JP2011196214A - Direct injection type combustion chamber of diesel engine - Google Patents
Direct injection type combustion chamber of diesel engine Download PDFInfo
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- JP2011196214A JP2011196214A JP2010062376A JP2010062376A JP2011196214A JP 2011196214 A JP2011196214 A JP 2011196214A JP 2010062376 A JP2010062376 A JP 2010062376A JP 2010062376 A JP2010062376 A JP 2010062376A JP 2011196214 A JP2011196214 A JP 2011196214A
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
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Abstract
Description
本発明は、ディーゼルエンジンの直接噴射式燃焼室に関し、詳しくは、燃料噴射時のキャビティ内での燃料の気化状態を均一化することができるディーゼルエンジンの直接噴射式燃焼室に関する。 The present invention relates to a direct injection combustion chamber of a diesel engine, and more particularly, to a direct injection combustion chamber of a diesel engine capable of uniformizing a fuel vaporization state in a cavity during fuel injection.
従来、ディーゼルエンジンの直接噴射式燃焼室として、シリンダ内にピストンを摺動自在に内嵌させ、ピストンの頂部にキャビティを設け、シリンダヘッドに燃料インジェクタを配置し、燃料インジェクタの先端部に周方向に所定間隔を保持して複数の燃料噴射孔を設け、シリンダの所定の径方向を前後方向とし、その一方を前側、他方を後側として、燃料インジェクタの先端部をキャビティの中心軸線よりも後寄りに偏倚させ、燃料インジェクタの中心軸線を前方下り傾斜させ、各燃料噴射孔からの燃料噴射時に、各噴射軸線がキャビティの内面に向かうようにするに当たり、燃料インジェクタの中心軸線の先端側延長線と前寄りの燃料噴射孔の噴射軸線との挟角よりも、後寄りの燃料噴射孔の噴射軸線との挟角を大きく設定して、前寄りの燃料噴射孔の噴射軸線がキャビティの内面の前寄りに向けられ、後寄りの燃料噴射孔の噴射軸線がキャビティの内面の後寄りに向けられるようにしたものがある。
この種の直接噴射式燃焼室によれば、燃料インジェクタからキャビティの前後寄りに分配して噴射した燃料がキャビティ内の圧縮空気の熱やキャビティの内面の熱を受け、気化して、空気と燃料の混合気が形成され、自発火が起こり、燃焼がスムーズに進行する利点がある。
また、この種の直接噴射式燃焼室では、前寄りの燃料噴射孔からキャビティの前寄りに噴射される燃料は、燃料インジェクタの中心軸線の先端側延長線と燃料噴射孔の噴射軸線との挟角が小さいため、流通抵抗が小さい分だけ噴射速度が速く、霧化が促進されるのに対し、後寄りの燃料噴射孔からキャビティの後寄りに噴射される燃料は、燃料インジェクタの中心軸線の先端側延長線と燃料噴射孔の噴射軸線との挟角が大きい分だけ流通抵抗が大きく、噴射速度が遅く、霧化が停滞する傾向がある。
しかし、この従来技術では、キャビティ後寄りに噴射した燃料の気化を促進する手段がないため、問題がある。
Conventionally, as a direct injection combustion chamber of a diesel engine, a piston is slidably fitted into a cylinder, a cavity is provided at the top of the piston, a fuel injector is disposed at the cylinder head, and a circumferential direction is provided at the tip of the fuel injector. A plurality of fuel injection holes are provided at predetermined intervals, the predetermined radial direction of the cylinder is the front-rear direction, one of which is the front side and the other is the rear side, and the tip of the fuel injector is located behind the central axis of the cavity. The center axis of the fuel injector is inclined forward and downward, and when the fuel is injected from each fuel injection hole, each injection axis is directed toward the inner surface of the cavity. Set the angle between the rear fuel injection hole and the injection axis of the front fuel injection hole to be larger than the front angle. Is injection axis of the fuel injection hole is directed to the front portion of the inner surface of the cavity, the injection axis of the post near the fuel injection hole is that as directed to deviation after the inner surface of the cavity.
