JP2007192186A - Internal combustion engine and its piston - Google Patents

Internal combustion engine and its piston Download PDF

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JP2007192186A
JP2007192186A JP2006013271A JP2006013271A JP2007192186A JP 2007192186 A JP2007192186 A JP 2007192186A JP 2006013271 A JP2006013271 A JP 2006013271A JP 2006013271 A JP2006013271 A JP 2006013271A JP 2007192186 A JP2007192186 A JP 2007192186A
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piston
valve side
intake valve
internal combustion
combustion engine
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JP4785539B2 (en
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Taizo Horigome
泰三 堀込
Masayuki Tomita
全幸 富田
Tsutomu Kikuchi
勉 菊池
Taro Sakai
太朗 酒井
Shinichi Okamoto
慎一 岡本
Makoto Yoshida
吉田  誠
Masahiko Inoue
雅彦 井上
Yusuke Kihara
裕介 木原
Takashi Ide
隆 井出
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Hitachi Ltd
Nissan Motor Co Ltd
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Hitachi Ltd
Nissan Motor Co Ltd
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    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00Road transport of goods or passengers
    • Y02T10/10Internal combustion engine [ICE] based vehicles
    • Y02T10/12Improving ICE efficiencies

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Abstract

<P>PROBLEM TO BE SOLVED: To improve combustion stability by forming an air-fuel mixture in the vicinity of an ignition plug stably and to minimize reduction of tumbling flow. <P>SOLUTION: A bottom face 25 of a substantially rectangular recessed part 22 on a crown face of a piston 4 forms a curved face being substantially parallel with a central axis of a piston pin along the tumbling flow. A step part 27 being parallel with the central axis of the piston pin is formed in a substantially central part of the bottom face 25 just below the ignition plug, and a rising part 27a is formed on an intake valve side. A rising stream going upward occurs when a spray passes above the step part 27 at stratified lean combustion time, and a part of the spray is guided onto an upper ignition plug side, thereby achieving stable combustion. Since cut-out parts 28, 28 are provided at both ends of the step part 27 and the bottom face 25 is continuous without a step, flow of the tumbling flow at homogeneous combustion time is not obstructed. <P>COPYRIGHT: (C)2007,JPO&INPIT

Description

この発明は、タンブル流を利用した筒内直接噴射式内燃機関に用いられるピストンに関する。   The present invention relates to a piston used in a direct injection type internal combustion engine using a tumble flow.

シリンダ内のガス流動としてタンブル流を利用した内燃機関において、吸気行程において生じたタンブル流が圧縮行程においても良好に保存されるように、ピストン冠面に、ピストンピン中心軸線と平行な円筒面を凹設したピストンが、例えば特許文献1に開示されている。このような構成によれば、シリンダヘッド側に凹設された燃焼室凹部との間で、ピストンピン軸方向から見て、円形ないしは楕円形の空間が形成され、シリンダの上下方向に沿ったタンブル流が円滑に旋回するようになる。
特開2000−186556号公報
In an internal combustion engine using a tumble flow as the gas flow in the cylinder, a cylindrical surface parallel to the piston pin central axis is provided on the piston crown so that the tumble flow generated in the intake stroke is well preserved in the compression stroke. A recessed piston is disclosed in Patent Document 1, for example. According to such a configuration, a circular or elliptical space is formed between the combustion chamber recess recessed on the cylinder head side when viewed from the piston pin axial direction, and the tumble along the vertical direction of the cylinder is formed. The flow turns smoothly.
JP 2000-186556 A

筒内直接噴射式内燃機関では、一般に、圧縮行程後期に燃料を噴射することで成層希薄燃焼を実現するのであるが、上記のようなピストンを用いた構成では、シリンダ側方に配置した燃料噴射弁から噴射された燃料噴霧を点火プラグの電極部へ安定的に案内することが難しく、燃焼が安定しない。従って、例えば始動直後のHC低減のために点火時期をリタードしようとしても、燃焼安定限界の制約によって大幅なリタードが困難となる。   In a direct injection internal combustion engine, in general, stratified lean combustion is realized by injecting fuel in the latter half of the compression stroke. However, in the configuration using the piston as described above, the fuel injection disposed on the side of the cylinder is performed. It is difficult to stably guide the fuel spray injected from the valve to the electrode part of the spark plug, and the combustion is not stable. Therefore, for example, even if an attempt is made to retard the ignition timing in order to reduce HC immediately after start-up, significant retarding becomes difficult due to restrictions on the combustion stability limit.

また、燃料噴霧を点火プラグ近傍へ供給するために、燃料噴霧をピストン冠面に衝突させて点火プラグ側へ反射させるような構成とすると、燃料の一部がピストン冠面に付着し、HC増加の要因となる。   In addition, in order to supply the fuel spray to the vicinity of the spark plug, if the fuel spray collides with the piston crown surface and reflects to the spark plug side, a part of the fuel adheres to the piston crown surface and the HC increases. It becomes a factor of.

