JPS5996475A - Fuel injection nozzle - Google Patents

Fuel injection nozzle

Info

Publication number
JPS5996475A
JPS5996475A JP20726082A JP20726082A JPS5996475A JP S5996475 A JPS5996475 A JP S5996475A JP 20726082 A JP20726082 A JP 20726082A JP 20726082 A JP20726082 A JP 20726082A JP S5996475 A JPS5996475 A JP S5996475A
Authority
JP
Japan
Prior art keywords
fuel
needle valve
injection
annular gap
fuel chamber
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
JP20726082A
Other languages
Japanese (ja)
Other versions
JPS622148B2 (en
Inventor
Hiroshi Miyake
博 三宅
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.)
Daihatsu Motor Co Ltd
Original Assignee
Daihatsu Motor Co Ltd
Daihatsu Kogyo KK
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 Daihatsu Motor Co Ltd, Daihatsu Kogyo KK filed Critical Daihatsu Motor Co Ltd
Priority to JP20726082A priority Critical patent/JPS5996475A/en
Publication of JPS5996475A publication Critical patent/JPS5996475A/en
Publication of JPS622148B2 publication Critical patent/JPS622148B2/ja
Granted legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M61/00Fuel-injectors not provided for in groups F02M39/00 - F02M57/00 or F02M67/00
    • F02M61/16Details not provided for in, or of interest apart from, the apparatus of groups F02M61/02 - F02M61/14

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Fuel-Injection Apparatus (AREA)

Abstract

PURPOSE:To approach injection properties to an ideal value, by installing a throttle mechanism which limits the substantial opening area of a fuel passage to a micro value in a primary injection area. CONSTITUTION:A throttle mechanism 9 is constituted such that a middle-sized column part 15, loosely engaged with the inner periphery of a shaft hole 11 with a fine annular gap 14, is formed between a large column part 12 of a needle valve 6, slidably mating with the shaft hole 11 in a nozzle body 2, and a taper part 13 of the needle valve 6 situated in a fuel chamber 3, an annular groove 16, communicated to the fuel chamber 3 through the annular gap 14, is provided in the vicinity of the lower end of the shaft hole 11, and a high-pressure fuel A, introduced from the start end of the fuel passage 1, can be guided to the fuel chamber 3 through the annular groove 16 and the annular gap 14. This constitution shows properties in that an injection rate is controlled to a low value until the lift amount of the needle valve 6 exceeds a specified value, and after exceeding the specified value, the injection rate is rapidly increased.

Description

【発明の詳細な説明】 本発明は、主としてディーゼルエンジンEこ使用される
燃料噴射ノズル1こ関するものである。
DETAILED DESCRIPTION OF THE INVENTION The present invention mainly relates to a fuel injection nozzle 1 used in a diesel engine E.

一般tこディーゼルエンジンでは、ノック音対策として
、燃料の噴射率を制御することが極めて重要であり、理
想的な噴射率としでは、第1図fこ実線aで示すようl
こ、初期Iζ低く次第1こ高(するのが望ましい。
In general diesel engines, it is extremely important to control the fuel injection rate as a countermeasure for knocking noise, and the ideal injection rate is as shown by the solid line a in Figure 1.
It is desirable that the initial value of Iζ be lower and then higher by one.

