JPH07317542A - Cylinder direct injection type engine - Google Patents

Cylinder direct injection type engine

Info

Publication number
JPH07317542A
JPH07317542A JP6112992A JP11299294A JPH07317542A JP H07317542 A JPH07317542 A JP H07317542A JP 6112992 A JP6112992 A JP 6112992A JP 11299294 A JP11299294 A JP 11299294A JP H07317542 A JPH07317542 A JP H07317542A
Authority
JP
Japan
Prior art keywords
combustion chamber
cylinder
piston
fuel injection
nozzle
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.)
Pending
Application number
JP6112992A
Other languages
Japanese (ja)
Inventor
Hirofumi Sakamoto
浩文 坂本
Ten Ito
天 伊藤
Yasuo Sato
康夫 佐藤
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.)
Toyota Industries Corp
Toyota Motor Corp
Original Assignee
Toyota Motor Corp
Toyoda Automatic Loom Works 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 Toyota Motor Corp, Toyoda Automatic Loom Works Ltd filed Critical Toyota Motor Corp
Priority to JP6112992A priority Critical patent/JPH07317542A/en
Publication of JPH07317542A publication Critical patent/JPH07317542A/en
Pending 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
    • F02B23/00Other engines characterised by special shape or construction of combustion chambers to improve operation
    • F02B23/02Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition
    • F02B23/06Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition the combustion space being arranged in working piston
    • F02B23/0675Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition the combustion space being arranged in working piston the combustion space being substantially spherical, hemispherical, ellipsoid or parabolic
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B2275/00Other engines, components or details, not provided for in other groups of this subclass
    • F02B2275/14Direct injection into combustion chamber
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B23/00Other engines characterised by special shape or construction of combustion chambers to improve operation
    • F02B23/02Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition
    • F02B23/06Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition the combustion space being arranged in working piston
    • F02B23/0645Details related to the fuel injector or the fuel spray
    • F02B23/066Details related to the fuel injector or the fuel spray the injector being located substantially off-set from the cylinder centre axis
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B23/00Other engines characterised by special shape or construction of combustion chambers to improve operation
    • F02B23/02Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition
    • F02B23/06Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition the combustion space being arranged in working piston
    • F02B23/0645Details related to the fuel injector or the fuel spray
    • F02B23/0669Details related to the fuel injector or the fuel spray having multiple fuel spray jets per injector nozzle
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B23/00Other engines characterised by special shape or construction of combustion chambers to improve operation
    • F02B23/02Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition
    • F02B23/06Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition the combustion space being arranged in working piston
    • F02B23/0696W-piston bowl, i.e. the combustion space having a central projection pointing towards the cylinder head and the surrounding wall being inclined towards the cylinder wall
    • 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

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Combustion Methods Of Internal-Combustion Engines (AREA)

Abstract

PURPOSE:To provide a small-sized compressive ignition type engine equipped with a fuel injection nozzle having a high injection pressure, wherein the fuel is injected uniformly into the combustion chamber and dispersed so that fuel sticking to the wall surface is prevented. CONSTITUTION:A combustion chamber 7 is formed by recesses 7a, 7b provided at the opposing surfaces of a cylinder head 5 and a piston 3, in such a shape as segment shells spreading downward aslant on the counter-side of piston 3 to the base point in which the position aslant over the cylinder head 5 and dislocated aside from the area right over the cylinder bore is used as the base point, and the jet 8a of a hole type fuel injection nozzle 8 having a high directionality and having an injection pattern similar to the shape of the combustion chamber 7 is located at this base point. The jet 8a is formed continuously in the combustion chamber spreading direction.

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、シリンダ内を上下動す
るピストンの上面に形成された凹部と、シリンダヘッド
における前記ピストンの上面に対向する面に形成された
凹部とで燃焼室を形成し、その燃焼室の上部に燃料噴射
弁を備えた筒内直噴式エンジンに関する。
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention forms a combustion chamber by a recess formed in the upper surface of a piston that moves up and down in a cylinder and a recess formed in a surface of a cylinder head that faces the upper surface of the piston. , An in-cylinder direct injection engine having a fuel injection valve in the upper part of its combustion chamber.