この発明は、シリンダ頂面の略中心部に点火プラグが配置されるとともに、吸気弁側の燃焼室側方に燃料噴射弁が配置されてなる筒内直接噴射式内燃機関に用いられるピストンであって、ピストン冠面に、シリンダ内のタンブル流に沿うように、ピストンピン中心軸線と略平行な湾曲面が凹設されてなる内燃機関のピストンにおいて、上記点火プラグの直下付近となる上記湾曲面の略中央部に、該湾曲面の吸気弁側部分から立ち上がる吸気弁側の立ち上がり部を形成するように、ピストンピン中心軸線と平行に延びた突条部もしくは段部が設けられている。そして、この突条部もしくは段部は、両端部が切り欠かれており、この切欠部分では、湾曲面の吸気弁側部分と排気弁側部分とが滑らかに連続している。   The present invention relates to a piston used in a direct injection type internal combustion engine in which a spark plug is disposed substantially at the center of a cylinder top surface and a fuel injection valve is disposed on the side of the combustion chamber on the intake valve side. In the piston of the internal combustion engine in which a curved surface substantially parallel to the piston pin central axis is recessed along the tumble flow in the cylinder on the piston crown surface, the curved surface that is in the vicinity immediately below the spark plug A ridge or step extending in parallel to the piston pin central axis is provided at substantially the center of the curved surface so as to form a rising portion on the intake valve side rising from the intake valve side portion of the curved surface. Then, both ends of the protruding portion or stepped portion are notched, and the intake valve side portion and the exhaust valve side portion of the curved surface are smoothly continuous at the notch portion.

望ましくは、吸気弁側の立ち上がり部が上記点火プラグの直下付近に位置している。   Desirably, the rising portion on the intake valve side is located in the vicinity immediately below the spark plug.

具体的な一つの態様では、上記ピストン冠面の略全面に、シリンダヘッド側へ膨らんだ凸部が設けられ、この凸部のピストンピン軸方向の端部寄りの部分を残すように上記湾曲面が矩形状に凹設されている。   In one specific aspect, a convex portion that swells toward the cylinder head is provided on substantially the entire surface of the piston crown surface, and the curved surface is left so as to leave a portion of the convex portion close to the end in the piston pin axial direction. Is recessed in a rectangular shape.

そして、この矩形状の凹部の側壁面から離れて上記突条部もしくは段部が上記湾曲面の中に島状に形成されている。   And the said protrusion or step part is formed in the island shape in the said curved surface away from the side wall surface of this rectangular recessed part.

すなわち、上記のように突条部もしくは段部からなる立ち上がり部を備えた構成では、成層希薄燃焼のために圧縮行程後期に燃料を噴射したときに、立ち上がり部の上方を噴霧が通過することによって該立ち上がり部に沿って上方へ向かう上昇流が局部的に発生し、これに乗って、一部の噴霧が上方の点火プラグ側へ向かう。従って、点火プラグ近傍に適宜な混合気を安定的に形成でき、安定した燃焼が得られる。   That is, in the configuration provided with the rising portion consisting of the ridge portion or the step portion as described above, when the fuel is injected at the latter stage of the compression stroke for the stratified lean combustion, the spray passes above the rising portion. An upward flow upward along the rising portion is locally generated, and a part of the spray travels upward toward the spark plug. Accordingly, an appropriate air-fuel mixture can be stably formed in the vicinity of the spark plug, and stable combustion can be obtained.

一方、例えば多量の排気還流を行いつつ均質燃焼する場合などに、シリンダ内にタンブル流が生成されると、このタンブル流は、ピストン冠面の湾曲面に沿って旋回することになるが、突条部もしくは段部は両端部が切り欠かれているので、この両側の切欠部分を通してタンブル流が円滑に流れる。従って、突条部もしくは段部を設けたことによるタンブル流の低下が最小限のものとなる。   On the other hand, when a tumble flow is generated in the cylinder, for example, when homogeneous combustion is performed with a large amount of exhaust gas recirculation, the tumble flow swirls along the curved surface of the piston crown surface. Since both ends of the strip or step are notched, the tumble flow smoothly flows through the notches on both sides. Therefore, the decrease in the tumble flow due to the provision of the protrusion or step is minimized.

この発明によれば、シリンダ側方の燃料噴射弁から噴射された燃料噴霧を点火プラグの電極部へ安定的に案内することができ、安定した成層希薄燃焼が得られる。従って、例えば始動直後のHC低減のために点火時期をリタードするに際して、点火時期の燃焼安定限界がより遅角側となり、大幅な点火時期リタードが可能となる。また同時に、タンブル流の低下を最小限にできる。   According to this invention, the fuel spray injected from the fuel injection valve on the cylinder side can be stably guided to the electrode portion of the spark plug, and stable stratified lean combustion can be obtained. Therefore, for example, when the ignition timing is retarded to reduce HC immediately after starting, the combustion stability limit of the ignition timing becomes more retarded, and a large ignition timing retard is possible. At the same time, the tumble flow can be minimized.

以下、この発明の一実施例を図面に基づいて詳細に説明する。   Hereinafter, an embodiment of the present invention will be described in detail with reference to the drawings.

