JP2000213439A - Fuel injection system of internal combustion engine - Google Patents

Fuel injection system of internal combustion engine

Info

Publication number
JP2000213439A
JP2000213439A JP11013703A JP1370399A JP2000213439A JP 2000213439 A JP2000213439 A JP 2000213439A JP 11013703 A JP11013703 A JP 11013703A JP 1370399 A JP1370399 A JP 1370399A JP 2000213439 A JP2000213439 A JP 2000213439A
Authority
JP
Japan
Prior art keywords
fuel
fuel injection
air passage
combustion engine
internal combustion
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.)
Pending
Application number
JP11013703A
Other languages
Japanese (ja)
Inventor
Akihiro Sakakida
明宏 榊田
Takayuki Arai
孝之 荒井
Akihiro Iiyama
明裕 飯山
Masaaki Kubo
賢明 久保
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.)
Nissan Motor Co Ltd
Original Assignee
Nissan Motor Co Ltd
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 Nissan Motor Co Ltd filed Critical Nissan Motor Co Ltd
Priority to JP11013703A priority Critical patent/JP2000213439A/en
Publication of JP2000213439A publication Critical patent/JP2000213439A/en
Pending legal-status Critical Current

Links

Landscapes

  • Fuel-Injection Apparatus (AREA)

Abstract

PROBLEM TO BE SOLVED: To realize a fuel injection system of internal combustion engine which is excellent in atomization characteristic at low fuel pressure and excellent in fuel flow linearity. SOLUTION: In this fuel injection system of internal combustion engine in which a nozzle hole 2 of a swirl nozzle 1 directly opens into a cylinder and fuel is directly injected into the cylinder, a fuel guide 3 diametrally enlarging along a injecting direction is provided at a downstream side of the nozzle hole 2 of the swirl nozzle 1. An assist air outlet 5 of an assist air passage 6 opens to inner surface of the fuel guide 3, a squish part is provided on a surface opposite to a piston of a cylinder head, and an air introducing port of the assist air passage 6 opens to the squish part.

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】この発明は、内燃機関の燃料
噴射装置における燃料噴射弁の改良に関し、噴孔から噴
射される燃料に空気を混ぜることで、噴霧の微粒化を向
上させ、これによりHC低減、燃費低減等の燃焼改善を
行うことのできる内燃機関の燃料噴射装置を提供するも
のである。
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to an improvement in a fuel injection valve in a fuel injection device for an internal combustion engine, and more specifically, to improve atomization of spray by mixing air into fuel injected from an injection hole, thereby improving HC. An object of the present invention is to provide a fuel injection device for an internal combustion engine capable of improving combustion such as reduction and fuel consumption.

【0002】[0002]

【従来の技術】従来の技術において、空気の利用で微粒
化を図るものとしては、特開平9−195894号公報
がある。これは、ホール型燃料噴射ノズルであって、燃
料噴射口に対してエアの導入口を設け、燃料のエジェク
タ効果により空気を導入するものである。特に、燃料通
路に対して、エア通路を鋭角に交差させること、燃料出
口付近にエア通路との交差点を持つこと、エアの導入口
はインジェクタの先端部であること、等を特徴とするも
のである。
2. Description of the Related Art Japanese Unexamined Patent Publication No. Hei 9-195894 discloses an example of the prior art in which atomization is achieved by using air. This is a hall-type fuel injection nozzle, in which an air introduction port is provided for a fuel injection port, and air is introduced by an ejector effect of fuel. In particular, the air passage intersects the fuel passage at an acute angle, has an intersection with the air passage near the fuel outlet, and the air inlet is at the tip of the injector. is there.