【0002】[0002]

【従来の技術】近年、排気ガス規制の強化に伴ない、殊
に圧縮着火式エンジンでは燃料の噴射圧力を増大させる
要求が強くなっている。そのため燃料噴霧の貫徹力が強
まってこれまでの燃焼室形状では噴霧を均一に拡散させ
にくい。レシプロエンジンにおいて、自然吸気式では、
図5に示す如く、ピストン3とシリンダヘッド5との各
対向面に夫々形成された一対の凹部7a、7bによって
略球形の燃焼室7を形成し、渦流的な高スワールにより
空気との混合促進を図る技術(特開昭59−60024
号公報に開示)が知られているし、筒内直噴式エンジン
では、図6に示す如く、シリンダヘッド5に形成した扁
平な燃焼室7とシリンダ室1aとの間に、ボア径より小
さな開口12aを有した仕切り壁12を設け、噴射ノズ
ル8を中央上方に配置した技術(特開昭63−5062
1号公報に開示)や、図7に示す如く、シリンダヘッド
5に円錐形の凹部7aを形成すると共に、ピストン3の
上面に燃料拡散溝13を形成し、ユニットインジェクタ
14の噴射口を前記凹部7a頂点に配置した技術(特開
昭64−35011号公報に開示)、更には図8に示す
如く、シリンダヘッド5の下面に形成された凹部7aに
4つのバルブ15,15・・をV状に配置すると共に、
その中央部にユニットインジェクタ14を配置し、ピス
トン3の頂面を円錐状に窪ませてその外周をトロイダル
形状とした技術(実開平2−1423号公報参照)等、
燃焼室をシリンダヘッド5とピストン3とに跨って形成
した構造が知られている。
2. Description of the Related Art In recent years, as exhaust gas regulations have been tightened, there has been an increasing demand for increasing fuel injection pressure, especially in compression ignition engines. Therefore, the penetrating force of the fuel spray is increased and it is difficult to uniformly diffuse the spray in the conventional combustion chamber shape. In the reciprocating engine, the naturally aspirated type,
As shown in FIG. 5, a substantially spherical combustion chamber 7 is formed by a pair of concave portions 7a and 7b formed on the respective facing surfaces of the piston 3 and the cylinder head 5, and a swirling high swirl promotes mixing with air. Technology for achieving the above (Japanese Patent Laid-Open No. 59-60024)
In the in-cylinder direct injection engine, as shown in FIG. 6, an opening smaller than the bore diameter is formed between the flat combustion chamber 7 formed in the cylinder head 5 and the cylinder chamber 1a. A technique in which a partition wall 12 having 12a is provided and the injection nozzle 8 is arranged in the upper center (Japanese Patent Laid-Open No. 63-5062).
No. 1) or as shown in FIG. 7, a conical recess 7a is formed in the cylinder head 5, a fuel diffusion groove 13 is formed in the upper surface of the piston 3, and the injection port of the unit injector 14 is formed in the recess. The technique of arranging at the apex of 7a (disclosed in Japanese Patent Laid-Open No. 64-35011), and further, as shown in FIG. 8, four valves 15, 15, ... Are V-shaped in a recess 7a formed in the lower surface of the cylinder head 5. And place it in
A technique in which the unit injector 14 is arranged in the central portion of the piston 3, the top surface of the piston 3 is conically recessed, and the outer periphery of the piston 3 has a toroidal shape (see Japanese Utility Model Publication No. 2-1423).
A structure is known in which a combustion chamber is formed across the cylinder head 5 and the piston 3.

【0003】[0003]

【発明が解決しようとする課題】これまでに開発された
従来の技術では、圧縮着火式エンジンの場合、排気量が
少ない(ボア径が100mm以下)と、噴射方向に対して
充分な燃焼室の容積を確保するのが難かしく、燃料が壁
面に付着して燃焼効率の低下を招く。又燃焼室の内壁面
積が少なく、バルブの径を大きくする余裕がないため、
吸気や排気の効率が悪く、高出力を得ることができな
い。更に燃焼室の容積を増加すべく上方に拡大すれば、
シリンダヘッドが巨大化して搭載性が悪くなり、そのた
め高性能で搭載性に優れた小型エンジンの製造ができな
かった。而も従来の燃焼室形状の場合、燃焼室内へ一様
に噴霧を供給するには、ピン型ノズルが好適に使用され
るが、ピン部の熱容量が大きいため、燃料等が冷やされ
易く、スモークの発生や噴孔詰まりを起こす虞れがあっ
た。
In the conventional technology developed so far, in the case of the compression ignition type engine, when the displacement is small (bore diameter is 100 mm or less), the combustion chamber which is sufficient in the injection direction can be obtained. It is difficult to secure the volume, and the fuel adheres to the wall surface, leading to a decrease in combustion efficiency. Also, because the inner wall area of the combustion chamber is small and there is no room to increase the valve diameter,
Intake and exhaust efficiency is poor, and high output cannot be obtained. If it is expanded upward to increase the volume of the combustion chamber,
Since the cylinder head became huge and the mountability deteriorated, it was not possible to manufacture a small engine with high performance and excellent mountability. In addition, in the case of the conventional combustion chamber shape, the pin type nozzle is preferably used to uniformly supply the spray into the combustion chamber, but since the heat capacity of the pin portion is large, the fuel and the like are easily cooled, and the smoke There is a possibility that the occurrence of a crack may occur or the nozzle hole may be clogged.

