JPS5985424A - Diesel engine of direct injection type - Google Patents

Diesel engine of direct injection type

Info

Publication number
JPS5985424A
JPS5985424A JP57196274A JP19627482A JPS5985424A JP S5985424 A JPS5985424 A JP S5985424A JP 57196274 A JP57196274 A JP 57196274A JP 19627482 A JP19627482 A JP 19627482A JP S5985424 A JPS5985424 A JP S5985424A
Authority
JP
Japan
Prior art keywords
fuel
piston
diesel engine
combustion chamber
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
JP57196274A
Other languages
Japanese (ja)
Inventor
Hiroyuki Sami
佐味 弘之
Mamoru Kamiya
守 神谷
Shinobu Ishiyama
忍 石山
Hiromichi Yanagihara
弘道 柳原
Noriyuki Tokoro
憲之 所
Tatsumi Furukubo
辰巳 古久保
Satoru Watabe
哲 渡部
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 Motor Corp
Original Assignee
Toyota Motor Corp
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 filed Critical Toyota Motor Corp
Priority to JP57196274A priority Critical patent/JPS5985424A/en
Publication of JPS5985424A publication Critical patent/JPS5985424A/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
    • F02B23/0645Details 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
    • F02B23/0675Other 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
    • F02B23/0618Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition the combustion space being arranged in working piston having in-cylinder means to influence the charge motion
    • F02B23/0621Squish flow
    • 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
    • F02B23/0648Means or methods to improve the spray dispersion, evaporation or ignition
    • F02B23/0651Means or methods to improve the spray dispersion, evaporation or ignition the fuel spray impinging on reflecting surfaces or being specially guided throughout the combustion space
    • 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
    • F02B23/0666Details related to the fuel injector or the fuel spray having a single fuel spray jet 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
    • 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 compact the construction of a Diesel engine with its rate of fuel consumption improved by locating the jet hole of the fuel injection nozzle in the neighborhood of the periphery of a dint of the top combustion chamber situated at the upper dead point and by setting the major stream in injection in an angle of 20-30 deg. to the top surface of the piston. CONSTITUTION:A recess 6 is provided in a part of periphery of a dint 5 of the combustion chamber of a piston 4, and a setting is made so that a jet hole 8 of a fuel injection nozzle 7 furnished at the cylinder head 2 is situated at this recess 6 at the time of upper dead point and that the angle alpha formed by the major stream in fuel injection from this jet hole 8 with respect to the top surface of the piston 4 will be 20-30 deg.. This setting of injection angle to 20-30 deg. will prolong the reach of atomized fuel sufficiently, which should enhance the rate of fuel consumption as well as reduce the density of black smoke in the exhaust gas. Thus a sufficient reach can be obtained without a larger compression height of piston, that ensures a compacted construction of Diesel engine.

Description

【発明の詳細な説明】 本発明は、直接噴射式ディーゼル機関に係り、特に自動
車等の車輌に用いられる単一噴霧方式の直接噴射式ディ
ーゼル機関に係る。
DETAILED DESCRIPTION OF THE INVENTION The present invention relates to a direct injection diesel engine, and particularly to a single spray type direct injection diesel engine used in vehicles such as automobiles.

直接11ft DJ式ディーゼル機関は、一般に、シリ
ンダヘッドに取付けられた燃料噴射ノズルを有し、核燃
料噴射ノズルよりピストンの頂部に設けられた燃焼室窪
み内へ向けて軽油の如きディーゼル機関用液体燃料を噴
射供給されるようになっている。
A direct 11ft DJ type diesel engine generally has a fuel injection nozzle attached to the cylinder head, and directs diesel engine liquid fuel such as light oil from the nuclear fuel injection nozzle into the combustion chamber recess provided at the top of the piston. It is supplied by injection.

