JP2014001660A - Fuel injection valve of internal combustion engine - Google Patents
Fuel injection valve of internal combustion engine Download PDFInfo
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- JP2014001660A JP2014001660A JP2012136647A JP2012136647A JP2014001660A JP 2014001660 A JP2014001660 A JP 2014001660A JP 2012136647 A JP2012136647 A JP 2012136647A JP 2012136647 A JP2012136647 A JP 2012136647A JP 2014001660 A JP2014001660 A JP 2014001660A
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- region
- central axis
- fuel injection
- diffusion region
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- 239000000446 fuel Substances 0.000 title claims abstract description 174
- 238000002347 injection Methods 0.000 title claims abstract description 158
- 239000007924 injection Substances 0.000 title claims abstract description 158
- 238000002485 combustion reaction Methods 0.000 title claims abstract description 50
- 238000009792 diffusion process Methods 0.000 claims abstract description 125
- 239000007921 spray Substances 0.000 claims abstract description 58
- 238000000034 method Methods 0.000 abstract description 10
- 239000000243 solution Substances 0.000 abstract 1
- 238000005507 spraying Methods 0.000 abstract 1
- 230000004048 modification Effects 0.000 description 16
- 238000012986 modification Methods 0.000 description 16
- 230000035515 penetration Effects 0.000 description 14
- 239000000203 mixture Substances 0.000 description 8
- 230000008859 change Effects 0.000 description 6
- 230000008569 process Effects 0.000 description 4
- 238000000889 atomisation Methods 0.000 description 3
- 230000002452 interceptive effect Effects 0.000 description 3
- 230000000087 stabilizing effect Effects 0.000 description 3
- 230000009471 action Effects 0.000 description 1
- 239000000567 combustion gas Substances 0.000 description 1
- 230000008878 coupling Effects 0.000 description 1
- 238000010168 coupling process Methods 0.000 description 1
- 238000005859 coupling reaction Methods 0.000 description 1
- 230000007423 decrease Effects 0.000 description 1
- 230000006866 deterioration Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 239000007789 gas Substances 0.000 description 1
- 230000002093 peripheral effect Effects 0.000 description 1
- 238000000746 purification Methods 0.000 description 1
- 230000006641 stabilisation Effects 0.000 description 1
- 238000011105 stabilization Methods 0.000 description 1
Classifications
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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
- F02M61/1826—Discharge orifices having different sizes
-
- 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
- F02M61/1833—Discharge orifices having changing cross sections, e.g. being divergent
-
- 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
- F02M61/184—Discharge orifices having non circular sections
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
Description
本発明は、内燃機関の燃料噴射弁に関する。 The present invention relates to a fuel injection valve for an internal combustion engine.
一般的なガソリンエンジン用の燃料噴射弁は、複数の噴孔を有する。燃焼室内に噴射される噴霧が所定の期間内に到達する距離(ペネトレーション)は、個々の噴孔からの噴霧の運動量に依存しており、同一径の噴孔から噴射される噴霧の運動量は同じとなるため、個々の噴霧のペネトレーションは同じである。一般に、噴孔径が大きくなると燃料噴霧の流量が増して運動量が増すので、ペネトレーションは増加すると考えられる。噴孔長が長くなると燃料の直進性がよくなり、噴孔から出た後に巻き込む空気量が減って空気で減速しにくくなり、ペネトレーションは増加すると考えられる。従って、燃焼室内に噴射される噴霧の状態を最適化するために、1つの燃料噴射弁に形成される複数の噴孔の噴孔径は同一とは限らない。 A fuel injection valve for a general gasoline engine has a plurality of injection holes. The distance (penetration) that the spray injected into the combustion chamber reaches within a predetermined period depends on the momentum of the spray from each nozzle hole, and the momentum of the spray injected from the nozzle hole of the same diameter is the same Therefore, the penetration of each spray is the same. In general, it is considered that the penetration increases because the flow rate of the fuel spray increases and the momentum increases as the nozzle hole diameter increases. As the nozzle hole length increases, the straightness of the fuel improves, and the amount of air entrained after exiting the nozzle hole decreases, making it difficult to decelerate with air, and penetration is considered to increase. Therefore, in order to optimize the state of the spray injected into the combustion chamber, the diameters of the plurality of nozzle holes formed in one fuel injection valve are not necessarily the same.
噴霧との干渉を回避する噴孔の拡散領域の形状と配置方法に関する公報開示の従来技術として、例えば、バルブ・クローズド・オリフィス(VCO)型燃料噴射弁において、複数の噴孔からの噴射量のばらつきを防止すると共に、各噴孔により形成される噴霧の均一性を向上し、排出ガス性能の改善、運転騒音の低減を図ることを目的とした、VCO型噴射弁の針弁の截頭円錐状をなすシート部の小径端部外周面に面取りを施し、針弁のフルリフト時に、上記面取り部が、ノズルボディのシート面における噴孔の開口端に対向する構成とする。また針弁内に、上記シート部の小径端部に開口する針弁内通路を設け、同針弁内通路は、ノズルボディ内の燃料溜めに針弁リフト時に連通することを開示する技術がある(特許文献1)。 As a prior art disclosed in the gazette regarding the shape and arrangement method of the diffusion region of the nozzle hole that avoids the interference with the spray, for example, in a valve closed orifice (VCO) type fuel injection valve, the injection amount of a plurality of nozzle holes VCO type injection valve needle conical cone with the aim of preventing variation and improving the uniformity of spray formed by each nozzle hole, improving exhaust gas performance and reducing operating noise The outer peripheral surface of the small-diameter end portion of the sheet portion having a shape is chamfered so that the chamfered portion faces the opening end of the nozzle hole in the seat surface of the nozzle body when the needle valve is fully lifted. Further, there is a technique for disclosing a needle valve passage that opens at a small-diameter end of the seat portion in the needle valve, and that the needle valve passage communicates with a fuel reservoir in the nozzle body when the needle valve is lifted. (Patent Document 1).
また、ノズルプレートのノズル孔を等径孔部と拡径孔部とから構成することにより、燃料の微粒化と噴射方向の安定化を図ることを課題として、燃料噴射弁の弁ケーシング内には、弁座部材の先端側に位置してノズルプレート15を取付け、その各ノズル孔16,17を、等しい孔径dをもって直線状に延設された等径孔部16A,17Aと、テーパ状に拡径して形成された拡径孔部16B,17Bとによって構成する。これにより、燃料の噴射時には、燃料の噴射流量と噴射方向とを等径孔部16A,17Aによって定め、その噴流を拡径孔部16B,17Bによって一定の領域へと拡げる。これにより、噴射燃料の方向性を安定させつつ、燃料が微粒化した状態を保持することを開示する技術がある(特許文献2)。 Further, the nozzle hole of the nozzle plate is composed of an equal-diameter hole portion and an enlarged-diameter hole portion, so that the atomization of the fuel and the stabilization of the injection direction can be achieved. The nozzle plate 15 is mounted on the front end side of the valve seat member, and the nozzle holes 16 and 17 are expanded in a taper shape with equal diameter holes 16A and 17A extending linearly with an equal hole diameter d. It is comprised by the enlarged diameter hole parts 16B and 17B formed by diameter. Thereby, at the time of fuel injection, the fuel injection flow rate and the injection direction are determined by the equal diameter holes 16A and 17A, and the jet flow is expanded to a certain region by the diameter expansion holes 16B and 17B. Thus, there is a technique for disclosing that the fuel is atomized while stabilizing the directionality of the injected fuel (Patent Document 2).
更に、内燃機関の成層燃焼時の燃焼性能を改善することを課題として、ピストンキャビティの吸気側への燃料噴射量を排気側(点火プラグに近い側)より多くするなど、非対称に噴射することで、噴射された燃料は、タンブル流動の作用によりピストンに受け止められた後、燃焼室上方へ巻き上がる際に吸気側が排気側に比べて大きく混合拡散した場合でも吸気側が希薄になったり、または、排気側が過濃になったりすることがなく、吸気および排気側の濃度が等しく均質な成層混合気を形成でき、燃焼が安定し、燃費、排気浄化性能が向上することを開示した技術がある(特許文献3)。 Furthermore, with the goal of improving the combustion performance of the internal combustion engine during stratified combustion, the amount of fuel injected to the intake side of the piston cavity is increased from the exhaust side (the side closer to the spark plug), etc. The injected fuel is received by the piston by the action of tumble flow, and when it is rolled up above the combustion chamber, the intake side becomes leaner or the exhaust side becomes lean even if the intake side is mixed and diffused more than the exhaust side There is a technology that discloses that a stratified air-fuel mixture can be formed in which the concentrations on the intake and exhaust sides are equal, and the combustion is stable, fuel efficiency and exhaust purification performance are improved (patented) Reference 3).
更にまた、燃料噴射弁において、均質燃焼と成層燃焼の双方で良好な性能を発揮させる噴霧を形成することを課題として、燃料噴射弁は、燃料を噴射する噴射孔を複数形成した噴射孔群230を備えると共に、噴射孔群の上流に、弁座と、この弁座との隙間を開閉することで燃料通路の開閉を行う弁体と、この弁体を駆動する駆動手段とを備える。噴射孔群230は、孔の軸が向く角度が異なるように穿孔された複数の噴射孔211〜216を有すると共に、これらの噴射孔の組み合わせで構成される複数の噴射孔の対を有する。複数の噴射孔の対は、噴射孔の軸の為す角度が大きい第1の組み合わせ230aと、噴射孔の軸の為す角度が第1の組み合わせ230aの角度より小さい第2の組み合わせ230bとを有することを開示する技術もある(特許文献4)。 Furthermore, in order to form a spray that exhibits good performance in both homogeneous combustion and stratified combustion in the fuel injection valve, the fuel injection valve has an injection hole group 230 in which a plurality of injection holes for injecting fuel are formed. And a valve body that opens and closes the fuel passage by opening and closing a gap between the valve seat and a drive means for driving the valve body. The injection hole group 230 includes a plurality of injection holes 211 to 216 drilled so that the angles at which the axes of the holes face are different, and a plurality of injection hole pairs configured by a combination of these injection holes. The plurality of injection hole pairs have a first combination 230a having a large angle formed by the axis of the injection hole and a second combination 230b having an angle formed by the axis of the injection hole that is smaller than the angle of the first combination 230a. There is also a technique for disclosing (Patent Document 4).
