JP3212457B2 - Combustion chamber of subchamber internal combustion engine - Google Patents
Combustion chamber of subchamber internal combustion engineInfo
- Publication number
- JP3212457B2 JP3212457B2 JP25000094A JP25000094A JP3212457B2 JP 3212457 B2 JP3212457 B2 JP 3212457B2 JP 25000094 A JP25000094 A JP 25000094A JP 25000094 A JP25000094 A JP 25000094A JP 3212457 B2 JP3212457 B2 JP 3212457B2
- Authority
- JP
- Japan
- Prior art keywords
- chamber
- sub
- combustion chamber
- piston
- cylinder
- 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.)
- Expired - Fee Related
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B19/00—Engines characterised by precombustion chambers
- F02B19/08—Engines characterised by precombustion chambers the chamber being of air-swirl type
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T10/00—Road transport of goods or passengers
- Y02T10/10—Internal combustion engine [ICE] based vehicles
- Y02T10/12—Improving 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)
Description
【0001】[0001]
【産業上の利用分野】本発明は副室式内燃機関の燃焼室
に関する。BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a combustion chamber of a sub-chamber internal combustion engine.
【0002】[0002]
【従来の技術】従来の副室式内燃機関の燃焼室を図5〜
7によって説明する。図5は従来例の副室式内燃機関の
燃焼室の断面図、図6は従来例のピストンの上面図、図
7は図6の VII−VII 断面図である。図において、1は
主燃焼室でピストン7の上面、シリンダ8、シリンダヘ
ッド4の下面でかこまれた空間である。2は副燃焼室で
シリンダヘッド4にシリンダ中心線A−Aから離れ片よ
って凹設され、副室口金9にあけられた副室噴口3を介
して、主燃焼室1と連通している。副燃焼室2の形状は
上部が半球形、下部は円錐台形で上部に燃料噴射弁5が
設置され、又機関の始動時に副燃焼室2内を予熱するグ
ロープラグ6が必要に応じ設置される。主燃焼室1の下
面をなすピストン7の上面にピストンキャビティが設け
られている。前記ピストンキャビティの形状は深さが副
室噴口3の出口附近で最も深く形成されシリンダ中心に
向って次第に遠浅となりやがてピストン頂面10に一致
しその巾は一定である。2. Description of the Related Art A combustion chamber of a conventional sub-chamber internal combustion engine is shown in FIGS.
7 will be described. 5 is a sectional view of a combustion chamber of a conventional sub-chamber internal combustion engine, FIG. 6 is a top view of a conventional piston, and FIG. 7 is a sectional view taken along line VII-VII of FIG. In the figure, reference numeral 1 denotes a main combustion chamber, which is a space surrounded by the upper surface of the piston 7, the cylinder 8, and the lower surface of the cylinder head 4. Reference numeral 2 denotes a sub-combustion chamber, which is recessed in the cylinder head 4 at a distance from the cylinder center line A-A and communicates with the main combustion chamber 1 via a sub-chamber injection hole 3 opened in a sub-chamber base 9. The shape of the sub-combustion chamber 2 is hemispherical at the top and frusto-conical at the bottom, with a fuel injection valve 5 installed at the top, and a glow plug 6 for preheating the inside of the sub-combustion chamber 2 when the engine is started. . A piston cavity is provided on an upper surface of a piston 7 which is a lower surface of the main combustion chamber 1. The shape of the piston cavity is formed deepest near the outlet of the sub-chamber injection port 3 and gradually becomes shallower toward the center of the cylinder, and eventually coincides with the piston top surface 10 and its width is constant.
【0003】前記従来例の作用を説明する。機関運転
時、圧縮行程において、ピストン7により主燃焼室1内
の空気が圧縮され、副室噴口3を通って副燃焼室2へ流
入し渦流5を生成する。渦流5の速度はピストン7が上
死点近傍にくると増大する。渦流5の方向に沿って燃料
噴射弁5から燃料を噴射すると、前記燃料は、渦流5と
共に副室2内を旋回しながら空気との混合気形成が行わ
れ、グロープラグ6付近から着火し始めて燃焼する。副
燃焼室2内の燃焼ガス及び未燃ガスは主燃焼室1と副燃
焼室との圧力差(主燃焼室圧力<副燃焼室圧力)とピス
トンの下降運動によって副室噴口3を通って主燃焼室1
へ噴出する。前記噴出ガスはピストン7に仕事をすると
同時に主燃焼室1内の空気と混合し合って更に拡散燃焼
が進む。The operation of the conventional example will be described. During operation of the engine, in the compression stroke, the air in the main combustion chamber 1 is compressed by the piston 7, flows into the sub-combustion chamber 2 through the sub-chamber injection port 3, and generates a vortex 5. The velocity of the vortex 5 increases as the piston 7 approaches the top dead center. When fuel is injected from the fuel injection valve 5 in the direction of the swirl 5, the fuel forms an air-fuel mixture while swirling in the sub-chamber 2 together with the swirl 5 and starts igniting from the vicinity of the glow plug 6. Burn. The combustion gas and unburned gas in the sub-combustion chamber 2 pass through the sub-chamber injection port 3 due to the pressure difference between the main combustion chamber 1 and the sub-combustion chamber (main combustion chamber pressure <sub-combustion chamber pressure) and the downward movement of the piston. Combustion chamber 1
Squirt to The ejected gas works on the piston 7 and at the same time mixes with the air in the main combustion chamber 1 to further diffuse combustion.
