JPS6153550B2 - - Google Patents

Info

Publication number
JPS6153550B2
JPS6153550B2 JP55024629A JP2462980A JPS6153550B2 JP S6153550 B2 JPS6153550 B2 JP S6153550B2 JP 55024629 A JP55024629 A JP 55024629A JP 2462980 A JP2462980 A JP 2462980A JP S6153550 B2 JPS6153550 B2 JP S6153550B2
Authority
JP
Japan
Prior art keywords
valve
nozzle
needle
fuel
hole
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired
Application number
JP55024629A
Other languages
Japanese (ja)
Other versions
JPS55117066A (en
Inventor
Fuhasu Piitaa
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.)
Sulzer AG
Original Assignee
Sulzer AG
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 Sulzer AG filed Critical Sulzer AG
Publication of JPS55117066A publication Critical patent/JPS55117066A/en
Publication of JPS6153550B2 publication Critical patent/JPS6153550B2/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
    • F02M45/00Fuel-injection apparatus characterised by having a cyclic delivery of specific time/pressure or time/quantity relationship
    • F02M45/02Fuel-injection apparatus characterised by having a cyclic delivery of specific time/pressure or time/quantity relationship with each cyclic delivery being separated into two or more parts
    • F02M45/04Fuel-injection apparatus characterised by having a cyclic delivery of specific time/pressure or time/quantity relationship with each cyclic delivery being separated into two or more parts with a small initial part, e.g. initial part for partial load and initial and main part for full load
    • F02M45/08Injectors peculiar thereto
    • F02M45/086Having more than one injection-valve controlling discharge orifices
    • 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
    • F02M61/18Injection nozzles, e.g. having valve seats; Details of valve member seated ends, not otherwise provided for
    • 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
    • F02M61/18Injection nozzles, e.g. having valve seats; Details of valve member seated ends, not otherwise provided for
    • F02M61/1806Injection nozzles, e.g. having valve seats; Details of valve member seated ends, not otherwise provided for characterised by the arrangement of discharge orifices, e.g. orientation or size

Landscapes

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

Description

【発明の詳細な説明】 本発明は往復ピストン式内燃機関用燃料噴射弁
にして、シリンダの燃焼室内に突出する弁体を有
し、該弁体がその内部に弁座と共働する弁針を備
えると共に該弁針の周囲に分散配置された複数の
ノズル孔を有し、該ノズル孔を通る燃料が律動的
に前記弁針を弁座から持上げて燃焼室内に噴出す
るようになつている燃料噴射弁に関する。
DETAILED DESCRIPTION OF THE INVENTION The present invention is a reciprocating piston type fuel injection valve for an internal combustion engine, which has a valve body protruding into a combustion chamber of a cylinder, and has a valve needle therein that cooperates with a valve seat. and a plurality of nozzle holes distributed around the valve needle, and the fuel passing through the nozzle holes rhythmically lifts the valve needle from the valve seat and is ejected into the combustion chamber. Regarding fuel injection valves.

燃料噴射弁は一般的に機関の全負荷時にはすぐ
れた燃料噴流を形成し、したがつてシリンダの燃
焼室内に好適な無煙燃焼を行わせるように設計さ
れている。この設計を行う時には直径の比較的大
きなノズル孔を1列に配置し、または該ノズル孔
を2列に配置し、後者の場合には孔の直径が対応
して小さくなるように選択される。内燃機関が部
分負荷で運転される場合には噴流の形成および燃
焼に対して最適の条件が得られないようになるこ
とはすでに知られている。
Fuel injection valves are generally designed to produce a good fuel jet at full engine load, thus ensuring good smokeless combustion within the combustion chamber of the cylinder. When carrying out this design, the nozzle holes with a relatively large diameter are arranged in one row, or the nozzle holes are arranged in two rows, in the latter case the diameter of the holes being selected to be correspondingly small. It is already known that when internal combustion engines are operated under partial load, optimal conditions for jet formation and combustion are not achieved.

本発明の目的は前述の型の燃料噴射弁におい
て、部分負荷時においても噴流が好適に形成さ
れ、したがつて燃料の燃焼を好適に維持し得るよ
うになつた燃料噴射弁を供することである。
An object of the present invention is to provide a fuel injection valve of the above-mentioned type, in which a jet flow is suitably formed even under partial load, and therefore fuel combustion can be suitably maintained. .