According to this type of direct injection combustion chamber, the fuel distributed and injected from the fuel injector to the front and rear sides of the cavity receives the heat of the compressed air in the cavity and the heat of the inner surface of the cavity, and is vaporized. There is an advantage that the mixture is formed, self-ignition occurs, and combustion proceeds smoothly.
In this type of direct injection combustion chamber, the fuel injected from the front fuel injection hole to the front of the cavity is sandwiched between the extension line on the front end side of the central axis of the fuel injector and the injection axis of the fuel injection hole. Because the angle is small, the injection speed is high and the atomization is accelerated by the small flow resistance, whereas the fuel injected from the rear fuel injection hole to the rear of the cavity is in the center axis of the fuel injector. There is a tendency that the flow resistance is large, the injection speed is slow, and the atomization is stagnated as the angle between the distal end side extension line and the injection axis of the fuel injection hole is large.
However, this conventional technique has a problem because there is no means for promoting the vaporization of the fuel injected toward the rear of the cavity.
《問題》 燃料噴射時のキャビティ内での燃料の気化状態が不均一になりやすい。
キャビティ後寄りに噴射した燃料の気化を促進する手段がないため、霧化が停滞する後寄りの燃料の気化が遅れ、燃料噴射時のキャビティ内での燃料の気化状態が不均一になりやすい。
これにより、出力低下、燃費悪化、排ガス悪化等の問題が生じる。
<Problem> The fuel vaporization state in the cavity during fuel injection tends to be uneven.
Since there is no means for promoting the vaporization of the fuel injected toward the rear of the cavity, the vaporization of the rear fuel where the atomization stagnates is delayed, and the vaporization state of the fuel in the cavity during fuel injection tends to be uneven.
As a result, problems such as output reduction, fuel consumption deterioration, and exhaust gas deterioration occur.
本発明の課題は、燃料噴射時のキャビティ内での燃料の気化状態を均一化することができるディーゼルエンジンの直接噴射式燃焼室を提供することにある。 An object of the present invention is to provide a direct injection combustion chamber of a diesel engine that can uniformize the vaporization state of fuel in a cavity during fuel injection.
請求項1に係る発明の発明特定事項は、次の通りである。
図1(A)〜(C)に例示するように、シリンダ(1)内にピストン(2)を摺動自在に内嵌させ、ピストン(2)の頂部にキャビティ(3)を設け、シリンダヘッド(4)に燃料インジェクタ(5)を配置し、燃料インジェクタ(5)の先端部に周方向に所定間隔を保持して複数の燃料噴射孔(6)を設け、
図1(A)(B)に例示するように、シリンダ(1)の所定の径方向を前後方向とし、その一方を前側、他方を後側として、
燃料インジェクタ(5)の先端部をキャビティ(3)の中心軸線(3b)よりも後寄りに偏倚させ、燃料インジェクタ(5)の中心軸線(5a)を前方下死点寄りに傾斜させ、各燃料噴射孔(6)からの燃料噴射時に、各噴射軸線(6a)がキャビティ(3)の内面に向かうようにするに当たり、
図1(B)に例示するように、燃料インジェクタ(5)の中心軸線(5a)の先端側延長線(5b)と前寄りの燃料噴射孔(6)の噴射軸線(6a)との挟角よりも、後寄りの燃料噴射孔(6)の噴射軸線(6a)との挟角を大きく設定して、前寄りの燃料噴射孔(6)の噴射軸線(6a)がキャビティ(3)の内面の前寄りに向けられ、後寄りの燃料噴射孔(6)の噴射軸線(6a)がキャビティ(3)の内面の後寄りに向けられるようにした、ディーゼルエンジンの直接噴射式燃焼室において、
図1(B)に例示するように、キャビティ(3)の内底面(3a)の後寄りに隆起部(15)を設け、この隆起部(15)の後面に左右方向に長い後寄りタンブル吸気流ガイド面(16)を形成した、ことを特徴とするディーゼルエンジンの直接噴射式燃焼室。
Invention specific matters of the invention according to
As illustrated in FIGS. 1A to 1C, a piston (2) is slidably fitted in a cylinder (1), a cavity (3) is provided at the top of the piston (2), and a cylinder head is provided. (4), a fuel injector (5) is disposed, and a plurality of fuel injection holes (6) are provided at the tip of the fuel injector (5) at predetermined intervals in the circumferential direction.