【0004】[0004]
【発明が解決しようとする課題】副室式内燃機関は通常
副室噴口面積を拡大して噴口絞り損失或は熱損失を低減
しながら性能の向上と未燃排気ガスの低減を図ってい
る。しかし副室噴口を拡げすぎると膨張行程での副燃焼
室から主燃焼室への噴流エネルギ低下を招き易く、主燃
焼室内の混合気形成が不足となり、燃焼が緩慢となり性
能が悪化する。In the sub-chamber internal combustion engine, the performance of the sub-chamber internal combustion engine is usually increased while reducing the throttling loss or heat loss of the sub-chamber to reduce the unburned exhaust gas. However, if the sub chamber injection port is too wide, the energy of the jet flow from the sub combustion chamber to the main combustion chamber during the expansion stroke tends to decrease, and the mixture in the main combustion chamber is insufficiently formed, so that the combustion becomes slow and the performance deteriorates.
【0005】本発明の目的は、副室噴口から主燃焼室へ
高速で噴出する未燃既燃ガスと主燃焼室内新気との混合
促進が図られるとともに、主燃焼室全体の空気利用率が
向上し、従って燃焼期間が短縮され等容度燃焼効率が向
上して、中、後期の拡散燃焼が促進される副室式内燃機
関の燃焼室を提供するにある。[0005] It is an object of the present invention to promote the mixing of unburned burned gas spouted from the sub chamber injection port into the main combustion chamber at high speed and fresh air in the main combustion chamber, and to reduce the air utilization rate of the entire main combustion chamber. An object of the present invention is to provide a combustion chamber of a sub-chamber internal combustion engine in which the combustion period is shortened, the isovolume combustion efficiency is improved, and the medium and late diffusion combustion is promoted.
【0006】[0006]
【課題を解決するための手段】本発明は副室式内燃機関
の燃焼室において、主燃焼室のピストンキャビティの形
状を、その深さが副室噴口出口付近からシリンダ中心方
向に向って遠浅になり、かつその巾が副室噴口出口附近
からシリンダ中心にかけて緩やかに狭くなりそれより先
は逆に緩やかに拡大して居り、かつ少なくとも前記ピス
トンキャビティの巾が狭くなりつつある区間の側壁の両
側を前記ピストンキャビティの底が廣くなる方向へ傾斜
させて構成したことを特徴としている。According to the present invention, in the combustion chamber of a sub-chamber internal combustion engine, the shape of the piston cavity of the main combustion chamber is made shallow from near the sub chamber injection port outlet toward the cylinder center. It becomes, and both of the side walls of the width is moderately narrows it earlier than toward the cylinder center from the auxiliary chamber injection port exit vicinity sediment expanding moderately Conversely, and is becoming narrow least width of said piston cavity section
Bottom side the piston cavity is characterized by being configured to be tilted to the direction in which Hiroshiku.
【0007】[0007]
【作用】副室噴口から主燃焼室へ噴出する未燃、既燃ガ
スは主にピストンキャビティ内をシリンダ中心部を通り
シリンダ壁面の方へ進んで行く。その途中周辺へ拡散し
ながら進むため、ペネトレーションが次第に低下して行
く。ピストンキャビティの側壁を内側へ傾斜させ且ピス
トンキャビティ巾を狭くしたため、周辺への拡散が減
り、ペネトレーションの低下が少なくなり周辺の空気を
巻き込みながらシリンダ壁へ向って進んで行き、未燃既
燃ガスと空気との混合が促進される。The unburned and burned gas ejected from the sub chamber injection port into the main combustion chamber travels mainly through the center of the cylinder in the piston cavity toward the cylinder wall. Penetration gradually decreases as it progresses while spreading to the surrounding area. Since the side wall of the piston cavity is inclined inward and the width of the piston cavity is narrowed, diffusion to the surroundings is reduced, and reduction in penetration is reduced. Mixing with air is promoted.