前記目的は本発明によれば前記燃料噴射弁に、
弁針から分離された装置を設け、それによつて機
関の部分負荷時には前記ノズル孔の少なくともい
くつかのノズル孔の面積を部分的に開放し、かつ
全負荷時にはすべてのノズル孔の全面積を開放す
るようになすことによつて達成される。
According to the invention, the purpose is to provide the fuel injection valve with:
A device separate from the valve needle is provided, by means of which the area of at least some of said nozzle holes is partially opened during partial loads of the engine, and the total area of all nozzle holes is opened during full loads. This is accomplished by doing what you want.

このような装置によれば機関の部分負荷時にお
いては前記ノズル孔の少なくともいくつかのノズ
ル孔の開口面積を小さくし、噴流の形成を容易に
し得ると共に燃料の燃焼状態を好適な状態に維持
することができる。機関の全負荷時においては前
記装置はすべてのノズル孔の全断面を開放するよ
うに作動する。
According to such a device, when the engine is under partial load, the opening area of at least some of the nozzle holes can be reduced, making it easier to form a jet flow and maintaining the combustion state of the fuel in a suitable state. be able to. At full engine load, the device operates to open the entire cross section of all nozzle holes.

次に添付図面によつて本発明の実施例を説明す
る。
Next, embodiments of the present invention will be described with reference to the accompanying drawings.

第1図に示される如く燃料噴射弁は弁体1を有
し、該弁体は上方部分2およびノズル部材3より
なり、これら部分は袋ナツト4によつて相互に結
合されている。弁体1はフランジ5によつてシリ
ンダヘツド6の上に触座し、該シリンダヘツドは
ピストン往復内燃機関のシリンダの燃焼室8を上
方から閉鎖している。前記弁体はシリンダヘツド
6を通り、そのノズル部材3の複数のノズル孔7
を有する端部が燃焼室8内に突出するようになつ
ている。
As shown in FIG. 1, the fuel injection valve has a valve body 1 consisting of an upper part 2 and a nozzle member 3, which parts are interconnected by a cap nut 4. The valve body 1 rests by means of a flange 5 on a cylinder head 6, which closes off a combustion chamber 8 of a cylinder of a reciprocating piston internal combustion engine from above. The valve body passes through the cylinder head 6 and into a plurality of nozzle holes 7 of the nozzle member 3.
An end portion having a diameter protrudes into the combustion chamber 8.

燃料を供給するために弁体1は管路10を有
し、この管路は先ずフランジ5を通つて半径方向
に延び、次に部分2,ノズル部材3を通つて実質
的に弁体の縦方向に延び、前記ノズル部材3の下
端区域に達するようになつている。前記管路10
は環状室11内で終つている。弁体1の中央には
軸線方向に移動し得る弁針12が設けられ、該弁
針の上端はばね座金13を介して圧縮ばね14に
よつて支持されている。弁針12の下端には球形
の座面15が設けられ、該座面は弁針12を取り
囲んで延び且つ弁針12の軸線方向に滑動自在で
あつてノズル孔7の開度を変化させる弁部材16
内の対応する球形座面と共働し、前記ブツシユは
針12を囲繞すると共に、弁体1のノズル部材3
内に軸線方向に移動し得るように軸持されてい
る。
For supplying fuel, the valve body 1 has a conduit 10 which first extends radially through the flange 5 and then through the section 2, nozzle member 3 and substantially longitudinally of the valve body. The nozzle member 3 extends in the direction to reach the lower end area of the nozzle member 3. Said conduit 10
terminates in an annular chamber 11. An axially movable valve needle 12 is provided in the center of the valve body 1, the upper end of which is supported by a compression spring 14 via a spring washer 13. A spherical seat surface 15 is provided at the lower end of the valve needle 12, and the seat surface extends around the valve needle 12 and is slidable in the axial direction of the valve needle 12 to change the opening degree of the nozzle hole 7. Member 16
Co-operating with a corresponding spherical seat within the bush, said bush surrounds the needle 12 and the nozzle member 3 of the valve body 1.
The shaft is supported for axial movement within the shaft.

