JP2865677B2 - Gasoline engine fuel supply system - Google Patents
Gasoline engine fuel supply systemInfo
- Publication number
- JP2865677B2 JP2865677B2 JP63251822A JP25182288A JP2865677B2 JP 2865677 B2 JP2865677 B2 JP 2865677B2 JP 63251822 A JP63251822 A JP 63251822A JP 25182288 A JP25182288 A JP 25182288A JP 2865677 B2 JP2865677 B2 JP 2865677B2
- Authority
- JP
- Japan
- Prior art keywords
- fuel
- spray
- flow
- branch
- passage
- 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 - Fee Related
Links
Landscapes
- Fuel-Injection Apparatus (AREA)
Description
【発明の詳細な説明】 [産業上の利用分野] 本発明はガソリンエンジンの燃料供給装置に係り、更
に詳細には燃料噴射弁から噴射される燃料を2つの噴霧
流に分ける分岐孔付きの燃料供給装置に関する。Description: BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a fuel supply device for a gasoline engine, and more particularly, to a fuel with a branch hole for dividing fuel injected from a fuel injection valve into two spray flows. It relates to a supply device.
[従来の技術] 近年、エンジンの高出力化を図るために1気筒当たり
2つの吸気弁を有するエンジン(例えばDOHCエンジン)
が広く普及されている。このようなエンジンに対応する
燃料供給装置では、例えば特開昭55−153852号公報等に
開示されているように燃料噴射弁の出口部に2つの分岐
通路を設け、この分岐通路によって1つの燃料噴射弁か
ら噴出した燃料を2方向に分け、対応する各吸気弁に燃
料を供給する方式が採用されている。[Related Art] In recent years, an engine having two intake valves per cylinder (eg, a DOHC engine) in order to increase the output of the engine
Is widely spread. In a fuel supply device corresponding to such an engine, for example, as disclosed in Japanese Patent Application Laid-Open No. 55-153852, two branch passages are provided at an outlet of a fuel injection valve, and one fuel passage is provided by the branch passages. A method is adopted in which fuel injected from an injection valve is divided into two directions and fuel is supplied to corresponding intake valves.
[発明が解決しようとする課題] ところで最近では、エンジンの出力向上・燃焼効率を
図るために噴霧燃料を微粒化(例えば噴霧粒径200〜100
μm程度)して均質混合気を形成することが望まれてい
るが、従来この要求に応えることは困難であった。その
理由としては、噴霧流を2方向に分ける従来の燃料供給
方式は一般に噴霧流を棒状にして2方向に分割している
が、この棒状の噴霧流は噴霧の広がりがあまりないため
燃料の液膜が薄くならず、噴霧の平均粒径を300μm以
下にすることが困難であること。また、分岐孔から噴出
する噴霧のうち、その一部が2つの分岐孔の間に形成さ
れる分岐部によって流れ方向が規制され、この規制を受
けた噴霧が分岐孔を出たところで隣の噴霧と合流(合
体)して噴霧粒径の一部が大きくなる傾向があることが
挙げられる。[Problems to be Solved by the Invention] By the way, recently, in order to improve engine output and combustion efficiency, atomized fuel is atomized (for example, spray particle diameter of 200 to 100).
(approximately μm) to form a homogeneous mixture, but it has been difficult to meet this requirement in the past. The reason is that in the conventional fuel supply system in which the spray flow is divided into two directions, the spray flow is generally divided into two directions by making the spray flow into a rod shape. The film is not thin, and it is difficult to reduce the average particle size of the spray to 300 μm or less. Further, the flow direction is regulated by a branch portion formed between the two branch holes, a part of the spray ejected from the branch hole. And a part of the spray particle diameter tends to increase.
