JP2003336563A - Fuel injection valve - Google Patents

Fuel injection valve

Info

Publication number
JP2003336563A
JP2003336563A JP2002143675A JP2002143675A JP2003336563A JP 2003336563 A JP2003336563 A JP 2003336563A JP 2002143675 A JP2002143675 A JP 2002143675A JP 2002143675 A JP2002143675 A JP 2002143675A JP 2003336563 A JP2003336563 A JP 2003336563A
Authority
JP
Japan
Prior art keywords
fuel injection
valve seat
fuel
injection valve
valve
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
JP2002143675A
Other languages
Japanese (ja)
Other versions
JP3784748B2 (en
Inventor
Kazuhiko Sato
和彦 佐藤
Kenichi Sato
健一 佐藤
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.)
Keihin Corp
Original Assignee
Keihin Corp
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 Keihin Corp filed Critical Keihin Corp
Priority to JP2002143675A priority Critical patent/JP3784748B2/en
Priority to US10/435,679 priority patent/US6854670B2/en
Publication of JP2003336563A publication Critical patent/JP2003336563A/en
Application granted granted Critical
Publication of JP3784748B2 publication Critical patent/JP3784748B2/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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Abstract

<P>PROBLEM TO BE SOLVED: To provide a fuel injection valve for an engine capable of promoting the atomization of injection fuel while improving the accuracy of fuel injection amount by reducing a space occupied by residual fuel from a valve seat to a fuel injection hole as much as possible when closing the valve. <P>SOLUTION: This fuel injection valve is provided with a valve seat member 3 having a valve seat 8 and an injector plate 36 joined with a front end face of the valve seat member 3. It forms a plurality of lateral passages 38 communicating with the downstream end of the valve seat 8 and a plurality of swirl chambers 39 in which downstream ends of these lateral passages 38 are opened in the tangential direction between the valve seat member 3 and the injector plate 36. It is formed with a plurality of fuel injection holes 40 for injecting fuel in these swirl chambers 39 to the outside in the injector plate 36. A plurality of side holes 37 whose one end each is opened in a peripheral fringe part at the downstream end of the valve seat 8 and other end each is connected with an upstream end of the lateral passage 38 are formed between the valve seat 8 and a plurality of lateral passages 38. <P>COPYRIGHT: (C)2004,JPO

Description

【発明の詳細な説明】Detailed Description of the Invention

【0001】[0001]

【発明の属する技術分野】本発明は,主として内燃機関
の燃料供給系に使用される燃料噴射弁に関し,特に,弁
体と,この弁体と協働する弁座の下流端が前端面に開口
する弁座部材と,前記弁座部材の前端面に接合されるイ
ンジェクタプレートとを備え,前記弁座部材及びインジ
ェクタプレートとの間に,前記弁座の下流端に連通し
て,前記弁座の軸線と略直交する横方向に延びる複数の
横方向通路と,これら横方向通路の下流端がそれぞれ接
線方向に開口する複数のスワール室とを形成し,これら
スワール室でスワールを付与された燃料をそれぞれ外部
に噴射させる複数の燃料噴孔を前記インジェクタプレー
トに穿設した燃料噴射弁の改良に関する。
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a fuel injection valve mainly used in a fuel supply system of an internal combustion engine, and more particularly to a valve body and a downstream end of a valve seat cooperating with the valve body, which is opened at a front end face. Valve seat member and an injector plate joined to the front end surface of the valve seat member, and communicating with the downstream end of the valve seat between the valve seat member and the injector plate, A plurality of lateral passages extending in the lateral direction substantially orthogonal to the axis and a plurality of swirl chambers whose downstream ends are opened tangentially are formed. The present invention relates to an improvement of a fuel injection valve in which a plurality of fuel injection holes for respectively injecting to the outside are formed in the injector plate.

【0002】[0002]

【従来の技術】かゝる燃料噴射弁は,例えば特許第26
59789号公報に開示されているように,既に知られ
ている。
2. Description of the Related Art Such a fuel injection valve is disclosed, for example, in Japanese Patent No. 26.
It is already known as disclosed in Japanese Patent No. 59789.

【0003】[0003]

【発明が解決しようとする課題】かゝる燃料噴射弁は,
燃料噴孔から噴射される燃料にスワールを付与すること
により,その噴射燃料の微粒化を促進しようとするもの
であるが,従来の燃料噴射弁では,弁座に連通する1つ
の中央開口から複数の横方向通路を放射状に延出させ,
開弁時,弁座を通過した燃料を中央開口に一旦集合さ
せ,それから複数の横方向通路に分配するようになって
いるため,中央開口には,燃料の集合及び分配をスムー
ズに行わせるに充分な容積を与えなければならない。し
かしながら,そのような中央開口の容積は,閉弁時には
デッドスペースボリュームとなり,そこに残留した燃料
が温度上昇や振動等に起因して燃料噴孔から流出し,燃
料噴射量を狂わせることがある。また上記中央開口での
燃料の集合及び分配により,分配燃料に乱流が起こるた
め,複数のスワール室への燃料の均等分配が難しく,し
たがって各燃料噴孔から発生する燃料フォームの均一化
を図ることが困難である。
[Problems to be Solved by the Invention] Such a fuel injection valve is
The swirl is given to the fuel injected from the fuel injection hole to promote atomization of the injected fuel. However, in the conventional fuel injection valve, a plurality of holes are formed from one central opening communicating with the valve seat. The lateral passages of the
When the valve is opened, the fuel that has passed through the valve seat is first gathered in the central opening and then distributed to multiple lateral passages. Therefore, the central opening can smoothly collect and distribute the fuel. Sufficient volume must be provided. However, such a volume of the central opening becomes a dead space volume when the valve is closed, and the fuel remaining therein may flow out from the fuel injection hole due to temperature rise, vibration, etc., and may distort the fuel injection amount. Further, due to the turbulent flow of the distributed fuel due to the collection and distribution of the fuel in the central opening, it is difficult to evenly distribute the fuel to the plurality of swirl chambers, and therefore the fuel foam generated from each fuel injection hole is made uniform. Is difficult.

【0004】本発明は,かゝる事情に鑑みてなされたも
ので,閉弁時,弁座から燃料噴孔までの残留燃料が占め
るスペースを極力小さくして,燃料噴射量の精度を向上
させつゝ,噴射燃料の微粒化を促進し得るようにした前
記燃料噴射弁を提供することを目的とする。
The present invention has been made in view of the above circumstances, and when the valve is closed, the space occupied by the residual fuel from the valve seat to the fuel injection hole is minimized to improve the accuracy of the fuel injection amount. That is, it is an object of the present invention to provide the fuel injection valve capable of promoting atomization of the injected fuel.

【0005】[0005]

【課題を解決するための手段】上記目的を達成するため
に,本発明は,弁体と,この弁体と協働する弁座の下流
端が前端面に開口する弁座部材と,前記弁座部材の前端
面に接合されるインジェクタプレートとを備え,前記弁
座部材及びインジェクタプレートとの間に,前記弁座の
下流端に連通して,前記弁座の軸線と略直交する横方向
に延びる複数の横方向通路と,これら横方向通路の下流
端がそれぞれ接線方向に開口する複数のスワール室とを
形成し,これらスワール室でスワールを付与された燃料
をそれぞれ外部に噴射させる複数の燃料噴孔を前記イン
ジェクタプレートに穿設した燃料噴射弁において,前記
弁座と複数の横方向通路との間に,該弁座の下流端周縁
部に各一端を開口すると共に,各他端を該横方向通路の
上流端に接続する複数の側孔を設けたことを第1の特徴
とする。
In order to achieve the above-mentioned object, the present invention provides a valve body, a valve seat member which cooperates with the valve body, and has a downstream end of the valve seat opened to a front end face, and the valve. An injector plate joined to the front end surface of the seat member, communicating with the valve seat member and the injector plate at the downstream end of the valve seat, and in a lateral direction substantially orthogonal to the axis of the valve seat. A plurality of lateral passages that extend and a plurality of swirl chambers whose downstream ends are tangentially open, and a plurality of fuels swirled in the swirl chambers are injected outside In a fuel injection valve having injection holes formed in the injector plate, one end is opened at the downstream end peripheral portion of the valve seat and the other end is provided between the valve seat and a plurality of lateral passages. Connect to the upstream end of the lateral passage A first feature in that a number of side holes.

【0006】この第1の特徴によれば,開弁時,弁座を
通過した燃料は,弁座の下流端周縁に連なる複数の側孔
を介して複数の横方向通路に直ちに均等に分流し,各対
応するスワール室に高速で接線方向に流入してスワール
が付与される。そして各対応する燃料噴孔から噴射され
た燃料は,噴射圧力と遠心力の作用で均一な中空円錐状
の燃料噴霧フォームを形成し,燃料の微粒化を促進する
ことができる。しかも各横方向通路に個別に連なる側孔
を弁座の周縁部に開口したことで,閉弁時,弁座から各
燃料噴孔までの残留燃料が占めるデッドスペースボリュ
ームを小さくすることが可能となり,また各スワール室
への燃料分配が均等であることゝ相俟って,燃料噴射量
の精度向上を図ることができる。
According to the first feature, when the valve is opened, the fuel passing through the valve seat is immediately and evenly divided into the plurality of lateral passages through the plurality of side holes connected to the peripheral edge of the downstream end of the valve seat. , Swirl is applied to each corresponding swirl chamber at high speed in the tangential direction. The fuel injected from the corresponding fuel injection holes forms a uniform hollow cone-shaped fuel spray foam by the action of the injection pressure and the centrifugal force, and can promote atomization of the fuel. Moreover, by opening the side holes individually connected to each lateral passage in the peripheral portion of the valve seat, it is possible to reduce the dead space volume occupied by the residual fuel from the valve seat to each fuel injection hole when the valve is closed. In addition, since the fuel distribution to each swirl chamber is even, the accuracy of the fuel injection amount can be improved.