従来、かかる噴射率特性を得るためIζ、いわゆるスロ
ットル型あるいはビントル型の燃料噴射ノズルが多く使
用されているが、実際には前述したような理想的な噴射
率特性を得ることができない場合が少なくない。すなわ
ち、この種の噴射ノズルは、燃料通路を通して燃料室内
1ζ導入される高圧燃料の圧力によって針弁をリフトさ
せ、前記燃料室内の燃料を前記針弁のリフト量より開口
する噴口を介して所定の方向に噴射させ得ろようIこし
たものにおいて、前記噴口内fζ府記針弁の先端fこ設
けた小径円柱部を環状隙間を介して遊嵌させておき、前
記針弁がリフトし始める初期段階lこおいて微小な燃料
ft前記環状隙間を通して予備的1ζ噴射し得るように
構成したものである。ところが従来のものは、噴射ポン
プから送給される高圧燃料を単なるボート状の燃料通路
を通して前記燃料室へ直接に供給するようInしている
ので、燃料送給系統内で発生する圧力波等の影響を受け
て前記燃料室内の圧力が急激1ζ高まる傾向があり、針
弁が飛び上るようにして急速にリフトする現象を招き易
い。そのため、前記針弁の先端部分による絞り効果が発
揮される期間がきわめて短いものになってしまい、理想
とかけはなれた燃料噴射率特性すなわち、第1図に破線
すで示すような不本意な燃料噴射率特性しか得られない
ことが多い。
Conventionally, Iζ, so-called throttle-type or bottle-type fuel injection nozzles have often been used to obtain such injection rate characteristics, but in reality, it is often not possible to obtain the ideal injection rate characteristics as described above. do not have. That is, in this type of injection nozzle, a needle valve is lifted by the pressure of high-pressure fuel introduced into a fuel chamber 1ζ through a fuel passage, and the fuel in the fuel chamber is injected into a predetermined amount through a nozzle that opens by a lift amount of the needle valve. In the case where the injection can be made in one direction, a small diameter cylindrical part provided at the tip of the needle valve is loosely fitted in the nozzle through an annular gap, and the initial stage when the needle valve starts to lift. The structure is such that a small amount of fuel ft can be preliminarily injected through the annular gap. However, in conventional systems, the high-pressure fuel supplied from the injection pump is directly supplied to the fuel chamber through a simple boat-shaped fuel passage, so pressure waves generated within the fuel supply system are avoided. As a result, the pressure in the fuel chamber tends to increase rapidly by 1ζ, which tends to cause the needle valve to jump up and lift rapidly. As a result, the period during which the throttling effect by the tip of the needle valve is exerted becomes extremely short, resulting in a fuel injection rate characteristic that is far from ideal, i.e., an undesired fuel injection rate as shown by the broken line in Figure 1. In many cases, only injection rate characteristics can be obtained.

また、この種ノズル1こ関する先行技術として実開昭5
0−106520号に示されるようIこ、前記針弁の小
径円柱部に凹部を設けて初期噴射段階における絞り効果
をさらに高め得るよう1こしたものもある。しかしなが
ら、このものは針弁の先端部分における絞り効果を高め
るようにしただけのものであり、針弁の飛び上がりを防
止する効果は全(ない。しかして、前記針弁がかかる急
激な挙動を示すと、苦心して高めた絞り効果も、その発
揮される期間がきわめて短いものになり、前述したもの
と同様、劣悪な燃料噴射率特性しか得られないという不
都合かめる。
In addition, as a prior art related to this type of nozzle,
As shown in No. 0-106520, there is also a needle valve in which a concave portion is provided in the small-diameter cylindrical portion of the needle valve to further enhance the throttling effect in the initial injection stage. However, this method only enhances the throttling effect at the tip of the needle valve, and is not effective in preventing the needle valve from jumping up. Even the throttling effect, which has been painstakingly enhanced, is only available for a very short period of time, resulting in the disadvantage that, as mentioned above, only poor fuel injection rate characteristics can be obtained.

本発明は、このような事情1こ着目してなされたもので
、針弁のリフト量が所定の値を上まわるまでの初期噴射
領域mおいて燃料通路の実質的な開路面積を微小な値1
こ制限する絞り機構を設けることによって、前述した不
都合を効果的に解消し理想的な噴射率特性を得ることが
できるようにした燃料噴射ノズルを提供するものである
The present invention has been made in view of the above-mentioned circumstances, and is aimed at reducing the substantial open area of the fuel passage to a minute value in the initial injection region m until the lift amount of the needle valve exceeds a predetermined value. 1
The present invention provides a fuel injection nozzle that effectively eliminates the above-mentioned disadvantages and can obtain ideal injection rate characteristics by providing a throttle mechanism that limits this.

以下、本発明の一実施例を第2図を参照して説明する。An embodiment of the present invention will be described below with reference to FIG.