ところで、一般的な直噴ガソリンエンジンでは、燃焼室内に燃料を噴射する燃料噴射弁(インジェクタ)は、シリンダの中心軸に対して傾斜してシリンダの側面に取り付けられることがある(サイドマウント方式)。また、燃料噴射弁は、先端に複数の噴孔を備えている。そして、噴孔から噴射される燃料の噴霧が燃焼室内で最適な混合気を生成するように、燃料噴射弁の各噴孔の開孔角度が決定される。例えば、燃焼室内でほぼ均質な混合気を生成する均質燃焼モードや、点火プラグ近傍に燃料噴霧を集中させて着火性を確保しつつ燃焼室全体ではより希薄な混合気を用いる成層燃焼モードである。すなわち、様々な燃焼状態に対応して、各噴孔の開孔角度は、燃料噴射弁の中心軸に対して必ずしも対称ではない。 By the way, in a general direct-injection gasoline engine, a fuel injection valve (injector) that injects fuel into the combustion chamber may be attached to the side surface of the cylinder inclined with respect to the center axis of the cylinder (side mount system). . The fuel injection valve has a plurality of injection holes at the tip. Then, the opening angle of each injection hole of the fuel injection valve is determined so that the fuel spray injected from the injection hole generates an optimal air-fuel mixture in the combustion chamber. For example, a homogeneous combustion mode that generates a substantially homogeneous air-fuel mixture in the combustion chamber, or a stratified combustion mode that uses a leaner air-fuel mixture in the entire combustion chamber while concentrating fuel spray in the vicinity of the spark plug to ensure ignitability. . That is, corresponding to various combustion states, the opening angle of each injection hole is not necessarily symmetrical with respect to the central axis of the fuel injection valve.
図面を用いて、以下に説明する。図1は、燃料噴射弁10を搭載した吸気2弁式のガソリンエンジン1であって、吸気工程中に燃料を噴射した場合のエンジン要部の一例を示す縦断面図である。 This will be described below with reference to the drawings. FIG. 1 is a longitudinal sectional view showing an example of a main part of an engine with an intake two-valve gasoline engine 1 equipped with a fuel injection valve 10 when fuel is injected during an intake process.
図1は、サイドマウント方式の燃料噴射弁10を採用した吸気2弁式のガソリンエンジン1の一例を示し、シリンダヘッド12の吸気マニホルド14側には吸気弁16が、中央部には点火プラグ18が、吸気弁16とは反対側には排気弁20が、それぞれ設けられている。吸気弁16及び排気弁20は、燃焼室22内に延在して設けられている。 FIG. 1 shows an example of a two-valve type gasoline engine 1 that employs a side-mount type fuel injection valve 10. An intake valve 16 is provided on the side of the intake manifold 14 of the cylinder head 12, and an ignition plug 18 is provided at the center. However, an exhaust valve 20 is provided on the side opposite to the intake valve 16. The intake valve 16 and the exhaust valve 20 are provided so as to extend into the combustion chamber 22.
ガソリンエンジン1のシリンダ24内に往復運動可能に設けられたピストン26は、クランクシャフト(不図示)の回転に応じてシリンダ24内を上下動する。シリンダ24の上部にはシリンダヘッド12が取り付けられており、シリンダ24と共に密閉空間(燃焼室22)を形成する。シリンダヘッド12には、スロットルバルブ(不図示)を内蔵した吸入空気量制御装置28を介して外部空気30を燃焼室22内に導く吸気マニホルド14と、燃焼室22内で燃焼した燃焼ガス32を排気装置(不図示)へ導く排気マニホルド34とが形成されている。 The piston 26 provided in the cylinder 24 of the gasoline engine 1 so as to be able to reciprocate moves up and down in the cylinder 24 according to the rotation of a crankshaft (not shown). A cylinder head 12 is attached to the upper part of the cylinder 24, and forms a sealed space (combustion chamber 22) together with the cylinder 24. In the cylinder head 12, an intake manifold 14 that guides external air 30 into the combustion chamber 22 via an intake air amount control device 28 that includes a throttle valve (not shown), and combustion gas 32 burned in the combustion chamber 22. An exhaust manifold 34 leading to an exhaust device (not shown) is formed.
燃料噴射弁10は、シリンダヘッド12の吸気マニホルド14の結合部付近に取り付けられており、図1の例では、燃料噴射弁10の軸線が燃焼室22内でやや下向きとなるように設定されている。 The fuel injection valve 10 is attached in the vicinity of the coupling portion of the intake manifold 14 of the cylinder head 12. In the example of FIG. 1, the axis of the fuel injection valve 10 is set to be slightly downward in the combustion chamber 22. Yes.
かかる構成を有するガソリンエンジン1において、燃料噴射弁10から燃焼室22内に燃料を噴射した場合の燃焼室22内の混合気の生成を説明する。図2は、図1に示すガソリンエンジン1で、吸気工程中に燃料を噴射した場合の燃焼室22内の混合気の噴射状態を示す斜視模式図である。 In the gasoline engine 1 having such a configuration, generation of an air-fuel mixture in the combustion chamber 22 when fuel is injected from the fuel injection valve 10 into the combustion chamber 22 will be described. FIG. 2 is a schematic perspective view showing an injection state of the air-fuel mixture in the combustion chamber 22 when fuel is injected during the intake process in the gasoline engine 1 shown in FIG.
一般的な燃料噴射弁10は、先端(図2における噴射点30)に備えられた複数の噴孔(図2では不図示)が同一径を有する場合、個々の噴孔から出る燃料噴霧32の運動量は同じである。複数の噴孔から燃焼室22内の各領域に噴射される噴霧32が所定の期間内に到達する距離(ペネトレーション)は、噴孔を出た後に燃焼室22内の空気との接触による減速の影響を受ける。一般に、噴孔の噴孔径が大きくなると噴霧32の流量が増して運動量が増すので、ペネトレーションは増加すると考えられる。噴孔の噴孔長が長くなると燃料の直進性がよくなり、噴孔から出た後に巻き込む空気量が減って空気で減速しにくくなり、ペネトレーションは増加すると考えられる。 When a plurality of nozzle holes (not shown in FIG. 2) provided at the tip (injection point 30 in FIG. 2) have the same diameter, a general fuel injection valve 10 has a fuel spray 32 that exits from each nozzle hole. The momentum is the same. The distance (penetration) that the spray 32 injected from each of the plurality of nozzle holes into each region in the combustion chamber 22 arrives within a predetermined period of time is a deceleration caused by contact with the air in the combustion chamber 22 after leaving the nozzle holes. to be influenced. Generally, if the nozzle hole diameter increases, the flow rate of the spray 32 increases and the momentum increases, so that the penetration is considered to increase. If the nozzle hole length of the nozzle hole is increased, the straightness of the fuel is improved, the amount of air drawn after coming out of the nozzle hole is reduced and it is difficult to decelerate with air, and the penetration is considered to increase.
様々な燃焼状態に対応して燃焼室22内において最適な混合気を生成するために、燃料噴射弁(図2では不図示)の先端には複数の噴孔が設けられており、噴霧32が燃焼室22内の各領域に分散して噴射されるように、各噴孔の軸の角度が最適化される。その結果、燃料噴射弁の中心軸(図2では不図示)に対して平行でない噴孔もあり、また、各噴孔の軸が、燃料噴射弁の中心軸に対して必ずしも対称ではない。 In order to generate an optimal air-fuel mixture in the combustion chamber 22 corresponding to various combustion states, a plurality of injection holes are provided at the tip of the fuel injection valve (not shown in FIG. 2), and the spray 32 is The angle of the axis of each nozzle hole is optimized so as to be dispersed and injected into each region in the combustion chamber 22. As a result, some nozzle holes are not parallel to the central axis (not shown in FIG. 2) of the fuel injection valve, and the axis of each injection hole is not necessarily symmetrical with respect to the central axis of the fuel injection valve.
次に、上記したガソリンエンジン1の燃料噴射弁10を説明する。図3は、図1に示すガソリンエンジン1に使用される燃料噴射弁10の縦断面図である。 Next, the fuel injection valve 10 of the gasoline engine 1 will be described. FIG. 3 is a longitudinal sectional view of the fuel injection valve 10 used in the gasoline engine 1 shown in FIG.
燃料噴射弁10は、通常時閉(NC)式の電磁弁であり、通常時はスプリング40によって付勢された弁体42のボール形状の先端部44と弁座プレート46の弁座部48(図4)とが密着して、燃料供給口50から供給される燃料が噴孔52(図4)から漏れ出ないようになっている。通電されると、弁体42がアンカ1054と共にコア1056の側に変位し、弁体42と弁座プレート46の弁座部48(図4)との間に隙間を生じる。燃料は、燃料供給口50から供給され、弁体42の横の空間を通り、流入溝64(図5)を通って、弁座プレート46に穿孔された複数の噴孔52(図4)から燃料噴霧として噴射される。 The fuel injection valve 10 is a normally closed (NC) type electromagnetic valve, and normally the ball-shaped tip 44 of the valve element 42 urged by the spring 40 and the valve seat 48 ( 4) is in close contact with each other so that fuel supplied from the fuel supply port 50 does not leak from the nozzle hole 52 (FIG. 4). When energized, the valve body 42 is displaced together with the anchor 1054 toward the core 1056, and a gap is generated between the valve body 42 and the valve seat portion 48 (FIG. 4) of the valve seat plate 46. The fuel is supplied from the fuel supply port 50, passes through the space next to the valve body 42, passes through the inflow groove 64 (FIG. 5), and from the plurality of injection holes 52 (FIG. 4) drilled in the valve seat plate 46. It is injected as a fuel spray.