弁部材16は環状室11の区域に複数の孔17
を有し、この孔は燃料を該環状室11から、弁部
材16と弁針12の区間18との間の環状室19
に移行させる。この環状室19はその下端におい
て座面15を画定している。弁部材16は孔17
の下方に球形座面20を有し、この座面は弁体1
のノズル部材3に設けられた対応する座面と共働
する。弁部材16は座面20,15の下方に外方
円筒形肩21を有し、該肩の下端は前縁22を形
成し、この前縁はノズル孔7と共働し、かつ弁部
材16の高さと関連して第2a図および第2b図
に示される如くノズル孔7の開口面積を変える。
The valve member 16 has a plurality of holes 17 in the area of the annular chamber 11.
, the hole carries fuel from the annular chamber 11 to an annular chamber 19 between the valve member 16 and the section 18 of the valve needle 12.
to be transferred to This annular chamber 19 defines a seat surface 15 at its lower end. Valve member 16 has hole 17
It has a spherical seat surface 20 below the valve body 1.
co-operates with a corresponding seating surface provided on the nozzle member 3. The valve member 16 has an outer cylindrical shoulder 21 below the seating surfaces 20, 15, the lower end of which forms a front edge 22 which cooperates with the nozzle bore 7 and which The opening area of the nozzle hole 7 is changed as shown in FIGS. 2a and 2b in relation to the height of the nozzle.

ノズル部材3に対して捩れないようにされてい
るノズル部材16はその上端においてピストン状
中間部材25に対して触座し、該中間部材は弁体
1の部分2の円筒形孔の中を摺動し、かつその上
端は別のブツシユ26に対して触座している。前
記ピストン状中間部材25と前記別のブツシユ2
6とは弁針12を囲繞している。前記ブツシユ2
6自体はばね座金27を介して圧縮ばね28に対
して支持され、ばね28の上端はばね座金29に
対して触座し、該ばね座金は弁体1内において圧
縮ばね14のばね座金13の下に配置されてい
る。ばね座金29は隔置スリーブ30およびフラ
ンジ5に螺着された中空ねじ31によつて弁体1
の中に固定されている。前記中空ねじ31は圧縮
ばね14の上端を囲繞し、該圧縮ばねは前記中空
ねじの中にねじ込まれたねじ32に触座してい
る。
The nozzle member 16 , which is prevented from twisting relative to the nozzle member 3 , rests at its upper end against a piston-like intermediate member 25 , which slides in a cylindrical bore in the part 2 of the valve body 1 . and its upper end rests against another bush 26. The piston-shaped intermediate member 25 and the another bush 2
6 surrounds the valve needle 12. The button 2
6 itself is supported via a spring washer 27 against a compression spring 28 , and the upper end of the spring 28 rests against a spring washer 29 , which presses against the spring washer 13 of the compression spring 14 within the valve body 1 . located below. The spring washer 29 is attached to the valve body 1 by means of a spacing sleeve 30 and a hollow screw 31 screwed onto the flange 5.
is fixed inside. The hollow screw 31 surrounds the upper end of the compression spring 14, which rests on a screw 32 screwed into the hollow screw.

前記ピストン状中間部材25を受入れるシリン
ダ室の中には管路36が開口し、該管路は実質的
に弁体1を通つて縦方向に延び、かつその上端は
フランジ5内を縦方向に延びるようになつてい
る。前記管路36は圧力媒体源(図示せず)に連
結され、該圧力媒体源は弁を介してフランジ5に
連結されている。前記シリンダ室の上方衝当面3
5は中間部材25の運動に対する衝当部材を形成
し、この衝当部材はなるべくは調節自在に形成さ
れ、かつこの調節には機械的または液圧的手段を
使用することができる。
A conduit 36 opens into the cylinder chamber receiving the piston-like intermediate member 25, which conduit 36 extends substantially longitudinally through the valve body 1 and whose upper end extends longitudinally into the flange 5. It's starting to lengthen. Said line 36 is connected to a pressure medium source (not shown), which is connected to the flange 5 via a valve. Upper impact surface 3 of the cylinder chamber
5 forms an abutment for the movement of the intermediate member 25, which is preferably designed to be adjustable, and mechanical or hydraulic means can be used for this adjustment.