図示しない燃料噴射ポンプから吐出される高圧燃料Aを
燃料通路1を介してノズル本体2の内部に形成した燃料
室8内艮導くようlこし、この燃料室8内の高圧燃料A
を弁座部4の中心部に形成した噴口5を通してノズル本
体2外へ噴射させ得るように構成している。そして、針
弁6を前記弁座部4に接離可能に設け、この針弁6で前
記噴口5と前記燃料室8との連通状態を断続させるよう
にしている。なお、この針弁6は、図示しないばねによ
って前記弁座部4Iこ押し付けられており、前記燃料室
8内艮高圧燃料Aが導入された際にだけ、その圧力によ
りリフトして前記弁座部4から離れるようになっている
。また、この針弁6の先端−こは小径円柱部7が一体に
設けである。そしてこの小径円柱部7を前記噴口5内層
ζ微小な環状隙間8を介して遊嵌させ、前記針弁6が前
記弁座部4から離れようとする初期段階において微少な
燃料を前記環状隙間8を通して予備的にノズル本体2外
へ噴射させ得るように構成している。
The high-pressure fuel A discharged from a fuel injection pump (not shown) is introduced into the fuel chamber 8 formed inside the nozzle body 2 through the fuel passage 1.
is configured to be able to be injected to the outside of the nozzle body 2 through a nozzle 5 formed in the center of the valve seat portion 4. A needle valve 6 is provided on the valve seat portion 4 so as to be able to come into contact with and separate from the valve seat portion 4, and the needle valve 6 connects and disconnects the communication state between the jet nozzle 5 and the fuel chamber 8. The needle valve 6 is pressed against the valve seat 4I by a spring (not shown), and is lifted by the pressure only when high-pressure fuel A is introduced into the fuel chamber 8. It's starting to move away from 4. Further, a small diameter cylindrical portion 7 is integrally provided at the tip of the needle valve 6. Then, this small-diameter cylindrical portion 7 is loosely fitted through a minute annular gap 8 in the inner layer of the nozzle 5, and a minute amount of fuel is poured into the annular gap 8 in the initial stage when the needle valve 6 is about to separate from the valve seat portion 4. The nozzle body 2 is configured to be able to be preliminarily injected to the outside of the nozzle body 2 through the nozzle body 2.

このような燃料噴射ノズルCζおいて、前記燃料通路1
の終端に、前記針弁6のリフト量が所定の値を上まわる
までの初期噴射領域で該燃料通路1の実質的な開路面積
を微小な値に制限する絞り機構9を設けている。具体的
に説明すれば、絞り機構9は、ノズル本体2の軸孔11
にスライド可能1こ嵌合する針弁6の大径円柱部12と
、燃料室8円に臨む針弁6のテーパ部18との間に、前
記軸孔11の内周Iこ微小な環状隙間14を介して遊嵌
する中径円柱部15を形成するととも1こ、前記軸孔1
1の下端近傍部に前記環状隙間14を介して前記燃料室
8に連通ずる環状溝16を設け、前記燃料通路1の始端
側から導入した高圧燃料Aを前記環状溝16および前記
環状隙間14を通して5− 前記燃料室8へ導き得るようにしたものである。
In such a fuel injection nozzle Cζ, the fuel passage 1
A throttle mechanism 9 is provided at the terminal end of the fuel passage 1 to limit the substantial open area of the fuel passage 1 to a small value in the initial injection region until the lift amount of the needle valve 6 exceeds a predetermined value. To be more specific, the aperture mechanism 9 has a shaft hole 11 in the nozzle body 2.
There is a small annular gap between the large-diameter cylindrical part 12 of the needle valve 6 that can be slid into the inner circumference of the shaft hole 11 and the tapered part 18 of the needle valve 6 that faces the fuel chamber 8. When forming a medium-diameter cylindrical portion 15 that fits loosely through the shaft hole 1,
An annular groove 16 communicating with the fuel chamber 8 via the annular gap 14 is provided near the lower end of the fuel passage 1, and high-pressure fuel A introduced from the starting end side of the fuel passage 1 passes through the annular groove 16 and the annular gap 14. 5- The fuel can be led to the fuel chamber 8.