かかる構成を有する燃料噴射弁10の燃料噴射部に関して、図4乃至図6を参照しつつ説明する。図4は、図3における弁座プレート46の近傍を拡大した縦断面図であり、図5は、図3の線V−Vにおける横断面図であり、図6は、図3における弁座プレート46の最小厚さを説明するための縦断面図である。弁座プレート46の内腔は、弁体42(図3)のボール形状の先端部44に適合するドーム形状を有している。そして、弁座プレート46の内側面には、先端部44が接する部分に弁座部48が形成され、先端部44と弁座部48とが接するときシールを形成する。また、弁座プレート46の内側先端には、サック部60が形成されている。サック部60は、先端部44が弁座部48から離れており、燃料噴射弁10(図3)が燃料を噴射する際に、噴射される噴霧を安定化させる機能を有する。 The fuel injection part of the fuel injection valve 10 having such a configuration will be described with reference to FIGS. 4 is an enlarged longitudinal sectional view of the vicinity of the valve seat plate 46 in FIG. 3, FIG. 5 is a transverse sectional view taken along line VV in FIG. 3, and FIG. 6 is a valve seat plate in FIG. It is a longitudinal cross-sectional view for demonstrating the minimum thickness of 46. FIG. The lumen of the valve seat plate 46 has a dome shape that fits the ball-shaped tip 44 of the valve body 42 (FIG. 3). A valve seat portion 48 is formed on the inner surface of the valve seat plate 46 at a portion where the tip portion 44 contacts, and a seal is formed when the tip portion 44 and the valve seat portion 48 contact each other. Further, a sack portion 60 is formed at the inner front end of the valve seat plate 46. The sack portion 60 has a function of stabilizing the spray to be injected when the fuel injection valve 10 (FIG. 3) injects fuel because the tip end portion 44 is separated from the valve seat portion 48.
燃料は、燃料噴射弁10(図3)内部に設けられた隙間及び流入溝64(図5)を通過して弁座プレート46の弁座部48に至る。弁体42の先端部44と弁座プレート46の弁座部48との間の狭窄部を通過した燃料は、燃料噴射弁10(図3)の中心軸62の方向に向かい、弁座プレート46に穿孔された複数の噴孔52に至り、噴孔52を通過して燃焼室22(図2)内に噴射される。各噴孔52は、軸の角度が異なるように穿孔されている。 The fuel passes through a clearance and an inflow groove 64 (FIG. 5) provided inside the fuel injection valve 10 (FIG. 3) and reaches the valve seat portion 48 of the valve seat plate 46. The fuel that has passed through the narrowed portion between the distal end portion 44 of the valve body 42 and the valve seat portion 48 of the valve seat plate 46 is directed toward the central axis 62 of the fuel injection valve 10 (FIG. 3), and the valve seat plate 46. To the plurality of nozzle holes 52 perforated through the nozzle hole 52 and injected through the nozzle holes 52 into the combustion chamber 22 (FIG. 2). Each nozzle hole 52 is drilled so that the angle of the shaft is different.
燃料噴射弁10の噴孔52は、図4に示されるように、流入側に形成された小径のガイド領域54と、噴射側に形成されガイド領域54より大径の座繰りで形成される拡散領域56とで構成される。拡散領域56の底面は、例えば、ガイド領域54の中心軸58に対して直角な段部が形成されている。ガイド領域54から拡散領域56を介して燃焼室22(図2)に流出する燃料噴流は、図2に示されるように、燃料噴霧となって拡散する。 As shown in FIG. 4, the injection hole 52 of the fuel injection valve 10 has a small-diameter guide region 54 formed on the inflow side and a diffusion formed on the injection side and having a larger diameter than the guide region 54. An area 56 is formed. On the bottom surface of the diffusion region 56, for example, a step portion perpendicular to the central axis 58 of the guide region 54 is formed. The fuel jet flowing out from the guide region 54 to the combustion chamber 22 (FIG. 2) through the diffusion region 56 is diffused as fuel spray as shown in FIG.
弁体42の先端部44と弁座プレート46の弁座部48との間の狭窄部を通過して噴孔52に至る燃料は、外側方向から燃料噴射弁10(図3)の中心軸62方向に向かう径方向の流れとなるので、噴孔52のガイド領域54内では、燃料噴射弁10(図3)の中心軸62から遠い部分で流れが壁面から剥離し、その結果、ガイド領域54内で流れ場の乱れが生じる。例えば、図4に符号Aで示した箇所で乱れが生じる。そして、その流れ場の乱れの影響を受けて、ガイド領域54から拡散領域56へと流出した燃料は、ガイド領域54の中心軸58から均等に円錐状に拡散するのではなく、燃料噴射弁10(図3)の中心軸62から遠い側が、より大きな噴霧角を有する拡散が観察される。 The fuel that passes through the narrowed portion between the tip end portion 44 of the valve body 42 and the valve seat portion 48 of the valve seat plate 46 and reaches the injection hole 52 from the outside direction is the central axis 62 of the fuel injection valve 10 (FIG. 3). Therefore, in the guide region 54 of the injection hole 52, the flow is separated from the wall surface at a portion far from the central axis 62 of the fuel injection valve 10 (FIG. 3), and as a result, the guide region 54. Disturbance of the flow field occurs inside. For example, the disturbance occurs at the location indicated by the symbol A in FIG. The fuel that has flowed out of the guide region 54 into the diffusion region 56 due to the influence of the disturbance of the flow field does not diffuse evenly from the central axis 58 of the guide region 54 in a conical shape, but instead of the fuel injection valve 10. Diffusion with a larger spray angle is observed on the side farther from the central axis 62 (FIG. 3).
かかる燃料噴霧は、燃料噴射弁10(図3)の中心軸62から遠い側で、拡散領域56の出口端部との間に最短距離が生じ、場合によっては、燃料噴霧が拡散領域の出口端部で壁面と干渉する恐れがあった。 Such fuel spray has a shortest distance between the outlet end of the diffusion region 56 on the side far from the central axis 62 of the fuel injection valve 10 (FIG. 3), and in some cases, the fuel spray is at the outlet end of the diffusion region. There was a possibility of interfering with the wall at the part.
一方、噴霧の干渉を避けるために座繰り径を大きくして拡散領域56を中心軸58対称に大きくすることも考えられるが、座繰り径を大きくすれば、弁座プレート46の最小厚さが確保できない恐れがある。例えば、図4において符号Bで示す拡散領域56の底面と弁座プレート46のサック部60の付近で、弁座プレート46の設計上許容できる部材の最小厚さが確保できない恐れがある。部材の設計上許容できる最小厚さとしては、例えば、燃料噴射弁が使用される環境における部材内外の圧力差に耐えるために要求される最小肉厚、などがある。このような部材の最小厚さを確保しようとして拡散領域(座繰り)56を浅くすれば、燃料が小径のガイド領域54を長く流れることになり、燃料噴流の直進性が良くなり、拡散領域56での微粒化性能の悪化及び/若しくは噴霧のペネトレーションの増加につながることがあり、良好な燃料噴霧が生成されない恐れがある。 On the other hand, in order to avoid spray interference, it is conceivable to increase the countersink diameter and increase the diffusion region 56 symmetrically with respect to the central axis 58. However, if the countersink diameter is increased, the minimum thickness of the valve seat plate 46 is reduced. There is a fear that it cannot be secured. For example, there is a possibility that the minimum thickness of the member that can be allowed in the design of the valve seat plate 46 cannot be secured near the bottom surface of the diffusion region 56 indicated by the symbol B in FIG. 4 and the sack portion 60 of the valve seat plate 46. The minimum allowable thickness in the design of the member includes, for example, the minimum thickness required to withstand a pressure difference inside and outside the member in the environment where the fuel injection valve is used. If the diffusion region (spotting) 56 is made shallow in order to ensure the minimum thickness of such a member, the fuel will flow through the small-diameter guide region 54 for a long time, and the straightness of the fuel jet will be improved, and the diffusion region 56 will be improved. This may lead to a deterioration in atomization performance and / or an increase in the penetration of the spray, and a good fuel spray may not be generated.
図6を用いて更に詳しく述べる。サック部60が形成された弁座プレート46の場合を図6(1)に、サック部が形成されていない弁座プレート46の場合を図6(2)に示す。拡散領域56の底部の隅部とサック部60との間に最小厚さ部分(図6(1)におけるL1〜L3、図6(2)におけるL4〜L6)が生じる。図6(1)のL1あるいは図6(2)のL4に該当する噴孔52形状を基準とすれば、拡散領域の出口端部で噴霧が壁面と干渉しないようにL1(L4)に対して拡散領域56の座繰り径を大きくした場合、L2(L5)の位置に最小厚さ部分が生じる。L1(L4)はL2(L5)より小さい。つまり、座繰り径を大きくする変更によって、L2(L5)が設計許容最小厚さを下回る恐れがある。L1(L4)に対してガイド領域54を長くし、且つ、拡散領域56の座繰り径を大きくした場合、L3(L6)の位置に最小厚さ部分が生じる。この場合は、L3(L6)をL1(L4)と同等以上の厚さとすることも可能であるが、ガイド領域54の延長によって燃料噴流の直進性が良くなってしまい、噴霧の微粒化性能の悪化及び/若しくは噴霧のペネトレーションの増加につながり、良好な燃料噴霧が生成されない恐れがある。 Further details will be described with reference to FIG. The case of the valve seat plate 46 in which the sack portion 60 is formed is shown in FIG. 6 (1), and the case of the valve seat plate 46 in which the sack portion is not formed is shown in FIG. 6 (2). A minimum thickness portion (L 1 to L 3 in FIG. 6 (1), L 4 to L 6 in FIG. 6 (2)) occurs between the bottom corner of the diffusion region 56 and the sack portion 60. If the shape of the nozzle hole 52 corresponding to L 1 in FIG. 6 (1) or L 4 in FIG. 6 (2) is used as a reference, L 1 (L 4) prevents the spray from interfering with the wall surface at the exit end of the diffusion region. When the countersink diameter of the diffusion region 56 is increased with respect to (), a minimum thickness portion is generated at the position of L 2 (L 5 ). L 1 (L 4 ) is smaller than L 2 (L 5 ). That is, L 2 (L 5 ) may fall below the design allowable minimum thickness due to a change that increases the counterbore diameter. When the guide region 54 is made longer than L 1 (L 4 ) and the countersink diameter of the diffusion region 56 is increased, a minimum thickness portion is generated at the position of L 3 (L 6 ). In this case, it is possible to make L 3 (L 6 ) equal to or greater than L 1 (L 4 ), but the extension of the guide region 54 improves the straightness of the fuel jet, and the spray flow is improved. The atomization performance may be deteriorated and / or the penetration of the spray may be increased, and a good fuel spray may not be generated.