本発明は以上の点に鑑みてなされたもので、その目的
とするところは、噴霧流を2方向に分ける方式のガソリ
ンエンジンの燃料供給装置において、エンジンの運転条
件や燃料噴射弁の弁ストロークに左右されることなく分
岐部に向かって確実に中空円錐形の燃料噴霧パターンを
形成し、また噴霧流の粒径をより微粒化して燃料の応答
性を高めることにある。The present invention has been made in view of the above points, and an object of the present invention is to provide a fuel supply device for a gasoline engine that divides a spray flow into two directions, in terms of engine operating conditions and valve stroke of a fuel injection valve. An object of the present invention is to form a fuel spray pattern of a hollow conical shape surely toward a branch portion without being influenced by the influence of the fuel, and to improve the responsiveness of the fuel by further reducing the particle size of the spray flow.
[課題を解決するための手段] 上記目的は、弁体の往復動によって開閉される燃料通
路を通して吸気通路に燃料を供給するガソリンエンジン
の燃料供給装置において、前記燃料通路の出口部に形成
された燃料噴孔から噴出する燃料を所定の開き角度をな
す2方向の燃料流に分岐する分岐部と、前記燃料噴孔上
流の燃料通路に設けられた旋回流発生部(20)と前記旋
回流発生部(20)の中心線から所定のオフセット寸法だ
け離れた位置に前記旋回流発生部(20)の接線方向に配
された複数の燃料通路(21)とから成る旋回流形成手段
とを備え、前記燃料噴孔から噴出する燃料の噴霧広がり
角(θ2)を24度乃至40度になるように前記オフセット
寸法を設定したことを特徴とするガソリンエンジンの燃
料供給装置をもちいることにより達成される。[MEANS FOR SOLVING THE PROBLEMS] An object of the present invention is to provide a fuel supply device for a gasoline engine that supplies fuel to an intake passage through a fuel passage that is opened and closed by reciprocating motion of a valve body. A branch portion for branching the fuel ejected from the fuel injection hole into a fuel flow in two directions having a predetermined opening angle, a swirl flow generating portion (20) provided in a fuel passage upstream of the fuel injection hole, and the swirl flow generation Swirling flow forming means comprising a plurality of fuel passages (21) arranged in a tangential direction of the swirling flow generating portion (20) at a position separated by a predetermined offset dimension from a center line of the portion (20), This is achieved by using a fuel supply device for a gasoline engine, wherein the offset dimension is set so that the spray divergence angle (θ 2 ) of the fuel ejected from the fuel injection hole becomes 24 degrees to 40 degrees. You.
[作用] 本発明によれば、エンジンの運転条件や燃料噴射弁の
弁ストロークに左右されることなく分岐部に向かって確
実に中空円錐形の燃料噴霧パターンを形成し、噴霧流は
分岐で2つに分けられ微粒化されて、吸気通路に噴射さ
れる。噴霧流の方向は分岐孔の方向によって設定でき
る。噴霧形成手段としては、燃料噴射弁の噴孔を通る燃
料を旋回させて噴孔から噴射した後の噴射広がり角を大
きくするスワール型のものを用いているので、スワラー
オフセットδを変えることによって噴霧広がり角を任意
に設定できる。また、エンジンの運転条件に左右される
ことなく分岐孔入口に向かって確実に中空円錐形の燃料
噴霧パターンを形成でき、壁面付着に伴う粒径の粗大化
を少なくできる。[Operation] According to the present invention, a hollow conical fuel spray pattern is reliably formed toward the branch portion without being influenced by the operating conditions of the engine or the valve stroke of the fuel injection valve. The mixture is divided into fine particles, and is atomized and injected into the intake passage. The direction of the spray flow can be set by the direction of the branch hole. As the spray forming means, a swirl type is used in which the fuel passing through the injection hole of the fuel injection valve is swirled to increase the injection divergence angle after being injected from the injection hole. The spread angle can be set arbitrarily. In addition, a hollow conical fuel spray pattern can be reliably formed toward the branch hole entrance without being affected by the operating conditions of the engine, and the increase in particle size due to the adhesion to the wall surface can be reduced.