始めに、この発明のピストン4が用いられる筒内直接噴射式内燃機関の構成を図1に基づいて説明する。図示するように、シリンダブロック1には、複数のシリンダ3が直列に配置されており、その上面を覆うように、シリンダヘッド2が固定されている。上記シリンダ3内には、ピストン4が摺動可能に嵌合している。また、上記シリンダヘッド2に凹設された燃焼室11は、いわゆるペントルーフ型に構成されており、その一方の傾斜面に一対の吸気弁5が、他方の傾斜面に一対の排気弁6がそれぞれ配置されている。そして、これらの一対の吸気弁5および一対の排気弁6によって囲まれたシリンダ3の略中心位置に、点火プラグ7が配置されている。   First, the configuration of a direct injection type internal combustion engine in which the piston 4 of the present invention is used will be described with reference to FIG. As illustrated, a plurality of cylinders 3 are arranged in series on the cylinder block 1, and a cylinder head 2 is fixed so as to cover the upper surface thereof. A piston 4 is slidably fitted in the cylinder 3. The combustion chamber 11 recessed in the cylinder head 2 has a so-called pent roof type, and a pair of intake valves 5 are provided on one inclined surface, and a pair of exhaust valves 6 are provided on the other inclined surface. Has been placed. A spark plug 7 is disposed at a substantially central position of the cylinder 3 surrounded by the pair of intake valves 5 and the pair of exhaust valves 6.

上記シリンダヘッド2には、一対の吸気弁5にそれぞれ対応する一対の吸気ポート8が形成されているとともに、一対の排気弁6に対応して排気ポート9が形成されている。   The cylinder head 2 is formed with a pair of intake ports 8 corresponding to the pair of intake valves 5, and an exhaust port 9 corresponding to the pair of exhaust valves 6.

筒内へ直接に燃料を噴射する電磁式燃料噴射弁10は、吸気弁5側のシリンダ3側壁寄りのシリンダヘッド2下面部に配置されており、その中心軸が斜め下方へ向かった姿勢で取り付けられている。特に、上記燃料噴射弁10は、2つの吸気弁5の間に配置され、点火プラグ7が位置するシリンダ3中心ヘ向かって、水平に近い傾斜角度でもって燃料を噴射するように構成されている。   The electromagnetic fuel injection valve 10 that directly injects fuel into the cylinder is disposed on the bottom surface of the cylinder head 2 near the side wall of the cylinder 3 on the intake valve 5 side, and is mounted with its center axis inclined downward. It has been. In particular, the fuel injection valve 10 is disposed between the two intake valves 5 and is configured to inject fuel at an inclination angle close to horizontal toward the center of the cylinder 3 where the spark plug 7 is located. .

なお、上記吸気ポート8は、シリンダ3内にいわゆる順方向のタンブル流を生成するのに適した形状を有しているが、さらに、ポート内を上下の流路に仕切る隔壁やその一方の流路を開閉するタンブル制御弁などのタンブル生成手段を必要に応じて設けることもできる。   The intake port 8 has a shape suitable for generating a so-called forward tumble flow in the cylinder 3, but further, a partition partitioning the inside of the port into upper and lower flow paths and one of the flow paths. Tumble generating means such as a tumble control valve for opening and closing the path can be provided as necessary.

上記の内燃機関の基本的な作用について簡単に説明すると、先ず、機関の全負荷時あるいは希薄燃焼域の中でも比較的空燃比が小さな領域では、シリンダ3内に均質な混合気を形成して点火する均質燃焼が行われる。この均質燃焼時には、燃料は、吸気行程中にシリンダ3内に噴射供給され、シリンダ3内に生成されるタンブル流によって積極的に拡散される。   The basic operation of the internal combustion engine will be briefly described. First, a homogeneous air-fuel mixture is formed in the cylinder 3 at the time of full load of the engine or in a region where the air-fuel ratio is relatively small in the lean combustion region. Homogeneous combustion is performed. During the homogeneous combustion, fuel is injected and supplied into the cylinder 3 during the intake stroke, and is actively diffused by the tumble flow generated in the cylinder 3.

一方、低負荷域で、かつ空燃比を非常に大きくする希薄燃焼域では、混合気の成層化により確実な着火を可能とする成層希薄燃焼を行う。この成層希薄燃焼時には、燃料は、圧縮行程の後半において、燃料噴射弁10から燃焼室11壁面とピストン4との間の空間へ向けて噴射される。この噴射された燃料は、後述するように点火プラグ7周辺に着火可能な混合気を形成するので、適宜なタイミングで点火することにより、着火燃焼が可能となる。なお、タンブル制御弁のようなタンブル流を可変制御する手段を有する場合には、成層希薄燃焼時には、タンブル流を抑制することが望ましい。   On the other hand, in a lean combustion region where the air-fuel ratio is very large in a low load region, stratified lean combustion is performed that enables reliable ignition by stratification of the air-fuel mixture. During this stratified lean combustion, fuel is injected from the fuel injection valve 10 toward the space between the combustion chamber 11 wall surface and the piston 4 in the latter half of the compression stroke. Since the injected fuel forms an ignitable air-fuel mixture around the spark plug 7 as will be described later, ignition and combustion are possible by igniting at an appropriate timing. In addition, when it has a means to variably control the tumble flow such as a tumble control valve, it is desirable to suppress the tumble flow during stratified lean combustion.

