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JP4191760B2 - Fuel injection valve - Google Patents
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JP4191760B2 - Fuel injection valve - Google Patents

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JP4191760B2
JP4191760B2 JP2006303711A JP2006303711A JP4191760B2 JP 4191760 B2 JP4191760 B2 JP 4191760B2 JP 2006303711 A JP2006303711 A JP 2006303711A JP 2006303711 A JP2006303711 A JP 2006303711A JP 4191760 B2 JP4191760 B2 JP 4191760B2
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fuel
valve
valve body
injection
swirl
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JP2008121448A (en
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章男 新宮
雅之 青田
穣 井倉
史也 茶園
学 平井
宏一 尾島
毅 宗実
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Mitsubishi Electric Corp
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Description

この発明は、主に内燃機関の燃料供給系に使用され、燃料を燃焼室内に直接噴射する筒内噴射用の燃料噴射弁に関するものである。   The present invention relates to a fuel injection valve for in-cylinder injection that is mainly used in a fuel supply system of an internal combustion engine and injects fuel directly into a combustion chamber.

近年、筒内直接噴射の内燃機関では、あらゆる走行状況において理想空燃比に近づける燃料噴射制御を目指しており、そのために噴射可能範囲の広い燃料噴射弁が要求されている。
電磁式の燃料噴射弁は、ソレノイド装置への通電時間により燃料の噴射量を調整している。しかし、高回転域では十分な通電時間を確保できないことや弁体の摺動応答性には限界があることから、近年では、燃圧(燃料圧力)を変化させる可変燃圧制御を併用し噴射可能範囲を拡大する方法が一般的となっている。
2. Description of the Related Art In-cylinder direct injection internal combustion engines have recently been aimed at fuel injection control that approaches an ideal air-fuel ratio in all driving situations, and for this purpose, fuel injection valves with a wide injection range are required.
The electromagnetic fuel injection valve adjusts the fuel injection amount according to the energization time of the solenoid device. However, due to the fact that sufficient energization time cannot be secured in the high speed range and the sliding response of the valve body is limited, in recent years, variable fuel pressure control that changes the fuel pressure (fuel pressure) is used in combination, and the injection range The method of enlarging is becoming common.

従来の筒内噴射用の燃料噴射弁として、例えば図5に示すようなものがある。図は燃料噴射弁の弁装置の先端部分を示すもので、(a)は側面断面図、(b)は(a)を矢印b−bから見た断面図である。図のように、燃料噴射弁30は、燃料噴射弁本体31と、その先端部に設けられて中心に燃料噴射孔32aを有する弁座32と、ソレノイド装置(図示せず)の駆動によって弁座32に離接して燃料噴射孔32aを開閉するニードル弁33と、ニードル弁33を案内すると共に径方向内向きに燃料噴射孔32aに流れ込もうとする燃料に旋回運動を与える旋回溝34aを有する旋回体34とを備えている。   An example of a conventional fuel injection valve for in-cylinder injection is shown in FIG. The figure shows the tip part of the valve device of the fuel injection valve, where (a) is a side cross-sectional view and (b) is a cross-sectional view of (a) as viewed from the arrow bb. As shown in the figure, the fuel injection valve 30 includes a fuel injection valve main body 31, a valve seat 32 provided at the tip thereof and having a fuel injection hole 32 a at the center, and a solenoid seat (not shown) driven by a solenoid device (not shown). A needle valve 33 that opens and closes the fuel injection hole 32a in contact with the nozzle 32; and a swirl groove 34a that guides the needle valve 33 and imparts a swirl motion to the fuel that is about to flow radially inward into the fuel injection hole 32a. And a revolving body 34.