As illustrated in FIGS. 1A and 1B, a predetermined radial direction of the cylinder (1) is a front-rear direction, one of which is a front side and the other is a rear side.
The tip of the fuel injector (5) is biased to the rear of the center axis (3b) of the cavity (3), and the center axis (5a) of the fuel injector (5) is inclined toward the front bottom dead center. When injecting fuel from the injection hole (6), each injection axis (6a) is directed toward the inner surface of the cavity (3).
As illustrated in FIG. 1B, the included angle between the distal end extension line (5b) of the central axis (5a) of the fuel injector (5) and the injection axis (6a) of the front fuel injection hole (6). The angle between the rear fuel injection hole (6) and the injection axis (6a) is set larger, and the front fuel injection hole (6) has the injection axis (6a) as the inner surface of the cavity (3). In the direct injection combustion chamber of the diesel engine, the injection axis (6a) of the rear fuel injection hole (6) is directed to the rear of the inner surface of the cavity (3).
As illustrated in FIG. 1B, a raised portion (15) is provided on the rear side of the inner bottom surface (3a) of the cavity (3), and a rearward tumble intake air that is long in the left-right direction is provided on the rear surface of the raised portion (15). A direct injection combustion chamber of a diesel engine, characterized in that a flow guide surface (16) is formed.
(請求項1に係る発明)
請求項1に係る発明は、次の効果を奏する。
《効果》 燃焼時のキャビティ内での燃料の気化状態を均一化することができる。
図1(B)に例示するように、キャビティ(3)の内底面(3a)の後寄りに隆起部(15)を設け、この隆起部(15)の後面に左右方向に伸びる後寄りタンブル吸気流ガイド面(16)を形成したので、ピストン(2)の上昇時に発生する後側タンブル吸気流(18)が、後寄りタンブル吸気流ガイド面(16)とこれに対向するキャビティ(3)の内周面(3c)との間の狭い短経路の空間で、数多く旋回し、霧化が停滞する後寄りの燃料の気化が促進され、その気化状態が前寄りの燃料の気化状態に近づき、燃料噴射時のキャビティ(3)内での燃料の気化状態を均一化することができる。
これにより、出力向上、燃費改善、排ガス改善を図ることができる。
(Invention of Claim 1)
The invention according to
<< Effect >> The vaporization state of the fuel in the cavity during combustion can be made uniform.
As illustrated in FIG. 1 (B), a raised portion (15) is provided on the rear side of the inner bottom surface (3a) of the cavity (3), and a rearward tumble intake air extending in the left-right direction on the rear surface of the raised portion (15). Since the flow guide surface (16) is formed, the rear tumble intake air flow (18) generated when the piston (2) rises is caused by the rear tumble intake air flow guide surface (16) and the cavity (3) opposed thereto. In the space of a narrow short path between the inner peripheral surface (3c), the vaporization of the rear fuel where the atomization stops and the atomization stops is promoted, the vaporization state approaches the vaporization state of the front fuel, The fuel vaporization state in the cavity (3) at the time of fuel injection can be made uniform.
Thereby, output improvement, fuel consumption improvement, and exhaust gas improvement can be aimed at.