この種の直接噴射式ディーピル機関に於ては、燃焼室窪
み内に於ける燃料の霧化、燃料と空気との混合状態が燃
焼速麿、燃焼効率に大きい影響を与え、一般に燃料が燃
料噴射ノズルより噴射されてから燃焼室窪みの壁面に到
達リーるまでの距離、所謂噴霧到達距離が長いことが燃
オ′々1の霧化、燃料と空気との混合状態を良くする上
で好ましく、燃料噴射ノズルより噴射された直後の燃料
は液柱状態であり、噴霧が形成されるためには最低の成
る噴霧到達距離が必要である。ビス1〜ンの燃焼室窪み
を大きくして燃料噴射ノズルの噴口に対向する燃焼室窪
みの壁面を燃料噴射ノズルから遠去【ノることにより前
記噴霧到達距離を艮くづることができるが、しかし、従
来の直接噴射式ディーげル機関に於ては、燃料噴射ノズ
ルの噴[]より噴射される燃料の噴射主流がピストンの
頂面に対しなJ角度が比較的大きくなるように燃料噴0
4ノズルがシリンダヘッドに取付けられ、燃料噴射ノズ
ルは燃焼室窪みの底部へ向けて燃料を噴口・J Jるよ
−うになっており、このため前記噴霧到達距離を大きく
Jるには燃焼室窪みを深くしなければならず、これに伴
いピストンのコンブレッジ」ンハイトが大きくなり、機
関全高が大きくなり、車載性が悪くなる。
In this type of direct injection type deep-pil engine, the atomization of the fuel in the combustion chamber cavity and the mixing state of the fuel and air have a large effect on the combustion speed and combustion efficiency, and generally the fuel is injected into the combustion chamber. It is preferable that the distance from when the fuel is injected from the nozzle to when it reaches the wall surface of the recess in the combustion chamber, the so-called spray arrival distance, is long in order to improve the atomization of the fuel 1 and the mixing state of the fuel and air. Immediately after being injected from the fuel injection nozzle, the fuel is in a liquid column state, and in order to form a spray, a minimum spray reach is required. By enlarging the recess of the combustion chamber with screws 1 to 1 and moving the wall surface of the recess of the combustion chamber facing the nozzle of the fuel injection nozzle further away from the fuel injection nozzle, it is possible to reduce the reach distance of the spray. However, in conventional direct injection diesel engines, fuel injection is performed so that the main stream of fuel injected from the fuel injection nozzle has a relatively large J angle with respect to the top surface of the piston. 0
4 nozzles are attached to the cylinder head, and the fuel injection nozzle directs the fuel toward the bottom of the recess in the combustion chamber. Therefore, in order to increase the spray reach distance, it is necessary to As a result, the combined height of the piston increases, increasing the overall height of the engine and making it difficult to mount it on a vehicle.

本発明はピストンのコンブレッジ」ンハイトをさほど大
きくすることなく十分な噴霧到達距離を得ることができ
、コンパクトで、しかも燃費、排気ガス性能が良好な直
接噴射式ディーゼル機関を提供することを目的としてい
る。
An object of the present invention is to provide a direct injection diesel engine that is compact and has good fuel efficiency and exhaust gas performance, which can provide a sufficient spray distance without significantly increasing the piston combination height. .

かかる目的は、本発明によれば、噴口が上死点にあるピ
ストンの頂部の燃焼窯窪みの周縁部の近傍に位置し旦前
記噴口より噴射される燃料の噴射主流がピストンの頂部
に対し20〜30度の角度をなす燃料噴射ノズルを有し
ている如ぎ直接IIJI射式デ(−ゼル機関によって達
成される。
According to the present invention, the jet nozzle is located near the periphery of the combustion furnace recess at the top of the piston at the top dead center, and once the main flow of fuel injected from the jet nozzle is 20 degrees to the top of the piston. This is accomplished by a direct injection diesel engine with fuel injection nozzles angled at ~30 degrees.