高圧ポンプ(図示せず)からの燃料は、燃料噴射弁本体31の中心部を通り先端部まで導かれ、矢印で示すように、旋回体34の側面に形成された燃料導入路34bから旋回溝34aへ流入し、燃料噴射孔32aから内燃機関の燃焼室(図示せず)に噴射されるようになっている。
燃料は、旋回溝34aにより旋回を与えられているので、燃料噴射孔32a内では空洞が生じ、噴霧は中空のホロコーン状に噴射される。
旋回の強さは旋回溝34aの通路断面積とオフセット量(図5(b)参照)で決定されるため、旋回溝34aの通路断面積が小さくなるほど、またオフセット量が大きくなるほど旋回の強さは増加し、燃料噴射孔32a内の空洞率は増加して噴射量は減少する(特許文献1参照)。
Fuel from a high-pressure pump (not shown) passes through the center of the fuel injection valve body 31 and is guided to the tip, and as shown by the arrow, from the fuel introduction path 34b formed on the side surface of the swivel body 34, the swirl groove 34a and is injected from the fuel injection hole 32a into a combustion chamber (not shown) of the internal combustion engine.
Since the fuel is swirled by the swirling groove 34a, a cavity is generated in the fuel injection hole 32a, and the spray is injected in a hollow holographic cone shape.
Since the turning strength is determined by the passage sectional area of the turning groove 34a and the offset amount (see FIG. 5B), the turning strength becomes smaller as the passage sectional area of the turning groove 34a becomes smaller and the offset amount becomes larger. Increases, the cavity ratio in the fuel injection hole 32a increases, and the injection amount decreases (see Patent Document 1).

特開平10−47208号公報(第4−5頁、図4)Japanese Patent Laid-Open No. 10-47208 (page 4-5, FIG. 4)

燃料噴射弁の燃料の噴射量や噴射角は、内燃機関の要求仕様や、運転状況(負荷状況)に応じて、できるだけ広範囲に対応できることが望ましい。
可変燃圧制御では、アイドル等の少量の噴射量が必要な場合は低燃圧を、高負荷時等の多量の噴射量が必要な場合は高燃圧を使用しているが、特許文献1に示す従来の燃料噴射弁では、旋回溝の断面積は一定であり、旋回の強さを制御する機構が無いことから噴射孔内の空洞率や噴射量の制御範囲が限られていた。
It is desirable that the fuel injection amount and the injection angle of the fuel injection valve can be as wide as possible in accordance with the required specifications of the internal combustion engine and the operation status (load status).
In the variable fuel pressure control, a low fuel pressure is used when a small amount of injection such as idle is required, and a high fuel pressure is used when a large amount of injection is required such as at high load. In this fuel injection valve, the cross-sectional area of the swirling groove is constant, and since there is no mechanism for controlling the strength of swirling, the control range of the cavity ratio in the injection hole and the injection amount is limited.

この発明は、上記のような問題点を解消するためになされたもので、可変燃圧制御を行う場合に、燃料の噴射可能範囲を拡大できる燃料噴射弁を得ることを目的とする。   The present invention has been made to solve the above-described problems, and an object of the present invention is to obtain a fuel injection valve capable of expanding the fuel injectable range when performing variable fuel pressure control.

この発明に係わる燃料噴射弁は、中空状の弁ボディと、この弁ボディの一端に設けられ中心に噴射孔を有する弁座と、弁ボディ内を移動し弁座に離接して噴射孔を開閉する弁体と、弁ボディ内に配置されて弁体を摺動可能に支持し噴射孔に向けて流入する燃料に旋回運動を与える複数の燃料旋回通路を有するスワラとを備え、内燃機関の筒内へ燃料を直接噴射する燃料噴射弁において、燃料旋回通路は溝状であり、燃料旋回通路の下流側が狭まるように、弾性を有する薄板部材を溝の側面に垂直方向に向けて燃料旋回通路内に配置すると共に、スワラの外周と嵌合するように一体に形成した保持部でスワラに保持し、燃料噴射弁に供給する燃料の圧力が上昇すると燃料旋回通路の断面積が大きくなり、圧力が下降すると断面積が小さくなるように構成したものである。 A fuel injection valve according to the present invention includes a hollow valve body, a valve seat provided at one end of the valve body and having an injection hole at the center thereof, and moves within the valve body so as to be in contact with and separated from the valve seat, thereby opening and closing the injection hole. And a swirler that is disposed in the valve body and slidably supports the valve body and has a plurality of fuel swirl passages that swirl the fuel flowing toward the injection holes. In a fuel injection valve that directly injects fuel into the fuel swirl passage , the fuel swirl passage has a groove shape, and an elastic thin plate member is directed vertically to the side surface of the groove so that the downstream side of the fuel swirl passage is narrowed. In addition, when the pressure of the fuel supplied to the fuel injection valve rises , the cross-sectional area of the fuel swirl passage increases and the pressure is increased. The cross-sectional area becomes smaller when descending It is those that you have configured.