(請求項2に係る発明)
請求項2に係る発明は、請求項1に係る発明の効果に加え、次の効果を奏する。
《効果》 燃焼噴射時のキャビティ内での燃料気化状態をより均一化することができる。
図1(B)に例示するように、後寄りタンブル吸気流ガイド面(16)とこれに対向するキャビティ(3)の内周面(3c)との離間距離を、前寄りタンブル吸気流ガイド面(17)とこれに対向するキャビティ(3)の内周面(3c)との離間距離よりも小さくし、後寄りタンブル吸気流ガイド面(16)の曲率を、前寄りタンブル吸気流ガイド面(17)の曲率よりも大きくしたので、ピストン(2)の上昇時に発生する前側タンブル吸気流(19)が、前寄りタンブル吸気流ガイド面(17)とこれに対向するキャビティ(3)の内周面(3c)との間の広い長経路の空間で、数少なく旋回し、霧化が促進されている前寄りの燃料の気化を抑制し、その気化状態を後寄りの燃料の気化状態と合致させ、燃料噴射時のキャビティ(3)内での燃料気化状態をより均一化することができる。
(Invention of Claim 2)
The invention according to
<< Effect >> The fuel vaporization state in the cavity at the time of combustion injection can be made more uniform.
As illustrated in FIG. 1B, the separation distance between the rear tumble intake flow guide surface (16) and the inner peripheral surface (3c) of the cavity (3) facing the rear tumble intake flow guide surface is defined as the front tumble intake flow guide surface. The curvature of the rear tumble intake flow guide surface (16) is made smaller than the separation distance between (17) and the inner peripheral surface (3c) of the cavity (3) opposite to the front tumble intake flow guide surface ( 17), the front tumble intake air flow (19) generated when the piston (2) ascends causes the front tumble intake air flow guide surface (17) and the inner periphery of the cavity (3) opposite to the front tumble intake air flow guide surface (17). In a space with a wide long path with the surface (3c), it turns a few, suppresses the vaporization of the front fuel where atomization is promoted, and matches the vaporization state with the vaporization state of the rear fuel The fuel vaporization state in the cavity (3) during fuel injection can be made more uniform. That.
図1〜図2は本発明の実施形態に係るディーゼルエンジンの直接噴射式燃焼室を説明する図である。 1 to 2 are views for explaining a direct injection combustion chamber of a diesel engine according to an embodiment of the present invention.
図1(A)〜(C)に示すように、シリンダ(1)内にピストン(2)を摺動自在に内嵌させ、ピストン(2)の頂部にキャビティ(3)を設け、シリンダヘッド(4)に燃料インジェクタ(5)を配置し、燃料インジェクタ(5)の先端部に周方向に所定間隔を保持して複数の燃料噴射孔(6)を設けている。 As shown in FIGS. 1A to 1C, a piston (2) is slidably fitted into a cylinder (1), a cavity (3) is provided at the top of the piston (2), and a cylinder head ( 4), a fuel injector (5) is arranged, and a plurality of fuel injection holes (6) are provided at a distal end portion of the fuel injector (5) at a predetermined interval in the circumferential direction.