【0004】[0004]

【課題を解決するための手段】本発明は、エンジンの排
気量が小さくても、搭載性を犠牲にすることなく大きな
容積の燃焼室を確保可能な筒内直噴式エンジンであっ
て、その構成は、燃焼室をシリンダボアの真上にあたる
エリアから側方に膨出形成し、その膨出部分に前記燃料
噴射弁を配置したことにあり、前記燃焼室は、燃料噴射
弁のノズルを基点として斜め下方へ向けて水平方向へ拡
がった扇状パターンに形成し、前記燃料噴射弁をホール
型燃料噴射ノズルにすると共に、そのノズル先端の噴口
を前記燃焼室の拡がり方向に沿って連続的に形成するこ
とができる。
SUMMARY OF THE INVENTION The present invention is an in-cylinder direct injection type engine capable of ensuring a large-capacity combustion chamber without sacrificing mountability even if the engine displacement is small. Is that the combustion chamber is formed to bulge laterally from the area directly above the cylinder bore, and the fuel injection valve is arranged in the bulging portion, and the combustion chamber is inclined with respect to the nozzle of the fuel injection valve. Forming a fan-shaped pattern that spreads downward in the horizontal direction, making the fuel injection valve a Hall-type fuel injection nozzle, and continuously forming an injection port at the tip of the nozzle along the expansion direction of the combustion chamber You can

【0005】そして前記燃焼室のシリンダヘッド側の内
壁面には断熱材をコーティングすることが望ましい。尚
本発明においての上下方向は、シリンダが垂直姿勢であ
る場合についての表現であり、シリンダが傾斜していた
り水平姿勢の場合は、ピストンの往復運動方向を上下方
向と解する。
It is desirable that the inner wall surface of the combustion chamber on the cylinder head side be coated with a heat insulating material. The vertical direction in the present invention is an expression when the cylinder is in a vertical posture, and when the cylinder is tilted or in a horizontal posture, the reciprocating movement direction of the piston is understood as a vertical direction.

【0006】[0006]

【作用】燃焼室の一部をシリンダボアの真上にあたるエ
リアから側方に膨出形成したので、低いスペースでも噴
射方向に距離を大きく取ることができると共に、広い燃
焼室と大きなバルブ開口面積も確保できるし、小型エン
ジンに噴射圧が高い噴射ノズルを採用した場合であって
も、燃料の壁面付着がおこりにくくなり、燃焼効率の低
下を招くことはない。又燃焼室を、燃料噴射弁のノズル
を基点として斜め下方へ向けて水平方向へ拡がった扇状
パターンに形成することにより、ピン型ノズルに比べて
熱容量の小さいホール型ノズルの使用が可能となって、
噴孔詰まりがなくなるし、ノズル先端の噴口を燃焼室の
拡がり方向に沿って連続的に形成したことにより、燃焼
室内の酸素が有効に無駄なく活用される。
[Function] Since a part of the combustion chamber is bulged laterally from the area directly above the cylinder bore, a large distance can be secured in the injection direction even in a low space, and a wide combustion chamber and a large valve opening area are secured. Even if the injection nozzle having a high injection pressure is adopted for the small engine, the fuel is less likely to adhere to the wall surface, and the combustion efficiency is not reduced. In addition, by forming the combustion chamber in a fan-shaped pattern that spreads in the horizontal direction diagonally downward from the nozzle of the fuel injection valve, it is possible to use a Hall-type nozzle with a smaller heat capacity than a pin-type nozzle. ,
The clogging of the injection hole is eliminated and the injection hole at the tip of the nozzle is continuously formed along the expansion direction of the combustion chamber, so that oxygen in the combustion chamber is effectively utilized without waste.