【0007】また本発明は,第1の特徴に加えて,前記
弁座部材及びインジェクタプレート間に中間プレートを
接合し,前記横方向通路及びスワール室を該中間プレー
トの前記インジェクタプレートとの対向面に溝状に形成
し,また前記側孔を該中間プレートにその表裏を貫通す
るように形成したことを第2の特徴とする。
In addition to the first feature of the present invention, an intermediate plate is joined between the valve seat member and the injector plate, and the lateral passage and the swirl chamber are provided on a surface of the intermediate plate facing the injector plate. The second feature is that the side hole is formed in a groove shape, and the side hole is formed in the intermediate plate so as to penetrate the front surface and the back surface thereof.

【0008】この第2の特徴によれば,複数の側孔,横
方向通路及びスワール室を小部品の中間プレートに高い
精度をもって容易に加工することができ,しかも溝状の
横方向通路及びスワール室は,その溝幅や深さの設定に
より,同一板厚の中間プレートに仕様の異なる横方向通
路及びスワール室を形成することが可能となり,汎用性
を得ることができる。
According to the second feature, the plurality of side holes, the lateral passages and the swirl chamber can be easily machined into the intermediate plate of the small parts with high accuracy, and the groove-shaped lateral passages and swirls can be formed. By setting the groove width and depth of the chamber, it becomes possible to form lateral passages and swirl chambers of different specifications in the intermediate plate having the same plate thickness, and it is possible to obtain versatility.

【0009】さらに本発明は,第1又は第2の特徴に加
えて,前記各スワール室を,それに対応する側孔より前
記弁座の半径方向外方に配置したことを第3の特徴とす
る。
Further, in addition to the first or second feature, the present invention has a third feature in that each of the swirl chambers is arranged radially outward of the valve seat with respect to the corresponding side hole. .

【0010】この第3の特徴によれば,スワール室及び
燃料噴孔を複数の側孔の周囲に比較的多く設けることが
可能となり,燃料の大流量仕様に好適である。
According to the third feature, it is possible to provide a relatively large number of swirl chambers and fuel injection holes around a plurality of side holes, which is suitable for large fuel flow rate specifications.

【0011】さらにまた本発明は,第1又は第2の特徴
に加えて,前記各スワール室を,それに対応する側孔よ
り前記弁座の半径方向内方に配置したことを第4の特徴
とする。
Furthermore, in addition to the first or second feature, the present invention has a fourth feature in that each of the swirl chambers is arranged radially inward of the valve seat from a corresponding side hole. To do.

【0012】この第4の特徴によれば,複数の燃料噴孔
のピッチ円を充分小さくすることが可能となり,燃料の
小流量仕様に好適である。
According to the fourth feature, the pitch circles of the plurality of fuel injection holes can be made sufficiently small, which is suitable for a small fuel flow rate specification.

【0013】さらにまた本発明は,第1〜第4の特徴の
何れかに加えて,前記側孔の総開口面積の,前記燃料噴
孔の総開口面積に対する倍率を1.5〜3.0に設定し
たことを第5の特徴とする。
Further, according to the present invention, in addition to any one of the first to fourth characteristics, the ratio of the total opening area of the side holes to the total opening area of the fuel injection holes is 1.5 to 3.0. The fifth feature is that the setting is made to.

【0014】この第5の特徴によれば,必要最小限のデ
ッドスペースボリュームをもって,全負荷時における燃
料噴孔からの燃料噴射量を,側孔の絞り抵抗の影響を受
けることなく,安定的に確保することができる。
According to the fifth feature, with a minimum required dead space volume, the fuel injection amount from the fuel injection hole at full load can be stabilized without being affected by the throttling resistance of the side hole. Can be secured.

【0015】さらにまた本発明は,第1〜5の特徴の何
れかに加えて,前記各側孔を,それに対応する横方向通
路に向かうにつれて前記弁座の半径方向外方へ変位する
ように傾斜させたことを第6の特徴とする。
Further, in addition to any one of the first to fifth features, the present invention is characterized in that each of the side holes is displaced radially outward of the valve seat toward the corresponding lateral passage. The sixth feature is that the tape is inclined.

【0016】この第6の特徴によれば,燃料が各側孔か
ら横方向通路に移る際,燃料の流れに急激な曲りを与え
ず,その流れがスムーズとなるから,燃料の速度損失が
少く,したがってスワール室での燃料に対するスワール
効果を高めることができる。
According to the sixth feature, when the fuel moves from each side hole to the lateral passage, the flow of the fuel is not sharply bent and the flow becomes smooth, so that the velocity loss of the fuel is small. Therefore, the swirl effect on the fuel in the swirl chamber can be enhanced.

【0017】さらにまた本発明は,第1〜第6の特徴の
何れかに加えて,前記各横方向通路を,それに対応する
側孔の中心を通る前記弁座の半径線に対して傾斜させ
て,各対応する側孔及びスワール室の前記弁座中心に対
する角度位置を互いにずらせたことを第7の特徴とす
る。
In addition to any one of the first to sixth features, the present invention further provides that each of the lateral passages is inclined with respect to the radial line of the valve seat passing through the center of the corresponding side hole. The seventh feature is that the angular positions of the corresponding side holes and swirl chambers with respect to the valve seat center are displaced from each other.

【0018】この第7の特徴によれば,複数の側孔のピ
ッチ円と複数のスワール室のピッチ円との直径差が小さ
い場合でも,各横方向通路を長く設定することが可能
で,各スワール室の接線方向への燃料の層流誘導を的確
に行い,各スワール室で燃料の良好なスワール効果を得
ることができ,また燃料噴霧フォームのコンパクト化を
可能にして,エンジン吸気ポート内壁への燃料の付着防
止に寄与し得る。
According to the seventh feature, even if the diameter difference between the pitch circles of the plurality of side holes and the pitch circles of the plurality of swirl chambers is small, it is possible to set each lateral passage to be long. Accurately guide the laminar flow of fuel in the tangential direction of the swirl chamber to obtain a good swirl effect of the fuel in each swirl chamber, and also to make the fuel spray foam compact to the inner wall of the engine intake port. Can contribute to the prevention of fuel adhesion.

【0019】さらにまた本発明は,第1〜第7の特徴の
何れかに加えて,前記各横方向通路を,それに対応する
スワール室に向かうにつれて軸方向外方に変位するよう
に傾斜させたことを第8の特徴とする。
In addition to any one of the first to seventh features, the present invention is such that each of the lateral passages is inclined so as to be displaced outward in the axial direction toward the corresponding swirl chamber. This is the eighth feature.

【0020】この第8の特徴によれば,燃料が各側孔か
ら横方向通路,スワール室へと流れる際,その燃料の流
れに急激な曲りを与えず,その流れがスムーズとなるか
ら,燃料の速度損失が少く,したがってスワール室での
燃料に対するスワール効果を高めることができる。
According to the eighth feature, when the fuel flows from each side hole to the lateral passage and the swirl chamber, the flow of the fuel is not sharply bent, and the flow becomes smooth. The velocity loss is small and therefore the swirl effect on the fuel in the swirl chamber can be enhanced.

【0021】さらにまた本発明は,第1〜第8の特徴の
何れかに加えて,前記複数の側孔を前記弁座と同心の2
つのピッチ円上で千鳥状に配置し,また前記複数のスワ
ール室を前記2つのピッチ円と同心でそれらより大径の
2つのピッチ円上で千鳥状に配置したことを第9の特徴
とする。
Furthermore, in addition to any one of the first to eighth features, the present invention further comprises a plurality of side holes which are concentric with the valve seat.
A ninth feature is that the plurality of swirl chambers are arranged in a staggered manner on one pitch circle, and the swirl chambers are arranged in a staggered manner on two pitch circles that are concentric with the two pitch circles and have a larger diameter than them. .

【0022】この第9の特徴によれば,側孔,スワール
室及び燃料噴孔をより多く設けることが可能となり,燃
料の更なる大流量仕様に好適である。
According to the ninth feature, more side holes, swirl chambers, and fuel injection holes can be provided, which is suitable for a larger fuel flow rate specification.

【0023】[0023]

【発明の実施の形態】本発明の実施の形態を,添付図面
に示す本発明の実施例に基づいて以下に説明する。
BEST MODE FOR CARRYING OUT THE INVENTION Embodiments of the present invention will be described below based on the embodiments of the present invention shown in the accompanying drawings.