この発明の燃料噴射弁によれば、燃料旋回通路は溝状であり、燃料旋回通路の下流側が狭まるように、弾性を有する薄板部材を溝の側面に垂直方向に向けて燃料旋回通路内に配置すると共に、スワラの外周と嵌合するように一体に形成した保持部でスワラに保持し、燃料噴射弁に供給する燃料の圧力が上昇すると燃料旋回通路の断面積が大きくなり、圧力が下降すると断面積が小さくなるように構成したので、高燃圧時にはスワラの燃料旋回通路の通路断面積が大きくなって旋回の強さが低下するため、噴射孔内の空洞率が低下してより多量の噴射が可能となる。逆に、低圧時には燃料旋回通路の通路断面積が小さくなって旋回の強さが増加するため、噴射孔内の空洞率が増加してより少量の噴射が可能となる。従って、燃料の噴射可能範囲を拡大した燃料噴射弁を簡単な構成で容易に得ることができる。 According to the fuel injection valve of the present invention, the fuel swirl passage has a groove shape, and the elastic thin plate member is disposed in the fuel swirl passage so that the downstream side of the fuel swirl passage narrows in the direction perpendicular to the side surface of the groove. At the same time, when the pressure of the fuel supplied to the fuel injection valve increases, the cross-sectional area of the fuel swirl passage increases and the pressure decreases. Since the cross-sectional area is configured to be small , the swirler fuel swirl passage has a large cross-sectional area at high fuel pressure, and the swirl strength is reduced. Injection is possible. On the contrary, when the pressure is low, the passage cross-sectional area of the fuel swirl passage is reduced and the swirl strength is increased, so that the cavity ratio in the injection hole is increased and a smaller amount of injection is possible. Therefore, it is possible to easily obtain a fuel injection valve having an expanded fuel injection range with a simple configuration .

実施の形態1.
図1はこの発明の実施の形態1による燃料噴射弁を示す縦断面図である。図2は、図1の燃料噴射弁の弁装置先端部に使用するスワラ部分の斜視図であり、(a)は分解図、(b)は組立図である。また、図3は、図1のIII−III断面から見た弁装置先端部の部分断面図である。
Embodiment 1 FIG.
1 is a longitudinal sectional view showing a fuel injection valve according to Embodiment 1 of the present invention. 2A and 2B are perspective views of a swirler portion used at the tip of the valve device of the fuel injection valve of FIG. 1, wherein FIG. 2A is an exploded view and FIG. 2B is an assembly view. FIG. 3 is a partial cross-sectional view of the distal end portion of the valve device viewed from the III-III cross section of FIG.

先ず、図1によって燃料噴射弁全体について説明する。
図において、燃料噴射弁1はソレノイド装置2を備えており、ソレノイド装置2は磁気回路のヨーク部分であるハウジング3と、磁気回路の固定鉄心部分であり中心部が燃料通路となっているコア4と、コア4の外側にあってボビンに巻回されたコイル5と、磁気回路の可動鉄心部分であるアマチュア6と、アマチュア6に接合された後述のニードル弁12を付勢するばね7と、ハウジング3と一体になって弁装置9を固定するホルダ8とを備えている。このソレノイド装置2は、弁装置9を開閉動作させる作動装置である。
First, the whole fuel injection valve will be described with reference to FIG.
In the figure, the fuel injection valve 1 is provided with a solenoid device 2, which is a housing 3 that is a yoke portion of a magnetic circuit, and a core 4 that is a fixed core portion of the magnetic circuit and that has a fuel passage at the center. A coil 5 on the outside of the core 4 and wound around a bobbin, an armature 6 that is a movable core portion of a magnetic circuit, and a spring 7 that energizes a needle valve 12 to be described later joined to the armature 6; A holder 8 that is integrated with the housing 3 and fixes the valve device 9 is provided. The solenoid device 2 is an operating device that opens and closes the valve device 9.