請求項2のように分岐孔を断面長円形とすることによ
り分岐孔から噴射される噴霧流が長軸方向の広がりが大
きく短軸方向の広がりが小さい扁平な扇形の広がりとな
る。そこで長円形断面通路の長軸が吸気通路を流れる空
気流に沿うようにして吸気通路壁面に設置することによ
って噴霧流が空気流の力で吸気通路の壁面側に偏向され
ることなく目標の位置に直接送られ、より一層混合気の
均質化を図り得ると共に燃料系の応答性を高めることが
できる。By forming the branch hole into an elliptical cross section as in claim 2, the spray flow injected from the branch hole has a flat fan-shaped spread with a large spread in the long axis direction and a small spread in the short axis direction. Therefore, by setting the long axis of the oval cross section passage along the air flow flowing through the intake passage on the intake passage wall surface, the spray flow is not deflected to the wall surface side of the intake passage by the force of the air flow. And the mixture can be further homogenized, and the responsiveness of the fuel system can be improved.
[実施例] 本発明の実施例を図面に基づき説明する。Example An example of the present invention will be described with reference to the drawings.
第1図(a)に本発明の実施例を示す。本実施例は燃
料に旋回流を加えてオリフィスから噴出するスワール型
の噴射弁1を用い、この噴射弁1の先端に、2つの分岐
孔3を有するアダプタ2が被着される。分岐孔3を設け
ることによって2方向に粒径の小さな噴霧流を形成する
ことができる。アダプタ2は円板形チップ状を呈し又は
円筒形キャップ状を呈し、燃料噴射弁1に“かしめ”又
は圧入、メタルフローで固定する。材質としてはステン
レス・黄銅等を用いる。耐ガソリン性の樹脂で噴射弁1
と一体成形しても良い。分岐孔3は第1図cに示すよう
に、長方形の両端にアールをつけたいわゆる長円形の細
長の孔形状に形成してある。この長円形分岐孔3の寸法
は幅をB、長さをLとすれば、B<Lの関係が成立する
よう幅狭に設定してある。このようにして形成される燃
料噴霧は、分岐孔3で2つの噴霧流に分けられてエンジ
ンの吸気通路に噴射される。FIG. 1A shows an embodiment of the present invention. In the present embodiment, a swirl type injection valve 1 is used which adds a swirling flow to fuel and jets out from an orifice. At the tip of the injection valve 1, an adapter 2 having two branch holes 3 is attached. By providing the branch holes 3, a spray flow having a small particle diameter can be formed in two directions. The adapter 2 has a disk-shaped tip shape or a cylindrical cap shape, and is fixed to the fuel injection valve 1 by "caulking" or press-fitting and metal flow. Stainless steel, brass or the like is used as the material. Injection valve 1 with gasoline resistant resin
It may be integrally molded with. As shown in FIG. 1c, the branch hole 3 is formed in a so-called elliptical elongated hole shape in which both ends of a rectangle are rounded. If the width of the oval branch hole 3 is B and the length is L, the width of the oval branch hole 3 is set narrow so that the relationship of B <L is satisfied. The fuel spray formed in this manner is split into two spray flows at the branch holes 3 and injected into the intake passage of the engine.
第2図は旋回流を発生させる動作原理を示し、第2図
(b)に示すように旋回流発生部(燃料通路の一部)20
の中心線からδ(スワラーオフセット)離れた位置に旋
回流発生部20の接線方向に複数の燃料通路21を配し、こ
の燃料通路21から旋回流発生部20に燃料を送ることで旋
回流を起こし噴霧を広がり形成することができる。噴霧
広がり角θ2は旋回速度成分を制御(スワラーオフセッ
トδを調整)することによって任意に変えることができ
る。FIG. 2 shows the principle of operation for generating a swirling flow. As shown in FIG. 2 (b), a swirling flow generating part (part of the fuel passage) 20
A plurality of fuel passages 21 are disposed at a position δ (swirler offset) away from the center line of the swirl flow generator 20 in the tangential direction of the swirl flow generator 20, and the fuel is sent from the fuel passage 21 to the swirl flow generator 20 to generate a swirl flow. The wake spray can be spread and formed. The spray spread angle θ 2 can be arbitrarily changed by controlling the swirling speed component (adjusting the swirler offset δ).