【0003】[0003]

【発明が解決しようとする課題】しかしながら、このよ
うな従来の空気利用微粒化噴射弁にあっては、噴孔内に
空気を導入するものであり、燃料計量部にエア通路を設
置するため、燃料計量が不安定になることが問題とな
る。特に、燃料噴射量が大きくエア導入量が大きい場合
と、燃料噴射量が小さくエア導入量が小さいか、また
は、ほとんど導入されない場合とで、燃料噴射率(mm
3 /ms)に差が出て、噴射量を時間制限できないとい
う欠点がある。また、微細な噴孔より小さい径を持つエ
ア導入口を設置する必要があり、加工困難である。ま
た、ホールノズルは、低燃圧での微粒化特性が悪く、ま
た噴孔でのエジェクタ効果も小さいため、高燃圧が必要
となり高燃圧ポンプの駆動ロスにより燃費が悪化すると
いう懸念がある。この発明は、このような従来の問題点
に着目してなされたもので、単噴孔のスワールノズルを
用いて、スキッシュ流を利用したエア流動と燃料の流れ
によるエジェクタ効果により、低燃圧で微粒化特性に優
れ、かつ燃料流量直線性に優れた内燃機関の燃料噴射装
置を提供し、上記問題点を解決することを目的としてい
る。
However, in such a conventional air-based atomizing injection valve, air is introduced into the injection hole, and an air passage is provided in the fuel metering section. The problem is that the fuel metering becomes unstable. In particular, when the fuel injection amount is large and the air introduction amount is large, and when the fuel injection amount is small and the air introduction amount is small or almost not introduced, the fuel injection rate (mm
3 / ms), and the injection amount cannot be limited in time. In addition, it is necessary to provide an air inlet having a diameter smaller than the fine injection hole, which is difficult to process. Further, since the hole nozzle has poor atomization characteristics at a low fuel pressure and a small ejector effect at an injection hole, a high fuel pressure is required, and there is a concern that fuel consumption may be deteriorated due to a drive loss of the high fuel pressure pump. The present invention has been made in view of such conventional problems, and uses a swirl nozzle having a single injection hole to generate fine particles at a low fuel pressure by an air flow utilizing a squish flow and an ejector effect by a fuel flow. It is an object of the present invention to provide a fuel injection device for an internal combustion engine having excellent fuel injection characteristics and excellent fuel flow linearity, and to solve the above problems.

【0004】[0004]