【0007】[0007]

【実施例】本発明に係る筒内直噴式エンジンを圧縮着火
式エンジンにおいて実施した一例を図面に基づいて説明
する。図1において、1はシリンダブロックであり、こ
のシリンダブロック1には気筒数に相当する数の縦に長
いシリンダ室1aが形成され、その周囲に冷却水を循環
させる水ジャケット2を備えたものとなっている。3は
前記シリンダ室1a内を上下方向へ往復移動自在に収容
されているピストンであり、このピストン3は、ピスト
ン3の往復運動方向と直交方向に架設されたピストンピ
ン3a及びそのピストンピン3aに軸着されたコネクテ
ィングロッド4を介して図示しないクランクシャフトと
連結されている。前記ピストン3の周面には、リング溝
を利用してピストンリング3b,3b,3bが嵌着され
ている。
DESCRIPTION OF THE PREFERRED EMBODIMENTS An example in which a direct injection type cylinder engine according to the present invention is implemented in a compression ignition type engine will be described with reference to the drawings. In FIG. 1, reference numeral 1 denotes a cylinder block, which is provided with a vertically long cylinder chamber 1a corresponding to the number of cylinders, around which a water jacket 2 for circulating cooling water is provided. Has become. Reference numeral 3 denotes a piston which is housed in the cylinder chamber 1a so as to be reciprocally movable in the vertical direction. The piston 3 is mounted on the piston pin 3a and the piston pin 3a which are installed in a direction orthogonal to the reciprocating direction of the piston 3. It is connected to a crankshaft (not shown) via a connecting rod 4 which is axially mounted. Piston rings 3b, 3b, 3b are fitted to the peripheral surface of the piston 3 by using ring grooves.

【0008】5はシリンダヘッドであり、前記シリンダ
ブロック1に対し、シリンダ室1aの開口上面を覆うよ
うに組み付けられ、密着面にはガスケット6が介在され
ている。尚シリンダヘッド5は、二分割構造となってい
る。シリンダヘッド5と前記ピストン3との対向面に
は、夫々凹部7a,7bが形成されており、図示の如く
ピストン3が上死点位置に到達した状態において、前記
凹部7aと凹部7bとで、シリンダボアの真上にあたる
エリアから側方に膨出した燃焼室7が形成される。凹部
7a,7bにより形成される燃焼室7は、図2に示す如
く、シリンダヘッド5の斜め上方が、シリンダボアの真
上にあたるエリアより側方に偏位した位置を基点に、反
対側の斜め下方へ向けて拡がった扇状二枚貝の如き形状
を呈し、シリンダヘッド5には、ホール型の噴射ノズル
8が、図3に示す如く、噴射方向を前記燃焼室7の斜め
下方に向けた噴口8aを前記基点位置に臨ませて、垂直
姿勢に取り付け配置されている。
Reference numeral 5 denotes a cylinder head, which is assembled to the cylinder block 1 so as to cover the upper surface of the opening of the cylinder chamber 1a, and a gasket 6 is interposed on the contact surface. The cylinder head 5 has a two-part structure. Recesses 7a and 7b are formed on the facing surfaces of the cylinder head 5 and the piston 3, respectively. When the piston 3 reaches the top dead center position as shown in the drawing, the recess 7a and the recess 7b A combustion chamber 7 is formed which bulges laterally from an area immediately above the cylinder bore. As shown in FIG. 2, the combustion chamber 7 formed by the recessed portions 7a and 7b has a diagonally upper side of the cylinder head 5 which is located at a position deviated laterally from an area immediately above the cylinder bore, and is diagonally lower on the opposite side. The cylinder head 5 has a shape like a fan-shaped bivalve, and a hole-type injection nozzle 8 has an injection port 8a whose injection direction is obliquely downward of the combustion chamber 7, as shown in FIG. It is installed in a vertical position facing the base point.

