JPH08100702A - Diesel engine - Google Patents

Diesel engine

Info

Publication number
JPH08100702A
JPH08100702A JP6237295A JP23729594A JPH08100702A JP H08100702 A JPH08100702 A JP H08100702A JP 6237295 A JP6237295 A JP 6237295A JP 23729594 A JP23729594 A JP 23729594A JP H08100702 A JPH08100702 A JP H08100702A
Authority
JP
Japan
Prior art keywords
intake
injection port
port
cylinder liner
valve
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
JP6237295A
Other languages
Japanese (ja)
Other versions
JP3330745B2 (en
Inventor
Seita Akimoto
成太 秋本
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Yanmar Co Ltd
Original Assignee
Yanmar Diesel Engine Co Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Yanmar Diesel Engine Co Ltd filed Critical Yanmar Diesel Engine Co Ltd
Priority to JP23729594A priority Critical patent/JP3330745B2/en
Publication of JPH08100702A publication Critical patent/JPH08100702A/en
Application granted granted Critical
Publication of JP3330745B2 publication Critical patent/JP3330745B2/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B3/00Engines characterised by air compression and subsequent fuel addition
    • F02B3/06Engines characterised by air compression and subsequent fuel addition with compression ignition
    • 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

Landscapes

  • Combustion Methods Of Internal-Combustion Engines (AREA)
  • Cylinder Crankcases Of Internal Combustion Engines (AREA)
  • Fuel-Injection Apparatus (AREA)

Abstract

PURPOSE: To prevent generation of a streamline of an intake air flow staying or a streamline of an intake air flow returning to a main line by smoothing the streamline of the intake air flow from an intake port into a cylinder liner. CONSTITUTION: In a diesel engine wherein an intake valve seat 4 and a discharge valve seat 14 project outward from the outer periphery of a cylinder liner 1, a lack part 5a is provided on the outlet side of an intake port 5 along the circular shape on the lower part of the cylinder liner 1. Moreover, a sub nozzle port 7 for injecting fuel atomized flow toward an intake valve vertically moving recessed part and an exhaust valve vertically moving recessed part is provided.

Description

【発明の詳細な説明】Detailed Description of the Invention

【0001】[0001]

【産業上の利用分野】本発明は、低速でかつ大型のディ
ーゼル機関であって、吸気を1弁と排気を1弁の2弁式
とした場合の、吸気ポートと燃料噴射弁の噴口の形状に
関する。
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a low-speed and large-sized diesel engine in which the intake port and the injection port of the fuel injection valve are of the two-valve type with one intake valve and one exhaust valve. Regarding

【0002】[0002]

【従来の技術】従来の低速大型のシリンダ径が300〜
400ミリ程度で2弁式のディーゼル機関においては、
吸気量を確保する為にバルブ座の径が大きくなり、シリ
ンダライナの外周よりも、バルブ座の外周の方が外側に
突出するので、バルブ上下動凹部を設けている。そし
て、このバルブ上下動凹部3の外周に沿った形状に吸気
ポート5の外径が構成されていたのである。しかし、こ
の場合には、吸気ポートからの吸気の流れが、バルブ上
下動凹部の部分で阻害され、バルブ径の大きさに似合っ
た有効吸気通路面積を得ることが出来ず、逆に、バルブ
上下動凹部に衝突した吸気の流れが、バルブ上下動凹部
に衝突せずに流れ込む吸気の流れを阻害し、吸気量を減
少させるという不具合があったのである。
2. Description of the Related Art Conventional low-speed large-sized cylinders have diameters of 300-
In a two-valve diesel engine of about 400 mm,
Since the diameter of the valve seat is increased in order to secure the intake amount and the outer circumference of the valve seat projects more outward than the outer circumference of the cylinder liner, the valve vertical movement recess is provided. Then, the outer diameter of the intake port 5 was formed in a shape along the outer periphery of the valve vertical movement concave portion 3. However, in this case, the flow of intake air from the intake port is blocked by the valve vertical movement recessed portion, and an effective intake passage area that matches the size of the valve diameter cannot be obtained. The flow of intake air that collides with the moving recessed portion impedes the flow of intake air that does not collide with the vertically moving recessed portion of the valve, thus reducing the amount of intake air.