【0024】図1は本発明の第1実施例に係る内燃機関
用電磁式燃料噴射弁の縦断面図,図2は図1の要部拡大
図,図3は図2の3−3線断面図,図4は図2の4−4
線断面図,図5は図2の5矢視図,図6は図2の6−6
線拡大断面図,図7は図5に対応した作用説明図,図8
は本発明の第2実施例を示す,図5との対応図,図9は
本発明の第3実施例を示す,図5との対応図,図10は
本発明の第4実施例を示す,図5との対応図,図11は
側孔総開口面積Aの燃料噴孔総開口面積Bに対する倍率
と最大燃料噴射量との関係を示すテストで得た線図,図
12は燃料噴孔を1個としたとき(A),燃料噴孔を2
個としたとき(B)及び燃料噴孔を,その隣接間隔を
(B)より狭くして3個としたとき(C)の燃料噴霧フ
ォームの対比説明図である。
FIG. 1 is a longitudinal sectional view of an electromagnetic fuel injection valve for an internal combustion engine according to a first embodiment of the present invention, FIG. 2 is an enlarged view of a main part of FIG. 1, and FIG. 3 is a sectional view taken along line 3-3 of FIG. 4 and 4 in FIG. 2 and FIG.
A line sectional view, FIG. 5 is a view taken in the direction of arrow 5 in FIG. 2, and FIG.
FIG. 8 is an enlarged cross-sectional view, FIG. 7 is an operation explanatory view corresponding to FIG.
Shows a second embodiment of the present invention, a correspondence diagram with FIG. 5, FIG. 9 shows a third embodiment of the present invention, a correspondence diagram with FIG. 5, and FIG. 10 shows a fourth embodiment of the present invention FIG. 11, a diagram corresponding to FIG. 5, FIG. 11 is a diagram obtained by a test showing the relationship between the ratio of the total opening area A of the side holes to the total opening area B of the fuel injection holes and the maximum fuel injection amount, and FIG. (A) with one fuel injection hole
It is a comparison explanatory view of the fuel spray foam at the time of making (B) and the fuel injection hole into three pieces by making the adjoining space narrower than (B).

【0025】先ず,図1〜図7に示す本発明の第1実施
例より説明する。
First, the first embodiment of the present invention shown in FIGS. 1 to 7 will be described.

【0026】図1において,内燃機関用電磁式燃料噴射
弁Iのケーシング1は,円筒状の弁ハウジング2(磁性
体)と,この弁ハウジング2の前端部に液密に結合され
る有底円筒状の弁座部材3と,弁ハウジング2の後端に
環状スペーサ4を挟んで液密に結合される円筒状の固定
コア5とから構成される。
In FIG. 1, a casing 1 of an electromagnetic fuel injection valve I for an internal combustion engine includes a cylindrical valve housing 2 (magnetic material) and a bottomed cylinder liquid-tightly coupled to a front end portion of the valve housing 2. And a cylindrical fixed core 5 which is liquid-tightly coupled to the rear end of the valve housing 2 with an annular spacer 4 interposed therebetween.

【0027】環状スペーサ4は,ステンレス鋼等の非磁
性金属製であり,その両端面に弁ハウジング2及び固定
コア5が突き当てられて液密に全周溶接される。
The annular spacer 4 is made of non-magnetic metal such as stainless steel, and the valve housing 2 and the fixed core 5 are abutted on both end faces thereof and liquid-tightly welded all around.

【0028】弁座部材3及び弁ハウジング2の対向端部
には,第1嵌合筒部3a及び第2嵌合筒部2aがそれぞ
れ形成される。そして第1嵌合筒部3aが第2嵌合筒部
2a内にストッパプレート6と共に圧入され,ストッパ
プレート6は,弁ハウジング2と弁座部材3間で挟持さ
れる。その後,第1嵌合筒部3aの外周面と第2嵌合筒
部2aの端面とに挟まれる隅部の全周にわたりレーザ溶
接又はビーム溶接を施すことにより,弁ハウジング2及
び弁座部材3が相互に液密に結合される。
A first fitting tubular portion 3a and a second fitting tubular portion 2a are formed at the opposite ends of the valve seat member 3 and the valve housing 2, respectively. Then, the first fitting tubular portion 3a is press-fitted into the second fitting tubular portion 2a together with the stopper plate 6, and the stopper plate 6 is sandwiched between the valve housing 2 and the valve seat member 3. After that, laser welding or beam welding is performed over the entire circumference of the corner portion sandwiched between the outer peripheral surface of the first fitting tubular portion 3a and the end surface of the second fitting tubular portion 2a, whereby the valve housing 2 and the valve seat member 3 are Are liquid-tightly coupled to each other.

【0029】弁座部材3には,その前端面に下流端を開
口する円錐状の弁座8と,この弁座8の上流端,即ち大
径部に連なる円筒状のガイド孔9とが設けられており,
そのガイド孔9は,前記第2嵌合筒部2aと同軸状に形
成される。
The valve seat member 3 is provided with a conical valve seat 8 having a downstream end opened at its front end surface, and a cylindrical guide hole 9 connected to the upstream end of the valve seat 8, that is, the large diameter portion. Has been
The guide hole 9 is formed coaxially with the second fitting tubular portion 2a.

【0030】弁ハウジング2及び環状スペーサ4内に
は,固定コア5の前端面に対向する可動コア12が摺動
自在に収容され,この可動コア12に,前記ガイド孔9
に軸方向摺動自在に収容される弁体16が一体的に結合
される。この弁体16は,弁座8に着座し得る球状の弁
部16aと,ガイド孔9に摺動自在に支承される前後一
対のジャーナル部16b,16bと,前記ストッパプレ
ート6に当接して弁体16の開弁限界を規定するフラン
ジ16cとを一体に備えており,各ジャーナル部16b
には,燃料の流通を可能にする複数の面取り部17,1
7…が設けられる。
A movable core 12 facing the front end surface of the fixed core 5 is slidably accommodated in the valve housing 2 and the annular spacer 4, and the guide hole 9 is provided in the movable core 12.
A valve body 16 is slidably housed in the valve body 16 and is integrally coupled to the valve body 16. This valve body 16 is in contact with the stopper plate 6 and a spherical valve portion 16a that can be seated on the valve seat 8, a pair of front and rear journal portions 16b and 16b slidably supported in the guide hole 9, and the valve plate 16a. A flange 16c that defines the valve opening limit of the body 16 is integrally provided, and each journal portion 16b
Includes a plurality of chamfered parts 17, 1 that enable the flow of fuel.
7 ... are provided.

【0031】固定コア5は,弁ハウジング2内と連通す
る中空部21を有しており,その中空部21に,可動コ
ア12を弁体16の閉じ方向,即ち弁座8への着座方向
に付勢するコイル状の弁ばね22と,この弁ばね22の
後端を支承するパイプ状のリテーナ23とが収容され
る。
The fixed core 5 has a hollow portion 21 which communicates with the inside of the valve housing 2. In the hollow portion 21, the movable core 12 is arranged in the closing direction of the valve body 16, that is, in the seating direction on the valve seat 8. A coil-shaped valve spring 22 that urges and a pipe-shaped retainer 23 that supports the rear end of the valve spring 22 are housed.

【0032】固定コア5の後端には,パイプ状のリテー
ナ23を介して固定コア5の中空部21に連通する燃料
入口25aを持つ入口筒25が一体に連設され,その燃
料入口25aに燃料フィルタ27が装着される。
At the rear end of the fixed core 5, an inlet cylinder 25 having a fuel inlet 25a communicating with the hollow portion 21 of the fixed core 5 through a pipe-shaped retainer 23 is integrally connected, and the fuel inlet 25a is connected to the inlet cylinder 25a. A fuel filter 27 is attached.

【0033】環状スペーサ4及び固定コア5の外周には
コイル組立体28が嵌装される。このコイル組立体28
は,環状スペーサ4及び固定コア5に外周面に嵌合する
ボビン29と,これに巻装されるコイル30とからなっ
ており,このコイル組立体28を囲繞するコイルハウジ
ング31の一端部が弁ハウジング2の外周面に溶接によ
り結合される。
A coil assembly 28 is fitted around the outer circumferences of the annular spacer 4 and the fixed core 5. This coil assembly 28
Is composed of a bobbin 29 fitted on the outer peripheral surface of the annular spacer 4 and the fixed core 5, and a coil 30 wound around the bobbin 29. One end of a coil housing 31 surrounding the coil assembly 28 is a valve. It is joined to the outer peripheral surface of the housing 2 by welding.

【0034】コイルハウジング31,コイル組立体28
及び固定コア5は合成樹脂製の被覆体32内に埋封さ
れ,この被覆体32の中間部には,前記コイル30に連
なる接続端子33を収容する備えたカプラ34が一体に
連設される。
Coil housing 31, coil assembly 28
The fixed core 5 and the fixed core 5 are embedded in a cover 32 made of synthetic resin, and a coupler 34 for accommodating a connection terminal 33 connected to the coil 30 is integrally connected to an intermediate portion of the cover 32. .

【0035】図2〜図5に示すように,弁座部材3の前
端面には,鋼板製の中間プレート35を挟んで同じく鋼
板製のインジェクタプレート36が液密に全周溶接され
る。
As shown in FIGS. 2 to 5, a steel plate injector plate 36 is liquid-tightly welded all around the front end surface of the valve seat member 3 with a steel plate intermediate plate 35 interposed therebetween.

【0036】中間プレート35には,弁座8の下流端周
縁部から中間プレート35の表裏を貫通するように略軸
方向に延びて,弁座8の軸線周りに等間隔に配列される
多数の側孔37,37…が穿設され,またこの中間プレ
ート35の,インジェクタプレート36との対向面に
は,上記側孔37,37…から弁座8の半径方向外方へ
放射状に延びる多数の横方向通路38,38…と,これ
ら横方向通路38,38…の下流端が接線方向に開口す
る多数のスワール室39,39…とが溝状に形成され
る。
The intermediate plate 35 has a large number of axially extending axially extending from the downstream edge of the valve seat 8 so as to penetrate the front and back surfaces of the intermediate plate 35 and arranged at equal intervals around the axis of the valve seat 8. Side holes 37, 37 ... Are bored, and a large number of radially extending outward from the side seats 37, 37 ... In the radial direction of the valve seat 8 are formed on the surface of the intermediate plate 35 facing the injector plate 36. The lateral passages 38, 38 ... And a large number of swirl chambers 39, 39 ... In which the downstream ends of the lateral passages 38, 38 ... Are opened tangentially are formed in a groove shape.