【課題を解決するための手段】上記目的を達成するため
請求項1記載の発明では、燃料噴射弁の噴孔をシリンダ
内に直接臨ませて、シリンダ内に直接燃料を噴射する内
燃機関の燃料噴射装置において、前記燃料噴射弁の噴孔
下流側に、噴射方向に沿って拡径する燃料ガイドを設
け、この燃料ガイドの内面にアシストエア通路の一端を
開口させるとともに、シリンダヘッドのピストンに対向
する面にスキッシュ部を設け、このスキッシュ部に前記
アシストエア通路の他端部を開口させたことを特徴とす
る。請求項2記載の発明では、請求項1記載の内燃機関
の燃料噴射装置において、前記燃料ガイドの内面に環状
凹部を設け、前記アシストエア通路の一端をこの環状凹
部に連通させたことを特徴とする。請求項3記載の発明
では、請求項1または2記載の内燃機関の燃料噴射装置
において、前記燃料噴射弁は、燃料に旋回成分を付与す
る旋回素子を備えるものであって、前記燃料ガイドに発
生するアシストエアの旋回方向を、旋回素子による燃料
の旋回方向と同一にしたことを特徴とする。請求項4記
載の発明では、請求項1ないし3記載の内燃機関の燃料
噴射装置において、前記燃料噴射弁のノズル部に噴孔中
心と同軸の環状エア通路を設け、前記アシストエア通路
の途中を、この環状エア通路に連通させたことを特徴と
する。請求項5記載の発明では、請求項1ないし4記載
の内燃機関の燃料噴射装置において、前記アシストエア
通路を、スキッシュ部に開口する他端部に向かって拡径
させたことを特徴とする。請求項6記載の発明では、請
求項1ないし5記載の内燃機関の燃料噴射装置におい
て、前記燃料ガイドの内面に開口するアシストエア通路
は、燃料噴射流に伴う流れを発生するよう噴孔中心に対
し所定の角度を有して開口することを特徴とする。請求
項7記載の発明では、請求項4記載の内燃機関の燃料噴
射装置において、前記スキッシュ部から環状エア通路に
連通するアシストエア通路の開口端を環状エア通路の中
心に対し偏倚させて設定したことを特徴とする。
According to the first aspect of the present invention, there is provided a fuel supply system for an internal combustion engine in which an injection hole of a fuel injection valve is made to directly face a cylinder and fuel is injected directly into the cylinder. In the injection device, a fuel guide that expands in diameter along the injection direction is provided on the downstream side of the injection hole of the fuel injection valve, and one end of an assist air passage is opened on the inner surface of the fuel guide, and the fuel guide faces the piston of the cylinder head. A squish portion is provided on the surface to be cut, and the other end of the assist air passage is opened in the squish portion. According to a second aspect of the present invention, in the fuel injection device for an internal combustion engine according to the first aspect, an annular recess is provided on an inner surface of the fuel guide, and one end of the assist air passage communicates with the annular recess. I do. According to a third aspect of the present invention, in the fuel injection device for an internal combustion engine according to the first or second aspect, the fuel injection valve includes a swirl element for imparting a swirl component to fuel, and the fuel injection valve is provided in the fuel guide. The turning direction of the assist air is the same as the turning direction of the fuel by the turning element. According to a fourth aspect of the present invention, in the fuel injection device for an internal combustion engine according to any one of the first to third aspects, an annular air passage coaxial with the center of the injection hole is provided in a nozzle portion of the fuel injection valve, and the middle of the assist air passage is provided. , And is communicated with the annular air passage. According to a fifth aspect of the present invention, in the fuel injection device for an internal combustion engine according to any one of the first to fourth aspects, the diameter of the assist air passage is increased toward the other end opening to the squish portion. According to a sixth aspect of the present invention, in the fuel injection device for an internal combustion engine according to the first to fifth aspects, the assist air passage opening to the inner surface of the fuel guide is formed at the center of the injection hole so as to generate a flow accompanying the fuel injection flow. The opening is provided at a predetermined angle. According to a seventh aspect of the present invention, in the fuel injection device for an internal combustion engine according to the fourth aspect, the opening end of the assist air passage communicating from the squish portion to the annular air passage is set so as to be deviated from the center of the annular air passage. It is characterized by the following.

【0005】[0005]