弁装置9は、ハウジング3の先端側に収納されホルダ8で固定されている中空状の弁ボディ10と、弁ボディ10の一端に設けられ中心に噴射孔11aを有する弁座11と、弁ボディ10内を軸方向に移動し弁座11に離接して噴射孔11aを開閉する弁体であるニードル弁12と、弁ボディ10内に配置されてニードル弁12を摺動可能に支持し噴射孔11aに向けて流入する燃料に旋回運動を与えるスワラ13と、ニードル弁12の移動を制限するストッパ14とを備えている。スワラ13の詳細については後述する。   The valve device 9 includes a hollow valve body 10 that is housed on the front end side of the housing 3 and is fixed by a holder 8, a valve seat 11 that is provided at one end of the valve body 10 and that has an injection hole 11a at the center, and a valve body. The needle valve 12 is a valve body that moves in the axial direction in the direction 10 and moves to and away from the valve seat 11 to open and close the injection hole 11a, and the needle valve 12 that is disposed in the valve body 10 and slidably supports the injection hole. A swirler 13 that gives a swirling motion to the fuel that flows toward 11a and a stopper 14 that restricts the movement of the needle valve 12 are provided. Details of the swirler 13 will be described later.

このように構成された燃料噴射弁1の動作は次のようになる。
ソレノイド装置2の端子に外部より動作信号が送られてコイル5に電流が通電されると、コア4,アマチュア6及びハウジング3で構成される磁気回路に磁束が発生し、アマチュア6はコア4側へ吸引され、アマチュア6と一体構造であるニードル弁12が弁座11から離れて噴射孔11aが開孔する。これにより、図示しない燃料供給管から供給される高圧の燃料は、コア4の中空部4aを通り、アマチュア6内周部及びニードル弁12外周部に形成した燃料通路からスワラ13の燃料通路(詳細は後述する)を経由する過程で旋回運動を与えられて、弁座11の噴射孔11aから図示しない内燃機関のシリンダー内に噴射される。コイル5への給電が遮断されると、ばね7の付勢力によってニードル弁12が弁座11側に移動し噴射孔11aを閉孔する。
The operation of the fuel injection valve 1 configured as described above is as follows.
When an operation signal is sent from the outside to the terminal of the solenoid device 2 and a current is passed through the coil 5, a magnetic flux is generated in the magnetic circuit composed of the core 4, the armature 6 and the housing 3. The needle valve 12 that is integral with the armature 6 is separated from the valve seat 11 and the injection hole 11a is opened. As a result, high-pressure fuel supplied from a fuel supply pipe (not shown) passes through the hollow portion 4a of the core 4 and from the fuel passage formed in the inner periphery of the armature 6 and the outer periphery of the needle valve 12 to the fuel passage (details) of the swirler 13 Is given a turning motion in the course of passing through (described later), and is injected into the cylinder of the internal combustion engine (not shown) from the injection hole 11a of the valve seat 11. When the power supply to the coil 5 is cut off, the urging force of the spring 7 moves the needle valve 12 toward the valve seat 11 to close the injection hole 11a.