【0037】その際,望ましくは,各側孔37は,それ
に対応する横方向通路38に向かうにつれて弁座8の半
径方向外方へ変位するように傾斜して配置され,また各
横方向通路38は,それに対応するスワール室39に向
かうにつれて軸方向外方に変位するように傾斜して配置
される。
At this time, preferably, each side hole 37 is arranged so as to be inclined so as to be displaced outward in the radial direction of the valve seat 8 toward the corresponding lateral passage 38, and each lateral passage 38 is also arranged. Are inclined so as to be displaced outward in the axial direction toward the corresponding swirl chamber 39.

【0038】前記多数のスワール室39,39…も,側
孔37,37…と同様に,弁座8の軸線周りに等間隔に
配列される。各横方向通路38の各スワール室39に開
口する接線方向は一定していて,各スワール室39で燃
料に付与されるスワール方向が一定するようになってい
る。
The plurality of swirl chambers 39, 39 ... Are also arranged at equal intervals around the axis of the valve seat 8, like the side holes 37, 37. The tangential direction of each lateral passage 38 opening to each swirl chamber 39 is constant, and the swirl direction imparted to the fuel in each swirl chamber 39 is constant.

【0039】インジェクタプレート36には,上記多数
のスワール室39,39…にそれぞれ開口する多数の燃
料噴孔40,40…が穿設される。インジェクタプレー
ト36は,その板厚が各燃料噴孔40の内径より小さく
なっており,また各燃料噴孔40は,その軸線が弁座8
の軸線と平行になるように配置される。
The injector plate 36 is provided with a large number of fuel injection holes 40, 40 ... Opening into the large number of swirl chambers 39, 39. The thickness of the injector plate 36 is smaller than the inner diameter of each fuel injection hole 40, and the axis line of each fuel injection hole 40 has a valve seat 8
It is arranged so as to be parallel to the axis line of.

【0040】図6に明示するように,各燃料噴孔40
は,それに対応するスワール室39の中心から対応する
横方向通路38の上流端側に所定距離eオフセットして
配置される。また多数の燃料噴孔40,40…は,図5
に示すように,それらの隣接間隔pが2.5mm以下と
なるように配置される。
As clearly shown in FIG. 6, each fuel injection hole 40
Are offset from the center of the corresponding swirl chamber 39 to the upstream end of the corresponding lateral passage 38 by a predetermined distance e. Further, a large number of fuel injection holes 40, 40 ...
As shown in FIG. 5, they are arranged so that their adjacent interval p is 2.5 mm or less.

【0041】こゝで,多数の側孔37,37…の総合開
口面積をA,多数の燃料噴孔40,40…の総合開口面
積をBとしたとき,A/B=1.5〜3.0となるよう
に,上記側孔37,37…及び燃料噴孔40,40…は
形成される。
When the total opening area of the large number of side holes 37, 37 ... Is A and the total opening area of the large number of fuel injection holes 40, 40 ... is B, A / B = 1.5 to 3 The side holes 37, 37 ... And the fuel injection holes 40, 40 ... Are formed so as to be 0.0.

【0042】再び,図1において,弁ハウジング2から
弁座部材3にかけて,それらの外周に環状のシールホル
ダ48が嵌合され,このシールホルダ48と,弁座部材
3の前端部に嵌着される合成樹脂製のキャップ45との
間に環状溝46が画成され,この環状溝46に,弁座部
材3の外周面に密接するOリング47が装着される。こ
のOリング47は,この電磁式燃料噴射弁Iを図示しな
い吸気マニホールドの燃料噴射弁取り付け孔に装着した
とき,その取り付け孔の内周面に密接するようになって
いる。
Again, in FIG. 1, an annular seal holder 48 is fitted around the valve housing 2 and the valve seat member 3 at their outer circumferences, and is fitted to the seal holder 48 and the front end portion of the valve seat member 3. An annular groove 46 is defined between the annular groove 46 and the synthetic resin cap 45, and an O-ring 47 that is in close contact with the outer peripheral surface of the valve seat member 3 is attached to the annular groove 46. When the electromagnetic fuel injection valve I is mounted in a fuel injection valve mounting hole of an intake manifold (not shown), the O-ring 47 comes into close contact with the inner peripheral surface of the mounting hole.

【0043】次に,この第1実施例の作用について説明
する。コイル30を消磁した状態では,弁ばね22の付
勢力で可動コア12及び弁体16が前方に押圧され,弁
部16aを弁座8に着座させている。したがって,燃料
フィルタ27及び入口筒25を通して弁ハウジング2内
に供給された高圧燃料は,弁ハウジング2内に待機させ
られる。
Next, the operation of the first embodiment will be described. When the coil 30 is demagnetized, the movable core 12 and the valve body 16 are pressed forward by the urging force of the valve spring 22, and the valve portion 16a is seated on the valve seat 8. Therefore, the high-pressure fuel supplied into the valve housing 2 through the fuel filter 27 and the inlet cylinder 25 is made to stand by in the valve housing 2.

【0044】コイル30を通電により励磁すると,それ
により生ずる磁束が固定コア5,コイルハウジング3
1,弁ハウジング2及び可動コア12を順次走り,その
磁力により可動コア12が弁体16と共に固定コア5に
吸引され,弁座8が開放されるので,弁ハウジング2内
の高圧燃料は,弁体16の面取り部17,17…を経て
弁座8を通過し,その周縁部から高速を維持したまゝ直
ちに多数の側孔37,37…に分流し,これら側孔3
7,37…からそれぞれ対応する横方向通路38,38
…を経て対応するスワール室39に高速で接線方向に流
入するため,それら燃料は各スワール室39を高速で旋
回することによりスワールが付与される。
When the coil 30 is excited by energization, the magnetic flux generated thereby is generated by the fixed core 5 and the coil housing 3.
1, the valve housing 2 and the movable core 12 are sequentially run, and the magnetic force causes the movable core 12 to be attracted to the fixed core 5 together with the valve body 16, and the valve seat 8 is opened. After passing through the valve seat 8 via the chamfered portions 17, 17, ... Of the body 16, immediately branch from the peripheral portion thereof to a large number of side holes 37, 37.
7, 37 ... From corresponding lateral passages 38, 38 respectively
Since the fuel flows into the corresponding swirl chamber 39 at a high speed in a tangential direction after passing through, the swirls are imparted to the fuel by swirling each swirl chamber 39 at a high speed.

【0045】特に,各側孔37が,対応する横方向通路
38に向かうにつれて弁座8の半径方向外方へ変位する
ように傾斜し,また各横方向通路38が,対応するスワ
ール室39に向かうにつれて軸方向外方に変位するよう
に傾斜して配置される場合には,各側孔37及び横方向
通路38を経てスワール室39に到達するまでの燃料の
流れの急激な屈曲がなくなり,その流れがスムーズとな
るから,燃料の速度損失が少ない。
In particular, each side hole 37 is inclined so as to be displaced outward in the radial direction of the valve seat 8 toward the corresponding lateral passage 38, and each lateral passage 38 is connected to the corresponding swirl chamber 39. When it is arranged so as to be displaced outward in the axial direction as it goes, there is no sharp bend in the fuel flow until it reaches the swirl chamber 39 through each side hole 37 and the lateral passage 38, Since the flow is smooth, there is little fuel velocity loss.

【0046】また各燃料噴孔40は各スワール室39の
中心から対応する横方向通路38の上流端側に所定距離
eオフセットして配置されているから,スワール室39
に流入した燃料の大部分はスワール室39を略1回転す
るうちに燃料噴孔40から噴射されることになり,スワ
ール室39での燃料の速度損失が少ない。
Further, since each fuel injection hole 40 is arranged offset from the center of each swirl chamber 39 on the upstream end side of the corresponding lateral passage 38 by a predetermined distance e, the swirl chamber 39 is formed.
Most of the fuel that has flowed into the fuel cell is injected from the fuel injection hole 40 while the swirl chamber 39 makes one revolution, and the velocity loss of the fuel in the swirl chamber 39 is small.

【0047】以上の結果,各スワール室39から対応す
る燃料噴孔40に噴射された燃料は,大なる噴射圧力と
遠心力の作用で中空円錐状の燃料噴霧フォームF1を形
成し,高いスワール速度を維持し得るので,燃料の微粒
化をより効果的促進することができ,しかも燃料噴射の
応答性を向上させることができる。
As a result, the fuel injected from the respective swirl chambers 39 into the corresponding fuel injection holes 40 forms a hollow conical fuel spray foam F1 by the action of a large injection pressure and centrifugal force, and a high swirl velocity. Therefore, the atomization of fuel can be promoted more effectively, and the responsiveness of fuel injection can be improved.