【発明の実施の形態】以下、この発明の実施の形態を図
面に基づいて説明する。図1は実施の形態の燃料噴射弁
を示す説明図、図2は実施の形態の燃料噴射弁のA矢視
図、図3は実施の形態の内燃機関の燃料噴射装置を示す
説明図、図4は実施の形態の内燃機関の燃料噴射装置の
B矢視図である。まず、構成を説明すると、本実施の形
態の内燃機関の燃料噴射装置は、筒内直接噴射式で燃料
に旋回流を発生させるスワールノズル1と、このスワー
ルノズル1の噴孔2の下流側に、下流側に行くに従って
断面直径が大きくなる燃料ガイド3と、この燃料ガイド
3に設けられた環状凹部4と、この環状凹部4に設けら
れたアシストエア出口5と、環状凹部4に旋回流を発生
させるように構成されたアシストエア通路6と、このア
シストエア通路6にエアを供給する環状エア通路7と、
スキッシュ部10に開口したスキッシュエア導入口8
と、環状エア通路7とスキッシュエア導入口8とを結ぶ
アシストエア通路9と、スキッシュ部10とから構成さ
れる。図5はアシストエア通路9の説明図、図6は図5
のS6−S6断面図である。図に示すように、アシスト
エア通路9は、エア導入口8側の開口面積が大きく、環
状エア通路7側が小さくなるように形成されている。
Embodiments of the present invention will be described below with reference to the drawings. FIG. 1 is an explanatory view showing a fuel injection valve according to an embodiment, FIG. 2 is a view of the fuel injection valve according to the embodiment as viewed from an arrow A, and FIG. 3 is an explanatory view showing a fuel injection device of an internal combustion engine according to the embodiment. 4 is a view on arrow B of the fuel injection device for an internal combustion engine according to the embodiment. First, the configuration will be described. The fuel injection device for an internal combustion engine according to the present embodiment includes a swirl nozzle 1 that generates a swirl flow in fuel by a direct injection type in a cylinder, and a swirl nozzle 1 downstream of an injection hole 2 of the swirl nozzle 1. The fuel guide 3 has a sectional diameter increasing toward the downstream side, an annular recess 4 provided in the fuel guide 3, an assist air outlet 5 provided in the annular recess 4, and a swirl flow through the annular recess 4. An assist air passage 6 configured to generate air, an annular air passage 7 that supplies air to the assist air passage 6,
Squish air inlet 8 opened in squish section 10
, An assist air passage 9 connecting the annular air passage 7 and the squish air inlet 8, and a squish portion 10. FIG. 5 is an explanatory view of the assist air passage 9, and FIG.
It is S6-S6 sectional drawing of. As shown in the drawing, the assist air passage 9 is formed such that the opening area on the air introduction port 8 side is large and the opening area on the annular air passage 7 side is small.

【0006】次に作用を説明する。針弁がリフトし、針
弁とスワールノズル1のシート部が離れると、その隙間
を通って燃料が流れ出す。この時、シート上流の燃料旋
回素子を通過した燃料は、旋回しながら噴孔2を通過
し、噴孔2を通過した燃料は、旋回力により、燃料ガイ
ド3に沿って流れる。この燃料ガイド3にアシストエア
通路出口5を設置すると、燃料のエジェクタ効果によ
り、アシストエア通路6内の空気を吸入する。このアシ
ストエアにより、燃料と空気との混合が進み、燃料が微
粒化される。さらに、アシストエアは、環状凹部4を旋
回することで噴霧に対して全周から供給されるため、噴
霧は均一に微粒化される。環状凹部4において、不連続
に直径が燃料ガイド3より大きくなるため、燃料の剥離
効果で一層空気を導入しやすくなる。さらに、アシスト
エア通路の導入口をスキッシュ部10に設置したこと
で、上昇するタンブル流、スキッシュ流を活用できる。
燃料噴霧中の微粒化効果に加えて、上死点付近の強いス
キッシュ流が、噴霧終了後のスワールノズル1に流れ込
むため、燃料ガイド3に滞留する燃料を燃焼室中央部へ
送り出すことができ、燃焼改善と、燃料のスワールノズ
ル1への付着を防止でき、HCの低減に効果がある。
Next, the operation will be described. When the needle valve lifts and the needle valve and the seat portion of the swirl nozzle 1 are separated, fuel flows out through the gap. At this time, the fuel that has passed through the fuel swirling element upstream of the seat passes through the injection hole 2 while swirling, and the fuel that has passed through the injection hole 2 flows along the fuel guide 3 by the swirling force. When the assist air passage outlet 5 is provided in the fuel guide 3, the air in the assist air passage 6 is sucked by the ejector effect of the fuel. By this assist air, mixing of the fuel and the air proceeds, and the fuel is atomized. Furthermore, since the assist air is supplied from around the entire circumference to the spray by turning the annular recess 4, the spray is uniformly atomized. Since the diameter of the annular recess 4 is discontinuously larger than that of the fuel guide 3, it becomes easier to introduce air due to the fuel separation effect. Further, by installing the introduction port of the assist air passage in the squish section 10, the rising tumble flow and squish flow can be utilized.
In addition to the atomization effect during fuel spraying, a strong squish flow near the top dead center flows into the swirl nozzle 1 after the spraying ends, so that the fuel remaining in the fuel guide 3 can be sent out to the center of the combustion chamber, It is possible to improve combustion and prevent the fuel from adhering to the swirl nozzle 1, which is effective in reducing HC.