次に、本実施の形態の発明の特徴部分である、スワラ13部分の詳細を図2に基づいて説明する。
図2(a)に示すように、スワラ13は、その軸心にニードル弁12が摺動可能な中心孔13aを有する中空筒状をしており、弁装置9内に組み込まれた時、弁座11に接する第1端面13bと、弁座11と反対側の第2端面13cと、外周を構成する周面13dとを備えている。この周面13dは、弁ボディ10の内周面に当接して弁ボディ10に対する位置を規定する複数の外周面部分と、それら外周面部分の間に設けられた平坦面とからなり、平坦面と弁ボディ10の内周面との間に形成される隙間が燃料の軸方向流路16(図3参照)となる。
第2端面13cには径方向に延びた通路溝13eが形成されており、内周部から外周部に燃料が流れるようになっている。
Next, details of the swirler 13 portion, which is a characteristic portion of the present invention, will be described with reference to FIG.
As shown in FIG. 2 (a), the swirler 13 has a hollow cylindrical shape having a central hole 13a in which the needle valve 12 is slidable at the axial center thereof. A first end surface 13b in contact with the seat 11, a second end surface 13c opposite to the valve seat 11, and a peripheral surface 13d constituting the outer periphery are provided. The peripheral surface 13d is composed of a plurality of outer peripheral surface portions that abut the inner peripheral surface of the valve body 10 to define the position with respect to the valve body 10, and a flat surface provided between the outer peripheral surface portions. A gap formed between the valve body 10 and the inner peripheral surface of the valve body 10 serves as a fuel axial flow path 16 (see FIG. 3).
A passage groove 13e extending in the radial direction is formed in the second end surface 13c, and fuel flows from the inner peripheral portion to the outer peripheral portion.

第1端面13bには、中心孔13aに隣接する内周辺に、所定幅の内周環状溝13fが形成されている。そして、一端が周面13dの平坦面に接続されて、そこからほぼ径方向内側に延びて、他端が内周環状溝13fの接線方向に接続された燃料旋回通路13gを有している。燃料旋回通路13gの断面は、図に示すように、スワラ13の軸方向に垂直な底面と軸方向に平行な側面とでコの字状に形成されている。   An inner peripheral annular groove 13f having a predetermined width is formed on the inner periphery adjacent to the center hole 13a on the first end face 13b. And it has the fuel turning channel | path 13g which one end was connected to the flat surface of the surrounding surface 13d, extended from there almost in the radial direction, and the other end was connected to the tangential direction of the inner periphery annular groove 13f. As shown in the drawing, the cross section of the fuel swirl passage 13g is formed in a U shape with a bottom surface perpendicular to the axial direction of the swirler 13 and a side surface parallel to the axial direction.

上記の燃料旋回通路13gの仮想壁を構成する薄板部材15が、スワラ13の周面13dと燃料旋回通路13gの側面に合わせて折り曲げて形成されている。薄板部材15は、ばね性を有する材料から成っている。
中心側に向かう直線部が仮想壁15aとなる部分である。この薄板部材15をスワラ13の第1端面13b側に組み合わせると図2(b)のようになる。
組み合わせ後に仮想壁15aとなる部分は、燃料旋回通路13gの底面とは垂直であり、かつ、燃料旋回通路13gの燃料の流れ方向、すなわち下流側(中心孔13a側)に向かって通路の断面積が小さくなるように配置されている。
図2(b)のように組み合わせた状態で、第1端面13bが弁座11側になるように弁ボディ10の先端部に組み込んで固定される。
The thin plate member 15 constituting the virtual wall of the fuel swirl passage 13g is formed by being bent along the peripheral surface 13d of the swirler 13 and the side surface of the fuel swirl passage 13g. The thin plate member 15 is made of a material having a spring property.
The straight part toward the center is a part that becomes the virtual wall 15a. When this thin plate member 15 is combined with the first end face 13b side of the swirler 13, the result is as shown in FIG.
The portion that becomes the virtual wall 15a after the combination is perpendicular to the bottom surface of the fuel swirl passage 13g, and the cross-sectional area of the passage toward the fuel flow direction of the fuel swirl passage 13g, that is, toward the downstream side (center hole 13a side). Is arranged to be small.
In the combined state as shown in FIG. 2B, the first end face 13b is assembled and fixed to the distal end portion of the valve body 10 so as to be on the valve seat 11 side.

このように構成されたスワラ13の燃料旋回通路13gの作用を、弁装置9先端部の部分断面図である図3によって説明する。
圧力を加えられて燃料噴射弁1に流入した燃料が、スワラ13の周面に形成した軸方向流路16から燃料旋回通路13gに導入されて燃料に旋回運動が与えられ、内周環状溝13fへ流れ込み旋回流となって弁座11の噴射孔11aから外部へ噴霧される。
The operation of the fuel swirl passage 13g of the swirler 13 configured as described above will be described with reference to FIG.
The fuel that has flowed into the fuel injection valve 1 under pressure is introduced into the fuel swirl passage 13g from the axial flow passage 16 formed on the peripheral surface of the swirler 13, and the swirl motion is given to the fuel. Into the swirl flow and sprayed from the injection hole 11a of the valve seat 11 to the outside.