【0048】しかも多数の横方向通路38,38…に個
別に連なる多数の側孔37,37…を弁座8の周縁部に
それぞれ開口したことで,閉弁時,弁座8から各燃料噴
孔40までの残留燃料が占めるデッドスペースボリュー
ムを小さくすることが可能となり,燃料噴射量の精度向
上に寄与し得る。特に,各側孔37及び各燃料噴孔40
を,前述のようにA/B=1.5〜3.0となるように
形成すれば,図11のテストデータから明らかなよう
に,必要最小限のデッドスペースボリュームをもって,
全負荷時における各燃料噴孔40からの燃料噴射量を,
各側孔37の絞り抵抗の影響を受けることなく,安定的
に確保することができる。
Moreover, by opening a large number of side holes 37, 37 ... Which are individually connected to a large number of lateral passages 38, 38 ... In the peripheral portion of the valve seat 8, each fuel injection from the valve seat 8 is performed when the valve is closed. The dead space volume occupied by the residual fuel up to the hole 40 can be reduced, which can contribute to the improvement of the accuracy of the fuel injection amount. In particular, each side hole 37 and each fuel injection hole 40
Is formed so that A / B = 1.5 to 3.0 as described above, as is clear from the test data of FIG. 11, with the minimum required dead space volume,
The amount of fuel injected from each fuel injection hole 40 at full load is
It is possible to ensure the stability without being affected by the throttling resistance of each side hole 37.

【0049】図12(A)は,燃料噴孔40を単一とし
てテストしたときの燃料噴霧フォームF1の形成状態を
示し,図12(B)は,2つの燃料噴孔40,40の間
隔を2.4mmに設定してテストしたときの燃料噴霧フ
ォームF1,F2の形成状態を示し,また図12(C)
は,3つの燃料噴孔40,40,40の各隣接間隔を
1.3mmに設定してテストしたときの燃料噴霧フォー
ムF1,F2の形成状態を示すものである。
FIG. 12 (A) shows the state of formation of the fuel spray foam F1 when tested with the single fuel injection hole 40, and FIG. 12 (B) shows the distance between the two fuel injection holes 40, 40. FIG. 12 (C) shows the formation state of the fuel spray foams F1 and F2 when set to 2.4 mm and tested.
Shows the formation state of the fuel spray foams F1 and F2 when the test was performed by setting the adjacent intervals of the three fuel injection holes 40, 40, 40 to 1.3 mm.

【0050】図12(A)に示すように,単一の燃料噴
孔40から生ずる中空円錐状の燃料噴霧フォームF1
は,燃料噴孔40を出た直後に層状の液膜状態を呈し,
その後,液糸状態を経て微粒化状態となるが,この第1
実施例では,弁座8の軸線周りに多数の燃料噴孔40,
40…が隣接間隔を2.5mm以下と狭くして配置さ
れ,しかも各スワール室39で燃料に同一方向のスワー
ルが付与されるため,多数の中空円錐状の燃料噴霧フォ
ームF1,F1…は,図7,並びに図12(B)及び
(C)に示すように,液膜状態において互いに隣り合う
もの同士で液膜部分を正面衝突させることになる。その
結果,全燃料噴霧フォームF1,F1…の液糸状態が早
まり,その分,燃料の微粒化を効果的に促進することが
できる。しかも,多数の燃料噴霧フォームF1,F1…
が互いに液膜部分を正面衝突させることで,最終的には
燃料密度が中心部で高く,外周部で低い1つ集合した燃
料噴霧フォームF1が形成されることになり,エンジン
の吸気路内壁への燃料付着を極力防ぎつゝ,吸入空気と
共にエンジンに吸入され,エンジンの始動性及び出力性
能の向上と燃費の低減に大いに寄与し得る。
As shown in FIG. 12A, a hollow cone-shaped fuel spray foam F1 generated from a single fuel injection hole 40.
Shows a layered liquid film state immediately after exiting the fuel injection hole 40,
After that, it goes through the liquid thread state and becomes the atomized state.
In the embodiment, a large number of fuel injection holes 40 are provided around the axis of the valve seat 8.
40 are arranged such that the adjacent intervals are as narrow as 2.5 mm or less, and swirls in the same direction are imparted to the fuel in each swirl chamber 39, so a large number of hollow cone-shaped fuel spray forms F1, F1 ... As shown in FIG. 7 and FIGS. 12 (B) and 12 (C), in the liquid film state, the liquid film portions are brought into frontal collision with each other. As a result, the liquid thread state of all the fuel spray foams F1, F1 ... Is accelerated, and the atomization of the fuel can be effectively promoted accordingly. Moreover, a large number of fuel spray forms F1, F1 ...
By causing the liquid film portions to collide with each other in the front direction, finally, a single fuel spray foam F1 in which the fuel density is high in the central portion and low in the outer peripheral portion is formed, and the fuel spray foam F1 is formed on the inner wall of the intake passage of the engine. While preventing the fuel from adhering to the engine as much as possible, it is sucked into the engine together with the intake air, which can greatly contribute to the improvement of engine startability and output performance and the reduction of fuel consumption.

【0051】テストによれば,多数の燃料噴霧フォーム
F1,F1…の液膜状態の終端は,インジェクタプレー
ト36から0.5〜3.0mm離れた領域にあり,この
領域で多数の燃料噴霧フォームF1,F1…を衝突させ
れば,燃料の微粒化を効果的に促進し得ることを確認で
きた。またこのような燃料噴霧フォームF1,F1…同
士の衝突を得るために,多数の燃料噴孔40,40…の
隣接間隔を前述のように2.5mm以下と設定すること
は極めて有効であった。
According to the test, the end of the liquid film state of many fuel spray foams F1, F1 ... Is in the area 0.5 to 3.0 mm away from the injector plate 36, and many fuel spray foams are in this area. It was confirmed that collision of F1, F1 ... Can effectively promote atomization of fuel. Further, in order to obtain such a collision between the fuel spray foams F1, F1 ..., It was extremely effective to set the adjoining intervals of the plurality of fuel injection holes 40, 40 ... to 2.5 mm or less as described above. .

【0052】またインジェクタプレート36に板厚を各
燃料噴孔40の内径より小さく設定したことで,中空円
錐状の各燃料噴霧フォームF1の中心角度を充分に拡大
できて,多数の燃料噴霧フォームF1,F1…を互いに
液膜状態で確実に衝突させることが可能であり,燃料の
微粒化を一層促進することができる。
By setting the thickness of the injector plate 36 to be smaller than the inner diameter of each fuel injection hole 40, the central angle of each hollow cone-shaped fuel spray foam F1 can be sufficiently expanded, and a large number of fuel spray foams F1 can be obtained. , F1 ... Can be reliably made to collide with each other in a liquid film state, and atomization of fuel can be further promoted.

【0053】さらに多数の燃料噴孔40,40…の軸線
を平行に配置したことで,これら燃料噴孔40,40…
を高精度をもって同軸加工が可能となる。その結果,全
燃料噴孔40,40…から発生する燃料噴霧フォームF
1,F1…は常に均一化し,それらの液膜部相互の正面
衝突により,常に安定した集合燃料噴霧フォームF2を
形成することができ,エンジンの始動性及び出力性能の
向上と燃費の低減に一層寄与し得る。
By arranging the axes of a larger number of fuel injection holes 40, 40 ... In parallel, these fuel injection holes 40, 40 ...
It is possible to perform coaxial processing with high accuracy. As a result, the fuel spray foam F generated from all the fuel injection holes 40, 40 ...
1, F1 ... are always uniformized, and the frontal collisions of the liquid film portions with each other can always form a stable aggregated fuel spray foam F2, which improves engine startability and output performance and reduces fuel consumption. Can contribute.

【0054】ところで,この第1の実施例では,多数の
横方向通路38,38…及びスワール室39,39…が
中間プレート35のインジェクタプレート36との対向
面に溝状に形成され,また多数の側孔37,37…が中
間プレート35にその表裏を貫通するように形成される
ので,複数の側孔37,37…,横方向通路38,38
…及びスワール室39,39…を小部品の中間プレート
35に高い精度をもって容易に加工することができ,し
かも溝状の横方向通路38,38…及びスワール室3
9,39…は,その溝幅や深さの設定により,同一板厚
の中間プレート(*)に仕様の異なる横方向通路38,
38…及びスワール室39,39…を形成することが可
能となり,汎用性を得ることができる。
By the way, in the first embodiment, a large number of lateral passages 38, 38 ... And swirl chambers 39, 39 ... Are formed in a groove shape on the surface of the intermediate plate 35 facing the injector plate 36, and a large number of them are formed. .. are formed in the intermediate plate 35 so as to penetrate the front and back surfaces thereof, the plurality of side holes 37, 37.
... and the swirl chambers 39, 39 ... Can be easily machined to the intermediate plate 35 of small parts with high accuracy, and the groove-shaped lateral passages 38, 38 ... And the swirl chamber 3
9, 39 ... are lateral passages 38 of different specifications in the intermediate plate (*) having the same plate thickness, depending on the setting of the groove width and depth.
38 and swirl chambers 39, 39 ... Can be formed, and versatility can be obtained.

【0055】また多数のスワール室39,39…は,環
状に配列される側孔37,37…群のピッチ円と同心で
且つそれより大きいピッチ円上に環状に配列されるか
ら,側孔37,37…群の周囲にスワール室39,39
…及び燃料噴孔40,40…を比較的多く設けることが
可能となり,燃料の大流量仕様に好適である。
The swirl chambers 39, 39 ... Are arranged annularly on a pitch circle concentric with and larger than the pitch circles of the group of side holes 37, 37. , 37 ... Swirl chambers 39, 39 around the group
, And the fuel injection holes 40, 40 can be provided in a relatively large number, which is suitable for large fuel flow rate specifications.

【0056】次に,図8に示す本発明の第2実施例につ
いて説明する。
Next, a second embodiment of the present invention shown in FIG. 8 will be described.