そして、前記環状隙間14の開口面積は、該環状隙間1
4部分における圧力損失が前記環状隙間8部分Iこおけ
る圧力損失よりも小さくなるような値に設定されている
。なお、17は、前記燃料室8内の燃料人を前記燃料通
路1へ直接に戻すための逆止弁であり、ボール18をば
ね19rこよりシート部2(H4弾接させてなる。この
逆止弁17は、針弁6の着座を迅速1ζ行なわせるため
に設けである。
The opening area of the annular gap 14 is the annular gap 1
The pressure loss in the 4th section is set to a value smaller than the pressure loss in the 8th section I of the annular gap. Reference numeral 17 is a check valve for directly returning the fuel in the fuel chamber 8 to the fuel passage 1, and the ball 18 is brought into elastic contact with the seat portion 2 (H4) by a spring 19r. The valve 17 is provided to quickly seat the needle valve 6.

このような構成のものであれば、基本的には従来のスロ
ットル型あるいはビントル型の燃料噴射弁と同様な作動
mより燃料室8内−導入された高圧燃料人が噴口5を通
してノズル本体2外、つまり、図示しないディーゼルエ
ンジンの燃焼室内に噴射されることCζなり、このとき
の噴射率は、針弁6のリフト量が一定の値を上まわるま
では低い値に抑制され、以後、急速に高くなるという特
性を示す。しかも、本発明では、前記燃料室8の前段側
に絞り機構9を設け、前記針弁6のリフト6− 量が一定の値lを上まわるまでの初期噴射領域で燃料通
路1の実質的な開路面積を微小な値[こ制限するよう1
こしている。すなわち、この実施例では針弁6のリフト
量が前記一定値lを上まわるまでは、該針弁6の中径円
柱部15とノズル本体2の軸孔11の内周面との間に微
小な環状隙間14が形成され、燃料通路1内「こ導入さ
れた高圧燃料Aが環状溝16および前記環状隙間14を
順次fこ通って前記燃料室8内1こ導びかれるよう1こ
なっている。そのため、前記高圧燃料Aが前記燃料室3
1こ達するまでに大きな圧力損失を伴うこと1ζなる。
With such a configuration, the high-pressure fuel introduced into the fuel chamber 8 is basically operated in the same way as a conventional throttle type or bottle type fuel injection valve, and the high-pressure fuel is pumped through the nozzle 5 and out of the nozzle body 2. In other words, the injection rate Cζ is injected into the combustion chamber of a diesel engine (not shown), and the injection rate at this time is suppressed to a low value until the lift amount of the needle valve 6 exceeds a certain value, and then rapidly increases. It exhibits the characteristic of becoming higher. Moreover, in the present invention, a throttle mechanism 9 is provided on the upstream side of the fuel chamber 8, and the substantial flow of the fuel passage 1 is provided in the initial injection region until the lift amount of the needle valve 6 exceeds a certain value l. 1 to limit the open circuit area to a small value [this]
It's straining. That is, in this embodiment, until the lift amount of the needle valve 6 exceeds the above-mentioned constant value l, there is a small gap between the medium diameter cylindrical part 15 of the needle valve 6 and the inner peripheral surface of the shaft hole 11 of the nozzle body 2. An annular gap 14 is formed so that the high-pressure fuel A introduced into the fuel passage 1 is guided into the fuel chamber 8 through the annular groove 16 and the annular gap 14 sequentially. Therefore, the high pressure fuel A is in the fuel chamber 3.
A large pressure loss is involved until the pressure reaches 1ζ.

その結果、前記燃料通路11ζ導入される高圧燃料へに
大きな圧力変動があっても、前記燃料室3内の圧力は比
較的なめらかζこ上昇することこなり、針弁6が飛び上
るよう1こしてリフトするという現象を無くすことがで
きる。すなわち、前記針弁6を安定した速度でリフトさ
せろことが可能となる。
As a result, even if there is a large pressure fluctuation in the high-pressure fuel introduced into the fuel passage 11ζ, the pressure inside the fuel chamber 3 will rise relatively smoothly, and the pressure in the fuel chamber 3 will rise relatively smoothly, causing the needle valve 6 to jump up. It is possible to eliminate the phenomenon of lifting. That is, it becomes possible to lift the needle valve 6 at a stable speed.

