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JP5822254B2 - Fuel injector for internal combustion engines - Google Patents

Fuel injector for internal combustion engines Download PDF

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Publication number
JP5822254B2
JP5822254B2 JP2011039839A JP2011039839A JP5822254B2 JP 5822254 B2 JP5822254 B2 JP 5822254B2 JP 2011039839 A JP2011039839 A JP 2011039839A JP 2011039839 A JP2011039839 A JP 2011039839A JP 5822254 B2 JP5822254 B2 JP 5822254B2
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Prior art keywords
notch
notch element
longitudinal cavity
fuel injector
group
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JP2012017732A (en
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イルディリム ターハン
イルディリム ターハン
ミオッティ ピエルパオロ
ミオッティ ピエルパオロ
シュルツ ライナー
シュルツ ライナー
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Winterthur Gas and Diesel AG
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Winterthur Gas and Diesel AG
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    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M61/00—Fuel-injectors not provided for in groups F02M39/00 - F02M57/00 or F02M67/00
    • F02M61/16—Details not provided for in, or of interest apart from, the apparatus of groups F02M61/02 - F02M61/14
    • F02M61/18—Injection nozzles, e.g. having valve seats; Details of valve member seated ends, not otherwise provided for
    • F02M61/1806—Injection 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
    • F02M61/182—Discharge orifices being situated in different transversal planes with respect to valve member direction of movement
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M61/00—Fuel-injectors not provided for in groups F02M39/00 - F02M57/00 or F02M67/00
    • F02M61/04—Fuel-injectors not provided for in groups F02M39/00 - F02M57/00 or F02M67/00 having valves, e.g. having a plurality of valves in series
    • F02M61/042—The valves being provided with fuel passages
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M61/00—Fuel-injectors not provided for in groups F02M39/00 - F02M57/00 or F02M67/00
    • F02M61/04—Fuel-injectors not provided for in groups F02M39/00 - F02M57/00 or F02M67/00 having valves, e.g. having a plurality of valves in series
    • F02M61/10—Other injectors with elongated valve bodies, i.e. of needle-valve type
    • F02M61/12—Other injectors with elongated valve bodies, i.e. of needle-valve type characterised by the provision of guiding or centring means for valve bodies

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

Description

本発明は、内燃機関のための燃料噴射機に関する。本発明は、特に船舶の推進のための内燃機関等の大型の２ストローク内燃機関のための燃料噴射機に関する。
より詳細には、本発明は、請求項１の前文に記載の燃料噴射機に関する。燃料噴射機は、弁案内部の下端部に固定され複数のノズル孔を備える噴霧器と、弁案内部の弁座と協動する弁部を有するスピンドルと、スピンドルが閉鎖位置にある場合にノズル孔と連通して容積を低減すべく噴霧器の長手方向腔内に延びる切り欠き要素とを備える。 The present invention relates to a fuel injector for an internal combustion engine. The present invention relates to a fuel injector for a large two-stroke internal combustion engine such as an internal combustion engine for propulsion of a ship.
More particularly, the invention relates to a fuel injector according to the preamble of claim 1. The fuel injector includes a sprayer having a plurality of nozzle holes fixed to a lower end portion of a valve guide portion, a spindle having a valve portion that cooperates with a valve seat of the valve guide portion, and a nozzle hole when the spindle is in a closed position. And a notch element extending into the longitudinal cavity of the nebulizer to reduce the volume in communication therewith.

特許文献１は、対応する弁案内部の弁座と協動する弁部を有し、かつ軸方向に移動可能なスピンドルと、弁スピンドルの弁部の下方を噴霧器の中央部腔内に延びる切り欠き要素とを備える燃料噴射機を開示する。切り欠き要素の外壁は、ノズル孔の入口開口部を開閉するために好適である。   Patent Document 1 has a valve portion that cooperates with a valve seat of a corresponding valve guide portion and is movable in the axial direction, and a cut extending below the valve portion of the valve spindle into the central cavity of the sprayer. Disclosed is a fuel injector comprising a missing element. The outer wall of the notch element is suitable for opening and closing the inlet opening of the nozzle hole.