第3図、第4図に噴霧広がり角θ2と噴霧平均粒径の
関係を示した。第3図は、分岐部2aの広がり角θ1を24
度一定とし、θ2を変化させて噴霧平均粒径の度合いを
調べたピントル型での実験データで、θ2が大きくなる
に従い粒径が小さくなる。ただし、θ2を40度以上とす
ると噴霧が分岐孔3の長円端に集まり、4つの棒状の噴
霧を形成するようになるため粒径が大きくなるので、θ
2をθ1より大きくする場合には限界があることに注意を
要する。また、噴霧広がり角θ2が24度以下では前述の
合流(合体)が起こり粒径が大きくなる。第4図にはス
ワール型での実験データを示した。θ12を24度一定と
し、θ2を小さくするとピントル型の場合と同様に噴霧
の合流(合体)が起こり粒径が大きくなる。FIGS. 3 and 4 show the relationship between the spray divergence angle θ 2 and the spray average particle diameter. FIG. 3 shows that the spread angle θ 1 of the branch portion 2a is 24
And degree constant, the experimental data in the pintle type of examination of the degree of mist average particle diameter by changing the theta 2, the particle diameter becomes smaller as theta 2 increases. However, if θ 2 is set to 40 degrees or more, the spray gathers at the end of the ellipse of the branch hole 3 to form four rod-like sprays, so that the particle size increases.
Is 2 when greater than theta 1 takes note that there is a limit. Further, the spray divergence angle theta 2 is above confluence (coalescence) is occurs particle size becomes large in the following 24 degrees. FIG. 4 shows experimental data of the swirl type. When θ 12 is fixed at 24 degrees and θ 2 is reduced, the merging of the sprays (coalescence) occurs as in the case of the pintle type, and the particle size increases.
噴霧形成手段として本実施例のように旋回流により液
膜を広げるタイプの噴射弁を用いると、雰囲気温度が−
30℃のように低い場合でも、ピントル型に比べて粒径の
小さな噴霧を形成することができる。When an injection valve of the type that spreads the liquid film by swirling flow as in this embodiment is used as the spray forming means, the ambient temperature becomes
Even when the temperature is as low as 30 ° C., a spray having a smaller particle size can be formed as compared with the pintle type.
次に分岐孔3から噴出する噴霧流の形状について第5
図により説明する。第5図(a)は細長の分岐孔3を矢
印A方向から見たときの噴霧流を表し、この方向から見
た噴霧流は分岐孔3が幅狭なので扁平状を呈する。第5
図(b)は細長の分岐孔3を矢印B方向から見たときの
噴霧流を表し、この方向から見た噴霧流は分岐孔3が一
方向に長くしてあるため扇形に広がる。以上からすれば
2つの分岐孔3によって扁平な扇形の噴霧流が2つ形成
される。ここで各噴霧流の扁平方向の広がり角度を
θs1、長手方向の広がり角をθs2、2つの噴霧流の間の
角度をθs3とする。しかして、長円形断面通路の長軸が
吸気通路を流れる空気流に沿うようにして吸気通路壁面
に設置すれば、扁平な扇形噴霧流は空気流の受けにくい
方向に向くことになり、噴霧流が吸気通路の壁面側に空
気流の力で無理に押し流される事態を防止でき、燃料噴
霧を壁面に付着させずに目標位置に直接送ることができ
る。Next, the shape of the spray flow ejected from the branch hole 3
This will be described with reference to the drawings. FIG. 5A shows the spray flow when the elongated branch hole 3 is viewed from the direction of arrow A. The spray flow viewed from this direction has a flat shape because the branch hole 3 is narrow. Fifth
FIG. 2B shows the spray flow when the elongated branch hole 3 is viewed from the direction of arrow B. The spray flow viewed from this direction spreads in a fan shape because the branch hole 3 is elongated in one direction. As described above, two flat fan-shaped spray flows are formed by the two branch holes 3. Here, the spread angle of each spray flow in the flat direction is θ s1 , the spread angle in the longitudinal direction is θ s2 , and the angle between the two spray flows is θ s3 . However, if the long axis of the elliptical cross-section passage is set on the intake passage wall surface along the air flow flowing through the intake passage, the flat fan-shaped spray flow will be directed in a direction that is difficult to receive the air flow. Can be prevented from being forcibly swept away by the force of the air flow to the wall surface side of the intake passage, and the fuel spray can be directly sent to the target position without adhering to the wall surface.