なお、図6は、説明をしやすくするため、最小厚さの場所を表す線分(注:最小厚さを与える場所は3次元空間内の”線分”になる)を含む断面が複数の噴孔形状の場合でたまたま同一平面上にある場合を表した説明図であるが、最小厚さの場所を表す線分が含まれる断面がそれぞれの噴孔形状の場合ごとに異なっても、その場合は同一の一枚の図に表現できないだけであって、考察すべき事情は複数の場合で線分がたまたま同一平面上にある場合と同じである。 For ease of explanation, FIG. 6 shows a plurality of cross sections including a line segment indicating a location of the minimum thickness (note: the location where the minimum thickness is provided is a “line segment” in the three-dimensional space). It is an explanatory diagram showing the case of the nozzle hole shape, and it happens to be on the same plane, but even if the cross section including the line segment representing the location of the minimum thickness is different for each nozzle hole shape, The case cannot be expressed in the same single figure, and the circumstances to be considered are the same as in the case where a line segment happens to be on the same plane in a plurality of cases.
かかる問題を解決するために本発明はなされたのであって、その課題とするところは、短いガイド領域を確保しつつ、弁座プレートの最小厚さを確保して、噴霧との干渉を極力回避する噴孔の拡散領域の形状と配置方法を提供することにある。 The present invention has been made in order to solve such a problem, and the object of the present invention is to prevent the interference with the spray as much as possible by ensuring the minimum thickness of the valve seat plate while ensuring a short guide region. Another object of the present invention is to provide a shape and arrangement method of the diffusion region of the injection hole.
以下、本発明について上記課題を解決するための手段を説明する。なお、本発明の理解を容易にするために添付図面の参照符号を括弧書きにて付記するが、それにより本発明が図示の形態に限定されるものではない。 Hereinafter, means for solving the above-mentioned problems will be described. In order to facilitate understanding of the present invention, reference numerals in the accompanying drawings are appended in parentheses, but the present invention is not limited to the illustrated embodiment.
上記課題を解決するために、本発明に係る燃料噴射弁は、内燃機関(1)の燃焼室(22)内に燃料を噴射する複数の噴孔(112;212)を有し、複数の噴孔の各々が、燃料を通過させて噴射する燃料量と噴射方向を決定するガイド領域(114;144;174;214)と、ガイド領域を通過した燃料を噴霧に変える拡散領域(116;146;176;216)とを備える、燃料噴射弁(10)において、複数の噴孔のうち少なくとも1つは、拡散領域の中心軸(118b;148b;178b;218b)が、ガイド領域の中心軸(118a;148a;178a;218a)に平行であり、且つ、ガイド領域の中心軸よりも燃料噴射弁の中心軸(120;150;180;220)から遠い側に偏心して形成されている、ことを特徴とする。 In order to solve the above-mentioned problems, a fuel injection valve according to the present invention has a plurality of injection holes (112; 212) for injecting fuel into a combustion chamber (22) of an internal combustion engine (1). Guide holes (114; 144; 174; 214) in which each of the holes determines the amount and direction of fuel to be injected through the fuel, and a diffusion region (116; 146; 176; 216), at least one of the plurality of nozzle holes has a central axis (118b; 148b; 178b; 218b) of the diffusion region and a central axis (118a) of the guide region. 148a; 178a; 218a), and eccentrically formed on the side farther from the central axis (120; 150; 180; 220) of the fuel injection valve than the central axis of the guide region; And features.
ここで、噴孔は、拡散領域の出口端に、更に座繰りが形成されていることを特徴とすれば、弁座プレートの最小厚さを確保しつつ、拡散領域から噴射される噴霧が出口端部で壁面と干渉することを避けることができる。 Here, if the nozzle hole is characterized in that a countersink is further formed at the outlet end of the diffusion region, the spray injected from the diffusion region is discharged while securing the minimum thickness of the valve seat plate. Interference with the wall at the end can be avoided.
また、燃料の噴射方向から見て、拡散領域は、円、長円、楕円のいずれかの形状を有することを特徴とすれば、噴射される噴霧が拡散領域の出口端部で壁面と干渉することを避けるために、拡散領域は多様な形状を取ることができる。 Further, if the diffusion region has a shape of any one of a circle, an ellipse, and an ellipse when viewed from the fuel injection direction, the spray to be injected interferes with the wall surface at the outlet end of the diffusion region. In order to avoid this, the diffusion region can take various shapes.
上記課題を解決するために、本発明に係る燃料噴射弁は、内燃機関(1)の燃焼室(22)内に燃料を噴射する複数の噴孔(312;342;412;442)を有し、複数の噴孔の各々が、燃料を通過させて噴射する燃料量と噴射方向を決定するガイド領域(314;344;414;444)と、ガイド領域を通過した燃料を噴霧に変える拡散領域(316;346;416;446)とを備える、燃料噴射弁(10)において、複数の噴孔のうち少なくとも1つは、拡散領域の中心軸(318b;348b;418b;448b)がガイド領域の中心軸(318a;348a;418a;448a)に平行ではなく、拡散領域の中心軸のうち拡散領域内にある部分がなす線分上の点のうち少なくとも一部が、ガイド領域の中心軸の延長線のうち拡散領域内または弁座プレート内にある部分がなす線分上の点のいずれの点よりも、燃料噴射弁の中心軸(320;350;420;450)から離れた位置にあるように拡散領域が形成されている、ことを特徴とする。 In order to solve the above problems, a fuel injection valve according to the present invention has a plurality of injection holes (312; 342; 412; 442) for injecting fuel into a combustion chamber (22) of an internal combustion engine (1). Each of the plurality of injection holes has a guide region (314; 344; 414; 444) for determining the fuel amount and the injection direction through which the fuel is injected, and a diffusion region for changing the fuel that has passed through the guide region into a spray ( 316; 346; 416; 446), wherein at least one of the plurality of nozzle holes has a center axis (318b; 348b; 418b; 448b) of the diffusion region at the center of the guide region At least a portion of the points on the line segment formed by the portion in the diffusion region of the central axis of the diffusion region that is not parallel to the axis (318a; 348a; 418a; 448a) is an extension of the central axis of the guide region The distance between the central axis (320; 350; 420; 450) of the fuel injection valve and the point on the line segment formed by the portion in the diffusion region or the valve seat plate A diffusion region is formed.
ここで、噴孔は、拡散領域の出口端に、更に座繰りが形成されていることを特徴とすれば、弁座プレートの最小厚さを確保しつつ、拡散領域から噴射される噴霧が出口端部で壁面と干渉することを避けることができる。 Here, if the nozzle hole is characterized in that a countersink is further formed at the outlet end of the diffusion region, the spray injected from the diffusion region is discharged while securing the minimum thickness of the valve seat plate. Interference with the wall at the end can be avoided.
上記課題を解決するために、本発明に係る燃料噴射弁は、内燃機関(1)の燃焼室(22)内に燃料を噴射する複数の噴孔を有し、燃料を通過させて噴射する燃料量と噴射方向を決定するガイド領域(814)と、ガイド領域を通過した燃料を噴霧に変える拡散領域(816)とを備える噴孔(812)を少なくとも1つ有する燃料噴射弁(10)において、燃料噴射弁の中心軸(820)を通りガイド領域の出口中心を通過する第1平面(830)に対して垂直でガイド領域の中心軸を含む第2平面(840)で、拡散領域を、燃料噴射弁の中心軸から遠い側の第1領域と中心軸から近い側の第2領域とに分割した場合、拡散領域の出口端の最浅部を通過して拡散領域の底面に平行な第3平面(850)において、第1領域の第2平面から最も遠い第1最遠点(P)と第2平面までの距離(d1)が第2領域の第2平面から最も遠い第2最遠点(Q)と第2平面までの距離(d2)より大きい、あるいは、第3平面と拡散領域の底面とで囲まれる領域において、第1領域側の容積(V1)が第2領域側の容積(V2)より大きい、ことを特徴とする。 In order to solve the above-mentioned problems, a fuel injection valve according to the present invention has a plurality of injection holes for injecting fuel into a combustion chamber (22) of an internal combustion engine (1), and injects fuel through the fuel. In a fuel injection valve (10) having at least one injection hole (812) comprising a guide region (814) for determining the amount and injection direction and a diffusion region (816) for converting the fuel that has passed through the guide region into spray. The diffusion region is defined by the second plane (840) perpendicular to the first plane (830) passing through the center axis (820) of the fuel injection valve and passing through the center of the outlet of the guide region. When divided into a first region far from the central axis of the injection valve and a second region near the central axis, a third region passing through the shallowest part of the outlet end of the diffusion region and parallel to the bottom surface of the diffusion region. In the plane (850), from the second plane of the first region The distance between the distance of the first farthest point also far and (P) to a second plane (d 1) is farthest second farthest point from the second plane of the second region (Q) to a second plane (d 2 ), Or in a region surrounded by the third plane and the bottom surface of the diffusion region, the volume (V 1 ) on the first region side is larger than the volume (V 2 ) on the second region side. .
本発明の構成を採用することで、外側に拡散した噴霧との干渉を避けつつ、内側の比較的拡散の小さい噴霧側の座繰りを減らし、弁座プレートの厚さを確保することが可能になる。 By adopting the configuration of the present invention, it is possible to reduce the countersink on the spray side with a relatively small diffusion on the inside and avoid the interference with the spray diffused on the outside, and to secure the thickness of the valve seat plate Become.
部材厚さの確保の制限のみにより、噴孔長を長くすることを回避できる。 It is possible to avoid increasing the length of the nozzle hole only by limiting the securing of the member thickness.
