JP6224754B2 - Electromagnetic fuel injection valve for in-cylinder injection - Google Patents

Electromagnetic fuel injection valve for in-cylinder injection Download PDF

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JP6224754B2
JP6224754B2 JP2016047125A JP2016047125A JP6224754B2 JP 6224754 B2 JP6224754 B2 JP 6224754B2 JP 2016047125 A JP2016047125 A JP 2016047125A JP 2016047125 A JP2016047125 A JP 2016047125A JP 6224754 B2 JP6224754 B2 JP 6224754B2
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fuel injection
valve
radius
diameter wall
cylinder
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JP2017160868A (en
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径裕 高橋
径裕 高橋
浩典 橋本
浩典 橋本
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Keihin Corp
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Priority to DE102017201448.2A priority patent/DE102017201448A1/en
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Description

本発明は、主として内燃機関の燃料供給系に使用される筒内噴射用電磁式燃料噴射弁に関し、特に、弁座及び環状に配列された複数の燃料噴孔を有して前記燃料噴孔から燃料を噴射する弁座部材と、前記弁座と協働して前記燃料噴孔を開閉する弁体とを備えた筒内噴射用電磁式燃料噴射弁の改良に関する。   The present invention relates to an in-cylinder injection electromagnetic fuel injection valve mainly used in a fuel supply system of an internal combustion engine, and in particular, has a valve seat and a plurality of annularly arranged fuel injection holes. The present invention relates to an improvement in an in-cylinder injection electromagnetic fuel injection valve that includes a valve seat member that injects fuel and a valve body that opens and closes the fuel injection hole in cooperation with the valve seat.

かゝる筒内噴射用電磁式燃料噴射弁は、下記特許文献1に開示されるように既に知られている。   Such an in-cylinder injection electromagnetic fuel injection valve is already known as disclosed in Patent Document 1 below.

特開2005−139989号公報JP 2005-13989 A

上記特許文献1に記載された筒内噴射用電磁式燃料噴射弁では、1つのインジェクタに、第1の角度をなす第1の噴孔と、第1の角度より大きい第2の角度をなし、第1の噴孔よりも貫徹力の小さい第2の噴孔とを設け、成層燃焼時は第1の噴孔から噴霧をキャビティを介して点火プラグ周りに集中させる一方、拡散燃焼時には第2の噴孔から噴霧を燃焼室全体に拡散させることで、成層燃焼時における混合気の層状化と、拡散燃焼時における混合気の均質化とを両立させている。   In the in-cylinder injection electromagnetic fuel injection valve described in Patent Document 1, a single injector has a first injection hole forming a first angle and a second angle larger than the first angle. A second nozzle hole having a penetrating force smaller than that of the first nozzle hole, and at the time of stratified combustion, the spray is concentrated around the spark plug through the cavity while the second nozzle is used at the time of diffusion combustion. By diffusing the spray from the nozzle hole to the entire combustion chamber, the stratification of the air-fuel mixture during stratified combustion and the homogenization of the air-fuel mixture during diffusion combustion are compatible.

このものでは、第2の噴孔の貫徹力を第1の噴孔の貫徹力よりも低減させるために噴孔の孔径を縮小させているが、噴孔の孔径を縮小させると流量が減少するので、貫徹力を低減させつつある程度以上の流量を確保することが困難となり、様々な燃焼形態や噴霧形態が要求される近年の実態と合わない事態が生じる虞がある。   In this case, the hole diameter of the nozzle hole is reduced in order to reduce the penetrating force of the second nozzle hole more than the penetrating force of the first nozzle hole, but the flow rate decreases when the hole diameter of the nozzle hole is reduced. Therefore, it is difficult to secure a flow rate of a certain level while reducing the penetration force, and there is a possibility that a situation that does not match the actual situation in recent years where various combustion forms and spray forms are required may occur.

本発明は、かゝる事情に鑑みてなされたもので、貫徹力を低減させた場合であっても必要な流量を確保し得るようにした、筒内噴射用電磁式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 such circumstances, and provides an in-cylinder injection electromagnetic fuel injection valve capable of ensuring a necessary flow rate even when penetrating force is reduced. For the purpose.