【0003】また、ディーゼル機関の高出力化に伴い、
噴射量を増加させる必要があり、その為に燃料弁の総噴
口面積を大きくする必要がある。総噴口面積を増加させ
る方法としては、噴口数の増加又は1つ当りの噴口面積
を大きくするしかない。しかし、噴口数の増加について
は、各噴口からの燃料噴霧のオーバーラップ等によって
限界がある。また1つ当りの噴口面積を大きくした場合
にも、噴射圧力の高い高負荷時は問題なくても、噴射圧
力の低い低負荷時は噴口面積が大きい為に噴霧特性が悪
化し燃焼性能が悪化してしまうのである。
In addition, with the increase in output of diesel engines,
It is necessary to increase the injection amount, and for that reason, it is necessary to increase the total injection port area of the fuel valve. The only way to increase the total nozzle area is to increase the number of nozzles or increase the area of each nozzle. However, there is a limit to the increase in the number of nozzles due to the overlap of fuel spray from each nozzle. Also, even if the area of each injection port is increased, there is no problem when the injection pressure is high and the load is high, but when the injection pressure is low and the load is low, the spray characteristics are large and the combustion performance deteriorates because of the large injection port area. It does.

【0004】[0004]

【発明が解決しようとする課題】本発明は、吸気ポート
の形状を適正なものとすることにより、吸気量の増大を
図り、また吸気量の増大により、燃費や排気色や熱負荷
の低減等のディーゼル機関性能の向上を図るのである。
また、副噴口から噴射された燃料噴霧が、シリンダライ
ナの壁面やピストン頂面に衝突しないようにシリンダラ
イナのバルブ上下動凹部を利用したものである。これに
より燃料噴霧流の到達距離を充分に得ることが出来て、
良好な燃焼が得られるのである。
SUMMARY OF THE INVENTION The present invention aims to increase the intake amount by optimizing the shape of the intake port, and the increase of the intake amount reduces fuel consumption, exhaust color and heat load. To improve the diesel engine performance.
Further, the valve vertical movement concave portion of the cylinder liner is used so that the fuel spray injected from the auxiliary injection port does not collide with the wall surface of the cylinder liner or the top surface of the piston. As a result, it is possible to obtain a sufficient distance for the fuel spray flow,
Good combustion is obtained.

【0005】[0005]

【課題を解決するための手段】本発明の解決しようとす
る課題は以上の如くであり、次に該課題を解決するため
の手段を説明する。請求項1においては、内燃機関のシ
リンダライナ1の外周よりも外側に、吸気バルブ2のバ
ルブ座4の外周が突出し、該シリンダライナ1の上端
に、該吸気バルブ2を上下動可能とするバルブ上下動凹
部3を設けた構成において、吸気バルブ2のバルブ座4
に連通する吸気ポート5の出口側をバルブ上下動凹部3
に沿わせずに、シリンダライナ1のバルブ上下動凹部3
より下部の円弧外周に沿った形状としたものである。
The problems to be solved by the present invention are as described above. Next, the means for solving the problems will be described. In Claim 1, the outer periphery of the valve seat 4 of the intake valve 2 projects outside the outer periphery of the cylinder liner 1 of the internal combustion engine, and the valve that allows the intake valve 2 to move up and down at the upper end of the cylinder liner 1. The valve seat 4 of the intake valve 2 in the configuration provided with the vertically movable recess 3
The outlet side of the intake port 5 communicating with the valve vertical movement recess 3
The valve vertical movement recess 3 of the cylinder liner 1 without
The shape is along the outer circumference of the lower circular arc.

【0006】請求項2においては、燃料弁の噴口とし
て、主噴口6に加えて副噴口7を有する内燃機関におい
て、副噴口7の噴口径は、主噴口6の噴口径よりも小さ
くし、副噴口7は主噴口6の噴口角よりも大きくし、シ
リンダライナ1のバルブ上下動凹部3の中心線上に副噴
口7を配置したものである。
According to a second aspect of the present invention, in the internal combustion engine having the auxiliary injection port 7 in addition to the main injection port 6 as the injection port of the fuel valve, the auxiliary injection port 7 has a smaller injection port diameter than the main injection port 6. The injection port 7 is larger than the injection port angle of the main injection port 6, and the sub injection port 7 is arranged on the center line of the valve vertical movement recess 3 of the cylinder liner 1.