第6図は従来の燃料供給装置を用いた場合の吸気通路
8内の燃料噴霧の様子を示す。燃料系の応答性を向上す
るためには、吸気弁6が開いているときに燃料を供給す
る必要がある。この場合エンジン回転数が高くなり吸気
通路8内の空気流速が大きくなると、従来は噴霧流の面
積のうち空気流の受ける部分が大きいので空気流によっ
て曲げられ、吸気通路8の内壁に付着する。そのため気
筒7内に流入する燃料が液状のまま流入することがあ
り、均質混合気の形成を阻害する要因となっている。FIG. 6 shows how fuel is sprayed in the intake passage 8 when a conventional fuel supply device is used. In order to improve the responsiveness of the fuel system, it is necessary to supply fuel when the intake valve 6 is open. In this case, when the engine speed is increased and the air flow velocity in the intake passage 8 is increased, the area of the spray flow that is conventionally received by the air flow is large, so that the spray flow is bent by the air flow and adheres to the inner wall of the intake passage 8. Therefore, the fuel flowing into the cylinder 7 may flow in a liquid state, which is a factor that hinders the formation of a homogeneous mixture.
第7図(a)、(b)に示すように、本実施例では燃
料噴射弁1から分岐孔を介して噴出される扁平噴霧流の
うち幅狭な噴霧角度θs1側を空気通路8の空気流に向
け、幅広な噴霧角度θs2を空気通路8の空気流と平行に
なるように、すなわち長円形断面通路の長軸が吸気通路
を流れる空気流に沿うようにして吸気通路壁面に設置す
れば、前述した如く扁平な扇形噴霧流が空気流の影響を
受けにくい方向に向くことになる。そして、このように
すれば噴霧流が空気流により曲げられることを極力防止
でき、噴霧流の進路を常に適正に保持し得るので吸気通
路8の壁面に燃料が付着しにくく、燃料が直ちに気筒7
に流入し蒸発が促進される。As shown in FIGS. 7A and 7B, in the present embodiment, the narrow spray angle θ s1 side of the flat spray flow ejected from the fuel injection valve 1 through the branch hole is connected to the air passage 8. A wide spray angle θ s2 is set on the intake passage wall so that the wide spray angle θ s2 is parallel to the air flow in the air passage 8, that is, the long axis of the oval cross-section passage is along the air flow flowing through the intake passage. Then, as described above, the flat fan-shaped spray flow is directed to a direction that is hardly affected by the air flow. In this way, the spray flow can be prevented from being bent by the air flow as much as possible, and the path of the spray flow can always be properly maintained, so that the fuel is less likely to adhere to the wall surface of the intake passage 8 and the fuel is immediately transferred to the cylinder 7.
And the evaporation is promoted.