次に、図2は、本発明に係るピストン4の構成、特にその頂部の構成を示している。図示するように、このピストン4は、冠面の略全面に、周囲の基準面20からシリンダヘッド1側へ膨らんだ凸部21を有しているとともに、この凸部21の中央部に、上面から見て矩形状をなす凹部22が設けられている。上記凸部21は、上死点位置においてシリンダヘッド1側の燃焼室11内に入り込み、その容積の一部を占めるように、ドーム型に膨らんでいるが、上記凹部22が大きく設けられていることから、実際には、ピストンピン軸方向の両端部に、それぞれ冠面の中の三日月型の領域を占める凸部21a,21bが部分的に残った形となっている。そして、ピストンピンと直交する方向の両端(つまり吸気弁側および排気弁側の端部)の2箇所には、三日月形のスキッシュエリア23,24が、基準面20と同一の平面として形成されている。   Next, FIG. 2 shows the configuration of the piston 4 according to the present invention, particularly the configuration of its top. As shown in the figure, the piston 4 has a convex portion 21 that swells from the surrounding reference surface 20 toward the cylinder head 1 on substantially the entire crown surface, and an upper surface at the center of the convex portion 21. A concave portion 22 having a rectangular shape as viewed from above is provided. The convex portion 21 enters the combustion chamber 11 on the cylinder head 1 side at the top dead center position and swells in a dome shape so as to occupy a part of the volume thereof, but the concave portion 22 is largely provided. Therefore, actually, the convex portions 21a and 21b occupying the crescent-shaped regions in the crown surface are partially left at both ends in the piston pin axial direction. Then, crescent-shaped squish areas 23 and 24 are formed as the same plane as the reference surface 20 at two locations on both ends in the direction orthogonal to the piston pin (that is, the ends on the intake valve side and the exhaust valve side). .

上記凹部22は、ピストンピン中心軸線と略平行な湾曲面からなる底面25と、ピストンピンと直交する方向に沿って延びた一対の側壁面26,26と、から形成されている。上記底面25は、一定の曲率半径を有する単純な円筒面であってもよく、曲率半径が部分的に異なる湾曲面であってもよいが、全体として、シリンダ3内のタンブル流の流れに沿うように湾曲している。   The concave portion 22 is formed of a bottom surface 25 having a curved surface substantially parallel to the piston pin central axis, and a pair of side wall surfaces 26 and 26 extending along a direction orthogonal to the piston pin. The bottom surface 25 may be a simple cylindrical surface having a constant radius of curvature, or may be a curved surface having a partially different radius of curvature, but as a whole, follows the flow of the tumble flow in the cylinder 3. Is so curved.

ここで、本実施例では、上記の湾曲面からなる底面25の長手方向の略中央部に、該底面25の吸気弁側部分25aと排気弁側部分25bとの間で若干の高低差が生じるように、ピストンピン中心軸線と平行に直線状に延びた段部27が設けられている。この段部27においては、上記の排気弁側部分25bが吸気弁側部分25aに対し相対的に高くなっており、これにより、図3にも示すように、吸気弁側部分25aから上方へ立ち上がる吸気弁側の立ち上がり部27aが形成されている。この吸気弁側の立ち上がり部27aは、上記点火プラグ7の電極部の直下に位置している。なお、吸気弁側の立ち上がり部27aの上方部分つまり点火プラグ7寄りの部分は、点火プラグ7へ向かって略垂直に直立している。   Here, in this embodiment, there is a slight difference in height between the intake valve side portion 25a and the exhaust valve side portion 25b of the bottom surface 25 at a substantially central portion in the longitudinal direction of the bottom surface 25 made of the curved surface. Thus, the step part 27 extended linearly in parallel with the piston pin center axis line is provided. In the stepped portion 27, the exhaust valve side portion 25b is relatively higher than the intake valve side portion 25a, and as a result, rises upward from the intake valve side portion 25a as shown in FIG. A rising portion 27a on the intake valve side is formed. The rising portion 27 a on the intake valve side is located immediately below the electrode portion of the spark plug 7. Note that the upper portion of the rising portion 27 a on the intake valve side, that is, the portion near the spark plug 7 stands substantially vertically toward the spark plug 7.

また、ピストンピン中心軸線に沿って延びた段部27は、その両端部が切り欠かれており、この一対の切欠部分28,28では、底面25の吸気弁側部分25aと排気弁側部分25bとが、段差を生じることなく滑らかに連続している。換言すれば、上記段部27は、凹部22の側壁面26,26から離れて形成されており、湾曲面からなる底面25の中に独立した島状に形成されている。   Further, the stepped portion 27 extending along the central axis of the piston pin is notched at both ends, and the pair of notched portions 28 and 28 has an intake valve side portion 25a and an exhaust valve side portion 25b of the bottom surface 25. Are smoothly continuous without causing a step. In other words, the stepped portion 27 is formed away from the side wall surfaces 26, 26 of the recess 22, and is formed in an independent island shape in the bottom surface 25 formed of a curved surface.