【0007】[0007]

【作用】次に作用を説明する。請求項1によれば、吸気
ポート5からの流入空気の流れの一部が、吸気バルブ上
下動凹部3に衝突しないように構成することが出来たの
で、見かけのポートの断面積は減少したが、吸気流の流
線をスムーズに揃えることにより、滞留してしまう吸気
流の流線dや、本線に戻ろうとする吸気流の流線gが無
くなり、吸入空気量は増大した。これにより、流入空気
量を増大することが出来るので、燃費と熱負荷の低減を
図り、排気色の悪化を防ぐことができた。
Next, the operation will be described. According to the first aspect of the present invention, since a part of the flow of the inflowing air from the intake port 5 can be configured not to collide with the intake valve vertical movement recessed portion 3, the apparent cross-sectional area of the port is reduced. By smoothly aligning the flow lines of the intake flow, the flow line d of the intake flow that stagnates and the flow line g of the intake flow that tries to return to the main line are eliminated, and the intake air amount is increased. As a result, the amount of inflowing air can be increased, fuel consumption and heat load can be reduced, and deterioration of exhaust color can be prevented.

【0008】請求項2によれば、噴霧到達距離を充分に
得ることが出来るので、良好な燃焼が得られる。
According to the second aspect, since the spray reaching distance can be sufficiently obtained, good combustion can be obtained.

【0009】[0009]

【実施例】次に実施例を説明する。図1は本発明のシリ
ンダライナ1とバルブ座4の部分を示す平面図、図2は
本発明のバルブ座4とシリンダライナ1と吸気バルブ2
の部分の側面一部断面図、図3は本発明の吸気バルブ座
4と吸気ポート5の関係位置を示す図面、図4は本発明
の吸気流の流線を示す俯瞰図、図5は従来の吸気バルブ
座4と吸気ポート5の関係位置を示す平面図と側面図、
図6は従来の吸気流の流線を示す俯瞰図、図7は本発明
の吸気ポート5の形状と、従来の吸気ポート5の形状と
の吸気流量の比較を示す図面、図8は主噴口6と副噴口
7を設けた発明の燃料噴霧流を示す側面図、図9は同じ
く主噴口6と副噴口7の燃料噴霧流の平面図、図10は
副噴口7と主噴口6の位置関係を示す側面断面図、図1
1は本発明と従来構造との、出力と排気色との関係を示
す図面である。
EXAMPLES Next, examples will be described. 1 is a plan view showing a cylinder liner 1 and a valve seat 4 of the present invention, and FIG. 2 is a valve seat 4, a cylinder liner 1 and an intake valve 2 of the present invention.
3 is a partial side sectional view of a portion of FIG. 3, FIG. 3 is a view showing a relational position between the intake valve seat 4 and the intake port 5 of the present invention, FIG. 4 is an overhead view showing a flow line of the intake flow of the present invention, and FIG. Of the intake valve seat 4 and the intake port 5 of FIG.
FIG. 6 is a bird's-eye view showing a streamline of a conventional intake flow, FIG. 7 is a drawing showing a comparison of the intake flow rate between the shape of the intake port 5 of the present invention and the shape of the conventional intake port 5, and FIG. 8 is a main injection port. 6 is a side view showing the fuel spray flow of the invention in which 6 and the sub injection port 7 are provided, FIG. 9 is a plan view of the fuel spray flow of the main injection port 6 and the sub injection port 7, and FIG. 10 is a positional relationship between the sub injection port 7 and the main injection port 6. 1 is a side sectional view showing FIG.
FIG. 1 is a drawing showing the relationship between output and exhaust color of the present invention and a conventional structure.