前記燃料噴射弁は次の如き態様で作動する。内
燃機関の全負荷時においては管路36を通る圧力
媒体の供給は遮断され、弁部材16は圧縮ばね2
8の圧力だけを受けている。周期的に管路10に
導かれた高圧の燃料は孔17を通つて環状室19
に達し、ここで先ず弁針12をばね14の圧力に
逆つて持上げる。したがつて弁の座面15が弁部
材16内の対応する座面から持上げられ、燃料は
ノズル孔7の前の室に達する。弁部材16の上端
に働らく力はばね28の圧力だけであるから、こ
のブツシユは燃料の圧力を受けて上昇し、その前
縁22はすべてのノズル7を開口し、かつ燃料は
孔7を通り、前縁22によつて妨げられることな
くシリンダの燃料室8に達する(第2b図)。こ
のようにして燃料圧力が低下した後、弁部材16
および弁針12は再び第1図に示された出発位置
に復帰する。
The fuel injection valve operates in the following manner. At full load of the internal combustion engine, the supply of pressure medium through the line 36 is cut off, and the valve member 16 is connected to the compression spring 2.
I am only under the pressure of 8. The high-pressure fuel periodically introduced into the line 10 passes through the hole 17 into the annular chamber 19.
, at which point the valve needle 12 is first lifted against the pressure of the spring 14. The valve seat 15 is thus lifted from the corresponding seat in the valve member 16 and the fuel reaches the chamber in front of the nozzle bore 7. Since the only force acting on the upper end of the valve member 16 is the pressure of the spring 28, this bush will rise under the pressure of the fuel, its leading edge 22 will open all the nozzles 7, and the fuel will flow through the holes 7. and reaches the fuel chamber 8 of the cylinder unobstructed by the leading edge 22 (FIG. 2b). After the fuel pressure has decreased in this way, the valve member 16
The valve needle 12 then returns to the starting position shown in FIG.

内燃機関が部分負荷で運転される場合には管路
36を通る圧力媒体の供給が行われ、弁部材16
に対してはばね28の圧力の他に、ピストン型中
間部材25に対する圧力媒体の圧力が作用し、か
つ弁部材16はその下方位置に押し下げられる。
管路10を通して供給された燃料は再び環状室1
1に達し、かつ孔17を通つて環状室19に至
り、ここで燃料は針12をばね14の圧力に逆つ
て上方に移動せしめ、ノズル孔7の前方の室に流
入し得るようになる。この室から出た燃料は次に
第2の各孔7を通つてシリンダの燃焼室8に流入
し、この時全部の孔7の開口面積が小さくなる。
その理由は弁部材16の前縁22が1つおきの各
ノズル孔7を部分的に被覆し、かつ残余のノズル
孔が弁部材16によつて完全に閉鎖されているか
らである(第2a図)。すなわち、弁部材16の
前縁22には第2a図で示されるように複数のノ
ズル孔7のうちの一部のみを開放するように周囲
にわたつて複数の凹所が備えられていて、機関の
部分負荷時におけるノズル孔7の面積の1部解放
が複数のノズル孔7のうちの一部のみに生ずるよ
うに構成されている。
When the internal combustion engine is operated under partial load, pressure medium is supplied through line 36 and valve member 16
In addition to the pressure of the spring 28, the pressure of the pressure medium on the piston-shaped intermediate member 25 acts on the valve member 16, and the valve member 16 is pushed down into its lower position.
The fuel supplied through the line 10 returns to the annular chamber 1
1 and passes through the hole 17 into the annular chamber 19, where the fuel causes the needle 12 to move upwards against the pressure of the spring 14 and can flow into the chamber in front of the nozzle hole 7. The fuel leaving this chamber then flows through the second holes 7 into the combustion chamber 8 of the cylinder, the opening area of all the holes 7 being reduced.
This is because the leading edge 22 of the valve member 16 partially covers every other nozzle hole 7, and the remaining nozzle holes are completely closed by the valve member 16 (second a). figure). That is, as shown in FIG. 2a, the front edge 22 of the valve member 16 is provided with a plurality of recesses around the periphery so as to open only a portion of the plurality of nozzle holes 7. The structure is such that a partial release of the area of the nozzle holes 7 occurs in only some of the plurality of nozzle holes 7 during a partial load.