特許文献１に開示される解決策において、ノズル孔は一列に並べられる。即ち、ノズル孔の入口開口部は全て噴霧器の下端部から略等距離に位置される。この解決策の課題は、最大角内に位置されるノズル孔の総数は、噴霧器の側壁の強度を妥協することなく増加させることができない点にある。   In the solution disclosed in Patent Document 1, the nozzle holes are arranged in a line. That is, all the inlet openings of the nozzle holes are located at substantially equal distances from the lower end of the sprayer. The problem with this solution is that the total number of nozzle holes located within the maximum angle cannot be increased without compromising the strength of the sprayer sidewalls.

特許文献２は、請求項１の前文による燃料噴射機を開示する。噴霧器のノズル孔の入口開口部は、軸方向に離間して位置される第１の列及び第２の列に並べられ、円筒状シール部によって相互に分離される。噴霧器の長手方向腔内に延びる切り欠き要素は、下方の列の入口開口部を開閉すべく位置される第１の円筒状区域と、弁スピンドルが閉じられた場合に上方の列の入口開口部を閉じるために二次弁座と協動する第２の円筒状区域とを有する。   Patent document 2 discloses a fuel injector according to the preamble of claim 1. The inlet openings of the nozzle holes of the sprayer are arranged in a first row and a second row that are spaced apart in the axial direction and are separated from each other by a cylindrical seal portion. A notch element extending into the longitudinal cavity of the nebulizer includes a first cylindrical section positioned to open and close the lower row of inlet openings, and the upper row of inlet openings when the valve spindle is closed. And a second cylindrical section that cooperates with the secondary valve seat to close the valve.

弁スピンドルが開放される場合に、下方の列の入口開口部には、切り欠き要素の中央部ダクトを通過して流れる燃料が供給され、上方の列の入口開口部には、噴霧器の内壁及び切り欠き要素の外側表面間に形成される環状流路を流れる燃料が供給される。   When the valve spindle is opened, the lower row of inlet openings is supplied with fuel flowing through the central duct of the notch element, and the upper row of inlet openings contains the inner wall of the atomizer and Fuel is supplied that flows through an annular passage formed between the outer surfaces of the notch elements.

特許文献２に開示される解決策の課題は、スピンドルの開放位置において、切り欠き要素が完全には案内されない点にある。従って、スピンドルの閉鎖段階において、切り欠き要素が下方に移動される場合に、切り欠き要素の端部が噴霧器の壁に衝突する可能性がある。これは、噴射孔の高さ部分において切り欠き要素に作用する流体の動的圧力により生じる。この圧力は、切り欠き要素を噴射孔に押圧して移動させ、更に切り欠き要素を屈曲させ得る。   The problem of the solution disclosed in Patent Document 2 is that the notch element is not completely guided in the open position of the spindle. Thus, when the notch element is moved downwards during the spindle closing phase, the end of the notch element can collide with the sprayer wall. This is caused by the dynamic pressure of the fluid acting on the notch element at the height of the injection hole. This pressure can push the notch element against the injection hole and move it, further bending the notch element.

欧州特許出願公開第０５２９３７号明細書European Patent Application No. 052937 国際公開第２００８／０７１１８７号パンフレットInternational Publication No. 2008/071187 Pamphlet

本発明の課題は、切り欠き要素に作用する流体の動的圧力により生じる問題を解決する改良された噴射機を提供することにある。   The object of the present invention is to provide an improved injector which solves the problems caused by the dynamic pressure of the fluid acting on the notch element.

本発明において、この課題は、請求項１に記載の特徴を有する燃料噴射機によって解決される。   In the present invention, this problem is solved by a fuel injector having the features of claim 1.

本発明の第１の実施例における噴射機を軸方向に示す部分断面図。The fragmentary sectional view which shows the injector in the 1st Example of this invention to an axial direction. 第２の実施例を示す部分断面図。The fragmentary sectional view showing the 2nd example. 開放位置における第３の実施例を示す部分断面図。The fragmentary sectional view which shows the 3rd Example in an open position. 閉鎖位置における第３の実施例を示す部分断面図。The fragmentary sectional view which shows the 3rd Example in a closed position.