【0008】[0008]
【実施例】本発明に係る第1実施例を図1〜5によって
説明する。図5は本発明に係る第1実施例の副室式内燃
機関の燃焼室の断面図、図1は本発明に係る第1実施例
のピストンの上面図、図2は図1のII−II断面図、図3
は図1の III−III 断面図、図4は図1のIV−IV断面図
である。図においてピストン以外は従来のものと同じで
ある。1は主燃焼室でシリンダ8、ピストン7の上面、
シリンダヘッド4の下面でかこまれた空間である。2は
副燃焼室でシリンダヘッド4に凹設され上部は半球形下
部は円錐台形で副室噴口3により主燃焼室1と連通して
いる。9は副室口金で副燃焼室2の下部を形成し副室噴
口3が設けられている。5は燃焼噴射弁、6はグロープ
ラグで何れも副燃焼室2に設けられている。DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS A first embodiment according to the present invention will be described with reference to FIGS. FIG. 5 is a sectional view of a combustion chamber of a sub-chamber internal combustion engine according to a first embodiment of the present invention, FIG. 1 is a top view of a piston according to the first embodiment of the present invention, and FIG. Sectional view, FIG. 3
1 is a sectional view taken along line III-III of FIG. 1, and FIG. 4 is a sectional view taken along line IV-IV of FIG. In the drawing, the parts other than the piston are the same as the conventional one. 1 is a main combustion chamber, an upper surface of a cylinder 8 and a piston 7,
This is a space surrounded by the lower surface of the cylinder head 4. Reference numeral 2 denotes a sub-combustion chamber, which is recessed in the cylinder head 4 and has a hemispherical upper part and a truncated conical lower part, and is communicated with the main combustion chamber 1 by a sub-chamber injection port 3. Reference numeral 9 denotes a sub-chamber base, which forms the lower part of the sub-combustion chamber 2 and is provided with a sub-chamber injection port 3. Reference numeral 5 denotes a combustion injection valve, and reference numeral 6 denotes a glow plug, all provided in the sub-combustion chamber 2.
【0009】ピストン7の上面にピストンキャビティが
設けられて居り、その深さは副室噴口3の下の部分で最
も深くシリンダ中心方向に向って遠浅になったくさび形
をしている。主燃焼室1へ噴出するガスの進行方向に向
けて前記ピストンキャビティの巾をシリンダ中心線A−
A付近までは緩やかに狭め、その後は逆に緩やかに拡大
する。さらに前記ピストンキャビティの側壁は副室噴口
開口部付近ではピストン頂面10に垂直(θ=0)と
し、ピストンキャビティの巾が狭くなりつつあるところ
以後ではシリンダ中心方向への傾斜角θが0<θ≦60
°としている。A piston cavity is provided on the upper surface of the piston 7 and has a wedge shape with a depth that is deepest and shallow toward the center of the cylinder below the sub chamber injection port 3. The width of the piston cavity is adjusted in the direction of travel of the gas injected into the main combustion chamber 1 by the cylinder center line A-.
It gradually narrows to around A, and then gradually expands. Further, the side wall of the piston cavity is perpendicular to the piston top surface 10 (θ = 0) in the vicinity of the opening of the sub-chamber injection port. θ ≦ 60
°.
【0010】前記第1実施例の作用を説明する。機関運
転時圧縮行程で、圧縮された空気は主燃焼室1から副室
噴口3を通って副燃焼室2へ流入し渦流5を生成する。
渦流Sの流れ方向に沿って燃料噴射弁5から燃料が噴射
されグロープラグ6付近で着火する。The operation of the first embodiment will be described. In the compression stroke during operation of the engine, the compressed air flows from the main combustion chamber 1 through the sub chamber injection port 3 into the sub combustion chamber 2 to generate a vortex 5.
Fuel is injected from the fuel injection valve 5 along the flow direction of the vortex S, and the fuel is ignited near the glow plug 6.