上記目的を達成するために、本発明は、弁座及び該弁座近傍に環状に配列された複数の燃料噴孔を有して前記燃料噴孔から燃料を噴射する弁座部材と、前記弁座と協働して前記燃料噴孔を開閉する弁体とを備えた筒内噴射用電磁式燃料噴射弁において、全ての前記燃料噴孔は長軸と短軸とを有する長孔であって、前記長軸は、その長手方向両端部を前記燃料噴孔の入口のピッチ円の中心側に向けて円弧状に湾曲しており、前記長軸の半径は、前記ピッチ円の半径よりも小さく、前記燃料噴孔の下流端は、前記弁座部材に形成された凹部の底面に開口することを第1の特徴とする。 In order to achieve the above object, the present invention provides a valve seat and a valve seat member having a plurality of fuel injection holes arranged annularly in the vicinity of the valve seat and injecting fuel from the fuel injection holes, and the valve In the in-cylinder injection electromagnetic fuel injection valve including a valve body that opens and closes the fuel injection hole in cooperation with a seat, all the fuel injection holes are long holes having a long axis and a short axis. , the long axis is curved in an arc shape that both longitudinal ends toward the center of the pitch circle of the inlet of the fuel injection hole, the radius of the long axis, the radius of the front Kipi pitch circle rather smaller than, a downstream end of the fuel injection hole, the first, characterized in that opening into the bottom surface of the recess formed in the valve seat member.

また本発明は、第1の特徴に加えて、前記燃料噴孔は、前記長軸の半径よりも大きい半径の大径壁と、前記長軸の半径よりも小さい半径の小径壁と、これら大径壁および小径壁を接続する接続壁とから構成されることを第2の特徴とする。   According to the present invention, in addition to the first feature, the fuel injection hole includes a large-diameter wall having a radius larger than the radius of the major axis, a small-diameter wall having a radius smaller than the radius of the major axis, A second feature is that it is composed of a connecting wall connecting the diameter wall and the small diameter wall.

さらに本発明は、第2の特徴に加えて、前記大径壁を構成する仮想円と、前記小径壁を構成する仮想円とが同一の中心を有することを第3の特徴とする。   Furthermore, in addition to the second feature, the third feature of the present invention is that a virtual circle constituting the large-diameter wall and a virtual circle constituting the small-diameter wall have the same center.

さらにまた本発明は、第1ないし第3の何れかの特徴に加えて、全ての前記燃料噴孔の入口が、単一の前記ピッチ円上に配置されることを第4の特徴とする。   Furthermore, in addition to any one of the first to third features, the present invention is characterized in that the inlets of all the fuel injection holes are arranged on a single pitch circle.

本発明の第1の特徴によれば、燃料噴孔が長軸と短軸とを有する長孔で、長軸が円弧状に湾曲しており、該長軸の半径は燃料噴孔の入口のピッチ円の半径よりも小さいので、燃料噴孔の内周壁も前記ピッチ円の半径よりも小さい半径で湾曲することになる。そのため噴射される燃料が湾曲した燃料噴孔の内周壁に沿って移動し、燃料噴孔内部で渦を巻くように乱流が発生するから、該発生した乱流によって貫徹力が低減される。そしてこの貫徹力の低減は、燃料噴孔の小径化によって行われるのでなく、燃料噴孔の形状の変更によって行われるので、長軸及び短軸の寸法を拡大させて流量を確保した場合でも、発生した乱流によって貫徹力を低減させることが可能となる。   According to the first feature of the present invention, the fuel injection hole is a long hole having a major axis and a minor axis, and the major axis is curved in an arc shape, and the radius of the major axis is the inlet of the fuel injection hole. Since it is smaller than the radius of the pitch circle, the inner peripheral wall of the fuel injection hole is also curved with a radius smaller than the radius of the pitch circle. Therefore, the injected fuel moves along the inner peripheral wall of the curved fuel injection hole, and turbulent flow is generated so as to vortex inside the fuel injection hole. Therefore, the penetration force is reduced by the generated turbulent flow. And this reduction of penetration force is not performed by reducing the diameter of the fuel injection hole, but by changing the shape of the fuel injection hole, even if the major axis and the minor axis are enlarged to ensure the flow rate, The penetrating force can be reduced by the generated turbulent flow.

また、燃料噴孔の下流端は、弁座部材に形成された凹部の底面に開口しているので、燃料噴孔の下流端を他部材との接触から保護することができる。Moreover, since the downstream end of the fuel injection hole is open to the bottom surface of the recess formed in the valve seat member, the downstream end of the fuel injection hole can be protected from contact with other members.

本発明の第2の特徴によれば、燃料噴孔が、長軸の半径よりも大きい半径の大径壁と、長軸の半径よりも小さい半径の小径壁と、これら大径壁および小径壁を接続する接続壁とから構成されるので、曲率の小さい大径壁側からは燃料噴孔内に燃料が入り易くなり、曲率の大きい小径壁側からは入り難くなる。そのため、動きの異なる燃料が燃料噴孔内で衝突することで、より大きな乱流を発生させることができるので、貫徹力を更に低減させることができる。   According to the second feature of the present invention, the fuel injection hole has a large-diameter wall having a radius larger than the radius of the long axis, a small-diameter wall having a radius smaller than the radius of the long-axis, and the large-diameter wall and the small-diameter wall. Therefore, the fuel can easily enter the fuel injection hole from the large-diameter wall side having a small curvature, and difficult to enter from the small-diameter wall side having a large curvature. Therefore, since the fuel with different motion collides in the fuel nozzle hole, it is possible to generate a larger turbulent flow, so that the penetration force can be further reduced.