本発明の特徴及び効果は、添付の図面を参照して後述する非制限的例の詳細な説明により明らかとなるであろう。
図１において、参照符号１０は、ディーゼルエンジンの燃料噴射機の噴霧機の下方部分を示す。 The features and advantages of the present invention will become apparent from the following detailed description of non-limiting examples with reference to the accompanying drawings.
In FIG. 1, reference numeral 10 indicates a lower portion of a sprayer of a fuel injector of a diesel engine.

後述する詳細な説明及び特許請求の範囲において、用語「上方」、「下方」、「頂部」、「底部」等は、噴射機の使用における通常の位置を示すものである。しかしながら、噴射機１０は、上下方向の軸に対して多かれ少なかれ斜めの位置に設けられてもよい。   In the detailed description and claims that follow, the terms “upper”, “lower”, “top”, “bottom” and the like indicate normal positions in use of the injector. However, the injector 10 may be provided at a more or less oblique position with respect to the vertical axis.

噴霧器１０は、丸みを帯びた底端部１２を備えた耐食材料から形成される円筒状本体から形成される。
噴霧器１０は、その底端部にて閉じられ長手方向軸Ａを有する長手方向腔１４を有する。複数のノズル孔１６が噴霧器１０の側壁に形成される。ノズル孔１６はそれぞれ長手方向腔１４に面する内側開口部１８、及び噴霧器の外側表面に開放する出口開口部２０を有する。ノズル孔１６の入口開口部１８は、上方の群と下方の群とに分けられ、これらは長手方向Ａにおいて相互に離間して設けられる。 The sprayer 10 is formed from a cylindrical body formed from a corrosion resistant material with a rounded bottom end 12.
The nebulizer 10 has a longitudinal cavity 14 which is closed at its bottom end and has a longitudinal axis A. A plurality of nozzle holes 16 are formed in the side wall of the sprayer 10. The nozzle holes 16 each have an inner opening 18 facing the longitudinal cavity 14 and an outlet opening 20 opening to the outer surface of the sprayer. The inlet opening 18 of the nozzle hole 16 is divided into an upper group and a lower group, which are provided apart from each other in the longitudinal direction A.

噴射機は、噴霧器１０の長手方向腔１４内に延びる切り欠き要素２２を有するスピンドル（図１に図示しない）を備える。
切り欠き要素２２は、開放位置及び閉鎖位置間を長手方向腔１４に対して長手方向Ａに移動可能である。 The injector includes a spindle (not shown in FIG. 1) having a notch element 22 extending into the longitudinal cavity 14 of the nebulizer 10.
The notch element 22 is movable in the longitudinal direction A relative to the longitudinal cavity 14 between an open position and a closed position.

長手方向腔１４は、上方円筒状シール部２４及び下方円筒状シール部２６を有する。上方シール部２４は、上方の群の内側開口部１８の上方に位置され、下方シール部２６は、下方の群の内側開口部１８の下方に位置される。   The longitudinal cavity 14 has an upper cylindrical seal portion 24 and a lower cylindrical seal portion 26. The upper seal portion 24 is positioned above the inner opening 18 of the upper group, and the lower seal portion 26 is positioned below the inner opening 18 of the lower group.

切り欠き要素２２は、上方円筒状シール部２８及び下方円筒状シール部３０を有する。閉鎖位置において、上方円筒状シール部２８及び下方円筒状シール部３０はそれぞれ長手方向腔１４の上方シール部２４及び下方シール部２６に対して気密に接触し、上方切り欠き区域３２及び下方切り欠き区域３４を形成する。   The notch element 22 has an upper cylindrical seal portion 28 and a lower cylindrical seal portion 30. In the closed position, the upper cylindrical seal portion 28 and the lower cylindrical seal portion 30 are in airtight contact with the upper seal portion 24 and the lower seal portion 26 of the longitudinal cavity 14, respectively, and the upper cutout area 32 and the lower cutout portion. Region 34 is formed.