【0057】この第2実施例は,多数の側孔37,37
…を同心の2つピッチ円C1,C2上で千鳥状に配置
し,それに伴い多数のスワール室39,39…は,上記
ピッチ円C1,C2より大径で且つそれらと同心の2つ
のピッチ円C3,C4上で千鳥状に配置した点を除け
ば,前実施例と同様の構成であり,図8中,前実施例と
対応する部分には同一の参照符号を付して,その説明を
省略する。
In this second embodiment, a large number of side holes 37, 37 are provided.
... are arranged in a staggered manner on two concentric pitch circles C1 and C2, and accordingly, a large number of swirl chambers 39, 39 ... Are two pitch circles having a diameter larger than and concentric with the pitch circles C1 and C2. The configuration is the same as that of the previous example except that the points are arranged in a staggered pattern on C3 and C4. In FIG. 8, parts corresponding to those of the previous example are designated by the same reference numerals, and description thereof will be given. Omit it.

【0058】この第2実施例によれば,側孔37,37
…,スワール室39,39…及び燃料噴孔40,40…
をより多く設けることが可能となり,燃料の更なる大流
量仕様に好適である。
According to this second embodiment, the side holes 37, 37
..., swirl chambers 39, 39 ... and fuel injection holes 40, 40 ...
It is possible to provide a larger number of fuel cells, which is suitable for higher fuel flow rate specifications.

【0059】次に,図9に示す本発明の第3実施例につ
いて説明する。
Next, a third embodiment of the present invention shown in FIG. 9 will be described.

【0060】この第3実施例では,複数のスワール室3
9,39…は,環状に配列される側孔37,37…群の
ピッチ円と同心で且つそれより小さいピッチ円上に環状
に配列される。また各横方向通路38は,それに対応す
る側孔37の中心を通る弁座8の半径線L1に対して角
度α傾斜していて,各対応する側孔37及びスワール室
39の前記弁座8中心に対する角度位置が互いにずらさ
れている。その他の構成は前記第1実施例と同様の構成
であるから,図9中,第1実施例と対応する部分には同
一の参照符号を付して,その説明を省略する。
In this third embodiment, a plurality of swirl chambers 3
.. are arranged annularly on a pitch circle concentric with and smaller than the pitch circles of the group of side holes 37, 37. Further, each lateral passage 38 is inclined at an angle α with respect to the radial line L1 of the valve seat 8 passing through the center of the corresponding side hole 37, and the corresponding lateral hole 37 and the valve seat 8 of the swirl chamber 39 are inclined. The angular positions with respect to the center are offset from each other. Since the other structure is the same as that of the first embodiment, in FIG. 9, the portions corresponding to those of the first embodiment are designated by the same reference numerals and the description thereof will be omitted.

【0061】この第3実施例によれば,スワール室3
9,39…及び燃料噴孔40,40…をあまり多くは設
けられないが,燃料噴孔40,40…群のピッチ円を充
分小さくすることが可能となり,燃料の小流量仕様に好
適である。また側孔37,37…群のピッチ円とスワー
ル室39,39…群のピッチ円との直径差が小さい場合
でも,各横方向通路38を長く設定することが可能で,
各スワール室39の接線方向への燃料の層流誘導を的確
に行い,各スワール室39において燃料の良好なスワー
ル効果を得ることができる。また各燃料噴霧フォームF
1,F2のコンパクト化を可能にして,エンジン吸気ポ
ート内壁への燃料の付着防止に寄与し得る。
According to this third embodiment, the swirl chamber 3
9 and 39 and the fuel injection holes 40, 40 ... Can not be provided so much, but the pitch circle of the fuel injection holes 40, 40 ... Group can be made sufficiently small, which is suitable for a small flow rate specification of fuel. . Further, even if the diameter difference between the pitch circle of the side holes 37, 37 ... Group and the pitch circle of the swirl chambers 39, 39 ... Group is small, it is possible to set each lateral passage 38 to be long.
Laminar flow of fuel in the tangential direction of each swirl chamber 39 can be accurately performed, and a good swirl effect of fuel can be obtained in each swirl chamber 39. In addition, each fuel spray form F
It is possible to make 1 and F2 compact and to contribute to the prevention of fuel adhesion to the inner wall of the engine intake port.

【0062】次に,図10に示す本発明の第4実施例に
ついて説明する。
Next, a fourth embodiment of the present invention shown in FIG. 10 will be described.

【0063】この第4実施例は,各横方向通路38を,
それに対応する側孔37の中心を通る弁座8の半径線L
2に対して角度β傾斜させて,各対応する側孔37及び
スワール室39の前記弁座8中心に対する角度位置を互
いにずらせた点を除けば,前記第1実施例と同様の構成
であり,図10中,第1実施例と対応する部分には同一
の参照符号を付して,その説明を省略する。
In this fourth embodiment, each lateral passage 38 is
The radial line L of the valve seat 8 passing through the center of the corresponding side hole 37
The configuration is the same as that of the first embodiment, except that the angle positions of the corresponding side holes 37 and swirl chambers 39 with respect to the center of the valve seat 8 are shifted from each other by an angle β with respect to 2. In FIG. 10, parts corresponding to those of the first embodiment are designated by the same reference numerals, and description thereof will be omitted.

【0064】この第4実施例によれば,側孔37,37
…群のピッチ円とスワール室39,39…群のピッチ円
との直径差が小さい場合でも,各横方向通路38を長く
設定することが可能で,各スワール室39の接線方向へ
の燃料の誘導を的確に行い,各スワール室39において
燃料の良好なスワール効果を得ることができる。
According to the fourth embodiment, the side holes 37, 37
Even when the diameter difference between the group pitch circle and the swirl chambers 39, 39 ... Group pitch circle is small, each lateral passage 38 can be set to be long, and the tangential direction of the fuel in each swirl chamber 39 can be set. The induction can be performed accurately and a good swirl effect of fuel can be obtained in each swirl chamber 39.

【0065】本発明は上記実施例に限定されるものでは
なく,その要旨を逸脱しない範囲で種々の設計変更が可
能である。
The present invention is not limited to the above embodiments, and various design changes can be made without departing from the scope of the invention.

【0066】[0066]

【発明の効果】以上のように本発明の第1の特徴によれ
ば,弁体と,この弁体と協働する弁座の下流端が前端面
に開口する弁座部材と,前記弁座部材の前端面に接合さ
れるインジェクタプレートとを備え,前記弁座部材及び
インジェクタプレートとの間に,前記弁座の下流端に連
通して,前記弁座の軸線と略直交する横方向に延びる複
数の横方向通路と,これら横方向通路の下流端がそれぞ
れ接線方向に開口する複数のスワール室とを形成し,こ
れらスワール室でスワールを付与された燃料をそれぞれ
外部に噴射させる複数の燃料噴孔を前記インジェクタプ
レートに穿設した燃料噴射弁において,前記弁座と複数
の横方向通路との間に,該弁座の下流端周縁部に各一端
を開口すると共に,各他端を該横方向通路の上流端に接
続する複数の側孔を設けたので,開弁時,弁座を通過し
た燃料は,複数の側孔を介して複数の横方向通路に直ち
に均等に分流し,各対応するスワール室に高速で接線方
向に流入してスワールが付与され,そして各対応する燃
料噴孔から噴射された燃料は,噴射圧力と遠心力の作用
で均一な中空円錐状の燃料噴霧フォームを形成し,燃料
の微粒化を促進することができる。しかも各横方向通路
に個別に連なる側孔を弁座の周縁部に開口したことで,
閉弁時,弁座から各燃料噴孔までの残留燃料が占めるデ
ッドスペースボリュームを小さくすることが可能とな
り,また各スワール室への燃料分配が均等であることゝ
相俟って,燃料噴射量の精度向上を図ることができる。
As described above, according to the first feature of the present invention, the valve body, the valve seat member that cooperates with the valve body, and the downstream end of the valve seat opens to the front end face, and the valve seat. An injector plate joined to a front end surface of the member, and communicating with the valve seat member and the injector plate at a downstream end of the valve seat, and extending in a lateral direction substantially orthogonal to an axis of the valve seat. A plurality of lateral passages and a plurality of swirl chambers whose downstream ends are open tangentially, and a plurality of fuel jets for injecting swirled fuel to the outside respectively. In the fuel injection valve having holes formed in the injector plate, one end is opened at the downstream end peripheral portion of the valve seat and the other end is formed between the valve seat and the plurality of lateral passages. Multiple side holes connected to the upstream end of the directional passage Since it is provided, when the valve is opened, the fuel that has passed through the valve seat is immediately and evenly diverted to the lateral passages through the side holes and swiftly flows tangentially into the corresponding swirl chambers at high speed. The fuel injected from the corresponding fuel injection holes can form a uniform hollow cone-shaped fuel spray foam by the action of the injection pressure and the centrifugal force, and can promote the atomization of the fuel. Moreover, by opening the side holes individually connected to each lateral passage in the peripheral portion of the valve seat,
When the valve is closed, the dead space volume occupied by the residual fuel from the valve seat to each fuel injection hole can be reduced, and the fuel distribution to each swirl chamber is even. The accuracy of can be improved.