本発明の第3の特徴によれば、大径壁を構成する仮想円と、小径壁を構成する仮想円とが同一の中心を有するので、短軸の長さが燃料噴孔の周方向で一定となって噴射流量の管理が容易となる。   According to the third feature of the present invention, since the virtual circle constituting the large-diameter wall and the virtual circle constituting the small-diameter wall have the same center, the length of the short axis is in the circumferential direction of the fuel injection hole. It becomes constant and management of the injection flow rate becomes easy.

本発明の第4の特徴によれば、全ての燃料噴孔の入口を、単一のピッチ円上に配置したので、各燃料噴孔から噴射される燃料の貫徹力及び噴射流量を均等化できる。   According to the fourth feature of the present invention, since the inlets of all the fuel injection holes are arranged on a single pitch circle, the penetration force and the injection flow rate of the fuel injected from each fuel injection hole can be equalized. .

本発明の実施形態に係る筒内噴射用電磁式燃料噴射弁の縦断側面図。1 is a longitudinal side view of an in-cylinder injection electromagnetic fuel injection valve according to an embodiment of the present invention. 図1の弁座部材の拡大断面図。The expanded sectional view of the valve seat member of FIG. 図2の3−3矢視図。FIG. 3 is a view taken along arrow 3-3 in FIG. 2.

図1において、エンジンのシリンダヘッドEには、燃焼室Eaに開口する装着孔Ebが設けられており、この装着孔Ebに筒内噴射用電磁式燃料噴射弁Iが装着される。この燃料噴射弁Iは、燃焼室Eaに向かって燃料を噴射し得る。尚、燃料噴射弁Iにおいて、燃料の噴射側を前方、燃料の流入側を後方とする。   In FIG. 1, the cylinder head E of the engine is provided with a mounting hole Eb that opens to the combustion chamber Ea, and the in-cylinder injection electromagnetic fuel injection valve I is mounted in the mounting hole Eb. The fuel injection valve I can inject fuel toward the combustion chamber Ea. In the fuel injection valve I, the fuel injection side is the front and the fuel inflow side is the rear.

この燃料噴射弁Iの弁ハウジング1は、中空円筒状の弁ハウジングボディ2と、この弁ハウジングボディ2の前端部内周面に嵌合して溶接される有底円筒状の弁座部材3と、弁ハウジングボディ2後端の大径部2aの外周に嵌合して溶接される磁性円筒体4と、この磁性円筒体4の後端に同軸に結合される非磁性円筒体5とで構成される。非磁性円筒体5の後端には固定コア6が同軸に結合され、この固定コア6の後端に燃料入口筒7が同軸に一体に連設される。固定コア6は、燃料入口筒7の内部に連通する中空部6aを有する。   A valve housing 1 of the fuel injection valve I includes a hollow cylindrical valve housing body 2, a bottomed cylindrical valve seat member 3 fitted and welded to the inner peripheral surface of the front end portion of the valve housing body 2, The magnetic cylinder 4 is fitted to the outer periphery of the large-diameter portion 2a at the rear end of the valve housing body 2 and welded thereto, and the non-magnetic cylinder 5 is coaxially coupled to the rear end of the magnetic cylinder 4. The A fixed core 6 is coaxially coupled to the rear end of the nonmagnetic cylindrical body 5, and a fuel inlet cylinder 7 is coaxially and continuously connected to the rear end of the fixed core 6. The fixed core 6 has a hollow portion 6 a communicating with the inside of the fuel inlet cylinder 7.

磁性円筒体4は、軸方向中間部にフランジ状のヨーク部4aを一体に有しており、このヨーク部4aが、シリンダヘッドEの前記装着孔Ebの上端開口部を囲繞する荷重受け孔Ecにクッション部材Cを介して支承され、燃料入口筒7の入口には燃料フィルタ8が装着される。   The magnetic cylindrical body 4 integrally has a flange-like yoke portion 4a at an axially intermediate portion, and this yoke portion 4a surrounds the upper end opening of the mounting hole Eb of the cylinder head E. The fuel filter 8 is attached to the inlet of the fuel inlet cylinder 7.

図2,図3を更に参照して、有底円筒状の弁座部材3は、その前端壁3aに円錐状の弁座9と、環状に配列されてこの弁座9の中心近傍に開口する複数の燃料噴孔10とを有する。   2 and 3, the bottomed cylindrical valve seat member 3 has a conical valve seat 9 on the front end wall 3a thereof, and is annularly arranged so as to open near the center of the valve seat 9. A plurality of fuel injection holes 10.