第3a図乃至第3c図に示された実施例におい
てはノズル孔7と共働する弁部材16の下端は鋸
歯状に形成され、ノズル孔と同数の歯40を有し
ている。各歯40は弁部材16から下方に向つて
細くなり、かつブツシユの外周から内周に向つて
先細に延び、刃先を形成するようになつている。
各歯40の最大幅はノズル孔の直径とほぼ等し
く、かつ各歯の高さはノズル孔の直径よりわずか
に大となるように形成されている。部分負荷の時
は弁部材16は第3a図に示された位置を占め、
この位置においては各ノズル孔7の前に歯40が
位置し、この歯は燃料が孔7の全面積の1部分を
通るようにすると共に、この孔7を通る燃料の噴
流を複数本に縦断し、燃焼室8内において大気酸
素を工合良く燃料部分に接近せしめ得るようにな
つている。したがつて部分負荷時においても完全
な燃焼が行われる。全負荷時においては弁部材1
6は第3b図に示された位置を占め、この位置に
おいては燃料は何物によつても妨げられることな
く鋸歯状の歯を通つてノズル7に流入する。
In the embodiment shown in FIGS. 3a to 3c, the lower end of the valve member 16 cooperating with the nozzle hole 7 is serrated and has the same number of teeth 40 as there are nozzle holes. Each tooth 40 tapers downward from the valve member 16 and tapers from the outer circumference to the inner circumference of the bush to form a cutting edge.
The maximum width of each tooth 40 is approximately equal to the diameter of the nozzle hole, and the height of each tooth is slightly larger than the diameter of the nozzle hole. At part load, the valve member 16 assumes the position shown in FIG. 3a;
In this position, each nozzle hole 7 is preceded by a tooth 40 which allows the fuel to pass through a portion of the total area of the hole 7 and which cuts the jet of fuel through this hole 7 longitudinally. However, atmospheric oxygen can be conveniently brought close to the fuel portion within the combustion chamber 8. Complete combustion therefore takes place even under partial load. At full load, valve member 1
6 occupies the position shown in FIG. 3b, in which the fuel flows unimpeded by anything into the nozzle 7 through the serrations.

第4a図および第4b図に示された実施例にお
いては弁部材16の前縁22は半径方向の切欠き
41を有し、各切欠きは各ノズル孔7と関連せし
められ、かつ三角形の断面を有している。この例
においても部分負荷時には各ノズル孔7の開口面
積の1部分だけが開放され(第4a図)、かつ孔
を通る燃料の噴流は切欠きによつて複数の小さな
部分に分割され、したがつて燃焼が工合良く行わ
れるようになる。これに反し全負荷時においては
燃料は妨げられることなくすべてのノズル孔の全
開口面積を通る(第4b図)。同様なことは第5
a図(部分負荷)および第5b図(全負荷)の実
施例の場合にも起こり、この時は弁部材16の前
縁22は各ノズル孔の区域に二つの半径方向の切
欠き42を有している。
In the embodiment shown in FIGS. 4a and 4b, the front edge 22 of the valve member 16 has a radial notch 41, each notch being associated with a respective nozzle hole 7 and having a triangular cross-section. have. In this example, too, at partial load only a portion of the opening area of each nozzle hole 7 is opened (Fig. 4a), and the jet of fuel passing through the hole is divided into a plurality of small portions by the notch. As a result, combustion can be carried out efficiently. At full load, on the other hand, the fuel passes unhindered through the entire opening area of all nozzle holes (FIG. 4b). The same thing is the fifth
This also occurs in the case of the embodiments of FIG. are doing.

第6a図および第6b図に示された実施例にお
いては前縁22は弁部材16の円周上に平らな縁
として形成され、かつノズル孔7はノズル部材3
内に2列に重なるように位置決めされている。部
分負荷の場合は上方列のノズル孔だけが部分的に
開放され、同時に下方列のすべてのノズル孔が開
放される(第6a図)。全負荷時においては下方
列のすべてのノズル孔の他に上方列のすべてのノ
ズル孔の全てが開放され、燃料を通すようになつ
ている(第6b図)。
In the embodiment shown in FIGS. 6a and 6b, the leading edge 22 is formed as a flat edge on the circumference of the valve member 16, and the nozzle hole 7 is formed as a flat edge on the circumference of the valve member 16.
They are positioned so that they overlap in two rows inside. In the case of partial load, only the nozzle holes of the upper row are partially opened, and at the same time all the nozzle holes of the lower row are opened (FIG. 6a). At full load, all the nozzle holes in the lower row as well as all the nozzle holes in the upper row are open to allow fuel to pass through (FIG. 6b).

前述の如く衝当面35は調整自在であるから、
第3a図乃至第6a図に示された実施例において
は、燃料の噴射時に前縁22が中間位置を占め、
ノズル孔の開口面積を変えるブツシユの機能が前
記中空針の中に軸持された棒によつて得られるよ
うになすことができる。
As mentioned above, since the impact surface 35 is adjustable,
In the embodiment shown in FIGS. 3a to 6a, the leading edge 22 occupies an intermediate position during fuel injection;
The function of the bush for changing the opening area of the nozzle hole can be achieved by a rod supported in the hollow needle.