上記のような実施例の構成においては、図3の説明図に示すように、成層希薄燃焼のために圧縮行程後期に燃料を噴射したときに、噴霧Fは、その進行方向が段部27の吸気弁側の立ち上がり部27aに沿って点火プラグ7へ向けられ、あるいは、段部27の上方を噴霧Fが通過することによって、該段部27の吸気弁側の立ち上がり部27aに沿って上方へ向かう上昇流が局部的に発生し、これに乗って、一部の噴霧Fが上方の点火プラグ7側へ案内される。従って、点火プラグ7近傍に適宜な混合気を安定的に形成でき、安定した燃焼が得られる。   In the configuration of the embodiment as described above, as shown in the explanatory diagram of FIG. 3, when fuel is injected in the late stage of the compression stroke for stratified lean combustion, the spray F has a traveling direction of the step portion 27. Directed toward the spark plug 7 along the rising portion 27a on the intake valve side, or upwards along the rising portion 27a on the intake valve side of the step portion 27 as the spray F passes above the step portion 27. An upward flow is generated locally, and a part of the spray F is guided to the upper spark plug 7 side. Therefore, an appropriate air-fuel mixture can be stably formed in the vicinity of the spark plug 7 and stable combustion can be obtained.

一方、均質燃焼の際には、前述したように、シリンダ内のタンブル流を利用して燃焼が行われるが、図4の説明図に示すように、矢印Tで示すタンブル流は、湾曲面からなる凹部22の底面25の上を、排気弁側から吸気弁側へと流れ、シリンダ3内で旋回する。ここで、段部27の両側に切欠部分28,28が設けられ、該切欠部分28,28では段差のない連続面をなしているので、タンブル流が円滑に流れ、段部27を設けたことによるタンブル流の低下が最小限のものとなる。   On the other hand, in the homogeneous combustion, as described above, combustion is performed using the tumble flow in the cylinder. However, as shown in the explanatory view of FIG. It flows on the bottom surface 25 of the concave portion 22 from the exhaust valve side to the intake valve side and turns in the cylinder 3. Here, notch portions 28 and 28 are provided on both sides of the step portion 27, and the notch portions 28 and 28 form a continuous surface without a step, so that the tumble flow smoothly flows and the step portion 27 is provided. The decrease in tumble flow due to is minimized.

また、仮に、上記の段部27が凹部22の側壁面26,26の間に連続して設けられていると、ピストン冠部の肉厚が、吸気弁側で薄く、排気弁側で全体として厚くなり、ピストン鋳造時に熱歪を生じやすいものとなるが、上記構成では、相対的に小さな体積の段部27が部分的に存在するだけなので、ピストンを鋳造で製造した場合に生じる熱歪が小さなものとなる。またピストン冠部の全体の肉厚の増加により機関の圧縮比を大きく低下させるようなこともない。   Further, if the stepped portion 27 is provided continuously between the side wall surfaces 26, 26 of the recess 22, the piston crown portion is thin on the intake valve side and overall on the exhaust valve side. Although it becomes thicker and heat distortion is likely to occur at the time of piston casting, in the above configuration, since the step portion 27 having a relatively small volume is only partially present, the heat distortion generated when the piston is manufactured by casting is increased. It will be small. Further, the compression ratio of the engine is not greatly reduced by increasing the overall thickness of the piston crown.

次に、図5および図6は、本発明の第2の実施例を示している。この実施例のピストン4においては、凹部22の底面25が段差のない連続したものとなっており、かつその長手方向の略中央部に、前述の段部27に代えて、ピストンピン中心軸線と平行に直線状に延びた突条部31が設けられている。この突条部31は、図7にも示すように、断面が略台形状をなし、かつ、底面25から該突条部31へと立ち上がる吸気弁側の立ち上がり部31aおよび排気弁側の立ち上がり部31bが、それぞれ滑らかに連続する円弧面をなしている。なお、前述の実施例と同じく、吸気弁側の立ち上がり部31aが上記点火プラグ7の電極部の直下に位置している。また、この吸気弁側の立ち上がり部31aの上方部分つまり突条部31の先端側の部分は、点火プラグ7へ向かって略垂直に直立している。   5 and 6 show a second embodiment of the present invention. In the piston 4 of this embodiment, the bottom surface 25 of the concave portion 22 is continuous without a step, and the piston pin center axis line is replaced with a substantially central portion in the longitudinal direction in place of the step portion 27 described above. A protrusion 31 extending linearly in parallel is provided. As shown in FIG. 7, the protrusion 31 has a substantially trapezoidal cross section, and the intake valve side rising part 31 a and the exhaust valve side rising part rising from the bottom surface 25 to the protrusion 31. Reference numerals 31b each form a smoothly continuous circular arc surface. As in the previous embodiment, the rising portion 31a on the intake valve side is located directly below the electrode portion of the spark plug 7. Further, the upper part of the rising part 31 a on the intake valve side, that is, the part on the tip side of the ridge part 31 stands upright substantially vertically toward the spark plug 7.