全ての燃料噴孔10は長軸11と短軸12とを有する長孔であって、長軸11は、その長手方向両端部を燃料噴孔10の入口のピッチ円Pの中心O側に向けて円弧状に湾曲している。また燃料噴孔10の入口は1つのピッチ円P上に等間隔に配置されており、長軸11の半径R1は該ピッチ円Pの半径R2よりも小さい。なお、これら燃料噴孔10の入口は複数のピッチ円P上に分かれて配置されていても良く、その間隔は等間隔でなくても良い。 All the fuel injection holes 10 are long holes having a major axis 11 and a minor axis 12, and the major axis 11 has its both longitudinal ends directed toward the center O side of the pitch circle P at the inlet of the fuel injection hole 10. Are curved in an arc. Further, the inlets of the fuel injection holes 10 are arranged at equal intervals on one pitch circle P, and the radius R1 of the long axis 11 is smaller than the radius R2 of the pitch circle P. The inlets of the fuel injection holes 10 may be arranged separately on a plurality of pitch circles P, and the intervals may not be equal.

燃料噴孔10の短軸12は、前記ピッチ円Pの中心Oから半径方向に延びる直線に沿って配置されており、燃料噴孔10の長軸11と前記ピッチ円Pとは燃料噴孔10の中心位置で接している。なお、該短軸12を前記直線に対して傾斜するように配置することも可能であり、その場合における該短軸12の前記直線に対する傾斜角は、全て同一であっても、相互に異なっていても良い。   The short axis 12 of the fuel injection hole 10 is arranged along a straight line extending in the radial direction from the center O of the pitch circle P. The long axis 11 of the fuel injection hole 10 and the pitch circle P are the fuel injection hole 10. It touches at the center position. It is also possible to arrange the minor axis 12 so as to be inclined with respect to the straight line. In this case, the inclination angles of the minor axis 12 with respect to the straight line are all the same, but are different from each other. May be.

燃料噴孔10は、長軸11の半径R1よりも大きい半径R3の大径壁10aと、長軸11の半径R1よりも小さい半径R4の小径壁10bと、これら大径壁10aおよび小径壁10bを接続する接続壁10cとから構成されており、大径壁10aを構成する仮想円Aと、小径壁10bを構成する仮想円Bとは同一の中心O′を有するが、これらの円A,Bの中心は異なる位置にあっても良い。   The fuel injection hole 10 includes a large-diameter wall 10a having a radius R3 larger than the radius R1 of the long axis 11, a small-diameter wall 10b having a radius R4 smaller than the radius R1 of the long-axis 11, and the large-diameter wall 10a and the small-diameter wall 10b. The virtual circle A constituting the large-diameter wall 10a and the virtual circle B constituting the small-diameter wall 10b have the same center O ′, but these circles A, The center of B may be at a different position.

弁座部材3の前端壁3aには、燃料噴孔10の軸線lに直交する底面14を有する凹部13が前側から形成されており、この凹部13の底面14に燃料噴孔10の下流端が開口する。   A recess 13 having a bottom surface 14 perpendicular to the axis l of the fuel injection hole 10 is formed on the front end wall 3 a of the valve seat member 3 from the front side, and the downstream end of the fuel injection hole 10 is formed on the bottom surface 14 of the recess 13. Open.

弁座部材3から非磁性円筒体5に至る弁ハウジング1内には弁体15及び可動コア16よりなる弁組立体17が収容される。弁体15は、前記弁座9と協働して燃料噴孔10を開閉する球状の弁部15aと、この弁部15aを支持して固定コア6の中空部6aまで延出する弁杆15bとで構成される。その弁部15aは、弁座部材3の内周面に摺動自在に支承されるよう球状に形成され、その外周面には、燃料の流通を可能にする複数の平坦部が設けられる。また可動コア16の半径方向中間部にも、燃料の流通する燃料通路16aが設けられる。   A valve assembly 17 including a valve body 15 and a movable core 16 is accommodated in the valve housing 1 extending from the valve seat member 3 to the nonmagnetic cylindrical body 5. The valve body 15 includes a spherical valve portion 15 a that opens and closes the fuel injection hole 10 in cooperation with the valve seat 9, and a valve rod 15 b that supports the valve portion 15 a and extends to the hollow portion 6 a of the fixed core 6. It consists of. The valve portion 15a is formed in a spherical shape so as to be slidably supported on the inner peripheral surface of the valve seat member 3, and a plurality of flat portions that allow fuel to flow are provided on the outer peripheral surface. Further, a fuel passage 16a through which fuel flows is also provided in the intermediate portion in the radial direction of the movable core 16.