本発明の実施形態を、図面を参照しつつ以下に説明する。 Embodiments of the present invention will be described below with reference to the drawings.
(平行偏心型)
図7は、平行偏心型の噴孔112が形成された弁座プレート110の縦断面図である。弁座プレート110の内側先端には、噴霧を安定化させるためのサック部122が形成されている。
(Parallel eccentric type)
FIG. 7 is a longitudinal sectional view of the valve seat plate 110 in which the parallel eccentric type nozzle holes 112 are formed. A sack portion 122 for stabilizing the spray is formed at the inner front end of the valve seat plate 110.
図7(1)において、弁座プレート110の噴孔112は、流入側に形成された小径のガイド領域114と、噴射側に形成されガイド領域114より大径の拡散領域116とで構成される。ガイド領域114の中心軸118aは燃料噴射弁10(図3)の中心軸120に対して平行に形成され、拡散領域116の中心軸118bはガイド領域114の中心軸118aに対して平行に形成されている。また、拡散領域116の中心軸118bは、ガイド領域114の中心軸118aに対して、燃料噴射弁10(図3)の中心軸120から遠い側に偏心して形成されている。拡散領域116の底面には、例えば、ガイド領域114の中心軸118aに対して直角な段部が形成されている。ガイド領域114から拡散領域116を介して燃焼室22(図2)に流出する燃料噴流は、燃料噴霧となって拡散する。 In FIG. 7A, the nozzle hole 112 of the valve seat plate 110 includes a small-diameter guide region 114 formed on the inflow side and a diffusion region 116 formed on the injection side and having a larger diameter than the guide region 114. . The central axis 118a of the guide region 114 is formed parallel to the central axis 120 of the fuel injection valve 10 (FIG. 3), and the central axis 118b of the diffusion region 116 is formed parallel to the central axis 118a of the guide region 114. ing. Further, the central axis 118b of the diffusion region 116 is formed eccentric to the far side from the central axis 120 of the fuel injection valve 10 (FIG. 3) with respect to the central axis 118a of the guide region 114. On the bottom surface of the diffusion region 116, for example, a step portion perpendicular to the central axis 118a of the guide region 114 is formed. The fuel jet flowing from the guide region 114 to the combustion chamber 22 (FIG. 2) through the diffusion region 116 diffuses as fuel spray.
かかる構成を有すれば、ガイド領域114を長くしないので噴霧のペネトレーションに変化はなく、拡散領域116の底面と弁座プレート110のサック部122の付近で弁座プレート110の最小厚さを確保しつつ、拡散領域116から噴射される噴霧が拡散領域116の出口端部で壁面と干渉することを避けることができる。 With such a configuration, since the guide region 114 is not lengthened, there is no change in the penetration of the spray, and the minimum thickness of the valve seat plate 110 is secured near the bottom surface of the diffusion region 116 and the sack portion 122 of the valve seat plate 110. However, it is possible to avoid the spray sprayed from the diffusion region 116 from interfering with the wall surface at the exit end of the diffusion region 116.
(平行偏心型の変形例1)
尚、拡散領域146の中心軸148bがガイド領域144の中心軸148aに対して平行な関係を維持した状態で、ガイド領域144の中心軸148aが燃料噴射弁10(図3)の中心軸150に対して、燃料の噴射方向に狭まる向きに傾斜して形成された変形例1も考えられる(図7(2)参照)。この場合も、ガイド領域144を長くしないので噴霧のペネトレーションに変化はなく、ガイド領域144の中心軸148aに平行な拡散領域146の中心軸148bは、ガイド領域144の中心軸148aに対して、燃料噴射弁10(図3)の中心軸150から遠い側に偏心することで、拡散領域146から噴射される噴霧が拡散領域146の出口端部で壁面との干渉を避けることが可能である。
(Modification 1 of parallel eccentric type)
In the state where the central axis 148b of the diffusion region 146 maintains a parallel relationship with the central axis 148a of the guide region 144, the central axis 148a of the guide region 144 is aligned with the central axis 150 of the fuel injection valve 10 (FIG. 3). On the other hand, the modification 1 formed by inclining in the direction narrowing in the fuel injection direction is also conceivable (see FIG. 7B). Also in this case, since the guide region 144 is not lengthened, there is no change in the penetration of the spray, and the central axis 148b of the diffusion region 146 parallel to the central axis 148a of the guide region 144 is fuel relative to the central axis 148a of the guide region 144. By decentering away from the central axis 150 of the injection valve 10 (FIG. 3), the spray injected from the diffusion region 146 can avoid interference with the wall surface at the outlet end of the diffusion region 146.
(平行偏心型の変形例2)
ガイド領域174の中心軸178a、中心軸178aに平行な拡散領域176の中心軸178bは、燃料噴射弁10(図3)の中心軸180に対して、拡がる向きに傾斜しても良い(図7(3)参照)。要するに、ガイド領域174を長くすることなく、拡散領域176の中心軸178bがガイド領域174の中心軸178aに対して偏心することで、拡散領域176から噴射される噴霧が拡散領域176の出口端部で壁面との干渉を避けるように構成されればよい。
(Modification 2 of parallel eccentric type)
The central axis 178a of the guide region 174 and the central axis 178b of the diffusion region 176 parallel to the central axis 178a may be inclined in an expanding direction with respect to the central axis 180 of the fuel injection valve 10 (FIG. 3) (FIG. 7). (See (3)). In short, the center axis 178b of the diffusion region 176 is eccentric with respect to the center axis 178a of the guide region 174 without increasing the length of the guide region 174, so that the spray injected from the diffusion region 176 is the exit end of the diffusion region 176. In order to avoid interference with the wall surface.
(長円型)
図8は、長円型の噴孔212が形成された弁座プレート210の縦断面図である。この実施形態では、噴孔212は、小径のガイド領域214と、ガイド領域214を含む大きさの長円形(角丸長方形)の拡散領域216とで構成される。ガイド領域214の中心軸218aは燃料噴射弁10(図3)の中心軸220に対して平行に形成され、拡散領域216の中心軸218bはガイド領域214の中心軸218aに対して平行に形成される。また、拡散領域216の中心軸218bは、ガイド領域214の中心軸218aに対して、燃料噴射弁10(図3)の中心軸220から遠い側に偏心して形成される。例えば、拡散領域216の長円形の一方の半円の軸をガイド領域214の中心軸218aに合致させることが考えられる。
(Oval type)
FIG. 8 is a longitudinal sectional view of the valve seat plate 210 in which an oval injection hole 212 is formed. In this embodiment, the nozzle hole 212 includes a small-diameter guide region 214 and an oval (cornered rectangle) diffusion region 216 having a size including the guide region 214. A central axis 218a of the guide region 214 is formed parallel to the central axis 220 of the fuel injection valve 10 (FIG. 3), and a central axis 218b of the diffusion region 216 is formed parallel to the central axis 218a of the guide region 214. The Further, the central axis 218b of the diffusion region 216 is formed eccentric to the side far from the central axis 220 of the fuel injection valve 10 (FIG. 3) with respect to the central axis 218a of the guide region 214. For example, it is conceivable to align the axis of one of the oval semicircles of the diffusion region 216 with the central axis 218 a of the guide region 214.
かかる構成を有すれば、ガイド領域214を長くしないので噴霧のペネトレーションに変化はなく、拡散領域216の底面と弁座プレート210のサック部222の付近で弁座プレート210の最小厚さを確保しつつ、拡散領域216から噴射される噴霧が拡散領域216の出口端部で壁面との干渉を避けることができる。 With such a configuration, since the guide region 214 is not lengthened, there is no change in spray penetration, and the minimum thickness of the valve seat plate 210 is secured near the bottom surface of the diffusion region 216 and the sack portion 222 of the valve seat plate 210. However, the spray sprayed from the diffusion region 216 can avoid interference with the wall surface at the exit end of the diffusion region 216.
(長円型の変形例1,2)
尚、長円形(角丸長方形)の変形例として、ガイド領域214を長くすることなく、拡散領域216を楕円形に形成しても同様の効果が得られる(変形例1)(図示省略)。また、偏心型の変形例と同様に、ガイド領域214を長くすることなく、ガイド領域214の中心軸218aが燃料噴射弁10(図3)の中心軸220に対して傾斜して形成しても良い(変形例2)(図示省略)。
(Oval-shaped variations 1 and 2)
As a modification of an oval (rounded rectangle), the same effect can be obtained even if the diffusion region 216 is formed in an oval shape without making the guide region 214 long (Modification 1) (not shown). Similarly to the eccentric type modification, the central axis 218a of the guide region 214 may be formed to be inclined with respect to the central axis 220 of the fuel injection valve 10 (FIG. 3) without lengthening the guide region 214. Good (Modification 2) (not shown).
(非平行型)
次に、非平行型の噴孔が形成された弁座プレートを、図9、図10を用いて説明する。図9は、非平行型の噴孔312、342が形成された弁座プレート310、340の断面図であり、図10は、図9に示す弁座プレート310、340の断面位置を説明する縦断面図である。図9において、噴孔312、342は、拡散領域316、346の中心軸318b、348bとガイド領域314、344の中心軸318a、348aとが非平行であり、且つ、同一の平面α上に配置されて形成されている。そして、平面αは、図10に示されるように、燃料噴射弁10(図3)の中心軸320、350に対して傾斜している。ここで、図10の平面αが、図9に示される断面位置である。従って、図9に示された燃料噴射弁10(図3)の中心軸320、350は、図9に示す断面上にない。図の下側に示された部分が紙面に近く、図の上側に向かって紙面から徐々に離れた配置となる。
(Non-parallel type)
Next, a valve seat plate in which non-parallel injection holes are formed will be described with reference to FIGS. FIG. 9 is a cross-sectional view of the valve seat plates 310 and 340 in which the non-parallel injection holes 312 and 342 are formed, and FIG. 10 is a longitudinal cross-sectional view for explaining the cross-sectional positions of the valve seat plates 310 and 340 shown in FIG. FIG. In FIG. 9, the nozzle holes 312 and 342 are arranged on the same plane α, with the central axes 318b and 348b of the diffusion regions 316 and 346 and the central axes 318a and 348a of the guide regions 314 and 344 being non-parallel. Has been formed. The plane α is inclined with respect to the central axes 320 and 350 of the fuel injection valve 10 (FIG. 3) as shown in FIG. 10. Here, the plane α in FIG. 10 is the cross-sectional position shown in FIG. 9. Accordingly, the central axes 320 and 350 of the fuel injection valve 10 (FIG. 3) shown in FIG. 9 are not on the cross section shown in FIG. The portion shown on the lower side of the figure is close to the paper surface, and is gradually separated from the paper surface toward the upper side of the drawing.