図1(A)〜(C)に示すように、キャビティ(3)は周壁が円筒形のトロイダル形であるが、開口部(3b)を絞ったリエントラント形であってもよい。キャビティ(3)の中心軸線(3b)はシリンダ(1)の中心軸線(1a)よりも後寄りに偏倚させている。燃料インジェクタ(5)の先端部も、キャビティ(3)の中心軸線(3b)と同様、シリンダ(1)の中心軸線(1a)よりも後寄りに偏倚させている。
図2(A)〜(C)に示すように、燃料インジェクタ(5)の先端部にノズル(10)を設け、ノズル(10)内に開弁作動室(11)と燃料分流室(12)とを設け、開弁作動室(11)と燃料分流室(12)との境界に弁座(13)を設け、弁座(13)にノズルスプリング(図外)で付勢した針弁(14)を着座させ、燃料分流室(12)から複数の燃料噴射孔(6)を導出している。燃料噴射ポンプ(図外)から開弁作動室(11)に燃料を圧送すると、ノズルスプリングの付勢力に抗して針弁(14)が開弁され、燃料が開弁作動室(11)と燃料分流室(12)とを介して複数の燃料噴射孔(6)から同時に噴射される。
図2(B)に示すように、燃料噴射孔(6)は燃料インジェクタ(5)の先端部の全周に等間隔で複数配置し、燃料インジェクタ(5)の中心軸線(5a)と平行な向きに見て、燃料噴射孔(6)の噴射軸線(6a)は燃料インジェクタ(5)の中心軸線(5a)から放射する向きに向けている。具体的には、燃料噴射孔(6)は燃料インジェクタ(5)の先端部の全周に90°毎に合計4個配置されている。
As shown in FIGS. 1A to 1C, the cavity (3) has a toroidal shape with a cylindrical peripheral wall, but may have a reentrant shape with a narrowed opening (3b). The central axis (3b) of the cavity (3) is biased rearward from the central axis (1a) of the cylinder (1). The tip of the fuel injector (5) is also biased rearward from the central axis (1a) of the cylinder (1), as is the central axis (3b) of the cavity (3).
As shown in FIGS. 2 (A) to (C), a nozzle (10) is provided at the tip of the fuel injector (5), and a valve opening working chamber (11) and a fuel branch chamber (12) are provided in the nozzle (10). A valve seat (13) is provided at the boundary between the valve opening working chamber (11) and the fuel flow dividing chamber (12), and a needle valve (14) energized by a nozzle spring (not shown) is provided on the valve seat (13). ) And a plurality of fuel injection holes (6) are led out from the fuel diversion chamber (12). When fuel is pumped from the fuel injection pump (not shown) to the valve opening working chamber (11), the needle valve (14) is opened against the urging force of the nozzle spring, and the fuel is opened to the valve opening working chamber (11). The fuel is simultaneously injected from the plurality of fuel injection holes (6) through the fuel diversion chamber (12).
As shown in FIG. 2 (B), a plurality of fuel injection holes (6) are arranged at equal intervals on the entire circumference of the tip of the fuel injector (5), and are parallel to the central axis (5a) of the fuel injector (5). Looking in the direction, the injection axis (6a) of the fuel injection hole (6) is directed to radiate from the central axis (5a) of the fuel injector (5). Specifically, a total of four fuel injection holes (6) are arranged every 90 ° on the entire circumference of the tip of the fuel injector (5).
図1(B)に示すように、シリンダ(1)の所定の径方向を前後方向とし、その一方を前側、他方を後側として、燃料インジェクタ(5)の先端部をキャビティ(3)の中心軸線(3b)よりも後寄りに偏倚させ、燃料インジェクタ(5)の中心軸線(5a)を前方下死点寄りに傾斜させ、各燃料噴射孔(6)からの燃料噴射時に、各噴射軸線(6a)がキャビティ(3)の内面に向かうようにするに当たり、次のようにしている。 As shown in FIG. 1B, the predetermined radial direction of the cylinder (1) is the front-rear direction, one of which is the front side and the other is the rear side, and the tip of the fuel injector (5) is the center of the cavity (3). The center axis (5a) of the fuel injector (5) is inclined closer to the front bottom dead center than the axis (3b), and when the fuel is injected from each fuel injection hole (6), each injection axis ( 6a) is directed to the inner surface of the cavity (3) as follows.