【0010】図1,図2,図3において、本発明の構成
を説明する。本発明のディーゼル機関は低速でピストン
ストロークが大きく、かつシリンダライナ1の径が大径
である。シリンダライナ1の径は例えば、300〜40
0ミリである。そして、弁は吸気バルブ2が1本と排気
バルブ12が1本の2弁式である。該吸気バルブ2と排
気バルブ12との間は或る程度の間隔が必要であり、ま
た吸気量を一定以上必要であるので、バルブ外径も大き
くなり、図1の如く、吸気バルブ座4と排気バルブ座1
4の外径が、シリンダライナ1の外径から突出してしま
うのである。該吸気バルブ座4に向かってシリンダヘッ
ドHの内部に吸気ポート5が穿設されており、同様に排
気バルブ座14に向かってシリンダヘッドHの内部に排
気ポート15が穿設されている。
The configuration of the present invention will be described with reference to FIGS. 1, 2 and 3. The diesel engine of the present invention has a low speed, a large piston stroke, and a large diameter of the cylinder liner 1. The diameter of the cylinder liner 1 is, for example, 300 to 40.
It is 0 mm. The valve is a two-valve type with one intake valve 2 and one exhaust valve 12. Since a certain distance is required between the intake valve 2 and the exhaust valve 12 and a certain amount of intake air is required, the outer diameter of the valve also becomes large, and as shown in FIG. Exhaust valve seat 1
The outer diameter of 4 projects from the outer diameter of the cylinder liner 1. An intake port 5 is bored inside the cylinder head H toward the intake valve seat 4, and an exhaust port 15 is bored inside the cylinder head H toward the exhaust valve seat 14 in the same manner.

【0011】そして、低速大型のディーゼル機関におい
て、吸気バルブ座4がシリンダライナ1の外径から突出
した場合には、シリンダライナ1の外周部分に、吸気バ
ルブ上下動凹部3と排気バルブ上下動凹部13が穿設
し、この部分において、吸気バルブ2と排気バルブ12
が上下可能に構成しているのである。本発明は、吸気ポ
ートからの吸気流の流線の一部がシリンダライナ1の吸
気バルブ上下動凹部3に衝突するのを防止する為に、吸
気ポート5の出口側即ち燃焼室側の形状をシリンダライ
ナ1の下部の円形の形状に沿った形状としたものであ
る。また吸気ポート5のながれがスムーズにシリンダラ
イナ1内に流入出来るように、吸気ポート5の出口形状
に沿ってポート形状を真っ直ぐに、立ち上げた形状とし
ている。排気ポート15の部分の形状は、そのまま排気
バルブ上下動凹部13に沿った形状としている。
In a low-speed large-sized diesel engine, when the intake valve seat 4 projects from the outer diameter of the cylinder liner 1, the intake valve vertical movement concave portion 3 and the exhaust valve vertical movement concave portion are formed in the outer peripheral portion of the cylinder liner 1. 13 is provided, and the intake valve 2 and the exhaust valve 12 are provided at this portion.
Is configured so that it can move up and down. In order to prevent a part of the flow line of the intake flow from the intake port from colliding with the intake valve vertical movement recessed portion 3 of the cylinder liner 1, the present invention has a shape on the outlet side of the intake port 5, that is, on the combustion chamber side. The cylinder liner 1 has a shape that follows the circular shape at the bottom. Further, in order that the flow of the intake port 5 can smoothly flow into the cylinder liner 1, the port shape is straight and raised along the outlet shape of the intake port 5. The shape of the exhaust port 15 is as it is along the exhaust valve vertical movement recess 13.

【0012】この吸気バルブ上下動凹部3と排気バルブ
上下動凹部13に向かって、吸気ポート5と排気ポート
15が穿設されるのであるが、従来は当然のことのよう
に、吸気バルブ上下動凹部3を含めた吸気バルブ座4の
全周に向かって、吸気ポート5が開口されていたのであ
る。この従来の構成は、図5において図示している。即
ち吸気ポート5が吸気バルブ座4に向かう端部が円形断
面に構成されていたのである。これに対して、本発明は
吸気ポート5が吸気バルブ座4に向かう部分の端面を、
シリンダライナ1の下方の円形部分の延長に沿うよう
に、半月形の部分だけ、内部に向かって突出した部分を
設け、吸気ポート5の端部の形状を、十六夜の月形に欠
落部5aを設けた形状としたものである。
Although the intake port 5 and the exhaust port 15 are bored toward the intake valve vertical movement recessed portion 3 and the exhaust valve vertical movement recessed portion 13, the intake valve vertical movement is conventional as a matter of course. The intake port 5 was opened toward the entire circumference of the intake valve seat 4 including the recess 3. This conventional configuration is shown in FIG. That is, the end of the intake port 5 toward the intake valve seat 4 had a circular cross section. On the other hand, in the present invention, the end surface of the portion where the intake port 5 faces the intake valve seat 4 is
Along the extension of the lower circular portion of the cylinder liner 1, only a half-moon shaped portion is provided with a portion projecting inward, and the shape of the end portion of the intake port 5 is the missing portion of the moon of the sixteenth night. 5a is provided.