図9(1)に示されるように、拡散領域316の中心軸318bのうち拡散領域316内にある部分は、線分S1で示される。ガイド領域314の中心軸318aは、「ガイド領域の中心軸の延長線のうち拡散領域内にある部分がなす線分」がT1で示され、「ガイド領域の中心軸の延長線のうち弁座プレート内にある部分がなす線分」がU1で示される。そして、拡散領域316の中心軸318bとガイド領域314の中心軸318aのいずれも、燃料の噴射方向に対して狭まる向きに傾斜している。本実施形態では、図9(1)では、線分S1上の点C1で示された部分(線分S1の最下点)が、線分T1及び線分U1上のいずれの点よりも、燃料噴射弁10(図3)の中心軸320から離れた位置となるように、噴孔312が形成されている。 As shown in FIG. 9 (1), the portion located in the diffusion region 316 of the central axis 318b of the diffusion region 316 is indicated by a line segment S 1. The central axis of the guide area 314 318a, the "line segment formed by the portion in the diffusion region of the extension line of the center axis of the guide region" is indicated by T 1, of which valve the extension line of the center axis of the "guide region A line segment formed by a portion in the seat plate is indicated by U 1 . Both the central axis 318b of the diffusion region 316 and the central axis 318a of the guide region 314 are inclined in a direction narrowing with respect to the fuel injection direction. In the present embodiment, in FIG. 9 (1), the line segment indicated by a point C 1 on the S 1 portion (lowest point of the line segment S 1) is, either on a line T 1 and line U 1 of The nozzle hole 312 is formed at a position farther from the central axis 320 of the fuel injection valve 10 (FIG. 3) than the point.
図9(2)に示された弁座プレート340が「ガイド領域の中心軸の延長線のうち弁座プレート内にある部分がなす線分」(図9(1)においてU1で示される部分)を有していない点で、図9(1)に示された弁座プレート310と相違する。図9(2)に示されるように、拡散領域346の中心軸348bのうち拡散領域346内にある部分は、線分S2で示される。ガイド領域344の中心軸348aは、「ガイド領域の中心軸の延長線のうち拡散領域内にある部分がなす線分」がT2で示される。そして、拡散領域346の中心軸348bとガイド領域344の中心軸348aのいずれも、燃料の噴射方向に対して狭まる向きに傾斜している。本実施形態では、図9(2)において線分S2上の点C2で示された部分が、線分T2上のいずれの点よりも、燃料噴射弁10(図3)の中心軸350から離れた位置となるように、噴孔342が形成されている。 The valve seat plate 340 shown in FIG. 9 (2) is “a line segment formed by a portion in the valve seat plate out of the extension line of the central axis of the guide region” (the portion indicated by U 1 in FIG. 9 (1)). ) Is different from the valve seat plate 310 shown in FIG. As shown in FIG. 9 (2), the portion located in the diffusion region 346 of the central axis 348b of the diffusion region 346 is indicated by a line segment S 2. The central axis 348a of the guide region 344, "a line segment forming a portion in the diffusion region among the extension line of the center axis of the guide region" is represented by T 2. Both the central axis 348b of the diffusion region 346 and the central axis 348a of the guide region 344 are inclined in a direction narrowing with respect to the fuel injection direction. In the present embodiment, the C 2 in the portion indicated by a point on the line segment S 2 in FIG. 9 (2), the central axis than any point on the segment T 2, the fuel injection valve 10 (FIG. 3) An injection hole 342 is formed at a position away from 350.
(非平行型の変形例1)
図11は、非平行型の変形例1の噴孔412が形成された弁座プレート410の縦断面図である。図9に示す実施形態は、拡散領域316、346の中心軸318b、348bとガイド領域314、344の中心軸318a、348aとを含む平面αが燃料噴射弁10(図3)の中心軸320、350に対して傾斜して配置された構成であるのに対して、変形例1は、拡散領域416の中心軸418bとガイド領域414の中心軸418aを含む平面が燃料噴射弁10(図3)の中心軸420に対して平行である点で相違する。
(Non-parallel type modification 1)
FIG. 11 is a longitudinal sectional view of the valve seat plate 410 in which the nozzle holes 412 of the non-parallel type modified example 1 are formed. In the embodiment shown in FIG. 9, the plane α including the central axes 318b and 348b of the diffusion regions 316 and 346 and the central axes 318a and 348a of the guide regions 314 and 344 has a central axis 320 of the fuel injection valve 10 (FIG. 3). In contrast to the configuration arranged to be inclined with respect to 350, in the first modification, the plane including the central axis 418b of the diffusion region 416 and the central axis 418a of the guide region 414 is the fuel injection valve 10 (FIG. 3). Is different in that it is parallel to the central axis 420 of the.
図11に示す変形例1は、噴孔412が、小径のガイド領域414と、ガイド領域414より大径の拡散領域416とで構成される。ガイド領域414の中心軸418aは、燃料噴射弁10(図3)の中心軸420に対して平行に形成される。一方、拡散領域416の中心軸418bは、ガイド領域414の出口中心を通り、燃料の噴射方向に向かって燃料噴射弁10(図3)の中心軸420から離れる向きに傾斜して形成される。その結果、拡散領域416の中心軸418bは、拡散領域416の中心軸418b及び燃料噴射弁10(図3)の中心軸420に対して平行でない配置となる。 In Modification 1 shown in FIG. 11, the nozzle hole 412 includes a guide region 414 having a small diameter and a diffusion region 416 having a larger diameter than the guide region 414. A central axis 418a of the guide region 414 is formed in parallel to the central axis 420 of the fuel injection valve 10 (FIG. 3). On the other hand, the central axis 418b of the diffusion region 416 is formed so as to be inclined in a direction away from the central axis 420 of the fuel injection valve 10 (FIG. 3) toward the fuel injection direction through the center of the outlet of the guide region 414. As a result, the central axis 418b of the diffusion region 416 is not parallel to the central axis 418b of the diffusion region 416 and the central axis 420 of the fuel injection valve 10 (FIG. 3).
拡散領域416の中心軸418bは、燃料の噴射方向に向かって中心軸420から離れる向きに傾斜して配置される。中心軸418bの傾斜角度は、拡散領域416から噴射される噴霧の噴流角(図4)を考慮して決定され、図11に示す実施形態では、拡散領域416から噴射される噴霧が拡散領域416の出口端部における壁面との距離が、中心軸420に近い側と遠い側とで同じなるように決定される。 The central axis 418b of the diffusion region 416 is disposed so as to be inclined away from the central axis 420 in the fuel injection direction. The inclination angle of the central axis 418b is determined in consideration of the jet angle of spray sprayed from the diffusion region 416 (FIG. 4). In the embodiment shown in FIG. 11, the spray sprayed from the diffusion region 416 is diffused region 416. The distance from the wall surface at the outlet end is determined to be the same on the side closer to the central axis 420 and on the far side.
かかる構成を有すれば、ガイド領域414を長くしないので噴霧のペネトレーションに変化はなく、拡散領域416の底面と弁座プレート410のサック部422の付近で弁座プレート410の最小厚さを確保しつつ、拡散領域416から噴射される噴霧が拡散領域416の出口端部で壁面との干渉を避けることができる。 With this configuration, since the guide region 414 is not lengthened, there is no change in the penetration of the spray, and the minimum thickness of the valve seat plate 410 is ensured near the bottom surface of the diffusion region 416 and the sac portion 422 of the valve seat plate 410. However, the spray sprayed from the diffusion region 416 can avoid interference with the wall surface at the exit end of the diffusion region 416.
(非平行型の変形例2)
図12は、非平行型の変形例2に係る噴孔442が形成された弁座プレート440の縦断面図である。この変形例2では、拡散領域446の中心軸448bはガイド領域444の出口中心を通過せず、拡散領域446の中心軸448bの中点が、ガイド領域444の出口中心に対して、燃料噴射弁10(図3)の中心軸450よりも離れた位置に配置して形成される。ガイド領域444を長くしないので噴霧のペネトレーションに変化はなく、拡散領域446の底面と弁座プレート440のサック部452の付近で弁座プレート440の最小厚さを確保しつつ、拡散領域446から噴射される噴霧が拡散領域446の出口端部で壁面との干渉を避けることができる。
(Non-parallel type modification 2)
FIG. 12 is a longitudinal sectional view of the valve seat plate 440 in which the injection holes 442 according to the non-parallel type modification 2 are formed. In the second modification, the central axis 448 b of the diffusion region 446 does not pass through the exit center of the guide region 444, and the middle point of the central axis 448 b of the diffusion region 446 is a fuel injection valve with respect to the exit center of the guide region 444. 10 (FIG. 3) is arranged at a position distant from the central axis 450. Since the guide area 444 is not lengthened, there is no change in the penetration of the spray, and the spray area 446 is injected from the diffusion area 446 while ensuring the minimum thickness of the valve seat plate 440 near the bottom surface of the diffusion area 446 and the sack portion 452 of the valve seat plate 440. The spray to be applied can avoid interference with the wall surface at the exit end of the diffusion region 446.
(非平行型の変形例3)
図9に示す実施形態では、拡散領域316、346の中心軸318b、348bとガイド領域314、344の中心軸318a、348aとが平行ではないが同一の平面α上に配置された構成を示したが、本発明はこれに限定されるものではなく、例えば、拡散領域の中心軸とガイド領域の中心軸とがねじれの位置に配置された構成であってもよい(図示省略)。
(Non-parallel type modification 3)
In the embodiment shown in FIG. 9, the central axes 318b and 348b of the diffusion regions 316 and 346 and the central axes 318a and 348a of the guide regions 314 and 344 are not parallel but are arranged on the same plane α. However, the present invention is not limited to this, and for example, a configuration in which the central axis of the diffusion region and the central axis of the guide region are arranged at a twisted position (not shown) may be employed.