この時、燃圧が上昇すると、図3(b)に示すように、仮想壁15aの弾性変形によるたわみ量が大きくなるため、高圧時では燃料旋回通路13gの通路断面積は大きくなる。これにより旋回の強さが低下するため噴射孔内11aの空洞率(燃料が噴射孔を通過するとき、中心部にできる空洞断面積が噴射孔断面積に占める割合)が低下し、より多量の燃料の噴射が可能となる。また、低圧時には燃料旋回通路13gの通路断面積は(a)に示すように小さくなり、旋回の強さが増加する。このため噴射孔11a内の空洞率が増加するので、より少量の噴射が可能となる。   At this time, when the fuel pressure rises, as shown in FIG. 3B, the amount of deflection due to elastic deformation of the virtual wall 15a increases, so that the passage cross-sectional area of the fuel swirl passage 13g increases at high pressure. As a result, the strength of the swirl is reduced, so that the cavity ratio in the injection hole 11a (the ratio of the cavity cross-sectional area formed at the center when the fuel passes through the injection hole occupies the cross-sectional area of the injection hole) is reduced. Fuel injection becomes possible. Further, when the pressure is low, the passage cross-sectional area of the fuel swirl passage 13g becomes small as shown in (a), and the swirl strength increases. For this reason, since the cavity ratio in the injection hole 11a increases, a smaller amount of injection becomes possible.

図2及び図3では、燃料旋回通路13gの仮想壁15aを構成する薄板部材15を、燃料旋回通路13gの底面に垂直方向となるように設けた場合について説明したが、次に別の例について説明する。
図4は、弁装置9の先端部に使用するスワラ13部分の他の例を示す斜視図であり、(a)は分解図、(b)は組立図である。
2 and 3, the case where the thin plate member 15 constituting the virtual wall 15a of the fuel swirl passage 13g is provided so as to be perpendicular to the bottom surface of the fuel swirl passage 13g has been described. Next, another example will be described. explain.
FIG. 4 is a perspective view showing another example of the swirler 13 portion used at the tip of the valve device 9, wherein (a) is an exploded view and (b) is an assembly view.

図2と同等部分は同一符号を付して説明は省略する。スワラ13は図2と同等のものである。図4(a)に示すように、薄板部材17は、燃料旋回通路13gの側面に対し垂直方向に向けて、かつ通路底面に合わせて形成されて仮想壁17aとなる部分と、それをスワラ13に保持する保持部17bとから成り、ばね性を有する、例えば薄板鋼板で構成されている。スワラ13に組み合わせた状態で、仮想壁17aは、下流側に向かって燃料旋回通路13gの断面積が小さくなるように、中心側を折り曲げている。
この薄板部材17を、図4(b)に示すようにスワラ13に組み合わせ、第1端面13b側が弁座11側になるように弁ボディ10に組み付けて使用する。
The same parts as those in FIG. The swirler 13 is equivalent to FIG. As shown in FIG. 4 (a), the thin plate member 17 is formed in a direction perpendicular to the side surface of the fuel swirl passage 13g and in conformity with the bottom surface of the passage to become a virtual wall 17a. For example, a thin steel plate having a spring property. When combined with the swirler 13, the virtual wall 17a is bent at the center so that the cross-sectional area of the fuel swirl passage 13g decreases toward the downstream side.
The thin plate member 17 is used by being combined with the swirler 13 as shown in FIG. 4B, and is assembled with the valve body 10 so that the first end face 13b side is the valve seat 11 side.