【0013】このように構成したことにより、図6に示
す如く、従来の形状の如く吸気ポート5の吸気バルブ座
4に向かった端部を円形とした場合の吸気流の流線にお
いて発生していた不具合を解消することが出来たのであ
る。即ち、従来は図6に示す如く、吸気ポート5から吸
気バルブ上下動凹部3に流れて、そこで滞留してしまう
吸気流の流線dが発生し、また吸気バルブ上下動凹部3
の部分で曲げられて、本線に戻ろうとする吸気流の流線
gが発生し、該吸気流の流線gは真っ直ぐに流れる吸気
流の流線eと衝突して吸気の滞留部分を構成し、これら
が重なりあって吸気量の減少となっていたのである。
With this structure, as shown in FIG. 6, when the end portion of the intake port 5 facing the intake valve seat 4 is formed into a circular shape as in the conventional shape, it occurs in the streamline of the intake flow. It was possible to eliminate the trouble. That is, conventionally, as shown in FIG. 6, a streamline d of the intake flow that flows from the intake port 5 to the intake valve vertical movement concave portion 3 and stays there is generated, and the intake valve vertical movement concave portion 3 is generated.
The flow line g of the intake air flow that is bent at the portion of the line to return to the main line is generated, and the flow line g of the intake air flow collides with the flow line e of the intake air flow that flows straight to form a stagnant portion of the intake air. However, these were overlapped with each other and the intake amount was reduced.

【0014】本発明においては、欠落部5aを構成した
ことにより、滞留してしまう吸気流の流線dや本線に戻
ろうとする吸気流の流線gが発生しなくなり、真っ直ぐ
に流れる吸気流の流線eのみであるので、スムースな吸
気の流れとなり、吸気ポート5の端部の形が欠落部5a
の部分だけ断面積が小さくなったにも関わらず、吸気流
量を多くすることが出来たのである。このように欠落部
5aを設けたことによる吸気量の増加の状態が、図7に
吸気バルブリフトと吸気流量の関係のグラフとしてしめ
されている。
In the present invention, since the lacking portion 5a is formed, the flow line d of the intake flow that stagnates and the flow line g of the intake flow that tries to return to the main line do not occur, and the intake flow that flows straight Since there is only the streamline e, the flow of intake air is smooth, and the shape of the end of the intake port 5 is the missing portion 5a.
It was possible to increase the intake flow rate, despite the fact that the cross-sectional area was reduced only in the area. The state of increase in the intake air amount due to the provision of the missing portion 5a is shown in FIG. 7 as a graph of the relationship between the intake valve lift and the intake air flow rate.

【0015】次に図8より図11において、吸気バルブ
上下動凹部3と排気バルブ上下動凹部13を設けたシリ
ンダライナ1において、燃料噴射バルブの噴口体10
に、副噴口7と主噴口6との2種類の噴口を設けた構成
を説明する。副噴口7の数は吸気バルブ上下動凹部3と
排気バルブ上下動凹部13の数だけとする。本実施例で
は、2個である。副噴口7の位置は、吸気バルブ上下動
凹部3と排気バルブ上下動凹部13の或る方向とする。
副噴口7を穿孔する位置は、副噴口7の中心線とシリン
ダライナ1の内壁の交点がトップクリアランスの1/2
となるように構成している。
Next, referring to FIGS. 8 to 11, in the cylinder liner 1 provided with the intake valve vertical movement concave portion 3 and the exhaust valve vertical movement concave portion 13, the injection port body 10 of the fuel injection valve is provided.
Next, a configuration in which two types of nozzles, the auxiliary nozzle 7 and the main nozzle 6, are provided will be described. The number of auxiliary injection holes 7 is the same as the number of intake valve vertical movement concave portions 3 and the number of exhaust valve vertical movement concave portions 13. In this embodiment, the number is two. The position of the auxiliary injection port 7 is set in a certain direction of the intake valve vertical movement concave portion 3 and the exhaust valve vertical movement concave portion 13.
At the position where the auxiliary injection hole 7 is bored, the intersection of the center line of the auxiliary injection hole 7 and the inner wall of the cylinder liner 1 is 1/2 of the top clearance.
It is configured to be