したがって、針弁6の小径円柱部7Iこより噴射率を制
御する時間が十分tこ確保され、初期噴射率がなめらか
lこ上昇することIこなって、第1図に実線aで示すよ
うな理想的な噴射率特性fこ近い特性を得ることができ
るものである。
Therefore, sufficient time is secured for controlling the injection rate through the small-diameter cylindrical portion 7I of the needle valve 6, and the initial injection rate rises smoothly. It is possible to obtain a characteristic similar to that of the injection rate characteristic f.

一部、I’nl記針弁6のリフト量が一定値を上まわる
と、該針弁6のテーバ部18が前記環状溝16に対向す
ること薯こなるため、前記燃料通路1内の高圧燃料Aは
抵抗なしCcOU記燃料室3内に導入される。また、燃
料噴射時期が終了し前記針弁6が着座する際1こは、前
記燃料室B内の燃料Aの一部が逆止弁17を介して前記
燃料通路1へ直接良戻される。そのため、前記針弁6の
着座が速かlこ完了する。
Partly, when the lift amount of the I'nl needle valve 6 exceeds a certain value, the tapered portion 18 of the needle valve 6 faces the annular groove 16, which causes high pressure in the fuel passage 1. Fuel A is introduced into the fuel chamber 3 without resistance. Furthermore, when the fuel injection period ends and the needle valve 6 is seated, a portion of the fuel A in the fuel chamber B is directly returned to the fuel passage 1 via the check valve 17. Therefore, the seating of the needle valve 6 is quickly completed.

なお、本発明は、スロットル型あるいはビントル型の噴
射ノズルに限らず、直噴型のノズル等あらゆる型式の噴
射ノズル1こ適用が可能である。
The present invention is not limited to throttle type or bottle type injection nozzles, but can be applied to all types of injection nozzles such as direct injection nozzles.

また、絞り機構の構成も前記実施例のものlこ限られな
いのは勿論であり、例えは、第8図Iこ示すようなもの
であってもよい。すなわち、第8図1こ示す絞り機構9
′は、ノズル本体2の軸孔11の内周1乙針弁6とのシ
C微小な環状隙間14’を形成する浅い環状溝21と燃
料通路IIL連通する探し)環状溝22とを並設すると
ともに、前記針弁6内1(、ボート2Bを、その一端を
前記環状溝21足対向させ他端を燃料室8Iζ連通させ
て形成したものであり、前記針弁6のリフト量が一定の
値l!Iを上まわるまでの間は、前記燃料通路1内fこ
導入された高圧燃料Aが微小な環状隙間14’を通して
前記ボート28内1ζ案内され前記燃料室8内(導びか
れるようになっている。
Furthermore, the configuration of the diaphragm mechanism is of course not limited to that of the embodiment described above, and may be as shown in FIG. 8, for example. That is, the aperture mechanism 9 shown in FIG.
' is a shallow annular groove 21 that forms a small annular gap 14' between the inner circumference 1 of the shaft hole 11 of the nozzle body 2 and the needle valve 6, and an annular groove 22 that communicates with the fuel passage IIL. At the same time, the needle valve 6 has a boat 2B with one end facing the annular groove 21 and the other end communicating with the fuel chamber 8Iζ, so that the lift amount of the needle valve 6 is constant. Until the value l!I is exceeded, the high-pressure fuel A introduced into the fuel passage 1 is guided into the boat 28 through a minute annular gap 14' and into the fuel chamber 8. It has become.

さらに、燃料室と燃料通路との間に設けた逆止弁は、か
ならずしも必要なものではないが、かかる逆止弁を設け
ておけば、針弁の着座が迅速に行なわれるtこめ、着座
のもたつきにより燃料の噴射状態が乱れて熱効率が低下
するという不都合を無くすことができる。
Further, although a check valve provided between the fuel chamber and the fuel passage is not necessarily necessary, if such a check valve is provided, the needle valve can be seated quickly. It is possible to eliminate the inconvenience that the fuel injection state is disturbed due to sluggishness and thermal efficiency is reduced.