【0007】以上、本発明の実施の形態を説明してきた
が、本発明の具体的な構成は本実施の形態に限定される
ものではなく、発明の要旨を逸脱しない範囲の設計変更
などがあっても本発明に含まれる。例えば、図7,図8
に示すように、アシストエア通路6aをスワールノズル
1の中心を指向するよう直線状に配置し、燃料ガイド3
aに環状凹部を設けない構成としてもよい。
Although the embodiments of the present invention have been described above, the specific configuration of the present invention is not limited to the embodiments, and there may be design changes within the scope of the present invention. This is also included in the present invention. For example, FIGS.
As shown in FIG. 3, the assist air passage 6a is linearly arranged so as to point toward the center of the swirl nozzle 1, and the fuel guide 3
It is good also as composition which does not provide an annular concave part in a.

【0008】[0008]

【発明の効果】以上説明してきたように、この発明によ
れば、その構成を、アシストエアの導入口をスキッシュ
部に設け、かつアシストエアの出口を噴霧ガイドに設け
た構成としたので、筒内のタンブル流、スキッシュ流の
利用と燃料のエジェクタ効果により微粒化向上を達成
し、かつ燃料流量直線性に優れた内燃機関の燃料噴射装
置を提供でき、これによりHC低減、燃費改善等の燃焼
改善を達成できる。
As described above, according to the present invention, the structure is such that the inlet for the assist air is provided in the squish portion and the outlet for the assist air is provided in the spray guide. The use of the tumble flow and squish flow inside the fuel tank and the ejector effect of the fuel have improved the atomization and provided a fuel injection device for an internal combustion engine with excellent fuel flow rate linearity, thereby reducing combustion and improving fuel efficiency. Improvements can be achieved.

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

【図1】本発明の実施の形態の燃料噴射弁を示す説明図
である。
FIG. 1 is an explanatory diagram showing a fuel injection valve according to an embodiment of the present invention.

【図2】実施の形態の燃料噴射弁のA矢視図である。FIG. 2 is a view as viewed from an arrow A of the fuel injection valve according to the embodiment;

【図3】実施の形態の内燃機関の燃料噴射装置を示す説
明図である。
FIG. 3 is an explanatory diagram showing a fuel injection device for an internal combustion engine according to the embodiment.

【図4】実施の形態の内燃機関の燃料噴射装置のB矢視
図である。
FIG. 4 is a view on arrow B of the fuel injection device for an internal combustion engine according to the embodiment;

【図5】アシストエア通路の説明図である。FIG. 5 is an explanatory diagram of an assist air passage.

【図6】図5のS6−S6断面図である。FIG. 6 is a sectional view taken along line S6-S6 of FIG.

【図7】他の実施の形態を示す説明図である。FIG. 7 is an explanatory diagram showing another embodiment.

【図8】他の実施の形態を示す説明図である。FIG. 8 is an explanatory diagram showing another embodiment.

【符号の説明】[Explanation of symbols]

1 スワールノズル 2 噴孔 3 燃料ガイド 4 環状凹部 5 アシストエア出口 6 アシストエア通路 7 環状エア通路 8 スキッシュエア導入口 9 アシストエア通路 10 スキッシュ部 Reference Signs List 1 swirl nozzle 2 injection hole 3 fuel guide 4 annular recess 5 assist air outlet 6 assist air passage 7 annular air passage 8 squish air inlet 9 assist air passage 10 squish portion