【0016】該主噴口6と副噴口7は、図10に示す如
く上下の位置に穿孔されている。そして主噴口6は円周
上を8等分した位置に噴口径mを大径として穿孔してい
る。また副噴口7は主噴口6よりも上方の位置に、噴口
径nを小径として穿孔している。また主噴口6の成す角
度aは副噴口7の成す角度bよりも小に構成している。
このように構成することにより、図8と図9に示す如
く、副噴口7からの燃料噴霧流9は上方で細く長く噴霧
され、主噴口6からの燃料噴霧流8は、太く短くピスト
ンPの頂部の穿設凹部に向かって噴霧されるように構成
している。
The main injection port 6 and the sub injection port 7 are perforated at upper and lower positions as shown in FIG. Further, the main injection port 6 is bored at a position that divides the circumference into eight equal parts with the injection port diameter m being large. Further, the auxiliary injection port 7 is bored at a position above the main injection port 6 with the injection port diameter n being small. The angle a formed by the main injection port 6 is smaller than the angle b formed by the sub injection port 7.
With this configuration, as shown in FIGS. 8 and 9, the fuel spray flow 9 from the sub injection port 7 is sprayed upward in a thin and long manner, and the fuel spray flow 8 from the main injection port 6 is thick and short and It is configured to be sprayed toward the perforated concave portion at the top.

【0017】そして、本発明の副噴口7から出た燃料噴
霧流9は、吸気バルブ上下動凹部3と排気バルブ上下動
凹部13の方向に向けられており、燃料噴霧流9は燃料
噴霧流8よりも到達距離を長く構成することが出来たの
である。そしてこのように、主噴口6と副噴口7を構成
したことによる効果は、図11に示す如く、出力を下げ
た場合にも、排気色が上昇しないディーゼル機関とする
ことが出来たのである。
The fuel spray flow 9 discharged from the auxiliary injection port 7 of the present invention is directed toward the intake valve vertical movement recess 3 and the exhaust valve vertical movement recess 13, and the fuel spray flow 9 is the fuel spray flow 8. It was possible to construct a longer reach. As described above, the effect obtained by constructing the main injection port 6 and the sub injection port 7 is that a diesel engine in which the exhaust color does not increase even when the output is reduced as shown in FIG.

【0018】[0018]

【発明の効果】本発明は以上の如く構成したので、次の
ような効果を奏するのである。請求項1の如く構成した
ので、吸気ポート5からの流入空気の流れの一部が、吸
気バルブ上下動凹部3に衝突しないように構成すること
が出来たので、見かけのポートの断面積は減少したが、
吸気流の流線をスムーズに揃えることにより、滞留して
しまう吸気流の流線dや本線に戻ろうとする吸気流の流
線gが無くなり、吸入空気量は増大した。これにより、
流入空気量を増大することが出来るので、燃費と熱負荷
の低減を図り、排気色の悪化を防ぐことができたのであ
る。
Since the present invention is constructed as described above, it has the following effects. According to the first aspect of the present invention, it is possible to prevent a part of the flow of the inflowing air from the intake port 5 from colliding with the intake valve vertical movement recessed portion 3, so that the apparent cross-sectional area of the port is reduced. However,
By smoothly aligning the flow line of the intake flow, the flow line d of the intake flow that stagnates and the flow line g of the intake flow that tries to return to the main line are eliminated, and the intake air amount is increased. This allows
Since the amount of inflowing air can be increased, fuel consumption and heat load can be reduced, and deterioration of exhaust color can be prevented.

【0019】請求項2の如く構成したので、噴霧到達距
離を充分に得ることが出来るので、良好な燃焼が得られ
るのである。
According to the second aspect of the invention, since the spray reaching distance can be sufficiently obtained, good combustion can be obtained.

【図面の簡単な説明】[Brief description of drawings]

【図1】本発明のシリンダライナ1とバルブ座4の部分
を示す平面図。
FIG. 1 is a plan view showing a cylinder liner 1 and a valve seat 4 of the present invention.

【図2】本発明のバルブ座4とシリンダライナ1と吸気
バルブ2の部分の側面一部断面図。
FIG. 2 is a partial side sectional view of a valve seat 4, a cylinder liner 1 and an intake valve 2 of the present invention.