以下に添付の図を参照して本発明を実施例について詳細
に説明Jる。
DESCRIPTION OF THE PREFERRED EMBODIMENTS The present invention will now be described in detail by way of example embodiments with reference to the accompanying drawings.

第1図は本発明による直接噴射式ディーゼル機関の一つ
の実施例をその要部について示す縦断面図、第2図は第
1図に示された直接噴射式ディーゼル機関のピストンの
平面図である。
FIG. 1 is a longitudinal sectional view showing the main parts of one embodiment of a direct injection diesel engine according to the present invention, and FIG. 2 is a plan view of a piston of the direct injection diesel engine shown in FIG. 1. .

図に於て、1はシリンダブロックを、2はシリンダブロ
ック1のシリンダボア3の一端部を塞ぐべくシリンダブ
ロック1に取イ・1けられたシリンダヘッドを、4はシ
リンダボア3内に設(〕られたピストンを各々示してい
る。
In the figure, 1 is a cylinder block, 2 is a cylinder head installed in the cylinder block 1 to close one end of the cylinder bore 3 of the cylinder block 1, and 4 is a cylinder head installed in the cylinder bore 3. Each piston is shown separately.

ピストン4はその頂部に燃焼室窪み5を右している。燃
焼室窪み5は比較的浅く、楕円形に近いピストン軸線方
向断面形状と円形のピストン径方向断面形状とを有して
いる。ピストンボア3の直径が10011I111以下
の小型直接噴射式ディーげル槻関に於ては、一般に燃焼
室窪み5の直径はビス1〜ンボア直径をDどした場合、
0.37−(1,43D程度である。燃焼室窪み5の開
口部直径を(1とした場合、燃焼室窪みの深さはOo:
)・−0,7(1程度であって良い。
The piston 4 has a combustion chamber recess 5 at its top. The combustion chamber recess 5 is relatively shallow and has a nearly elliptical cross-sectional shape in the piston axial direction and a circular piston radial cross-sectional shape. In small direct injection type diesel engines with a piston bore 3 diameter of 10011I111 or less, the diameter of the combustion chamber recess 5 is generally as follows:
It is about 0.37-(1.43D. If the opening diameter of the combustion chamber recess 5 is (1), the depth of the combustion chamber recess is Oo:
)・-0,7 (may be about 1).

ピストン4の燃焼室n:み5の周縁部の一部には燃焼室
窪み5の一部を接線方向外方へ拡大すべく凹部6が設(
〕られている。シリンダヘッド2には燃料噴射ノズル7
が設けられており、該燃料噴口・1ノズルは単噴ロホー
ル型のものであり、その先端部に一つの噴口8をイiし
ている。燃料噴射ノズル7はこの噴口8が図示されてい
る如く」死点位置にあるピストン4の四部6に位置し、
し力(もその噴口8より噴射される燃料の噴霧主流が噴
口4の頂部に対しなす角度αが20〜30度の角度とな
るにうにシリンダヘッド2に取付Gtられて0る。
A recess 6 is provided in a part of the peripheral edge of the combustion chamber n: groove 5 of the piston 4 in order to expand a part of the combustion chamber recess 5 tangentially outward.
] The cylinder head 2 has a fuel injection nozzle 7
The fuel injection port/nozzle is of a single-injection hole type, and has one injection port 8 at its tip. The fuel injection nozzle 7 is located at the fourth part 6 of the piston 4, where the injection port 8 is at the dead center position, as shown in the figure.
It is attached to the cylinder head 2 so that the main stream of the fuel spray injected from the nozzle 8 makes an angle α of 20 to 30 degrees with respect to the top of the nozzle 4.