このように構成されたスワラ13の燃料旋回通路13gの作用について説明する。
燃料旋回通路13gに燃料が流れるとき、燃圧が高い場合は、仮想壁17aの弾性変形によるたわみ量が大きくなるため、燃料旋回通路13gの断面積は大きくなり、これにより旋回の強さが低下するため、噴射孔11a内の空洞率が低下し、より多量の燃料の噴射が可能となる。また低圧時には燃料旋回通路13gの断面積は小さくなり旋回の強さが増加するため、噴射孔13a内の空洞率が増加し、より少量の燃料の噴射が可能となる。
The operation of the fuel swirl passage 13g of the swirler 13 configured as described above will be described.
When the fuel flows through the fuel swirl passage 13g, if the fuel pressure is high, the amount of deflection due to the elastic deformation of the virtual wall 17a increases, so the cross-sectional area of the fuel swirl passage 13g increases, thereby reducing the strength of the swirl. Therefore, the cavity ratio in the injection hole 11a is reduced, and a larger amount of fuel can be injected. Further, since the cross-sectional area of the fuel swirl passage 13g becomes smaller and the swirl strength increases at low pressure, the cavity ratio in the injection hole 13a increases, and a smaller amount of fuel can be injected.

なお、スワラ13に形成する燃料旋回通路13gの個数は、6個に限定するものではなく、例えば4個や8個であっても良い。また、燃料旋回通路13gのオフセット量(図5(b)参照)も、図に限定するものではなく適宜設定すればよい。
更に、燃料旋回通路13gの断面積を変化させる機構として、薄板部材からなる仮想壁を設けて構成したが、これに限定するものではなく、燃料の圧力変化に応じて断面積を変化させるものであれば、他の構造でも良い。
The number of fuel swirl passages 13g formed in the swirler 13 is not limited to six, and may be four or eight, for example. Further, the offset amount of the fuel turning passage 13g (see FIG. 5B) is not limited to the figure, and may be set as appropriate.
Furthermore, the virtual wall made of a thin plate member is provided as a mechanism for changing the cross-sectional area of the fuel swirl passage 13g. However, the present invention is not limited to this, and the cross-sectional area is changed in accordance with a change in fuel pressure. Other structures may be used as long as they exist.

以上のように、本実施の形態の発明によれば、燃料旋回通路は溝状であり、燃料旋回通路の下流側が狭まるように、弾性を有する薄板部材を溝の側面に垂直方向に向けて燃料旋回通路内に配置すると共に、スワラの外周と嵌合するように一体に形成した保持部でスワラに保持し、燃料噴射弁に供給する燃料の圧力が上昇すると燃料旋回通路の断面積が大きくなり、圧力が下降すると断面積が小さくなるように構成したので、高燃圧時にスワラの燃料旋回通路の通路断面積が大きくなり旋回の強さが低下するため噴射孔内の空洞率は低下することからより多量の噴射が可能となる。逆に、低圧時には燃料旋回通路の通路断面積が小さくなり旋回の強さが増加するため、噴射孔内の空洞率は増加してより少量の噴射が可能となる。従って、燃料の噴射可能範囲を拡大した燃料噴射弁を簡単な構成で容易に実現することができる。 As described above, according to the invention of the present embodiment, the fuel swirl passage has a groove shape, and the thin plate member having elasticity is directed vertically to the side surface of the groove so that the downstream side of the fuel swirl passage is narrowed. When the pressure of the fuel supplied to the fuel injection valve rises, the cross-sectional area of the fuel swirl passage increases as it is placed in the swirl passage and held in the swirler by a holding part that is integrally formed to fit the outer periphery of the swirler. Since the cross-sectional area is reduced when the pressure decreases, the cross-sectional area of the swirler fuel swirl passage increases at high fuel pressure and the swirl strength decreases, so the cavity ratio in the injection hole decreases. From this, a larger amount of injection becomes possible. Conversely, when the pressure is low, the cross-sectional area of the fuel swirl passage is reduced and the swirl strength is increased, so that the cavity ratio in the injection hole is increased and a smaller amount of injection is possible. Therefore, it is possible to easily realize a fuel injection valve having an expanded fuel injection range with a simple configuration .