【0009】前記噴射ノズル8は噴射圧力の高いタイプ
が装備され、指向性が強く、前記燃焼室の拡がり方向に
沿って連続的に形成された噴口8aからは、燃料が前記
燃焼室7の形状に近似したパターンで噴射される。即
ち、燃焼室7は装備される噴射ノズル8の噴射パターン
形状と略一致した形状になっているのである。前記噴口
8aとしては、例えば針穴9,9・・を横一列に並べて
構成されるタイプ(図4a)、一本のスリット10のみ
で構成されるタイプ(図4b)を始めとし、それら針穴
9やスリット10を複数列設けるタイプ(図4c及び
d)、更にはそれらの針穴やスリットを組み合わせた複
合タイプなどのパターンが考えられ、それらの噴出口か
ら噴射される燃料の噴射パターンは、扇状二枚貝の如き
実施例に示す形状に限定するものでなく、紡錐形、或は
先端が分裂した二股や八ツ手状等の噴射パターンを有し
た噴射ノズルを採用することも可能であって、その場
合、燃焼室はそれらの噴射パターンの外形に近似した形
状を理想とする。熱容量の小さいホール型ノズルの使用
によって、燃料等の温度低下が少なく、スモークの発生
や噴孔詰まりがなくなるし、特に、噴口が図4b,図4
dのようなスリット状の場合は、燃焼室内の酸素を有効
に利用される。前記燃焼室7の内壁面には、シリンダヘ
ッド5側、即ち凹部7a内壁面に断熱材としてのセラミ
ックのコーティング層11が設けられている。
The injection nozzle 8 is equipped with a type having a high injection pressure, has a strong directivity, and a fuel is formed in the shape of the combustion chamber 7 from an injection port 8a which is continuously formed along the spreading direction of the combustion chamber. It is injected in a pattern similar to. That is, the combustion chamber 7 has a shape that substantially matches the shape of the injection pattern of the installed injection nozzle 8. The injection port 8a includes, for example, a type in which needle holes 9, 9, ... Are arranged side by side in a row (FIG. 4a) and a type in which only one slit 10 is formed (FIG. 4b). 9 and slits 10 are provided in a plurality of rows (FIGS. 4c and d), and further, a pattern such as a composite type in which those needle holes and slits are combined is conceivable, and the injection pattern of the fuel injected from these injection ports is It is not limited to the shape shown in the embodiment such as a fan-shaped bivalve, it is also possible to adopt a spray nozzle, or a spray nozzle having a spray pattern such as a bifurcated or eight-handed split tip, In this case, the combustion chamber ideally has a shape similar to the outer shape of those injection patterns. By using the hole type nozzle with a small heat capacity, the temperature of fuel and the like is less likely to drop, smoke is not generated, and the nozzle hole is not clogged.
In the case of a slit like d, oxygen in the combustion chamber is effectively used. On the inner wall surface of the combustion chamber 7, a ceramic coating layer 11 as a heat insulating material is provided on the cylinder head 5 side, that is, on the inner wall surface of the recess 7a.

【0010】燃焼室がこのように形成されたエンジンで
は、燃料の噴射パターンと燃焼室形状とが略一致してい
るので、高圧で噴射された燃料も燃焼室内で均一に拡散
し、壁面に燃料が付着することがなくなり、小型の筒内
直噴式エンジンにあっても、理想の燃焼状態が実現され
る。而も上下方向に対して燃料噴射方向を傾斜させたの
で、その分シリンダヘッドの高さが低くなって、小型化
の要求に対し設計上有利となるし、噴射ノズルを横姿勢
に配置してシリンダヘッドをより薄型化することが可能
となる。又ボア径が100mm以下の小型エンジンであっ
ても、バルブの開口面積を大きくできるし、更に燃焼室
の内壁面に設けたセラミックのコーティング層による断
熱効果により、水ジャケット内の冷却水の影響を受け難
く、着火タイミングの遅れが極めて少ないため、完全燃
焼に近い燃焼状態となって、炭化水素化合物(ハイドロ
カーボン)等や有害ガス(窒素酸化物)の排出が少なく
なるといったメリットがある。
In an engine in which the combustion chamber is formed in this way, the fuel injection pattern and the shape of the combustion chamber are substantially the same, so the fuel injected at high pressure is also diffused uniformly in the combustion chamber, and the fuel is deposited on the wall surface. Is adhered, and an ideal combustion state is realized even in a small direct injection cylinder engine. Moreover, since the fuel injection direction is inclined with respect to the vertical direction, the height of the cylinder head is lowered correspondingly, which is advantageous in design for the demand for miniaturization, and the injection nozzle is arranged in a horizontal position. The cylinder head can be made thinner. Even for a small engine with a bore diameter of 100 mm or less, the valve opening area can be increased, and the ceramic coating layer provided on the inner wall of the combustion chamber can also prevent the influence of cooling water in the water jacket. Since it is hard to receive and the ignition timing is very little delayed, there is an advantage that the combustion state becomes close to complete combustion and the emission of hydrocarbon compounds (hydrocarbons) and harmful gas (nitrogen oxides) is reduced.