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

第1図は本発明による燃料噴射弁の軸線方向断
面図;第2a図および第2b図はそれぞれ第1図
を拡大して示したノズル孔区域の部分的展開図;
第3a図および第3b図はそれぞれ本発明による
燃料噴射弁の変型のノズル孔区域における断面
図;第3c図は第3a図の線―に沿つて取ら
れた断面図;第4a図および第4b図はそれぞれ
別の変型実施例ノズル孔区域における断面図;5
a図,5b図および第6a図,第6b図はそれぞ
れ二つの変型実施例のノズル孔区域における断面
図である。 図において1は弁体、2は上方部分、3はノズ
ル部材、6はシリンダヘツド、7はノズル孔、8
は燃焼室、10は管路、11は環状室、12は弁
針、16は弁部材、17は孔、19は環状室、2
2は前縁、26はブツシユ、30は隔置スリー
ブ、36は管路である。
FIG. 1 is an axial sectional view of a fuel injection valve according to the present invention; FIGS. 2a and 2b are partially exploded views of the nozzle hole area, respectively, which are enlarged views of FIG. 1;
3a and 3b are respectively sectional views in the nozzle hole area of a variant of the fuel injection valve according to the invention; FIG. 3c is a sectional view taken along the line - of FIG. 3a; FIGS. 4a and 4b The figures are cross-sectional views in the nozzle hole area of different variant embodiments; 5
Figures a, 5b and 6a, 6b each show cross-sections in the area of the nozzle bore of two variant embodiments. In the figure, 1 is a valve body, 2 is an upper part, 3 is a nozzle member, 6 is a cylinder head, 7 is a nozzle hole, and 8
1 is a combustion chamber, 10 is a pipe, 11 is an annular chamber, 12 is a valve needle, 16 is a valve member, 17 is a hole, 19 is an annular chamber, 2
2 is a front edge, 26 is a bush, 30 is a spacing sleeve, and 36 is a conduit.

Claims (1)

【特許請求の範囲】[Claims] 1 往復動内燃機関用の燃料噴射弁にして、シリ
ンダの燃焼室8内に突出するノズル部材3を含む
弁体1を有し、該ノズル部材3はその内部に弁座
15と協働する弁針12を有するとともに、その
周囲に分散配置された複数のノズル孔7を有して
おり、該弁針12が該弁座15から離れた時に燃
料が該ノズル孔7を通つて該燃焼室8内に周期的
に流出するようになつており、該弁針12を取り
囲んで延び且つ該弁針12の軸線方向に滑動自在
であつて該ノズル孔7の開閉を制御する弁部材1
6を有し、この弁部材16は機関の全負荷時には
すべてのノズル孔7の全面積を開放するようにな
つている燃料噴射弁において、該弁部材16の前
縁22は、機関の部分負荷時には、すべてのノズ
ル孔7のうちの一部のノズル孔のみを部分的に開
放する形状に構成されていることを特徴とする燃
料噴射弁。
1 A fuel injection valve for a reciprocating internal combustion engine, comprising a valve body 1 including a nozzle member 3 projecting into a combustion chamber 8 of a cylinder, the nozzle member 3 having a valve inside thereof cooperating with a valve seat 15. It has a needle 12 and a plurality of nozzle holes 7 distributed around the needle 12, and when the valve needle 12 leaves the valve seat 15, fuel passes through the nozzle hole 7 and enters the combustion chamber 8. A valve member 1 is adapted to periodically flow out into the nozzle hole 7, extends around the valve needle 12, is slidable in the axial direction of the valve needle 12, and controls opening and closing of the nozzle hole 7.
6, and this valve member 16 is designed to open the entire area of all nozzle holes 7 when the engine is under full load. A fuel injection valve characterized in that it is configured in such a shape that only some of the nozzle holes 7 are sometimes partially opened.
JP2462980A 1979-03-01 1980-02-28 Injection valve for internal combustion engine with reciprocating piston Granted JPS55117066A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CH203079A CH636409A5 (en) 1979-03-01 1979-03-01 Injection valve on a reciprocating piston internal combustion engine

Publications (2)

Publication Number Publication Date
JPS55117066A JPS55117066A (en) 1980-09-09
JPS6153550B2 true JPS6153550B2 (en) 1986-11-18