噴霧が得られる最低噴霧到達距離は燃料噴射ノズルの燃
料噴蘭圧、燃料噴射ノズル7の噴口の口径、噴口の形状
等により異るが、一般に(よ30〜40 mmであり、
この最低噴霧到達距離番よ上3本の如き小型直接噴射式
ディーゼル機関に於て(よ、上3!Isの如く噴口8が
上、死点位置にあるピストンのTU allの燃焼室窪
み5の周縁部の近傍に位置し旦噴口8より噴射される燃
料の噴射主流が噴口4の1頁面に対し20〜30 r(
Jtの角度をなすよう燃料噴射ノズル7がシリンダヘッ
ド2に取付けられることにより得られる。
The minimum spray reach distance at which a spray can be obtained varies depending on the fuel injection pressure of the fuel injection nozzle, the diameter of the nozzle of the fuel injection nozzle 7, the shape of the nozzle, etc., but is generally (30 to 40 mm).
In a small direct injection diesel engine such as the one shown in the top three (see above), the minimum spray reach is in the combustion chamber recess 5 of the piston TU all with the nozzle 8 at the top and the dead center position. The main flow of fuel injected from the nozzle 8 located near the peripheral edge is 20 to 30 r(
This is obtained by attaching the fuel injection nozzle 7 to the cylinder head 2 so as to form an angle of Jt.

燃料噴射ノズル7よりの燃料噴霧方向と、噴霧の時間当
りの噴射量と、燃焼室窪み5内1こ発生する渦流の強さ
は噴霧粒子が小さい良好な混合気を得るために重要な因
子であり、これらの因子を同時に適正に1゛ることが大
切である。噴霧h(渦流に沿って且有効にそのエネルギ
を利用でさる方向に燃料が噴射されることを狙うために
、燃料噴射ノズル7は、第2図にQく示されている如く
、燃焼室窪み5の中心より一方の側に偏った位置より燃
焼室窪み5内へ向(プて燃料を噴口・1′IJるように
なっている。
The direction of the fuel spray from the fuel injection nozzle 7, the amount of spray per unit time, and the strength of the vortex generated in the combustion chamber depression 5 are important factors in order to obtain a good air-fuel mixture with small spray particles. Therefore, it is important to properly adjust these factors to 1 at the same time. In order to inject the fuel in the direction along the vortex flow and effectively utilize its energy, the fuel injection nozzle 7 is inserted into the recess of the combustion chamber, as shown by Q in FIG. The fuel is directed into the combustion chamber recess 5 from a position biased to one side from the center of the recess 5 to the nozzle 1'IJ.

第3図は噴口より噴射される燃Hの噴射主流がピストン
の頂面に対しなす角度α、即ら噴射角αと燃費率との関
係を示している。第7図は前記噴射角αと排気ガス中の
黒煙濃度との関係を示している。この二つのグラフから
明らかイT如く、噴射角αが20〜30麿であれば燃費
率が良く、また排気ガス中の黒in度が低いが、噴射角
が301αを越えると燃費率が悪化し、また1ノ1気ガ
ス中の黒煙角度が増大“りる。
FIG. 3 shows the angle α formed by the main stream of fuel H injected from the nozzle with respect to the top surface of the piston, that is, the relationship between the injection angle α and the fuel consumption rate. FIG. 7 shows the relationship between the injection angle α and the black smoke concentration in the exhaust gas. It is clear from these two graphs that if the injection angle α is between 20 and 30 degrees, the fuel efficiency is good and the degree of blackness in the exhaust gas is low, but when the injection angle exceeds 301 α, the fuel efficiency deteriorates. Also, the black smoke angle in the 1-no-1 gas increases.

これは、噴射角αが30度以上になると、十分な噴霧到
達距離が得られず、燃Hの霧化及び燃料との空気どの混
合状態が悪くなり、燃焼効率及び燃焼速度が悪化−4る
からであると推測される。
This is because when the injection angle α exceeds 30 degrees, sufficient spray reach cannot be obtained, the atomization of fuel H and the mixing state of fuel and air deteriorate, and the combustion efficiency and combustion speed deteriorate. It is assumed that this is because

第5図及び第6図は各々本発明による直接噴剣式ディー
ピル機関の伯の実施例をその要部について示している。
FIGS. 5 and 6 each show the main parts of an embodiment of the direct injection type deep-pillar engine according to the present invention.