そして、ピストンピン中心軸線に沿って延びた突条部31は、その両端部が切り欠かれており、この一対の切欠部分32,32では、底面25の吸気弁側部分25aと排気弁側部分25bとが滑らかに連続している。換言すれば、上記突条部31は、凹部22の側壁面26,26から離れて形成されており、湾曲面からなる底面25の中に独立した島状に形成されている。   The protruding portion 31 extending along the central axis of the piston pin is notched at both ends. The pair of notched portions 32 and 32 has an intake valve side portion 25a and an exhaust valve side portion of the bottom surface 25. 25b is smoothly continuous. In other words, the protruding portion 31 is formed away from the side wall surfaces 26, 26 of the recess 22, and is formed in an independent island shape in the bottom surface 25 formed of a curved surface.

上記のような実施例の構成においては、図7の説明図に示すように、成層希薄燃焼のために圧縮行程後期に燃料を噴射したときに、噴霧Fは、その進行方向が突条部31の吸気弁側の立ち上がり部31aに沿って点火プラグ7へ向けられ、あるいは、突条部31の上方を噴霧Fが通過することによって、該突条部31の吸気弁側の立ち上がり部31aに沿って上方へ向かう上昇流が局部的に発生し、これに乗って、一部の噴霧Fが上方の点火プラグ7側へ案内される。従って、点火プラグ7近傍に適宜な混合気を安定的に形成でき、安定した燃焼が得られる。   In the configuration of the embodiment as described above, as shown in the explanatory diagram of FIG. 7, when fuel is injected in the latter stage of the compression stroke for stratified lean combustion, the traveling direction of the spray F is the ridge 31. Is directed toward the ignition plug 7 along the rising portion 31a on the intake valve side, or along the rising portion 31a on the intake valve side of the protruding portion 31 by the spray F passing above the protruding portion 31. Thus, an upward flow upward is generated locally, and a part of the spray F is guided to the upper spark plug 7 side. Therefore, an appropriate air-fuel mixture can be stably formed in the vicinity of the spark plug 7 and stable combustion can be obtained.

一方、均質燃焼の際には、前述したように、シリンダ内のタンブル流を利用して燃焼が行われるが、図8の説明図に示すように、矢印Tで示すタンブル流は、湾曲面からなる凹部22の底面25の上を、排気弁側から吸気弁側へと流れ、シリンダ3内で旋回する。ここで、突条部31の両側に切欠部分32,32が設けられているので、タンブル流が円滑に流れ、突条部31を設けたことによるタンブル流の低下が最小限のものとなる。   On the other hand, in the homogeneous combustion, as described above, combustion is performed using the tumble flow in the cylinder. As shown in the explanatory view of FIG. 8, the tumble flow indicated by the arrow T starts from the curved surface. It flows on the bottom surface 25 of the concave portion 22 from the exhaust valve side to the intake valve side and turns in the cylinder 3. Here, since the notched portions 32 are provided on both sides of the ridge 31, the tumble flow smoothly flows, and the decrease in the tumble flow due to the provision of the ridge 31 is minimized.

なお、吸気弁側の立ち上がり部31aのみが生じるように凹部22底面25全幅に亘って段部を設けると、前述したように、ピストン冠部の肉厚が、吸気弁側で薄く、排気弁側で厚くなり、ピストン鋳造時に熱歪を生じやすいものとなるが、上記構成では、相対的に小さな体積の突条部31が存在するだけなので、ピストンを鋳造で製造した場合に熱歪を生じることがない。またピストン冠部の肉厚の増加により機関の圧縮比を低下させることもない。   If the stepped portion is provided over the entire width of the bottom surface 25 of the recess 22 so that only the rising portion 31a on the intake valve side occurs, as described above, the thickness of the piston crown is thin on the intake valve side, and the exhaust valve side However, in the above configuration, there is only a protrusion 31 having a relatively small volume, so that when the piston is manufactured by casting, thermal distortion occurs. There is no. Further, the compression ratio of the engine is not reduced by increasing the thickness of the piston crown.

図9は、上記の突条部31を設けたことによる成層希薄燃焼時の安定性向上についての実験結果を示したものであり、特に、冷間始動直後の触媒早期活性化のために点火時期をリタードしたときの特性を、突条部31を具備しない比較例と突条部31を備えた実施例とで対比して示している。なお、実験条件としては、1250rpmのファストアイドル状態、空燃比16、水温20℃、である。   FIG. 9 shows the results of an experiment for improving the stability during stratified lean combustion by providing the above-mentioned ridges 31, and in particular, the ignition timing for the early activation of the catalyst immediately after the cold start. The characteristic when this is retarded is shown in comparison between the comparative example not including the protrusion 31 and the example including the protrusion 31. The experimental conditions are a 1250 rpm fast idle state, an air-fuel ratio of 16, and a water temperature of 20 ° C.