【0067】また本発明の第2の特徴によれば,前記弁
座部材及びインジェクタプレート間に中間プレートを接
合し,前記横方向通路及びスワール室を該中間プレート
の前記インジェクタプレートとの対向面に溝状に形成
し,また前記側孔を該中間プレートにその表裏を貫通す
るように形成したので,複数の側孔,横方向通路及びス
ワール室を小部品の中間プレートに高い精度をもって容
易に加工することができ,しかも溝状の横方向通路及び
スワール室は,その溝幅や深さの設定により,同一板厚
の中間プレートに仕様の異なる横方向通路及びスワール
室を形成することが可能となり,汎用性を得ることがで
きる。
Further, according to the second feature of the present invention, an intermediate plate is joined between the valve seat member and the injector plate, and the lateral passage and the swirl chamber are provided on a surface of the intermediate plate facing the injector plate. Since it is formed in the shape of a groove and the side holes are formed in the intermediate plate so as to penetrate the front and back sides, a plurality of side holes, lateral passages and swirl chambers can be easily and easily machined in the intermediate plate of small parts. Moreover, the groove-shaped lateral passage and swirl chamber can be formed in the intermediate plate of the same plate thickness with different specifications by setting the groove width and depth. , The versatility can be obtained.

【0068】さらに本発明の第3の特徴によれば,前記
各スワール室を,それに対応する側孔より前記弁座の半
径方向外方に配置したので,スワール室及び燃料噴孔を
複数の側孔の周囲に比較的多く設けることが可能とな
り,燃料の大流量仕様に好適である。
Further, according to the third aspect of the present invention, since the swirl chambers are arranged radially outward of the valve seat with respect to the corresponding side holes, the swirl chambers and the fuel injection holes are provided on a plurality of sides. A relatively large number of holes can be provided around the hole, which is suitable for large fuel flow specifications.

【0069】さらにまた本発明の第4の特徴によれば,
前記各スワール室を,それに対応する側孔より前記弁座
の半径方向内方に配置したので,複数の燃料噴孔のピッ
チ円を充分小さくすることが可能となり,燃料の小流量
仕様に好適である。
Furthermore, according to the fourth aspect of the present invention,
Since each of the swirl chambers is arranged radially inward of the valve seat with respect to the corresponding side hole, the pitch circle of the plurality of fuel injection holes can be made sufficiently small, which is suitable for the small fuel flow rate specification. is there.

【0070】さらにまた本発明の第5の特徴によれば,
前記側孔の総開口面積の,前記燃料噴孔の総開口面積に
対する倍率を1.5〜3.0に設定したので,必要最小
限のデッドスペースボリュームをもって,全負荷時にお
ける燃料噴孔からの燃料噴射量を,側孔の絞り抵抗の影
響を受けることなく,安定的に確保することができる。
Furthermore, according to the fifth feature of the present invention,
Since the ratio of the total opening area of the side holes to the total opening area of the fuel injection holes is set to 1.5 to 3.0, the dead space volume from the fuel injection holes at full load is maintained with the minimum dead space required. The fuel injection amount can be stably secured without being affected by the throttling resistance of the side holes.

【0071】さらにまた本発明の第6の特徴によれば,
前記各側孔を,それに対応する横方向通路に向かうにつ
れて前記弁座の半径方向外方へ変位するように傾斜させ
たので,燃料が各側孔から横方向通路に移る際,燃料の
流れに急激な曲りを与えず,その流れがスムーズとなる
から,燃料の速度損失が少く,したがってスワール室で
の燃料に対するスワール効果を高めることができる。
Furthermore, according to the sixth feature of the present invention,
Since each side hole is inclined so as to be displaced radially outward of the valve seat toward the corresponding lateral passage, when the fuel moves from each side hole to the lateral passage, the Since the flow becomes smooth without giving a sharp bend, the velocity loss of the fuel is small, and therefore the swirl effect on the fuel in the swirl chamber can be enhanced.

【0072】さらにまた本発明の第7の特徴によれば,
前記各横方向通路を,それに対応する側孔の中心を通る
前記弁座の半径線に対して傾斜させて,各対応する側孔
及びスワール室の前記弁座中心に対する角度位置を互い
にずらせたので,複数の側孔のピッチ円と複数のスワー
ル室のピッチ円との直径差が小さい場合でも,各横方向
通路を長く設定することが可能で,各スワール室の接線
方向への燃料の層流誘導を的確に行い,各スワール室で
燃料の良好なスワール効果を得ることができ,また燃料
噴霧フォームのコンパクト化を可能にして,エンジン吸
気ポート内壁への燃料の付着防止に寄与し得る。
Furthermore, according to the seventh feature of the present invention,
Since each of the lateral passages is inclined with respect to the radial line of the valve seat passing through the center of the corresponding side hole, the angular positions of the corresponding side holes and swirl chambers with respect to the center of the valve seat are offset from each other. , Even if the diameter difference between the pitch circles of the side holes and the pitch circles of the swirl chambers is small, it is possible to set each lateral passage long, and the laminar flow of fuel in the tangential direction of each swirl chamber The induction can be performed accurately, a good swirl effect of fuel can be obtained in each swirl chamber, and the fuel spray foam can be made compact, which can contribute to the prevention of fuel adhesion to the inner wall of the engine intake port.

【0073】さらにまた本発明の第8の特徴によれば,
前記各横方向通路を,それに対応するスワール室に向か
うにつれて軸方向外方に変位するように傾斜させたの
で,燃料が各側孔から横方向通路,スワール室へと流れ
る際,その燃料の流れに急激な曲りを与えず,その流れ
がスムーズとなるから,燃料の速度損失が少く,したが
ってスワール室での燃料に対するスワール効果を高める
ことができる。
Furthermore, according to the eighth feature of the present invention,
Since each of the lateral passages is inclined so as to be displaced outward in the axial direction toward the corresponding swirl chamber, when the fuel flows from each side hole to the lateral passage or swirl chamber, the flow of the fuel Since there is no sharp bend and the flow becomes smooth, the fuel velocity loss is small and therefore the swirl effect on the fuel in the swirl chamber can be enhanced.

【0074】さらにまた本発明の第9の特徴によれば,
前記複数の側孔を,前記弁座と同心の2つのピッチ円上
で千鳥状に配置すると共に,前記複数のスワール室も前
記2つのピッチ円と同心でそれらより大径の2つのピッ
チ円上で千鳥状に配置したので,側孔,スワール室及び
燃料噴孔をより多く設けることが可能となり,燃料の更
なる大流量仕様に好適である。
Furthermore, according to the ninth feature of the present invention,
The plurality of side holes are arranged in a staggered manner on two pitch circles concentric with the valve seat, and the plurality of swirl chambers are also concentric with the two pitch circles on two pitch circles having a larger diameter than them. The staggered arrangement makes it possible to provide more side holes, swirl chambers, and fuel injection holes, which is suitable for higher fuel flow specifications.

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

【図1】本発明の第1実施例に係る内燃機関用電磁式燃
料噴射弁の縦断面図
FIG. 1 is a vertical sectional view of an electromagnetic fuel injection valve for an internal combustion engine according to a first embodiment of the present invention.

【図2】図1の要部拡大図FIG. 2 is an enlarged view of a main part of FIG.

【図3】図2の3−3線断面図3 is a sectional view taken along line 3-3 of FIG.

【図4】図2の4−4線断面図FIG. 4 is a sectional view taken along line 4-4 of FIG.

【図5】図2の5矢視図5 is a view taken in the direction of arrow 5 in FIG.

【図6】図2の6−6線拡大断面図6 is an enlarged sectional view taken along line 6-6 of FIG.

【図7】図5に対応した作用説明図FIG. 7 is an operation explanatory diagram corresponding to FIG.

【図8】本発明の第2実施例を示す,図5との対応図FIG. 8 is a diagram showing a second embodiment of the present invention, corresponding to FIG.

【図9】本発明の第3実施例を示す,図5との対応図FIG. 9 is a diagram corresponding to FIG. 5, showing a third embodiment of the present invention.

【図10】本発明の第4実施例を示す,図5との対応図FIG. 10 is a diagram showing a fourth embodiment of the present invention, corresponding to FIG.

【図11】側孔総開口面積Aの燃料噴孔総開口面積Bに
対する倍率と最大燃料噴射量との関係を示すテストで得
た線図
FIG. 11 is a diagram obtained by a test showing a relationship between a ratio of a total opening area A of side holes to a total opening area B of fuel injection holes and a maximum fuel injection amount.

【図12】燃料噴孔を1個としたとき(A),燃料噴孔
を2個としたとき(B)及び燃料噴孔を,その隣接間隔
を(B)より狭くして3個としたとき(C)の燃料噴霧
フォームの対比説明図
FIG. 12: When the number of fuel injection holes is one (A), when there are two fuel injection holes (B), and the distance between adjacent fuel injection holes is smaller than that of (B), there are three. (C) Fuel spray foam comparison explanatory diagram

【符号の説明】[Explanation of symbols]

C1,C2・・・千鳥状配置の側孔群の2つのピッチ円 C3,C4・・・千鳥状配置のスワール室群の2つのピ
ッチ円 I・・・・・燃料噴射弁 L1,L2・・・弁座の半径線 3・・・・・弁座部材 8・・・・・弁座 35・・・・中間プレート 36・・・・インジェクタプレート 37・・・・側孔 38・・・・横方向通路 39・・・・スワール室 40・・・・燃料噴孔
C1, C2 ... Two pitch circles of side hole group of staggered arrangement C3, C4 ... Two pitch circles of swirl chamber group of staggered arrangement I ... Fuel injection valves L1, L2 ...・ Radius line of valve seat 3 ... Valve seat member 8 ... Valve seat 35 ... Intermediate plate 36 ... Injector plate 37 ... Side hole 38 ... Direction passage 39 ... Swirl chamber 40 ... Fuel injection hole