[発明の効果] 本発明によれば、エンジンの運転条件や燃料噴射弁の
弁ストロークに左右されることなく分岐部に向かって確
実に中空円錐形の燃料噴霧パターンを形成でき、噴射燃
料が壁面に付着することなく微粒化の優れた燃料噴霧
(例えば100μm程度の噴霧)を送れるので、応答性の
良い燃料を供給することができる。よって、2つの吸気
弁から微粒化された燃料を気筒内に均一に供給できるの
で、気筒内に均質な混合気を供給でき、エンジン性能
(出力・燃費)を改善する効果がある。また、請求項
2、3により空気流の影響を受けずに燃料を目標位置に
直接送れるので、適正な燃料供給ができる。[Effects of the Invention] According to the present invention, a hollow cone-shaped fuel spray pattern can be reliably formed toward a branch portion without being influenced by engine operating conditions or the valve stroke of a fuel injection valve, and the injected fuel can be formed on a wall surface. A fuel spray with excellent atomization (for example, a spray of about 100 μm) can be sent without adhering to the fuel, so that a fuel with good responsiveness can be supplied. Therefore, atomized fuel can be uniformly supplied from the two intake valves into the cylinder, so that a homogeneous air-fuel mixture can be supplied into the cylinder, which has the effect of improving engine performance (output and fuel efficiency). According to the second and third aspects, the fuel can be directly sent to the target position without being affected by the air flow, so that an appropriate fuel supply can be performed.
第1図は本発明の実施例を示す要部断面図と,アダプタ
の位置関係と寸法を表す説明図である。第2図は旋回流
形成手段の動作説明図である。第3図は分岐分の広がり
角θ1=24度一定とした場合における噴霧粒径と燃料噴
霧広がり角θ2の関係を表す説明図であり、ピントル型
のデータである。第4図は第3図同様、噴霧粒径と燃料
噴霧広がり角θ2の関係を表す説明図であり、スワール
型のデータである。第5図は分岐孔の方向を変えて燃料
噴霧流の形状を見た説明図である。第6図は従来の問題
点を指摘した説明図である。第7図は2吸気弁タイプの
シリンダに適用した場合の動作説明図である。 [符号の説明] 1……燃料噴射弁、2……アダプタ、2a……分岐部、3
……分岐孔、6……吸気弁、7……シリンダ、8……吸
気通路FIG. 1 is a sectional view of an essential part showing an embodiment of the present invention, and an explanatory diagram showing a positional relationship and dimensions of an adapter. FIG. 2 is an explanatory view of the operation of the swirling flow forming means. FIG. 3 is an explanatory diagram showing the relationship between the spray particle diameter and the fuel spray spread angle θ 2 when the spread angle θ 1 = 24 degrees is constant, and is pintle type data. FIG. 4 is an explanatory diagram showing the relationship between the spray particle diameter and the fuel spray spread angle θ 2 , similarly to FIG. 3, and is swirl-type data. FIG. 5 is an explanatory view showing the shape of the fuel spray flow by changing the direction of the branch hole. FIG. 6 is an explanatory view showing a conventional problem. FIG. 7 is an explanatory view of the operation when applied to a two-intake valve type cylinder. [Explanation of Symbols] 1 ... Fuel injection valve, 2 ... Adapter, 2a ... Branch section, 3