図１に示す開放位置において、切り欠き要素２２の上方シール部２８及び下方シール部３０は、長手方向腔１４の上方シール部２４及び下方シール部２６に対して軸方向に偏移する。この位置において、上方切り欠き区域３２及び下方切り欠き区域３４は、開放される。切り欠き要素２２の下方シール部３０は、内側開口部１８の上方の群及び下方の群の間に位置される。   In the open position shown in FIG. 1, the upper seal portion 28 and the lower seal portion 30 of the notch element 22 are axially displaced with respect to the upper seal portion 24 and the lower seal portion 26 of the longitudinal cavity 14. In this position, the upper notch area 32 and the lower notch area 34 are opened. The lower seal portion 30 of the notch element 22 is located between the upper group and the lower group of the inner opening 18.

切り欠き要素は、切り欠き要素２２の閉鎖位置においてて上方切り欠き区域３２の上方及び下方切り欠き区域３４の下方の両者にて長手方向腔１４と連通する中央部ダクト３６を有する。   The notch element has a central duct 36 that communicates with the longitudinal cavity 14 in the closed position of the notch element 22 both above the upper notch area 32 and below the lower notch area 34.

切り欠き要素２２は、切り欠き要素２２の上方シール部２８の下方を延びる補助的な案内区域３８を備える。
補助的な案内区域３８は、周方向において相互に離間して設けられ且つ上方シール部２４に対して摺動自在に接触する外側円筒状表面を有する複数の案内リブ４０を含む。チャネル４２が、隣接する案内リブ４０間に形成される。チャネル４２により、燃料は、切り欠き要素２２の開放位置において上方切り欠き区域３２を通過して流れることができる。 The notch element 22 includes an auxiliary guide area 38 that extends below the upper seal 28 of the notch element 22.
The auxiliary guide section 38 includes a plurality of guide ribs 40 that are spaced apart from one another in the circumferential direction and have an outer cylindrical surface that slidably contacts the upper seal 24. A channel 42 is formed between adjacent guide ribs 40. The channel 42 allows fuel to flow past the upper notch area 32 in the open position of the notch element 22.

切り欠き要素の開放位置において、圧力下の燃料は、長手方向腔１４の内側表面及び切り欠き要素２２の外側表面の間に形成される環状流路に流れる。第１の燃料の流れは、チャネル４２を通過して流れ、上方の群の入口開口部１８に至る。第２の燃料の流れは、切り欠き要素２２の軸方向ダクト３６内に流れ、下方の群の入口開口部１８に至る。開放位置において、案内リブ４０は、噴霧器１０の上方シール部２４に接触する。案内リブ４０は、切り欠き要素２２に作用する流体の動的圧力による切り欠き要素と噴霧器の内壁との間における衝突の危険性を取り払う。切り欠き要素２２と長手方向腔１４との間の空隙は最小限に保持されている。これにより燃料の漏れを低減する。   In the open position of the notch element, fuel under pressure flows in an annular flow path formed between the inner surface of the longitudinal cavity 14 and the outer surface of the notch element 22. The first fuel flow flows through the channel 42 to the upper group of inlet openings 18. The second fuel flow flows into the axial duct 36 of the notch element 22 and reaches the lower group of inlet openings 18. In the open position, the guide rib 40 contacts the upper seal portion 24 of the sprayer 10. The guide rib 40 eliminates the risk of a collision between the notch element and the inner wall of the sprayer due to the dynamic pressure of the fluid acting on the notch element 22. The gap between the notch element 22 and the longitudinal cavity 14 is kept to a minimum. This reduces fuel leakage.

図２は、別例において切り欠き要素２２の下方シール部３０が切り欠き要素２２の閉鎖位置及び開放位置の両者において、下方の群の入口開口部の下方を延びることを示す。
図２に示す開放位置において、燃料全体は、上方及び下方の群の内側開口部１８に向かって上方切り欠き区域３２を通して下方に流れる。全ての噴射孔１６には、切り欠き要素２２の外側を流れる燃料が供給される。従って、流れ方向における大きな流れの制約や変化が不要であるため、流体の圧力の低下は、制限される。 FIG. 2 shows that in another example the lower seal 30 of the notch element 22 extends below the lower group of inlet openings in both the closed and open positions of the notch element 22.
In the open position shown in FIG. 2, the entire fuel flows downward through the upper cutout area 32 toward the upper and lower groups of inner openings 18. All the injection holes 16 are supplied with fuel flowing outside the notch element 22. Accordingly, the reduction of fluid pressure is limited because large flow constraints and changes in the flow direction are not required.