第5図に示された実施例に於ては、燃料噴射ノズル7が
ビントル型のものにより構成されている。ビントル型の
燃料噴射ノズルが用いられた場合には燃料噴射ノズル7
自身が前記噴射角に・応じてピストン頂面に対し比較的
小さい角度にて取付(プられなければならない。
In the embodiment shown in FIG. 5, the fuel injection nozzle 7 is of a bottle type. If a bottle-type fuel injection nozzle is used, the fuel injection nozzle 7
It must be mounted at a relatively small angle to the top surface of the piston depending on the injection angle.

第6図に示された実施例に於ては、燃焼室窪み5の形状
が変更されている。
In the embodiment shown in FIG. 6, the shape of the combustion chamber recess 5 has been changed.

何れの実施例に於ても噴射角が20〜30度とイrるよ
うに燃料噴射ノズルがシリンダヘッドに取付けられるこ
とにより最低必要噴霧到達距離が得られる。
In any of the embodiments, by attaching the fuel injection nozzle to the cylinder head so that the injection angle is between 20 and 30 degrees, the minimum required spray travel distance can be obtained.

以上に於ては本発明を特定の実施例について詳細に説明
したが、本発明はこれらに限定されるものではなく、本
発明の範囲内にて種々の実施例が可能であることは当業
者にとって明らかであろう。
Although the present invention has been described in detail above with reference to specific embodiments, it is understood by those skilled in the art that the present invention is not limited to these and that various embodiments are possible within the scope of the present invention. It would be obvious for

【図面の簡単な説明】[Brief explanation of the drawing]

第1図は本発明による直接噴射式ディーゼル機関の一つ
の実施例をその要部について示す縦断面図、第2図は第
1図に示された直接噴射式ディーゼル機関のピストンの
平面図、第3図は噴射角と燃費率との関係を示づグラフ
、第4図は噴射角と排気ガス中の黒煙濃度との関係を示
Jグラフ、第5図及び第6図は各々本発明による直接噴
射式ディーゼル機関の他の実施例をその要部について示
す縦断面図である。 1・・・シリンダブロック、2・・・シリンダヘッド。 3・・・シリンダボア、4・・・ピストン、5・・・燃
焼室窪み、6・・・凹部、7・・・燃料噴射ノズル、8
・・・噴口性 許 出 願 人  トヨタ自動車株式会
社代   埋   人  弁理士  明イーi 昌毅第
1図 第2図 第3図 第4図 噴射角;α(deg) (自 発) 手続補正書 昭和58年5月25 特許庁長官 若 杉 和 夫  殿 1、事件の表示 昭和571[特許願第196274月
2、発明の名称 直接噴射式ディーゼル機関 3、補正をする者 事件との関係  特許出願人 住 所  愛知県豊田市トヨタ町1番地名 称  (3
20)トヨタ自動中株式会社4、代理人 居 所  @104東京都中央区新川1丁目5番19号
茅場町長岡ビル3階 電話551−4176、補正にJ
:り増加覆る発明の数   0(1)特許請求の範囲を
以下の如く補正する。 r噴口が上死点にあるピストンの頂部の燃焼室穿口 面に対し20〜30度の角度をなす燃料噴射ノズルを有
する直接噴射式ディーゼル機関。j(2)明ll書第3
頁第10行の1主流が」と[ピストンJの間にr上死点
にある」を加入する。 (3)同第5頁第2行及び第12行の[噴口4Jをそれ
ぞれr を死点位置にあるピストン4」と訂正する。 〈4)同第6頁第7行〜第8行の「主流が」と「ピスト
ン」の間に「上死点位置にある」を加入する。
FIG. 1 is a longitudinal sectional view showing essential parts of an embodiment of a direct injection diesel engine according to the present invention, FIG. 2 is a plan view of a piston of the direct injection diesel engine shown in FIG. 1, and FIG. Figure 3 is a graph showing the relationship between injection angle and fuel consumption rate, Figure 4 is a J graph showing the relationship between injection angle and black smoke concentration in exhaust gas, and Figures 5 and 6 are each according to the present invention. FIG. 3 is a longitudinal cross-sectional view showing the main parts of another embodiment of the direct injection diesel engine. 1...Cylinder block, 2...Cylinder head. 3... Cylinder bore, 4... Piston, 5... Combustion chamber recess, 6... Recess, 7... Fuel injection nozzle, 8
・・・Nozzle property Applicant: Toyota Motor Corporation representative Patent attorney: Meiyi Chang Yi Figure 1 Figure 2 Figure 3 Figure 4 Injection angle; α (deg) (Voluntary) Procedural amendment 1982 May 25, 2015 Kazuo Wakasugi, Commissioner of the Japan Patent Office1, Indication of the case: Showa 571 [Patent Application No. 19627 April 2, Name of the invention: Direct injection diesel engine 3, Relationship with the amended person's case: Patent applicant's address 1 Toyota-cho, Toyota City, Aichi Prefecture Name (3)
20) Toyota Jidosha Co., Ltd. 4, agent address: 3rd floor, Kayabacho Nagaoka Building, 1-5-19 Shinkawa, Chuo-ku, Tokyo 104 Tel: 551-4176, J for amendments
:Increase in the number of covered inventions 0 (1) The scope of claims is amended as follows. A direct injection diesel engine having a fuel injection nozzle whose nozzle is at an angle of 20 to 30 degrees with respect to the perforation surface of the combustion chamber at the top of the piston at top dead center. j (2) Mei ll book 3
Add "1 main flow is at top dead center between piston J" and "R top dead center" on the 10th line of the page. (3) Correct the lines 2 and 12 of page 5 to read, ``The piston 4 with the nozzle 4J at its dead center position, respectively.''<4) Add ``located at top dead center'' between ``mainstream flow'' and ``piston'' on page 6, lines 7 to 8.