(拡散領域を2段にする変形例)
図13は、ガイド領域514,614,714の中心軸に対して同軸の座繰り530,630,730が拡散領域516,616,716の出口側に形成された噴孔512,612,712を有する弁座プレート510,610,710の縦断面図である。図13(1)は図7に示した偏心型噴孔512を有する弁座プレート510に座繰り530が形成された例を、図13(2)は図7に示した長円型噴孔612を有する弁座プレート610に座繰り630が形成された例を、図13(3)は図7に示した非平行型噴孔712を有する弁座プレート710に座繰り730が形成された例を示す。いずれの例も、弁座プレート510,610,710の最小厚さを確保しつつ、拡散領域516,616,716から噴射される噴霧が出口端部で壁面との干渉を避けることができる。なお、拡散領域に対してさらに設ける座繰りは、本実施例においてはガイド領域の中心軸に対して同軸である場合を説明したが、その他拡散領域に対して同軸であってもよく、また、これらのいずれとも同軸でなくてもよい。
(Modification example in which the diffusion region has two stages)
13 has nozzle holes 512, 612, and 712 in which countersinks 530, 630, and 730 coaxial with the central axis of the guide regions 514, 614, and 714 are formed on the outlet side of the diffusion regions 516, 616, and 716, respectively. It is a longitudinal cross-sectional view of the valve seat plate 510,610,710. FIG. 13 (1) shows an example in which the countersink 530 is formed on the valve seat plate 510 having the eccentric type injection hole 512 shown in FIG. 7, and FIG. 13 (2) shows the oval injection hole 612 shown in FIG. FIG. 13 (3) shows an example in which the countersink 730 is formed on the valve seat plate 710 having the non-parallel injection hole 712 shown in FIG. Show. In any case, the spray injected from the diffusion regions 516, 616, and 716 can avoid interference with the wall surface at the outlet end portion while ensuring the minimum thickness of the valve seat plates 510, 610, and 710. Note that the countersink further provided for the diffusion region has been described in the present embodiment as being coaxial with the central axis of the guide region, but may be coaxial with the other diffusion region, None of these may be coaxial.
(燃料噴射弁の中心軸に対する噴孔の形状)
図14,図15は、本発明に係る弁座プレート810(即ち燃料噴射弁10(図3))の中心軸820に対する噴孔812の形状を説明する図である。図14(1)において、第1平面830は、弁座プレート810の中心軸820を含み、ガイド領域814(図15)の出口中心を通過する平面である。第2平面840は、第1平面830に垂直でガイド領域814(図15)の中心軸818a(図15)を含む平面である。第4平面860は、第2平面840に垂直で拡散領域816(図15)の中心軸818b(図15)を含む平面である。図14(2)は、第2平面840と第4平面860との交線の方向から見た図である。図14(3)は、第4平面860で弁座プレート810を切断した状態の斜視図である。
(Shape of the injection hole with respect to the central axis of the fuel injection valve)
14 and 15 are views for explaining the shape of the injection hole 812 with respect to the central axis 820 of the valve seat plate 810 (that is, the fuel injection valve 10 (FIG. 3)) according to the present invention. 14 (1), the first plane 830 is a plane that includes the central axis 820 of the valve seat plate 810 and passes through the outlet center of the guide region 814 (FIG. 15). The second plane 840 is a plane that is perpendicular to the first plane 830 and includes the central axis 818a (FIG. 15) of the guide region 814 (FIG. 15). The fourth plane 860 is a plane that is perpendicular to the second plane 840 and includes the central axis 818b (FIG. 15) of the diffusion region 816 (FIG. 15). FIG. 14 (2) is a view seen from the direction of the line of intersection between the second plane 840 and the fourth plane 860. FIG. 14 (3) is a perspective view of a state in which the valve seat plate 810 is cut along the fourth plane 860.
図15(1)は、第4平面860における弁座プレート810の断面図であり(図15(2)参照)、図15(2)は、燃料噴射弁10(図3)の中心軸820に対する第4平面860の位置関係を示す図である。図15(1)において、第2平面840(図14)は、ガイド領域814の中心軸818aの位置に相当する。第3平面850は、点P(後述)を通過し、拡散領域816の底面に平行な面である。拡散領域816の底面は、拡散領域816の中心軸に垂直であるから、第3平面850は、第4平面860に垂直となる。図15に示す実施形態では、ガイド領域814の中心軸818aは、弁座プレート810の中心軸820に対してねじれの関係にある。 15 (1) is a sectional view of the valve seat plate 810 in the fourth plane 860 (see FIG. 15 (2)), and FIG. 15 (2) is relative to the central axis 820 of the fuel injection valve 10 (FIG. 3). It is a figure which shows the positional relationship of the 4th plane 860. FIG. In FIG. 15A, the second plane 840 (FIG. 14) corresponds to the position of the central axis 818a of the guide region 814. The third plane 850 is a plane that passes through a point P (described later) and is parallel to the bottom surface of the diffusion region 816. Since the bottom surface of the diffusion region 816 is perpendicular to the central axis of the diffusion region 816, the third plane 850 is perpendicular to the fourth plane 860. In the embodiment shown in FIG. 15, the central axis 818 a of the guide region 814 is twisted with respect to the central axis 820 of the valve seat plate 810.
拡散領域816を第2平面840(図14)(即ち図15におけるガイド領域814の軸818aの位置)で当該燃料噴射弁の当該中心軸から遠い側の第1領域と当該中心軸から近い側の第2領域とに分割した場合、拡散領域816の出口端の最浅部を通過して拡散領域816の底面に平行な第3平面850において、第1領域の第2平面840(図14)(即ち軸818a)から最も遠いところにある点Pから第2平面840(図14)(即ち図15における軸818a)までの距離d1が、第2領域の第2平面840(図14)(即ち軸818a)から最も遠いところにある点Qから第2平面840(図14)までの距離d2よりΔd(=d1−d2)だけ大きい。このことは、ガイド領域の中心軸と弁座プレートの中心軸とがねじれの関係にない上記実施形態にも当てはまる。 The diffusion region 816 is arranged on the second plane 840 (FIG. 14) (that is, the position of the axis 818a of the guide region 814 in FIG. 15) on the side far from the central axis of the fuel injection valve and the side near the central axis. When divided into the second region, the second flat surface 840 of the first region passes through the shallowest part of the exit end of the diffusion region 816 and is parallel to the bottom surface of the diffusion region 816 (FIG. 14). That is, the distance d 1 from the point P farthest from the axis 818a) to the second plane 840 (FIG. 14) (ie, axis 818a in FIG. 15) is the second plane 840 (FIG. 14) of the second region (ie The distance d 2 from the point Q farthest from the axis 818a) to the second plane 840 (FIG. 14) is larger by Δd (= d 1 −d 2 ). This also applies to the above-described embodiment where the central axis of the guide region and the central axis of the valve seat plate are not in a torsional relationship.
また、このとき、第3平面850と拡散領域816の底面とで囲まれる領域において、第1領域側の容積V1は第2領域側の容積V2より大きい。このことも、ガイド領域の中心軸と弁座プレートの中心軸とがねじれの関係にない上記実施形態にも当てはまる。 At this time, in the region surrounded by the third plane 850 and the bottom surface of the diffusion region 816, the volume V 1 on the first region side is larger than the volume V 2 on the second region side. This also applies to the above-described embodiment in which the central axis of the guide region and the central axis of the valve seat plate are not in a torsional relationship.
なお、以上の実施例においては、本発明がサイドマウント方式の直噴エンジンにおいて適用される場合について説明したが、本発明はサイドマウント方式の場合に限られるものではなく、センターマウント方式などの他の方式のエンジンにも適用可能である。 In the above embodiments, the case where the present invention is applied to a side-mount type direct injection engine has been described. However, the present invention is not limited to the case of the side-mount type. It can also be applied to other types of engines.
1:ガソリンエンジン(内燃機関)、10:燃料噴射弁、22:燃焼室、
112;212;312;342;412;442;812:複数の噴孔、
114;144;174;214;314;344;414;444;814:ガイド領域、
116;146;176;216;316;346;416;446;816:拡散領域、
118a;148a;178a;218a;318a;348a;418a;448a:ガイド領域の中心軸、
118b;148b;178b;218b;318b;348b;418b;448b:拡散領域の中心軸、
120;150;180;220;320;350;420;450;820:燃料噴射弁の中心軸、
830:第1平面、840:第2平面、850:第3平面
1: gasoline engine (internal combustion engine), 10: fuel injection valve, 22: combustion chamber,
112; 212; 312; 342; 412; 442; 812: a plurality of nozzle holes;
114; 144; 174; 214; 314; 344; 414; 444; 814: guide region;
116; 146; 176; 216; 316; 346; 416; 446; 816: diffusion region;
118a; 148a; 178a; 218a; 318a; 348a; 418a; 448a: the central axis of the guide region;
118b; 148b; 178b; 218b; 318b; 348b; 418b; 448b: the central axis of the diffusion region;
120; 150; 180; 220; 320; 350; 420; 450; 820: the central axis of the fuel injector;
830: First plane, 840: Second plane, 850: Third plane
Claims (6)
前記複数の噴孔の各々が、燃料を通過させて噴射する燃料量と噴射方向を決定するガイド領域(114;144;174;214)と、当該ガイド領域を通過した燃料を噴霧に変える拡散領域(116;146;176;216)と、を備える、燃料噴射弁(10)において、
前記複数の噴孔のうち少なくとも1つは、前記拡散領域の中心軸(118b;148b;178b;218b)が、前記ガイド領域の中心軸(118a;148a;178a;218a)に平行であり、且つ、当該ガイド領域の当該中心軸よりも前記燃料噴射弁の中心軸(120;150;180;220)から遠い側に偏心して形成されている、燃料噴射弁。 A fuel injection valve having a plurality of injection holes (112; 212) for injecting fuel into a combustion chamber (22) of an internal combustion engine (1),
Each of the plurality of injection holes has a guide region (114; 144; 174; 214) for determining the amount and direction of fuel to be injected through the fuel and a diffusion region for converting the fuel that has passed through the guide region into spray. (116; 146; 176; 216), in a fuel injector (10),
At least one of the plurality of nozzle holes has a central axis (118b; 148b; 178b; 218b) of the diffusion region parallel to a central axis (118a; 148a; 178a; 218a) of the guide region; The fuel injection valve is eccentrically formed on a side farther from the central axis (120; 150; 180; 220) of the fuel injection valve than the central axis of the guide region.