... branch hole, 6 ... intake valve, 7 ... cylinder, 8 ... intake passage
───────────────────────────────────────────────────── フロントページの続き (72)発明者 柏谷 峰雄 茨城県勝田市大字高場2520番地 株式会 社日立製作所佐和工場内 (56)参考文献 特開 昭62−131969(JP,A) 特開 昭63−50667(JP,A) 特開 昭62−174563(JP,A) 特開 昭57−46062(JP,A) 特開 昭59−70871(JP,A) 特開 昭55−64151(JP,A) 実開 昭61−149772(JP,U) 実開 昭63−63573(JP,U) 実開 平1−179171(JP,U) 実開 昭61−164470(JP,U) 実開 平1−105768(JP,U) 実開 昭61−33966(JP,U) 実開 昭62−105363(JP,U) 実開 平1−148059(JP,U) 特公 昭62−3313(JP,B2) 特公 昭61−54948(JP,B2) 実公 昭60−1267(JP,Y2) (58)調査した分野(Int.Cl.6,DB名) F02M 61/18 F02M 69/04 F02M 61/06 F02M 51/08 F02M 51/06──────────────────────────────────────────────────続 き Continuation of the front page (72) Inventor Mineo Kashiwaya 2520, Oaza Takaba, Katsuta-shi, Ibaraki Prefecture Sawa Plant, Hitachi, Ltd. (56) References JP-A-62-131969 (JP, A) JP-A Sho JP-A-62-174563 (JP, A) JP-A-57-46062 (JP, A) JP-A-59-70871 (JP, A) JP-A-55-64151 (JP, A) A) Fully open 1986-149772 (JP, U) Fully open 1988-63573 (JP, U) Fully open 1-179171 (JP, U) Fully open 1986-164470 (JP, U) Fully open 1 -105768 (JP, U) Fully open sho 61-33966 (JP, U) Fully open sho 62-105363 (JP, U) Fully open flat 1-148059 (JP, U) Tokubo Sho 62-3313 (JP, B2 ) Tokuoyake Akira 61-54948 (JP, B2) real public Akira 60-1267 (JP, Y2) (58 ) investigated the field (Int.Cl. 6 , DB name) F02M 61/18 F02M 69/04 F02M 61/06 F02M 51/08 F02M 51/06
Claims (2)
を通して吸気通路に燃料を供給するガソリンエンジンの
燃料供給装置において、 前記燃料通路の出口部に形成された燃料噴孔から噴出す
る燃料を所定の開き角度をなす2方向の燃料流に分岐す
る分岐部と、 前記燃料噴孔上流の燃料通路に設けられた旋回流発生部
(20)と前記旋回流発生部(20)の中心線から所定のオ
フセット寸法だけ離れた位置に前記旋回流発生部(20)
の接線方向に配された複数の燃料通路(21)とから成る
旋回流形成手段とを備え、 前記燃料噴孔から噴出する燃料の噴霧広がり角(θ2)
を24度乃至40度になるように前記オフセット寸法を設定
したことを特徴とするガソリンエンジンの燃料供給装
置。1. A fuel supply device for a gasoline engine for supplying fuel to an intake passage through a fuel passage opened and closed by reciprocating movement of a valve body, wherein fuel injected from a fuel injection hole formed at an outlet of the fuel passage is supplied. A bifurcation branching into two directions of fuel flow having a predetermined opening angle; a swirl flow generating unit (20) provided in a fuel passage upstream of the fuel injection hole; and a center line of the swirl flow generating unit (20). The swirling flow generating section (20) at a position separated by a predetermined offset dimension
Swirling flow forming means comprising a plurality of fuel passages (21) arranged in a tangential direction of the fuel injection port, and a spray divergence angle (θ 2 ) of the fuel ejected from the fuel injection holes.
Wherein the offset dimension is set so as to be 24 to 40 degrees.