Claims (1)

【特許請求の範囲】[Claims] 噴口が上死点にある頂部の燃焼室窪みの周縁部の近傍に
位置し且前記噴口より噴射される燃料の噴射主流がピス
トンの頂面に対し20〜30度の角度をなす燃料噴射ノ
ズルを有づる直接噴射式ディーゼル機関。
A fuel injection nozzle in which the injection port is located near the periphery of the recess of the combustion chamber at the top at the top dead center, and the main stream of fuel injected from the injection port forms an angle of 20 to 30 degrees with respect to the top surface of the piston. A direct injection diesel engine.
JP57196274A 1982-11-08 1982-11-08 Diesel engine of direct injection type Pending JPS5985424A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP57196274A JPS5985424A (en) 1982-11-08 1982-11-08 Diesel engine of direct injection type

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP57196274A JPS5985424A (en) 1982-11-08 1982-11-08 Diesel engine of direct injection type

Publications (1)

Publication Number Publication Date
JPS5985424A true JPS5985424A (en) 1984-05-17

Family

ID=16355073

Family Applications (1)

Application Number Title Priority Date Filing Date
JP57196274A Pending JPS5985424A (en) 1982-11-08 1982-11-08 Diesel engine of direct injection type

Country Status (1)

Country Link
JP (1) JPS5985424A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS61132718A (en) * 1984-12-01 1986-06-20 Mitsubishi Heavy Ind Ltd Combustion unit of diesel engine
EP0237065A2 (en) * 1986-03-14 1987-09-16 Isuzu Motors Limited Combustion chamber for internal combustion engines

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS61132718A (en) * 1984-12-01 1986-06-20 Mitsubishi Heavy Ind Ltd Combustion unit of diesel engine
EP0237065A2 (en) * 1986-03-14 1987-09-16 Isuzu Motors Limited Combustion chamber for internal combustion engines

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