a, 11b...Axle core (injection fuel passages 8a, 8b
), 12...Top of the fuel branch, 13...Bottom surface of the merging part, H...Outer diameter pitch of the opening cross section of the injection fuel passages 8a, 8b to the merging part 9, D...Passway diameter of the merging part, W: Passage width at the merging section.

Claims (1)

【実用新案登録請求の範囲】 燃料を計量する燃料噴孔が、弁軸芯と同芯状
に、1つだけ設けられており; 前記燃料噴孔より下流側に、通路断面積が通路
長手方向に一定とされた噴射燃料通路が、該噴射
燃料通路の上流側部分が下流側部分よりも前記弁
軸芯に近づく傾きをもつて前記弁軸芯に対して傾
けられて、複数個、設けられており; 前記燃料噴孔と前記噴射燃料通路との間には、
合流部が、複数の前記噴射燃料通路の前記合流部
への開口断面を包絡する形状かそれより大の断面
形状をもつて該断面形状を前記弁軸芯に沿う方向
に一定にして、設けられており、; 複数の前記噴射燃料通路の間には、燃料が前記
燃料噴孔から噴射されて前記合流部を飛行してき
たときに該燃料を複数の前記噴射燃料通路に分配
する燃料分岐部が形成されている; 電磁制御式燃料噴射弁において; 複数の前記噴射燃料通路は、前記弁軸芯に対す
る傾きを、複数の前記噴射燃料通路の間に形成さ
れる前記燃料分岐部がその頂部に、複数の前記噴
射燃料通路の壁面の重複する交わりによつて形成
される上方に向つて尖つたエツジ部を有するよう
に、定められており; 前記合流部は、前記燃料分岐部頂部の前記弁軸
芯上で前記燃料噴孔に対向する部位から、上流側
に隔てられて形成されており、この隔てた形成に
よつて前記燃料分岐部頂部に、前記合流部の形成
において削りとられないエツジ部が前記燃料噴孔
に対向する部位に残されている、 ことを特徴とする電磁制御式燃料噴射弁。
[Claims for Utility Model Registration] Only one fuel injection hole for metering fuel is provided concentrically with the valve shaft; downstream of the fuel injection hole, the cross-sectional area of the passage is in the longitudinal direction of the passage. A plurality of injection fuel passages are provided, each of which has a constant angle, and is inclined with respect to the valve axis such that an upstream portion of the injection fuel passage is closer to the valve axis than a downstream portion of the injection fuel passage. between the fuel nozzle hole and the injection fuel passage;
The merging portion is provided with a cross-sectional shape that envelops or has a larger cross-sectional shape that surrounds the cross-section of the opening of the plurality of injected fuel passages to the merging portion, and that the cross-sectional shape is constant in a direction along the valve axis. and; a fuel branching section is provided between the plurality of injection fuel passages for distributing the fuel to the plurality of injection fuel passages when the fuel is injected from the fuel nozzle hole and flies through the merging section. In an electromagnetically controlled fuel injection valve, the plurality of injected fuel passages are inclined with respect to the valve axis, and the fuel branch portion formed between the plurality of injected fuel passages is at the top thereof. The plurality of injection fuel passages are defined to have upwardly pointed edges formed by overlapping intersections of the wall surfaces of the plurality of injection fuel passages; An edge portion is formed on the core so as to be separated from a portion facing the fuel nozzle hole on the upstream side, and as a result of this separated formation, an edge portion that is not scraped off in the formation of the merging portion is provided at the top of the fuel branch portion. An electromagnetically controlled fuel injection valve characterized in that: is left at a portion facing the fuel injection hole.
JP1985034717U 1985-03-13 1985-03-13 Expired JPH0231570Y2 (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
JP1985034717U JPH0231570Y2 (en) 1985-03-13 1985-03-13
US06/838,290 US4657189A (en) 1985-03-13 1986-03-10 Electromagnetic fuel injection valve for an internal combustion engine having a plurality of intake valves

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP1985034717U JPH0231570Y2 (en) 1985-03-13 1985-03-13

Publications (2)

Publication Number Publication Date
JPS61152765U JPS61152765U (en) 1986-09-20
JPH0231570Y2 true JPH0231570Y2 (en) 1990-08-27

Family

ID=30538352

Family Applications (1)

Application Number Title Priority Date Filing Date
JP1985034717U Expired JPH0231570Y2 (en) 1985-03-13 1985-03-13

Country Status (1)

Country Link
JP (1) JPH0231570Y2 (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2559515B2 (en) * 1990-02-23 1996-12-04 株式会社日立製作所 Fuel injection valve device and manufacturing method thereof
BR112015002190A2 (en) * 2012-08-01 2017-07-04 3M Innovative Properties Co fuel injectors with improved fuel discharge coefficient

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS60113065A (en) * 1983-11-24 1985-06-19 Toyota Motor Corp Fuel injection valve for dual-intake air engine

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS59123660U (en) * 1983-02-10 1984-08-20 トヨタ自動車株式会社 Fuel injection valve for electronically controlled engines

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS60113065A (en) * 1983-11-24 1985-06-19 Toyota Motor Corp Fuel injection valve for dual-intake air engine

Also Published As

Publication number Publication date
JPS61152765U (en) 1986-09-20

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