岐孔を有し、各分岐孔はその軸心に直角な断面形状が長
円形であって、それぞれの長軸が互いに平行に形成され
ていることを特徴とするガソリンエンジンの燃料供給装
置。2. The branch portion according to claim 1, wherein the branch portion has two branch holes, each of the branch holes has an oval cross section perpendicular to the axis thereof, and the respective long axes are formed parallel to each other. A fuel supply device for a gasoline engine, comprising:
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP63251822A JP2865677B2 (en) | 1988-10-07 | 1988-10-07 | Gasoline engine fuel supply system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP63251822A JP2865677B2 (en) | 1988-10-07 | 1988-10-07 | Gasoline engine fuel supply system |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPH0299758A JPH0299758A (en) | 1990-04-11 |
| JP2865677B2 true JP2865677B2 (en) | 1999-03-08 |
Family
ID=17228436
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP63251822A Expired - Fee Related JP2865677B2 (en) | 1988-10-07 | 1988-10-07 | Gasoline engine fuel supply system |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JP2865677B2 (en) |
Families Citing this family (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2619088B2 (en) * | 1989-12-28 | 1997-06-11 | 株式会社日立製作所 | Fuel injection device |
| JPH0681754A (en) * | 1992-07-16 | 1994-03-22 | Unisia Jecs Corp | Fuel injection valve |
| JP2652512B2 (en) * | 1994-03-25 | 1997-09-10 | 株式会社ケーヒン | Electromagnetic fuel injection valve |
| DE102004033283A1 (en) * | 2004-07-09 | 2006-02-02 | Robert Bosch Gmbh | Fuel injection valve for internal combustion engines |
| DE102005000620A1 (en) * | 2005-01-03 | 2006-07-13 | Robert Bosch Gmbh | Multi-fan jet nozzle and fuel injector with multi-fan jet nozzle |
Family Cites Families (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS61149772U (en) * | 1985-03-09 | 1986-09-16 | ||
| JPH0444845Y2 (en) * | 1985-03-30 | 1992-10-22 | ||
| JPS62131969A (en) * | 1985-12-02 | 1987-06-15 | Nippon Denso Co Ltd | Fuel injection valve |
| JPS6350667A (en) * | 1986-08-19 | 1988-03-03 | Aisan Ind Co Ltd | Nozzle structure for electromagnetic type fuel injection valve |
| JPS6363573U (en) * | 1986-10-16 | 1988-04-26 | ||
| JPH01105768U (en) * | 1987-12-29 | 1989-07-17 | ||
| JPH01179171U (en) * | 1988-06-07 | 1989-12-22 |
-
1988
- 1988-10-07 JP JP63251822A patent/JP2865677B2/en not_active Expired - Fee Related
Also Published As
| Publication number | Publication date |
|---|---|
| JPH0299758A (en) | 1990-04-11 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| JP3771361B2 (en) | Fuel injection valve | |
| US6382600B1 (en) | Device for introducing a reducing agent into an exhaust pipe segment of an internal combustion engine | |
| US4982716A (en) | Fuel injection valve with an air assist adapter for an internal combustion engine | |
| JP2996525B2 (en) | Fuel injection valve | |
| KR930004967B1 (en) | Electronic fuel injector | |
| US5516047A (en) | Electromagnetically actuated fuel injection valve | |
| DE2820695A1 (en) | FUEL SUPPLY DEVICE WORKING WITH A HOLLOW CYLINDER-SHAPED ULTRASONIC VIBRATING PART | |
| KR20000070784A (en) | A swirl generator in a fuel injector | |
| JPH01271656A (en) | Fuel injection valve | |
| JPS6350667A (en) | Nozzle structure for electromagnetic type fuel injection valve | |
| US10280885B2 (en) | Fluid injection valve and spray generator | |
| JPH07208303A (en) | Injection nozzle | |
| JP2865677B2 (en) | Gasoline engine fuel supply system | |
| JPH03202673A (en) | Fuel injection device | |
| JP4043966B2 (en) | Fuel injection valve | |
| JP2773095B2 (en) | Fuel injection valve | |
| JPS61272460A (en) | Electromagnetic type fuel injection valve | |
| JP2771254B2 (en) | Electromagnetic fuel injection valve | |
| JP2832555B2 (en) | Electromagnetic fuel injection valve | |
| US5411212A (en) | Fuel injection valve | |
| US5597121A (en) | Fuel injection valve | |
| JP3132283B2 (en) | Liquid injection valve | |
| JPH01273874A (en) | Feeding of fuel | |
| JP2725624B2 (en) | Fuel injection valve for internal combustion engine | |
| JPS6035169A (en) | fuel injection valve |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| LAPS | Cancellation because of no payment of annual fees |