図2(A)に示すように、燃料インジェクタ(5)の中心軸線(5a)の先端側延長線(5b)と前寄りの燃料噴射孔(6)の噴射軸線(6a)との挟角よりも、後寄りの燃料噴射孔(6)の噴射軸線(6a)との挟角を大きく設定して、前寄りの燃料噴射孔(6)の噴射軸線(6a)がキャビティ(3)の内面の前寄りに向けられ、後寄りの燃料噴射孔(6)の噴射軸線(6a)がキャビティ(3)の内面の後寄りに向けられるようにしている。
図1(A)〜(C)中で、各噴射軸線(6a)の先端に示す点は、各噴射軸線(6a)とキャビティ(3)の内底面(3a)との交点である。
As shown in FIG. 2 (A), the angle between the extension line (5b) at the front end of the central axis (5a) of the fuel injector (5) and the injection axis (6a) of the front fuel injection hole (6). Also, the angle between the rear fuel injection hole (6) and the injection axis (6a) is set to be large so that the front fuel injection hole (6) has the injection axis (6a) on the inner surface of the cavity (3). The injection axis (6a) of the rear fuel injection hole (6) is directed toward the front and is directed toward the rear of the inner surface of the cavity (3).
1A to 1C, the point shown at the tip of each
図1(B)に示すように、シリンダ中心軸線(1a)に対して燃料インジェクタ(5)の中心軸線(5a)は60°の角度で傾斜させ、図2(A)(C)に示すように、燃料インジェクタ(5)の中心軸線(5a)の先端側延長線(5b)と各燃料噴射孔(6)の噴射軸線(6a)との挟角は、前側が30°、後側が90°、横側が45°に設定している。 As shown in FIG. 1 (B), the central axis (5a) of the fuel injector (5) is inclined at an angle of 60 ° with respect to the cylinder central axis (1a), as shown in FIGS. 2 (A) and (C). In addition, the included angle between the tip extension line (5b) of the central axis (5a) of the fuel injector (5) and the injection axis (6a) of each fuel injection hole (6) is 30 ° on the front side and 90 ° on the rear side. The horizontal side is set to 45 °.
図1(B)に示すように、キャビティ(3)の内底面(3a)の後寄りに隆起部(15)を設け、この隆起部(15)の後面に左右方向に伸びる後寄りタンブル吸気流ガイド面(16)を形成している。
図1(A)中の矢印(16)は、スワール吸気流である。このスワール吸気流(16)は吸気スワールポート(図外)による吸気の導入により、キャビティ(3)内に形成される。
As shown in FIG. 1 (B), a raised portion (15) is provided on the rear side of the inner bottom surface (3a) of the cavity (3), and a rearward tumble intake flow extending in the left-right direction on the rear surface of the raised portion (15). A guide surface (16) is formed.
An arrow (16) in FIG. 1 (A) indicates a swirl intake flow. This swirl intake flow (16) is formed in the cavity (3) by the introduction of intake air through the intake swirl port (not shown).
図2(B)に示すように、後寄りタンブル吸気流ガイド面(16)は、横側から見て、後方に行くほど下死点寄りの円弧状に形成し、隆起部(15)の前面に左右方向に長い前寄りタンブル吸気流ガイド面(17)を形成し、この前寄りタンブル吸気流ガイド面(17)は、横側から見て、前方に行くほど下死点寄りの円弧状に形成し、後寄りタンブル吸気流ガイド面(16)とこれに対向するキャビティ(3)の内周面(3c)との離間距離を、前寄りタンブル吸気流ガイド面(17)とこれに対向するキャビティ(3)の内周面(3c)との離間距離よりも小さくし、後寄りタンブル吸気流ガイド面(16)の曲率を、前寄りタンブル吸気流ガイド面(17)の曲率よりも大きくしている。 As shown in FIG. 2 (B), the rear tumble intake flow guide surface (16) is formed in an arc shape closer to the bottom dead center as viewed from the side, and the front surface of the raised portion (15). The front tumble intake flow guide surface (17) that is long in the left-right direction is formed, and the front tumble intake flow guide surface (17) has an arc shape that is closer to the bottom dead center as it goes forward as viewed from the side. The separation distance between the rear tumble intake flow guide surface (16) and the inner peripheral surface (3c) of the cavity (3) facing the rear tumble intake flow guide surface (17) is opposed to the front tumble intake flow guide surface (17). The curvature of the rear tumble intake flow guide surface (16) is made larger than the curvature of the front tumble intake flow guide surface (17) by making it smaller than the distance from the inner peripheral surface (3c) of the cavity (3). ing.