【0011】副燃焼室2で着火燃焼した既燃ガス、未燃
ガスは副室噴口3を通って主燃焼室1へ高速で噴出す
る。該噴流ガスは前記ピストンキャビティ最深部に衝突
しピストンキャビティ底面に沿ってシリンダヘッド4下
面とピストン頂面10とに囲まれた極小間隙を進みシリ
ンダ8壁面に達する。その際同時に主燃焼室1内の空気
と混合しながら拡散燃焼が行われ、その圧力によってピ
ストン7を押し下げ仕事をする。Burned gas and unburned gas ignited and burned in the sub-combustion chamber 2 are spouted into the main combustion chamber 1 at high speed through the sub-chamber injection port 3. The jet gas collides with the deepest part of the piston cavity, travels along the bottom surface of the piston cavity, through a very small gap surrounded by the lower surface of the cylinder head 4 and the top surface 10 of the piston, and reaches the wall surface of the cylinder 8. At the same time, diffusion combustion is performed while mixing with air in the main combustion chamber 1, and the pressure pushes down the piston 7 to perform work.
【0012】しかし従来副室噴口絞り損失低減による性
能向上を図っているため、副室噴口3がある程度拡げら
れている。このため副室噴口3を通って主燃焼室1へ高
速で噴出したガスの貫徹力も、シリンダ中心線A−Aか
らシリンダ8壁にかけてはかなり低下する。そこで高速
で噴出したガスの進行方向においてピストンキャビティ
の巾を緩やかに絞り後拡げ、更にピストンキャビティの
側壁角θを0<θ≦60°の範囲内でガスの進行方向に
対して内側へ傾斜させて、噴流ガスのピストンキャビテ
ィ外へのはみ出しを防いで拘束する。However, in order to improve the performance by reducing the throttle loss of the sub chamber injection port, the sub chamber injection port 3 is expanded to some extent. For this reason, the penetration force of the gas injected at high speed through the sub chamber injection port 3 to the main combustion chamber 1 is also considerably reduced from the cylinder center line AA to the cylinder 8 wall. Therefore, the width of the piston cavity is gently reduced and then expanded in the traveling direction of the gas ejected at a high speed, and the side wall angle θ of the piston cavity is inclined inward with respect to the traveling direction of the gas within the range of 0 <θ ≦ 60 °. Thus, the jet gas is prevented from protruding out of the piston cavity and is restrained.
【0013】噴流ガスの流れを拘束することによりシリ
ンダ中心付近からシリンダ8壁までの噴流ガス分散とペ
ネトレーションの減少が抑制される。この作用はピスト
ン7が上死点のとき特に大きい。前記のように主燃焼室
1へ噴出したガスは運動エネルギの低下及び貫徹力の低
下を少くしつつ進行するため、ピストンキャビティ周辺
の空気導入やシリンダ8周壁の空気を含めた主燃焼室1
内の混合気形成が盛んとなり、主燃焼室1全体の空気利
用率が向上する。尚ピストンキャビティ巾の絞り具合は
性能を損ねない適正な絞りとする必要がある。By restricting the flow of the jet gas, the dispersion of the jet gas from the vicinity of the cylinder center to the wall of the cylinder 8 and a decrease in penetration are suppressed. This effect is particularly large when the piston 7 is at the top dead center. As described above, the gas ejected into the main combustion chamber 1 travels while decreasing the kinetic energy and the penetration force, so that the main combustion chamber 1 including the air introduction around the piston cavity and the air on the peripheral wall of the cylinder 8 is included.
The air-fuel mixture in the inside becomes active, and the air utilization rate of the entire main combustion chamber 1 is improved. In addition, it is necessary to set the degree of reduction of the piston cavity width to an appropriate degree which does not impair the performance.
【0014】[0014]
【発明の効果】副室噴口から主燃焼室へ高速で噴出する
未燃、既燃ガスと、主燃焼室内の新気との混合が早期に
図られると共に、主燃焼室の空気利用率が向上する。従
って燃焼期間が短縮され、等容度燃焼効率が向上して主
燃焼室内の中、後期の拡散燃焼が促進される。即ち機関
の始動性、出力が向上すると共に吐煙、未燃炭化水素等
の排ガス低減が可能となる。According to the present invention, mixing of unburned and burned gas spouted from the sub chamber injection port into the main combustion chamber at high speed and fresh air in the main combustion chamber is achieved at an early stage, and the air utilization rate of the main combustion chamber is improved. I do. Therefore, the combustion period is shortened, the isovolume combustion efficiency is improved, and the later-stage diffusion combustion in the main combustion chamber is promoted. In other words, the startability and output of the engine are improved, and the emission of smoke, unburned hydrocarbons and the like can be reduced.
【図1】本発明に係る第1実施例のピストンの上面図。FIG. 1 is a top view of a piston according to a first embodiment of the present invention.