固定コア6の内周面には、円筒状のガイドブッシュ18が圧入される。その際、ガイドブッシュ18は、その前端部が固定コア6の前端面、即ち吸引面6bより僅かに突出するように配置される。   A cylindrical guide bush 18 is press-fitted into the inner peripheral surface of the fixed core 6. At this time, the guide bush 18 is disposed such that its front end portion slightly protrudes from the front end surface of the fixed core 6, that is, the suction surface 6 b.

前記弁杆15bには、前記ガイドブッシュ18の内周面に摺動自在に嵌合する摺動部材19と、前記可動コア16及び前記弁部15a間に配置されるストッパ部材20とが溶接等により固設され、摺動部材19は、その下端面が弁体15の閉弁位置では前記ガイドブッシュ18の下端面より突出するように配置される。そして固定コア6の吸引面6bに対置される可動コア16は、これが上記摺動部材19及びストッパ部材20間で限られたストロークを移動し得るように弁杆15bに摺動自在に嵌装される。   A sliding member 19 slidably fitted to the inner peripheral surface of the guide bush 18 and a stopper member 20 disposed between the movable core 16 and the valve portion 15a are welded to the valve rod 15b. The sliding member 19 is disposed so that its lower end surface protrudes from the lower end surface of the guide bush 18 at the valve closing position of the valve body 15. The movable core 16 facing the suction surface 6b of the fixed core 6 is slidably fitted to the valve rod 15b so that it can move a limited stroke between the sliding member 19 and the stopper member 20. The

ガイドブッシュ18及び摺動部材19は、固定コア6より硬度が高い非磁性又は弱磁性材料、例えばマルテンサイト系のステンレス鋼で構成される。したがってガイドブッシュ18及び摺動部材19の硬度は略同等にされる。   The guide bush 18 and the sliding member 19 are made of a nonmagnetic or weak magnetic material having a higher hardness than the fixed core 6, for example, martensitic stainless steel. Therefore, the hardness of the guide bush 18 and the sliding member 19 is made substantially equal.

固定コア6の中空部6aにはパイプ状のリテーナ21が嵌挿されてかしめ固定され、このリテーナ21と摺動部材19との間に弁体15を弁座9への着座方向、即ち閉弁方向へ付勢する弁ばね22が縮設される。その際、リテーナ21の固定コア6への嵌挿深さにより弁ばね22のセット荷重が調整される。摺動部材19は、前述のように固定コア6より高硬度であるから、弁ばね22のばね座となる箇所は、耐摩耗の高いものとなる。   A pipe-like retainer 21 is fitted into the hollow portion 6a of the fixed core 6 and fixed by caulking, and the valve element 15 is seated on the valve seat 9 between the retainer 21 and the sliding member 19, that is, the valve is closed. A valve spring 22 that biases in the direction is retracted. At that time, the set load of the valve spring 22 is adjusted by the insertion depth of the retainer 21 into the fixed core 6. Since the sliding member 19 is harder than the fixed core 6 as described above, the portion serving as the spring seat of the valve spring 22 has high wear resistance.

また、摺動部材19と可動コア16との間には補助ばね23が縮設され、この補助ばね23は、上記弁ばね22のセット荷重より小さいセット荷重で摺動部材19及び可動コア16を離間させるように作用する。   Further, an auxiliary spring 23 is contracted between the sliding member 19 and the movable core 16, and the auxiliary spring 23 causes the sliding member 19 and the movable core 16 to move with a set load smaller than the set load of the valve spring 22. Acts to separate.

前記弁杆15bの後端部は、摺動部材19の後端面より突出し、弁ばね22の可動端部の内周面に嵌合して、その位置決めの役割を果たすと共に、摺動部材19は、補助ばね23の内周面に嵌合して、その位置決めの役割を果たす。また、前記摺動部材19の外周には、燃料流路となる複数の切欠きが設けられる。   The rear end portion of the valve rod 15b protrudes from the rear end surface of the sliding member 19, is fitted to the inner peripheral surface of the movable end portion of the valve spring 22, plays a role of positioning, and the sliding member 19 It is fitted to the inner peripheral surface of the auxiliary spring 23 and plays the role of positioning. A plurality of notches serving as fuel flow paths are provided on the outer periphery of the sliding member 19.

磁性円筒体4の後端部から固定コア6に至る外周面にコイル組立体24が嵌装される。このコイル組立体24は、上記外周面に嵌合するボビン25と、これに巻装されるコイル26とからなっており、このコイル組立体24を収容するコイルハウジング27の前端部が磁性円筒体4の前記ヨーク4a上に載置され、溶接される。   A coil assembly 24 is fitted on the outer peripheral surface from the rear end portion of the magnetic cylindrical body 4 to the fixed core 6. The coil assembly 24 includes a bobbin 25 fitted to the outer peripheral surface and a coil 26 wound around the bobbin 25, and a front end portion of a coil housing 27 that houses the coil assembly 24 is a magnetic cylindrical body. 4 is placed on the yoke 4a and welded.