───────────────────────────────────────────────────── フロントページの続き Fターム(参考) 3G066 AD07 BA03 BA51 CC06U CC15 CC25 CC26 CC37 CC43 CC70 CD30 CE22    ─────────────────────────────────────────────────── ─── Continued front page    F term (reference) 3G066 AD07 BA03 BA51 CC06U                       CC15 CC25 CC26 CC37 CC43                       CC70 CD30 CE22

Claims (9)

【特許請求の範囲】[Claims] 【請求項1】 弁体(16)と,この弁体(16)と協
働する弁座(8)の下流端が前端面に開口する弁座部材
(3)と,前記弁座部材(3)の前端面に接合されるイ
ンジェクタプレート(36)とを備え,前記弁座部材
(3)及びインジェクタプレート(36)との間に,前
記弁座(8)の下流端に連通して,前記弁座(8)の軸
線と略直交する横方向に延びる複数の横方向通路(3
8)と,これら横方向通路(38)の下流端がそれぞれ
接線方向に開口する複数のスワール室(39)とを形成
し,これらスワール室(39)でスワールを付与された
燃料をそれぞれ外部に噴射させる複数の燃料噴孔(4
0)を前記インジェクタプレート(36)に穿設した燃
料噴射弁において,前記弁座(8)と複数の横方向通路
(38)との間に,該弁座(8)の下流端周縁部に各一
端を開口すると共に,各他端を該横方向通路(38)の
上流端に接続する複数の側孔(37)を設けたことを特
徴とする燃料噴射弁。
1. A valve body (16), a valve seat member (3) in which a downstream end of a valve seat (8) cooperating with the valve body (16) opens to a front end face, and the valve seat member (3). ) And an injector plate (36) joined to the front end surface of the valve seat member (3) and the injector plate (36), and communicating with the downstream end of the valve seat (8), A plurality of lateral passages (3) extending in a lateral direction substantially orthogonal to the axis of the valve seat (8).
8) and a plurality of swirl chambers (39) each having a downstream end of each of the lateral passages (38) opening in a tangential direction, and the swirl-filled fuel is respectively discharged to the outside. A plurality of fuel injection holes (4
0) in the injector plate (36), in the fuel injection valve, between the valve seat (8) and the plurality of lateral passages (38), at the peripheral edge of the downstream end of the valve seat (8). A fuel injection valve characterized in that a plurality of side holes (37) are provided which open one end and connect the other end to the upstream end of the lateral passage (38).
【請求項2】 請求項1記載の燃料噴射弁において,前
記弁座部材(3)及びインジェクタプレート(36)間
に中間プレート(35)を接合し,前記横方向通路(3
8)及びスワール室(39)を該中間プレート(35)
の前記インジェクタプレート(36)との対向面に溝状
に形成し,また前記側孔(37)を該中間プレート(3
5)にその表裏を貫通するように形成したことを特徴と
する燃料噴射弁。
2. The fuel injection valve according to claim 1, wherein an intermediate plate (35) is joined between the valve seat member (3) and the injector plate (36), and the lateral passage (3) is connected.
8) and the swirl chamber (39) to the intermediate plate (35)
Is formed in a groove shape on the surface facing the injector plate (36), and the side hole (37) is formed on the intermediate plate (3).
5) A fuel injection valve characterized by being formed so as to penetrate the front and back thereof.
【請求項3】 請求項1又は2記載の燃料噴射弁におい
て,前記各スワール室(39)を,それに対応する側孔
(37)より前記弁座(8)の半径方向外方に配置した
ことを特徴とする燃料噴射弁。
3. The fuel injection valve according to claim 1, wherein each of the swirl chambers (39) is arranged radially outward of the valve seat (8) from a corresponding side hole (37). Fuel injection valve characterized by.
【請求項4】 請求項1又は2記載の燃料噴射弁におい
て,前記各スワール室(39)を,それに対応する側孔
(37)より前記弁座(8)の半径方向内方に配置した
ことを特徴とする燃料噴射弁。
4. The fuel injection valve according to claim 1, wherein each swirl chamber (39) is arranged radially inward of the valve seat (8) from a corresponding side hole (37). Fuel injection valve characterized by.
【請求項5】 請求項1〜4の何れかに記載の燃料噴射
弁において,前記側孔(37)の総開口面積の,前記燃
料噴孔(40)の総開口面積に対する倍率を1.5以上
に設定したことを特徴する燃料噴射弁。
5. The fuel injection valve according to claim 1, wherein the ratio of the total opening area of the side holes (37) to the total opening area of the fuel injection holes (40) is 1.5. A fuel injection valve having the above settings.
【請求項6】 請求項1〜5の何れかに記載の燃料噴射
弁において,前記各側孔(37)を,それに対応する横
方向通路(38)に向かうにつれて前記弁座(8)の半
径方向外方へ変位するように傾斜させたことを特徴とす
る,燃料噴射弁。
6. The fuel injection valve according to claim 1, wherein each side hole (37) has a radius of the valve seat (8) as it goes to a corresponding lateral passage (38). A fuel injection valve characterized by being inclined so as to be displaced outward in the direction.
【請求項7】 請求項1〜6の何れかに記載の燃料噴射
弁において,前記各横方向通路(38)を,それに対応
する側孔(37)の中心を通る前記弁座(8)の半径線
(L1,L2)に対して傾斜させて,各対応する側孔
(37)及びスワール室(39)の前記弁座(8)中心
に対する角度位置を互いにずらせたことを特徴とする,
燃料噴射弁。
7. The fuel injection valve according to any one of claims 1 to 6, wherein the valve seat (8) passes through each lateral passage (38) through the center of a corresponding side hole (37). Inclining with respect to the radial lines (L1, L2), the angular positions of the corresponding side holes (37) and swirl chambers (39) with respect to the center of the valve seat (8) are offset from each other.
Fuel injection valve.
【請求項8】 請求項1〜7の何れかに記載の燃料噴射
弁において,前記各横方向通路(38)を,それに対応
するスワール室(39)に向かうにつれて軸方向外方に
変位するように傾斜させたことを特徴とする,燃料噴射
弁。
8. The fuel injection valve according to claim 1, wherein each lateral passage (38) is displaced axially outwardly toward a swirl chamber (39) corresponding thereto. A fuel injection valve characterized by being tilted to.
【請求項9】 請求項1〜8何れかに記載の燃料噴射弁
において,前記複数の側孔(37)を前記弁座(8)と
同心の2つのピッチ円(C1,C2)上で千鳥状に配置
し,また前記複数のスワール室(39)を前記2つのピ
ッチ円(C1,C2)と同心でそれらより大径の2つの
ピッチ円(C3,C4)上で千鳥状に配置したことを特
徴とする,燃料噴射弁。
9. The fuel injection valve according to claim 1, wherein the plurality of side holes (37) are staggered on two pitch circles (C1, C2) concentric with the valve seat (8). And the plurality of swirl chambers (39) are arranged in a staggered manner on two pitch circles (C3, C4) which are concentric with the two pitch circles (C1, C2) and have a larger diameter than them. Fuel injection valve characterized by.
JP2002143675A 2002-05-17 2002-05-17 Fuel injection valve Expired - Fee Related JP3784748B2 (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
JP2002143675A JP3784748B2 (en) 2002-05-17 2002-05-17 Fuel injection valve
US10/435,679 US6854670B2 (en) 2002-05-17 2003-05-12 Fuel injection valve

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP2002143675A JP3784748B2 (en) 2002-05-17 2002-05-17 Fuel injection valve

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JP3784748B2 JP3784748B2 (en) 2006-06-14

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Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2010265865A (en) * 2009-05-18 2010-11-25 Mitsubishi Electric Corp Fuel injection valve
JP2011196354A (en) * 2010-03-24 2011-10-06 Hitachi Automotive Systems Ltd Fuel injection valve
DE102010048146A1 (en) 2010-04-16 2011-10-20 Mitsubishi Electric Corp. Fuel injection valve
JP2014526376A (en) * 2011-09-15 2014-10-06 ザ プロクター アンド ギャンブル カンパニー Spray nozzle for dispensing liquid and spray provided with the spray nozzle
EP2690279A3 (en) * 2012-07-27 2015-08-12 Hitachi Automotive Systems, Ltd. Fuel injection valve
JP5893110B1 (en) * 2014-10-01 2016-03-23 三菱電機株式会社 Fuel injection valve
CN107355328A (en) * 2016-05-09 2017-11-17 三菱电机株式会社 Fuelinjection nozzle

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Cited By (13)

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Publication number Priority date Publication date Assignee Title
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DE102009056409A1 (en) 2009-05-18 2010-12-23 Mitsubishi Electric Corporation Fuel injection valve
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JP2010265865A (en) * 2009-05-18 2010-11-25 Mitsubishi Electric Corp Fuel injection valve
US8888024B2 (en) 2009-05-18 2014-11-18 Mitsubishi Electric Corporation Fuel injection valve
JP2011196354A (en) * 2010-03-24 2011-10-06 Hitachi Automotive Systems Ltd Fuel injection valve
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JP2014526376A (en) * 2011-09-15 2014-10-06 ザ プロクター アンド ギャンブル カンパニー Spray nozzle for dispensing liquid and spray provided with the spray nozzle
EP2690279A3 (en) * 2012-07-27 2015-08-12 Hitachi Automotive Systems, Ltd. Fuel injection valve
JP5893110B1 (en) * 2014-10-01 2016-03-23 三菱電機株式会社 Fuel injection valve
CN107355328A (en) * 2016-05-09 2017-11-17 三菱电机株式会社 Fuelinjection nozzle
CN107355328B (en) * 2016-05-09 2019-05-14 三菱电机株式会社 Fuel injection valve

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