【図2】図1におけるII−II断面図。FIG. 2 is a sectional view taken along the line II-II in FIG.
【図3】図1における III−III 断面図。FIG. 3 is a sectional view taken along the line III-III in FIG. 1;
【図4】図1におけるIV−IV断面図。FIG. 4 is a sectional view taken along line IV-IV in FIG. 1;
【図5】本発明に係る第1実施例及び従来例の副室式内
燃機関の燃焼室の断面図。FIG. 5 is a cross-sectional view of a combustion chamber of a sub-chamber internal combustion engine according to a first embodiment of the present invention and a conventional example.
【図6】従来例のピストンの上面図。FIG. 6 is a top view of a conventional piston.
【図7】図6における VII−VII 断面図。FIG. 7 is a sectional view taken along the line VII-VII in FIG. 6;
1…主燃焼室、2…副燃焼室、3…副室噴口、4…シリ
ンダヘッド、5…燃料噴射弁、6…グロープラグ、7…
ピストン、8…シリンダ、9…副室口金、10…ピスト
ン頂面、A−A…シリンダ中心線、θ…ピストンキャビ
ティの側壁角。DESCRIPTION OF SYMBOLS 1 ... Main combustion chamber, 2 ... Sub combustion chamber, 3 ... Sub chamber injection port, 4 ... Cylinder head, 5 ... Fuel injection valve, 6 ... Glow plug, 7 ...
Piston, 8: Cylinder, 9: Sub chamber base, 10: Piston top surface, AA: Cylinder center line, θ: Side wall angle of piston cavity.
───────────────────────────────────────────────────── フロントページの続き (56)参考文献 特開 昭58−126421(JP,A) 特開 平6−336928(JP,A) 特開 平6−159134(JP,A) 特開 平5−118220(JP,A) 特開 平6−264744(JP,A) 実開 昭54−178806(JP,U) 実開 昭62−18329(JP,U) 特許3080816(JP,B2) (58)調査した分野(Int.Cl.7,DB名) F02B 19/00 - 19/18 ────────────────────────────────────────────────── ─── Continuation of the front page (56) References JP-A-58-126421 (JP, A) JP-A-6-336928 (JP, A) JP-A-6-159134 (JP, A) 118220 (JP, A) JP-A-6-264744 (JP, A) JP-A 54-178806 (JP, U) JP-A 62-18329 (JP, U) Patent 3080816 (JP, B2) (58) Field (Int.Cl. 7 , DB name) F02B 19/00-19/18
Claims (1)
焼室のピストンキャビティの形状を、その深さが副室噴
口出口付近からシリンダ中心方向に向って遠浅になり、
かつその巾が副室噴口出口附近からシリンダ中心にかけ
て緩やかに狭くなりそれより先は逆に緩やかに拡大して
居り、かつ少なくとも前記ピストンキャビティの巾が狭
くなりつつある区間の側壁の両側を前記ピストンキャビ
ティの底が廣くなる方向へ傾斜させて構成したことを特
徴とする副室式内燃機関の燃焼室。In a combustion chamber of a sub-chamber internal combustion engine, the shape of a piston cavity of a main combustion chamber becomes shallower from a vicinity of an outlet of a sub-chamber toward a center of a cylinder from an outlet of a sub-chamber.
And moderately narrows it earlier than its width is toward the cylinder center from the auxiliary chamber injection port exit vicinity sediment expanding moderately Conversely, and said both side walls of at least the piston cavity width is becoming narrower interval piston combustion chamber of the subchamber type internal combustion engine in which the bottom of the cavity is characterized by being configured to be tilted to a direction that Hiroshiku.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP25000094A JP3212457B2 (en) | 1994-09-19 | 1994-09-19 | Combustion chamber of subchamber internal combustion engine |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
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JP25000094A JP3212457B2 (en) | 1994-09-19 | 1994-09-19 | Combustion chamber of subchamber internal combustion engine |
Publications (2)
Publication Number | Publication Date |
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JPH0893475A JPH0893475A (en) | 1996-04-09 |
JP3212457B2 true JP3212457B2 (en) | 2001-09-25 |
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JP25000094A Expired - Fee Related JP3212457B2 (en) | 1994-09-19 | 1994-09-19 | Combustion chamber of subchamber internal combustion engine |
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JP2024027998A (en) * | 2022-08-19 | 2024-03-01 | 三菱重工エンジン&ターボチャージャ株式会社 | Auxiliary chamber type engine |
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JPH0893475A (en) | 1996-04-09 |
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