コイルハウジング27の後端部から固定コア6の後端部にわたりそれらの外周面を被覆する合成樹脂製の被覆層28がモールド成形される。この被覆層28には、固定コア6の一側方に張り出すカプラ29が一体に連設され、このカプラ29により、コイル26に連なる端子30が保持される。   A covering layer 28 made of synthetic resin is molded from the rear end portion of the coil housing 27 to the rear end portion of the fixed core 6 so as to cover the outer peripheral surfaces thereof. A coupler 29 extending to one side of the fixed core 6 is integrally connected to the covering layer 28, and the terminal 30 connected to the coil 26 is held by the coupler 29.

次に、この実施形態の作用について説明する。   Next, the operation of this embodiment will be described.

コイル26の非通電状態では、弁体15は、弁ばね22のセット荷重により前方に押圧され、弁座9に着座して燃料噴孔10を閉鎖する。即ち閉弁状態にあり、可動コア16は、固定コア6の吸引面6bより突出したガイドブッシュ18の前端との間に所定のギャップを保っている。   In the non-energized state of the coil 26, the valve body 15 is pressed forward by the set load of the valve spring 22 and is seated on the valve seat 9 to close the fuel injection hole 10. That is, the movable core 16 is in a closed state, and a predetermined gap is maintained between the movable core 16 and the front end of the guide bush 18 protruding from the suction surface 6 b of the fixed core 6.

コイル26に通電すると、それにより生ずる磁束が固定コア6,コイルハウジング27,磁性円筒体4及び可動コア16を順次走り、その磁力により、先ず可動コア16が固定コア6に吸引され、補助ばね23を圧縮しながら摺動部材19の前端に当接する。このとき可動コア16は、補助ばね23の弱いセット荷重に抗して上昇・加速しながら摺動部材19に当接し、摺動部材19を弁ばね22のセット荷重に抗して速やかに後方へ押し上げて、ガイドブッシュ18の前端に衝突して停止する。その間、後方へ押し上げられる摺動部材19は、それと一体化された弁杆15bを伴なうので、弁体15の開弁応答性が高められる。   When the coil 26 is energized, the magnetic flux generated thereby sequentially travels through the fixed core 6, the coil housing 27, the magnetic cylindrical body 4, and the movable core 16, and by this magnetic force, the movable core 16 is first attracted to the fixed core 6 and the auxiliary spring 23. Is brought into contact with the front end of the sliding member 19 while being compressed. At this time, the movable core 16 abuts against the sliding member 19 while rising and accelerating against the weak set load of the auxiliary spring 23, and promptly moves the sliding member 19 backward against the set load of the valve spring 22. It pushes up and collides with the front end of the guide bush 18 and stops. Meanwhile, the sliding member 19 pushed upward is accompanied by the valve rod 15b integrated therewith, so that the valve opening response of the valve body 15 is enhanced.

可動コア16が摺動部材19を押し上げながらガイドブッシュ18の前端に当接することで、弁体15は所定の開弁位置に保持される。   The movable core 16 abuts against the front end of the guide bush 18 while pushing up the sliding member 19, whereby the valve body 15 is held at a predetermined valve opening position.

弁体15が開弁すると、図示せぬ燃料分配管から燃料入口筒7に圧送された高圧の燃料は、パイプ状のリテーナ21内部,固定コア6の中空部6a,摺動部材19の切欠き,可動コア16の燃料通路16a,弁ハウジング1の内部,弁座9を順次経て燃料噴孔10からエンジンの燃焼室Eaに直接噴射される。   When the valve body 15 is opened, the high-pressure fuel pumped from the fuel distribution pipe (not shown) to the fuel inlet cylinder 7 is inside the pipe-shaped retainer 21, the hollow portion 6 a of the fixed core 6, and the notch of the sliding member 19. The fuel passage 16a of the movable core 16, the inside of the valve housing 1, and the valve seat 9 are sequentially injected from the fuel injection hole 10 into the combustion chamber Ea of the engine.