本発明は、以上のような構成であるから、初期噴射領域
において針弁を安定した速度でスムーズにリフトさせる
ことが可能であり、したがって初期噴射率の特性をより
理想lこ近づけることができる燃料噴射ノズルを提供で
きるものでみる。
Since the present invention has the above-described configuration, it is possible to lift the needle valve smoothly at a stable speed in the initial injection region, and therefore it is possible to obtain a fuel that can bring the characteristics of the initial injection rate closer to the ideal. Let's take a look at what spray nozzles we can provide.

【図面の簡単な説明】[Brief explanation of the drawing]

9− 第1図は噴射率特性を説明するための図、第2図は本発
明の一実施例を示す断面図、第8図は本発明の他の実施
例を示す断面図である。 1・・・燃料通路  8・・・燃料室 5・・・噴口  6・・・針弁 9.9′・・・絞り機構 代理人 弁理士 赤澤−博 10−
9- FIG. 1 is a diagram for explaining injection rate characteristics, FIG. 2 is a cross-sectional view showing one embodiment of the present invention, and FIG. 8 is a cross-sectional view showing another embodiment of the present invention. 1... Fuel passage 8... Fuel chamber 5... Nozzle 6... Needle valve 9.9'... Throttle mechanism agent Patent attorney Hiroshi Akazawa 10-

Claims (1)

【特許請求の範囲】[Claims] 燃料通路を通して燃料室内lこ導入される高圧燃料の圧
力によって針弁をリフトさせ、前記燃料室内の高圧夜料
を前記針弁のリフトlこより開口する噴口を介して所定
の方向lこ噴射させ得るようfこ構成した燃料噴射ノズ
ルにおいて、前記針弁のリフト量が所定の値を上まわる
までの初期噴射領域で前記燃料通路の実質的な開路面積
を微小な値に制限する絞り機構を設けたことを特徴とす
る燃料噴射ノズル。
The needle valve is lifted by the pressure of high-pressure fuel introduced into the fuel chamber through the fuel passage, and the high-pressure fuel in the fuel chamber is injected in a predetermined direction through a nozzle opening from the lift of the needle valve. In the fuel injection nozzle configured as shown in FIG. A fuel injection nozzle characterized by:
JP20726082A 1982-11-25 1982-11-25 Fuel injection nozzle Granted JPS5996475A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP20726082A JPS5996475A (en) 1982-11-25 1982-11-25 Fuel injection nozzle

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP20726082A JPS5996475A (en) 1982-11-25 1982-11-25 Fuel injection nozzle

Publications (2)

Publication Number Publication Date
JPS5996475A true JPS5996475A (en) 1984-06-02
JPS622148B2 JPS622148B2 (en) 1987-01-17

Family

ID=16536842

Family Applications (1)

Application Number Title Priority Date Filing Date
JP20726082A Granted JPS5996475A (en) 1982-11-25 1982-11-25 Fuel injection nozzle

Country Status (1)

Country Link
JP (1) JPS5996475A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS6371564A (en) * 1986-10-23 1988-03-31 Kubota Ltd Accumulation fuel injector
JPS6371565A (en) * 1986-10-23 1988-03-31 Kubota Ltd Accumulator fuel injection device
WO2005068824A1 (en) * 2004-01-15 2005-07-28 Robert Bosch Gmbh Fuel injection valve for internal combustion engines

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS6371564A (en) * 1986-10-23 1988-03-31 Kubota Ltd Accumulation fuel injector
JPS6371565A (en) * 1986-10-23 1988-03-31 Kubota Ltd Accumulator fuel injection device
WO2005068824A1 (en) * 2004-01-15 2005-07-28 Robert Bosch Gmbh Fuel injection valve for internal combustion engines

Also Published As

Publication number Publication date
JPS622148B2 (en) 1987-01-17

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