(1) シリンダ
(1a) シリンダ中心軸線
(2) ピストン
(3) キャビティ
(3a) 内底面
(3b) キャビティの中心軸線
(3c) キャビティの内周面
(4) シリンダヘッド
(5) 燃料インジェクタ
(5a) 中心軸線
(5b) 先端側延長線
(6) 燃料噴射孔
(6a) 噴射軸線
(15) 隆起部
(16) 後側タンブル吸気流ガイド面
(17) 前側タンブル吸気流ガイド面
(1) Cylinder
(1a) Cylinder center axis
(2) Piston
(3) Cavity
(3a) Inner bottom
(3b) Cavity center axis
(3c) Cavity inner surface
(4) Cylinder head
(5) Fuel injector
(5a) Center axis
(5b) Extension line on the tip side
(6) Fuel injection hole
(6a) Injection axis
(15) Raised part
(16) Rear tumble intake flow guide surface
(17) Front tumble intake flow guide surface
Claims (2)
シリンダ(1)の所定の径方向を前後方向とし、その一方を前側、他方を後側として、
燃料インジェクタ(5)の先端部をキャビティ(3)の中心軸線(3b)よりも後寄りに偏倚させ、燃料インジェクタ(5)の中心軸線(5a)を前方下死点寄りに傾斜させ、各燃料噴射孔(6)からの燃料噴射時に、各噴射軸線(6a)がキャビティ(3)の内面に向かうようにするに当たり、
燃料インジェクタ(5)の中心軸線(5a)の先端側延長線(5b)と前寄りの燃料噴射孔(6)の噴射軸線(6a)との挟角よりも、後寄りの燃料噴射孔(6)の噴射軸線(6a)との挟角を大きく設定して、前寄りの燃料噴射孔(6)の噴射軸線(6a)がキャビティ(3)の内面の前寄りに向けられ、後寄りの燃料噴射孔(6)の噴射軸線(6a)がキャビティ(3)の内面の後寄りに向けられるようにした、ディーゼルエンジンの直接噴射式燃焼室において、
キャビティ(3)の内底面(3a)の後寄りに隆起部(15)を設け、この隆起部(15)の後面に左右方向に長い後寄りタンブル吸気流ガイド面(16)を形成した、ことを特徴とするディーゼルエンジンの直接噴射式燃焼室。 A piston (2) is slidably fitted in the cylinder (1), a cavity (3) is provided at the top of the piston (2), a fuel injector (5) is disposed on the cylinder head (4), and a fuel injector A plurality of fuel injection holes (6) are provided at the tip of (5) at predetermined intervals in the circumferential direction,
The predetermined radial direction of the cylinder (1) is the front-rear direction, one of which is the front side and the other is the rear side.
The tip of the fuel injector (5) is biased to the rear of the center axis (3b) of the cavity (3), and the center axis (5a) of the fuel injector (5) is inclined toward the front bottom dead center. When injecting fuel from the injection hole (6), each injection axis (6a) is directed toward the inner surface of the cavity (3).
The fuel injection hole (6) located at the rear of the fuel injector (5) is located closer to the rear side than the angle between the extension line (5b) at the front end of the central axis (5a) of the fuel injector (5a) and the injection axis (6a) ) With the injection axis (6a) is set large, the injection axis (6a) of the front fuel injection hole (6) is directed toward the front of the inner surface of the cavity (3), and the rear fuel In a direct injection combustion chamber of a diesel engine in which the injection axis (6a) of the injection hole (6) is directed toward the rear of the inner surface of the cavity (3),
A raised portion (15) is provided on the rear side of the inner bottom surface (3a) of the cavity (3), and a rearward tumble intake flow guide surface (16) that is long in the left-right direction is formed on the rear surface of the raised portion (15). A diesel engine direct injection combustion chamber.