噴射孔に供給される燃料の流れを妨害することを回避すべく、切り欠き要素は下方シール部３０に、且つ下方の群の入口開口部１８の下方に案内される。
図２に示される実施例において切り欠き要素２２の製造は、切り欠き要素２２の比較的大きな穴のドリリングによる形成が回避され、且つ切り欠き要素の端部面に作用する圧力の平衡を保持すべく小さな穴の形成が必要とされるのみであるため、単純化される。切り欠き要素２２の径の３５％より大きな穴は形成されない。従って、切り欠き要素２２は、公知技術の設計と比較してより小さな応力にさらされるため、要素の信頼性が向上する。更に、この設計により袋の容量が大幅に低減する。 In order to avoid obstructing the flow of fuel supplied to the injection holes, the notch element is guided to the lower seal 30 and below the lower group of inlet openings 18.
In the embodiment shown in FIG. 2, the manufacture of the notch element 22 avoids the formation of a relatively large hole in the notch element 22 and maintains a balance of pressures acting on the end face of the notch element. Since it is only necessary to form as small a hole as possible, it is simplified. Holes larger than 35% of the diameter of the notch element 22 are not formed. Thus, the notch element 22 is exposed to less stress compared to prior art designs, thus improving element reliability. In addition, this design greatly reduces bag capacity.

図３及び４は、ノズル壁及び弁体の間に摩擦を生じさせる、流体の動的な流れによって生じる径方向の応力を伴わない、略ゼロの袋容量を備えた噴射口を閉鎖するための更なる解決策を示す。   FIGS. 3 and 4 are for closing a jet with a substantially zero bag volume without radial stress caused by the dynamic flow of fluid causing friction between the nozzle wall and the valve body. Indicates a further solution.

切り欠き要素は、パイプとして構成され、球等の球状要素４４は長手方向腔１４の底端部に位置される。閉鎖位置において、切り欠き要素２２の底端部は、球状要素４４に隣接し、球状要素４４のシール面における主要な流れを閉鎖する。   The notch element is configured as a pipe, and a spherical element 44 such as a sphere is located at the bottom end of the longitudinal cavity 14. In the closed position, the bottom end of the notch element 22 is adjacent to the spherical element 44 and closes the main flow at the sealing surface of the spherical element 44.

更に長手方向腔１４及び切り欠き要素２２間の空隙を通した円筒体内への漏れを防止すべく、弾性ディスク４６が長手方向腔１４の上端部に設けられる。スピンドル４８には、切り欠き要素２２の上方に円錐状シール部５０が設けられる。円錐状シール部５０及びディスク４６の間のシール領域は、切り欠き要素２２の底端部が球状要素４４に接触すると同時に閉じられる。   In addition, an elastic disk 46 is provided at the upper end of the longitudinal cavity 14 to prevent leakage into the cylinder through the gap between the longitudinal cavity 14 and the notch element 22. The spindle 48 is provided with a conical seal 50 above the notch element 22. The sealing area between the conical seal 50 and the disk 46 is closed as soon as the bottom end of the notch element 22 contacts the spherical element 44.

図示しないが、図２、３、及び４に示す実施例において、図１に示すものと同じ案内部３８が設けられる。   Although not shown, in the embodiment shown in FIGS. 2, 3, and 4, the same guide 38 as shown in FIG. 1 is provided.

Claims (6)