図の(c)は、燃焼変動を示す筒内圧のばらつきσPiと点火時期との関係を示しており、一般に、点火時期の遅角に伴って燃焼変動が大となる。ここで、L1が燃焼安定限界である。比較例では、点火時期が上死点後10°CA付近で燃焼安定限界L1を越えてしまい、これよりも遅角することはできない。これに対し、突条部31を備えた実施例では、筒内圧のばらつきσPiが相対的に小さくなり、上死点後18°CA付近まで遅角することが可能である。   (C) of the figure shows the relationship between the variation σPi of the in-cylinder pressure indicating the combustion fluctuation and the ignition timing. In general, the combustion fluctuation increases as the ignition timing is retarded. Here, L1 is the combustion stability limit. In the comparative example, the ignition timing exceeds the combustion stability limit L1 in the vicinity of 10 ° CA after the top dead center, and cannot be delayed more than this. On the other hand, in the embodiment provided with the ridge 31, the in-cylinder pressure variation σPi is relatively small and can be retarded to about 18 ° CA after top dead center.

図の(a)は、機関で発生するHCの特性を示しており、一般に、点火時期の遅角に伴ってHCが減少する。同一の点火時期で比較すると、実施例の方が比較例よりもHC発生量が大となるが、燃焼安定限界まで遅角することを前提とすると、上死点後10°CA付近の点火時期の下での比較例のHC発生量(点A1で示す)に比較して、上死点後18°CA付近の点火時期の下での実施例のHC発生量(点A2で示す)の方が、40%程度低くなる。   (A) of the figure shows the characteristics of HC generated in the engine, and in general, HC decreases as the ignition timing is retarded. When compared at the same ignition timing, the amount of HC generated in the example is larger than that in the comparative example, but assuming that the combustion is retarded to the combustion stability limit, the ignition timing near 10 ° CA after top dead center Compared to the amount of HC generated in the comparative example (indicated by point A1) under the above, the amount of HC generated in the example (indicated by point A2) under the ignition timing near 18 ° CA after top dead center However, it is about 40% lower.

また、図の(b)は、内燃機関の排気マニホルドに取り付けられた触媒装置入口での排気温度を示しており、一般に、点火時期の遅角に伴って排気温度が上昇する傾向となる。同一の点火時期で比較しても、実施例の方が比較例よりも高い排気温度が得られるが、燃焼安定限界まで遅角することを前提とすると、上死点後10°CA付近の点火時期の下での比較例の排気温度(点B1で示す)に比較して、上死点後18°CA付近の点火時期の下での実施例の排気温度(点B2で示す)は、200℃近く高く得られる。   Further, (b) in the figure shows the exhaust temperature at the inlet of the catalytic device attached to the exhaust manifold of the internal combustion engine, and generally the exhaust temperature tends to increase with the retard of the ignition timing. Even when compared at the same ignition timing, the exhaust gas temperature in the example is higher than that in the comparative example. However, if it is assumed that the engine is retarded to the combustion stability limit, ignition at around 10 ° CA after top dead center Compared to the exhaust temperature of the comparative example under time (indicated by point B1), the exhaust temperature of the example (indicated by point B2) under the ignition timing near 18 ° CA after top dead center is 200. Highly obtained near ℃.

このように、本発明によれば、燃焼安定性が向上する結果、始動直後などに点火時期の大幅な遅角が可能となり、HC発生量を低減するとともに、排気温度が高く得られ、触媒の早期活性化が図れる。   As described above, according to the present invention, as a result of improving the combustion stability, ignition timing can be greatly retarded immediately after starting, etc., the amount of HC generated can be reduced, the exhaust temperature can be increased, and the catalyst Early activation can be achieved.

また、図10は、シリンダ3内に生じるタンブル流の強さつまりタンブル比のサイクル中の変化を示したものであって、縦軸のタンブル比は、図の下方ほどタンブル流が強いものとして示してあるが、基本的に、タンブル強さは、吸気行程において大となり、圧縮上死点に向かって減衰していく傾向となる。ここで、比較例1は、突条部31を具備しない場合の特性、比較例2は、両端が側壁面26,26に連続した形で突条部31を設けた場合の特性である。図示するように、切欠部分32,32を備えない比較例2では、突条部31を具備しない比較例1に比べて、タンブル比が大きく低下する。これに対し、一対の切欠部分32,32を有する形で突条部31を備えた実施例では、比較例1に近い特性となり、タンブル比の低下が抑制される。   FIG. 10 shows the strength of the tumble flow generated in the cylinder 3, that is, the change in the tumble ratio during the cycle. The tumble ratio on the vertical axis indicates that the tumble flow is stronger toward the bottom of the figure. Basically, however, the tumble strength increases during the intake stroke and tends to attenuate toward the compression top dead center. Here, the comparative example 1 is a characteristic when the protrusion 31 is not provided, and the comparative example 2 is a characteristic when the protrusion 31 is provided in a form in which both ends are continuous with the side wall surfaces 26 and 26. As shown in the figure, in the comparative example 2 that does not include the notched portions 32 and 32, the tumble ratio is greatly reduced as compared with the comparative example 1 that does not include the protruding portion 31. On the other hand, in the Example which provided the protrusion part 31 in the form which has a pair of notch parts 32 and 32, it becomes a characteristic close to the comparative example 1, and the fall of a tumble ratio is suppressed.