前記噴孔は、前記拡散領域の出口端に、更に座繰りが形成されている、燃料噴射弁。 The fuel injection valve according to claim 1, wherein
The injection hole is a fuel injection valve in which a countersink is further formed at an outlet end of the diffusion region.
燃料の噴射方向から見て、前記拡散領域は、円、長円、楕円のいずれかの形状を有する、燃料噴射弁。 The fuel injection valve according to claim 1, wherein
The fuel injection valve, wherein the diffusion region has any one of a circle, an ellipse, and an ellipse as viewed from the fuel injection direction.
前記複数の噴孔の各々が、燃料を通過させて噴射する燃料量と噴射方向を決定するガイド領域(314;344;414;444)と、当該ガイド領域を通過した燃料を噴霧に変える拡散領域(316;346;416;446)と、を備える、燃料噴射弁(10)において、
前記複数の噴孔のうち少なくとも1つは、
前記拡散領域の中心軸(318b;348b;418b;448b)が前記ガイド領域の中心軸(318a;348a;418a;448a)に平行ではなく、
前記拡散領域の前記中心軸のうち前記拡散領域内にある部分がなす線分上の点のうち少なくとも一部が、前記ガイド領域の前記中心軸の延長線のうち前記拡散領域内または弁座プレート内にある部分がなす線分上の点のいずれの点よりも、前記燃料噴射弁の中心軸(320;350;420;450)から離れた位置にあるように当該拡散領域が形成されている、燃料噴射弁。 A fuel injection valve having a plurality of injection holes (312; 342; 412; 442) for injecting fuel into a combustion chamber (22) of an internal combustion engine (1),
Each of the plurality of nozzle holes has a guide region (314; 344; 414; 444) for determining the amount and direction of fuel to be injected through the fuel and a diffusion region for converting the fuel that has passed through the guide region into spray. (316; 346; 416; 446), comprising:
At least one of the plurality of nozzle holes is
The central axis (318b; 348b; 418b; 448b) of the diffusion region is not parallel to the central axis (318a; 348a; 418a; 448a) of the guide region;
At least a part of points on a line segment formed by a portion in the diffusion region of the central axis of the diffusion region is in the diffusion region or a valve seat plate in an extension line of the central axis of the guide region. The diffusion region is formed so as to be farther from the central axis (320; 350; 420; 450) of the fuel injection valve than any point on the line segment formed by the inner portion. , Fuel injection valve.
前記噴孔は、前記拡散領域の出口端に、更に座繰りが形成されている、燃料噴射弁。 The fuel injection valve according to claim 4, wherein
The injection hole is a fuel injection valve in which a countersink is further formed at an outlet end of the diffusion region.
前記燃料噴射弁の中心軸(820)を通り前記ガイド領域の出口中心を通過する第1平面(830)に対して垂直で当該ガイド領域の中心軸を含む第2平面(840)で、前記拡散領域を、当該燃料噴射弁の当該中心軸から遠い側の第1領域と当該中心軸から近い側の第2領域とに分割した場合、当該拡散領域の出口端の最浅部を通過して当該拡散領域の底面に平行な第3平面(850)において、当該第1領域の当該第2平面から最も遠い第1最遠点(P)と当該第2平面までの距離(d1)が当該第2領域の当該第2平面から最も遠い第2最遠点(Q)と当該第2平面までの距離(d2)より大きい、あるいは、
前記第3平面と前記拡散領域の前記底面とで囲まれる領域において、前記第1領域側の容積(V1)が前記第2領域側の容積(V2)より大きい、燃料噴射弁。 A fuel injection valve having a plurality of injection holes for injecting fuel into the combustion chamber (22) of the internal combustion engine (1), wherein the guide region determines the amount of fuel to be injected and the injection direction (814). A fuel injection valve (10) having at least one injection hole (812) comprising: a diffusion region (816) that converts the fuel that has passed through the guide region into spray;
The diffusion in a second plane (840) perpendicular to the first plane (830) passing through the central axis (820) of the fuel injection valve and passing through the outlet center of the guide area and including the central axis of the guide area When the region is divided into a first region far from the central axis of the fuel injection valve and a second region near the central axis, the region passes through the shallowest part at the outlet end of the diffusion region. In the third plane (850) parallel to the bottom surface of the diffusion region, the distance (d 1 ) between the first farthest point (P) farthest from the second plane of the first region and the second plane is the first plane. Greater than the distance (d 2 ) between the second farthest point (Q) farthest from the second plane of the two regions and the second plane, or
The fuel injection valve, wherein a volume (V 1 ) on the first region side is larger than a volume (V 2 ) on the second region side in a region surrounded by the third plane and the bottom surface of the diffusion region.
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Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2015135062A (en) * | 2014-01-16 | 2015-07-27 | 株式会社日本自動車部品総合研究所 | fuel injection valve |
| JP2018053846A (en) * | 2016-09-30 | 2018-04-05 | 日立オートモティブシステムズ株式会社 | Fuel injection valve, control device for fuel injection valve, and control method |
| US10995655B2 (en) | 2016-11-30 | 2021-05-04 | Hitachi Automotive Systems, Ltd. | Fuel injection device |
| KR20220051404A (en) | 2019-09-25 | 2022-04-26 | 봇슈 가부시키가이샤 | Fuel injection valve and internal combustion engine with fuel injection valve |
Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS5987271A (en) * | 1982-11-09 | 1984-05-19 | Yanmar Diesel Engine Co Ltd | Fuel injection valve for diesel engine |
| JPH0735002A (en) * | 1993-07-27 | 1995-02-03 | Shin A C Ii:Kk | Fuel injection nozzle of direct injection type diesel engine |
| JP2003506626A (en) * | 1999-08-11 | 2003-02-18 | ローベルト ボツシユ ゲゼルシヤフト ミツト ベシユレンクテル ハフツング | Fuel injection valve and method for manufacturing a discharge opening of the valve |
| JP2008064094A (en) * | 2006-09-05 | 2008-03-21 | Robert Bosch Gmbh | Fuel injection valve |
| JP2009243323A (en) * | 2008-03-31 | 2009-10-22 | Hitachi Ltd | Fuel injection valve and method for processing orifice |
| JP2009270448A (en) * | 2008-05-01 | 2009-11-19 | Mitsubishi Electric Corp | Fuel injection valve |
| JP2011001864A (en) * | 2009-06-18 | 2011-01-06 | Hitachi Automotive Systems Ltd | Fuel injection valve |
Family Cites Families (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2001214839A (en) * | 2000-01-27 | 2001-08-10 | Unisia Jecs Corp | Fuel injection valve |
| DE102005036951A1 (en) * | 2005-08-05 | 2007-02-08 | Robert Bosch Gmbh | Fuel injection valve and method for forming injection openings |
| DE102006047136A1 (en) * | 2006-10-05 | 2008-04-10 | Robert Bosch Gmbh | Fuel injection valve for mixture-compressing, external-ignition internal-combustion engine, has atomizer device implemented as multi-fan jet-nozzle with openings, such that openings have exits that are shifted from center axes of openings |
| JP4883102B2 (en) * | 2009-02-05 | 2012-02-22 | 株式会社デンソー | Fuel injection nozzle |
| CN103717875B (en) * | 2011-08-08 | 2016-03-23 | 三菱电机株式会社 | Fuelinjection nozzle |
-
2012
- 2012-06-18 JP JP2012136647A patent/JP2014001660A/en active Pending
-
2013
- 2013-06-14 EP EP13171964.3A patent/EP2677158B1/en active Active
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS5987271A (en) * | 1982-11-09 | 1984-05-19 | Yanmar Diesel Engine Co Ltd | Fuel injection valve for diesel engine |
| JPH0735002A (en) * | 1993-07-27 | 1995-02-03 | Shin A C Ii:Kk | Fuel injection nozzle of direct injection type diesel engine |
| JP2003506626A (en) * | 1999-08-11 | 2003-02-18 | ローベルト ボツシユ ゲゼルシヤフト ミツト ベシユレンクテル ハフツング | Fuel injection valve and method for manufacturing a discharge opening of the valve |
| JP2008064094A (en) * | 2006-09-05 | 2008-03-21 | Robert Bosch Gmbh | Fuel injection valve |
| JP2009243323A (en) * | 2008-03-31 | 2009-10-22 | Hitachi Ltd | Fuel injection valve and method for processing orifice |
| JP2009270448A (en) * | 2008-05-01 | 2009-11-19 | Mitsubishi Electric Corp | Fuel injection valve |
| JP2011001864A (en) * | 2009-06-18 | 2011-01-06 | Hitachi Automotive Systems Ltd | Fuel injection valve |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2015135062A (en) * | 2014-01-16 | 2015-07-27 | 株式会社日本自動車部品総合研究所 | fuel injection valve |
| JP2018053846A (en) * | 2016-09-30 | 2018-04-05 | 日立オートモティブシステムズ株式会社 | Fuel injection valve, control device for fuel injection valve, and control method |
| US10995655B2 (en) | 2016-11-30 | 2021-05-04 | Hitachi Automotive Systems, Ltd. | Fuel injection device |
| KR20220051404A (en) | 2019-09-25 | 2022-04-26 | 봇슈 가부시키가이샤 | Fuel injection valve and internal combustion engine with fuel injection valve |
| US11815057B2 (en) | 2019-09-25 | 2023-11-14 | Bosch Corporation | Fuel injector and internal combustion engine including fuel injector |
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| EP2677158B1 (en) | 2016-12-21 |
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