【0011】尚本発明の筒内直噴式エンジンにおける燃
焼室構造は、小型の圧縮着火式エンジンにおいて顕著な
効果を発揮するが、大型のエンジンや電気着火式エンジ
ンにも適用可能である。
The combustion chamber structure of the direct injection type cylinder engine of the present invention exerts a remarkable effect in a small compression ignition engine, but can be applied to a large engine or an electric ignition engine.

【0012】[0012]

【発明の効果】本発明によれば、傾斜燃焼室の採用によ
り、ボア径の小さい小型の筒内直噴式エンジンに、噴射
圧力の高い燃料噴射ノズルを取り付けても、燃料噴射時
における燃焼室内壁への付着が防止され、完全燃焼に近
い状態が期待でき、ディーゼル黒煙やハイドロカーボン
の排出量が減少する。又シリンダヘッドの高さが低くな
るので、エンジン全体を小型化するには好適であり、燃
焼室設計の大きさに対する制限が少なくなって、搭載性
も良くなる。更に燃焼室の内壁面にセラミックのコーテ
ィング層を設けることにより、冷却水の影響を受けにく
くなって、着火遅れの時間が短く、窒素酸化物の排出量
が激減し、燃焼音も静かになる利点がある。更にホール
型ノズルの使用が可能となり、噴孔詰まりを起こしにく
くなる。
According to the present invention, by adopting the inclined combustion chamber, even if a fuel injection nozzle having a high injection pressure is attached to a small in-cylinder direct injection engine having a small bore diameter, a combustion chamber inner wall at the time of fuel injection is provided. It is possible to expect the state to be close to complete combustion, and to reduce the emission of diesel black smoke and hydrocarbons. Further, since the height of the cylinder head is low, it is suitable for downsizing the entire engine, and the restrictions on the size of the combustion chamber are reduced, and the mountability is improved. Furthermore, by providing a ceramic coating layer on the inner wall surface of the combustion chamber, it is less affected by cooling water, the ignition delay time is shorter, the emission of nitrogen oxides is drastically reduced, and the combustion noise is quiet. There is. Furthermore, it becomes possible to use a hole-type nozzle, and it becomes difficult for clogging of the injection hole to occur.

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

【図1】 本発明に係る筒内直噴式エンジンの燃焼室部
分を示す説明図である。
FIG. 1 is an explanatory view showing a combustion chamber portion of a direct injection type cylinder engine according to the present invention.

【図2】 燃焼室形状の説明図である。FIG. 2 is an explanatory view of the shape of a combustion chamber.

【図3】 ホール型燃料噴射ノズルが、その噴口を燃焼
室内に臨ませて配置された状態の説明図である。
FIG. 3 is an explanatory diagram showing a state in which the Hall-type fuel injection nozzle is arranged with its injection port facing the combustion chamber.

【図4】 燃料噴射ノズルの噴口を例示した説明図であ
る。
FIG. 4 is an explanatory view illustrating an injection port of a fuel injection nozzle.

【図5】 従来例の説明図である。FIG. 5 is an explanatory diagram of a conventional example.

【図6】 従来例の説明図である。FIG. 6 is an explanatory diagram of a conventional example.

【図7】 従来例の説明図である。FIG. 7 is an explanatory diagram of a conventional example.

【図8】 従来例の説明図である。FIG. 8 is an explanatory diagram of a conventional example.

【符号の説明】[Explanation of symbols]

1・・シリンダブロック、1a・・シリンダ室、2・・
水ジャケット、3・・ピストン、3a・・ピストンピ
ン、3b・・ピストンリング、4・・コネクティングロ
ッド、5・・シリンダヘッド、6・・ガスケット、7・
・燃焼室、7a,7b・・凹部、8・・噴射ノズル、8
a・・噴口、9・・針穴、10・・スリット、11・・
コーテング層、12・・仕切り壁、12a・・開口、1
3・・燃料拡散溝、14・・ユニットインジェクタ、1
5・・バルブ。
1 ... Cylinder block, 1a ... Cylinder chamber, 2 ...
Water jacket, 3 ・ ・ Piston, 3a ・ ・ Piston pin, 3b ・ ・ Piston ring, 4 ・ ・ Connecting rod, 5 ・ ・ Cylinder head, 6 ・ ・ Gasket, 7 ・
・ Combustion chambers, 7a, 7b ... Recesses, 8 ... Injection nozzles, 8
a ... Nozzle, 9 ... Needle hole, 10 ... Slit, 11 ...
Coating layer, 12 ... Partition wall, 12a ... Opening, 1
3 ... Fuel diffusion groove, 14 ... Unit injector, 1
5 ... Valve.