───────────────────────────────────────────────────── フロントページの続き (72)発明者 久保 賢明 神奈川県横浜市神奈川区宝町2番地 日産 自動車株式会社内 Fターム(参考) 3G066 AA02 AA03 AB02 AD12 BA03 BA17 BA26 BA32 CC14 CC37 CC43 CC46  ────────────────────────────────────────────────── ─── Continuing on the front page (72) Inventor: Kenmei Kubo F-term in Nissan Motor Co., Ltd. 2 Takaracho, Kanagawa-ku, Yokohama-shi, Kanagawa 3G066 AA02 AA03 AB02 AD12 BA03 BA17 BA26 BA32 CC14 CC37 CC43 CC46

Claims (7)

【特許請求の範囲】[Claims] 【請求項1】 燃料噴射弁の噴孔をシリンダ内に直接臨
ませて、シリンダ内に直接燃料を噴射する内燃機関の燃
料噴射装置において、 前記燃料噴射弁の噴孔下流側に、噴射方向に沿って拡径
する燃料ガイドを設け、この燃料ガイドの内面にアシス
トエア通路の一端を開口させるとともに、 シリンダヘッドのピストンに対向する面にスキッシュ部
を設け、このスキッシュ部に前記アシストエア通路の他
端部を開口させたことを特徴とする内燃機関の燃料噴射
装置。
1. A fuel injection device for an internal combustion engine in which an injection hole of a fuel injection valve is directly made to face a cylinder and directly injects fuel into the cylinder. A fuel guide is provided along the fuel guide, and one end of the assist air passage is opened on the inner surface of the fuel guide, and a squish portion is provided on a surface of the cylinder head facing the piston. A fuel injection device for an internal combustion engine, wherein an end is opened.
【請求項2】 前記燃料ガイドの内面に環状凹部を設
け、前記アシストエア通路の一端をこの環状凹部に連通
させたことを特徴とする請求項1記載の内燃機関の燃料
噴射装置。
2. The fuel injection device for an internal combustion engine according to claim 1, wherein an annular recess is provided on an inner surface of the fuel guide, and one end of the assist air passage communicates with the annular recess.
【請求項3】 前記燃料噴射弁は、燃料に旋回成分を付
与する旋回素子を備えるものであって、前記燃料ガイド
に発生するアシストエアの旋回方向を、旋回素子による
燃料の旋回方向と同一にしたことを特徴とする請求項1
または2記載の内燃機関の燃料噴射装置。
3. The fuel injection valve according to claim 1, further comprising a swirl element for imparting a swirl component to the fuel, wherein a swirling direction of the assist air generated in the fuel guide is made the same as a swirling direction of the fuel by the swirl element. 2. The method according to claim 1, wherein
3. A fuel injection device for an internal combustion engine according to claim 2.
【請求項4】 前記燃料噴射弁のノズル部に噴孔中心と
同軸の環状エア通路を設け、前記アシストエア通路の途
中を、この環状エア通路に連通させたことを特徴とする
請求項1ないし3記載の内燃機関の燃料噴射装置。
4. The fuel injection valve according to claim 1, wherein an annular air passage coaxial with the center of the injection hole is provided in a nozzle portion of the fuel injection valve, and a midway of the assist air passage communicates with the annular air passage. 4. The fuel injection device for an internal combustion engine according to claim 3.
【請求項5】 前記アシストエア通路を、スキッシュ部
に開口する他端部に向かって拡径させたことを特徴とす
る請求項1ないし4記載の内燃機関の燃料噴射装置。
5. The fuel injection device for an internal combustion engine according to claim 1, wherein the diameter of the assist air passage increases toward the other end of the squish portion.
【請求項6】 前記燃料ガイドの内面に開口するアシス
トエア通路は、燃料噴射流に伴う流れを発生するよう噴
孔中心に対し所定の角度を有して開口することを特徴と
する請求項1ないし5記載の内燃機関の燃料噴射装置。
6. An assist air passage opening on an inner surface of the fuel guide, wherein the assist air passage opens at a predetermined angle with respect to a center of an injection hole so as to generate a flow accompanying a fuel injection flow. 6. The fuel injection device for an internal combustion engine according to any one of claims 5 to 5.
【請求項7】 前記スキッシュ部から環状エア通路に連
通するアシストエア通路の開口端を環状エア通路の中心
に対し偏倚させて設定したことを特徴とする請求項4記
載の内燃機関の燃料噴射装置。
7. The fuel injection device for an internal combustion engine according to claim 4, wherein an opening end of an assist air passage communicating from the squish portion to the annular air passage is set so as to be deviated from a center of the annular air passage. .
JP11013703A 1999-01-22 1999-01-22 Fuel injection system of internal combustion engine Pending JP2000213439A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP11013703A JP2000213439A (en) 1999-01-22 1999-01-22 Fuel injection system of internal combustion engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP11013703A JP2000213439A (en) 1999-01-22 1999-01-22 Fuel injection system of internal combustion engine