この発明の実施の形態1における燃料噴射弁の縦断面図である。It is a longitudinal cross-sectional view of the fuel injection valve in Embodiment 1 of this invention. 図1の燃料噴射弁の弁装置先端部に使用するスワラ部分を示す斜視図であり、(a)は分解図、(b)は組立図である。It is a perspective view which shows the swirler part used for the valve apparatus front-end | tip part of the fuel injection valve of FIG. 1, (a) is an exploded view, (b) is an assembly drawing. 図1のIII−III断面から見た弁装置先端部の部分断面図である。It is the fragmentary sectional view of the valve device tip part seen from the III-III section of Drawing 1. 図1の燃料噴射弁の弁装置先端部に使用するスワラ部分の他の例を示す斜視図であり、(a)は分解図、(b)は組立図である。It is a perspective view which shows the other example of the swirler part used for the valve apparatus front-end | tip part of the fuel injection valve of FIG. 1, (a) is an exploded view, (b) is an assembly drawing. 従来の燃料噴射弁の弁装置先端部の部分断面図である。It is a fragmentary sectional view of the valve device tip of a conventional fuel injection valve.

符号の説明Explanation of symbols

1 燃料噴射弁 2 ソレノイド装置
3 ハウジング 4 コア
4a 中空部 5 コイル
6 アマチュア 7 ばね
8 ホルダ 9 弁装置
10 弁ボディ 11 弁座
11a 噴射孔 12 ニードル弁(弁体)
13 スワラ 13a 中心孔
13b 第1端面 13c 第2端面
13d 周面 13e 通路溝
13f 内周環状溝 13g 燃料旋回通路
14 ストッパ 15 薄板部材
15a 仮想壁 16 軸方向流路
17 薄板部材 17a 仮想壁
17b 保持部。
DESCRIPTION OF SYMBOLS 1 Fuel injection valve 2 Solenoid apparatus 3 Housing 4 Core 4a Hollow part 5 Coil 6 Amateur 7 Spring 8 Holder 9 Valve apparatus 10 Valve body 11 Valve seat 11a Injection hole 12 Needle valve (valve body)
13 swirler 13a center hole 13b first end surface 13c second end surface 13d peripheral surface 13e passage groove 13f inner peripheral annular groove 13g fuel swirl passage 14 stopper 15 thin plate member 15a virtual wall 16 axial flow path 17 thin plate member 17a virtual wall 17b holding portion .

Claims (1)

中空状の弁ボディと、この弁ボディの一端に設けられ中心に噴射孔を有する弁座と、前記弁ボディ内を移動し前記弁座に離接して前記噴射孔を開閉する弁体と、前記弁ボディ内に配置されて前記弁体を摺動可能に支持し前記噴射孔に向けて流入する燃料に旋回運動を与える複数の燃料旋回通路を有するスワラとを備え、内燃機関の筒内へ燃料を直接噴射する燃料噴射弁において、
前記燃料旋回通路は溝状であり、前記燃料旋回通路の下流側が狭まるように、弾性を有する薄板部材を前記溝の側面に垂直方向に向けて前記燃料旋回通路内に配置すると共に、前記スワラの外周と嵌合するように一体に形成した保持部で前記スワラに保持し、前記燃料噴射弁に供給する燃料の圧力が上昇すると前記燃料旋回通路の断面積が大きくなり、前記圧力が下降すると前記断面積が小さくなるように構成したことを特徴とする燃料噴射弁。
A hollow valve body, a valve seat provided at one end of the valve body and having an injection hole at the center thereof, a valve body that moves within the valve body, contacts and closes the valve seat, and opens and closes the injection hole; And a swirler having a plurality of fuel swirling passages disposed in the valve body to slidably support the valve body and to swirl the fuel flowing toward the injection hole, and into the cylinder of the internal combustion engine In a fuel injection valve that directly injects
The fuel swirl passage has a groove shape, and an elastic thin plate member is disposed in the fuel swirl passage in a direction perpendicular to the side surface of the groove so that the downstream side of the fuel swirl passage is narrowed. When the pressure of the fuel supplied to the fuel injection valve rises , the cross-sectional area of the fuel swirl passage increases, and when the pressure drops, the holding part integrally formed to fit with the outer periphery holds the swirler. A fuel injection valve configured to have a small cross-sectional area.
JP2006303711A 2006-11-09 2006-11-09 Fuel injection valve Expired - Fee Related JP4191760B2 (en)

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