このとき、 全ての燃料噴孔10が長軸11と短軸12とを有する長孔であって、長軸11が、その長手方向両端部を燃料噴孔10の入口のピッチ円Pの中心O側に向けて円弧状に湾曲しており、長軸11の半径はピッチ円Pの半径よりも小さいので、燃料噴孔10の内周壁10a,10bもピッチ円の半径よりも小さい半径で湾曲することになる。そのため噴射される燃料が湾曲した燃料噴孔10の内周壁10a〜10cに沿って移動し、燃料噴孔10内部で渦を巻くように乱流が発生するから、該発生した乱流によって貫徹力が低減される。そしてこの貫徹力の低減は、燃料噴孔10の小径化によって行われるのでなく、燃料噴孔10の形状の変更によって行われるので、長軸11及び短軸12の寸法を拡大させて流量を確保した場合でも、発生した乱流によって貫徹力を低減させることが可能となる。 At this time, all the fuel injection holes 10 are long holes having a major axis 11 and a minor axis 12, and the major axis 11 has both longitudinal ends at the center O of the pitch circle P at the inlet of the fuel injection hole 10. towards the side is curved in an arc shape, because the radius of the major axis 11 is smaller than the radius of the pitch circle P, the inner peripheral wall 10a of the fuel injection hole 10, 10b is also curved with a radius smaller than the radius of the pitch circle Will do. Therefore, the injected fuel moves along the inner peripheral walls 10a to 10c of the curved fuel injection hole 10, and a turbulent flow is generated so as to make a vortex inside the fuel injection hole 10. Therefore, the penetration force is generated by the generated turbulent flow. Is reduced. The penetration force is not reduced by reducing the diameter of the fuel injection hole 10, but by changing the shape of the fuel injection hole 10. Therefore, the dimensions of the long axis 11 and the short axis 12 are enlarged to secure the flow rate. Even in this case, the penetration force can be reduced by the generated turbulent flow.

特に本実施形態においては、燃料噴孔10が、長軸11の半径よりも大きい半径の大径壁10aと、長軸11の半径よりも小さい半径の小径壁10bと、これら大径壁10aおよび小径壁10bを接続する接続壁10cとから構成されているので、曲率の小さい大径壁10a側からは燃料噴孔10内に燃料が入り易くなり、曲率の大きい小径壁10b側からは入り難くなる。そのため、動きの異なる燃料が燃料噴孔10内で衝突することで、より大きな乱流を発生させることができて、貫徹力を更に低減させることができる。   Particularly in this embodiment, the fuel injection hole 10 has a large-diameter wall 10a having a radius larger than the radius of the long axis 11, a small-diameter wall 10b having a radius smaller than the radius of the long axis 11, and the large-diameter wall 10a and Since the connecting wall 10c is connected to the small-diameter wall 10b, the fuel can easily enter the fuel injection hole 10 from the large-diameter wall 10a side having a small curvature, and is difficult to enter from the small-diameter wall 10b side having a large curvature. Become. For this reason, the fuel having different motion collides in the fuel injection hole 10, so that a larger turbulent flow can be generated and the penetration force can be further reduced.

しかも、大径壁10aを構成する仮想円Aと、小径壁10bを構成する仮想円Bとは同一の中心O′を有するので、短軸12の長さが燃料噴孔10の周方向で一定となって噴射流量の管理が容易となるとともに、複数の燃料噴孔10の入口を、単一のピッチ円P上に配置したので、各燃料噴孔10から噴射される燃料の貫徹力及び噴射流量を均等化できる。   Moreover, since the virtual circle A constituting the large-diameter wall 10a and the virtual circle B constituting the small-diameter wall 10b have the same center O ′, the length of the short axis 12 is constant in the circumferential direction of the fuel injection hole 10. Thus, the injection flow rate can be easily managed, and the inlets of the plurality of fuel injection holes 10 are arranged on a single pitch circle P. Therefore, the penetration force and injection of the fuel injected from each fuel injection hole 10 The flow rate can be equalized.

また更に、弁座部材3の前端壁3aには、燃料噴孔10の軸線lに直交する底面14を有する凹部13が前方から穿設されており、この凹部13の底面14に燃料噴孔10の下流端が開口しているので、燃料噴孔10の下流端を他部材との接触から保護することができる。   Furthermore, a recess 13 having a bottom surface 14 perpendicular to the axis l of the fuel injection hole 10 is formed in the front end wall 3a of the valve seat member 3 from the front, and the fuel injection hole 10 is formed in the bottom surface 14 of the recess 13. Therefore, the downstream end of the fuel injection hole 10 can be protected from contact with other members.

本発明は上記実施形態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。例えば、上記実施形態では可動コア16を摺動部材19及びストッパ部材20間で移動可能としているが、この可動コア16を弁杆15bに固定することもできる The present invention is not limited to the above-described embodiment, and various design changes can be made without departing from the gist thereof. For example, although the movable core 16 is movable between the sliding member 19 and the stopper member 20 in the above embodiment, the movable core 16 can be fixed to the valve rod 15b .