Family

ID=4224276

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2462980A Granted JPS55117066A (en) 1979-03-01 1980-02-28 Injection valve for internal combustion engine with reciprocating piston

Country Status (7)

Country Link
JP (1) JPS55117066A (en)
AT (1) AT367867B (en)
CH (1) CH636409A5 (en)
DE (1) DE3002129A1 (en)
DK (1) DK148007C (en)
FR (1) FR2450358B1 (en)
NL (1) NL8001150A (en)

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3236046C2 (en) * 1982-09-29 1986-03-20 Daimler-Benz Ag, 7000 Stuttgart Fuel injector for internal combustion engines
DE3311138A1 (en) * 1983-03-26 1984-10-04 L'Orange GmbH, 7000 Stuttgart FUEL INJECTION SYSTEM FOR AN INTERNAL COMBUSTION ENGINE
JPS6036772A (en) * 1983-08-10 1985-02-25 Diesel Kiki Co Ltd Fuel injection valve
DE3332920A1 (en) * 1983-09-13 1985-03-21 Klöckner-Humboldt-Deutz AG, 5000 Köln Fuel injection nozzle
JPS61286576A (en) * 1985-06-14 1986-12-17 Tech Res Assoc Highly Reliab Marine Propul Plant Fuel injection valve
JPS62130172U (en) * 1986-02-12 1987-08-17
JPS62130171U (en) * 1986-02-12 1987-08-17
DE4235948C2 (en) * 1992-10-23 1995-08-31 Mtu Friedrichshafen Gmbh Fuel injection nozzle for internal combustion engines
JPH08193560A (en) * 1994-11-15 1996-07-30 Zexel Corp Variable nozzle hole type fuel injection nozzle
DE19681434T1 (en) * 1995-06-09 1998-05-07 Zexel Corp Variable nozzle type fuel injector
AT2164U3 (en) * 1997-08-07 1999-02-25 Avl List Gmbh INJECTION NOZZLE FOR A DIRECTLY INJECTING INTERNAL COMBUSTION ENGINE
GB9903496D0 (en) * 1999-02-16 1999-04-07 Lucas Ind Plc Fuel injector

Family Cites Families (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE407830C (en) * 1925-01-06 Maschf Augsburg Nuernberg Ag Method and device for introducing liquid fuel into internal combustion engines
DE102198C (en) * 1899-10-05
US1856089A (en) * 1930-04-11 1932-05-03 Brown James Henry Liquid fuel injection valve for diesel and like engines
DE701456C (en) * 1937-07-29 1941-01-16 Maschf Augsburg Nuernberg Ag Nozzle for injecting fuel into diesel engines
FR925343A (en) * 1945-11-14 1947-09-01 Saurer Ag Adolph Needle fuel injector for combustion engines
DE1270883B (en) * 1966-10-28 1968-06-20 Bosch Gmbh Robert Fuel injector
DE2147719A1 (en) * 1971-09-24 1973-03-29 Bosch Gmbh Robert FUEL INJECTION VALVE
DD102198A1 (en) * 1973-02-02 1973-12-05
DE2451462A1 (en) * 1974-10-30 1976-05-06 Maschf Augsburg Nuernberg Ag INJECTION VALVE FOR RECEPTACLE COMBUSTION MACHINERY
JPS5158216U (en) * 1974-10-31 1976-05-07
DE2710138A1 (en) * 1977-03-09 1978-09-14 Maschf Augsburg Nuernberg Ag MULTI-HOLE INJECTION NOZZLE
DE2711391A1 (en) * 1977-03-16 1978-09-21 Bosch Gmbh Robert FUEL INJECTOR
DE2726296A1 (en) * 1977-06-10 1978-12-21 Bosch Gmbh Robert FUEL INJECTOR
CH622588A5 (en) * 1977-09-01 1981-04-15 Sulzer Ag

Also Published As

Publication number Publication date
ATA107580A (en) 1981-12-15
FR2450358A1 (en) 1980-09-26
AT367867B (en) 1982-08-10
JPS55117066A (en) 1980-09-09
DE3002129A1 (en) 1980-09-04
CH636409A5 (en) 1983-05-31
DK148007C (en) 1985-07-15
DK76480A (en) 1980-09-02
FR2450358B1 (en) 1985-12-13
NL8001150A (en) 1980-09-03
DK148007B (en) 1985-01-28

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