長手方向腔（１４）、及び同長手方向腔（１４）に面する入口開口部（１８）を有する複数のノズル孔（１６）を有する噴霧器（１０）と、該入口開口部（１８）は上方の群及び下方の群に分けられ、長手方向（Ａ）において相互に離間して設けられることと、
該噴霧器（１０）の長手方向腔（１４）内に延びる切り欠き要素（２２）とを備え、同切り欠き要素（２２）は、長手方向腔（１４）に対して長手方向（Ａ）において開放位置及び閉鎖位置間を移動自在であることと、
該長手方向腔（１４）及び切り欠き要素（２２）はそれぞれ、切り欠き要素（２２）の閉鎖位置において相互に協動し上方の群の入口開口部（１８）の上方を延びる上方切り欠き区域（３２）及び下方の群の入口開口部（１８）の下方を延びる下方切り欠き区域（３４）を形成する上方シール部（２４，２８）及び下方シール部（２６，３０）を有する内燃機関のための燃料噴射機であって、
該切り欠き要素（２２）には、長手方向腔（１４）の上方シール部（２４）に案内接触し切り欠き要素（２２）の開放位置において燃料を流れさせる補助的な案内区域（３８）が設けられ、
前記切り欠き要素（２２）の下部シール部（３０）は、切り欠き要素（２２）の開放位置において、上方の群及び下方の群の内部開口部（１８）の間を延びることを特徴とする燃料噴射機。 A nebulizer (10) having a longitudinal cavity (14) and a plurality of nozzle holes (16) having an inlet opening (18) facing the longitudinal cavity (14), the inlet opening (18) being upward Divided into a group and a lower group, and spaced apart from each other in the longitudinal direction (A),
A notch element (22) extending into the longitudinal cavity (14) of the nebulizer (10), the notch element (22) being open in the longitudinal direction (A) relative to the longitudinal cavity (14). Movable between position and closed position;
The longitudinal cavity (14) and the notch element (22) each cooperate with each other in the closed position of the notch element (22) and extend above the upper group of inlet openings (18). (32) and an internal combustion engine having an upper seal portion (24, 28) and a lower seal portion (26, 30) forming a lower notch area (34) extending below an inlet opening (18) of the lower group. A fuel injector for
The notch element (22) has an auxiliary guide zone (38) for guiding and contacting the upper seal (24) of the longitudinal cavity (14) and allowing fuel to flow in the open position of the notch element (22). Provided ,
The notch lower sealing portion of the element (22) (30) is in the open position of the notch element (22), and wherein Rukoto extending between the inner opening of the upper group and a group of lower (18) Fuel injectors. 前記補助的な案内区域（３８）は、切り欠き要素（２２）の開放位置において長手方向腔（１４）の上方円筒状シール部（２４）に摺動して接触する円筒状外側表面を有する複数の案内リブ（４０）を備えることを特徴とする請求項１に記載の燃料噴射機。   The auxiliary guide zone (38) has a plurality of cylindrical outer surfaces that slide into and contact the upper cylindrical seal (24) of the longitudinal cavity (14) in the open position of the notch element (22). The fuel injector according to claim 1, further comprising a guide rib (40). 前記案内リブ（４０）は、燃料の流路のためにチャネル（４２）によって相互に周方向に離間して設けられることを特徴とする請求項２に記載の燃料噴射機。 The fuel injector according to claim 2, wherein the guide ribs (40) are spaced apart from each other in the circumferential direction by a channel (42) for fuel flow . 前記切り欠き要素（２２）の下部シール部（３０）は、切り欠き要素（２２）の開放位置において、下方の群の内部開口部（１８）の下方を延びることを特徴とする請求項１に記載の燃料噴射機。   2. The lower seal part (30) of the notch element (22) extends below the inner opening (18) of the lower group at the open position of the notch element (22). The fuel injector as described. 前記切り欠き要素（２２）は、閉鎖位置において球状要素（４４）と機密に隣接する底端部を有することを特徴とする請求項１に記載の燃料噴射機。   The fuel injector according to claim 1, characterized in that the notch element (22) has a bottom end secretly adjacent to the spherical element (44) in the closed position. 変形可能なディスク（４６）が長手方向腔（１４）の上端部に設けられることと、円錐状シール部（５０）が切り欠き要素（２２）の上端部に設けられることと、該円錐状シール部（５０）は、切り欠き要素（２２）の閉鎖位置において変形可能なディスク（４６）に隣接することとを特徴とする請求項５に記載の燃料噴射機。 A deformable disc (46) is provided at the upper end of the longitudinal cavity (14), a conical seal (50) is provided at the upper end of the notch element (22), and the conical seal; 6. Fuel injector according to claim 5 , characterized in that the part (50) is adjacent to the deformable disc (46) in the closed position of the notch element (22).
JP2011039839A 2010-07-07 2011-02-25 Fuel injector for internal combustion engines Expired - Fee Related JP5822254B2 (en)

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