Publications (1)

Publication Number Publication Date
JP2000213439A true JP2000213439A (en) 2000-08-02

Family

ID=11840580

Family Applications (1)

Application Number Title Priority Date Filing Date
JP11013703A Pending JP2000213439A (en) 1999-01-22 1999-01-22 Fuel injection system of internal combustion engine

Country Status (1)

Country Link
JP (1) JP2000213439A (en)

Similar Documents

Publication Publication Date Title
KR930004967B1 (en) Electronic fuel injector
EP1042604B1 (en) Flat needle for pressurized swirl fuel injector
JPH01271656A (en) Fuel injection valve
JPS6350667A (en) Nozzle structure for electromagnetic type fuel injection valve
JPH07133727A (en) Air intake device of internal combustion engine
JPS5943962A (en) Fuel injection valve device of double suction engine
JP2778292B2 (en) Fuel injection device for internal combustion engine
JP2000213439A (en) Fuel injection system of internal combustion engine
JP2822847B2 (en) Fuel injection valve
US5597121A (en) Fuel injection valve
JP3132283B2 (en) Liquid injection valve
JPH05340326A (en) Fuel supply device for internal combustion engine
JP3286772B2 (en) Air assist type fuel injection valve
JP2617445B2 (en) Fuel injection valve
CN116733650A (en) Fuel injector, control method thereof and vehicle
JPH06317231A (en) Electromagnetic fuel injection valve and fuel injection device
JP2000314359A (en) Fuel injection valve
JP2004324596A (en) Fuel injection valve and internal combustion engine mounted with the same
JPH01285656A (en) Fuel injection device
JPH04350361A (en) Assist air type fuel injection valve
JPH11270444A (en) Air-assisted injector
JP2002349353A (en) Piston type carburetor
JPH04365968A (en) Fuel supply device of internal combustion engine
JPH09195894A (en) Hole type fuel injection nozzle
JPH08218985A (en) Air intake device of internal combustion engine

Legal Events

Date Code Title Description
A621 Written request for application examination

Free format text: JAPANESE INTERMEDIATE CODE: A621

Effective date: 20051124

A977 Report on retrieval

Free format text: JAPANESE INTERMEDIATE CODE: A971007

Effective date: 20070914

A131 Notification of reasons for refusal

Free format text: JAPANESE INTERMEDIATE CODE: A131

Effective date: 20071009

RD03 Notification of appointment of power of attorney

Free format text: JAPANESE INTERMEDIATE CODE: A7423

Effective date: 20071019

A521 Written amendment

Free format text: JAPANESE INTERMEDIATE CODE: A523

Effective date: 20071210

A131 Notification of reasons for refusal

Free format text: JAPANESE INTERMEDIATE CODE: A131

Effective date: 20080527

A02 Decision of refusal

Free format text: JAPANESE INTERMEDIATE CODE: A02

Effective date: 20081104