3・・・・・・弁座部材
9・・・・・・弁座
10・・・・・燃料噴孔
10a・・・・大径壁
10b・・・・小径壁
10c・・・・接続壁
11・・・・・長軸
12・・・・・短軸
15・・・・・弁体
A・・・・・・大径壁を構成する仮想円
B・・・・・・小径壁を構成する仮想円
O′・・・・・両仮想円の中心
P・・・・・・ピッチ円
R1・・・・・長軸の半径
R2・・・・・ピッチ円の半径
R3・・・・・大径壁の半径
R4・・・・・小径壁の半径
3 ... Valve seat member 9 ... Valve seat 10 ... Fuel injection hole 10a ... Large diameter wall 10b ... Small diameter wall 10c ... Connection wall 11... Long axis 12... Short axis 15... Valve body A... Virtual circle B constituting a large diameter wall. Imaginary circle O '... center P of both imaginary circles ... pitch circle R1 ... radius of major axis R2 ... radius of pitch circle R3 ... Radius of large diameter wall R4 ... Radius of small diameter wall

Claims (4)

弁座(9)及び該弁座(9)近傍に環状に配列された複数の燃料噴孔(10)を有して前記燃料噴孔(10)から燃料を噴射する弁座部材(3)と、前記弁座(9)と協働して前記燃料噴孔(10)を開閉する弁体(15)とを備えた筒内噴射用電磁式燃料噴射弁において、
全ての前記燃料噴孔(10)は長軸(11)と短軸(12)とを有する長孔であって、前記長軸(11)は、その長手方向両端部を前記燃料噴孔(10)の入口のピッチ円(P)の中心(O)側に向けて円弧状に湾曲しており、前記長軸(11)の半径(R1)は、前記ピッチ円(P)の半径(R2)よりも小さく、
前記燃料噴孔(10)の下流端は、前記弁座部材(3)に形成された凹部(13)の底面に開口することを特徴とする筒内噴射用電磁式燃料噴射弁。
A valve seat (9) and a valve seat member (3) having a plurality of fuel injection holes (10) arranged annularly in the vicinity of the valve seat (9) and injecting fuel from the fuel injection holes (10); In-cylinder injection electromagnetic fuel injection valve comprising a valve body (15) for opening and closing the fuel injection hole (10) in cooperation with the valve seat (9),
All the fuel injection holes (10) are long holes having a major axis (11) and a minor axis (12), and the major axis (11) has both end portions in the longitudinal direction at the fuel injection holes (10). entrance of the pitch circle of) (is curved in an arc shape toward the center (O) side of the P), a radius (R1) of the long axis (11), the radius of the front Kipi pitch yen (P) rather smaller than (R2),
An in-cylinder injection electromagnetic fuel injection valve characterized in that the downstream end of the fuel injection hole (10) opens at the bottom of a recess (13) formed in the valve seat member (3) .
前記燃料噴孔(10)は、前記長軸(11)の半径(R1)よりも大きい半径(R3)の大径壁(10a)と、前記長軸(11)の半径(R1)よりも小さい半径(R4)の小径壁(10b)と、これら大径壁(10a)および小径壁(10b)を接続する接続壁(10c)とから構成されることを特徴とする請求項1記載の筒内噴射用電磁式燃料噴射弁。   The fuel injection hole (10) has a large-diameter wall (10a) having a radius (R3) larger than the radius (R1) of the long axis (11) and a radius (R1) of the long axis (11). The in-cylinder assembly according to claim 1, comprising a small-diameter wall (10b) having a radius (R4) and a connecting wall (10c) connecting the large-diameter wall (10a) and the small-diameter wall (10b). Electromagnetic fuel injection valve for injection. 前記大径壁(10a)を構成する仮想円(A)と、前記小径壁(10b)を構成する仮想円(B)とが同一の中心(O′)を有することを特徴とする請求項2記載の筒内噴射用電磁式燃料噴射弁。   The virtual circle (A) constituting the large diameter wall (10a) and the virtual circle (B) constituting the small diameter wall (10b) have the same center (O '). The in-cylinder injecting electromagnetic fuel injection valve. 全ての前記燃料噴孔(10)の入口が、単一の前記ピッチ円(P)上に配置されることを特徴とする請求項1ないし請求項3の何れかに記載の筒内噴射用電磁式燃料噴射弁。   The in-cylinder injection electromagnetic according to any one of claims 1 to 3, wherein the inlets of all the fuel injection holes (10) are arranged on a single pitch circle (P). Fuel injection valve.
JP2016047125A 2016-03-10 2016-03-10 Electromagnetic fuel injection valve for in-cylinder injection Expired - Fee Related JP6224754B2 (en)

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US15/416,199 US10344727B2 (en) 2016-03-10 2017-01-26 Electromagnetic fuel injection valve for in-cylinder injection
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