この発明に係るピストンが用いられる筒内噴射式内燃機関の構成を示す断面図。Sectional drawing which shows the structure of the cylinder injection type internal combustion engine in which the piston which concerns on this invention is used. この発明に係るピストンの頂部の斜視図。The perspective view of the top part of the piston which concerns on this invention. 燃料噴射時の様子を示す要部の断面説明図。Cross-sectional explanatory drawing of the principal part which shows the mode at the time of fuel injection. タンブル流の流れを示す斜視説明図。The perspective explanatory view showing the flow of the tumble flow. 第2の実施例を示す内燃機関の断面図。Sectional drawing of the internal combustion engine which shows a 2nd Example. この実施例のピストン頂部の斜視図。The perspective view of the piston top part of this Example. 燃料噴射時の様子を示す要部の断面説明図。Cross-sectional explanatory drawing of the principal part which shows the mode at the time of fuel injection. タンブル流の流れを示す斜視説明図。The perspective explanatory view showing the flow of the tumble flow. 点火時期と、(a)HC発生量、(b)触媒入口排気温度、(c)筒内圧のばらつきσPi、との関係を、実施例と比較例とで対比して示した特性図。The characteristic view which showed the relationship between ignition timing, (a) HC generation amount, (b) catalyst inlet exhaust temperature, and (c) dispersion | variation (sigma) Pi of in-cylinder pressure by contrast in an Example and a comparative example. タンブル比のサイクル中の変化を、実施例と比較例とで対比して示した特性図。The characteristic view which showed the change in the cycle of tumble ratio in the Example and the comparative example by contrast.

符号の説明Explanation of symbols

4…ピストン
22…凹部
25…底面(湾曲面)
27…段部
28…切欠部分
31…突条部
32…切欠部分
4 ... Piston 22 ... Recess 25 ... Bottom (curved surface)
27 ... Step part 28 ... Notch part 31 ... Projection part 32 ... Notch part

Claims (5)

シリンダ頂面の略中心部に点火プラグが配置されるとともに、吸気弁側の燃焼室側方に燃料噴射弁が配置されてなる筒内直接噴射式内燃機関に用いられるピストンであって、ピストン冠面に、シリンダ内のタンブル流に沿うように、ピストンピン中心軸線と略平行な湾曲面が凹設されてなる内燃機関のピストンにおいて、
上記点火プラグの直下付近となる上記湾曲面の略中央部に、該湾曲面の吸気弁側部分から立ち上がる吸気弁側の立ち上がり部を形成するように、ピストンピン中心軸線と平行に延びた突条部もしくは段部が設けられているとともに、
この突条部もしくは段部は、両端部が切り欠かれており、この切欠部分では、湾曲面の吸気弁側部分と排気弁側部分とが滑らかに連続していることを特徴とする内燃機関のピストン。
A piston used in an in-cylinder direct injection internal combustion engine in which a spark plug is disposed at a substantially central portion of a cylinder top surface and a fuel injection valve is disposed at a side of a combustion chamber on an intake valve side. In the piston of the internal combustion engine in which a curved surface substantially parallel to the piston pin central axis is recessed so that the surface follows the tumble flow in the cylinder,
A ridge extending in parallel with the piston pin central axis so as to form a rising portion on the intake valve side that rises from the intake valve side portion of the curved surface at a substantially central portion of the curved surface that is directly below the spark plug. Part or step,
Both ends of the protruding portion or stepped portion are cut out, and the intake valve side portion and the exhaust valve side portion of the curved surface are smoothly continuous at the cutout portion. Piston.
吸気弁側の立ち上がり部が上記点火プラグの直下付近に位置することを特徴とする請求項1に記載の内燃機関のピストン。   2. The piston of an internal combustion engine according to claim 1, wherein a rising portion on the intake valve side is located in the vicinity of directly below the spark plug. 上記ピストン冠面の略全面に、シリンダヘッド側へ膨らんだ凸部が設けられ、この凸部のピストンピン軸方向の端部寄りの部分を残すように上記湾曲面が矩形状に凹設されていることを特徴とする請求項1または2に記載の内燃機関のピストン。   A convex portion bulging toward the cylinder head is provided on substantially the entire surface of the piston crown surface, and the curved surface is recessed in a rectangular shape so as to leave a portion of the convex portion near the end in the piston pin axial direction. The piston of the internal combustion engine according to claim 1 or 2, wherein 矩形状の凹部の側壁面から離れて上記突条部もしくは段部が上記湾曲面の中に島状に形成されていることを特徴とする請求項3に記載の内燃機関のピストン。   4. The piston for an internal combustion engine according to claim 3, wherein the protruding portion or the stepped portion is formed in an island shape in the curved surface apart from the side wall surface of the rectangular concave portion. 請求項1〜4のいずれかに記載のピストンを備えた内燃機関。   The internal combustion engine provided with the piston in any one of Claims 1-4.
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