───────────────────────────────────────────────────── フロントページの続き (72)発明者 佐藤 康夫 愛知県豊田市トヨタ町1番地 トヨタ自動 車株式会社内 ─────────────────────────────────────────────────── ─── Continuation of the front page (72) Inventor Yasuo Sato 1 Toyota-cho, Toyota-shi, Aichi Toyota Automobile Co., Ltd.

Claims (3)

【特許請求の範囲】[Claims] 【請求項1】 シリンダ内を上下動するピストンの上面
に形成された凹部と、シリンダヘッドにおける前記ピス
トンの上面に対向する面に形成された凹部とで燃焼室を
形成し、その燃焼室の上部に燃料噴射弁を備えた筒内直
噴式エンジンにおいて、前記燃焼室の一部をシリンダボ
アの真上にあたるエリアから側方に膨出形成し、その膨
出部分に前記燃料噴射弁を配置した筒内直噴式エンジ
ン。
1. A combustion chamber is formed by a recess formed in an upper surface of a piston that moves up and down in a cylinder and a recess formed in a surface of a cylinder head that faces the upper surface of the piston, and an upper portion of the combustion chamber. In a direct injection engine having a fuel injection valve in a cylinder, a part of the combustion chamber is formed to bulge laterally from an area directly above the cylinder bore, and the fuel injection valve is arranged in the bulging portion. Direct injection engine.
【請求項2】 前記燃焼室を、燃料噴射弁のノズルを基
点として斜め下方へ向けて水平方向へ拡がった扇状パタ
ーンに形成し、前記燃料噴射弁をホール型燃料噴射ノズ
ルにすると共に、そのノズル先端の噴口を前記燃焼室の
拡がり方向に沿って連続的に形成した請求項1に記載の
筒内直噴式エンジン。
2. The combustion chamber is formed in a fan-shaped pattern that extends in a horizontal direction diagonally downward from the nozzle of the fuel injection valve as a base point, and the fuel injection valve is a Hall-type fuel injection nozzle, and the nozzle thereof is provided. The in-cylinder direct injection engine according to claim 1, wherein the injection port at the tip is continuously formed along the spreading direction of the combustion chamber.
【請求項3】 前記燃焼室のシリンダヘッド側の内壁面
に断熱材をコーティングした請求項1又は2に記載の筒
内直噴式エンジン。
3. The in-cylinder direct injection engine according to claim 1, wherein an inner wall surface of the combustion chamber on the cylinder head side is coated with a heat insulating material.
JP6112992A 1994-05-26 1994-05-26 Cylinder direct injection type engine Pending JPH07317542A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP6112992A JPH07317542A (en) 1994-05-26 1994-05-26 Cylinder direct injection type engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP6112992A JPH07317542A (en) 1994-05-26 1994-05-26 Cylinder direct injection type engine

Publications (1)

Publication Number Publication Date
JPH07317542A true JPH07317542A (en) 1995-12-05

Family

ID=14600718

Family Applications (1)

Application Number Title Priority Date Filing Date
JP6112992A Pending JPH07317542A (en) 1994-05-26 1994-05-26 Cylinder direct injection type engine

Country Status (1)

Country Link
JP (1) JPH07317542A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1241332A1 (en) * 2001-03-16 2002-09-18 Renault s.a.s. Combustion chamber roof
JP2006194190A (en) * 2005-01-14 2006-07-27 Toyota Motor Corp Compression ignition internal combustion engine

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1241332A1 (en) * 2001-03-16 2002-09-18 Renault s.a.s. Combustion chamber roof
JP2006194190A (en) * 2005-01-14 2006-07-27 Toyota Motor Corp Compression ignition internal combustion engine
JP4552660B2 (en) * 2005-01-14 2010-09-29 トヨタ自動車株式会社 Compression ignition internal combustion engine

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