【図3】本発明の吸気バルブ座4と吸気ポート5の関係
位置を示す図面。
FIG. 3 is a drawing showing a relational position between an intake valve seat 4 and an intake port 5 of the present invention.

【図4】本発明の吸気流の流線を示す俯瞰図。FIG. 4 is an overhead view showing the streamline of the intake air flow of the present invention.

【図5】従来の吸気バルブ座4と吸気ポート5の関係位
置を示す平面図と側面図。
5A and 5B are a plan view and a side view showing a related position of a conventional intake valve seat 4 and an intake port 5.

【図6】従来の吸気流の流線を示す俯瞰図。FIG. 6 is an overhead view showing a streamline of a conventional intake air flow.

【図7】本発明の吸気ポート5の形状と、従来の吸気ポ
ート5の形状との吸気流量の比較を示す図面。
FIG. 7 is a drawing showing a comparison of intake flow rates between the shape of the intake port 5 of the present invention and the shape of the conventional intake port 5.

【図8】主噴口6と副噴口7を設けた発明の燃料噴霧流
を示す側面図。
FIG. 8 is a side view showing a fuel spray flow of the invention in which a main injection port 6 and a sub injection port 7 are provided.

【図9】同じく主噴口6と副噴口7の燃料噴霧流の平面
図。
FIG. 9 is a plan view of the fuel spray flow of the main injection port 6 and the sub injection port 7 in the same manner.

【図10】副噴口7と主噴口6の位置関係を示す側面断
面図。
FIG. 10 is a side cross-sectional view showing the positional relationship between the sub injection port 7 and the main injection port 6.

【図11】本発明と従来構造との、出力と排気色との関
係を示す図面。
FIG. 11 is a drawing showing the relationship between output and exhaust color between the present invention and a conventional structure.

【符号の説明】[Explanation of symbols]

1 シリンダライナ 2 吸気バルブ 3 吸気バルブ上下動凹部 4 吸気バルブ座 5 吸気ポート 6 主噴口 7 副噴口 8 燃料噴霧流 9 燃料噴霧流 13 排気バルブ上下動凹部 14 排気バルブ座 15 排気ポート 1 Cylinder liner 2 Intake valve 3 Intake valve vertical movement recess 4 Intake valve seat 5 Intake port 6 Main injection port 7 Sub injection port 8 Fuel spray flow 9 Fuel spray flow 13 Exhaust valve vertical movement recess 14 Exhaust valve seat 15 Exhaust port

Claims (2)

【特許請求の範囲】[Claims] 【請求項1】 内燃機関のシリンダライナ1の外周より
も外側に、吸気バルブ2のバルブ座4の外周が突出し、
該シリンダライナ1の上端に、該吸気バルブ2を上下動
可能とする吸気バルブ上下動凹部3を設けた構成におい
て、吸気バルブ2のバルブ座4に連通する吸気ポート5
の出口側を吸気バルブ上下動凹部3に沿わせずに、シリ
ンダライナ1のバルブ上下動凹部3より下部の円弧外周
に沿った形状としたことを特徴とするディーゼル機関。
1. An outer periphery of a valve seat 4 of an intake valve 2 projects outside the outer periphery of a cylinder liner 1 of an internal combustion engine,
An intake port 5 communicating with a valve seat 4 of the intake valve 2 in a structure in which an intake valve vertical movement recess 3 that allows the intake valve 2 to move vertically is provided at the upper end of the cylinder liner 1.
The diesel engine is characterized in that the outlet side of the intake valve vertical movement concave portion 3 is not provided, and the shape is along the arc outer periphery of the cylinder liner 1 below the valve vertical movement concave portion 3.
【請求項2】 燃料弁の噴口として、主噴口6に加えて
副噴口7を有する内燃機関において、副噴口7の噴口径
は、主噴口6の噴口径よりも小さくし、副噴口7は主噴
口6の噴口角よりも大きくし、シリンダライナ1の吸気
バルブ上下動凹部3の中心線上に副噴口7を配置したこ
とを特徴とするディーゼル機関。
2. In an internal combustion engine having a secondary injection port 7 in addition to the main injection port 6 as the injection port of the fuel valve, the auxiliary injection port 7 has a smaller injection port diameter than the main injection port 6, and the auxiliary injection port 7 is the main injection port. A diesel engine, characterized in that the auxiliary injection port 7 is larger than the injection port angle of the injection port 6 and is arranged on the center line of the intake valve vertical movement recessed portion 3 of the cylinder liner 1.
JP23729594A 1994-09-30 1994-09-30 Diesel engine Expired - Fee Related JP3330745B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP23729594A JP3330745B2 (en) 1994-09-30 1994-09-30 Diesel engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP23729594A JP3330745B2 (en) 1994-09-30 1994-09-30 Diesel engine