後寄りタンブル吸気流ガイド面(16)は、横側から見て、後方に行くほど下死点寄りの円弧状に形成し、
隆起部(15)の前面に左右方向に長い前寄りタンブル吸気流ガイド面(17)を形成し、この前寄りタンブル吸気流ガイド面(17)は、横側から見て、前方に行くほど下死点寄りの円弧状に形成し、
後寄りタンブル吸気流ガイド面(16)とこれに対向するキャビティ(3)の内周面(3c)との離間距離を、前寄りタンブル吸気流ガイド面(17)とこれに対向するキャビティ(3)の内周面(3c)との離間距離よりも小さくし、
後寄りタンブル吸気流ガイド面(16)の曲率を、前寄りタンブル吸気流ガイド面(17)の曲率よりも大きくした、ことを特徴とするディーゼルエンジンの直接噴射式燃焼室。
In the direct injection combustion chamber of the diesel engine according to claim 1,
The rear tumble intake flow guide surface (16) is formed in an arc shape closer to the bottom dead center as it goes rearward as viewed from the side,
A front tumble intake flow guide surface (17) that is long in the left-right direction is formed on the front surface of the raised portion (15), and the front tumble intake flow guide surface (17) is lowered toward the front as viewed from the side. Formed in an arc shape near the dead center,
The separation distance between the rear tumble intake flow guide surface (16) and the inner peripheral surface (3c) of the cavity (3) opposed to the rear tumble intake flow guide surface (16) is defined as the cavity (3 ) Smaller than the distance from the inner peripheral surface (3c),
A direct injection combustion chamber of a diesel engine, characterized in that the curvature of the rear tumble intake flow guide surface (16) is larger than the curvature of the front tumble intake flow guide surface (17).
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DE102015005469A1 (en) * | 2015-04-29 | 2016-11-03 | Caterpillar Motoren Gmbh & Co. Kg | PISTON CROWN WITH PISTON BOTTLE |
CN108590879A (en) * | 2018-05-29 | 2018-09-28 | 重庆隆鑫发动机有限公司 | Heavy fuel burning engine piston and aero-engine |
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JPS5257105U (en) * | 1975-10-23 | 1977-04-25 | ||
JPS5525522A (en) * | 1978-08-11 | 1980-02-23 | Hino Motors Ltd | Combustion chamber in direct injection type diesel engine |
JPS5872424U (en) * | 1981-11-11 | 1983-05-17 | ヤンマーディーゼル株式会社 | Three-valve direct injection internal combustion engine |
JPS62282117A (en) * | 1986-05-30 | 1987-12-08 | Isuzu Motors Ltd | Direct injection type internal combustion engine |
JPS6342826U (en) * | 1986-09-08 | 1988-03-22 |
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JPS5257105U (en) * | 1975-10-23 | 1977-04-25 | ||
JPS5525522A (en) * | 1978-08-11 | 1980-02-23 | Hino Motors Ltd | Combustion chamber in direct injection type diesel engine |
JPS5872424U (en) * | 1981-11-11 | 1983-05-17 | ヤンマーディーゼル株式会社 | Three-valve direct injection internal combustion engine |
JPS62282117A (en) * | 1986-05-30 | 1987-12-08 | Isuzu Motors Ltd | Direct injection type internal combustion engine |
JPS6342826U (en) * | 1986-09-08 | 1988-03-22 |
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DE102015005469A1 (en) * | 2015-04-29 | 2016-11-03 | Caterpillar Motoren Gmbh & Co. Kg | PISTON CROWN WITH PISTON BOTTLE |
CN108590879A (en) * | 2018-05-29 | 2018-09-28 | 重庆隆鑫发动机有限公司 | Heavy fuel burning engine piston and aero-engine |
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