Publications (2)

Publication Number Publication Date
JPH08100702A true JPH08100702A (en) 1996-04-16
JP3330745B2 JP3330745B2 (en) 2002-09-30

Family

ID=17013256

Family Applications (1)

Application Number Title Priority Date Filing Date
JP23729594A Expired - Fee Related JP3330745B2 (en) 1994-09-30 1994-09-30 Diesel engine

Country Status (1)

Country Link
JP (1) JP3330745B2 (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2008041084A2 (en) * 2006-10-02 2008-04-10 Toyota Jidosha Kabushiki Kaisha Internal combustion engine
JP2008088900A (en) * 2006-10-02 2008-04-17 Toyota Motor Corp Intake port shape for internal combustion engine
JP2009062971A (en) * 2007-08-14 2009-03-26 Mazda Motor Corp Fuel injection device of diesel engine
WO2016121482A1 (en) * 2015-01-29 2016-08-04 三菱自動車工業株式会社 Intake port structure for engine
JP2020143607A (en) * 2019-03-05 2020-09-10 株式会社Ihi engine

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2008041084A2 (en) * 2006-10-02 2008-04-10 Toyota Jidosha Kabushiki Kaisha Internal combustion engine
JP2008088900A (en) * 2006-10-02 2008-04-17 Toyota Motor Corp Intake port shape for internal combustion engine
WO2008041084A3 (en) * 2006-10-02 2008-05-29 Toyota Jidosha Kabushiki Kaisy Internal combustion engine
JP4692459B2 (en) * 2006-10-02 2011-06-01 トヨタ自動車株式会社 Intake port shape of internal combustion engine
JP2009062971A (en) * 2007-08-14 2009-03-26 Mazda Motor Corp Fuel injection device of diesel engine
WO2016121482A1 (en) * 2015-01-29 2016-08-04 三菱自動車工業株式会社 Intake port structure for engine
JP2020143607A (en) * 2019-03-05 2020-09-10 株式会社Ihi engine

Also Published As

Publication number Publication date
JP3330745B2 (en) 2002-09-30

Similar Documents

Publication Publication Date Title
JP6215943B2 (en) Diesel engine combustion chamber structure
KR0149975B1 (en) Water injection type diesel engine
US4995359A (en) Combustion chamber for internal combustion engine
US3273551A (en) Cylinder inlet passage for an internal combustion engine
US5335634A (en) Combustion chamber structure for an engine
US6062192A (en) Internal combustion engine with spark ignition
EP0769610B1 (en) A fuel injection system for a lean burn engine
JPH08100702A (en) Diesel engine
EP0595316B1 (en) Cylinder head and valve arrangement of a multi-valve internal combustion engine
JP2017025929A (en) Combustion chamber structure of diesel engine
JPH10252477A (en) Direct cylinder fuel injection type spark ignition engine
US6666186B2 (en) Spark ignited internal combustion engine with at least one cylinder
JPH0735002A (en) Fuel injection nozzle of direct injection type diesel engine
JP2532390Y2 (en) Combustion chamber of a direct injection diesel engine
JPH0921321A (en) Fuel injection method for direct injection type diesel engine, piston and injection nozzle employed by the method
JP2900805B2 (en) Diesel engine intake system
US2672852A (en) Combustion chamber for four cycle diesel engines
JPH0723537Y2 (en) Combustion chamber of direct injection diesel engine
JPH0861188A (en) Hole type injection nozzle
JPH0736089Y2 (en) Direct injection diesel engine
KR100219205B1 (en) Cylinder head for direct injection
JP4039393B2 (en) Cylinder head structure of direct-injection spark ignition internal combustion engine
JP2022039691A (en) Internal combustion engine
JPH0223789Y2 (en)
JPH09217626A (en) Direct injection four valve diesel engine

Legal Events

Date Code Title Description
LAPS Cancellation because of no payment of annual fees